RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-1
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Year of Launch 2000
Name
[Launcher]
Fragments
D
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
DSCS-3B 6
(USA 148)
[Atlas-2A]
2000-01 A
[26052]
CC-LC36A
2000 Jan 21.05
> million years
Box + 2 panels 1.93 x 1.96 No elements available; orbit from amateur observations.
1175
x 2.06
2009 Jun 28.83
0.71
1435.98 42163 35732 35836
11.62 span
0.001
342
Atlas-2A 2nd stage
(Centaur AC-138)
2000-01 B
[26053]
2000 Jan 21.05
Cylinder
1815
10.1 long
3.05 dia
IABS
2000-01 C
[26054]
2000 Jan 21.05
Cylindrical
272
2.9 dia
0.69 high
Galaxy 10R
[Ariane-42L]
(V-126)
2000-02 A
[26056]
KOU-ELA2
2000 Jan 25.05
> million years
Ariane 3rd stage
(H-10-3) + VEB
2000-02 B
[26057]
Feng Huo 1
(Zhong Xing-22)
(Chinasat 22)
[CZ-3A-4(60)]
2000 Jan 21.13
2004 Jun 3.10
25.60
26.12
Box + 2 panels 6.0 x 3.4
3651
x 2.28
26.2 span
2000
2000
2000
2000
2000
2000
2000
2005
25.20
27.72
29.19
31.21
1.02
1.99
6.62
17.47
6.86
6.97
3.69
0.58
0.19
0.11
0.10
0.01
2000 Jan 25.05
1543 days
2004 Apr 16
Cylinder
1780
2000 Jan 24.88
2004 Apr 9.68
6.24
7.20
2000-03 A
[26058]
XI-LC2
2000 Jan 25.70
> million years
Box + 2 panels 2.2 x 1.72
2300
x 2.0
18.1 span
2000
2000
2000
2000
2005
25.98
26.50
4.00
8.68
15.59
25.00
24.91
0.75
0.75
0.05
CZ-3A 3rd stage
(H-18)
2000-03 B
[26059]
2000 Jan 25.70
424 days
2001 Mar 24
Cylinder
3500
8.84 long
3 dia
2000 Jan 25.98
2001 Mar 23.35
25.04
24.57
Jawsat *
2000-04 A
[26061]
VDB-CLF
2000 Jan 27.13
Payload frame
191.4
0.89x0.89
x1.07
2000 Jan 27.31
2003 Oct 30.41
100.23
100.19
11.7 long
2.6 dia
Jan
Jan
Jan
Jan
Feb
Feb
Feb
Dec
Jan
Jan
Feb
Feb
Dec
622.62 24153
523.05 21505
257
235
35292
30016
0.725
0.692
176
258
266
525
6407
21496
34231
35785
35781
35777
33249
35825
35816
35799
35783
35810
35792
35795
0.713
0.719
0.535
0.204
0.019
0.0003
0.0001
0.0002
175
178
177
188
191
3
12
231
262
123
33428
1674
0.714
0.107
176
40
194
493
35779
35782
35775
41888
42266
35859
35789
35797
0.760
0.752
0.0009
0.00009
0.0003
180
180
266
285
34
753.90 27439
88.25 6566
191
94
41930
281
0.761
0.014
180
288
100.42 7157
100.13 7143
749
740
808
789
0.004
0.003
183
282
583.70
638.17
756.02
1087.27
1396.48
1436.68
1436.12
1436.08
23136
24554
27491
35026
41386
42176
42165
42165
587.02 23224
102.97 7277
753.10
767.08
1437.78
1436.07
1436.08
27420
27758
42198
42164
42164
[Minotaur 1OSP/SLV-1]
2000-04 continued on next page
*
Joint Air Force Academy / Weber State Satellite consists of a secondary payload adapter on which 4 secondary satellites were mounted and a fixed
experiment. All 4 secondary payloads were deployed successfully. The fixed experiment is PEST (Plasma Experiment Satellite Test).
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-2
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
D
*
$
%
&
^
#
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
OSCE *
2000-04 B
[26062]
2000 Jan 27.13
403 days
2001 Mar 5
Hexagonal
Cylinder +
Inflated
sphere
21 + 1.7
0.48 long
1.41 dia
3.6 dia
2000 Jan 27.24
2001 Mar 5.24
100.22
100.17
100.37 7155
88.88 6598
750
199
802
239
0.004
0.003
191
170
OPAL $
(OPAL-OSCAR 38)
2000-04 C
[26063]
2000 Jan 27.13
Hexagonal
Cylinder
25.5
0.235 high
0.42 dia
2000 Jan 27.24
2005 Dec 16.85
100.22
100.19
100.38 7155
100.28 7151
749
746
803
798
0.004
0.004
193
261
FalconSat 1 %
2000-04 D
[26064]
2000 Jan 27.13
Cube
52
0.445x0.445 2000 Jan 27.24
x0.432
2005 Dec 18.17
100.24
100.19
100.38 7156
100.32 7152
751
747
803
801
0.004
0.004
190
261
Asusat &
2000-04 E
[26065]
2000 Jan 27.13
Cylinder
5.9
0.245 high
0.32 dia
2000 Jan 27.24
2005 Dec 18.17
100.23
100.19
100.47 7159
100.28 7151
752
746
809
798
0.004
0.004
176
258
Minotaur 4th stage
2000-04 F
[26066]
2000 Jan 27.13
Cone-cyl
176
2.08 long
0.97 dia
2000 Jan 27.24
2005 Dec 17.67
100.23
100.19
100.35 7154
100.23 7148
750
745
800
793
0.003
0.003
187
251
MEMS 1 & 2 ^
(Picosat 1+2)
2000-04 H
[26080]
2000 Jan 27.13
2 boxes
2x 0.275
0.10x0.075 Ejected from OPAL 2000 Feb 7.15; connected by 32 m tether
0.025 thick 2000 Feb 8.03
100.23
100.33 7153
749
800
2005 Dec 16.28
100.19
100.00 7137
735
781
0.004
0.003
161
237
Picosat 3 #
(Stensat?)
2000-04 J
[26091]
2000 Jan 27.13
Box
0.235
0.10x0.075 Ejected from OPAL 2000 Feb 10
0.025 thick 2000 Feb 14.17
100.22
100.40 7156
2005 Dec 16.75
100.19
99.80 7128
751
727
804
771
0.004
0.003
139
217
Picosat 4 #
(JAK?)
2000-04 K
[26092]
2000 Jan 27.13
Box
0.5
0.10x0.075 Ejected from OPAL 2000 Feb 10
0.025 thick 2000 Feb 14.17
100.21
100.38 7155
2005 Dec 17.99
100.18
100.00 7137
749
734
804
783
0.004
0.003
141
230
Optical Calibration Sphere Experiment ejected from Jawsat stack. Shortly after orbit insertion of OSCE the balloon was deployed and inflated.
Orbiting Picosat Automated Launcher that ejected 6 picosats, see 2000 04 H-M
Build by cadets of the US Air Force Academy, Colorado Springs, CO, ejected from JAWSAT. Failed after 1 month due to problems with the power supply.
Arizona State University
Micro Electro Mechanical Systems (Picosat 1.0). The mission lasted till 2000 Feb 9 when battery power decayed.
Picosats 3 to 6 ID not certain due to non-communications with the sats.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-3
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
Box
0.611
Box
0.611
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Picosat 5 #
(Thelma?)
2000-04 L
[26093]
2000 Jan 27.13
Picosat 6 #
(Louise?)
2000-04 M
[26094]
2000 Jan 27.13
Fragment
2000-04 G
[26079]
2000-04 N
[26097]
2001 Feb 07
D
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
0.20x0.075 Ejected from OPAL 2000 Feb 12
0.025 thick 2000 Feb 15.22
100.22
100.40 7156
2005 Dec 18.11
100.18
99.70 7123
749
721
805
768
0.004
0.003
138
204
0.20x0.075 Ejected from OPAL 2000 Feb 12
0.025 thick 2000 Feb 15.22
100.23
100.40 7156
2005 Dec 18.24
100.18
100.05 7139
752
735
802
786
0.003
0.004
140
235
377 days
Date of
orbital
determination
2000
2005
2000
2001
Feb
Dec
Feb
Feb
6.22
18.26
19.12
7.31
Orbital
Inclination
(deg)
Nodal
period
(min)
100.23
100.19
100.22
100.13
100.40
100.00
100.38
88.68
7156
7137
7155
6588
752
734
748
196
804
783
805
223
0.004
0.003
0.004
0.002
161
232
121
189
6554
6601
6612
6688
6689
6702
6730
6708
-2138
209
232
298
302
319
348
327
2489
235
236
320
320
328
354
333
0.353
0.002
0.0003
0.002
0.001
0.0006
0.0004
0.0004
88
305
179
304
315
164
285
156
183
142
204
149
0.002
0.0006
42
62
D
Progress-M1 1 *
[Soyuz-11A511U
A15000-669]
2000-05 A
[26067]
BAI-LC1
2000 Feb 1.28
85.53 days
2000 Apr 26.81
Cyl+2 panels+ 7.9 long
2000 Feb 1.34
beehive+sphere 2.72 maxdia 2000 Feb 1.45
7250
2000 Feb 1.65
2000 Feb 4.07
2000 Feb 5.84
2000 Feb 7.91
2000 Feb 12.10
2000 Apr 26.11
52.84
51.63
51.65
51.65
51.65
51.65
51.65
51.65
88.00
88.95
89.18
90.72
90.75
91.00
91.57
91.13
D
Soyuz-U 3rd stage
(Block I)
2000-05 B
[26068]
2000 Feb 1.28
1.65 day
2000 Feb 2.93
Cylinder
2300
51.63
51.62
88.37 6573
87.40 6524
#
*
Picosats 3 to 6 ID not certain due to non-communications with the sats.
Progress-M1 1 docked with MIR (Kvant 1 port) 2000 Feb 3.33; raised MIR’s orbit; undocked 2000 Apr 26.69 and de-orbited.
2016 - Version 1.15
8.1 long
2.66 dia
2000 Feb 1.64
2000 Feb 2.80
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-4
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Cosmos 2369
2000-06 A
[Zenit-2 45025801] [26069]
BAI-LC45/1
2000 Feb 3.39
Cyl + 6 panels
3250
Zenit-2 2nd stage
2000-06 B
[26070]
2000 Feb 3.39
Cylinder
8300
Zenit-2 separation 2000-06 C
Motor cap
[26073]
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Date of
orbital
determination
Orbital
Inclination
(deg)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
2000 Feb 3.46
2000 Feb 4.17
2005 Dec 18.50
71.01
71.01
70.99
101.90 7227
101.93 7229
101.90 7227
845
848
840
853
853
857
0.0006
0.0004
0.001
12
12
121
2000 Feb 3.46
2005 Dec 16.92
71.01
71.00
101.77 7221
101.75 7220
836
828
849
855
0.0009
0.002
292
260
2000 Feb 3.39
2000 Feb 6.23
2005 Dec 16.77
71.09
71.08
104.90 7369
104.85 7366
847
841
1133
1133
0.019
0.020
62
239
Zenit-2 separation 2000-06 D
Motor cap
[26074]
2000 Feb 3.39
2000 Feb 6.17
2005 Dec 17.84
70.97
70.96
105.25 7384
105.18 7382
848
844
1164
1163
0.021
0.022
82
318
Zenit-2 separation 2000-06 E
Motor cap
[26075]
2000 Feb 3.39
2000 Feb 6.23
2005 Dec 17.76
71.08
71.06
104.80 7364
104.73 7360
845
839
1125
1124
0.019
0.019
88
259
Zenit-2 separation 2000-06 G
Motor cap
[26077]
2000 Feb 3.39
2000 Feb 6.16
2005 Dec 16.69
70.97
70.97
105.02 7374
104.95 7371
843
839
1148
1145
0.021
0.021
58
279
Fragments
2000-06 F
2000-06 H
[R26076] Re-assigned to 1999- 40 E
[R26078] Re-assigned to 1999- 40 F
2000 Feb 6.14 71.08 101.70 7218
2000 Feb 6.15 71.01 102.00 7232
786
750
893
956
0.007
0.014
Hispasat 1C
[Atlas-2AS]
2000-07 A
[26071]
CC-LC36B
2000 Feb 3.98
> million years
Box + 2 panels 1.8 x 2.3
3112
x 2.3
26.3 span
2000
2000
2000
2005
3.71
15.68
27.15
12.09
18.72
0.10
0.03
0.10
220
35770
35771
35767
45783
35800
35802
35807
0.778
0.0004
0.0004
0.0005
179
47
40
234
Atlas-2AS 2nd stage 2000-07 B
(Centaur AC-158)
[26072]
2000 Feb 3.98
Cylinder
1815
2000 Feb 3.71
2005 Dec 16.37
18.72
18.09
830.47 29267
257.97 13424
200
295
45577
13796
0.775
0.503
180
312
Globalstar 63
[Delta-2 (7420)
10C #276]
2000 Feb 8.89
Trapezoidal
0.60 x 1.50
box + 2 panels x 1.60
450 full
12 span
400 empty
2000
2001
2001
2001
2005
52.00
52.01
52.00
52.00
52.00
103.47
111.43
114.00
114.07
114.07
914
1290
1408
1412
1411
931
1294
1412
1414
1415
0.001
0.0002
0.0002
0.0001
0.0003
260
338
110
136
114
2000-08 A
[26081]
CC-LC17B
Size
(m)
Lifetime
10.41 long
3.9 dia
10.1 long
3.05 dia
2000-08 comtinued on next page
2016 - Version 1.15
Feb
Feb
Mar
Dec
Feb
Nov
Dec
Dec
Dec
8.96
28.15
3.47
10.91
18.46
Nodal
period
(min)
835.28
1436.02
1436.10
1436.13
29380
42163
42165
42166
7301
7671
7789
7792
7792
155
357
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-5
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Globalstar 62
2000-08 B
[26082]
2000 Feb 8.89
Trapezoidal
0.60 x 1.50
box + 2 panels x 1.60
450 full
12 span
400 empty
2000
2000
2000
2000
2000
2000
2000
2000
2005
Feb
Feb
Feb
Mar
Mar
Mar
Mar
Mar
Dec
9.03
26.12
29.78
1.96
3.67
3.70
5.04
10.03
18.34
52.00
52.01
52.01
51.70
51.70
52.02
52.00
52.00
52.01
103.47
105.80
110.87
112.05
113.65
113.68
113.85
114.07
114.07
7301
7411
7645
7699
7772
7774
7782
7792
7792
914
984
1217
1168
1240
1382
1393
1412
1413
930
1080
1316
1473
1548
1408
1413
1414
1414
0.001
0.006
0.006
0.020
0.020
0.002
0.001
0.0001
0.00005
262
293
302
79
83
126
88
101
11
Globalstar 60
2000-08 C
[26083]
2000 Feb 8.89
Trapezoidal
0.60 x 1.50
box + 2 panels x 1.60
450 full
12 span
400 empty
2000
2001
2001
2001
2005
Feb
Oct
Oct
Oct
Dec
9.03
3.65
4.03
10.20
17.74
52.01
52.01
52.01
52.01
52.00
103.42
106.77
111.02
114.07
114.07
7299
7455
7652
7792
7792
911
1065
1271
1413
1412
929
1088
1275
1413
1415
0.001
0.002
0.0003
0.00003
0.0002
258
109
276
58
77
Globalstar 64
2000-08 D
[26084]
2000 Feb 8.89
Trapezoidal
0.60 x 1.50
box + 2 panels x 1.60
450 full
12 span
400 empty
2000
2005
2005
2005
2005
Feb
Aug
Aug
Sep
Dec
9.03
28.18
31.17
1.28
16.94
52.00
52.01
52.01
52.00
52.00
103.32
106.72
113.82
114.07
114.07
7294
7453
7780
7792
7792
901
1066
1400
1412
1411
929
1083
1403
1414
1415
0.002
0.001
0.0002
0.00008
0.0003
306
99
102
148
87
Delta-2 2nd stage
2000-08 E
[26085]
2000 Feb 8.89
96.91 days
2000 May 15.80
Cylinder
919
2000 Feb 8.96
2000 May 15.70
49.57
49.52
96.03 6947
87.40 6525
226
123
910
169
0.049
0.004
260
313
Dumsat
[Soyuz-11A511U
A15000-079
/IKAR ST07]
2000-09 A
[26086]
BAI-LC31
2000 Feb 8.97
2000 Feb 9.10
2005 Dec 18.11
64.86
64.86
96.55 6972
96.40 6964
581
571
606
600
0.002
0.002
279
278
Soyuz-U 4th stage
(Fregat) *
2000-09 B
[26087]
2000 Feb 8.97
0.36 day
2000 Feb 9.33
Spheres
+ motor
1100
2000 Feb 9.10
2000 Feb 9.31
64.86
64.86
96.52 6971
96.50 6970
581
578
603
604
0.002
0.002
279
271
IRDT **
2000-09 C
[NNA]
2000 Feb 8.97
0.36
2000 Feb 9.33
110
2000-10 A
[26088]
CC-LC39A
2000 Feb 11.74
11.25 days
2000 Feb 22.97
227
229
226
245
239
235
0.001
0.0007
0.0006
283
248
262
D STS-99 #
6M Endeavour F14
R [Shuttle]
5.88 long
2.44 dia
966
1.5 high
3.3 dia
Attached to Fregat until after de-orbit burn
Delta wing
102363
37.3 long
5.5 dia
23.8 span
2000 Feb 11.76
2000 Feb 19.85
2000 Feb 22.25
57.00
57.01
57.01
89.23 6615
89.18 6613
89.10 6609
* Fregat deployed 14 m dia inflatable heat shield and landed in the Orenberg area, but bad weather prevented recovery.
** Inflatable Reentry and Descent Technology deployed 3.6 m dia inflatable heat shield (only deployed to 2.5 m) and landed in the Orenberg area.
# Crew of six astronauts (Kriegel, Gorie, Thiele, Kavandi, Voss and Nohri) extended a radar mast to a length of 61 m for the Shuttle Radar
Topography Mission.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-6
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Garuda 1
[Proton-8K82K
/DM-2M 399-02]
2000-11 A
[26089]
BAI-LC81/23
2000 Feb 12.38
> million years
Box + 2 panels
+ 2 12 m antennae
4500
2000
2000
2000
2000
2000
2000
2000
2000
2004
2005
12.44
12.68
14.26
16.20
18.74
20.79
25.40
1.70
6.16
14.65
51.41
16.34
14.03
10.19
6.71
3.39
3.03
3.02
0.02
0.20
Proton-K 4th stage
(Block DM-2M) $
2000-11 B
[26090]
2000 Feb 12.38
Cylinder
2140
2000 Feb 12.92
2005 Dec 17.54
16.72
17.60
Superbird 4
[Ariane-44LP]
(V-127)
2000-12 A
[26095]
KOU-ELA2
2000 Feb 18.04
> million years
Box + 2 panels 2.3 x 2.6
4057
x 2.8
26 span
2000
2000
2000
2000
2000
2000
2000
2000
2005
18.13
20.09
22.18
24.88
26.27
28.34
29.14
17.67
16.49
5.03
3.39
1.90
0.77
0.31
0.02
0.09
0.03
0.01
Ariane-4 3rd stage
(H-10-3) + VEB
2000-12 B
[26096]
2000 Feb 18.04
Cylinder
1780
11.7 long
2.6 dia
2000 Feb 17.84
2005 Dec 17.05
5.05
4.52
Ekspress-A 2
[Proton-K
DM-2M 399-01]
2000-13 A
2000 Mar 12.17
[26098]
> million years
BAI-LC200/39
Cylindrical
+ 2 panels
2600
5 long
2 dia
26.5 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
12.23
12.79
18.72
21.41
10.22
29.58
1.00
10.20
12.99
23.82
23.76
48.74
0.25
0.20
0.19
0.15
0.10
0.10
0.10
0.09
0.08
0.12
Proton-K 3rd stage
2000-13 B
[26099]
Cylinder
4185
4 long
4.1 dia
2000 Mar 12.35
2000 Mar 14.18
51.63
51.63
2000 Mar 12.17
1.92 day
2000 Mar 14.09
6.22 long
3.7 maxdia
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Mar
Feb
Dec
Feb
Feb
Feb
Feb
Feb
Feb
Feb
Mar
Dec
Mar
Mar
Mar
Mar
Apr
Apr
May
May
May
May
Dec
Nodal
period
(min)
635.28
764.92
805.17
907.92
1051.52
1388.68
1438.80
1436.12
1436.17
1436.10
24480
27706
28669
31059
34686
41232
42218
42165
42166
42165
755.13 27469
755.08 27468
630.43
730.09
862.02
1109.60
1417.73
1433.82
1436.18
1436.08
1436.10
24355
26859
30004
35504
41805
42120
42167
42165
42165
655.15 24987
616.67 23999
629.87
1432.45
1435.10
1436.10
1436.17
1439.30
1442.05
1439.18
1436.00
1436.10
1436.12
24340
42094
42145
42165
42166
42227
42281
42225
42163
42165
42165
88.28 6568
87.02 6505
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
195
6661
8589
13367
20623
33714
35772
35775
35771
35774
36008
35993
35993
35995
35993
35992
35907
35798
35804
35799
0.731
0.529
0.478
0.364
0.222
0.028
0.002
0.0003
0.0004
0.0003
1
0
0
0
1
0
315
348
173
190
6233
6343
35948
35836
0.541
0.537
0
116
220
5182
11474
22488
35068
35688
35777
35756
35777
35734
35779
35776
35763
35784
35795
35799
35816
35796
0.729
0.570
0.405
0.187
0.009
0.001
0.0003
0.0007
0.0002
179
178
181
185
300
338
58
350
14
213
286
37005
34954
0.736
0.722
178
113
222
35690
35752
35779
35781
35845
35884
35816
35781
35782
35781
35702
35740
35782
35793
35794
35853
35992
35878
35787
35791
35792
0.729
0.0006
0.0004
0.0002
0.0002
0.00009
0.0005
0.0007
0.00007
0.0001
0.0001
0
124
146
172
227
137
306
113
53
267
191
186
124
193
128
0.0006
0.0003
325
281
2000-13 continued on next page
$
New launch profile, with 3rd stage and 4th stage casing in sub-orbital trajectories, and the 4th stage performing the initial orbital injection.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-7
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
186
156
207
160
0.002
0.0003
63
68
35601
35617
35698
35681
0.001
0.0008
3
202
Proton-K 4th stage
Casing
2000-13 C
[26100]
2000 Mar 12.17
0.91 day
2000 Mar 13.08
Hollow cyl
800
4.0 long
3.7 dia
2000 Mar 12.35
2000 Mar 12.92
51.62
51.61
88.43 6575
87.65 6536
Proton-K 4th stage
(Block DM-2M)
2000-13 D
[26101]
2000 Mar 12.17
> million years
Cylinder
2350
6.22 long
3.7 dia
2000 Mar 12.80
2005 Dec 22.37
0.25
4.95
1429.12 42028
1429.08 42027
D
Ullage motor
2000-13 E
[26104]
2000 Mar 12.17
207.31 days
2000 Oct 15.48
Cylinder
55
0.90 long
0.68 dia
2000 Mar 16.61
2000 Jun 1.29
2000 Oct 5.19
47.58
47.42
47.12
631.67 24387
629.68 24336
107.32 7481
307
236
100
35709
35678
2104
0.726
0.728
0.134
1
21
68
D
Ullage motor
2000-13 F
[26105]
2000 Mar 12.17
183.95 days
2000 Sep 3.12
Cylinder
55
0.90 long
0.68 dia
2000 Mar 14.41
2000 Jun 30.00
2000 Sep 2.82
47.56
47.31
47.03
635.67 24490
605.90 23719
112.78 7733
257
155
92
35965
34526
2617
0.729
0.725
0.163
1
30
65
MTI #
[Taurus T5 1110]
2000-14 A
[26102]
VDB-LC576E
2000 Mar 12.40
Box+ 4 panels
587
2000 Mar 12.44
2005 Dec 25.19
97.40
97.24
96.52 6971
95.32 6913
573
520
611
548
0.003
0.002
210
190
Taurus 4th stage
2000-14 B
[26103]
2000 Mar 12.40
Cylinder
120
1.34 long
0.97 dia
2000 Mar 12.44
2005 Dec 23.88
97.40
97.18
96.75 6982
95.87 6939
588
544
618
577
0.002
0.002
169
235
Dumsat 2/Fregat *
[Soyuz-U 11A511
Fregat ST08]
2000-15 A
[26106]
BAI-LC31
2000 Mar 20.77
Drum +
spheres
3530
?? +
1.5 high
3.3 dia
2000 Mar 20.96
2005 Dec 23.36
64.54
65.14
320.72 15251
316.37 15380
263
519
18022
17484
0.572
0.552
7
267
Fragment
2000-15 B
[27763]
1 piece, in orbit
2003 Apr 18.57
2003 Oct 10.79
64.77
64.67
261.55 13548
260.77 13521
394
436
13944
13849
0.500
0.496
315
305
Asiastar
[Ariane-5G]
(505 V128)
2000-16 A
[26107]
KOU-ELA3
2000 Mar 21.98
> million years
Box + 2 panels 1.7 x 2.6
2777
x 3
28 span
2000
2000
2000
2000
2000
2005
21.78
24.73
29.22
3.83
5.77
22.65
6.97
2.42
0.03
0.04
0.07
0.02
636.67
856.60
1426.05
1436.53
1436.10
1436.13
24515
29878
41968
42173
42165
42166
587
11338
35520
35670
25782
35770
35687
35660
35659
35920
25790
35804
0.716
0.407
0.002
0.003
0.00009
0.0004
177
180
94
136
178
265
Insat 3B
2000-16 B
[26108]
2000 Mar 21.98
> million years
Box + 2 panels 1.93 x 1.70 2000 Mar 22.11
2070
x 1.65
2000 Mar 23.13
14.70 span 2000 Mar 24.41
2000 Mar 24.44
2000 Mar 26.26
2000 Mar 26.97
2000 Mar 28.00
2000 Mar 28.28
2000 Mar 29.28
2000-16 continued on next page
7.01
2.03
0.25
0.23
0.11
0.34
0.46
0.34
0.11
637.77
930.45
1337.62
1414.88
1425.17
1411.15
1415.72
1410.82
1425.15
24544
31571
40214
41749
41951
41675
41568
41668
41950
568
14690
32011
32624
35479
32978
31647
33064
35506
35762
35695
35660
38116
35666
37615
38731
37516
35637
0.717
0.333
0.045
0.066
0.002
0.056
0.085
0.053
0.002
178
180
202
154
228
157
267
157
206
D
*
#
Mar
Mar
Mar
Apr
Apr
Dec
2nd test flight of the Soyuz-U/Fregat launcher with a mock-up of the ESA Cluster-2 satellites.
Multispectral Thermal Imager; USAF Space Test Program mission P97-3.
2016 - Version 1.15
Year of Launch 2000
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-8
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
2000
2000
2000
2000
2005
4.60
6.94
7.83
23.94
22.66
0.09
0.25
0.01
0.01
0.01
Apr
Apr
Apr
Apr
Dec
Nodal
period
(min)
1431.75
1435.77
1436.02
1436.08
1436.07
42080
42158
42163
42165
42164
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
35288
35720
35748
35743
35784
36114
35840
35821
35829
35787
0.010
0.001
0.0009
0.001
0.00003
259
144
292
279
188
Sylda upperpart
2000-16 C
[26109]
2000 Mar 21.98
Hollow cone
900
4.90 long
4.56 dia
2000 Mar 22.22
2005 Dec 23.09
7.04
6.79
636.20 24503
635.03 24473
575
571
35674
35618
0.716
0.716
178
316
Ariane-5 2nd stage
(EPS)
2000-16 D
[26110]
2000 Mar 21.98
Drum-cone
1190
3.3 long
3.94 dia
2000 Mar 22.22
2005 Dec 23.14
7.04
6.93
634.58 24462
633.90 24444
615
762
35551
35370
0.714
0.708
178
265
IMAGE
2000-17 A
[Delta-2 (7326-9.5) [26113]
#277]
VDB-SLC2W
2000 Mar 25.86
8-sided drum
494
2.3 dia
1 high
2000 Mar 25.90
2005 Dec 22.91
89.93
89.77
858.98 29933
853.88 29815
994
1659
46115
45213
0.754
0.730
320
76
Delta-2 2nd stage
2000-17 B
[26114]
2000 Mar 25.86
52.49 days
2000 May 17.35
Cylinder
919
5.88 long
2.44 dia
2000 Mar 25.90
2000 Apr 30.91
2000 May 17.22
93.91
91.31
91.28
97.18 7002
92.82 6791
87.48 6528
179
178
125
1068
647
174
0.063
0.035
0.004
173
36
308
Delta-2 3rd stage
(Star 37FM)
2000-17 C
[26115]
2000 Mar 25.86
80
1.68 long
0.93 dia
2000 Mar 26.49
2005 Dec 23.68
89.92
89.77
853.95 29816
856.13 29867
990
1662
45885
45314
0.753
0.731
320
76
Fragment
2000-17 D
[28548]
Fragment
2000-17 E
[28549]
Fragment
2000-17 F
[29041]
2005
2005
2005
2005
2006
Feb
Dec
Feb
Dec
Mar
13.36
23.51
12.93
24.59
31.80
89.87
89.85
89.73
89.75
89.93
853.98
853.97
851.53
851.47
852.50
29817
29816
29760
29758
29782
1405
1654
1362
1585
1692
45472
45222
45400
45174
45116
0.739
0.731
0.740
0.732
0.729
110
75
109
75
67
2000-18 A
[26116]
BAI-LC1
2000 Apr 4.21
72.82 days
2000 Jun 16.03
Cyl+2 panels+ 7.5 long
beehive+sphere 2.3 to
7250
2.72 dia
2000
2000
2000
2000
2000
2000
Apr
Apr
May
May
May
Jun
4.57
6.06
1.49
2.83
87
14.92
51.65
51.65
51.65
51.65
51.65
51.65
89.67
91.10
91.67
91.97
92.07
91.90
6637
6707
6735
6750
6754
6747
258
328
351
358
367
359
259
330
361
384
384
377
0.00009
0.0002
0.0007
0.002
0.001
0.001
187
170
157
266
273
47
2000-18 B
[26117]
2000 Apr 4.21
1.12 day
2000 Apr 5.33
Cylinder
2300
2000 Apr 4.63
2000 Apr 5.24
51.65
51.66
88.22 6565
87.33 6521
172
141
201
144
0.002
0.0003
121
93
D Soyuz-TM 30 *
2M [Soyuz-U 11A511U]
R
D
Soyuz-U 3rd stage
(Block I)
*
Cosmonauts Zaletin and Kaleri docked with MIR (front port) 2000 Apr 6.27; undocked 2000 Jun 15.89. This was the last manned visit to MIR.
Orbit of MIR raised by Progress-M1 2.
2016 - Version 1.15
8.1 long
2.66 dia
Year of Launch 2000
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-9
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
235
36037
35983
35740
35854
35764
35773
35781
36033
36103
36023
35785
35900
35805
35801
35790
0.730
0.0008
0.0005
0.0005
0.0005
0.0005
0.00003
0.0001
0
138
157
99
149
325
351
206
Cylindrical
+ 2 panels
2500
5 long
2 dia
26.5 span
2000
2000
2000
2000
2000
2000
2000
2005
17.93
18.26
1.00
2.72
3.70
8.00
30.68
22.78
49.15
0.02
0.03
0.04
0.03
0.04
0.06
0.06
Proton-K 3rd stage
(8S812)
2000-19 B
[26244]
2000 Apr 17.88
1.88 day
2000 Apr 19.70
Cylinder
4185
4 long
4.1 dia
2000 Apr 18.12
2000 Apr 19.60
51.64
51.64
88.27 6567
87.22 6515
184
133
193
139
0.0006
0.0005
315
272
Proton-K 4th stage
Casing
2000-19 C
[26245]
2000 Apr 17.88
2 days
2000 Apr 19
Hollow cyl
800
4.0 long
3.7 dia
2000 Apr 18.05
2000 Apr 18.42
51.63
51.63
88.37 6572
87.10 6510
182
110
204
152
0.002
0.003
41
158
Proton-K 4th stage
(Block DM-2M)
2000-19 D
[26246]
2000 Apr 17.88
> million years
Cylinder
2350
6.22 long
3.7 dia
2000 Apr 18.17
2005 Dec 22.53
0.05
5.09
1446.72 42372
1446.32 42365
35950
35924
36037
36048
0.001
0.001
153
120
Ullage motor
2000-19 E
[26710]
2000 Apr 17.88
312.67 days
2001 Feb 24.55
Cylinder
55
0.90 long
0.68 dia
2001 Feb 22.02
2001 Feb 24.48
47.85
47.78
163.77 9915
96.17 6954
97
85
6977
1065
0.347
0.070
89
97
Ullage motor
2000-19 F
[26711]
2000 Apr 17.88
Cylinder
55
0.90 long
0.68 dia
2001 Feb 20.08
2001 Sep 20.17
47.83
47.57
623.57 24178
90.65 6685
173
91
35426
521
0.729
0.032
79
203
Galaxy 4R
[Ariane-42L]
(V129)
2000-20 A
[26298]
KOU-ELA2
2000 Apr 18.02
> million years
Box+ 2 panels
3668
4.00x3.60
x2.7
26 span
2000
2000
2000
2000
2000
2000
2000
2000
2005
18.85
24.12
24.66
27.59
3.76
9.86
12.22
19.72
25.48
7.10
4.55
4.16
0.04
0.04
0.01
0.01
0.02
0.01
219
4362
5678
35760
35778
35595
35795
35783
35777
32075
35017
35761
35792
35795
35849
35874
35790
35796
0.707
0.588
0.555
0.0003
0.0002
0.003
0.0009
0.00008
0.0002
178
181
180
349
343
31
183
106
330
Ariane-4 3rd stage
(H-10-3) + VEB
2000-20 B
[26299]
2000 Apr 18.02
Cylinder
1780
11.7 long
2.6 dia
+ 4x1
2000 Apr 18.87
2005 Dec 24.28
7.09
7.21
174
251
31912
24534
0.708
0.647
176
72
560.77
698.10
739.88
1435.58
1436.12
1432.82
1438.55
1436.12
1436.12
24512
42449
42381
42141
42255
42163
42165
42164
Apogee
height
(km)
2000-19 A
2000 Apr 17.88
[26243]
> million years
BAI-LC200/39
Apr
Apr
Apr
Apr
May
May
May
May
Dec
636.55
1450.62
1447.17
1434.88
1440.72
1436.02
1436.13
1436.07
Perigee
height
(km)
SESAT
[Proton-K
DM-2M 397-01]
2016 - Version 1.15
Apr
Apr
May
May
May
May
May
Dec
Nodal
period
(min)
22526
26068
27098
42154
42165
42101
42213
42165
42165
556.87 22422
426.57 18771
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-10
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Progress-M1 2 *
[Soyuz-U 11A511U]
2000-21 A
[26301]
BAI-LC1
2000 Apr 25.84
174 days
2000 Oct 16
Cyl+2 panels+ 7.9 long
beehive+sphere 2.3 to
7280
2.72 dia
2000
2000
2000
2000
2000
2000
2000
25.89
26.09
28.19
1.49
2.83
7.87
22.51
51.64
51.65
51.65
51.65
51.65
51.65
51.65
88.70
89.40
91.12
91.67
91.97
92.07
91.12
6589
6624
6708
6735
6750
6754
6708
186
236
327
351
358
367
324
234
254
332
361
384
384
334
0.004
0.001
0.0003
0.0007
0.002
0.001
0.0007
82
132
162
157
266
273
175
D
Soyuz-U 3rd stage
(Block I)
2000-21 B
[26302]
2000 Apr 25.84
1.61 day
2000 Apr 27.45
Cylinder
2300
8.1 long
2.66 dia
2000 Apr 25.89
2000 Apr 27.36
51.64
51.63
88.70 6589
87.23 6516
186
133
234
141
0.004
0.0007
82
139
Goes 11
[Atlas-2A]
2000-22 A
[26352]
CC-LC36A
2000 May 3.30
> million years
Cube+ panel
+ boom+sail
2217
2 side
4.81 span
17.71 long
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
3.90
5.42
8.22
10.24
15.18
16.86
18.62
20.74
21.61
22.40
25.38
20.04
5.87
1.25
0.27
0.58
0.27
0.26
0.24
0.26
0.25
0.05
244
11223
29196
35625
35756
35664
35748
35744
35785
35781
35758
42205
42229
43548
42353
35795
35986
35982
35787
35794
35793
35805
0.760
0.468
0.168
0.074
0.0005
0.004
0.003
0.0005
0.0001
0.0001
0.0006
180
182
165
51
293
65
65
33
270
250
36
D
Atlas-2A 2nd stage
(Centaur AC-137)
2000-22 B
[26353]
2000 May 3.30
4936 days
2013 Nov 7
Cylinder
1815
10.1 long
3.05 dia
2000 May 3.89
2005 Dec 26.04
2013 Nov 7.68
20.16
20.50
20.33
240
177
133
41581
17160
289
0.759
0.564
0.012
182
354
105
D
Cosmos 2370
[Soyuz-U 11A511
A15000-649]
2000-23 A
[26354]
BAILC1
2000 May 3.57
366 days
2001 May 4
Cylindrical
+ 2 panels
7000
6.5 long
2.7 dia
May
May
May
May
May
Jun
Jun
Jun
Jul
Jul
Jul
Jul
Aug
Aug
Aug
Sep
Sep
Sep
Oct
Oct
183
241
225
232
226
242
223
237
222
241
224
241
223
240
224
241
225
240
224
241
277
302
272
304
273
306
265
304
263
309
275
307
270
304
267
304
272
312
278
305
0.007
0.005
0.004
0.005
0.004
0.005
0.003
0.005
0.003
0.005
0.004
0.005
0.004
0.005
0.003
0.005
0.004
0.005
0.004
0.005
63
77
68
100
89
108
90
100
69
80
73
85
75
103
91
105
92
100
94
78
*
Docked with MIR (Kvant1 port) 2000 Apr 27.89; undocked 2000 Oct 15.76.
2016 - Version 1.15
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000-23 continued on next page
Apr
Apr
Apr
May
May
May
Oct
Nodal
period
(min)
May
May
May
May
May
May
May
May
May
May
Dec
3.61
4.38
17.89
18.10
31.72
1.06
21.47
22.60
10.35
10.66
26.94
27.33
13.83
14.10
31.89
1.85
18.22
18.65
5.12
5.56
64.78
64.76
64.76
64.76
64.76
64.76
64.75
64.74
64.75
64.75
64.74
64.74
64.74
64.74
64.74
64.74
64.74
64.73
64.73
64.73
760.67
999.07
1464.13
1602.80
1435.57
1438.08
1440.12
1435.03
1436.25
1436.15
1435.87
27603
33105
42751
45368
42154
42204
42244
42144
42168
42166
42161
753.28 27424
306.13 15047
88.72 6590
89.10
89.95
89.48
89.87
89.50
90.00
89.38
89.93
89.35
90.02
89.48
90.00
89.43
89.95
89.40
89.97
89.47
90.03
89.52
89.97
6609
6650
6627
6647
6628
6653
6623
6649
6621
6653
6628
6653
6625
6650
6624
6651
6627
6655
6629
6651
Year of Launch 2000
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-11
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
64.73
64.73
64.72
64.72
64.72
64.72
64.72
64.72
64.72
64.71
64.71
64.71
64.71
64.71
64.70
64.70
64.70
64.70
64.70
64.70
64.70
64.69
64.69
89.53
90.03
89.53
90.07
89.52
90.00
89.57
90.50
89.88
90.10
89.58
90.07
89.62
90.25
89.88
90.10
89.90
90.10
89.90
90.12
89.85
90.07
89.02
64.75
64.78
Oct
Oct
Nov
Nov
Nov
Nov
Nov
Nov
Dec
Dec
Jan
Jan
Feb
Feb
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Apr
May
17.97
18.23
1.75
1.97
15.53
15.86
29.25
29.82
27.91
28.35
18.56
18.95
6.35
6.79
3.19
3.51
20.94
21.20
28.96
29.08
5.89
5.95
3.80
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6630
6654
6630
6656
6629
6653
6631
6678
6648
6658
6632
6657
6634
6665
6647
6658
6648
6658
6648
6659
6646
6656
6604
226
240
224
240
224
243
227
249
230
251
232
251
235
250
241
255
250
257
249
254
242
247
203
278
311
278
315
276
306
278
349
308
308
275
305
276
323
295
304
289
302
290
306
292
308
248
0.004
0.005
0.004
0.006
0.004
0.005
0.004
0.007
0.006
0.004
0.003
0.004
0.003
0.005
0.004
0.004
0.003
0.003
0.003
0.004
0.004
0.005
0.003
72
83
74
100
89
119
100
93
80
74
63
103
86
102
80
55
18
352
345
323
320
302
296
89.02 6605
87.13 6511
180
121
272
143
0.007
0.002
58
67
Soyuz-U 3rd stage
(Block I)
2000-23 B
[26355]
2000 May 3.57
2.86 days
2000 May 6.43
Cylinder
2400
8.1 long
2.66 dia
2000 May 3.62
2000 May 6.38
USA 149 (DSP 20)
[Titan-4B-29]
2000-24 A
[26356]
CC-LC40
2000 May 8.67
> million years
Stepped cyl
+ 2 panels
2380
11.5 long
3.2 dia
6.7 span
No elements available; orbits from amateur observations.
2010 Mar 16.14
5.86
1436.12 42165 35755 35818
0.0007
244
Titan-4B 2nd stage
2000-24 B
[26357]
2000 May 8.67
79.75 days
2000 Jul 27.42
Cylinder
2000
9.94 long
3.05 dia
2000 May 9.15
2000 Jun 29.63
2000 Jul 27.28
0.041
0.024
0.004
78
313
290
IUS stage 1
2000-24 C
[26358]
2000 May 8.67
Drum+cone
1050
3.52 long
2.34 dia
Geosynchronous transfer orbit
No elements available
IUS stage 2
2000-24 D
[26359]
2000 May 8.67
> million years
Drum+cone
985
2 long
1.61 dia
No elements available; orbits from amateur observations.
2010 Aug 8.66
6.29
1444.25 42324 35915 35977
0.0007
11
2000-24 E
[28156]
2000 May 8.67
> million years
Plate
1 dia
No elements available; orbits from amateur observations.
2010 Aug 7.55
6.53
1444.27 42325 34947 36945
0.024
220
Lens cover
2016 - Version 1.15
28.64
28.63
28.63
93.92 6844
91.45 6724
87.43 6526
187
187
124
744
504
170
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-12
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Navstar 47
2000-25 A
(USA 150, GPS-2R-4) [26360]
[Delta-2 (7925-9.5) CC-LC17A
#278]
2000 May 11.08
1 million years
Box+ 2 panels
2032
1.52x1.93
x1.93
19.3 span
2000
2000
2000
2000
2005
11.18
15.67
26.67
27.92
24.24
38.90
54.88
54.89
54.91
54.97
356.73
712.45
715.23
718.03
717.93
Delta-2 2nd stage
2000-25 B
[26361]
2000 May 11.08
104.22 days
2000 Aug 23.30
Cylinder
919
5.88 long
2.44 dia
2000 May 11.12
2000 Jul 1.19
2000 Aug 23.19
37.66
37.64
37.60
Delta-2 3rd stage
(PAM-D)
2000-25 C
[26362]
2000 May 11.08
Cone-cyl
205
2.29 long
1.5 dia
2000 May 11.18
2005 Dec 26.13
SIMSAT 1 *
[Rokot/Breeze-KM]
2000-26 A
[26365]
PLE-LC133
2000 May 16.35
SIMSAT 2 *
2000-26 B
[26366]
2000 May 16.35
2000-26 C
[26367]
2000 May 16.35
36.11 days
2000 Jun 21.46
Cylindrical
1700
2000-27 A
[26368]
CC-LC39A
2000 May 19.42
9.84 days
2000 May 29.26
Delta wing
101834
Year of Launch 2000
Name
[Launcher]
Fragments
D
D
Rokot 3rd stage
(Breeze-KM)
D STS-101 #
7M Atlantis F21
R [Shuttle]
*
#
Cospar ID
[Norad #] Launchsite
Cospar ID
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
168
19884
20012
20126
20121
20399
20208
20216
20240
20241
0.607
0.006
0.004
0.002
0.002
194
186
172
131
77
100.17 7145
96.58 6973
87.57 6533
198
187
122
1315
1003
186
0.080
0.058
0.005
174
198
280
38.95
38.85
356.43 16653
172.13 10251
187
188
20361
7556
0.606
0.359
194
202
2000 May 16.47
2005 Dec 24.92
86.39
86.35
95.65 6929
95.23 6908
543
520
558
539
0.001
0.001
11
42
2000 May 16.47
2000 May 16.87
2005 Dec 25.90
86.36
86.38
86.35
95.28 6911
95.62 6927
95.18 6906
520
542
521
544
555
534
0.002
0.001
0.0009
247
346
8
3 long
2.5 dia
2000 May 16.47
2000 Jun 3.70
2000 Jun 21.34
86.37
86.36
86.33
91.88 6745
90.88 6697
87.20 6515
178
169
118
556
467
154
0.028
0.022
0.003
318
243
187
37.5 long
5.5 dia
23.8 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
51.58
51.59
51.58
51.60
51.58
51.58
51.58
51.58
51.58
51.58
89.38
90.30
91.00
91.12
91.17
91.45
91.77
92.07
92.05
91.87
159
257
315
322
328
340
355
372
369
352
329
321
332
336
335
352
367
381
380
380
0.013
0.005
0.001
0.001
0.0005
0.0009
0.0009
0.0007
0.0008
0.002
13
11
270
300
226
328
256
347
352
7
657.4
660.3
May
May
May
May
Dec
May
May
May
May
May
May
May
May
May
May
19.45
20.25
20.46
21.14
21.20
24.25
25.25
26.15
27.22
28.57
Nodal
period
(min)
16662
26424
26493
26562
26559
6622
6668
6702
6708
6710
6725
6740
6755
6753
6745
Dummy payloads to simulate the launch of 2 GRACE satellites.
Crew of seven astronauts (Halsell, Horowitz, Weber, Williams, Voss, Helms and Usachev) docked with ISS (PMA-2) 2000 May 21.19; undocked
2000 May 26.92.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-13
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
230
5095
21888
34189
34162
35043
35497
35784
35704
35535
36059
35779
35771
45777
45758
45800
45771
35873
36342
36017
35788
35782
36040
36143
35749
35800
0.775
0.639
0.297
0.125
0.021
0.015
0.006
0.00004
0.0009
0.006
0.001
0.0002
0.0004
179
180
182
203
208
290
265
98
180
107
152
292
254
194
225
45072
28756
0.773
0.683
182
198
Box+ 2 panels
3190
4.6x2.5
x1.8
29.0 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
25.08
26.67
29.52
30.98
2.89
4.90
8.88
10.87
24.74
7.13
11.15
11.82
22.78
19.91
11.14
2.37
0.27
0.11
0.10
0.08
0.08
0.05
0.05
0.16
0.02
0.06
Atlas-3A 2nd stage
(Centaur AC-201)
2000-28 B
[26370]
2000 May 24.97
Cylinder
1905
10.1 long
3.05 dia
2000 May 24.70
2005 Dec 25.14
20.45
19.78
Gorizont 33 #
[Proton-8K82K
Breeze-M 392-01]
2000-29 A
[26372]
BAI-LC81/24
2000 Jun 6.12
> million years
Cylindrical
+ 2 panels
2125
5 long
2 dia
2000
2000
2000
2000
2000
2000
2005
48.75
1.48
1.40
1.46
1.40
1.35
3.49
619.02
1408.05
1423.53
1434.88
1435.95
1436.08
1436.13
24060
41614
41918
42141
42162
42165
42166
368
35030
35410
35749
35781
35786
35778
34995
35441
35670
35776
35785
35786
35796
0.720
0.005
0.003
0.0003
0.00005
0
0.0002
0
289
316
87
124
268
211
Proton-K 4th stage 2000-29 B
(Breeze-M)
[26373]
2000 Jun 6.12
Cylinder
1220
2.61 long
2.4 dia
2000 Jun 13.00
2000 Jun 20.90
2005 Dec 26.26
1.06
1.64
3.30
1434.30 42130
1434.20 42128
1434.28 42129
35497
34666
35657
36005
36832
36844
0.006
0.026
0.026
72
231
137
Breeze-M
Propellant tank
2000 Jun 6.12
Torus
1290
4.1 dia
0.80 cross
2.5 high
2000 Jun 13.92
2005 Dec 24.35
2008 Oct 6.81
48.76
48.49
47.99
618.88 24057
578.85 23008
93.58 6828
370
389
86
34986
32869
814
0.719
0.706
0.053
2
178
111
2008 Oct 6
*
#
$
Orbital
Argument
eccentricity of perigee
(deg)
2000 May 24.97
> million years
6.71
14.60
16.76
19.79
24.50
27.66
26.35
29382
31805
40223
46359
41397
42071
42135
42164
42122
42166
42479
42165
42164
Apogee
height
(km)
2000-28 A
[26369]
CC-LC36B
Jun
Jun
Jun
Jun
Jun
Jul
Dec
835.37
940.82
1338.02
1655.62
1397.02
1431.28
1434.60
1436.07
1433.90
1436.15
1452.20
1436.10
1436.07
Perigee
height
(km)
Eutelsat-W 4
[Atlas-3A] *
2000-29 C
[26377]
May
May
May
May
Jun
Jun
Jun
Jun
Jun
Jul
Jul
Jul
Dec
Nodal
period
(min)
819.63 29012
500.03 20869
TSX 5 $
2000-30 A
[L-1011/Pegasus XL][26374]
VDB-RW30
2000 Jun 7.56
12-sided drum
250
0.95 across 2000 Jun 7.60
0.82 long
2005 Dec 26.86
68.95
68.94
106.28 7433
105.07 7376
404
406
1704
1590
0.087
0.080
208
201
PegasusXL 3rd stage 2000-30 B
[26375]
2000 Jun 7.56
Cone-cyl
176
2.08 long
0.97 dia
68.96
68.96
106.22 7430
104.43 7346
403
405
1700
1530
0.087
0.077
208
175
2000 Jun 7.60
2005 Dec 26.72
Maiden flight of Atlas-3A.
Final Gorizont launch; first successful launch of Proton-K with Breeze-M upperstage.
Tri Service Experiment
2016 - Version 1.15
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-14
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
247
35898
35967
36078
35961
35779
35959
35780
35785
36064
36082
36081
36119
36080
35794
36081
35794
35787
0.730
0.002
0.001
0.0005
0.001
0.0002
0.001
0.0002
0.00002
0
90
22
180
22
117
18
126
17
Cylindrical
+ 2 panels
2600
5 long
2 dia
26.5 span
2000
2000
2000
2000
2000
2000
2000
2000
2005
24.07
24.35
25.81
17.14
17.93
23.80
23.99
26.89
26.77
48.63
0.04
0.10
0.16
0.17
0.14
0.16
0.14
0.02
D
Proton-K 3rd stage
2000-31 B
[26379]
2000 Jun 24.02
2.19 day
2000 Jun 26.21
Cylinder
4185
4 long
4.1 dia
2000 Jun 24.07
2000 Jun 26.15
51.37
51.63
88.53 6580
87.15 6512
190
121
213
145
0.002
0.002
77
44
D
Proton-K 4th stage
Casing
2000-31 C
[26380]
2000 Jun 24.02
1.12 day
2000 Jun 25.13
Hollow cyl
800
4.0 long
3.7 dia
2000 Jun 24.32
2000 Jun 24.75
51.61
51.61
88.27 6567
87.82 6545
183
164
195
169
0.0009
0.0004
90
86
Proton-K 4th stage
(Block DM-2M)
2000-31 D
[26381]
2000 Jun 24.02
> million years
Cylinder
2350
6.22 long
3.7 dia
2000 Jun 24.81
2000 Jun 26.01
2005 Dec 25.45
0.27
0.24
4.73
1453.30 42501
1448.43 42406
1448.05 42399
36109
35892
35972
36136
36163
36068
0.0003
0.003
0.001
167
135
264
D
Ullage motor
2000-31 E
[26499]
2000 Jun 24.02
211.03 days
2001 Jan 21.05
Cylinder
55
0.90 long
0.68 dia
2000 Sep 18.31
2000 Nov 18.70
2001 Jan 20.99
47.07
46.82
46.58
634.82 24468
625.02 24216
92.10 6756
216
154
87
35962
35519
668
0.730
0.730
0.043
23
41
84
D
Ullage motor
2000-31 F
[26500]
2000 Jun 24.02
2123 days
2006 Apr 17
Cylinder
55
0.90 long
0.68 dia
2000 Sep 19.46
2005 Dec 27.05
2006 Apr 16.94
47.14
46.62
46.42
638.13 24553
117.50 7947
87.78 6544
263
159
206
36086
2978
124
0.730
0.178
0.006
23
303
54
Feng-Yun-2 2
[CZ-3 (13-61)]
2000-32 A
[26382]
XI-LC1
2000 Jun 25.49
> million years
Drum
1400
4.1 long
2.1 dia
2000
2000
2000
2000
2000
2005
1.10
1.09
1.07
1.07
1.02
1.08
35642
35818
35801
35776
35778
35785
35934
35930
35864
35790
35796
35789
0.003
0.001
0.0007
0.0002
0.0002
0.00005
336
328
304
105
163
303
CZ-3 3rd stage
(H-8)
2000-32 B
[26383]
2000 Jun 25.49
Cylinder
2000
7.48 long
2.25 dia
2000 Jun 27.92
2005 Dec 26.88
27.43
27.48
632.35 24405
534.43 21815
230
229
35822
30644
0.729
0.697
181
121
Apogee motor
2000-32 C
[26460]
2000 Jun 25.49
Cone-cyl
100
1.5 long
0.7 dia
2000 Jul 29.63
2005 Dec 24.78
1.08
3.90
1438.07 42203
1438.17 42205
35713
35719
35936
35935
0.003
0.003
335
189
26.61
27.59
2.42
6.22
29.76
25.14
1436.18
1440.60
1438.47
1435.93
1436.13
1436.15
24534
42368
42403
42477
42399
42165
42399
42166
42165
Apogee
height
(km)
2000-31 A
2000 Jun 24.02
[26378]
> million years
BAI-LC200/39
Jun
Jun
Jul
Jul
Jul
Dec
637.40
1446.52
1448.25
1452.10
1448.08
1436.10
1448.05
1436.13
1436.08
Perigee
height
(km)
Ekspress-A 3
[Proton-8K82K
DM-2M 394-02]
2016 - Version 1.15
Jun
Jun
Jun
Jul
Jul
Jul
Jul
Jul
Dec
Nodal
period
(min)
42167
42253
42211
42162
42166
42166
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-15
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Nadezhda 6
[Kosmos-3M]
2000-33 A
[26384]
PLE-LC132/1
2000 Jun 28.44
Cylinder
2 dia
+ gravity boom 2.1 high
800
2000 Jun 28.58
2005 Dec 26.08
98.12
98.39
98.67 7074
98.37 7059
683
670
707
691
0.002
0.002
12
213
Tsinghua 1
2000-33 B
[26385]
2000 Jun 28.44
Box
50
0.36x0.36
x0.69
2000 Jun 28.64
2005 Dec 26.05
98.13
98.40
98.65 7073
98.45 7063
683
674
705
696
0.002
0.002
7
230
SNAP 1
2000-33 C
[26386]
2000 Jun 28.44
Drum
6.5
0.33 dia
0.33 high
2000
2000
2000
2005
28.64
28.91
29.89
27.11
98.13
98.12
98.13
98.39
98.67
98.72
98.65
98.30
7074
7076
7073
7056
684
684
683
669
707
710
706
685
0.002
0.002
0.002
0.001
7
2
4
191
Kosmos-3M 2nd stage 2000-33 D
(S3M)
[26387]
2000 Jun 28.44
Cylinder
1434
6.21 long
2.4 to
3.2 dia
2000 Jun 28.65
2005 Dec 26.01
98.13
98.39
98.55 7068
98.25 7054
672
659
707
691
0.002
0.002
12
209
TDRS 8
[Atlas-2A]
2000-34 A
[26388]
CC-LC36A
2000 Jun 30.54
> million years
Box+ 2 panels
+ 2 antennea
3180
3.4x3.4
x8.4
21 span
13 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
30.39
3.58
5.60
8.14
8.49
11.40
12.28
13.16
14.62
25.78
25.58
27.38
26.85
17.34
8.20
7.63
7.87
7.08
7.08
7.05
7.02
2.21
232
397
6052
28061
34396
35455
35619
35611
35613
35633
35775
27687
35981
35971
35973
36057
35931
35928
35912
35953
35944
35800
0.675
0.724
0.546
0.103
0.020
0.006
0.004
0.004
0.004
0.004
0.0003
179
179
180
177
157
187
187
185
186
188
0
Atlas-2A 2nd stage
(Centaur AC-139)
2000-34 B
[26389]
2000 Jun 30.54
Cylinder
1815
10.1 long
3.05 dia
2000 Jun 30.39
2005 Dec 25.83
26.99
26.67
224
247
27645
22336
0.675
0.625
178
50
Sirius SR-1
[Proton-8K82K
DM3 400-01]
2000-35 A
[26390]
BAI-LC81/24
2000 Jun 30.92
> million years
Box+ 2 panels
3800
5.2x5.6
24.8 span
2000
2000
2000
2000
2000
2000
2005
30.96
1.01
4.23
6.62
9.18
14.16
24.66
63.40
63.36
63.43
63.35
63.33
63.33
62.77
183
6158
11346
23848
24407
24424
24296
24397
47085
47048
47101
47098
47142
47271
0.649
0.620
0.502
0.278
0.269
0.269
0.272
225
270
271
271
270
270
271
D
Proton-K 3rd stage
(8S812)
2000-35 B
[26391]
2000 Jun 30.92
0.71 day
2000 Jul 1.63
Cylinder
4185
4 long
4.1 dia
2000 Jun 30.94
2000 Jul 1.46
64.85
64.84
87.73 6541
87.25 6517
154
130
170
147
0.001
0.001
275
280
D
Proton-K 4th stage
Casing
2000-35 C
[26392]
2000 Jun 30.92
0.69 day
2000 Jul 1.61
Hollow cyl
800
4.0 long
3.7 dia
2000 Jul 1.10
2000 Jul 1.34
64.84
64.83
87.30 6519
87.48 6529
137
136
143
164
0.0005
0.002
255
9
Proton-K 4th stage
(Block-DM3)
2000-35 D
[26393]
2000 Jun 30.92
Cylinder
2140
6.22 long
3.7 dia
2000 Jul 1.01
2005 Dec 26.67
63.36
62.58
995.33 33022
988.62 32874
6188
8866
47120
44124
0.620
0.536
270
258
2016 - Version 1.15
Jun
Jun
Jun
Dec
Jun
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Dec
Jun
Jul
Jul
Jul
Jul
Jul
Dec
481.08
638.72
751.87
1247.90
1407.60
1431.35
1435.43
1434.83
1435.93
1436.22
1436.17
20338
24568
27390
38396
41605
42072
42152
42140
42162
42167
42166
480.20 20313
389.58 17670
423.08
994.35
1112.97
1420.18
1434.38
1435.93
1435.95
18669
33001
35576
41853
42131
42162
42162
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-16
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
2000
2000
2000
2000
2000
2000
2005
48.61
1.44
1.44
1.44
1.41
1.36
3.44
633.87
1441.60
1439.58
1433.20
1436.00
1436.08
1436.13
Orbital
Argument
eccentricity of perigee
(deg)
252
35872
35823
35707
35782
35781
35773
35878
35916
35886
35752
35786
35791
35800
0.729
0.0005
0.0008
0.0005
0.00005
0.0001
0.0003
0
290
343
282
322
72
195
Box+ 2 panels
2300
D
Proton-K 3rd stage
2000-36 B
[26395]
2000 Jul 4.99
2.55 days
2000 Jul 7.54
Cylinder
4185
4 long
4.1 dia
2000 Jul 5.17
2000 Jul 7.48
51.62
51.62
88.43 6575
86.95 6502
190
118
203
128
0.001
0.0007
343
266
D
Proton-K 4th stage
Casing
2000-36 C
[26396]
2000 Jul 4.99
0.89 day
2000 Jul 5.88
Hollow cyl
800
4.0 long
3.7 dia
2000 Jul 5.17
2000 Jul 5.78
51.61
51.60
88.70 6589
87.37 6522
180
143
241
144
0.005
0.0001
37
28
Proton-K 4th stage
(Block DM-2M)
2000-36 D
[26397]
2000 Jul 4.99
> million years
Cylinder
2350
6.22 long
3.7 dia
2000 Jul 18.45
2000 Jul 19.74
2005 Dec 25.48
1.52
1.46
3.41
1404.43 41543
1438.02 42202
1436.77 42178
34494
35736
35723
35834
35911
35876
0.016
0.002
0.002
62
346
223
Ullage motor
2000-36 E
[26398]
2000 Jul 4.99
Cylinder
55
0.90 long
0.68 dia
84
2000 Jul 6.37
2005 Dec 26.83
47.38
46.57
635.93 24497
382.18 17445
356
170
35880
21964
0.725
0.625
0
113
Ullage motor
2000-36 F
[26399]
2000 Jul 4.99
256 days
2001 Mar 17
Cylinder
55
0.90 long
0.68 dia
2000 Jul 6.36
2000 Nov 1.22
2001 Mar 16.68
47.32
46.86
46.53
634.72 24465
630.15 24348
89.85 6646
302
194
94
35871
35744
440
0.727
0.730
0.026
0
32
126
Zvezda *
[Proton-8K82K
398-01]
2000-37 A
[26400]
BAI-LC81/23
2000 Jul 12.21
Stepped cyl
+ sphere
19710
13.11 long
4.1 maxdia
30.73 span
2000 Jul
2000 Jul
2000 Jul
2000 Jul
2000 Jul
2000 Jul
2000 Jul
For more
6634
6701
6704
6733
6738
6738
6738
179
288
297
351
352
350
351
333
358
354
358
368
367
368
0.012
0.005
0.004
0.0006
0.001
0.001
0.001
86
90
94
91
166
170
172
D
Proton-K 3rd stage
(8S812)
2000-37 B
[26401]
2000 Jul 12.21
5.50 days
2000 Jul 17.71
Cylinder
4185
4 long
4.1 dia
2000 Jul 12.22
2000 Jul 14.55
2000 Jul 17.62
89.40 6624
88.98 6603
87.20 6514
177
171
124
313
278
147
0.010
0.008
0.002
85
93
108
*
Docked 2000 Jul 26.03 with ISS (Zarya rear port).
12.38
51.60
89.63
14.45
51.58
90.98
20.26
51.58
91.03
23.16
51.58
91.63
24.18
51.58
91.73
25.98
51.58
91.72
26.14
51.58
91.73
orbital info see 1998-67 A
51.60
51.60
51.60
24443
42273
42233
42108
42163
42165
42165
Apogee
height
(km)
2000-36 A
2000 Jul 4.99
[26394]
> million years
BAI-LC200/39
2016 - Version 1.15
5.18
11.83
15.83
17.97
30.73
25.81
26.68
Perigee
height
(km)
Cosmos 2371
[Proton-8K82K
DM2 389-02]
D
Jul
Jul
Jul
Jul
Jul
Aug
Dec
Nodal
period
(min)
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-17
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
2000 Jul 14.26
> million years
Box+ 2 panels
+ antenna
3700
8.66 wide
5.5 high
30.7 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
14.37
15.41
16.69
19.70
23.32
23.44
23.52
27.54
28.50
26.52
26.33
8.41
0.21
0.18
0.15
0.16
0.15
0.17
0.15
0.01
Cylinder
1815
10.1 long
3.05 dia
2000 Jul 14.02
2000 Aug 31.67
2000 Oct 1.14
26.48
26.43
26.38
170
2000 Jul 15.56
2001 Feb 1.40
2001 Aug 14.98
550
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Echostar 6
[Atlas-2AS]
2000-38 A
[26402]
CC-LC36B
D
Atlas-2AS 2nd stage 2000-38 B
(Centaur AC-161)
[26403]
2000 Jul 14.26
79.32 days
2000 Oct 1.58
D
MITA-O (NINA)
[Kosmos-3M
47136-414]
2000-39 A
[26404]
PLE-132/1
2000 Jul 15.50
396 days
2001 Aug 15
CHAMP
2000-39 B
[26405]
2000 Jul 15.50
Kosmos-3M 2nd stage 2000-39 C
+ Rubin
[26406]
2000 Jul 15.50
411 days
2001 Aug 30
D
Cylinder
1434+37
4.21 long
2.4 to
3.2 dia
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
178
9847
33973
33857
35399
35667
35651
35764
35763
35772
38040
38046
37951
35916
35841
35964
35910
35811
35810
35800
0.743
0.465
0.047
0.025
0.005
0.004
0.003
0.0006
0.0006
0.0003
180
181
149
163
172
127
144
305
308
299
668.72 25331
588.42 23260
104.98 7372
142
128
88
37764
33635
1899
0.743
0.721
0.123
179
210
270
87.29
87.25
87.23
93.60 6829
92.55 6778
87.20 6514
427
379
128
475
420
143
0.004
0.003
0.001
328
253
272
2000 Jul 15.56
2000 Jul 15.62
2005 Dec 26.88
87.26
87.27
87.23
93.40 6820
93.53 6826
91.43 6723
408
418
342
474
476
347
0.005
0.004
0.0003
312
324
70
2000 Jul 15.56
2000 Jul 15.62
87.31
87.27
93.57 6828
93.52 6825
390
416
508
477
0.009
0.004
345
326
2001 Aug 30.03
87.22
86.98 6503
118
131
0.001
283
165
20285
20037
19893
20464
20430
20325
20470
0.608
0.003
0.005
0.011
195
265
219
229
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Dec
674.92
875.90
1445.08
1390.37
1427.62
1437.60
1435.82
1436.17
1436.13
1436.08
25488
30325
42341
41265
41999
42194
42159
42166
42165
42165
Navstar 48
2000-40 A
(USA 151, GPS-2R 5) [26407]
[Delta-2 (7925-9.5) CC-LC17A
#279]
2000 Jul 16.39
1 million years
Box+ 2 panels
2032
1.52x1.93
x1.93
19.3 span
2000
2000
2000
2005
16.99
20.50
18.00
26.57
39.06
55.07
55.02
55.00
357.73
725.12
717.93
717.97
D
Delta-2 2nd stage
2000-40 B
[26408]
2000 Jul 16.39
89.61 days
2000 Oct 14.30
Cylinder
919
5.88 long
2.44 dia
2000 Jul 16.56
2000 Aug 31.62
2000 Oct 14.05
37.56
37.56
37.54
100.00 7137
96.50 6969
87.98 6553
195
187
138
1322
994
211
0.079
0.058
0.006
176
164
167
D
Delta-2 3rd stage
(PAM-D)
2000-40 C
[26409]
2000 Jul 16.39
1106 days
2003 Jul 27
Cone-cyl
205
2.29 long
1.5 dia
2000
2000
2001
2002
2003
16.49
16.53
1.62
1.21
27.12
38.32
39.11
38.98
38.87
38.73
356.85
356.27
271.85
189.75
88.10
16666
16648
13901
10938
6559
150
173
166
158
121
20425
20365
14879
8962
241
0.608
0.606
0.529
0.402
0.009
194
194
207
86
174
PAM-D fragment
2000-40 D
[27765]
2000 Jul 16.39
2003 Apr 19.43
2005 Dec 26.50
38.96
38.98
272.40 13920
222.65 12169
174
184
14909
11396
0.529
0.461
168
198
2016 - Version 1.15
Jul
Jul
Aug
Dec
Nodal
period
(min)
Jul
Jul
Jul
Jul
Jul
16693
26736
26559
26560
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-18
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Cluster-2 6*(Salsa) 2000-41 A
[Soyuz-U 11A511U
[26410]
A15000-069
BAI-LC31
Fregat ST09]
2000 Jul 16.53
> million years
Drum +
4 50 m wire
antennea
1200
2.9 dia
1.3 high
2000
2000
2000
2000
2000
2005
Jul
Jul
Jul
Jul
Aug
Dec
16.58
17.77
18.40
23.21
31.50
27.54
64.68
65.00
65.10
90.43
90.76
91.42
321.30
422.67
616.80
3432.28
3428.65
3425.73
Cluster-2 7*(Samba) 2000-41 B
[26411]
2000 Jul 16.53
> million years
Drum
4 50 m wire
antennea
1200
2.9 dia
1.3 high
2000
2000
2000
2000
2000
2005
Jul
Jul
Jul
Jul
Aug
Dec
16.58
17.77
18.36
22.04
31.50
27.58
64.81
64.99
65.02
90.48
90.86
91.42
321.53
424.05
622.27
3431.15
3426.50
3425.27
Soyuz-U 4th stage
(Fregat)
2000-41 C
[26412]
2000 Jul 16.53
0.3 day?
2000 Jul 16.8?
Spheres+motor
1100
3.3 dia
1.5 high
2000 Jul 16.58
64.83
MightySat-2 1
[Minotaur 2]
2000-42 A
[26414]
VDB-CLF
2000 Jul 19.84
846 days
2002 Nov 12
2000 Jul 19.88
2001 Sep 1.64
2002 Nov 11.95
D
Minotaur 4th stage
2000-42 B
[26415]
2000 Jul 19.84
4996 days
2014 Mar 24
D
Picosat 7 & 8 #
2000-42 C
[26904]
2000 Jul 19.84
722 days
2002 Jul 11
PAS 9
[Zenit-3SL]
2000-43 A
[26451]
ODS
2000 Jul 28.95
> million years
Year of Launch 2000
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
119
Cone-cylinder
176
Box+ 2 panels
3659
2.08 long
0.97 dia
2.7x3.6
x 4
26 span
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
15540
18656
24003
75373
75320
75277
250
245
241
16910
17400
21670
18072
24310
35007
121078
120483
116126
0.573
0.645
0.724
0.691
0.684
0.627
1
1
2
358
358
31
15547
18697
24144
75357
75288
75270
259
247
245
16716
17437
21669
18078
24390
35286
121240
120383
116115
0.573
0.646
0.726
0.694
0.684
0.927
1
1
2
357
358
31
319.62 15485
156
18058
0.578
1
97.81
97.78
97.75
95.97 6944
95.22 6907
87.38 6523
546
514
138
585
543
151
0.003
0.002
0.001
192
245
263
2000 Jul 19.88
2005 Dec 26.94
2014 Mar 23.92
97.81
97.90
97.82
95.97 6944
94.32 6864
87.35 6522
548
477
137
583
494
149
0.003
0.001
0.0009
179
186
258
2001 Sep 8.13
2002 Feb 9.26
2002 Jul 10.87
97.78
97.76
97.75
95.13 6904
93.85 6841
87.97 6553
511
454
163
540
471
185
0.002
0.001
0.002
233
51
275
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
1.19
0.22
0.13
0.07
0.08
0.02
0.07
0.04
0.07
0.07
0.06
0.05
0.04
0.01
1925
6596
12239
33124
35405
35697
35786
35777
35777
35747
35784
35785
35692
35778
35800
35750
35757
35780
35781
35789
35808
35794
35791
35781
35788
35789
35785
35794
0.671
0.529
0.387
0.033
0.004
0.001
0.0003
0.0002
0.0002
0.0004
0.00004
0.00004
0.001
0.0002
181
164
160
108
55
133
328
254
91
350
180
320
161
263
Jul
Jul
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Dec
28.75
31.11
1.66
3.79
4.80
7.32
9.12
9.26
12.50
14.20
23.07
28.42
30.33
25.11
Nodal
period
(min)
665.15
758.55
878.13
1368.47
1426.23
1433.90
1436.63
1436.08
1435.97
1434.95
1436.08
1436.13
1433.63
1436.08
25241
27552
30377
40381
41972
42122
42175
42165
42162
42143
42165
42165
42117
42164
2000-43 continued on next page
*
#
First replacement pair for the original 4 Cluster satellites lost in the maiden flight explosion of Ariane-5 in June 1996.
Will fly in formation with the 2nd pair to study in 3-D the interaction of the solar wind with the magnetosphere.
2 small sats, connected by a tether, released from MightySat.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-19
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Zenit-3SL 3rd stage 2000-43 B
(Block DM-SL)
[26452]
2000 Jul 28.95
Cylinder
2140
6.22 long
3.7 maxdia
2000 Jul 28.75
2005 Dec 27.32
1.18
2.01
D
Progress-M1 3 #
[Soyuz-U 11A511U
K15000-668]
2000-44 A
[26461]
BAI-LC1
2000 Aug 6.77
86.53 days
2000 Nov 1.30
Cyl+2 panels+ 7.9 long
beehive+sphere 2.3 to
7280
2.72 dia
2000
2000
2000
2000
2000
2000
2000
2000
51.33
51.58
51.57
51.58
51.58
51.58
51.57
51.57
89.10
90.18
91.67
91.80
92.18
92.10
92.27
92.22
D
Soyuz-U 3rd stage
(Block I)
2000-44 B
[26462]
2000 Aug 6.77
1.81 day
2000 Aug 8.58
Cylinder
2300
8.1 long
2.66 dia
2000 Aug 6.95
2000 Aug 8.47
51.63
51.64
Cluster-2 5*(Rumba) 2000-45 A
[Soyuz-U 11A511U
[26463]
A15000-070
BAI-LC31
Fregat ST10]
2000 Aug 9.47
> million years
Drum
4 50 m wire
antennea
1200
2.9 dia
1.3 high
2000
2000
2000
2000
2000
2000
2000
2000
2005
Aug
Aug
Aug
Aug
Aug
Aug
Aug
Sep
Dec
9.63
10.59
11.17
12.01
14.75
14.90
17.25
14.79
27.50
64.67
64.84
64.94
65.35
90.84
90.64
90.89
90.73
93.83
306.30
409.22
595.67
996.80
3427.28
3840.48
3431.10
3424.55
3425.98
Cluster-2 8*(Tango) 2000-45 B
[26464]
2000 Aug 9.47
> million years
Drum
4 50 m wire
antennea
1200
2.9 dia
1.3 high
2000
2000
2000
2000
2000
2005
Aug
Aug
Aug
Aug
Sep
Dec
9.62
10.65
11.23
14.75
14.79
27.50
64.79
64.87
64.93
90.81
90.71
89.94
306.22
401.55
999.38
3423.55
3424.63
2426.25
Soyuz-U 4th stage
(Fregat)
2000 Aug 9.47
0.4 day?
2000 Aug 9.8?
Spheres+motor
1100
3.3 dia
1.5 high
2000 Aug 9.53
2000 Aug 9.62
2000 Aug 9.70
Year of Launch 2000
Name
[Launcher]
Fragments
#
*
Cospar ID
[Norad #] Launchsite
Cospar ID
2000-45 C
[26465]
Aug
Aug
Aug
Aug
Sep
Oct
Oct
Oct
6.95
7.76
9.08
18.88
17.89
15.84
21.15
31.90
64.87
64.77
64.86
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1912
1904
35767
35781
0.671
0.672
179
142
6609
6662
6734
6742
6760
6756
6764
6762
214
271
348
357
376
374
381
379
246
296
364
369
387
380
390
387
0.002
0.002
0.001
0.0009
0.0008
0.0004
0.0007
0.0006
68
269
228
315
224
342
84
130
88.55 6581
87.35 6522
184
139
221
147
0.003
0.0006
75
89
15052
18258
23451
33055
75300
81236
75356
75260
75281
256
237
237
881
17163
17255
17240
17683
21499
17092
23522
33908
52471
120679
132461
120714
120079
116306
0.559
0.638
0.718
0.780
0.687
0.709
0.687
0.680
0.630
358
358
356
358
357
358
357
358
25
15049
18030
23022
75245
75261
75285
243
240
237
17239
17596
21429
17098
23062
33050
120494
120169
116383
0.560
0.633
0.713
0.686
0.681
0.631
358
358
358
358
358
23
-160
254
-158
17080
17083
17075
0.581
0.559
0.581
358
358
358
664.23 25218
664.37 25221
299.80 14839
306.15 15047
299.75 14837
First unmanned cargo supply ship to ISS, docked 2000 Aug 8.84 (Zvezda rear port); undocked 2000 Nov 1.17.
Second replacement pair for the original 4 Cluster satellites lost in the maiden flight explosion of Ariane-5 in June 1996.
Will fly in formation with the 1st pair to study in 3-D the interaction of the solar wind with the magnetosphere.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-20
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Brasilsat-B 4
[Ariane-44 LP]
(V131)
2000-46 A
[26469]
KOU-ELA2
2000 Aug 17.97
> million years
Drum
1757
3.43 dia
3.65 to
8.3 high
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
Aug
Aug
Aug
Aug
Aug
Aug
Sep
Oct
Oct
Dec
18.42
19.36
20.76
22.73
25.87
30.27
19.11
3.65
6.80
27.30
2.97
0.18
0.32
0.06
0.10
0.10
0.11
0.07
0.08
0.05
633.25
752.23
1004.93
1379.02
1436.18
1436.12
1440.03
1436.82
1436.08
1436.12
24427
27399
33234
41040
42166
42165
42242
42179
42165
42165
272
6289
17969
33567
35752
35754
35833
35792
35780
35776
35826
35752
35742
35756
35823
35819
35894
35809
35792
35797
0.728
0.538
0.267
0.027
0.0008
0.0008
0.0007
0.0002
0.004
0.0002
178
220
173
122
227
222
196
69
55
105
Nilesat 102
2000-46 B
[26470]
2000 Aug 17.97
> million years
Box+ 2 panels
1827
2.4x2.3
x1.7
21.5 span
2000
2000
2000
2000
2000
2000
2000
2005
Aug
Aug
Aug
Aug
Aug
Sep
Sep
Dec
18.59
19.52
20.42
24.15
24.90
6.88
7.85
22.81
2.95
0.99
0.45
0.05
0.01
0.16
0.05
0.02
631.78
756.12
1108.12
1437.77
1434.07
1436.25
1436.10
1436.08
24390
27493
35472
42198
42125
42168
42165
42165
277
6938
22411
35734
35625
35763
35769
35762
35745
35290
35776
35904
35868
35815
35804
35809
0.727
0.516
0.188
0.002
0.003
0.0006
0.0004
0.0006
178
158
176
275
289
274
277
352
Spelda
upper section
2000-46 C
[26471]
2000 Aug 17.97
Hollow drum
410
2.8 long
4 dia
2000 Aug 18.21
2005 Dec 27.05
2.95
3.01
632.42 24406
466.30 19919
294
274
35761
26807
0.727
0.666
178
9
Ariane-4 3rd stage 2000-46 D
(H-10-3) + VEB +
[26490]
Spelda lower section
2000 Aug 17.97
Cylinder
1780
11.05 long
2.6 dia
2000 Sep 11.27
2005 Dec 26.53
2.91
3.25
655.47 24996
606.20 23727
291
306
36943
34391
0.733
0.718
195
0
USA 152
2000-47 A
(Lacrosse 4)
[26473]
[Titan-4B 28 K-25] VDB-LC4E
2000 Aug 17.99
Cylindrical
+ 2 panels +
radar antenna
14500
12 long
4 dia
45 span
2000 Aug 19.45
2000 Aug 20.47
2000 Aug 22.45
68.00
68.00
68.00
97.23 7004
98.30 7056
98.53 7067
575
663
685
677
692
692
0.007
0.002
0.0005
179*
224*
162*
Titan-4B 2nd stage
2000-47 B
[26474]
2000 Aug 17.99
Cylinder
2000
9.94 long
3.05 dia
2000 Aug 18.08
2005 Dec 27.87
68.01
68.00
97.17 7002
96.73 6981
571
553
676
651
0.008
0.007
181
219
Fragment
2000-47 C
[27469]
2002 Jul 14.73
2005 Feb 19.58
2005 Dec 26.79
68.00
68.00
68.00
96.92 6990
96.85 6986
96.85 6986
563
558
556
659
658
659
0.007
0.007
0.007
151
200
223
2000-47 D
2000 47 E
2000 47 F
[35415]
[40528]
[40529]
2015 Mar 23.02
2015 Mar 23.01
68.00
68.00
96.52 6970
96.50 6969
550
550
633
632
0.006
0.006
146
145
DM-F3 #
[Delta-3 (8930)
#280]
2000-48 A
[26476]
CC-LC17B
2000 Aug 23.46
Cyl + top and
base plate
4348
3 long
0.8 dia
2000 Aug 23.51
2005 Dec 30.20
27.60
27.52
361.07 16797
164.43 9943
194
185
20643
6944
0.609
0.340
173
343
Delta-3 2nd stage
2000-48 B
[26475]
2000 Aug 23
Cylinder +
engine nozzle
2475
8.8 long
4 dia
2000 Aug 23.65
2005 Dec 28.96
27.87
27.44
353.78 16570
346.53 16343
163
201
20219
19728
0.605
0.597
174
152
2016 - Version 1.15
Year of Launch 2000
Name
[Launcher]
Fragments
*
#
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-21
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Size
(m)
Lifetime
Date of
orbital
determination
No elements available; orbits based on visual observations.
Dummy payload on the 3rd Delta-3 launch. Catalgue numbers interchanged 2006 Jun.
2016 - Version 1.15
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-22
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital
Argument
eccentricity of perigee
(deg)
225
36408
36257
35780
35337
35762
35770
35781
35779
35757
36470
36583
36507
35814
36092
35813
35795
35797
35796
35811
0.7329
0.002
0.003
0.0004
0.009
0.0006
0.0003
0.0002
0.002
0.0006
0
262
326
320
37
335
324
322
281
152
2000 Aug 28.84
> million years
Cylindrical
2000
5 long
2 dia
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
28.89
29.16
2.73
14.01
15.32
18.91
13.98
14.69
30.77
29.82
48.59
2.22
1.85
1.45
1.45
1.47
1.40
1.40
1.36
3.30
D
Proton-K 3rd stage
2000-49 B
[26478]
2000 Aug 28.84
2.07 days
2000 Aug 30.91
Cylinder
4185
4 long
4.1 dia
2000 Aug 29.02
2000 Aug 30.72
51.64
51.64
88.27 6567
87.33 6521
183
139
194
146
0.0008
0.0006
298
332
D
Proton-K 4th stage
Casing
2000-49 C
[26479]
2000 Aug 28.84
2.09 day
2000 Aug 30.93
Hollow cyl
800
4.0 long
3.7 dia
2000 Aug 29.01
2000 Aug 30.75
51.63
51.64
88.38 6573
87.37 6523
185
140
203
148
0.001
0.0006
42
285
Proton-K 4th stage
(Block DM-2M)
2000-49 D
[26480]
2000 Aug 28.84
> million years
Cylinder
2350
6.22 long
3.7 dia
2000 Sep 13.89
2005 Dec 26.23
1.51
3.36
1466.52 42758
1466.57 42759
36277
36305
36482
36456
0.002
0.002
321
178
D
Fragment
2000-49 E *
[26472]
2000 Sep 1
4 days
2000 Aug 29.98
2000 Aug 31.56
51.63
51.64
91.40 6722
90.58 6682
182
175
504
431
0.024
0.019
70
76
D
Ullage motor
2000-49 F *
[26501]
2000 Aug 28.84
489 days
2001 Dec 30
Cylinder
55
0.90 long
0.68 dia
2000 Sep 18.12
2001 Apr 28.70
2001 Dec 30.28
47.41
46.62
46.30
647.20 24785
600.42 23576
91.50 6727
335
135
105
36478
35259
592
0.729
0.724
0.036
5
66
20
D
Ullage motor
2000-49 G *
[26502]
2000 Aug 28.84
268 days
2001 May 23
Cylinder
55
0.90 long
0.68 dia
2000 Sep 19.43
2001 Jan 15.002
2001 May 23.13
47.38
46.86
46.52
645.88 24752
625.13 24218
89.17 6612
274
159
68
36472
35521
399
0.731
0.730
0.025
5
37
146
D
JB-3 A
(Zi Yuan 2)
[CZ-4B 3(62)]
2000-50 A
[26481]
WUZ-LC1
2000 Sep 1.14
5670 days
2016 Mar 11
Box + panel
1500
2.0x1.8
x2.2
9.8 span
2000
2000
2000
2000
2005
2016
97.44
97.41
97.42
97.42
97.19
97.14
94.20
94.27
94.38
94.45
94.30
87.45
6859
6862
6867
6870
6863
6527
468
474
483
484
483
145
492
493
495
499
487
152
0.002
0.001
0.0009
0.001
0.0003
0.0006
293
308
234
207
338
181
D
CZ-4B 3rd stage
2000-50 B
[26482]
2000 Sep 1.14
791 days
2002 Nov 1
Drum
1000
2 long
2.9 dia
2000 Sep 1.19
2001 Oct 1.20
2002 Nov 1.33
97.42
97.37
97.32
94.17 6857
93.47 6823
87.32 6520
466
434
136
490
455
146
0.002
0.002
0.0008
304
10
270
*
USSPACECOM first reserved 26472 for the Ariane 3r stage (2000-46 D, now 26490); the 2000-49 E designation is also used for 26501 and F for 26502.
1.19
1.41
8.20
10.82
30.13
10.84
24726
42874
42761
42175
42093
42166
42161
42168
42166
42162
Apogee
height
(km)
2000-49 A
[26477]
BAI-LC81/24
Sep
Sep
Sep
Sep
Dec
Mar
644.88
1472.48
1466.63
1436.63
1432.43
1436.15
1435.88
1436.25
1436.17
1435.97
Perigee
height
(km)
Raduga-1 5
[Proton-8K82K
DM-2 401-02]
2016 - Version 1.15
Aug
Aug
Sep
Sep
Sep
Sep
Oct
Oct
Oct
Dec
Nodal
period
(min)
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-23
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
63.38
63.38
63.37
63.37
63.36
63.27
63.35
63.35
63.36
63.55
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
994.47
687.63
1144.02
1420.77
1434.32
1432.82
1435.93
1436.03
1436.08
1436.02
Orbital
Argument
eccentricity of perigee
(deg)
6192
6085
12658
23918
24448
24446
24596
24551
24528
24541
47057
46861
47052
47054
47055
46998
46970
47019
47044
47028
0.619
0.621
0.475
0.276
0.268
0.268
0.265
0.266
0.267
0.267
270
270
270
270
270
271
270
269
269
269
2000 Sep 5.41
> million years
Box+ 2 panels
3800
5.2x5.6
24.8 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
D
Proton-K 3rd stage
(8S812)
2000-51 B
[26484]
2000 Sep 5.41
0.69 day
2000 Sep 6.10
Cylinder
4185
4 long
4.1 dia
2000 Sep 5.58
2000 Sep 6.07
64.84
64.87
87.70 6539
86.88 6499
145
118
176
121
0.002
0.0002
326
218
D
Proton-K 4th stage
Casing
2000-51 C
[26485]
2000 Sep 5.41
0.24 day
2000 Sep 5.65
Hollow cyl
800
4.0 long
3.7 dia
2000 Sep 5.58
64.82
87.45 6526
143
153
0.0007
67
Proton-K 4th stage
(Block-DM3)
2000-51 D
[26486]
2000 Sep 5.41
Cylinder
2140
6.22 long
3.7 dia
2000 Sep 5.49
2005 Sep 29.21
63.37
63.33
994.68 33008
987.88 32857
6194
1928
47065
51029
0.619
0.747
270
264
Eutelsat-W1R
[Ariane-44P]
(V132)
2000-52 A
[26487]
KOU-ELA2
2000 Sep 6.94
> million years
Box+ 2 panels
3250
4.6x2.5
x3.4
31.7 span
2000
2000
2000
2000
2000
2005
6.74
8.58
9.66
19.10
22.37
28.02
6.83
2.87
0.12
0.09
0.08
0.05
275
8604
31444
35773
35772
35751
35570
35744
35761
35802
35800
35820
0.726
0.475
0.054
0.0003
0.0003
0.0008
176
179
145
269
267
305
Ariane-4 3rd stage
(H-10-3) + VEB
2000-52 B
[26488]
2000 Sep 6.94
Cylinder
1775
11.05 long
2.6 dia
2000 Sep 6.74
2005 Dec 29.24
6.84
7.15
383
375
37312
36268
0.732
0.726
178
230
628.33
800.25
1326.00
1436.17
1436.08
1436.07
33003
32852
36234
41864
42130
42101
42162
42164
42165
42163
Apogee
height
(km)
2000-51 A
[26483]
BAI-LC81/23
Sep
Sep
Sep
Sep
Sep
Dec
5.49
6.17
7.55
11.09
13.66
16.66
18.65
19.47
15.40
27.32
Perigee
height
(km)
Sirius SR-2
[Proton-8K82K
DM3 400-02]
2016 - Version 1.15
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Nov
Dec
Dec
Nodal
period
(min)
24301
28553
39982
42166
42165
42164
664.55 25226
643.87 24700
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-24
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D STS-106 *
7M Atlantis F22
R [Shuttle]
2000-53 A
[26489]
CC-LC39B
2000 Sep 8.53
11.80 days
2000 Sep 20.33
Delta wing
100368
37.5 long
5.5 dia
23.8 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Sep
Sep
8.58
8.69
9.49
10.19
11.57
14.38
15.9
17.45
18.25
19.92
51.58
51.58
51.58
51.58
51.58
51.58
51.58
51.58
51.58
51.58
89.33
90.62
91.07
91.72
91.83
91.95
92.07
92.18
92.15
92.17
6620
6683
6706
6737
6743
6749
6754
6760
6759
6759
158
279
296
352
361
368
372
376
375
375
324
331
358
365
369
372
379
387
385
386
0.013
0.004
0.005
0.001
0.0006
0.0003
0.0005
0.0008
0.0008
0.0009
11
338
304
36
55
117
179
217
245
255
D
2000-53 B
[26492]
2000 Sep 20
12 days
2000-53 C
[26493]
2000 Sep 25
17 days
2000
2000
2000
2000
Sep
Sep
Sep
Sep
12.98
20.52
14.38
24.62
51.58
51.59
51.58
51.55
91.52
89.00
91.47
88.72
6728
6604
6725
6589
346
215
340
208
353
235
352
213
0.0005
0.001
0.0009
0.0004
82
308
34
111
Astra-2 B
[Ariane-5G (506)]
(V130)
2000-54 A
[26494]
KOU-ELA3
2000 Sep 14.95
> million years
Box+ 2 panels
3315
2.8x1.7
x2.5
32.3 span
2000
2000
2000
2000
2000
2000
2005
Sep
Sep
Sep
Sep
Sep
Sep
Dec
14.76
16.72
18.63
23.31
27.98
30.99
29.61
7.36
1.61
0.53
0.18
0.14
0.12
0.02
629.38
959.55
1343.18
1436.07
1436.32
1436.12
1436.05
24328
32226
40326
42164
42169
42165
42164
457
15920
32108
35777
35579
35769
35745
35442
35774
35787
35794
36002
35804
35826
0.719
0.308
0.046
0.0002
0.005
0.004
0.001
181
174
158
180
37
32
349
AMC 7 (GE 7)
2000-54 B
[26495]
2000 Sep 14.95
> million years
Box+ 2 panels
1935
3.6 across
4.1 high
14.5 span
2000
2000
2000
2000
2005
Sep
Sep
Oct
Oct
Dec
24.27
27.88
14.72
25.40
29.33
0.09
0.06
0.03
0.03
0.05
1438.65
1436.13
1432.07
1436.10
1436.08
42215
42166
42086
42165
42165
35764
35768
35693
35773
35774
35908
35806
35722
35800
35798
0.002
0.0004
0.0003
0.0003
0.0003
42
137
234
288
169
Ariane-5 2nd stage
(EPS)
2000-54 C
[26496]
2000 Sep 14.95
Drum+cone
1190
3.3 long
3.94 dia
2000 Sep 15.41
2005 Dec 29.07
6.87
6.85
642.92 24675
642.62 24668
576
575
36017
36003
0.718
0.718
178
165
Sylda-5
2000-54 D
[26497]
2000 Sep 14.95
Hollow cone
900
4.56 dia
4.90 high
2000 Sep 15.40
2005 Dec 28.64
7.01
6.97
644.38 24713
635.08 24475
578
557
36091
35635
0.718
0.717
179
189
NOAA 16 %
[Titan 23G-13
/Star 37XFP]
2000-55 A
[26536]
VDB-SLC4W
2000 Sep 21.43
Box+ panel
2234
4.2 long
1.9 dia
2000 Sep 21.62
2005 Dec 30.18
98.79
99.04
102.05 7234
101.95 7230
848
844
863
858
0.001
0.001
275
234
Fragments
2000-55 B-PW 357 pieces; 1 has decayed.
Fragments #
D
*
#
%
For orbital information see extra pages at end of year
Crew of seven astronauts (Willcutt, Altman, Lu, Mastracchio, Burbank, Malenchenko and Morukov) docked with ISS (Unity/PMA-2 port) 2000 Sep 10.24;
raised orbit of ISS and undocked 2000 Sep 18.16 and landed at Kennedy Space Center. On 2005 Sep 11 an EVA was performed to install cables on the ISS.
Not certain if fragments belong to Atlantis or ISS.
NOAA 16 suffered a possible break up on 2015 Nov 25.305 and 10 hours later 19 pieces of debris were detected close to NOAA 16.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-25
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 2372
[Zenit-2]
2000-56 A
[26538]
BAI-LC45/1
2000 Sep 25.42
207 days
2001 Apr 20
Cylindrical
+ 2 panels
12000
10 long
3.9 dia
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
2001
25.48
25.73
5.90
6.02
17.63
17.83
31.97
1.74
7.56
9.92
17.33
17.95
6.21
6.30
28.76
29.14
8.59
8.85
16.80
17.68
21.17
26.55
29.16
29.49
14.18
14.32
3.83
4.17
23.51
23.83
23.96
31.55
31.69
20.15
64.97
64.78
64.78
64.78
64.77
64.78
64.77
64.76
64.77
64.77
64.77
64.77
64.77
64.77
64.76
64.76
64.76
64.76
64.76
64.76
64.76
64.76
64.76
64.76
64.76
64.76
64.75
64.75
64.74
64.75
64.74
64.74
64.74
64.74
90.10
89.98
89.62
89.98
89.60
90.12
89.50
89.62
89.35
89.77
89.52
89.73
89.10
89.43
89.37
89.78
89.45
89.63
89.33
89.58
89.22
89.95
89.87
89.95
89.43
89.63
88.65
91.45
91.20
91.73
89.90
89.45
89.77
88.63
6658
6652
6634
6652
6633
6659
6629
6634
6621
6641
6629
6640
6608
6639
6621
6643
6626
6635
6620
6633
6614
6650
6646
6651
6625
6635
6586
6724
6712
6738
6648
6626
6642
6585
205
211
202
207
199
212
200
208
199
209
203
246
218
221
207
211
204
204
197
198
189
197
196
205
195
207
181
244
239
279
188
180
211
179
353
337
309
340
309
348
300
303
286
317
297
276
241
300
278
317
291
308
286
310
282
346
338
340
298
306
235
446
428
439
350
314
315
234
0.011
0.009
0.008
0.010
0.008
0.010
0.008
0.007
0.007
0.008
0.007
0.002
0.002
0.006
0.005
0.008
0.007
0.008
0.007
0.008
0.007
0.011
0.011
0.010
0.008
0.007
0.004
0.015
0.014
0.012
0.012
0.010
0.008
0.004
76
75
69
92
76
105
98
107
103
127
123
353
343
19
30
112
105
109
104
111
105
130
128
126
116
69
61
52
44
58
120
116
115
102
D
Zenit-2 2nd stage
2000-56 B
[26539]
2000 Sep 25.42
16.33 days
2000 Oct 11.75
Cylinder
8300
10.41 long
3.9 dia
2000 Sep 25.54
2000 Oct 3.39
2000 Oct 11.72
64.56
64.78
64.77
90.05 6656
89.42 6624
86.95 6502
265
196
120
289
295
126
0.002
0.007
0.0004
26
63
14
D
Separation
Motor cap
2000-56 C
[26540]
2000 Sep 25.42
29 days
2000 Oct 24
1
2000 Sep 25.82
2000 Oct 10.12
2000 Oct 13.48
64.73
64.71
64.73
92.67 6784
90.13 6660
88.58 6583
209
183
154
602
379
255
0.029
0.015
0.008
69
66
66
Separation
Motor cap
2000-56 D
[26541]
2000 Sep 25.42
17 days
2000 Oct 12
1
2000 Sep 25.82
2000 Oct 3.71
2000 Sep 9.53
64.84
64.84
64.82
92.52 6776
91.05 6704
88.53 6581
209
183
153
587
469
251
0.028
0.021
0.007
70
69
67
Separation
Motor cap
2000-56 E
[26542]
2000 Sep 25.42
13 days
2000 Oct 8
1
2000 Sep 25.82
2000 Oct 2.87
2000 Oct 8.50
2000-56 continued on next page
64.83
64.83
64.81
92.18 6760
91.08 6706
88.40 6574
206
195
153
556
460
238
0.026
0.020
0.006
89
87
85
D
D
2016 - Version 1.15
Sep
Sep
Oct
Oct
Oct
Sep
Oct
Nov
Nov
Nov
Nov
Nov
Dec
Dec
Dec
Dec
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Feb
Feb
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Apr
Nodal
period
(min)
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-26
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
D
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Separation
Motor cap
2000-56 F
[26543]
2000 Sep 25.42
16 days
2000 Oct 11
1
Fragments
2000-56 G
[26544]
2000 Sep 26
1 day
2000-56 H
[26748]
2001 Apr 21
208 days
D
Date of
orbital
determination
Orbital
Inclination
(deg)
2000 Sep 25.89
2000 Oct 3.77
2000 Oct 10.59
64.72
64.72
64.72
2000
2000
2001
2001
25.93
26.78
21.17
21.23
Sep
Sep
Apr
Apr
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
92.30 6766
91.12 6708
88.55 6581
207
188
158
568
470
247
0.027
0.021
0.007
89
87
79
64.79
64.86
64.66
64.62
89.77
88.17
89.08
88.53
6641
6562
6607
6580
190
117
147
132
335
251
311
271
0.011
0.010
0.012
0.011
76
28
107
111
Saudisat 1A
{Dnepr 1]
2000-57 A
2000 Sep 26.42
[26545]
BAI-LC109/95
Cube
10
0.23 side
2000 Sep 26.68
2005 Dec 30.18
64.56
64.56
97.48 7017
97.27 7007
634
588
642
668
0.0006
0.006
18
275
Megsat
2000-57 B
[26546]
2000 Sep 26.42
Cube
56
0.45 side
2000 Sep 26.68
2000 Sep 27.09
2005 Dec 29.55
64.56
64.56
64.56
97.67 7026
97.67 7025
97.02 6996
638
640
582
655
654
652
0.001
0.001
0.005
93
115
269
Unisat
2000-57 C
[26547]
2000 Sep 26.42
2000 Sep 26.68
2000 Sep 29.46
2005 Dec 29.56
64.56
64.56
64.56
97.33 7020
97.55 7020
97.17 7002
637
640
580
646
643
667
0.0006
0.0002
0.006
75
48
280
Tiungsat 1
2000-57 D
[26548]
2000 Sep 26.42
Box
52
2000 Sep 26.68
2000 Sep 29.06
2005 Dec 29.57
64.56
64.56
64.56
97.58 7022
97.67 7025
97.10 6998
637
640
583
649
654
656
0.0008
0.001
0.005
91
117
271
Saudisat 1B
2000-57 E
[26549]
2000 Sep 26.42
Cube
10
2000 Sep 26.62
2000 Sep 26.89
2005 Dec 28.49
64.56
64.56
64.56
97.60 7023
97.73 7028
97.35 7010
631
640
589
657
660
674
0.002
0.001
0.006
145
121
278
Dnepr 3rd stage
2000-57 F
[26550]
2000 Sep 26.42
2000 Sep 26.55
2005 Dec 29.90
64.57
64.56
104.47 7348
104.32 7343
585
579
1353
1349
0.052
0.052
130
25
Gas Dynamics
Shield
2000-57 G
[26551]
2000 Sep 26.42
2000 Sep 26.82
2005 Dec 28.84
64.56
64.54
97.70 7027
94.92 6893
631
489
666
541
0.002
0.004
51
266
2016 - Version 1.15
10
0.23 side
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-27
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 2373
(Yantar-1KFT)
[Soyuz-U 11A511U]
2000-58 A
[26552]
BAI-LC31
2000 Sep 29.40
45.55 days
2000 Nov 13.95
Stubby cyl
+sphere+cone
6600
6.6 long
2.7 maxdia
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
29.45
29.65
30.90
1.22
5.10
5.25
16.78
17.40
25.53
25.86
25.99
29.54
29.85
13.87
70.37
70.35
70.35
70.35
70.34
70.36
70.34
70.34
70.34
70.35
70.34
70.34
70.34
70.33
89.12
89.12
89.67
89.40
89.30
89.47
89.35
89.47
89.28
89.45
88.85
88.52
89.48
89.22
6610
6609
6637
6624
6618
6627
6621
6627
6618
6626
6596
6581
6628
6614
192
194
230
211
208
213
208
213
208
228
210
195
212
204
271
268
286
278
272
283
277
283
271
265
225
209
286
268
0.006
0.006
0.004
0.005
0.005
0.005
0.005
0.005
0.005
0.003
0.001
0.001
0.006
0.005
70
71
16
354
346
0
343
12
354
340
214
223
192
173
D
Soyuz-U 3rd stage
(Block I)
2000-58 B
[26553]
2000 Sep 29.40
3.03 days
2000 Oct 2.43
Cylinder
2400
8.1 long
2.66 dia
2000 Sep 29.45
2000 Sep 2.34
70.34
70.35
89.03 6605
87.27 6517
206
130
246
147
0.003
0.001
135
78
NSS 11
(AAP-1, GE-1A) #
[Proton-8K82K
DM3 401-01]
2000-59 A
[26554]
BAI-LC81/23
2000 Oct 1.92
> million years
Box+ 2 panels
3800
3.1x2.5
x6.1
27 span
2000
2000
2000
2000
2000
2000
2000
2000
2005
48.54
15.98
9.84
5.24
4.65
2.50
0.05
0.08
0.04
210
7247
12349
19379
20941
26158
35768
35777
35781
35715
34906
35813
35758
35758
35767
35775
35796
35792
0.729
0.504
0.385
0.241
0.213
0.129
0.00009
0.0002
0.0001
0
358
1
0
1
2
81
234
13
D
Proton-K 3rd stage
(8S812)
2000-59 B
[26555]
2000 Oct 1.92
1.63 day
2000 Oct 3.55
Cylinder
4185
4 long
4.1 dia
2000 Oct 2.09
2000 Oct 3.25
51.60
51.60
88.22 6565
87.00 6505
151
113
221
139
0.005
0.002
288
268
D
Proton-K 4th stage
Casing
2000-59 C
[26556]
2000 Oct 1.92
0.54 day
2000 Oct 2.46
Hollow cyl
800
4.0 long
3.7 dia
2000 Oct 2.09
2000 Oct 2.45
51.59
51.57
88.23 6566
87.57 6532
165
63
209
244
0.003
0.014
277
291
Proton-K 4th stage
(Block-DM3)
2000-59 D
[26557]
2000 Oct 1.92
Cylinder
2140
6.22 long
3.7 dia
2000 Oct 2.43
2005 Dec 31.52
15.94
14.23
776.50 27985
771.55 27866
7393
7399
35819
35576
0.508
0.506
359
25
#
Renamed to AAP-1; reneamed to NSS 11 when SES and New Skies Satellite merged.
2016 - Version 1.15
Sep
Sep
Sep
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Nov
Nodal
period
(min)
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Dec
1.97
2.46
3.52
5.28
7.44
8.17
11.47
16.63
30.60
89.88
754.55
881.73
1037.42
1073.43
1196.85
1435.35
1436.12
1436.12
24341
27455
30459
33947
34728
37341
42150
42165
42165
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-28
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
D
#
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Dec
Nodal
period
(min)
Orbital
Argument
eccentricity of perigee
(deg)
194
9192
20104
26226
35562
35789
35774
35782
35783
36886
35743
35738
35757
35749
35801
35791
35790
35790
0.736
0.460
0.228
0.128
0.002
0.0001
0.0002
0.0001
0.00008
180
180
177
175
298
355
322
3
54
2000 Oct 6.96
> million years
Box+ 2 panels
3531 (launch)
1669 (dry)
6.0 high
26.4 span
2000
2000
2000
2000
2000
2000
2000
2000
2005
7.15
9.00
10.15
11.65
13.70
18.62
23.31
24.71
30.60
7.16
2.21
1.03
0.53
0.07
0.01
0.01
0.06
0.03
Ariane-4 2nd stage
(H-10-3) + VEB
2000-60 B
[26560]
2000 Oct 6.96
1528 days
2004 Dec 12
Cylinder
1670+750
11.05 long
2.6 dia
1.03 high
4.0 dia
2000 Oct 6.76
2002 Nov 1.63
2004 Dec 12.67
6.98
7.93
7.89
630.80 24364
395.17 17838
88.35 6572
216
177
100
35755
22742
286
0.729
0.633
0.014
178
315
221
HETE 2 *
[L-1011/Pegasus
H F30/P-35]
2000-61 A
[26561]
KWA-RW06
2000 Oct 9.23
Box+ 4 panels
124
0.66x0.66
x0.89
~2.5 span
2000 Oct 9.28
2005 Dec 31.04
1.96
1.95
97.02 6994
96.30 6960
595
564
636
598
0.003
0.002
109
42
Pegasus 3rd stage
2000-61 B
[26562]
2000 Oct 9.23
Cone-cyl
176
2.08 long
0.97 dia
2000 Oct 9.28
2004 Mar 20.93
1.96
1.96
96.98 6993
96.28 6959
595
565
633
596
0.003
0.002
105
196
2000-62 A
[26563]
CC-LC39A
2000 Oct 11.97
12.91 days
2000 Oct 24.88
Delta wing
92740
37.5 long
5.5 dia
23.8 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
51.57
51.57
51.57
51.57
51.58
51.58
51.58
51.57
51.57
89.30
89.78
91.40
92.12
92.15
92.22
92.27
92.23
92.23
158
179
311
375
379
381
381
379
378
322
349
375
381
381
385
391
389
389
0.012
0.013
0.005
0.0005
0.0001
0.0003
0.0007
0.0008
0.0008
11
29
104
326
332
67
79
56
60
12.00
12.38
13.00
13.92
16.96
18.00
19.25
20.66
24.25
24919
28846
34300
37370
42034
42173
42161
42165
42165
Apogee
height
(km)
2000-60 A
[26559]
KOU-ELA2
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Oct
652.43
812.60
1053.63
1198.23
1429.42
1436.53
1435.90
1436.10
1436.12
Perigee
height
(km)
N-sat 110
(Superbird 5)
[Ariane-42L]
(V133)
D STS-92 #
7M Discovery F28
R [Shuttle]
*
Cospar ID
[Norad #] Launchsite
Cospar ID
6619
6643
6722
6757
6759
6762
6764
6763
6763
Replacement for High Energy Transient Experiment which remained attached to Pegasus 3rd stage (1996-61 A). First launch from airplane that took off
from Kwajalein Atoll in the Pacific Ocean. Pegasus dropped at 7.65ºN, 167.7ºE.
The 100th flight of the shuttle with a crew of seven astronauts (Duffy, Melroy, Chiao, Wakata, Wisoff, Lopez-Alegria and McArthur) docked with ISS
(Unity/PMA-2 port) 2000 Oct 13.70; installed Z-1 truss on Unity and the PMA-3 to Unity. Also installed 2 Control Moment Gyros.
Undocked 2000 Oct 20.63 and landed at Edwards AFB.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-29
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 2375 $
[Proton-8K82K
DM2 393-01]
2000-63 A
[26564]
BAI-LC81/24
2000 Oct 13.59
1 million years
Cylindrical
+ 2 panels
1400
2.4 dia
3.7 high
7.23 span
2000
2000
2000
2000
2005
Oct
Oct
Oct
Oct
Dec
13.86
14.54
21.18
24.86
31.70
64.84
64.85
64.83
64.82
64.54
676.08
675.53
676.65
675.72
675.73
25517
25503
25531
25508
25508
19125
19122
19125
19124
19115
19152
19127
19180
19134
19144
0.0005
0.0001
0.001
0.0002
0.0006
213
301
48
15
40
Cosmos 2376 $
2000-63 B
[26565]
2000 Oct 13.59
1 million years
Cylindrical
+ 2 panels
1400
2.4 dia
3.7 high
7.23 span
2000
2000
2000
2000
2005
Oct
Oct
Nov
Nov
Dec
13.60
28.76
4.13
6.01
30.70
64.83
64.84
64.84
64.81
64.54
675.42
669.20
675.60
675.72
675.73
25500
25344
25505
25508
25508
19119
18799
19114
19125
19124
19125
19131
19138
19133
19134
0.0001
0.007
0.0005
0.0002
0.0002
201
237
238
303
27
Cosmos 2374 $
2000-63 C
[26566]
2000 Oct 13.59
1 million years
Cylindrical
+ 2 panels
1400
2.4 dia
3.7 high
7.23 span
2000
2000
2000
2000
2005
Oct
Oct
Nov
Dec
Dec
13.89
14.07
4.31
1.24
30.55
64.80
64.80
64.78
64.79
64.52
675.72
675.55
677.53
675.73
675.73
25508
25504
25554
25508
25508
19122
19122
19120
19034
19016
19136
19128
19231
19225
19243
0.0003
0.0001
0.002
0.004
0.004
195
169
234
234
218
D
Proton-K 4th stage
Casing
2000-63 D
[26567]
2000 Oct 13.59
2 days
2000 Oct 15
Hollow cyl
800
4.0 long
3.7 dia
2000 Oct 13.83
64.80
87.28 6518
128
151
0.002
9
D
Proton-K 3rd stage
(8S812)
2000-63 E
[26568]
2000 Oct 13.59
2 days
2000 Oct 15
Cylinder
4185
4 long
4.1 dia
2000 Oct 13.77
2000 Oct 14.32
64.84
64.84
87.43 6526
87.43 6526
141
141
154
154
0.001
0.001
260
260
Proton-K 4th stage
(Block DM-2M)
2000-63 F
[26569]
2000 Oct 13.59
> million years
Cylinder
2350
6.22 long
3.7 dia
2000 Oct 13.86
2005 Dec 30.42
64.82
64.54
774.73 25483
674.70 25482
19084
19082
19124
19125
0.0008
0.0008
295
348
D
Ullage motor
2000-63 G
[26573]
2000 Oct 13.59
2634 days
2007 Dec 30
Cylinder
55
0.90 long
0.68 dia
2000 Oct 18.84
2005 Dec 30.13
2007 Dec 30.31
64.79
64.43
63.69
340.22 16144
338.68 16095
87.97 6552
406
265
102
19124
19169
246
0.580
0.587
0.011
297
219
202
D
Ullage motor
2000-63 H
[26574]
2000 Oct 13.59
2463 days
2007 Jul 12
Cylinder
55
0.90 long
0.68 dia
2000 Oct 18.84
2005 Dec 31.05
2007 Jul 12.03
64.86
64.47
63.82
340.05 16138
338.13 16078
87.50 6530
401
246
100
19118
19152
252
0.580
0.588
0.008
297
217
210
$
Triple Glonass payload.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-30
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Progress-M 43 *
{Soyuz-U 11A511U
K15000-085]
2000-64 A
[26570]
BAI-LC1
2000 Oct 16.89
104.23 days
2001 Jan 29.12
Cyl+ 2 panels+ 7.9 long
beehive+sphere 2.3 to
6860
2.72 dia
2000
2000
2000
2000
2000
2000
2001
16.91
18.39
20.11
20.87
21.21
25.04
29.05
51.65
51.65
51.64
51.65
51.65
51.65
51.64
88.62
89.60
90.70
91.13
91.13
91.42
90.02
6585
6634
6688
6709
6709
6723
6654
189
188
282
326
325
330
271
222
322
336
335
335
358
280
0.003
0.01
0.004
0.0007
0.0008
0.002
0.0007
74
60
132
173
170
292
91
D
Soyuz-U 3rd stage
(Block I)
2000-64 B
[26571]
2000 Oct 16.89
1.45 day
2000 Oct 18.34
Cylinder
2300
2000 Oct 16.95
2000 Oct 18.23
51.65
51.64
88.65 6586
87.37 6522
189
138
227
149
0.003
0.0008
78
62
DSCS-3B 8
(USA 153)
[Atlas-2A]
2000-65 A
[26575]
CC-LC36A
2000 Oct 20.03
> million years
Box + 2 panels 1.93 x 1.96 No elements available; orbits from amateur observations.
1175
x 2.06
2010 Jun 21.50
0.93
1436.07 42164 35754 35817
11.62 span
0.0007
54
Atlas-2A 2nd stage
(Centaur AC-140)
2000-65 B
[26576]
2000 Oct 20.03
1303 days
2004 May 15
Cylinder
1815
10.1 long
3.05 dia
2000 Oct 19.83
2002 Jul 30.53
2004 May 15.68
0.726
0.631
0.016
176
29
17
IABS
2000-65 C
[26577]
2000 Oct 20.03
Cylindrical
272
2.9 dia
0.69 high
In near-geosynchronous orbit
No elements available
D
*
8.1 long
2.66 dia
Docked with MIR (Kvant 1 port) 2000 Oct 20.89; undocked 2001 Jan 25.22.
2016 - Version 1.15
Oct
Oct
Oct
Oct
Oct
Oct
Jan
Nodal
period
(min)
26.04
26.09
25.97
620.68 24104
393.82 17798
88.93 6601
218
180
115
35232
22658
329
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-31
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital
Argument
eccentricity of perigee
(deg)
231
4706
8269
16682
34380
33812
35740
35682
35738
35744
35766
35807
35774
35744
35751
35769
40166
35827
35828
35830
35829
35807
0.729
0.584
0.484
0.293
0.017
0.073
0.001
0.002
0.001
0.001
0.0005
49
57
101
55
41
354
331
327
327
214
291
150
161
106
35762
27156
1464
0.732
0.674
0.095
49
350
97
224
5974
10005
18761
28604
35749
35766
35750
35778
35783
35739
35774
35767
35760
35773
35849
35873
35756
35795
35790
0.729
0.547
0.440
0.253
0.093
0.001
0.001
0.00007
0.0002
0.00008
0
0
0
1
2
290
201
166
229
240
2000 Oct 21.24
> million years
Box+ 2 panels
5108
3.75x3.75
x7.6
34.5 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
21.44
24.66
26.78
28.57
31.34
3.85
8.67
10.22
13.94
7.89
30.59
6.44
5.73
5.18
5.87
6.37
6.11
6.26
6.25
6.25
6.20
3.33
Zenit-3 3rd stage
(Block DM-SL)
2000-66 B
[26579]
2000 Oct 21.24
1315 days
2004 May 28
Cylinder
2140
6.22 long
3.7 maxdia
2000 Oct 21.43
2002 Jul 30.57
2004 May 22.82
6.36
6.17
5.93
AMC 6 (GE-6)
[Proton-8K82K
DM3 402-01]
2000-67 A
[26580]
BAI-LC81/23
2000 Oct 21.92
> million years
Box+ 2 panels
3800
3.1x2.5
x6.1
27 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
2005
21.97
22.57
24.18
26.89
29.08
31.01
31.47
2.24
4.74
29.15
48.75
18.68
12.39
5.56
1.76
0.03
0.03
0.03
0.02
0.05
D
Proton-K 3rd stage
(8S812)
2000-67 B
[26581]
2000 Oct 21.92
1.56 day
2000 Oct 23.48
Cylinder
4185
4 long
4.1 dia
2000 Oct 22.15
2000 Oct 23.43
51.59
51.56
88.22 6565
87.05 6507
156
109
217
148
0.005
0.003
267
282
D
Proton-K 4th stage
Casing
2000-67 C
[26582]
2000 Oct 21.92
0.58 day
2000 Oct 22.49
Hollow cyl
800
4.0 long
3.7 dia
2000 Oct 22.15
2000 Oct 22.40
51.59
51.58
88.25 6566
87.63 6536
168
148
207
166
0.003
0.001
271
280
Proton-K 4th stage
(Block-DM3)
2000-67 D
[26583]
2000 Oct 21.92
Cylinder
2140
6.22 long
3.7 dia
2000 Oct 22.45
2005 Dec 30.66
18.64
16.96
742.25 27156
742.82 27169
5832
5837
35723
35745
0.550
0.550
0
84
Europestar 1
[Ariane-44LP]
(V134)
2000-68 A
[26590]
KOU-ELA2
2000 Oct 29.25
> million years
Box+ panels
4167 full
1717 empty
2.7x3.5
x5.5
24.7 span
2000
2000
2000
2000
2000
2000
2005
29.04
2.77
3.86
3.88
11.76
12.83
29.41
6.98
0.21
0.12
0.04
0.01
0.01
0.04
180
34616
35936
35685
35749
35779
35776
37121
35720
38831
35758
35825
35794
35796
0.738
0.013
0.033
0.0009
0.0009
0.0002
0.0002
178
1
179
338
302
16
21
Ariane-4 3rd stage
(H-10-3) + VEB
2000-68 B
[26591]
2000 Oct 29.25
Cylinder
1670+520
11.05 long
2.6 dia
+1.03x4.0
2000 Oct 29.04
2005 Dec 31.00
6.85
6.51
173
298
35805
32817
0.731
0.709
177
350
2016 - Version 1.15
Oct
Nov
Nov
Nov
Nov
Nov
Dec
24397
26618
28385
32595
41453
43367
42162
42133
42162
42165
42165
Apogee
height
(km)
2000-66 A
[26578]
ODS
Oct
Oct
Oct
Oct
Oct
Oct
Oct
Nov
Nov
Dec
632.07
720.32
793.22
976.07
1399.88
1497.97
1435.95
1434.50
1435.97
1436.12
1436.12
Perigee
height
(km)
Thuraya 1
[Zenit-3/DM-SL 5]
D
Oct
Oct
Oct
Oct
Oct
Nov
Nov
Nov
Nov
Dec
Dec
Nodal
period
(min)
629.63 24335
470.45 20038
100.57 7164
630.63
746.23
830.38
1023.35
1256.25
1436.73
1437.78
1434.38
1436.10
1436.13
656.78
1404.62
1518.47
1432.80
1436.13
1436.10
1436.08
24360
27253
29265
33639
38567
42177
42198
42131
42165
42165
25029
41546
43762
42100
42166
42165
42165
630.92 24367
576.15 22936
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-32
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
197
35772
35766
41857
35801
35806
0.760
0.0003
0.0005
180
154
251
198
126
95
41882
38498
398
0.760
0.747
0.023
180
215
331
Bei Dou 1
[CZ-3A 5(63)]
2000-69 A
[26599]
XI-LC2
2000 Oct 30.67
> million years
Box+ 2 panels
2300
2.2x1.72
x2.0
18.1 span
2000 Oct 30.76
2000 Nov 9.75
2005 Dec 30.53
25.00
0.17
0.01
752.50 27405
1436.12 42165
1436.08 42165
CZ-3A 3rd stage
(H-18)
2000-69 B
[26600]
2000 Oct 30.67
112.11 days
2001 Feb 19.78
Cylinder
2300
8.84 long
3 dia
2000 Oct 30.75
2000 Dec 31.90
2001 Feb 19.53
24.99
25.18
24.82
753.05 27418
753.00 25691
89.43 6625
D Soyuz-TM 31 *
3M [Soyuz-U 11A511U
R A15000-666]
2000-70 A
[26603]
BAI-LC1
2000 Oct 31.33
186.91 days
2001 May 6.24
Cyl+2 panels+ 7.5 long
beehive+sphere 2.3 to
7150
2.72 dia
2000
2000
2000
2001
31.38
31.57
10.05
4.87
51.66
51.58
51.57
51.57
88.65
89.67
92.18
92.37
6586
6636
6760
6769
184
246
377
379
230
270
385
402
0.004
0.002
0.0006
0.002
104
127
167
11
Soyuz-U 3rd stage
(Block I)
2000-70 B
[26604]
2000 Oct 31.33
1.26 day
2000 Nov 1.58
Cylinder
2300
8.1 long
2.66 dia
2000 Oct 31.50
2000 Nov 1.54
51.67
51.65
88.48 6578
87.22 6515
181
129
218
143
0.003
0.001
109
130
Navstar 49
2000-71 A
(USA 154, GPS-2R) [26605]
[Delta-2 (7925-9.5) CCLC17A
#281]
2000 Nov 10.72
1 million years
Box+ 2 panels
2032
1.52x1.93
x1.93
19.3 span
2000
2000
2000
2000
2006
10.97
12.63
24.88
2.40
2.15
39.41
55.07
55.09
55.09
56.42
106
20177
20112
20106
20113
20457
20497
20416
20271
20249
0.611
0.006
0.006
0.003
0.003
196
10
343
327
246
D
Delta-2 2nd stage
2000-71 B
[26606]
2000 Nov 10.72
90.08 days
2001 Feb 8.80
Cylinder
919
5.88 long
2.44 dia
2000 Nov 10.83
2000 Dec 25.81
2001 Feb 8.75
37.57
37.56
37.50
89.93 7134
86.18 6954
87.30 6519
196
187
92
1315
964
189
0.078
0.056
0.007
175
158
158
D
Delta-2 3rd stage
(PAM-D)
2000-71 C
[26607]
2000 Nov 10.72
1525 days
2005 Jan 13
Cone-cyl
205
2.29 long
1.5 dia
2000 Nov 10.83
2002 Jul 1.42
2005 Jan 13.63
39.14
39.02
38.79
354.90 16605
253.62 13273
88.07 6557
179
177
117
20274
13611
240
0.605
0.506
0.009
194
129
222
PAS 1R
[Ariane-5G (507))
(V135)
2000-72 A
[26608]
KOU-ELA3
2000 Nov 16.05
> million years
Box+ 2 panels
4793 launch
3000 dry
3.5x3.5
x6.2
40.95 span
2000
2000
2000
2000
2000
2000
2000
2000
2001
2001
2006
6.47
3.16
1.04
0.19
0.18
0.16
0.14
0.14
0.06
0.06
0.02
623
5486
20367
31593
32388
32596
33845
34321
35785
35779
35785
39353
39060
39086
39080
39072
39003
37730
37223
35790
35793
35788
0.734
0.586
0.259
0.090
0.079
0.076
0.046
0.034
0.00006
0.0002
0.00003
176
178
171
139
146
154
146
143
17
33
339
D
Oct
Oct
Nov
May
Nov
Nov
Nov
Dec
Jan
Nov
Nov
Nov
Nov
Nov
Dec
Dec
Dec
Jan
Jan
Jan
16.33
19.76
22.80
26.00
27.94
4.98
11.95
19.93
18.54
19.21
3.83
356.67
724.28
721.30
718.25
717.93
710.12
804.42
1137.92
1413.18
1433.22
1436.78
1436.17
1435.37
1436.17
1436.10
1436.12
16660
26716
26642
26567
26559
26366
28652
36105
41715
42108
42178
42166
42151
42166
42165
42165
2000-72 continued on next page
*
Expedition 1 crew (Shepard, Krikalev and Gidzenko) docked with ISS (Zvezda port) 2000 Nov 2.39; undocked 2001 Feb 24.42 and re-docked to the
Zarya nadir port 2001 Feb 24.44; returned to earth in STS-102 Discovery 2001 Mar 21.31 after 160.98 days. Soyuz-TM 31 undocked from ISS (Zarya nadir port
2001 Apr 18.53 with Expedition 2 crew and re-docked to Zvezda port 2001 Apr 18.54; Undocked from ISS Zvezda port 2001 May 6.10 with crew of
Musabayev, Baturin and Tito (launched on Soyuz-TM 32) and landed in Kazachstan.
2016 - Version 1.15
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-33
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Orbital
Argument
eccentricity of perigee
(deg)
610
557
364
344
1194
39254
59257
58869
58981
58627
0.734
0.809
0.813
0.813
0.791
178
192
195
199
118
2000-72 B
[26609]
2000 Nov 16.05
6 sided cyl
630
397 dry
2.23 across 2000 Nov 18.28
0.68 high
2000 Dec 11.67
6 span
2000 Dec 17.43
2000 Dec 28.43
2006 Jan 2.97
6.44
6.42
6.30
6.04
7.39
STRV 1C
2000-72 C
[26610]
2000 Nov 16.05
Cube
100
0.7 side
2000 Nov 18.29
2005 Dec 31.34
6.43
7.19
708.38 26323
707.77 26308
614
598
39276
39261
0.734
0.735
177
322
STRV 1D
2000-72 D
[26611]
2000 Nov 16.05
Cube
100
0.7 side
2000 Nov 20.74
2006 Jan 2.14
6.42
7.18
708.38 26323
708.23 26320
613
591
39277
26320
0.734
0.735
179
322
Ariane-5 2nd stage
(EPS) +VEB
2000-72 E
[26612]
2000 Nov 16.05
Drum-cone
1190
3.36 long
5.46 dia
2000 Nov 16.33
2006 Jan 2.27
6.44
7.27
704.13 26218
713.95 26461
617
600
39062
39565
0.733
0.736
176
306
Sylda-5 upperpart
2000-72 F
[26613]
2000 Nov 16.05
Hollow cone
900
4.56 dia
4.90 high
2000 Nov 18.29
2006 Jan 3.24
6.43
7.21
710.07 26365
709.70 26356
617
593
39356
39362
0.735
0.735
177
319
D
Progress-M1 4 #
[Soyuz-U 11A511U
K15000-671]
2000-73 A
[26615]
BAI-LC1
2000 Nov 16.06
84.52 days
2001 Feb 8.58
Cyl+2 panels+ 7.9 long
beehive+sphere 2.3 to
7280
2.72 dia
2000
2000
2000
2000
2000
2000
2000
2001
16.30
18.37
1.92
20.40
20.77
25.56
26.38
4.07
51.58
51.57
51.58
51.58
51.57
51.58
51.57
51.57
89.80
92.15
92.08
91.95
92.08
91.82
91.93
91.70
6643
6759
6755
6749
6755
6742
6748
6737
259
377
374
367
372
356
364
351
270
383
379
374
382
371
374
365
0.0008
0.0005
0.0003
0.0005
0.0007
0.001
0.0008
0.001
184
198
252
341
282
152
276
67
D
Soyuz-U 3rd stage
(Block I)
2000-73 B
[26616]
2000 Nov 16.06
1.77 day
2000 Nov 17.83
Cylinder
2300
8.1 long
2.66 dia
2000 Nov 16.25
2000 Nov 17.77
51.64
51.62
88.52 6580
87.00 6505
186
120
217
131
0.002
0.0008
89
101
D
Quickbird 1 *
2000-74 A
[Kosmos-3M
[26617]
47165-631]
PLE-LC132/1
plus
Kosmos 3M 2nd stage
2000 Nov 20.96
0.05 day
2000 Nov 21.01
Box+ 2 panels
+ cylinder
931
+ 1434
1.6 dia
3.0 high
5.2 span
4.21 long
2.4 to
3.2 dia
2000 Nov 20.95
2000 Nov 20.98
65.78
65.78
91.50 6726
91.40 6722
81
77
614
610
0.040
0.040
358
358
#
*
$
Docked with ISS (Zarya nadir port) 2000 Nov 18.13; undocked 2000 Dec 1.68; re-docked 2000 Dec 26.45 to Zarya nadir port. Undocked 2001 Feb 8.48.
Satellite didn’t separate from 2nd stage; due to timer malfunction (launch was delayed 1 hour and timer not reset) solar panels opened early.
Satellite de Aplicaciones Cientificas.
2016 - Version 1.15
26311
36286
35995
36041
36289
Apogee
height
(km)
Amsat P-3D
(Oscar 40)
Nov
Nov
Dec
Dec
Dec
Dec
Dec
Feb
707.87
1146.47
1132.73
1134.90
1146.63
Perigee
height
(km)
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-34
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Semi
major axis
(km)
Earth Observing 1 2000-75 A
[Delta-2 (7320-10) [26619]
#282]
VDB-SLC2W
2000 Nov 21.77
Box
573
1.73 across 2000
1.75 high
2000
2000
2000
2000
2000
2000
2006
Nov
Nov
Nov
Dec
Dec
Dec
Dec
Jan
21.81
22.70
30.80
9.74
11.32
11.39
15.92
4.16
98.28
98.20
98.21
98.22
98.22
98.22
98.21
98.18
98.88
98.75
99.02
98.93
98.78
98.82
98.82
98.67
SAC C $
2000-75 B
[26620]
2000 Nov 21.77
Box+ 2 panels
475
2.1x1.9
x1.7
Nov
Nov
Nov
Feb
Jan
21.81
22.31
27.70
7.20
2.98
98.23
98.21
98.29
98.28
98.08
98.82
98.72
98.55
98.63
98.87
Munin
2000-75 C
[26621]
2000 Nov 21.77
2000 Nov 22.19
2006 Jan 2.73
2000-75 D
[26622]
2000 Nov 21.77
Cylinder
919
DPAF (Dual Payload 2000-75 E
Attachment Fairing) [26623]
Upper part
2000 Nov 21.77
Hollow cyl
186
Fragment
2000-75 F
[29363]
Anik-F 1
[Ariane-44L]
(V136 #101)
2000-76 A
[26624]
KOU-ELA2
2000 Nov 22.00
> million years
Box+ 2 panels
4852
2950 dry
Ariane-4 3rd stage
(H-10-3) + VEB
2000-76 B
[26625]
2000 Nov 22.00
Cylinder
1250 +
Cylinder
520
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Delta-2 2nd stage
2016 - Version 1.15
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7084
7078
7090
7086
7079
7081
7081
7074
682
691
704
702
697
700
701
693
729
707
719
712
704
704
703
696
0.003
0.001
0.001
0.0007
0.0005
0.0003
0.0002
0.0002
347
235
176
178
47
90
120
349
7081
7075
7068
7072
7083
693
687
672
679
703
711
707
706
707
705
0.001
0.001
0.002
0.002
0.0001
313
233
257
41
96
95.45
95.42
110.48 7627
110.45 7626
696
700
1801
1795
0.072
0.072
162
41
2000 Nov 21.81
2000 Nov 22.19
2006 Jan 3.33
98.22
95.45
95.44
98.77 7078
110.50 7628
110.42 7325
692
693
696
708
1806
1796
0.001
0.073
0.072
223
162
38
2000 Nov 21.81
2006 Jan 4.09
98.22
98.04
98.73 7077
97.55 7020
688
633
707
649
0.001
0.001
230
67
2006 Aug 26.87
95.41
109.38 7577
689
1707
0.067
123
3.50x3.30
x6.24
45.6 span
2000
2000
2000
2000
2000
2000
2000
2001
2001
2001
2006
22.08
29.36
3.84
4.87
5.92
6.23
30.01
9.19
19.00
22.99
3.47
5.95
2.97
0.20
0.13
0.16
0.15
0.21
0.11
0.08
0.08
0.06
267
6156
28275
29477
29609
29575
31651
34265
35784
35784
35776
38178
41220
41244
41231
41227
41223
40078
37498
35791
35789
35796
0.740
0.583
0.158
0.141
0.139
0.139
0.100
0.038
0.00007
0.00007
0.0002
176
181
166
330
173
175
177
203
160
99
128
11.05 long
2.6 dia
4.0 dia
1.03 high
2000 Nov 22.05
2001 Dec 24.18
2002 Jan 25.15
5.99
6.32
6.26
250
126
108
38120
10810
572
0.741
0.451
0.035
176
293
136
6
5.88 long
2.44 dia
Date of
orbital
determination
2000
2000
2000
2001
2006
Nov
Nov
Dec
Dec
Dec
Dec
Dec
Jan
Jan
Jan
Jan
Orbital
Inclination
(deg)
Nodal
period
(min)
679.42
864.73
1383.97
1434.07
1437.30
1436.37
1440.10
1440.98
1436.17
1436.10
1436.08
25601
30067
41138
41732
41796
41778
42243
42261
42166
42165
42165
677.95 25564
213.85 11846
91.33 6719
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-35
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Semi
major axis
(km)
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
Orbital
Argument
eccentricity of perigee
(deg)
6183
12538
23518
24332
24491
24483
47091
47084
47087
47196
47074
47087
0.620
0.477
0.283
0.271
0.268
0.268
270
270
270
268
270
270
2000 Nov 30.83
> million years
Box+ 2 panels
3800
5.2x5.6
24.8 span
2000
2000
2000
2000
2000
2006
30.92
3.64
6.50
8.48
13.79
2.97
63.39
63.42
63.40
63.39
63.39
63.43
D
Proton-K 3rd stage
(8S812)
2000-77 B
[26627]
2000 Nov 30.83
0.58 day
2000 Dec 1.41
Cylinder
4185
4 long
4.1 dia
2000 Nov 30.83
2000 Dec 1.25
64.83
64.84
88.47 6577
87.28 6519
191
125
206
155
0.001
0.002
52
3
D
Proton-K 4th stage
Casing
2000-77 C
[26628]
2000 Nov 30.83
0.58 day
2000 Dec 1.41
Hollow cyl
800
4.0 long
3.7 dia
2000 Dec 1.01
2000 Dec 1.37
64.84
64.86
87.53 6531
86.88 6498
139
112
166
127
0.002
0.001
29
277
Proton-K 4th stage
(Block-DM3)
2000-77 D
[26629]
2000 Nov 30.83
Cylinder
2140
6.22 long
3.7 dia
2000 Nov 30.92
2006 Jan 1.78
63.41
63.30
994.97 33014
989.02 32883
6181
6495
47091
46513
0.620
0.608
271
272
2000-78 A
[26630]
CC-LC39B
2000 Dec 1.14
10.84 days
2000 Dec 11.96
Delta wing
89757
37.5 long
5.5 dia
23.8 span
2000
2000
2000
2000
2000
2000
2000
2000
2000
51.58
51.58
51.59
51.58
51.58
51.57
51.58
51.57
51.57
88.52
89.70
89.78
90.65
92.08
92.02
91.98
91.72
91.70
6580
6638
6642
6685
6755
6752
6750
6737
6737
81
197
205
238
374
368
365
352
351
321
322
322
374
379
378
378
365
365
0.018
0.009
0.009
0.010
0.0004
0.0008
0.001
0.0009
0.001
16
10
10
52
263
209
203
349
355
Floating Potential 2000-78 B
Probe **
[28896]
2000 Dec 1.14
6 sides box
+ 3 panels
27
2005 Nov 7.96
2006 Jan 4.22
51.64
51.65
91.38 6721
90.67 6686
338
305
346
310
0.0006
0.0003
89
146
D
EROS-A1
[Start-1]
2000-79 A
[26631]
SVO-LC5
2000 Dec 5.52
5692.62 days
2016 Jul 7.14
Box+ 2 panels
250
0.7 to 1.2
across
2.3 high
2000 Dec 5.52
2006 Jan 4.14
2016 Jul 7.05
97.32
97.40
97.52
94.58 6877
94.47 6871
87.23 6516
491
489
123
506
496
151
0.001
0.0005
0.002
117
54
337
D
Start-1 5th stage
2000-79 B
[26632]
2000 Dec 5.52
1138 days
2004 Jan 17
Drum
100
0.5 long
1.5 dia
2000 Dec 5.58
2004 Jan 17.45
97.32
97.12
94.57 6876
87.18 6514
491
133
503
137
0.0008
0.0003
121
213
*
1.14
1.16
1.29
2.25
2.84
9.58
9.85
10.25
11.58
33016
36190
41681
42143
42161
42164
Apogee
height
(km)
2000-77 A
[26626]
BAI-LC81/23
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
995.03
1141.93
1411.45
1434.97
1435.92
1436.05
Perigee
height
(km)
Sirius SR-3
[Proton-8K82K
DM3 402-02]
D STS-97
5M Endeavour F15
R [Shuttle]
Nov
Dec
Dec
Dec
Dec
Jan
Nodal
period
(min)
Docked with ISS (Unity/PMA-3 nadir port) 2000 Dec 2.83 with 5 astronauts (Jett, Bloomfield, Tanner, Garneau and Noriega); installed P6 solar arrays
atop Z-1 truss; arrays, wide 11.4 m, span 73 m when deployed. Undocked 2000 Dec 9.80 and landed at KSC.
** Removed from P6 Solar arrays Truss during space walk by McArthur and Tokarev during STS-114. Tossed into space by McArthur 2005 Nov 7.805
2016 - Version 1.15
Year of Launch 2000
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
USA 155
(Great Bear)
[Atlas-2AS]
2000-80 A
[26635]
CC-LC36A
Launchdate
Lifetime + Descent date
[Norad]
RAE Table of Earth Satellites (extended)
(Compiled 2006)
Page 2000-36
Shape and
weight (kg)
Descent date
Semi
major axis
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Size
(m)
Lifetime
2000 Dec 6.12
> million years
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Perigee
height
(km)
Apogee
height
(km)
No elements available; orbit from amateur observations.
2009 Apr 6.61
2.79
1436.13 42165 35743 35831
0.001
131
Atlas-2AS 2nd stage 2000-80 B
(Centaur AC-157)
[26636]
2000 Dec 6.12
Cylinder
1815
10.1 long
3.05 dia
Geosynchronous transfer orbit
No elements available
Astra-2D
[Ariane-5G (508)]
(V138)
2000-81 A
[26638]
KOU-ELA3
2000 Dec 20.02
> million years
Cylinder
1414
2.17 dia
8 high
(deployed)
2000
2000
2000
2000
2001
2005
Dec
Dec
Dec
Dec
Jan
Dec
20.04
20.69
22.44
28.11
6.92
28.85
2.00
1.98
2.18
0.30
0.23
0.07
630.57
629.70
633.82
1436.23
1436.10
1436.08
24359
24336
24442
42168
42165
42165
185
216
292
35785
35761
35774
35775
35699
35835
35793
35812
35798
0.731
0.729
0.727
0.0001
0.0006
0.0003
178
178
177
350
291
182
AMC-8
(GE 8, Aurora 3)
2000-81 B
[26639]
2000 Dec 20.02
> million years
Box+ 2 panels
2015
919 dry
3.6x4.1
14.50 span
2000
2000
2000
2000
2000
2006
Dec
Dec
Dec
Dec
Dec
Jan
20.70
24.70
28.70
29.13
29.80
3.37
2.01
0.36
0.06
0.08
0.04
0.01
631.43
1020.95
1428.17
1434.85
1436.12
1436.05
24381
33586
42009
42140
42165
42164
213
18657
35483
35751
35780
35775
35792
35759
35779
35773
35793
35795
0.730
0.255
0.004
0.0003
0.0002
0.0002
178
178
198
220
1
47
LDREX antenna *
2001-81 C
(Large-scale De[26640]
ployable Reflector
Experiment)
2000 Dec 20.02
Dish
140
6 dia
2001 Jan 3.62
2006 Jan 3.67
2.00
1.96
627.93 24291
372.00 17134
242
209
35582
21302
0.727
0.615
192
308
D
Ariane-5 2nd stage
(EPS)+VEB
+ LDREX box
2000-81 D
[26641]
2000 Dec 20.02
527 days
2002 May 31
Drum-cone
1190
Box
42
3.36 long
5.46 dia
0.7x0.7
x1.8
2000 Dec 21.14
2001 Feb 24.51
2001 May 31.69
2.00
1.77
2.09
636.22 24504
630.95 24368
92.20 6761
215
200
92
36036
35779
673
0.731
0.730
0.043
179
237
201
D
Sylda-5 upperpart
2000-81 E
[26642]
2000 Dec 20.02
556 days
2002 Jun 29
Hollow cone
900
4.56 dia
4.90 high
2000 Dec 23.74
2001 Jan 29.59
2002 Jun 29.48
2.01
1.85
2.14
626.87 24263
602.02 23618
90.28 6667
214
217
126
35555
34261
451
0.728
0.721
0.024
181
214
344
Bei Dou 2
[CZ-3A 6(64)]
2000-82 A
[26643]
XI-LC2
2000 Dec 20.68
> million years
Box+ 2 panels
2300
2.2x1.72
x2.0
18.1 span
2000
2000
2000
2006
20.79
27.51
27.94
3.86
25.02
0.11
0.12
0.02
197
35767
35775
35774
41786
35808
35796
35797
0.760
0.0005
0.0002
0.0003
180
132
163
167
D
CZ-3A 3rd stage
(H-18)
2000-82 B
[26644]
2000 Dec 20.68
2492 days
2007 Oct 17
Cylinder
3500
8.84 long
3 dia
2000 Dec 20.44
2006 Jan 4.11
2007 Oct 16.92
25.03
24.71
24.63
196
175
118
41760
6372
186
0.760
0.321
0.005
179
50
263
*
Large-scale Reflector Experiment: Antenna released from box, which remained attached to 2nd stage. Half-scale test for ETS 8 antenna deployment
filmed by on-board camera.
2016 - Version 1.15
Dec
Dec
Dec
Jan
751.05
1436.17
1436.05
1436.07
37370
42166
42164
42164
750.50 27357
157.28 9652
87.53 6531
RAE Table of Earth Satellites (extented)
Year of Launch 2000
Cospar ID
[Norad number]
Descent date
Lifetime
Date of
orbital
Determination
Orbital
Inclination
(deg)
Nodal
period
(min)
(Compiled 2006)
Extra Page 2000 -1
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
721
519
265
832
837
844
844
851
820
833
755
800
754
827
853
816
851
825
730
825
855
843
828
852
830
848
672
695
462
842
848
820
706
547
558
840
831
852
844
741
843
836
826
823
779
855
777
741
545
284
857
859
854
855
860
857
861
1005
856
858
857
876
858
890
859
863
859
899
881
862
871
856
857
912
876
855
863
1277
854
855
884
866
1011
1269
1067
855
958
1171
1143
856
857
855
877
859
0.001
0.002
0.001
0.002
0.002
0.0007
0.0008
0.0006
0.003
0.002
0.017
0.004
0.007
0.002
0.002
0.003
0.003
0.002
0.009
0.002
0.003
0.003
0.002
0.001
0.002
0.0005
0.017
0.013
0.028
0.001
0.029
0.002
0.001
0.024
0.022
0.012
0.029
0.015
0.0008
0.015
0.022
0.021
0.002
0.002
0.005
0.001
0.006
121
228
251
116
128
117
114
9
103
145
186
99
105
107
216
106
216
118
116
120
243
192
138
216
101
129
147
41
81
161
288
87
68
122
66
231
228
270
99
359
294
294
85
104
94
247
114
NOAA 16 fragments; 357 pieces, 1 has decayed.
NOAA 16 suffered a break up 2015 Nov 25.305 most likely due to a battery explosion. 53 pieces were catalogued 2015 Dec 5.
D
2000 55 B
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
C
D
E
F
G
H
J
K
L
M
N
P
Q
R
S
T
U
V
W
X
Y
Z
AA
AB
AC
AD
AE
AF
AG
AH
AJ
AK
AL
AM
AN
AP
AQ
AR
AS
AT
AU
AV
AW
AX
AY
2016 - Version 1.15
2005 Jul 15
[41045]
[41046]
[41047]
[41048]
[41049]
[41050]
[41051]
[41052]
[41053]
[41054]
[41055]
[41056]
[41057]
[41058]
[41059]
[41060]
[41061]
[41062]
[41063]
[41064]
[41065]
[41066]
[41067]
[41068]
[41069]
[41070]
[41071]
[41072]
[41073]
[41074]
[41075]
[41076]
[41077]
[41078]
[41079]
[41080]
[41081]
[41082]
[41083]
[41084]
[41085]
[41086]
[41087]
[41088]
[41089]
1758 days
2002
2005
2005
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
Aug
Feb
Jul
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
1.82
10.10
15.15
4.16
4.59
4.45
4.60
4.61
4.58
2.96
4.44
4.63
4.44
4.58
4.63
4.57
4.64
4.58
4.42
4.58
4.58
4.62
4.59
4.62
4.58
4.60
4.42
4.41
4.64
4.60
4.42
4.57
4.40
4.68
4.68
4.38
4.40
4.37
4.38
4.38
4.39
4.43
4.65
4.65
4.39
4.63
4.40
98.77
98.71
98.76
98.90
98.94
98.93
98.92
98.90
98.94
98.92
99.01
98.96
98.99
98.91
98.91
98.94
98.92
98.94
98.96
98.93
98.93
98.95
98.91
98.93
98.94
98.93
99.14
98.72
98.80
98.96
98.84
98.91
98.77
99.08
99.19
99.22
98.92
99.07
98.92
99.15
98.77
99.00
98.93
98.93
98.84
98.94
98.92
99.42
95.28
90.00
101.82
101.88
101.90
101.93
102.03
101.68
101.87
102.57
101.47
101.00
101.45
102.23
101.67
102.37
101.75
100.80
101.77
102.50
102.18
101.83
102.18
101.78
101.98
100.70
100.60
97.90
101.98
106.47
101.65
100.47
99.10
99.03
103.53
106.18
104.27
101.92
101.92
105.27
104.90
101.73
101.72
101.23
102.27
101.25
7109
6911
6653
7223
7226
7227
7228
7234
7217
7226
7259
7207
7184
7220
7243
7216
7249
7220
7175
7221
7256
7241
7224
7240
7222
7231
7170
7166
7037
7231
7442
7215
7159
7094
7091
7304
7429
7338
7228
7228
7386
7368
7219
7218
7196
7244
7197
RAE Table of Earth Satellites (extented)
Year of Launch 2000
Cospar ID
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
[Norad number]
AZ
BA
BB
BC
BD
BE
BF
BG
BH
BJ
BK
BL
BM
BN
BP
BQ
BR
BS
BT
BU
BV
BW
BX
BY
BZ
CA
CB
CC
CD
CE
CF
CG
CH
CJ
CK
CL
CM
CN
CP
CQ
CR
CS
CT
CU
CV
CW
CX
CY
CZ
2016 - Version 1.15
[41090]
[41091]
[41092]
[41093]
[41094]
[41095]
[41096]
[41097]
[41126]
[41127]
[41128]
[41129]
[41130]
[41131]
[41132]
[41133]
[41134]
[41135]
[41136]
[41137]
[41138]
[41139]
[41140]
[41141]
[41142]
[41143]
[41144]
[41145]
[41146]
[41147]
[41148]
[41149]
[41150]
[41151]
[41152]
[41153]
[41154]
[41155]
[41156]
[41157]
[41158]
[41159]
[41160]
[41161]
[41162]
[41163]
[41164]
[41165]
[41196]
Descent date
Lifetime
Date of
orbital
Determination
Orbital
Inclination
(deg)
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
98.93
99.03
98.88
98.89
99.01
99.00
98.87
98.93
98.92
98.84
99.05
98.88
98.94
98.97
98.87
98.92
98.94
98.87
99.10
98.90
98.92
98.98
98.84
98.98
98.87
98.89
98.84
98.01
98.91
98.95
98.88
98.93
98.83
98.91
98.93
98.92
98.98
98.95
98.94
98.97
98.97
98.86
98.91
98.94
98.91
99.03
99.03
98.81
98.94
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
4.63
4.45
4.42
4.41
4.44
4.39
4.41
4.39
15.64
14.98
14.97
14.63
15.03
15.66
15.66
15.65
15.66
14.43
14.41
15.42
15.66
14.39
15.64
15.40
15.64
14.40
14.66
14.94
15.41
14.94
15.64
15.04
15.43
14.40
15.41
15.41
15.65
15.42
15.63
15.63
14.42
14.97
15.65
15.45
15.43
15.66
14.66
14.44
30.15
Nodal
period
(min)
(Compiled 2006)
Extra Page 2000 -2
Semi
major axis
(km)
101.53
102.60
100.70
100.60
100.98
101.18
99.28
103.63
103.00
100.67
102.10
100.67
101.65
103.10
101.32
101.95
102.35
101.13
101.37
102.20
102.00
103.17
101.17
101.05
101.20
103.60
101.97
100.13
102.15
103.43
100.50
100.98
101.20
103.20
101.78
101.80
103.00
101.87
101.12
102.53
101.80
101.70
102.32
102.35
102.28
100.93
103.07
102.30
102.92
7210
7261
7170
7165
7184
7193
7128
7309
7279
7169
7236
7168
7215
7283
7199
7229
7248
7191
7202
7242
7232
7287
7192
7187
7194
7307
7230
7144
7239
7299
7161
7183
7194
7289
7222
7222
7279
7225
7190
7257
7222
7218
7247
7248
7245
7181
7282
7246
7275
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
805
837
728
717
752
774
643
855
843
726
852
723
819
853
784
847
847
768
793
842
849
851
766
758
768
853
828
672
838
851
712
750
769
850
833
829
850
831
768
847
833
821
851
837
841
749
852
847
853
858
927
855
856
858
855
856
1006
957
855
863
856
854
956
857
854
892
856
854
884
858
966
861
859
863
1004
875
858
882
990
851
860
861
970
853
858
951
862
855
909
855
857
886
902
893
856
956
889
939
0.004
0.006
0.009
0.010
0.007
0.006
0.015
0.010
0.008
0.009
0.0008
0.009
0.002
0.007
0.005
0.0005
0.003
0.006
0.004
0.003
0.0006
0.008
0.007
0.007
0.007
0.010
0.003
0.013
0.003
0.010
0.010
0.008
0.006
0.008
0.001
0.002
0.007
0.002
0.006
0.004
0.002
0.002
0.002
0.005
0.004
0.007
0.007
0.003
0.006
115
216
90
93
69
95
85
268
262
57
276
47
41
231
42
89
186
46
44
288
132
224
26
79
23
247
334
71
295
220
56
76
84
216
48
13
217
2
66
203
49
85
276
161
285
33
258
188
183
RAE Table of Earth Satellites (extented)
Year of Launch 2000
Cospar ID
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
[Norad number]
DA
DB
DC
DD
DE
DF
DG
DH
DJ
DK
DL
DM
DN
DP
DQ
DR
DS
DT
DU
DV
DW
DX
DY
DZ
EA
EB
EC
ED
EE
EF
EG
EH
EJ
EK
EL
EM
EN
EP
EQ
ER
ES
ET
EU
EV
EW
EX
EY
EZ
FA
FB
FC
2016 - Version 1.15
[41197]
[41198]
[41199]
[41200]
[41201]
[41202]
[41203]
[41204]
[41205]
[41206]
[41207]
[41208]
[41209]
[41210]
[41211]
[41212]
[41213]
[41214]
[41215]
[41216]
[41217]
[41218]
[41219]
[41220]
[41221]
[41222]
[41223]
[41224]
[41225]
[41226]
[41227]
[41228]
[41229]
[41230]
[41231]
[41232]
[41233]
[41234]
[41235]
[41236]
[41237]
[41243]
[41244]
[41245]
[41246]
[41247]
[41248]
[41249]
[41250]
[41251]
[41252]
Descent date
Lifetime
Date of
orbital
Determination
Orbital
Inclination
(deg)
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2015
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
98.77
98.94
98.96
98.89
98.98
98.93
98.94
98.97
98.97
98.86
98.90
98.89
98.89
98.95
98.94
98.97
99.00
98.88
98.88
98.92
98.91
98.92
98.87
98.62
98.93
98.87
98.90
98.95
98.94
98.95
99.05
98.93
98.90
98.97
98.93
98.96
98.91
98.87
98.92
98.05
98.98
98.92
99.02
98.92
98.96
98.91
98.91
98.94
99.06
99.02
98.97
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Dec
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
30.43
29.40
29.96
29.43
29.40
30.64
30.40
29.38
30.41
30.44
29.40
29.40
29.41
30.16
30.66
30.65
30.65
29.97
29.96
30.14
30.40
29.41
30.41
30.64
30.45
29.39
30.68
30.43
27.97
30.64
29.40
30.45
28.64
29.42
29.44
29.40
29.42
28.98
30.42
30.66
27.13
25.38
25.66
26.14
25.41
26.41
25.45
25.41
26.46
26.14
26.13
Nodal
period
(min)
(Compiled 2006)
Extra Page 2000 -3
Semi
major axis
(km)
102.68
102.60
103.00
101.62
102.82
103.32
102.42
102.33
101.83
102.10
100.92
102.62
100.95
102.32
102.33
101.88
101.88
101.55
101.53
103.75
102.62
101.98
102.02
102.28
101.12
103.00
102.58
102.48
101.70
102.48
101.53
102.13
102.90
101.38
101.05
102.82
102.45
100.48
102.02
101.50
101.27
102.07
101.93
102.25
101.05
101.40
103.48
101.27
102.42
102.50
102.95
7264
7260
7279
7214
7270
7294
7251
7248
7224
7236
7181
7261
7182
7247
7248
7226
7227
7210
7210
7314
7261
7231
7233
7245
7190
7279
7259
7255
7218
7254
7210
7238
7274
7202
7187
7270
7253
7160
7232
7208
7197
7235
7229
7244
7187
7203
7302
7197
7252
7255
7277
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
849
852
850
817
854
853
844
851
829
848
751
853
752
847
846
831
823
807
810
853
846
808
849
853
767
853
853
846
808
850
805
842
832
794
762
849
840
707
847
797
780
852
839
852
758
774
852
784
832
830
853
921
910
952
852
929
978
901
887
862
868
853
912
855
889
892
864
873
856
853
1019
919
897
860
880
856
948
908
906
871
902
857
878
960
854
853
934
909
856
861
862
857
860
861
878
858
876
995
853
914
923
943
0.005
0.003
0.007
0.002
0.005
0.009
0.004
0.003
0.002
0.001
0.007
0.004
0.007
0.003
0.003
0.002
0.003
0.003
0.003
0.011
0.005
0.006
0.0007
0.002
0.006
0.007
0.004
0.004
0.004
0.004
0.004
0.002
0.009
0.004
0.006
0.006
0.005
0.010
0.0009
0.005
0.005
0.0005
0.001
0.002
0.007
0.007
0.010
0.005
0.006
0.006
0.006
180
180
172
14
211
189
129
232
315
260
20
218
7
151
132
83
96
353
1
200
219
94
271
222
32
206
210
147
72
226
351
119
149
30
23
166
147
9
185
332
355
95
7
77
270
339
131
289
181
66
128
RAE Table of Earth Satellites (extented)
Year of Launch 2000
Cospar ID
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
[Norad number]
FD
FE
FF
FG
FH
FJ
FK
FL
FM
FN
FP
FQ
FR
FS
FT
FU
FV
FW
FX
FY
FZ
GA
GB
GC
GD
GE
GF
GG
GH
GJ
GK
GL
GM
GN
GP
GQ
GR
GS
GT
GU
GV
GW
GX
GY
GZ
HA
HB
HC
HD
HE
HF
2016 - Version 1.15
[41253]
[41254]
[41255]
[41256]
[41257]
[41258]
[41259]
[41260]
[41261]
[41262]
[41263]
[41264]
[41265]
[41266]
[41267]
[41268]
[41269]
[41270]
[41271]
[41272]
[41273]
[41274]
[41275]
[41276]
[41277]
[41278]
[41279]
[41280]
[41281]
[41282]
[41283]
[41284]
[41285]
[41286]
[41287]
[41288]
[41289]
[41290]
[41291]
[41292]
[41293]
[41294]
[41295]
[41296]
[41297]
[41298]
[41299]
[41300]
[41301]
[41302]
[41303]
Descent date
Lifetime
Date of
orbital
Determination
Orbital
Inclination
(deg)
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
99.00
99.08
98.83
98.09
98.98
98.98
98.85
98.99
98.89
98.87
98.93
98.88
98.82
98.91
98.83
98.02
99.00
99.04
98.82
98.94
98.91
98.84
98.88
98.90
98.95
98.87
99.00
98.83
98.93
98.90
98.89
98.88
98.92
98.92
98.92
98.97
98.91
98.01
98.97
98.95
98.94
98.87
98.90
98.97
99.01
98.93
98.94
98.95
98.86
98.93
99.00
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
Jan
26.43
25.39
25.49
26.44
25.46
25.42
26.04
25.40
25.65
25.99
24.96
26.44
25.40
26.02
26.13
26.43
26.43
26.43
25.41
26.15
26.43
26.05
25.39
25.39
26.43
26.04
25.97
26.40
26.15
25.45
25.45
25.45
26.13
26.67
25.40
25.13
26.13
26.41
26.64
26.17
25.04
25.97
25.44
25.45
26.65
25.39
26.41
25.97
26.02
26.41
25.01
Nodal
period
(min)
(Compiled 2006)
Extra Page 2000 -4
Semi
major axis
(km)
101.12
101.58
101.28
101.68
102.05
101.17
100.68
102.32
102.62
103.07
103.38
102.05
102.57
102.05
101.20
102.50
102.50
102.50
100.92
102.38
100.88
101.17
102.18
102.18
101.45
101.37
102.57
102.57
102.62
103.13
103.13
103.48
102.12
101.48
102.67
102.58
102.60
101.65
101.22
101.27
102.55
101.72
102.55
102.42
103.10
102.18
102.35
102.68
102.42
102.35
100.48
7190
7212
7198
7217
7235
7193
7170
7247
7261
7282
7297
7234
7258
7234
7194
7256
7256
7256
7181
7250
7184
7193
7241
7241
7206
7202
7259
7259
7261
7285
7285
7302
7237
7207
7264
7259
7260
7215
7195
7197
7258
7219
7250
7251
7284
7241
7248
7264
7251
7248
7160
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
764
808
785
821
835
770
715
849
850
853
853
852
852
852
772
851
851
850
752
848
758
767
843
850
793
794
852
854
853
853
855
851
815
806
853
849
851
817
778
782
851
823
849
850
850
819
832
850
851
849
706
858
859
853
855
877
858
867
888
915
954
984
859
907
859
858
903
902
904
852
896
852
861
882
875
861
853
908
906
913
960
958
995
902
851
917
912
912
856
853
855
908
858
894
896
960
905
908
921
894
890
857
0.007
0.004
0.005
0.002
0.003
0.006
0.011
0.003
0.004
0.007
0.009
0.0005
0.004
0.0005
0.006
0.004
0.004
0.004
0.007
0.003
0.007
0.007
0.003
0.002
0.005
0.004
0.004
0.004
0.004
0.007
0.007
0.010
0.006
0.003
0.004
0.004
0.004
0.003
0.005
0.005
0.004
0.002
0.003
0.003
0.008
0.006
0.005
0.005
0.003
0.003
0.011
323
343
292
266
44
325
258
78
144
131
128
149
140
89
317
145
132
150
290
74
300
334
171
211
323
275
140
125
122
112
116
137
22
337
123
149
145
300
296
274
138
255
142
87
142
28
41
93
143
160
314
RAE Table of Earth Satellites (extented)
Year of Launch 2000
Cospar ID
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
[Norad number]
HG
HH
HJ
HK
HL
HM
HN
HP
HQ
HR
HS
HT
HU
HV
HW
HX
HY
HZ
JA
JB
JC
JD
JE
JF
JG
JH
JJ
JK
JL
JM
JN
JP
JQ
JR
JS
JT
JU
JV
JW
JX
JY
JZ
KA
KB
KC
KD
KE
KF
KG
KH
KJ
2016 - Version 1.15
[41304]
[41305]
[41306]
[41307]
[41343]
[41344]
[41345]
[41346]
[41347]
[41348]
[41349]
[41350]
[41351]
[41352]
[41353]
[41354]
[41355]
[41356]
[41357]
[41358]
[41359]
[41360]
[41361]
[41362]
[41363]
[41364]
[41365]
[41366]
[41367]
[41368]
[41369]
[41370]
[41371]
[41372]
[41373]
[41374]
[41375]
[41376]
[41377]
[41378]
[41379]
[41396]
[41397]
[41398]
[41399]
[41400]
[41401]
[41402]
[41403]
[41404]
[41405]
Descent date
Lifetime
Date of
orbital
Determination
Orbital
Inclination
(deg)
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
99.08
98.83
98.91
98.96
98.81
99.04
98.86
98.91
98.88
98.85
98.94
99.01
98.85
98.91
98.93
98.92
98.88
98.92
98.96
98.88
98.91
98.97
98.91
98.92
98.92
98.85
98.91
98.99
98.97
99.01
98.65
98.90
98.92
98.98
98.92
98.95
98.96
98.91
98.96
98.88
98.88
98.86
98.91
98.91
98.94
98.89
98.87
98.91
98.92
98.99
98.92
Jan
Jan
Jan
Jan
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Feb
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
25.38
25.65
26.14
25.69
2.42
1.43
1.46
1.40
1.97
1.40
1.40
3.42
1.97
2.42
2.42
1.14
1.99
2.45
1.41
2.41
2.44
2.00
1.45
1.14
1.40
1.36
2.43
3.02
2.01
1.38
2.44
2.05
1.45
2.41
3.44
2.37
2.02
2.14
2.41
1.38
29.99
25.45
25.00
25.45
25.14
25.39
25.38
25.39
25.17
23.43
25.42
Nodal
period
(min)
(Compiled 2006)
Extra Page 2000 -5
Semi
major axis
(km)
102.40
102.75
100.85
101.93
101.85
101.55
100.75
104.27
102.12
102.03
101.37
101.72
102.20
101.33
102.22
102.22
101.98
102.47
103.35
101.98
101.43
102.00
102.53
101.27
101.58
102.08
101.48
102.68
101.50
101.88
102.00
100.68
101.88
100.82
101.35
102.47
101.78
101.85
101.98
102.47
101.53
100.08
101.43
101.75
102.63
101.82
102.35
102.53
101.57
101.47
102.13
7251
7267
7177
7229
7225
7211
7173
7338
7237
7233
7202
7218
7241
7200
7242
7242
7231
7254
7295
7231
7205
7232
7257
7197
7212
7235
7208
7265
7208
7226
7232
7168
7227
7176
7212
7254
7222
7225
7231
7254
7210
7141
7205
7220
7262
7223
7249
7257
7211
7207
7238
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
834
854
742
834
825
806
734
838
842
824
791
817
853
783
844
847
844
843
854
839
797
833
851
780
812
843
795
853
789
822
832
724
829
737
811
850
822
831
835
843
806
668
791
824
850
827
854
854
809
796
846
911
922
856
866
866
858
854
1082
876
886
856
862
872
860
883
880
861
908
979
866
855
874
907
857
855
870
864
918
870
872
875
855
867
857
856
900
865
862
871
908
857
857
861
859
916
862
885
903
857
861
873
0.005
0.005
0.008
0.002
0.003
0.004
0.008
0.017
0.002
0.004
0.004
0.003
0.001
0.005
0.003
0.002
0.001
0.004
0.009
0.002
0.004
0.003
0.004
0.005
0.003
0.002
0.005
0.004
0.006
0.003
0.003
0.009
0.003
0.008
0.003
0.003
0.003
0.002
0.003
0.004
0.004
0.013
0.005
0.002
0.005
0.002
0.002
0.003
0.003
0.005
0.002
187
138
308
28
260
176
187
1
293
109
215
151
79
158
305
316
134
314
10
270
187
284
58
168
180
102
219
43
232
271
110
196
110
207
203
331
135
251
278
328
170
98
149
159
275
181
342
343
144
170
232
RAE Table of Earth Satellites (extented)
Year of Launch 2000
Cospar ID
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
[Norad number]
KK
KL
KM
KN
KP
KQ
KR
KS
KT
KU
KV
KW
KX
KY
KZ
LA
LB
LC
LD
LE
LF
LG
LH
LJ
LK
LL
LM
LN
LP
LQ
LR
LS
LT
LU
LV
LW
LX
LY
LZ
MA
MB
MC
MD
ME
MF
MG
MH
MJ
MK
ML
MM
2016 - Version 1.15
[41406]
[41407]
[41408]
[41409]
[41410]
[41411]
[41412]
[41413]
[41414]
[41415]
[41416]
[41417]
[41418]
[41419]
[41420]
[41421]
[41422]
[41423]
[41424]
[41425]
[41426]
[41427]
[41428]
[41429]
[41430]
[41431]
[41432]
[41433]
[41491]
[41492]
[41493]
[41494]
[41495]
[41496]
[41497]
[41498]
[41499]
[41500]
[41501]
[41502]
[41503]
[41504]
[41505]
[41506]
[41507]
[41508]
[41509]
[41510]
[41511]
[41512]
[41513]
Descent date
Lifetime
Date of
orbital
Determination
Orbital
Inclination
(deg)
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
98.92
98.96
98.90
98.83
98.92
98.91
98.80
98.89
98.97
98.90
98.89
98.92
98.98
98.91
98.94
98.93
98.93
98.87
98.96
98.95
98.96
98.97
98.92
98.92
98.95
98.97
98.86
99.01
98.92
98.84
98.90
98.92
98.88
98.89
98.92
98.95
98.83
98.98
98.74
98.90
98.84
98.93
98.91
98.81
98.92
98.93
98.93
98.94
98.93
98.92
98.88
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
Mar
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
25.42
25.39
25.42
25.39
25.40
25.40
25.41
25.38
25.39
24.98
25.40
25.38
25.16
23.39
25.39
25.42
25.14
23.43
25.41
25.43
25.40
25.42
25.41
25.46
25.06
24.98
25.16
25.17
23.37
21.41
22.43
22.42
23.39
23.46
24.00
23.43
23.45
22.41
23.45
23.42
23.42
22.42
22.99
23.43
23.41
21.45
23.44
23.44
23.39
23.45
43.36
Nodal
period
(min)
(Compiled 2006)
Extra Page 2000 -6
Semi
major axis
(km)
101.32
101.45
101.83
101.75
102.43
101.70
102.37
102.17
101.27
101.90
101.77
101.98
101.38
102.22
101.15
101.37
102.15
101.78
101.78
101.13
102.17
102.55
101.83
102.00
101.42
101.03
100.45
101.55
103.47
104.08
101.50
101.42
102.65
101.72
102.45
101.75
101.87
101.42
101.07
102.18
101.45
102.38
101.78
101.10
101.65
101.78
101.95
102.03
102.28
101.32
102.92
7199
7206
7224
7220
7252
7218
7249
7240
7197
7227
7221
7231
7203
7242
7192
7202
7239
7221
7221
7191
7240
7258
7224
7232
7204
7186
7159
7211
7301
7330
7208
7204
7263
7219
7253
7220
7226
7204
7188
7241
7206
7250
7221
7189
7215
7222
7230
7234
7246
7200
7275
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
786
796
833
812
857
823
851
845
764
841
814
835
793
851
771
781
849
829
819
770
847
852
830
837
787
763
696
805
839
854
805
801
850
826
845
828
814
791
769
851
802
843
810
771
824
819
834
832
844
791
850
855
860
858
872
890
856
890
877
873
855
870
871
855
876
856
865
872
856
866
855
876
906
861
869
864
853
864
859
1005
1049
854
850
918
854
904
856
880
859
849
873
853
900
876
850
849
867
868
878
890
851
943
0.005
0.004
0.002
0.004
0.002
0.002
0.003
0.002
0.008
0.001
0.004
0.002
0.004
0.002
0.006
0.006
0.002
0.002
0.003
0.006
0.002
0.004
0.002
0.002
0.005
0.006
0.012
0.004
0.011
0.013
0.003
0.003
0.005
0.002
0.004
0.002
0.005
0.005
0.006
0.001
0.004
0.004
0.005
0.006
0.002
0.003
0.002
0.003
0.003
0.004
0.006
116
135
161
192
323
122
276
12
159
119
56
204
129
358
115
154
23
139
79
133
23
280
80
204
160
133
90
103
180
168
342
314
148
353
97
354
50
358
313
138
347
96
240
296
312
30
50
58
96
303
151
RAE Table of Earth Satellites (extented)
Year of Launch 2000
Cospar ID
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
2000
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
55
[Norad number]
MN
MP
MQ
MR
MS
MT
MU
MV
MW
MX
MY
MZ
NA
NB
NC
ND
NE
NF
NG
NH
NJ
NK
NL
NM
NN
NP
NQ
NR
NS
NT
NU
NV
NW
NX
NY
NZ
PA
PB
PC
PD
PE
PF
PG
PH
PJ
PK
PL
PM
PN
PP
PQ
2016 - Version 1.15
[41514]
[41515]
[41516]
[41517]
[41518]
[41519]
[41520]
[41521]
[41522]
[41523]
[41524]
[41525]
[41526]
[41527]
[41528]
[41529]
[41530]
[41531]
[41532]
[41533]
[41534]
[41535]
[41536]
[41537]
[41538]
[41539]
[41540]
[41652]
[41653]
[41654]
[41655]
[41656]
[41657]
[41658]
[41659]
[41660]
[41661]
[41662]
[41663]
[41664]
[41665]
[41666]
[41667]
[41668]
[41669]
[41705]
[41706]
[41707]
[41708]
[41709]
[41710]
Descent date
Lifetime
Date of
orbital
Determination
Orbital
Inclination
(deg)
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
2016
98.91
99.02
98.87
98.83
98.87
98.87
98.94
98.80
98.89
98.94
98.89
98.89
98.97
99.00
98.80
98.93
98.78
98.91
98.90
98.82
98.92
98.94
98.89
98.92
98.85
98.88
98.93
98.94
98.93
98.85
98.88
98.90
98.84
98.91
98.93
98.87
98.99
98.91
98.89
98.92
98.91
98.90
98.90
98.93
98.83
98.91
98.93
98.88
98.92
98.98
98.90
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
May
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
Jul
23.44
22.97
22.45
23.41
22.97
23.44
23.40
23.43
23.40
23.42
16.41
23.43
23.41
23.40
23.43
23.41
22.43
21.38
23.41
23.43
23.44
23.44
23.38
23.16
23.37
23.42
21.15
8.40
8.42
8.39
8.13
8.41
8.42
8.38
8.45
8.39
8.15
8.43
8.39
8.06
8.38
8.39
8.38
8.04
8.39
26.43
25.40
27.40
27.63
27.67
27.42
Nodal
period
(min)
(Compiled 2006)
Extra Page 2000 -7
Semi
major axis
(km)
101.47
101.75
101.80
101.08
101.67
101.93
102.28
101.73
101.63
102.10
101.53
101.98
101.62
101.22
101.90
102.67
100.77
102.52
101.82
100.53
102.40
101.62
101.77
101.92
102.88
101.58
102.48
102.42
101.82
102.03
101.68
102.08
101.92
101.70
101.87
101.65
101.67
101.83
101.68
101.67
102.52
101.53
101.57
101.38
101.67
101.78
102.55
101.53
101.92
101.72
101.37
7207
7220
7222
7188
7216
7229
7245
7219
7215
7237
7210
7231
7214
7194
7227
7263
7174
7256
7223
7163
7250
7214
7221
7228
7274
7212
7254
7251
7223
7233
7217
7236
7228
7217
7225
7215
7216
7224
7217
7216
7257
7210
7211
7203
7216
7222
7257
7210
7228
7219
7202
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
799
830
834
770
816
838
820
792
818
848
809
844
813
780
827
851
726
851
837
714
850
819
831
844
852
815
845
838
839
819
822
851
836
813
831
820
816
832
823
822
848
808
809
787
817
831
852
805
836
813
791
857
852
853
849
860
862
912
889
854
869
854
862
857
852
869
918
864
905
852
854
894
851
853
855
938
851
906
908
851
890
856
864
862
865
862
853
859
860
853
854
908
854
856
862
858
856
906
857
863
867
855
0.004
0.001
0.001
0.005
0.003
0.002
0.006
0.007
0.003
0.001
0.003
0.001
0.003
0.005
0.003
0.005
0.010
0.004
0.001
0.010
0.003
0.002
0.002
0.0008
0.006
0.002
0.004
0.005
0.0008
0.005
0.002
0.0009
0.002
0.004
0.002
0.002
0.003
0.002
0.002
0.002
0.004
0.003
0.003
0.005
0.003
0.002
0.004
0.004
0.002
0.004
0.004
273
18
294
305
24
217
69
43
275
97
355
237
4
331
54
156
351
159
271
334
165
180
338
17
147
310
112
312
208
99
156
334
119
129
136
181
236
117
191
150
332
217
164
219
244
154
295
163
73
82
154
RAE Table of Earth Satellites (extented)
Year of Launch 2000
Cospar ID
2000
2000
2000
2000
2000
2000
2000
55
55
55
55
55
55
55
[Norad number]
PR
PS
PT
PU
PV
PW
PX
2016 - Version 1.15
[41711]
[41712]
[41713]
[41714]
[41715]
[41716]
[41717]
Descent date
Lifetime
Date of
orbital
Determination
Orbital
Inclination
(deg)
2016
2016
2016
2016
2016
2016
2016
98.89
98.90
98.90
98.93
98.79
98.89
98.89
Jul
Jul
Jul
Jul
Jul
Jul
Jul
27.45
27.44
27.38
25.38
27.42
24.41
27.40
Nodal
period
(min)
(Compiled 2006)
Extra Page 2000 -8
Semi
major axis
(km)
101.75
102.02
103.52
103.77
102.02
101.93
101.65
7220
7232
7304
7315
7232
7229
7215
Perigee
height
(km)
Apogee
height
(km)
Orbital
eccentric.
Argument
of perigee
(deg)
827
816
841
847
844
845
819
856
891
1009
1025
864
855
854
0.002
0.005
0.011
0.012
0.001
0.0007
0.002
162
37
14
16
232
96
114