1967
advertisement
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Page
125
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Intelsat 2-2
[Thor Delta E
468 #44]
1967-01 A
[02639]
CC-LC17B
1967 Jan 11.45
> million years
Cylinder
87
0.67 1ong
1.42 dia
1967 Jan 22.9
1977 may 13.0
2001 Feb 17.21
2.14
6.62
13.89
1448.5
1437.31
1437.33
42408
42198
42189
35563
35758
35763
36496
35883
35858
0.011
0.001
0.001
26
3
162
Intelsat 2-2
second stage
1967-01 B
[02640]
1967 Jan 11.45
92 days
1967 Apr 13
Cylinder
400?
4.9 long
1.43 dia
1967 Feb 5.4
1967 Mar 8.0
28.75
28.74
91.95
91.04
6754
6710
241
232
511
432
0.02
0.015
58
-
Intelsat 2-2
third stage
1967-0l D
[02643]
1967 Jan 11.45
60 years
Cylinder
24
1.5 long
0.46 dia
1967 Jan 31.5
2001 Feb 17.07
26.18
26.19
652.9
461.60
24927
19785
288
356
36810
25458
0.733
0.660
52
Intelsat 2-2
Altair PKM
1967-01 AB * 1967 Jan 11.45
[R13907]
Fragments *
1967-01 C, E-W ,Z, AL, AT
D Discoverer 112
1967-02 A
r? (KH 4A-49)
[02642]
[Thor 2C 495
VDB-SLC3W
Agena D SS-01B 1629]
1967 Jan 14.89
18.7 days
1967 Feb 2.6
D
39 pieces, 21 have decayed
Cylinder
lst 15 days
1500?
8 long?
1.5 dia
For orbital information see extra pages at the end of the year
1967 Jan 15.6
1967 Feb 1.94
80.07
80.08
90.13
88.12
6658
6560
180
146
380
217
0.015
0.005
161
77
then 700?
Fragment
1967-02 B
[02662]
1967 Jan 28
14 days
1967 Jan 27.98
80.06
88.25
6566
141
235
0.007
97
IDCSP 2-1
[Titan 3C #13]
1967-03 A
[02645]
CC-LC41
1967 Jan 18.60
> million years
Polyhedron
(26 faces)
45
0.3 long
0.9 dia
1967 Jan 28.7
2001 Jan 17.00
0.07
9.22
1329.6
1329.5
40055
40052
33557
33500
33800
33846
0.003
0.004
352
7
IDCSP 2-2
1967-03 B
[02649]
1967 Jan 18.6o
> million years
Polyhedron
(26 faces)
45
0.8 long
0.9 dia
1967 Jan 28.3
2001 Jan 17.03
0.05
9.22
1330.0
1309.18
40064
39643
33526
29332
33846
37196
0.004
0.099
117
322
IDCSP 2-3
1967-03 C
[02650]
1967 Jan 18.60
> million years
Polyhedron
(26 faces)
0.8 long
0.9 dia
1967 Jan 28.3
2001 Jan 17.00
0.06
9.24
1330.7
1330.68
40077
40075
33579
33548
33819
33846
0.003
0.004
95
357
Oo8 long
0.9 dia
1967 Jan 28.3
2001 Jan 17.00
0.07
9.53
1332.1
1332.10
40l05
40104
33606
33559
33847
33892
0.003
0.004
l04
346
45
IDCSP 2-4
1967-03 D
[02651]
1967 Jan 18.60
> million years
Polyhedron
(26 faces)
45
*
1967-01
1967-01
1967-01
1967-01
1967-01
1967-01
X reassigned to 1971-116 B Intelsat 4-3 Atlas SLV-3C 5006C-Centaur 26 stage per Jul 1999
Y, AC-AF have been reassigned to the 1981-88 launch per Jul 1999
AA, AG, AJ, AK, AM-AR have been reassigned to the 1965-108 launch
AB has been reassigned to the 1977-108 launch per Sep 1998
AH has been reassigned to the 1973-23 launch per Aug 1999
AS has been reassigned to the 1990-65 launch
2004 December 31 – version 1.01
1967- 03 continued on page 126
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
IDCSP 2-5 #
1967-03 E
[02652]
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
1967 Jan 18.60
> million years
Polyhedron
(26 faces)
0.8 long
0.9 dia
1967 Jan 28.3
2001 Jan 17.00
0.03
9.52
Page
126
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
1334.2
1334.12
40147
40144
33608
33570
33929
33961
0.004
0.005
89
332
45
IDCSP 2-6 #
1967-03 F
[02653]
1967 Jan 18.60
> million years
Polyhedron
(26 faces)
0.8 long
0.9 dia
1967 Jan 28.2
2001 Jan 17.00
0.06
9.41
1336.5
1336.53
40195
40193
33656
33588
33978
34041
0.004
0.006
28
321
IDCSP 2-7
1967-03 G
[02654]
1967 Jan 18.60
> million years
45
Polyhedron
(26 faces)
0.8 long
0.9 dia
1967 Jan 28.2
2001 Jan 17.00
0.03
9.66
1339.5
1339.5
40254
40252
33675
33620
34077
34127
0.005
0.006
16
303
33665
33640
34229
34243
45
IDCSP 2-8
1967-03 H
[02655]
1967 Jan 18.60
> million years
Polyhedron
(26 faces)
45
0.8 long
0.9 dia
1967 Jan 28.2
2001 Jan 17.00
0.05
9.80
1343.0
1332.90
40325
40320
0.007
0.007
32
300
Transtage 9
[Titan 3C-13]
1967-03 J
[02660]
1967 Jan 18.60
> million years
Cylinder
1500?
6 long?
3 dia
1967 Jan 18.6
1967 Jan 28.2
1995 Jul 19.00
28
0.17
11.37
87.88
1347.67
1329.77
6554
170
132
0.001
404l4? 33712? 34359? 0.008
40057 33561 33796 0.003
195
D
R
Cosmos 138
[Vostok 8A92]
1967-04 A
[02646]
PLE-LC41/1
1967 Jan 19.53
7.73 days
1967 Jan 27.26
Spherecylinder
4750?
4.3 long
2.4 dia
1967 Jan 23.3
64.55
89.15
6610
191
273
0.006
27
D
Cosmos 138
Block E 3rd stage
1967-04 B
[02648]
1967 Jan 19.53
8.5 days
1967 Jan 28.0
Cylinder
1440
3.8 long
2.6 dia
1967 Jan 26.6
64.57
88.31
6570
183
201
0.001
74
D Cosmos 139
R? [R-36-0]
1967-05 A
[02656]
BAI
1967 Jan 25.58
0.06 day
1967 Jan 25.64
Cylinder?
2 long?
1 dia?
1967 Jan 25.6
49.7
87.97
6555
144
210
0.005
-
D
Cosmos 139
2nd stage
1967-05 B
[02658]
1967 Jan 25.58
0.3 day?
1967 Jan 25.9?
Cylinder
5000
9.4 long
3.0 dia
1967 Jan 25.81
50.16
0rbit similar to 1967-05 A
87.40
6525
123
169
0.003
355
D
Cosmos 139
platform
1967-05 C
[02659]
1967 Jan 25.58
0.4 day?
1967 Jan 25
Irregular
#
originally listed on page 125.
2004 December 31 – version 1.01
0rbit similar to 1967-05 A
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Page
127
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Essa 4 (TIROS 14)
[Thor Delta E
472 #45
1967-06 A
[02657]
VDB-SLC2E
1967 Jan 26.73
10000 years
Cylinder
132
0.56 long
1.07 dia
1967 Jan 29.4
2001 Feb 15.63
102.00
102.06
113.48
113.40
7764
7761
1328
1326
l443
1439
0.007
0.007
55
104
Essa 4
Delta 3rd stage
1967-06 B
[02661]
1967 Jan 26.73
5000 years
Cylinder
24
1.5 long
0.46 dia
1967 Jan 27.4
2001 Feb 17.91
101.98
101.98
113.68
113.58
7773
7769
1344
1340
1344
1441
0.006
0.006
69
177
Essa 4
De-spin weight
1967-06 C
[02706]
1967 Jan 26.73
2001 Feb 17.39
102.06
114.22
7798
1392
1448
0.004
190
Essa 4
De-spin weight
1967-06 D
[02707]
1967 Jan 26.73
2001 Feb 18.29
101.81
112.58
7724
1230
1460
0.015
261
Fragment
1967-06 E
[05971]
2001 Feb 18.71
101.92
113.10
7747
1281
1456
0.011
286
D
KH 7-36 Gambit
[Atlas SLV-3
7126-Agena D]
1967-07 A
[02664]
VDB-SLC4E
1967 Feb 2.83
9 days
1967 Feb 12
2000
1.5 dia?
1967 Feb 6.0
l02.96
89.47
6625
136
357
0.017
123
D
Agena D
rocket
1967-07 B
[02665]
1967 Feb 2. 83
1.5 days
1967 Feb 4.3
Cylinder
700?
8 long?
1.5 dia?
1967 Feb 3
103.13
89.75
6639
176
345
0.013
-
D
Lunar Orbiter 3
[Atlas SLV-3 5803
Agena D 6632]
1967-08 A
[02666]
CC-LC13
1967 Feb 5.05
246.38 days
1967 Oct 9.43
Truncated
cone
389
1.52 dia
1.68 high
1967
1967
1967
Sent
Lunar Orbiter 3
Agena D
1967-08 B
[NNA]
1967 Feb 5.05
Cylinder
7 long
D
R
Cosmos 140 *
[Soyuz 11A511]
1967-09 A
[02667]
BAI-LC1
1967 Feb 7.14
1.99 days
1967 Feb 9.13
Spherecylinder + 2
wings 6450?
7.5 long
2.2 dia
1967 Feb 8.4
51.66
88.27
6570
165
218
0.004
335
D
p
Cosmos 140
Block I 3rd stage
1967-09 B
[02668]
1967 Feb 7.14
1 day
1967 Feb 8
Cylinder
2500?
7.5 long
2.6 dia
1967 Feb 8.0
51.72
87.79
6546
148
187
0.003
329
DMSP B4A-02
[Thor Burner 2
#169]
1967-10 A
1967 Feb 8.33
[02669]
70 years
VDB-LC4300B6
12-sided
frustum 195
1.64 long
1.31 to
1.10 dia
1967 Feb 8.5
2001 Feb 15.91
98.34
98.99
101.55
101.05
72l0
7187
796
771
868
845
0.005
0.005
45
80
Burner 2
2nd stage
1967-10 B
[02741]
Sphere-cone
66
1.32 long
0.94 dia
1967 May 24.1
2001 Feb 13.80
98.83
98.90
10l.53
101.00
7209
7185
790
766
871
846
0.006
0.006
98
53
*
$
Soyuz capsule testflight #3
Moon orbit
2004 December 31 – version 1.01
1967 Feb 8.33
70 years
Feb 8.91
21
216
2740
216
1791
0.287
-$
Feb 12.76
20.93
208
2687
55
1844
0.333
-$
Aug 30.82
20.9
131
1968
144
316
0.044
-$
crashing into moon from selenocentric orbit. Impact 91.7W, 14.6N
Missed moon
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
L
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
(Revised 2001)
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
128
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Diademe 1*(D-1C)
[Diamant A #3]
1967-11 A
1967 Feb 8.40
[02674]
50 years
HAM-Brigitte
Cylinder +
4 vanes 22.7
0.20 long
0.5 dia
1967 Feb 28.5
1973 Feb 1.0
2001 Feb 18.18
39.98
39.98
39.94
104.17
103.7
110.52
7338
7315
7162
569
561
539
1350
1312
1028
0.053
0.051
0.003
34
Diademe 1*
Diamant 3rd stage
1967-11 B
[02671]
1967 Feb 8.40
100 years
Cylinder
68
2.1 long
0.65 dia
1967 Mar 6.0
2001 Feb 17.17
39.92
39.97
103.97
101.77
7328
7220
574
549
1323
1134
0.051
0.041
140
D
Fragments*
l967-11 C-Q
13 pieces, all have decayed
D
R
Cosmos 141
[Voskhod 11A57]
1967-12 A
[02670]
PLE
1967 Feb 8.43
7.79 days
1967 Feb 16.22
Spherecylinder
5530?
5 long?
2.4 dia
1967 Feb 13.4
72.85
89.74
6639
205
316
0.008
45
D
Cosmos 141
Block I 3rd stage
1967-12 B
[02672]
1967 Feb 8.43
7.74 days
1967 Feb 16.17
Cylinder
25007
7.5 long
2.6 dia
1967 Feb 12.3
72.87
89.25
6615
197
276
0.006
35
D
Cosmos 142
[Kosmos 11K63]
1967-13 A
[02678]
KY-LC86/1
1967 Feb 14.42
142.19 days
1967 Jul 6.61
Ellipsoid
400?
1.8 long
1.2 dia
1967 Feb 14.6
1967 May 23.5
48.3
48.39
100.25
94.61
7150
6880
207
197
1336
807
0.079
0.044
101
-
D
Cosmos 142
2nd stage
1967-13 B
[02679]
1967 Feb 14.42
121.28 days
1967 Jun 15.70
Cylinder
1500?
8 long
1.65 dia
1967 Feb 14.6
1967 May 8.0
48.4
48.38
100.35
94.44
7156
6872
210
199
1346
788
0.079
0.043
103
-
L
Diademe 2 (D1-D)
[Diamant A #4]
1967-14 A
1967 Feb 15.44
[02680]
200 years
HAM-Brigitte
Cylinder +
4 vanes 22.7
0.20 long
0.5 dia
1967 Apr 15.5
2001 Feb 15.89
39.45
39.45
110.01
108.17
7614
7521
591
579
1881
1705
0.085
0.075
263
Diademe 2
Diamant stage
1967-14 B
02682]
1967 Feb 15.44
100 years
Cylinder
68
2.1 long
0.65 dia
1967 Apr 15.5
2001 Feb 17.57
39.45
39.46
l10.09
108.43
7618
7546
590
580
1890
1754
0.085
0.078
181
Fragments
1967-14 C-P
12 pieces, 8 have decayed
* Originally listed on page 127
2004 December 31 – version 1.01
For orbital information see extra pages at the end of the year
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Discoverer 113
1967-15 A
(KH 4A-50)
[02686]
[Thor 2C 493
VDB-SLC3W
Agena D SS-01B 1635]
1967 Feb 22.92
17.02 days
1967 Mar 11.94
Cylinder
1st 14 days
1500?
8 long?
1.5 dia
1967 Feb 23.8
1967 Mar 10.73
80.03
80.01
90.12
88.57
D
KH 8-04
[Titan 3B-4
Agena D]
1967-16 A
[02687]
VDB-SLC4W
1967 Feb 24.83
10.15 days
1967 Mar 6.98
Cylinder
3000?
8 long?
1.5 dia
1967 Feb 25.4
1967 Mar 2.80
l06.98
107.01
D
R
Cosmos 143
[Vostok 8A92]
1967-17 A
[02693]
BAI-LC1
1967 Feb 27.35
7.89 days
1967 Mar 7.24
Spherecylinder
4750?
4.3 long
2.4 dia
1967 Feb 27.7
1967 Mar 7.11
D
Cosmos 143
Block E 3rd stage
1967-17 B
[02694]
1967 Feb 27.35
9.78 days
1967 Mar 9.13
Cylinder
1440
3.8 long
2.6 dia
D
Cosmos 144
(Meteor)
[Vostok 8A92M]
1967-18 A
[02695]
PLE
1967 Feb 28.61
5677 days
1982 Sep 14
Cylinder +
2 vanes
2000?
D
Cosmos 144
Block E 3rd stage
1967-18 B
[02696]
1967 Feb 28.61
8221 days
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Page
129
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6658
6582
180
165
380
241
0.015
0.006
159
101
90.02
89.47
6653
6627
135
135
414
361
0.021
0.017
138
123
64.99
64.98
89.53
89.33
6629
6620
204
199
297
283
0.007
0.006
15
12
1967 Feb 28.5
1967 Mar 8.27
65.02
64.98
89.65
88.15
6635
6562
217
174
297
192
0.006
0.001
55
84
5 long?
1.5 dia?
1967 Feb 28.8
1982 Sep 14.54
81.25
81.11
96.88
87.63
6987
6536
574
153
644
162
0.005
0.0007
274
203
Cylinder
1440
3.8 long
2.6 dia
1967 Mar 2.2
1989 Sep 1.34
81.21
81.15
97.01
87.20
6993
6514
521
128
709
143
0.013
0.001
190
95
then 700?
1989 Sep 1
D
Fragment
1967-18 C
[03095]
1971 Apr 8
1500 days
1971 Apr 7.55
81.15
88.85
6596
197
238
0.003
121
D
Cosmos 145
[Kosmos 11K63]
1967-19 A
[02697]
KY-LC86/1
1967 Mar 3.28
371.11 days
1968 Mar 8.39
Ellipsoid
250
1.8 long
1.2 dia
1967 Mar 3.7
1967 Nov 8.0
1968 Jan 8.0
48.42
49.42
48.35
l08.60
99.96
96.51
7544
7136
6972
215
2014
197
2116
1312
991
0.126
0.078
0.057
101
-
D
Cosmos 145
2nd stage
1967-19 B
02698]
1967 Mar 3.28
272.86 days
1967 Dec 1.14
Cylinder
1500?
8 long
1.65 dia
1967 Mar 3.7
1967 Sep 8.0
1967 Oct 23.7
48.40
48.39
48.37
108.33
100.55
96.15
7533
7165
6954
213
203
194
2096
1371
958
0.125
0.081
0.055
102
-
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
130
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
OSO 3
[Thor Delta C
431 #46]
1967-20 A
[02703]
CC-LC17A
1967 Mar 8.68
5506 days
1982 Apr 4
Nonagon
281
0.94 long
1.12 dia
1967 Mar 9.6
1972 Feb 1.0
1982 Apr 4.41
32.87
32.87
32.83
95.53
94.98
87.73
6928
6900
6541
534
510
160
564
533
164
0.002
0.002
0.0002
200
284
D
OSO 3
Delta 3rd stage
1967-20 B
[02704]
1967 Mar 8.68
1137.71 days
1970 Apr 19.39
Cylinder
24
1.5 long
0.46 dia
1967
1968
1969
1970
9.6
14.5
16.0
19.14
32.86
32.86
32.86
32.81
95.48
94.96
93.47
88.05
6925
6899
6824
6557
540
510
441
175
554
531
451
181
0.001
0.001
0.001
0.0004
206
327
D
Fragment
1967-20 C
[02987]
1970 Jan 30
1059 days
1970 Jan 14.87
32.82
90.03
6655
276
276
0
152
D
Cosmos 146*
[Proton 8K82K
227-01 / 11S824]
1967-21 A
[02705]
BAI-LC81L
1967 Mar 10.54
0.99 day
1967 Mar 11.53
Spherecylinder + 2
wings 5375?
5.3 long
2.2 dia
1967 Mar 10.7
51.44
89.2
6615
177
296
0.009
92
D
Service
Module?
1967-21 B
[02709]
1967 Mar 10.54
8.65 days
1967 Mar 19.19
Cylinder + 2
wings? 2615?
3.0 long
2.3 dia?
1967 Mar 15.0
51.52
89.16
6613
175
294
0.009
107
D
Cosmos 146
3rd stage
1967-21 C
[02815]
1967 Mar 10.54
1 day
1967 Mar 11
Cylinder
6.5 long?
1967 Mar 11.52
51.51
89.22
6614
184
287
0.008
101
D
Descent
module?
1967-21 D
[NNA]
1967 Mar 10.54
8.35 days
1967 Mar 18.89
Spheroid?
2760?
2.3 dia?
1967 Mar 15.0
51.51
89.15
6612
176
292
0.009
-
D
R
Cosmos 147
[Vostok 8A92]
1967-22 A
[02710]
PLE-LC41/1
1967 Mar 13.51
7.76 days
1967 Mar 21.27
Spherecylinder
4750?
4.3 long
2.4 dia
1967 Mar 14.1
64.57
89.42
6626
195
301
0.008
39
D
Cosmos 147
Block E 3rd stage
1967-22 B
[02711]
1967 Mar 13.51
8.78 days
1967 Mar 22.29
Cylinder
1440
3.8 long
2.6 dia
1967 Mar 17.2
64.58
89.27
6617
206
272
0.005
74
D
Cosmos 148
[Kosmos 11K63]
1967-23 A
[02712]
PLE-LC133/1
1967 Mar 16.74
51.77 days
1967 May 7.51
Ellipsoid
400?
1.8 long
1.2 dia
1967 Mar 19.6
1967 May 6.06
71.00
70.97
91.26
88.30
6715
6569
270
181
404
200
0.010
0.001
68
335
D
Cosmos 148
2nd stage
1967-23 B
[02713]
1967 Mar 16.74
28.66 days
1967 Apr 14.40
Cylinder
1500?
8 long
1.65 dia
1967 Mar 19.4
1967 Apr 13.45
71.02
71.00
91.08
88.35
6706
6572
274
193
381
193
0.008
0
69
0
*
Cosmos 146 was a Zond test flight and apparently split into 2 modules on 1967 Mar 11.53 while over Tyuratam (1967-21 D retained the 21 A designation in USA)
2004 December 31 – version 1.01
Mar
Mar
Sep
Apr
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
131
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 149
[Kosmos 11K63]
1967-24 A
[02714]
KY-LC86/1
1967 Mar 21.42
17.23 days
1967 Apr 7.70
Ellipsoid +
annular tail
300?
6.5 long
1.2 dia
1967 Mar 23.1
1967 Apr 5.85
48.40
48.39
89.76
88.50
6643
6579
245
201
285
201
0.003
0
277
0
D
Cosmos 149
2nd stage
1967-24 B
[02716]
1967 Mar 21.42
3.05 days
1967 Mar 24.47
Cylinder
1500?
8 long
1.65 dia
1967 Mar 22.03
1967 Mar 23.8
48.45
48.44
89.30
88.43
6618
6579
222
181
267
221
0.003
0.003
122
273
D
Fragments
1967-24 C-T
16 pieces, all have decayed
D
R
Cosmos 150
[Voskhod 11A57]
1967-25 A
[02715]
PLE
1967 Mar 22.53
7.75 days
1967 Mar 30.28
Spherecylinder
5530?
5 long?
2.4 dia
1967 Mar 24.1
1967 Mar 26.71
65.64
65.64
90.04
89.98
6655
6652
204
199
350
347
0.011
0.011
54
52
D
Cosmos 150
Block I 3rd stage
1967-25 B
[02718]
1967 Mar 22.53
8.32 days
1967 Mar 30.85
Cylinder
2500?
7.5 long
2.6 dia
1967 Mar 24.1
1967 Mar 29.33
65.67
65.63
89.65
88.18
6636
6563
191
156
324
214
0.0l0
0.004
39
33
Intelsat 2-3
[Thor Delta E1
470 #47]
1967-26 A
[02717]
CC-LC17B
1967 Mar 23.06
> million years
Cylinder
87
0.67 long
1.42 dia
1967 Apr 7.7
1977 May 13.0
2001 Feb 14.52
1.37
7.30
13.20
1434
1434.95
1436.62
42l07
42142
42175
35687
35687
35700
35771
35841
35893
0.001
0.002
0.002
81
313
156
D
Intelsat 2-3
Delta 2nd stage
1967-26 B
[02719]
1967 Mar 23.06
106.4 days
1967 Jul 7.5
Cylinder
400?
4.9 long
1.43 dia
1967 Mar 24.0
1967 May 31.5
1967 Jun 21.97
28.80
28.76
28.74
92.98
91.16
89.95
6804
6716
6651
242
231
217
610
445
327
0.027
0.0l6
0.008
145
113
D
Intelsat 2-3
Delta 3rd stage
1967-26 C
[11984]
1967 Mar 23.06
40 years ?
Cylinder
24
1.5 long
0.46 dia
1967 Mar 25.0
1980 Nov 1.0
2001 Apr 7.45
26.68
26.9
26.06
669.8
232.4
326.70
25351
12521
15713
289
158
294
37656
12128
18375
0.737
0.478
0.575
178*
272
*Approximate orbit.
2004 December 31 – version 1.01
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
132
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 151
(Strela-2)
[Kosmos 11K65]
1967-27 A
[02720]
BAI-LC41
1967 Mar 24.49
8809 days
1991 May 6
Cylinder +
paddles
850
2 long?
1 dia?
1967 Mar 24.9
1991 May 6.75
56.07
56.00
97.14
87.20
7002
6514
596
130
652
141
0.004
0.0008
125
273
D
Cosmos 151
2nd stage
1967-27 B
[02721]
1967 Mar 24.49
7772 days
1988 Jul 3
Cylinder
2200?
7.4 long
2.4 dia
1967 Mar 31.5
1988 Jul 3.63
56.06
56.01
97.13
86.83
7001
6496
594
115
653
121
0.004
0.0004
288
D
Fragments
1967-27 C
1967-27 D
[02776]
[02797]
1967 Nov 28
1970 Oct 12
249 days
1298 days
1967 Nov 17.87
1970 Aug 20.76
56.13
56.11
90.98
92.33
6702
6767
304
358
342
420
0.003
0.005
138
69
D
Cosmos 152
[Kosmos 11K63]
1967-28 A
[02722]
PLE-LC133/1
1967 Mar 25.29
132.88 days
1967 Aug 5.17
Ellipsoid
400?
1.8 long
1.2 dia
1967 Mar 26.6
1967 Jun 23.0
70.98
70.99
92.13
90.63
6758
6684
272
245
488
367
0.016
0.009
78
-
D
Cosmos 152
2nd stage
1967-28 B
[02723]
1967 Mar 25.29
57.78 days
1967 May 22.07
Cylinder
1500?
8 long
1.65 dia
1967 Mar 26.6
1967 May 8.0
71.00
70.97
92.00
90.27
6752
6667
273
242
475
335
0.015
0.007
79
-
D
Discoverer 114
1967-29 A
(KH 4A-51)
[02736]
[Thor 2C 501
VDB-SLC3W
Agena D SS-01B 1636]
1967 Mar 30.79
17.65 days
1967 Apr 17.44
Cylinder
1500?
8 long?
1.5 dia
1967 Mar 3O.9
85.03
89.45
6625
167
326
0.012
181
D
R
Cosmos 153
[Vostok 8A92]
1967-30 A
[02740]
PLE-LC41/1
1967 Apr 4.58
7.74 days
1967 Apr 12.32
Spherecylinder
4750?
4.3 long
2.4 dia
1967 Apr 5.3
64.59
89.26
6617
199
279
0.006
36
D
Cosmos 153
Block E 3rd stage
1967-30 B
[02742]
1967 Apr 4.58
7.06 days
1967 Apr 11.64
Cylinder
1440
3.8 long
2.6 dia
1967 Apr 7.3
64.58
89.09
6608
210
250
0.003
-
D
ATS 2
[Atlas SLV-3 5102
Agena D 6152]
1967-31 A
[02743]
CC-LC12
1967 Apr 6.14
880.81 days
1969 Sep 2.95
Cylinder
370
1.83 long
1.42 dia
1967 Apr 9.2
1968 Mar 12.4
1969 Feb 15.3
28.40
28.42
28.27
218.9
177.5
132.3
12029
l0486
8601
178
176
169
11124
8040
4276
0.455
0.375
0.239
15
-
D
ATS 2
Agena D stage
+ OPS 8916
1967-31 B
[02744]
1967 Apr 6.14
450.1 days
1968 Jun 29.2
Cylinder
700?
6 long?
1.5 dia
1967 Apr 9.8
1968 Mar 9.2
1968 May 8.0
28.51
28.39
28.30
218.2
157.9
l29.4
11999
9739
8474
149
147
140
11092
6575
4052
0.456
0.330
0.231
43
-
D
Cosmos 154* #
[Proton 8K82K
228-01 / 11S824]
1967-32 A
[02745]
BAI-LC81L
1967 Apr 8.38
2.2 days
1967 Apr l0.6
Spherecylinder + 2
wings 5375?
5.3 long
2.2 dia
1967 Apr 8.7
51.30
88.5
6581
183
223
0.003
100
*
#
Cosmos 154 and Cosmos 146 were Zond test flights.
Originally listed on page 133.
2004 December 31 – version 1.01
1967-32 continued on page 133.
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
1967 Apr 10.2
51.35
87.70
Page
133
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6542
157
170
0.001
-
D
Cosmos 154
third stage
1967-32 B
[02747]
1967 Apr 8.38
2.3 days
1967 Apr 10.7
Cylinder
6.5 long?
4 dia
D
Fragment
1967-32 C
[02746]
1967 Apr 19
11 days
D
R
Cosmos 155
[Voskhod 11A57]
1967-33 A
[02750]
BAI
1967 Apr 12.46
7.98 days
1967 Apr 20.44
Spherecylinder
553O?
5 long?
2.4 dia
1967 Apr 12.8
51.30
89.11
6611
193
272
0.006
17
D
Cosmos 155
Block I 3rd stage
1967-33 B
[02751]
1967 Apr 12.46
4.02 days
1967 Apr 16.48
Cylinder
2500?
7.5 long
2.6 dia
1967 Apr 13.5
51.78
89.00
6605
l94
260
0.005
-
D
Fragments
1967-33 C
1967-33 D
[02752]
[02753]
1967 Apr 13
1967 Apr 16
1 day
4 days
Transit 0-12 (15)
[Scout A S154C]
1967-34 A
[02754]
VDB-SLC5
1967 Apr 14.14
1000 years
Octagon +
4 vanes 60?
0.25 long
0.46 dia
1967 Apr 14.3
2001 Feb 15.93
90.23
90.12
l06.60
106.22
7446
7430
1053
1037
1083
1066
0.002
0.002
101
167
Altair 4th stage
1967-34 B
[02755]
1967 Apr 14.14
1000 years
Cylinder
24
1.5 long
0.46 dia
1967 May 2.4
2001.Feb 18.45
90.25
90.13
106.59
106.40
7445
7438
1052
1044
1083
1075
0.002
0.002
58
240
Fragments
1967-34 C-H
6 pieces, 2 have decayed
D
For orbital information see extra pages at the end of the year
Surveyor 3
1967-35 A
[Atlas LV-3C AC-12[02756]
Centaur D 292D]
CC-LC36B
1967 Apr 17.30
64.99 days
1967 Apr 20.00
Pyramid frame
302
3.05 high
Soft-landed on moon 1967 Apr 17 at 0h 4m 17s. Impact: 3.20S; 21.38W
4.27 dia
Retrorocket (0.94 dia sphere, 66 kg) separated and landed close by.
(of tripod)
Surveyor 3
Centaur 12 stage
1967-35 B
[02764]
1967 Apr 17.30
Cylinder
2000
9.1 long
3.05 dia
In highly eccentric orbit. Period about 10 days.
Essa 5
(TOS-C)(TIROS 15)
[Thor Delta E
484 #48]
1967-36 A
[02757]
VDB-SLC2E
1967 Apr 20.47
10000 years
Cylinder
145
0.56 long
1.07 dia
1967 Apr 21.3
2001 Feb 18.21
101.97
101.87
113.63
113.52
7770
7767
1361
1355
1423
1421
0.004
0.004
353
120
Essa 5
Delta 3rd stage
1967-36 B
[02758]
1967 Apr 20.47
5000 years
Cylinder
24
1.5 long
0.46 dia
1967 Apr 22.6
2001 Feb 16.58
101.95
102.02
113.63
113.50
7770
7766
1361
1356
1423
1419
0.004
0.004
349
176
Essa 5
De-spin weight
1967-36 C
[02976]
1967 Apr 20.47
2001 Feb 16.52
102.20
112.33
7712
1257
1410
0.010
230
Essa 5
De-spin weight
1967-36 D
[02977]
1967 Apr 20.47
2001 Feb 16.97
101.86
114.58
7815
1390
1483
0.006
328
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
134
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
M
P
Soyuz 1 *
[Soyuz 11A511]
1967-37 A
[02759]
BAI-LC1
1967 Apr 23.03
1.11 days
1967 Apr 24.14
Spherecylinder + 2
wings 6450
7.5 long
2.2 dia
1967 Apr 23.4
51.64
88.52
6583
198
211
0.001
324
D
Soyuz 1
Block I 3rd stage
1967-37 B
[02760]
1967 Apr 23.03
1.88 days
1967 Apr 24.91
Cylinder
2500?
7.5 long
2.6 dia
1967 Apr 23.6
51.66
88.39
6576
185
211
0.002
328
D
San Marco 2 **
[Scout B S153C]
1967-38 A
[02761]
SMC
1967 Apr 26.42
171.l0 days
1967 Oct 14.52
Sphere
129
0.66 dia
1967 Apr 26.6
1967 Aug 14.5
2.89
2.89
93.93
91.76
6856
6745
217
199
738
535
0.038
0.025
296
-
D
San Marco 2
Scout 4th stage
1967-38 B
[02771]
1967 Apr 26.42
33 days
1967 May 29
Cylinder
24
1.5 long
0.46 dia
1967 Apr 30.5
3.16
93.52
6835
204
710
0.037
349
D
Cosmos 156
(Meteor)
[Vostok 8A92M]
1967-39 A
[02762]
PLE
1967 Apr 27.53
8215 days
1989 Oct 23
Cylinder +
2 vanes
2000?
5 long?
1.5 dia?
1967 Apr 28.8
81.17
96.96
6992
593
635
0.003
275
D
Cosmos 156
Block E 3rd stage
1967-39 B
[02763]
1967 Apr 27.53
8949 days
1991 Oct 27
Cylinder
1440
3.8 long
2.6 dia
1967 Apr 29.4
1991 Oct 27.35
81.23
81.12
97.20
87.38
7003
6524
540
141
710
150
0.012
0.0007
190
290
Vela Hotel 7
[Titan 3C-10]
1967-40 A
[02765]
CC-LC41
1967 Apr 28.42
>million years
Icosahedron
231
1.17 long
1.42 dia
1967 May 1.4
1971 May 3.80
33.06
37.35
6671.8
6689.67
117353 107337 114612 0.031
117606 102990 119465 0.070
87
250
Vela Hotel 8
1967-40 B
[02766]
1967 Apr 28.42
> million years
Icosahedron
231
1.17 long
1.42 dia
1967 May 1.4
1974 Sep 8
33.06
37.17
6671.8
6688.75
117353 107337 114612 0.031
117830 99054 123848 0.105
87
73
ERS 18
(ORS 4)
1967-40 C
[02767]
1967 Apr 28.42
million years?
Octahedron
9
0.28 side
1967 May 1.4
1968 May 31
32.8
35.67
2829.6
2831.98
66295
66306
8604
10236
111229 0.774
109619 0.749
173
184
ERS 20
(OV5-3)
1967-40 D
[02768]
1967 Apr 28.42
million years?
Octahedron
8.6
0.28 side
1967 May 1.4
1968 May 31
32.8
35.12
2829.6
2830.97
66295
66290
8604
10205
111229 0.774
109618 0.750
173
182
ERS 27
(OV5-1)
1967-40 E
[02769]
1967 Apr 28.42
million years?
Octahedron
7.4
0.28 side
1967 May 1.4
1980 Feb 10.25
32.8
36.76
2829.6
2829.55
66295
66268
8604
4237
111229 0.774
115542 0.840
173
25
Transtage 10
[Titan 3C]
1967-40 F
[02770]
1967 Apr 28.42
million years?
Cylinder
1500?
6 long?
3 dia
1967 Apr 28.59
32.85
2831.22
66294
8589
111242 0.774
173
* Crashed after unstable re-entry (one solar panel may not have unfolded).
** First satellite launch from Indian 0cean platform (Kenya).
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
(Revised 2001)
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
135
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
2700
77
6000
3943
0.27
0.516
-
Lunar Orbiter 4
[Atlas SLV-3 5804
Agena D 6633]
1967-41 A
[02772]
CC-LC13
1967 May 4.93
154 days
1967 Oct 6.5
Truncated
cone
390
1.68 high
1.52 dia
1967 May 8.64
85.48
720
6090
1967 Jun 8.94
84.4
344
3748
Decayed naturally from selenocentric orbit
Lunar Orbiter
Agena D stage
1967-41 B
[NNA]
1967 May 4.93
Cylinder
1000?
7 long
4.52 dia
Missed moon; initially in earth orbit
D
Ariel 3 (UK 3)
[Scout A S155C]
1967-42 A
[02773]
VDB-SLC5
1967 May 5.67
1318.37 days
1970 Dec 14.04
Cylinder
4 paddles
89.8
0.91 long
0.76 dia
1967 May 5.8
1969 Sep 16.0
1970 May 1.0
80.17
80.18
80.1
95.69
94.33
93.40
6931
6863
6818
497
451
414
608
518
466
O.008
0.005
0.004
170
-
D
Ariel 3
Scout 4th stage
1967-42 B
[02774]
1967 May 5.67
1309.98 days
1970 Dec 5.65
Cylinder
24
1.5 long
0.46 dia
1967 May 9.1
1969 Sep 16.0
1970 May 1.0
80.18
80.18
80.1
95.80
94.40
93.42
6935
6866
93.42
494
449
412
619
527
470
0.009
0.006
0.004
161
-
D
Fragments
1967-42 C
1967-42 D
[02859]
[02860]
1968 May 5
1968 Mar 9
366 days
309 days
D
Discoverer 115
1967-43 A
(KH 4B-02)
[02779]
[Thor 2L 508
VDB-SLC1E
Agena D SS-01B 1634]
1967 May 9.91
64.62 days
1967 Jul 13.53
Cylinder
2000?
8 long?
1.5 dia?
1967 May 10.1
85.10
94.36
6867
200
777
0.042
154
D
Hitchhiker 14
1967-43 B
[02780]
1967 May 9.91
9441 days
1993 Mar 14
Octagon?
60?
0.3 long?
0.9 dia?
1967 May 10.0
85.10
98.38
7060
555
809
0.013
173
D
Fragment
1967-43 C
[02824]
1967 Jun 6
28 days
D
R
Cosmos 157
[Vostok 8A92]
1967-44 A
[02781]
BAI-LC1
1967 May 12.44
7.93 days
1967 May 20.37
Spherecylinder
4750?
4.3 long
2.4 dia
1967 May 12.8
51.26
89.60
6634
249
262
0.001
67
D
Cosmos 157
Block E 3rd stage
1967-44 B
[02782]
1967 May 12.44
11.94 days
1967 May 24.38
Cylinder
1440
3.8 long
2.6 dia
1967 May 15.7
51.28
89.40
6625
234
260
0.002
121
D
Fragments
1967-44 C
1967-44 D
1967-44 E
[02783]
[02784]
[02785]
1967 May 13
1967 May 12
1967 May 14
1 day
<1 day
2 days
Cosmos 158
[Kosmos 11K65M]
1967-45 A
[02801]
PLE-LC132
1967 May 15.46
200 years
Cylinder?
750?
1.4 long
2.0 dia?
1967 May 15.7
2001 Feb 13.76
74.03
74.04
100.40
100.27
7158
7150
738
731
822
812
0.006
0.006
148
100
Cosmos 158
2nd stage
1967-45 B
[02802]
1967 May 15.46
200 years
Cylinder
2200?
7.4 long
2.4 dia
1967 May 16.1
2001 Feb 18.16
74.01
74.01
100.59
99.95
7168
7135
732
707
847
806
0.008
0.007
148
134
Fragments
1967-45 C
1967-45 D
[02823]
[03737]
1991 Dec 21
1989 Nov 16
8986 days
8221 days
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Page
136
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 159
[Molniya 8K78M
Ya716-56]
1967-46 A
[02805]
BAI
1967 May 16.91
3832 days?
1977 Nov 11?
Cylinder
4490 full?
1465 empty?
3.0 long?
2.3 dia?
1967 May 31.5
1970 May 16.5
1974 Mar 1.0
51.60
53.38
53.6
1174.2
1174.1
1174.0
36872
36864
36865
350
2502
1124
60637
58470
59849
0.818
0.759
0.796
-
D
Cosmos 159
Block I 3rd stage
1967-46 B
[02804]
1967 May 16.91
12.70 days
1967 May 29.61
Cylinder
2500?
7.5 long
2.6 dia
1967 May 17.3
51.84
90.80
6695
203
431
0.017
70
D
Cosmos 159 *
SL-06 4th stage
casing
1967-46 C
[02803]
1967 May 16.91
17.00 days
1967 Jun 2.91
Irregular
2 long?
1 dia?
1967 May 18.2
51.74
90.50
6680
208
395
0.014
72
D
Cosmos 159
SL-06 ullage
motor
1967-46 D
[02808]
1967 May 16.91
6 days
1967 May 22
D
Cosmos 159
SL-06 ullage
motor
1967-46 E
[02809]
1967 May 16.91
6 days
1967 May 22
D
Cosmos 159
Block L 4th stage
1967-46 F
[02924]
1967 May 16.91
3986 days
1978 Apr 14
Annulus
1875 full?
215 empty?
0.62 long?
1.23 to
2.25 dia?
1967 Jun 13.0
1970 May 16.5
1974 Mar 1.0
50.4
53.37
53.6
1171.0
1171.0
1171.1
36802
36801
36804
380
2490
1129
60467
58356
59722
0.816
0.759
0.796
-
D
Cosmos 160**
[R-36-0]
1967-47 A
[02806]
BAI
1967 May 17.67
0.8 day
1967 May 18.5
Cylinder?
2 long?
1 dia?
1967 May 17.8
49.66
87.58
6535
137
177
0.003
-
D
Cosmos 160
2nd stage
1967-47 B
[02810]
1967 May 17.67
0.8 day
1967 May 18.5
Cylinder
15007
8 long?
2.5 dia?
Transit 0-13 (16)
[Scout A S156C]
1967-48 A
[02807]
VDB-SLC5
1967 May 18.38
1000 years
Octagon +
4 vanes 60?
0.25 long
0.46 dia
1967 May 19.8
2001 Feb 16.82
89.57
89.60
lO7.04
106.73
7467
7454
1074
1059
1105
1091
0.002
0.002
187
25
Altair rocket
Scout 4th stage
1967-48 B
[02811]
1967
1000
Cylinder
24
1.5 long
0.46 dia
1967 Jun 2.7
2001 Feb 16.85
89.58
89.59
l07.04
106.80
7466
7457
1073
1062
1106
1094
0.002
0.002
144
325
Fragments
1967-48 C-F
4 pieces, 2 have decayed
D
R
Cosmos 161
[Voskhod 11A57]
1967-49 A
[02812]
PLE
1967 May 22.58
7.79 days
1967 May 30.37
Spherecylinder
5530?
5 long?
2.4 dia
1967 May 24.8
65.64
89.71
6639
201
321
0.009
51
D
Cosmos 161
Block I 3rd stage
1967-49 B
[02814]
1967 May 22.58
6.07 days
1967 May 28.65
Cylinder
2500?
7.5 long
2.6 dia
1967 May 24.3
65.64
89.45
6626
195
301
0.008
42
May 18.38
years
* Probably a test of the Soyuz propulsion module.
** Disintegrated into more than 16 pieces on first revolution
2004 December 31 – version 1.01
Orbit similar to 1967-47 A
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
137
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
KH 7-37 Gambit
[Atlas SLV-3
7127-Agena D]
1967-50 A
[02813]
VDB-SLC4E
1967 May 22.77
8.18 days
1967 May 30.95
Cylinder
700?
6.3 long
1.5 dia
1967 May 28.4
91.49
88.82
6592
135
293
0.012
117
D
LOGACS *
1967-50 B
[02816]
1967 May 22.77
4.9 days
1967 May 27.7
500?
1.5 dia?
1967 May 27.0
91.49
88.42
6572
148
240
O.O07
125
D
Explorer 34
(Imp 5)
[Thor Delta E1
486 #49]
1967-51 A
[02817]
VDB-SLC2E
1967 May 24.59
710.47 days
1969 May 4.06
Octagon +
4 vanes 75
0.25 long
0.71 dia
1967 May 24.6
1968 Jul 26.5
1969 Feb 15.5
67.17
66.97
68.50
6346.1
6222.8
6218.3
113691 242
112071 4006
112015 2031
214383 O.942
207380 0.907
209242 0.925
180
-
D
Explorer 34
rocket
1967-51 B
[NNA]
1967 May 24.59
23 months?
1969 May ?
Cylinder
24
1.5 long
0.46 dia
D
Molniya-1 5
[Molniya 8K78M]
1967-52 A
[02822]
BAI
1967 May 24.95
1647 days
1971 Nov 26
Windmill
1000?
3.4 long
1.6 dia
1967 May 29.9
1969 Mar 31.7
1970 Oct 31.7
64.88
64.87
64.8
715.5
710.4
711.87
26500
26376
26408
460
1188
567
39785
38807
39492
0.742
0.713
0.737
285
-
D
Molniya-1 5
Block I 3rd stage
1967-52 B
[02818]
1967 May 24.95
11 days
1967 Jun 5
Cylinder
2500?
7.5 long
2.6 dia
1967 May 25.4
64.87
90.88
6696
197
438
0.018
55
D
Molniya-1 5
SL-06 4th stage
casing
1967-52 C
[02819]
1967 May 24.95
21.98 days
1967 Jun 15.93
Irregular
2 long?
1 dia?
1967 May
64.85
91.26
6716
203
472
0.020
62
D
Molniya-1 5
SL-06 ullage
Motor
1967-52 D
[02820]
1967 May 24.95
4 days
1967 May 28
D
Molniya-1 5
SL-06 ullage
Motor
1967-52 D
[02821]
1967 May 24.95
4 days
1967 May 28
D
Molniya-1 5
Block L 4th stage
1967-52 F
[03224]
1967 May 24.95
1667 days
1971 Dec 16
Cy1inder
440
2.0 long
2.0 dia
1969 May 16.3
1970 Dec 1.0
64.37
64.8
709.62
709.54
26354
26352
1194
554
38758
39394
0.713
0.737
-
D
Fragment
1967-52 G
[05439]
1971 Sep 1
1561 days
*
Low Gravity Accelerometer Calibration system.
2004 December 31 – version 1.01
Orbit similar to 1967-51 A
25.8
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Ferret Surcal 160 1967-53 A
[Thor 2A 443 Agena [02826]
D SS-01B 2704]
VDB-SLC2W
1967 May 31.40
500 years
Sphere
2.48
0.51 dia
1967 Jun 1.5
2001 Feb 13.65
69.98
69.94
103.45
100.92
Ferret 16
Agena D stage
1967-53 B
[02825]
1967 May 31.40
500 years
Cylinder
700?
6 long?
1.51 dia
1967 Jun 1.1
2001 Feb 14.54
69.98
69.97
GGSE 4
1967-53 C
[02828]
1967 May 31.40
500 years
Ellipsoid?
4?
0.3 dia?
1967 Jun 1.1
2001 Feb 18.22
GGSE 5
1967-53 D
[02834]
1967 May 31.40
500 years
Ellipsoid?
4?
0.3 dia?
Timation 1*
(ORS 20)
1967-53 E
[02847]
1967 May 31.40
500 years
Rectangular
box 38
0.81 x
0.41 x
Surcal 159
Calsphere 3
1967-53 F
[02872]
1967 May 31.40
500 years
Sphere
38
Ferret
Surcal 152
1967-53 G
[02873]
1967 May 31.40
500 years
-
Ferret
Surcal 153
1967-53 H
[02874]
1967 May 31.40
500 years
Surcal 150B
1967-53 J
[02909]
1967 May 31.40
50 years
Timation 1 Fragm
1967-53 K
[19245]
D
R
Cosmos 162
[Voskhod 11A57]
1967-54 A
[02827]
BAI
1967 Jun 1.45
7.99 days
1967 Jun 9.44
Spherecylinder
5530?
D
Cosmos 162
Block I 3rd stage
1967-54 B
[02829]
1967 Jun 1.45
3.06 days
1967 Jun 4.51
D
Fragment
1967-54 C
[02830]
*
TIMe/navixATION satellite
2004 December 31 – version 1.01
Page
138
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7299
7181
914
787
928
807
0.001
0.001
343
343
103.55
103.15
7305
7286
919
900
934
914
0.001
0.001
33
294
69.98
69.97
103.45
103.13
7300
7285
915
899
929
914
0.001
0.001
13
293
1967 Jun 5.7
2001 Feb 18.24
69.98
69.97
103.45
103.21
7300
7289
915
904
929
917
0.001
0.001
20
301
1968 Jan 15.5
2001 Feb 18.06
69.91
69.96
103.39
102.88
7298
7274
915
888
926
902
0.00l
0.001
263
1967 Jun 15.5
2001 Feb 18.54
69.91
69.97
103.38
103.05
7297
7281
916
896
921
910
0.001
0.001
273
-
1968 Jan 15.5
2001 Feb 18.20
69.91
69.97
103.40
103.12
7299
7284
915
898
927
913
0.001
0.001
289
-
-
1968 Jan 15.5
2001 Feb 17.69
69.91
69.97
103.39
103.18
7298
7288
915
903
926
916
0.00l
0.001
300
Sphere
1.55
0.41 dia
1968 Jan 15.5
2001 Feb 16.87
69.91
69.95
103.38
100.55
7297
7163
917
780
922
789
0.0003
0.0006
249
2001 Feb 15.23
69.96
102.18
7240
853
870
0.001
245
5 long?
2.4 dia
1967 Jun 1.7
51.81
89.19
6614
196
275
0.006
19
Cylinder
2500?
7.5 long
2.6 dia
1967 Jun 3.8
51.78
88.15
6563
159
211
0.004
9
1967 Jun 2
1 day
0.20
-
Semi
major axis
(km)
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
139
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
KH 7-38 Gambit
[Atlas SLV-3
7128-Agena D
SS-01B 4837]
1967-55 A
[02831]
VDB-SLC4E
1967 Jun 4.75
8.17 days
1967 Jun 12.92
500?
1.5 dia?
1967 Jun 6.9
1967 Jun 10.4
l04.88
104.87
90.57
90.33
6681
6668
149
145
456
434
0.023
0.022
153
139
D
Agena D
stage
1967-55 B
[02835]
1967 Jun 4.75
1 day
1967 Jun 6
Cylinder
700?
8 long?
1.5 dia
1967 Jun 5.4
104.87
90.28
6668
143
436
0.022
150
D
Cosmos 163
[Kosmos 11K63]
1967-56 A
[02832]
KY-LC86/1
1967 Jun 5.21
128.51 days
1967 Oct 11.72
Ellipsoid
400?
1.8 long
1.2 dia
1967 Jun 5.4
1967 Aug 15.8
48.38
48.39
93.07
92.01
6806
6754
244
247
611
504
0.027
0.0l9
124
-
D
Cosmos 163
2nd stage
1967-56 B
[02833]
1967 Jun 5.21
99.20 days
1967 Sep 12.41
Cylinder
1500?
8 long
1.65 dia
1967 Jun 5.9
48.43
93.05
802
254
594
0.025
1ll
D
R
Cosmos 164
[Voskhod 11A57]
1967-57 A
[02836]
PLE-LC41/1
1967 Jun 8.55
5.76 days
1967 Jun 14.31
Sphere
cylinder
5530?
5 long?
2.4 dia
1967 Jun 9.2
65.59
89.51
6629
185
317
0.010
44
D
Cosmos 164
Block I 3rd stage
1967-57 B
[02837]
1967 Jun 8.55
9.11 days
1967 Jun 17.66
Cylinder
2500?
7.5 long
2.6 dia
1967 Jun 9.2
65.65
89.37
6622
197
290
0.007
32
D
Fragment
1967-57 C
[02838]
1967 Jun 9
1 day
D
Venus 4*
(Capsule)
[Molniya 8K78M]
1967-58 A
[02840]
BAI
1967 Jun 12.11
128.15 days
1967 Oct 18.26
Sphere
383
1.2 dia
Crushed by Venus atmosphere near equator on 1967 Oct 18 at 6h 14m 6s
D
Venus 4
SL-06 4th stage
casing
1967-58 B
[02841]
1967 Jun 12.11
1.76 days
1967 Jun 13.87
Irregular
2 long?
1 dia?
1967 Jun 12.4
51.80
87.92
6553
162
188
0.002
16
D
Venus 4
Block I 3rd stage
1967-58 C
[02839]
1967 Jun 12.11
0.78 day
1967 Jun 12.89
Cylinder
2500?
7.5 long
2.6 dia
1967 Jun 12.4
51.78
88.30
6571
173
212
0.003
271
D
Fragment
1967-58 D
[02844]
1967 Jun 13
1 day
Venus 4
Rocket
1967-58 E
[NNA]
1967 Jun 12.11
Indefinitely?
Cylinder
2.0 long
Orbit unknown
D
Venus 4 *
(Compartment
1967-58 F
{NNA]
1967 Jun 12.11
128.08 days
Ellipsoid
723
1.7 long?
1.2 dia
Decayed in Venusian atmosphere 1967 Oct 18 at 4h 40m
*
Venus 4 Capsule and Compartment were joined until shortly before reaching Venus
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
140
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 165
[Kosmos 11K63]
1967-59 A
[02842]
PLE-LC133/1
1967 Jun 12.76
216.90 days
1968 Jan 15.66
Ellipsoid
400?
1.8 long
1.2 dia
1967 Jun 14.0
1967 Nov 8.0
81.89
81.88
102.08
96.13
7235
6951
198
190
1515
957
0.091
0.055
71
-
D
Cosmos 165
2nd stage
1967-59 B
[02843]
1967 Jun 12.76
142.16 days
1967 Nov 1.92
Cylinder
1500?
8 long
1.65 dia
1967 Jun 15.7
1967 Sep 15.5
81.91
81.88
l0l.88
96.73
7226
6980
197
197
1498
1007
0.090
0.058
66
-
Mariner 5
[Atlas SLV-3 5401
Agena D 6933]
1967-60 A
[02845]
CC-LC12
1967 Jun 14.25
Indefinitely
Octagonal
Cylinder 246
2.90 long
1.27 dia
Heliocentr. orbit 1.37
195*
0.579
Passed 4000 km behind Venus 1967 Oct 19.733
0.735
0.119
Mariner 5
1967-60 B
Agena D 6933 stage[02846]
1967 Jun 14.25
Indefinitely
Cylinder
1100?
7 long
Missed Venus, in heliocentric orbit
D
Cosmos 166
[Kosmos 11K63]
1967-61 A
[02848]
KY-LC86/1
1967 Jun 16.20
130.89 days
1967 Oct 25.08
Ellipsoid
+ 8 panels
400?
1.8 long
1.2 dia
l967 Jun 24.6
1967 Sep 8.0
48.43
48.42
92.84
91.78
6795
6741
281
270
553
456
0.020
0.014
159
-
D
Cosmos 166
2nd stage
1907-61 B
[02849]
1967 Jun 16.20
116.81 days
1967 Oct 11.01
Cylinder
1500?
8 long
1.65 dia
1967 Jun 17.5
1967 Sep 8.0
48.43
48.42
92.83
91.46
6794
6726
280
266
552
430
0.020
0.012
128
-
D
Discoverer 116
1967-62 A
(KH 4B-03)
[02850]
[Thor 2L 509
VDB-SLC1W
Agena D SS-01B 1633]
1967 Jun 16.90
33.16 days
1967 Jul 20.06
Cylinder
2000?
8 long?
1.5 dia
1967 Jun 17.7
80.02
89.97
6652
181
367
0.014
166
D
Hitchhiker 15 **
1967-62 B
[02851]
1967 Jun 16.90
493.12 days
1968 Oct 22.02
Octagon?
60?
0.3 long?
0.9 dia?
1967 Jun 30.8
1968 Mar 14.5
1968 Jun 30.5
80.20
80.19
80.13
94.81
93.76
92.89
6887
6835
6793
501
451
407
517
464
42.3
0.001
0.001
0.001
278
-
D
Cosmos 167 *
[Molniya 8K78M]
1967-63 A
[02852]
BAI-LC1
1967 Jun 17.11
7.99 days
1967 Jun 25.10
Cylinder
6560? full
7 long?
2.0 max
dia
1967 Jun 17.5
51.79
89.22
6616
211
264
0.004
38
D
Cosmos 167
Sl-06 4th stage
casing
1967-63 B
[02853]
1967 Jun 17.11
4.88 days
1967 Jun 21.99
Irregular
2 long?
1 dia?
1967 Jun 18.5
51.80
89.00
6605
187
266
0.006
26
D
Cosmos 167
Block L 4th stage
1967-63 C
[02856]
1967 Jun 17.11
9.32 days
1967 Jun 26.43
Cy1inder
440
2.0 long
2.0 dia
1967 Jun 17.7
51.87
88.10
6560
149
215
0.005
87
D
Cosmos 167
Block I 3rd stage
1967-63 D
[02854]
1967 Jun 17.11
1 day
1967 Jun 18
Cylinder
2500?
7.5 long
2.6 dia
* Possibly an attempted Venus Probe, (payload about l106 kg)
** 1967-62 B ejected from 1967-62 A on 1967 Jun 16.97.
2004 December 31 – version 1.01
1967-62 continued on page 141
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
D
D
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Launchdate
Lifetime + Descent date
[Norad]
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
141
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Cosmos 167 *
SL-06 Ullage
Motor
Cosmos 167 *
SL-06 Ullage
Motor
1967-63 E
[02855]
KH 8-06
[Titan 3B-8
Agana D]
1967-64 A
[02858]
VDB-SLC4W
1967 Jun 20.68
10.22 days
1967 Jun 30.90
Cylinder
3000?
3 long?
1.5 dia
1967 Jun 22.6
111.40
89.01
6604
127
325
0.015
107
Secor 9
(EGRS 9)
1967-65 A
[02861]
1967 Jun 29.88
100000 years
Rectangular
box 20
0.33xO.28
x 0.23
1967 Jun 30.9
2001 Feb 18.51
89.ll
90.21
172.22
172.12
10253
10250
3803
3803
3947
3940
0.007
0.007
343
220
Aurora 1 (P67-1)
[Thor Burner 2
171]
1967-65 B
[02876]
VDB-LE-6
1967 Jun 29.88
100000 years
Rectangular
box 21.5
0.6lxO.36
x 0.24
1967 Jul 19.7
2001 Feb 18.11
89.82
90.21
172.18
172.12
10251
10250
3800
3808
3947
3935
0.007
0.006
319
221
Burner 2
stage
1967-65 C
[02877]
1967 Jun 29.88
100000 years
Sphere-cone?
66?
1.32 long?
0.914 dia?
1967 Jul 24.5
2001 Feb 15.60
89.83
90.21
172.18
172.12
10251
10250
3801
3819
3945
3924
0.007
0.005
305
201
Fragments
1967-65 D
1967-65 E
[25101]
[25122]
2001 Feb 15.99
2001 Feb 16.09
90.24
90.05
171.85
172.47
10239
10264
3758
3855
3963
3915
0.010
0.003
213
64
IDCSP 3-1
[Titan 3C-14]
1967-66 A
[02862]
CC-LC41
1967 Jul 1.55
>million years
Polyhedron
(26 faces) 45
0.8 long
0.9 dia
1967 Jul 24.5
2001 Jan 20.03
7.18
12.24
1308.9
1309.62
39635
39651
32986
33024
33528
33521
0.007
0.006
157
IDCSP 3-2
1967-66 B
[02863]
1967 Jul 1.55
>million years
Polyhedron
(26 faces) 45
0.8 long
0.9 dia
1967 Jul 24.5
2001 Jan 17.00
7.22
12.23
1309.8
1310.08
39655
39661
33006
33046
33548
33518
0.007
0.006
155
IDCSF 3-3
1967-66 C
[02864]
1967 Jul 1.55
>million years
Polyhedron
(26 faces) 45
0.8 long
0.9 dia
1967 Jul 6.2
2001 Jan 17.00
7.2
12.28
1311.6
1311.63
39695
39692
33079
33086
33555
33541
0.006
0.006
306
147
IDCSP 3-4
(DATS)**
1967-66 D
[02865]
1967 Jul 1.55
>million years
Polyhedron
(26 faces) 68
0.8 long
0.9 dia
1967 Jul 6.2
2001 Jan 25.09
7.1
12.28
1313.6
1313.57
39733
39731
33156
33142
33553
33563
0.005
0.005
297
138
LES 5
1967-66 E
[02866]
1967 Jul 1.55
>million years
Cylinder
102
1.67 long
1.37 dia
1968 Jan 15.5
2001 Feb 15.25
6.8
12.31
1316.2
1316.03
39785
39781
33178
33211
33636
33593
0.006
0.005
128
DODGE 1 #
1967-66 F
[02867]
1967 Jul 1.55
> million years
Octagonal
door-knob
195
2.41 long
1.22 dia
1968 Jan 15.5
2001 Feb 16.99
6.2
12.36
1318.9
1319.07
39843
39842
33270
33273
33659
33654
0.005
0.005
109
Transtage 11
[Titan 3C-14]
1967-66 G
[02868]
1967 Jul 1.55
> million years
Cylinder
1500?
6 long?
3 dia
1967 Sep 15.5
2001 Feb 15.66
7.0
12.37
1320.8
1322.23
39884
39906
33327
33221
33635
33833
0.004
0.008
-***
88
1967-63 F
[02857]
* Originally listed on page 140
***Approximate orbit
2004 December 31 – version 1.01
1967 Jun
2 days
1967 Jun
1967 Jun
11 days
1967 Jun
(Revised 2001)
Shape and
weight (kg)
Descent date
17.11
19
17.11
28
** De-spun Antenna Test Satellite
# Department Of Defense Gravity Experiment.
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
142
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 168
[Voskhod 11A57]
1967-67 A
[02869]
BAI-LC31
1967 Jul 4.25
7.98 days
1967 Jul 12.23
Spherecylinder
5530?
5 long?
2.4 dia
1967 Jul 4.9
51.81
89.05
6609
198
264
0.005
15
D
Cosmos 168
Block I 3rd stage
1967-67 B
[02870]
1967 Jul 4.25
3.98 days
1967 Jul 8.23
Cylinder
2500?
7.5 long
2.6 dia
1967 Jul 5.5
51.81
88.80
6592
187
240
0.004
341
D
Fragment
1967-67 C
[02871]
1967 Jul 8
4 days
D
Surveyor 4 *
1967-68 A
[Atlas LV-3C AC-11 [02875]
Centaur D 291D]
CC-LC36A
1967 Jul 14.50
62.21 hours
1967 Jul 17.09
Pyramid frame
302
3.05 high
Landed on moon 1967 Jul 17 at 2h 25 m. Impact: 0.4N, 1.33W.
1.27 dia
(of tripod)
Surveyor 4
Centaur 11 stage
1967-68 B
[02883]
1967 Jul 14.50
Cylinder
2000
9.1 long
3.05 dia
In high eccentric orbit, period about 11 days.
Passed 23000 km from moon 1967 Jul 17.42
D Cosmos 169
R? [R-36-0]
1967-69 A
[02878]
BAI
1967 Jul 17.70
0.06 day
1967 Jul 17.76
Cylinder?
2 long?
1 dia?
1967 Jul 17.7
49.68
87.78
6546
135
200
0.005
69
D
Cosmos 169
platform
1967-69 B
[02879]
1967 Jul 17.70
0.5 day?
1967 Jul 18
Irregular
-
1967 Jul 17.7
49.60
87.02
6507
128?
129?
0
-
D
Cosmos 169
2nd stage
1967-69 C
[02880]
1967 Jul 17.70
0.31 day
1967 Jul 18.01
Cylinder
15OO?
8 long?
2.5 dia?
1967 Jul 17.9
49.60
86.51
6481
102?
103?
0
-
D
Fragments
1967-69 D-E
2 pieces, all have decayed
Explorer 35
(Imp 6)
[Thor Delta E1
488 #50]
Explorer 35
Delta 2nd stage
1967-70 A
[02884]
CC-LC17B
1967 Jul 19.60
Octagonal
cylinder
104.5
0.86 long
0.71 dia
1967 Jul 22.6
1967 Dec 8.5
1971 Aug 16.5
147.3
143.9
166.0
710
692
691.5
6063
5980
5980
764
784
809
7886
7700
7675
0.587
0.58
0.574
-
1967-70 B
[02885]
1967 Jul 19.60
42.92 days
1967 Aug 31.52
Cylinder
350?
4.9 long
1.43 dia
1967 Jul 20.3
1967 Aug 14.5
29.56
29.55
103.30
97.28
7298
7011
155
149
1686
1ll6
0.105
0.069
77
-
Explorer 35
3rd stage [Altair]
1967-70 C
[NNA]
1967 Jul 19.60
Indefinitely
Cylinder
24
1.5 long
0.46 dia
0.5?
367?
0.99? 1.02?
In heliocentric orbit. Passed moon on 1967 Jul 22.6
0.012?
-
1967-70 D
[NNA]
1967 Jul 19.60
36
-
Separated 1967 Jul 22.7 from 1967-70 A.
1967 Jul 25.16
681.00 days
1969 Jun 5.16
Cylinder
1500?
8 long?
1.5 dia
1967 Jul 30.4
1968 Feb 29.8
1968 Oct 15.8
0.004
0.004
0.003
42
-
D
D? Explorer 35
Retro rocket
For orbital information see extra pages at the end of the year
D
Ferret 17
1967-71 A
[Thor 2C 496
[02890]
Agena D SS-01B 2732] VDB-SLC2W
D
*
Fragments
1967-71 B-D 3 pieces, all have decayed
For orbital information see extra pages at the end of the year
Surveyor 4 retrorocket (0.91 m diameter sphere of mass 65 kg) may have exploded before impact.
2004 December 31 – version 1.01
75.03
75.03
75.03
94.30
93.83
93.13
6864
6841
6806
458
437
410
513
488
446
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
143
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
OV 1-11 (86)
[Atlas 92 D]
1967-72 A
[02893]
VDB-ABRESB3
1967 Jul 27.79
1670.91 days
1972 Feb 22.70
Cylinder +
hemisphere
118
1.40 long
0.69 dia
1967 Aug 3.5
1969 Sep 16.0
1970 Sep 16.0
101.72
101.72
101.72
95.48
94.51
93.58
6920
6871
6826
480
446
415
634
540
481
0.009
0.007
0.005
51
-
D
OV 1-11
X-258 stage
1967-72 B
[02894]
1967 Jul 27.79
1207 days
1970 Nov 15
Cylinder
70?
2.05 long
0.72 dia
1967 Aug 2.3
1969 Jan 31.7
1969 Dec 31.7
101.72
101.72
101.72
95.47
94.43
93.55
6919
6867
6825
479
426
400
603
552
493
0.009
0.009
0.007
53
-
D
OV 1-12
FW-4S stage
1967-72 C
[02897]
1967 Jul 27.79
3567 days
1977 May 2
Cylinder
70?
2.05 long
0.72 dia
1967 Aug 2.2
1969 Sep 16.0
1973 Feb 15.0
101.61
l0l.61
101.59
95.59
95.01
93.61
6925
6896
6828
540
510
445
554
526
454
0.001
0.001
0.001
287
-
D
OV 1-12
(Faro)
1967-72 D
[02901]
1967 Jul 27.79
4744 days
1980 Jul 22
Cylinder +
hemisphere
141
1.40 long
0.69 dia
1967 Aug 2.2
1970 Oct 31.7
101.62
101.62
95.62
95.04
6927
6898
542
513
556
526
0.001
0.00l
282
-
D
Fragment
1967-72 E
[02918]
1967 Nov 2
98 days
D
OGO 4
1967-73 A
[Thor 2C 478
[02895]
Agena D SS-01B 6802] VDB-SLC2E
1967 Jul 28.60
1845.84 days
1972 Aug 16.44
Box + booms
552
1.73 long
0.84 high
0.84 wide
1967 Jul 29.2
1969 Jul 31.7
1971 Aug 1.0
86.03
85.93
85.93
97.89
96.53
93.97
7035
6967
6846
411
403
370
903
775
565
0.035
0.027
0.014
153
-
D
OGO 4
2nd stage
1967-73 B
[02896]
1967 Jul 28.60
2483.18 days
1974 May 15.7
Cylinder
700?
8
8 long
1.5 dia
1967 Aug 1.3
1969 Jul 31.7
1972 Aug 1.0
86.0l
85.97
85.99
97.82
96.58
93.97
7032
6970
6846
415
402
367
893
782
568
0.034
0.027
0.015
146
-
D Cosmos 170
R? [R-36-0]
1967-74 A
[02902]
BAI
1967 Jul 31.70
0.06 day
1967 Jul 31.76
Cylinder?
2 long?
1 dia?
1967 Jul 31.7
49.46
88.19
6565
121
252
0.010
35
D
Cosmos 170
2nd stage
1967-74 B
[02903]
1967 Jul 31.70
0.30 day
1967 Aug 1.00
Cylinder?
1500?
8 long?
2.5 dia?
1967 Jul 31.7
49.40
88.33
6573
126
263
0.010
-
D
Cosmos 170
platform
1967-74 C
[02904]
1967 Jul 31.70
0.5 day?
1967 Aug 1
Irregular
-
1967 Jul 31.7
49.40
87.59
6535
12.3
191
0.005
-
D
Fragments
1967-74 D
1967-74 E
[02905]
[02906]
1967 Aug 2
1967 Aug 1
2 days
1 days
D
Lunar Orbiter 5
1967-75 A
[Atlas SLV-3
[02907]
5805 Agena D 6634] CC-LC13
1967 Aug 1.940
182.392 days
1968 Jan 31.332
Truncated
cone
390
1.68 high
1.52 dia
1967 Aug 5.70
1967 Aug 7.36
1967 Oct 10.82
85.0
84.6
85.15
506
498
225.29
4860
4810
2831
196
100
200
6040
6050
1986
0.60
0.62
0.315
-$
-$
-$
Lunar Orbiter 5
Agena D 6634
stage
1967 Aug 1.940
1000
Cylinder
1.52 dia
7 long
In high-eccentricity orbit, period about 10 days.
Passed 25000 km from Moon.
$
1967-75 B
[02908]
Moon orbit
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
1967 Aug 8.3
79.94
89.72
Page
144
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
6638
174
346
0.0l3
180
D
Discoverer 117
KH 4B-04
[Thor 2C 510
Agena D 1637]
1967-76 A
[02910]
VDB-SLC1E
1967 Aug 7.90
24.85 days
1967 Sep 1.75
Cylinder
2000?
8 long?
1.5 dia
D
Fragment
1967-76 B
[02923]
1967 Aug 25
18 days
D Cosmos 171
R? [R-36-0]
1967-77 A
[02911]
BAI
1967 Aug 8.67
0.06 day
1967 Aug 8.73
Cylinder?
2 long?
1 dia?
1967 Aug 8.7
49.60
87.58
653
138
177
0.003
-
D
Cosmos 171
2nd stage
1967-77 B
[02912]
1967 Aug 8.67
0.60 day
1967 Aug 8.96
Cylinder
1500?
8 long?
2.5 dia?
1967 Aug 8.7
49.61
87.41
6528
134?
165?
0.002?
-
D
Cosmos 171
platform
1967-77 D
[02915]
1967 Aug 8.67
0.29 day
1967 Aug 9.27
Irregular
-
1967 Aug 9.0
49.62
87.69
6541
130
200
0.005
59
D
Fragments
1967-77 C
[02913]
1967 Aug 9
1 day
1967-77 E
[02916]
1967 Aug 9
1 day
D
R
Cosmos 172
[Voskhod 11A57]
1967-78 A
[02914]
BAI
1967 Aug 9.24
7.94 days
1967 Aug 17.18
Spherecylinder
5530?
5 long?
2.4 dia
1967 Aug 9.6
51.80
89.40
6625
200
293
0.007
33
D
Cosmos 172
Block I 3rd stage
1967-78 B
[02917]
1967 Aug 9.24
4.25 days
1967 Aug 13.49
Cylinder
2500?
7.5 long
2.6 dia
1967 Aug 9.9
51.80
89.11
6612
188
280
0.007
15
D
KH 8-07
[Titan 3B-9
Agena D]
1967-79 A
[02919]
VDB-SLC4W
1967 Aug 16.71
13 days
1967 Aug 29
Cylinder
3000?
8 long?
1.5 dia
1967 Aug 17.3
111.88
90.43
6674
142
449
0.023
128
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
145
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
DMSP B4A-03
(P-35-18)
[Thor Burner 2
266]
1967-80 A
[02920]
VDB-LE-6
1967 Aug 23.20
100 years
12-sided
frustum
195
1.64 long
1.31 to
1.10 dia
1967 Aug 23.6
2001 Feb 18.13
98.97
98.58
102.2
101.87
7241
7226
834
818
892
876
0.004
0.004
101
46
Burner 2
2nd stage
1967-80 B
[02940]
1967 Aug 23.20
80 years
Sphere-cone
66
1.32 long
0.94 dia
1967 Oct 9.2
2001 Feb 17.03
98.95
98.56
102.20
101.78
7241
7221
831
815
895
871
0.004
0.004
333
354
D
Cosmos 173
[Kosmos 11K63]
1967-81 A
[02921]
PLE-LC133/1
1967 Aug 24.21
115.53 days
1967 Dec 17.74
Ellipsoid
400?
1.8 long
1.2 dia
1967 Aug 24.8
1967 Nov 8.0
71.03
71.02
92.10
90.85
6757
6694
277
247
480
396
0.015
0.010
81
-
D
Cosmos 173
2nd stage
1967-81 B
[02922]
1967 Aug 24.21
67.33 days
1967 Oct 30.54
Cylinder
1500?
8 long
1.65 dia
1967 Aug 26.8
1967 Oct 8.0
71.02
71.02
92.06
90.70
6754
6687
281
262
470
357
0.014
0.007
78
-
D
Cosmos 174*
[Molniya 8K78M]
1967-82 A
[02925]
BAI
1967 Aug 31.33
487 days
1968 Dec 30
Windmill
1000?
3.4 long
1.6 dia
1967 Sep 6.4
1968 Mar 15.8
1968 Aug 15.8
64.85
64.87
65.0
715.0
714.5
711.4
26491
26474
26399
430
347
189
39796
39845
39853
0.743
0.746
0.751
285
-
D
Cosmos 174
Block I 3rd stage
1967-82 B
[02926]
1967 Aug 31.33
15.19 days
1967 Sep 15.52
Cylinder
2500?
7.5 long
2.6 dia
1967 Sep 1.5
64.84
91.06
6705
199
454
0.019
59
D
Cosmos 174
SL-06 4th stage
casing
1967-82 C
[02927]
1967 Aug 31.33
18.87 days
1967 Sep 19.20
Irregular
-
1967 Sep 1.2
64.79
91.33
6721
202
484
0.012
62
D
Cosmos 174
rocket
1967-82 E
[NNA]
1967 Aug 31.33
492 days
1969 Jan 4
Cylinder
440
2.0 long
2.0 dia
1967 Dec 27
64.86
710.9
26386
381
39635
0.744
-
D
Cosmos 174
SL-06 ullage
motor
1967-82 D
[02928]
1967 Aug 31.33
5 days
1967 Sep 5
D
Biosatellite 2**
adapter
[Thor Delta G
475 #51]
1967-83 A
[02935]
CC-LC17B
1967 Sep 7.92
26.18 days
1967 Oct 4.10
Cylinder
360?
1.8 long
1.45 dia
1967 Sep 16.6
33.46
90.38
6678
286
313
0.002
55
D
Biosatellite 2
Delta 2nd stage
1967-83 B
[02936]
1967 Sep 7.92
133.84 days
1968 Jan 19.76
Cylinder
400?
4.9 long
1.43 dia
1967 Sep 8.8
1967 Dec 8.0
32.94
32.94
92.08
90.82
6761
6700
321
285
445
358
0.009
0.005
211
-
D
R
B
Biosatellite 2#
capsule
1967-83 C
[NNA]
1967 Sep 7.92
1.87 days
1967 Sep 9.79
Blunt cone
150?
1.2 long
1.02 dia
1967 Sep 8.4
33.48
90.53
6685
296
318
0.002
20
* This is probably a Molniya satellite, later replaced by Molniya 1F (1967-95 A).
** Before 1967 Sep 9.8, Blos 2 adapter was attached to Bios 2 capsule, 1967-83 C. # Originally listed on page 146.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
Perigee
height
(km)
146
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Surveyor 5
1967-84 A
[Atlas SLV-3 AC-13[02937]
Centaur D-1A 5901C] CC-LC36B
1967 Sep 8.31
64.82 hours
1967 Sep 11.03
Pyramid
frame
303
3.05 high
Softlanded on moon 1967 Sep 11 at 0h46m44s
4.27 dia
Impact: 1.41N; 23.18E
(of tripod)
Surveyor 5
Centaur 14 stage
1967-84 B
[02938]
1967 Sep 8.31
Cylinder
2000
9.1 long
3.05 dia
In highly eccentric orbit. Period about 11 days.
D
Surveyor 5
Retrorocket
1967-84 C
[NNA]
1967 Sep 8.31
64.82 hours
1967 Sep 11.03
Sphere
(+ nozzle)
65
1.32 long
0.91 dia
Landed on moon alongside 1967-84 A
D
R
Cosmos 175
[Voskhod 11A57]
1967-85 A
[02939]
PLE
1967 Sep 11.44
7.82 days
1967 Sep 19.26
Spherecylinder
5530
5 long?
2.4 dia
1967 Sep 11.8
72.93
90.20
6663
D
Cosmos 175
Block I 3rd stage
1967-85 B
[02941]
1967 Sep 11.44
12.13 days
1967 Sep 23.57
Cylinder
2500?
7.5 long
2.6 dia
1967 Sep 12.4
72.88
90.05
D
Fragment
1967-85 C
[02943]
1967 Sep 13
2 days
D
Cosmos 176
[Kosmos 11K63]
1967-86 A
[02942]
PLE-LC133/1
1967 Sep 12.71
172.91 days
1968 Mar 3.62
Ellipsoid
400?
1.8 long
1.2 dia
1967 Sep 13.0
1968 Jan 8.0
81.89
81.8
D
Cosmos 176
2nd stage
1967-86 B
[02945]
1967 Sep 12.71
54.13 days
1967 Dec 12.84
Cylinder*
1500?
8 long*
1.65 dia
1967 Sep 23.0
1967 Nov 8.0
81.83
81.8
D
Fragments
1967-84 C-M
10 pieces, all have decayed
D
Discoverer 118
KH 4B-05
[Thor 2L 512
Agena D 1641]
1967-87 A
[02946]
VDB-SLC1W
1967 Sep 15.82
18.69 days
1967 Oct 4.51
Cylinder
2000?
8 long?
1.5 dia
1967 Sep 16.4
80.07
89.95
6648
150
389
0.0l8
174
D
R
Cosmos 177
[Voskhod 11A57]
1967-88 A
[02947]
BAI-LC1
1967 Sep 16.25
7.99 days
1967 Sep 24.24
Spherecylinder
5530?
5 long?
2.4 dia
1967 Sep 16.4
51.84
89.29
6618
200
280
0.006
34
D
Cosmos 177
Block I 3rd stage
1967-88 B
[02948]
1967 Sep 16.25
3.42 days
1967 Sep 19.67
Cylinder
2500?
7.5 long
2.6 dia
1967 Sep 16.7
51.81
89.04
6607
196
262
0.005
14
*
Before explosion.
2004 December 31 – version 1.01
Date of
orbital
determination
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
D
Cospar ID
[Norad #] Launchsite
Cospar ID
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
211
358
0.011
56
6656
205
351
0.011
49
102.19
96.08
7239
6949
196
183
1525
958
0.092
0.056
74
-
101.85
96.71
7222
6979
204
196
1484
1006
0.089
0.058
-
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
147
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D Cosmos 178
R? [R-36-0]
1967-89 A
[02951]
BAI
1967 Sep 19.62
0.06 day
1967 Sep 19.68
Cylinder
2 long ?
1 dia ?
1967 Sep 19.6
49.65
88.39
6576
138
258
0.009
-
D
Cosmos 178
platform
1967-89 B
[02953]
1967 Sep 19.62
0.45 day
1967 Sep 20.07
Irregular
-
1967 Sep 19.8
49.66
87.85
6548
130
209
0.006
60
D
Cosmos 178
2nd stage
1967-89 C
[02954]
1967 Sep 19.62
0.2 day
1967 Sep 19.8
Cylinder
1500 ?
8 long ?
2.5 dia ?
1967 Sep 19.7
49.60
87.41
6528
137
163
0.002
-
D
Fragment
1967-89 D
[02955]
1967 Sep 19
< 1 day
D
KH 8-08
[Titan 3B-10
Agena D]
1967-90 A
[02952]
VDB-SLC4W
1967 Sep 19.77
10.23 days
1967 Sep 30.00
Cylinder
3000?
8 long?
1.5 dia?
1967 Sep 21.4
106.10
89.75
6640
122
40l
0.021
119
D Cosmos 179
R? [R-36-0]
1967-91 A
[02962]
BAI
1967 Sep 22.59
0.06 day
1967 Sep 22.65
Cylinder
2 long?
1 dia?
1967 Sep 22.6
49.57
87.87
6551
139
207
0.005
-
D
Cosmos 179
platform
1967-91 B
[02963]
1967 Sep 22.59
0.03 day
1967 Sep 23.02
Irregular
1967 Sep 22.8
49.52
87.74
6544
120
212
0.007
32
D
Cosmos 179
2nd stage
1967-91 C
[02964]
1967 Sep 22.59
0.24 day
1967 Sep 22.83
Cylinder
1500?
8 long?
2.5 dia?
1967 Sep 22.7
49.40
87.39
6527
141
156
0.001
-
Transit O-14 (17)
(NNSS 30140)
[Scout A S157C]
1967-92 A
[02965]
VDB-SLC5
1967 Sep 25.35
1000 years
Octagon
+ 4 vanes
60?
0.25 long
0.46 dia
1967 Sep 26.4
2001 Feb 17.89
89.28
89.26
106.81
106.52
7457
7444
1041
1030
1116
1100
0.005
0.005
189
244
Scout 4th stage
Altair
1967-92 B
[02967]
1967 Sep 25.35
1000 years
Cylinder
24
1.5 long
0.46 dia
1967 Sep 26.0
2001 Feb 16.22
89.29
89.25
106.80
106.57
7456
7446
l040
1034
1115
1101
0.005
0.004
187
257
Fragments
1967-92 C-L
9 pieces, 6 have decayed
2004 December 31 – version 1.01
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
148
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 180
[Voskhod 11A57]
1967-93 A
[02966]
PLE-LC41/1
1967 Sep 26.43
7.82 days
1967 Oct 4.25
Spherecylinder
5530?
5 long?
2.4 dia
1967 Sep 27.2
72.89
90.04
6653
208
341
0.010
56
D
Cosmos 180
Block I 3rd stage
1967-93 B
[02968]
1967 Sep 26.43
9.41 days
1967 Oct 5.84
Cylinder
2500?
7.5 long
2.6 dia
1967 Sep 26.8
72.89
90.00
6650
205
338
0.010
52
Intelsat 2-4
[Thor Delta E1
442 #52]
1967-94 A
[02969]
CC-LC17B
1967 Sep 28.03
> million years
Cylinder
87
0.67 long
1.42 dia
1967
1967
1977
2001
28.1
15.5
13.0
9.75
26.43
0.93
7.41
13.67
655.0
l438.3
1437.51
1434.90
24980
42208
42192
42142
305
35747
35805
35711
36897
35913
35823
35815
0.732
0.002
0.0002
0.001
179
63
109
Intelsat 2-4
Delta 2nd stage
1967-94 B
[02970]
1967 Sep 28.03
89.01 days
1967 Dec 26.04
Cylinder
400?
4.9 long
1.43 dia
1967 Oct 2.6
1967 Nov 23.0
28.74
28.74
92.65
9l.33
6790
6724
242
231
582
461
0.025
0.017
182
-
Intelsat 2-4
Delta 3rd stage
1967-94 C
[02971]
1967 Sep 26.03
40 years?
Cylinder
24
1.5 long
0.46 dia
1967 Sep 28.3
2001 Feb 17.65
26.44
27.99
625.4
523.40
24235
21514
307
312
35406
29959
0.724
0.689
179
73
D
Fragment
Delta 2nd stage
1967-94 D
[02972]
1967 Oct 29
31 days
D
Molniya-1 6
[Molniya 8K78M
Ya716-83]
1967-95 A
[02973]
BAI
1967 Oct 3.21
518.76 davs
1969 Mar 4.97
Windmill
1600
3.4 long
1.6 dia
1967 Oct 9.7
1968 Mar 15.8
1968 Oct 23.5
64.96
64.93
65.2
718.03
716.23
707.35
26563
26519
26299
502
338
173
39668
39943
39668
0.741
0.747
0.751
285
-
D
Molniya-1 6
Block I 3rd stage
1967-95 B
[02974]
1967 Oct 3.21
18.25 days
1967 Oct 2l.46
Cylinder
2500?
7.5 long
2.6 dia
1967 Oct 9.0
64.79
90.95
6699
200
44l
0.0l8
65
D
Molniya-1 6
SL-06 4th stage
casing
1967-95 C
[02975]
1967 Oct 3.21
14.16 days
1967 Oct 17.37
Irregular
-
1967 Oct 11.0
64.8l
90.27
6667
195
382
0.0l4
64
D
Molniya-1 6
Block L 4th stage
1967-95 D
[03225]
1967 Oct 3.21
496.70 days
1969 Feb lO.91
Cylinder
440
2.0 long
2.0 dia
1967 Dec 27
1968 Aug 15.8
1968 Nov 8.0
64.94
65.00
65.2
709.7
708.5
699.5
26356
26343
26104
420
227
151
39536
39703
3930l
0.742
0.749
0.750
-
D
2004 December 31 – version 1.01
Sep
Oct
May
Feb
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
149
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
DMSP B4A-04
(P-35-19)
[Thor Burner 2
268]
1967-96 A
[02980]
VDB-LE-6
1967 Oct 11.33
80 years
l2-sided
frustum
195
1.64 long
1.31 to
1.10 dia
1967 Oct 15.8
2001 Feb 15.97
99.16
99.23
100.18
99.03
7144
7091
667
636
866
789
0.014
0.011
355
334
Burner 2
stage
1967-96 B
[02985]
1967 Oct 11.33
60 years
Sphere-cone
66
1.32 long
0.94 dia
1967 Oct 13.0
2001 Feb 18.00
99.12
99.17
100.18
98.80
7144
7080
673
630
859
772
0.013
0.010
3
184
D
R
Cosmos 181
[Voskhod 11A57]
1967-97 A
[02981]
PLE-LC41/1
1967 Oct 11.48
7.78 days
1967 Oct 19.26
Spherecylinder
5530?
5 long?
2.4 dia
1967 Oct 12.0
65.61
89.72
6639
194
327
0.010
47
D
Cosmos 181
Block I 3rd stage
1967-97 B
[02982]
1967 Oct 11.48
7.53 days
1967 Oct 19.01
Cylinder
2500?
7.5 long
2.6 dia
1967 Oct 14.1
65.62
89.15
6612
188
280
0.007
32
D
R
Cosmos 182
[Voskhod 11A57]
1967-98 A
[02995]
BAI
1967 Oct 16.33
7.93 days
1967 Oct 24.26
Spherecylinder
5530?
5 long?
2.4 dia
1967 Oct 16.7
64.99
89.90
6648
210
330
0.009
54
D
Cosmos 182
Block I 3rd stage
1967-98 B
[02996]
1967 Oct 16.33
7.96 days
1967 Oct 24.29
Cylinder
2500?
7.5 long
2.6 dia
1967 Oct 17.1
64.98
89.75
6642
204
324
0.009
45
D
Fragment
1967-98 C
[02999]
1967 Oct 24
8 days
D Cosmos 183
R? [R-36-0]
1967-99 A
[03001]
BAI
1967 Oct 18.56
0.07 day
1967 Oct 18.63
Cylinder
2 long?
1 dia?
1967 Oct 18.6
49.63
88.90
660l
130
315
0.0l4
63
D
Cosmos 183
platform
1967-99 B
[03002]
1967 Oct 18.56
0.48 day
1967 Oct 19.04
Irregular
-
1967 Oct 18.9
49.66
87.50
6531
127
179
0.004
41
D
Cosmos 183
2nd stage
1967-99 C
[03003]
1967 Oct 18.56
0.26 day
1967 Oct 18.82
Cylinder
1500?
8 long?
2.5 dia?
1967 Oct 18.7
49.3
88.05
6559
151
211
0.005
-
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
150
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
0S0 4
[Thor Delta C1
490 #53]
1967-l00 A
[03000]
CC-LC17B
1967 Oct 18.67
5354 days
1982 Jun 15
Nonagonal
box
272
0.94 long
1.12 dia
1967 Oct 19.5
33.04
95.58
6931
546
560
0.001
140
D
0S0 4
Delta 3rd stage
1967-100 B
[03004]
1967 Oct 18.67
4560 days
1980 May 2
Cylinder
24
1.5 long
0.46 dia
1967 Oct 20.3
1972 Mar 11.3
32.99
32.9
95.58
94.78
6931
6892
539
501
567
526
0.002
0.002
261
-
D
Molniya-1 7
[Molniya 8K78M
Ya716-82]
1967-101 A
[03008]
BAI
1967 Oct 22.36
80l days
1969 Dec 31
Windmill
1000?
3.4 long
1.6 dia
1967 Oct 22.9
1969 Jan 15.8
1969 Sep 8.5
65.00
64.7
64.8
715.0
733.45
732.35
26487
26942
26915
508
471
197
39710
40657
40877
0.740
0.746
0.756
285
-
D
Molniya-1 7
SL-06 4th stage
casing
1967-101 B
[03005]
1967 Oct 22.36
15.78 days
1967 Nov 7.14
Irregular
-
1967 Oct 24.7
64.80
90.99
6701
202
443
0.0l8
63
D
Molniya-1 7
Block I 3rd stage
1967-l01 C
[03006]
1967 Oct 22.36
11.87 days
1967 Nov 3.23
Cylinder
2500?
7.5 long
2.6 dia
1967 Oct 22.7
64.82
90.95
6698
199
440
0.0l8
58
D
Molniya-1 7
SL-06 ullage
Motor
1967-101 D
[03007]
1967 Oct 22.36
6 days
1967 Oct 28
-
-
D
Molniya-1 7
SL-06 ullage
Motor
1967-101 E
[03009]
1967 Oct 22.36
5 days
1967 Oct 27
-
-
1967 Oct 23.56
64.82
90.88
6696
200
435
0.018
63
D
Molniya-1 7
Block L 4th stage
1967-101 F
[03226]
1967 Oct 22.36
817 days
1970 Jan 16
Cylinder
440
2.0 long
2.0 dia
1967 Dec 27
1968 Aug 23.5
1969 May 8.5
64.9
64.70
64.73
711.7
711.6
711.6
26406
26405
26405
517
584
414
39539
39470
39640
0.739
0.736
0.743
-
D
Cosmos 184
(Meteor)
[Vostok 8A92M]
1967-102 A
[03010]
PLE
1967 Oct 24.96
7831 davs
1989 Apr 2
Cylinder + 2
vanes 20007
5 long ?
1.5 dia?
1967 Oct 25.1
81.19
97.09
6997
600
638
0.003
282
D
Cosmos 184
Block E 3rd stage
1967-102 B
[03011]
1967 Oct 24.96
8822 days
1991 Dec 19
Cylinder
1440
3.8 long
2.6 dia
1967 Oct 25.3
81.20
97.27
7006
544
711
0.012
177
D
KH 8-09
[Titan 3B-11
Agena D]
1967-103 A
[03012]
VDB-SLC4W
1967 Oct 25.80
9 days
1967 Nov 4
Cylinder
3000?
8 long?
1.5 dia
1967 Oct 26.1
111.57
90.15
6661
136
429
0.022
130
D
Cosmos 185
[Tsyklon]
1967-l04 A
[03013]
BAI-LC90
1967 Oct 27.10
445.61 days
1969 Jan 14.71
Spheroid +
paddles
1.5 dia?
1967 Oct 28.4
1968 Mar 28.2
1968 Aug 15.8
64.09
64.0
64.0
98.67
97.46
96.52
7074
7017
6972
518
493
466
873
784
722
0.025
0.021
1018
47
-
Cosmos 185
rocket
1967-104 B
[03019]
1967 Oct 27.10
50 years
Cylinder
1500?
6 long?
2 dia?
1967 Oct 29.5
2001 Feb 18.74
64.09
64.05
98.60
93.68
7070
6833
510
371
874
539
0.026
0.012
47
249
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
151
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
R
Cosmos 186 *
[Soyuz 11A511]
1967-105 A
[03014]
BAI
1967 Oct 27.4O
3.87 days
1967 Oct 31.27
Cylinder +
2 wings
6480 ?
7.5 long
2.2 dia
1967 Oct 27.5
1967 Oct 31.0
51.67
51.61
88.29
88.96
6570
6604
172
193
212
258
0.003
0.005
274
57
D
Cosmos 186
Block I 3rd stage
1967-l05 B
[03015]
1967 Oct 27.40
1.91 days
1967 Oct 29.31
Cylinder
2500?
7.5 long
2.6 dia
1967 Oct 27.7
51.67
88.58
6584
199
212
0.001
41
D Cosmos 187
R? [R-36-0]
1967-106 A
[03016]
BAI
1967 Oct 28.55
0.07 day
1967 Oct 28.62
Cylinder
5000
2 long?
1 dia
1967 Oct 28.7
49.63
88.88
6600
143
301
0.012
82
D
Cosmos 187
platform
1967-106 B
[03017]
1967 Oct 28.55
O.44 day
1967 Oct 28.99
Irregular
-
1967 Oct 28.7
49.63
88.80
6597
139
298
0.012
82
D
Cosmos 187
2nd stage
1967-106 C
[03018]
1967 Oct 28.55
0.3 day
1967 Oct 28.8
Cylinder
1500?
8 long?
2.5 dia?
1967 Oct 28.7
49.6
88.23
6568
139
240
0.008
-
D
R
Cosmos 188 *
[Soyuz 11A511]
1967-107 A
[03020]
BAI
1967 Oct 30.34
3.03 days
1967 Nov 2.37
Cylinder +
2 wings
6480?
7.5 long
2.2 dia
1967 Oct 30.5
51.65
88.70
6592
180
247
0.005
96
D
Cosmos 188
Block I 3rd stage
1967-107 B
[03022]
1967 Oct 30.34
2.74 days
1967 Nov 2.08
Cylinder
2500?
7.5 long
2.6 dia
1967 Oct 31.2
51.64
88.71
6592
185
242
0.004
81
D
Cosmos 189
[Kosmos 11K65M]
1967-108 A
[03021]
PLE-LC132
1967 Oct 30.75
3874 days
1978 Jun 8
Cylinder
+ paddles
900?
2 long?
1 dia?
1967 Oct 31.1
1970 Nov 7.0
1976 Feb 16.5
74.01
73.99
73.99
95.53
94.74
93.15
6923
6883
6807
524
488
420
565
522
438
0.003
0.002
0.001
162
-
D
Cosmos 189
2nd stage
1967-108B
[03023]
1967 Oct 30.75
4512 days
1980 Mar 7
Cylinder
2200 ?
7.4 long
2.4 dia
1967 Nov 4.5
1972 May 1.0
74.01
73.99
95.77
94.94
6935
6893
531
497
582
533
0.004
0.003
115
-
D
Fragments **
1967-108 C-L 9 pieces, all have decayed
For orbital information see extra pages at the end of the year
* Cosmos 186 and Cosmos 188 docked Oct 30.39 and separated Oct 30.53. Cosmos 188 self-destruct on uncontrolled reenty.
** Fragments designated 1967-108F to 108L possibly belong to the 1972-88, 1973-03 and 1973-10 launches.
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
152
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Discoverer 119
KH 4B-06
[Thor 2L 513
Agena D 1639]
1967-109 A
[03024]
VDB-SLC1E
1967 Nov 2.90
29.83 days
1967 Dec 2.73
Cylinder
2000?
8 long?
1.5 dia
1967 Nov 4.9
81.53
90.47
6675
183
410
0.017
168
D
Hitchhiker 16
(Module 283)
1967-l09 B
[03025]
1967 Nov 2.90
511.93 days
1969 Mar 28.83
Octagon?
60?
0.3 long?
0.9 dia?
1967 Nov 6.9
1968 Apr 30.5
1968 Oct 15.8
81.68
81.6
81.6
94.41
93.77
93.07
6868
6836
6802
455
431
403
524
485
444
0.005
0.004
O.003
227
-
D
R
Cosmos 190
[Voskhod 11A57]
1967-11O A
[03026]
PLE
1967 Nov 3.47
7.80 days
1967 Nov 11.27
Spherecylinder
5530?
5 long
2.4 dia
1967 Nov 3.8
65.73
89.80
6643
191
338
0.011
43
D
Cosmos 190
Block I 3rd stage
1967-11O B
[03027]
1967 Nov 3.47
6.03 days
1967 Nov 9.50
Cylinder
2500?
7.5 long
2.6 dia
1967 Nov 5.8
65.67
89.22
6614
183
289
0.008
31
ATS 3
[Atlas SLV-3 5103
Agena D 6153]
1967-111 A
[03029]
CC-LC12
1967 Nov 5.98
> million years
Cylinder
365
1.83 long
1.42 dia
1967 Nov 20.4
1968 Jan 8.0
2001 Feb 17.28
0.53
0.45
13.96
1444.9
1436.8
1436.08
42339
42172
42165
35791
35776
35709
36130
35812
35863
0.004
0.0004
0.002
123
327
D
ATS 3
Agena D
6153 stage
1967-111 B
[03030]
1967 Noy 5.98
276 days
1968 Aug 8
Cylinder
700?
6 long ?
1.5 dia
1967 Nov 14.9
1968 Jul 15.8
28.39
28.07
624.5
205.4
24196
11489
179
123
35457
10099
0.729
0.434
186
-
D
Surveyor 6
1967-112 A
[Atlas SLV-3C AC-14 [03031]
Centaur D-1A 5902C] CC-LC36B
1967 Nov 7.32
65.37 hours
1967 Nov 10.04
Pyramid
frame
300
3.05 high
Soft-landed on moon 1967 Nov 10 at 01h01m05s
4.27 dia
Impact: 0.49N; 1.40W
(of tripod) (Craft made to hop on Nov 17)
Surveyor 6
Centaur 14 stage
1967-112 B
[03034]
1967 Nov 7.32
Indefinitely
Cylinder
2000
9.1 long
3.05 dia
In high-eccentricity orbit
Passed 28000 km behind moon on 1967 Nov 10.63
D
Surveyor 6
Retrorocket
1967-112 C
[NNA]
1967 Nov 7.32
65.37 hours
1967 Nov 10.04
Sphere +
nozzle
66
1.32 long
0.91 dia
Landed on moon alongside 1967-112 A
D
r
Apollo 4*
[Saturn 501]
1967-113 A
[03032]
CC-LC39A
1967 Nov 9.50
0.36 day
1967 Nov 9.86
Conecylinder
30440
10.30 long
3.91 dia
1967 Nov 9.5
1967 Nov 9.7
1967 Nov 9.8
32.7
30.2
30.13
88.08
307.4
319.5
6564
15109
15501
183
60?
80?
188
17402
18326
0.0004
0.571
0.588
-
D
LEM Model 1 Saturn IV B
1967-113 B
[03033]
1967 Nov 9.50
0.34 day
1967 Nov 9.84
Conecylinder
29300
24.2 long
6.6 dia
1967 Nov 9.5
1967 Nov 9.7
32.7
30.2
88.08
3O7.4
6564
15109
183
60?
188
17402
0.0004
0.571
-
Essa 6
[Thor Delta E1
480 #54]
1967-114 A
[03035]
VDB-SLC2E
1967 Nov 10.75
10000 years
Cylinder
132
0.56 long
1.07 dia
1967 Nov 23.0
2001 Feb 15.90
102.12
102.06
114.82
114.82
7827
7825
1410
1408
l488
1485
0.005
0.005
69
48
*
Before Nov 9.63, 1967-113 A and B were joined.
2004 December 31 – version 1.01
1967-114 continued on page 153.
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Cylinder
24
1.50 long
0.46 dia
1967 Noy 14.8
2001 Feb 15.87
102.12
102.05
Page
153
Semi
major axis
(km)
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
114.83
114.82
7828
7826
1411
1410
1489
1485
0.005
0.005
88
58
Essa 6 *
Delta 3rd stage
1967-114 B
[03036]
1967 Nov 10.75
5000 years
Essa 6 *
de-spin weight
1967-114 C
[03051]
1967 Nov 10.75
2001 Feb 18.46
101.87
114.10
7793
1345
1483
0.009
78
Essa 6 *
de-spin weight
1967-114 D
[03123]
1967 Nov 10.75
2001 Feb 16.54
102.56
115.38
7852
1451
1495
0.003
53
Fragment *
1967-114 E
[05443]
2001 Feb 17.51
102.05
114.58
7815
1388
1485
0.006
105
D
Cosmos 191
[Kosmos 11K63]
1967-115 A
[03043]
PLE-LC133/1
1967 Nov 21.60
102.37 days
1968 Mar 2.97
Ellipsoid
400?
1.8 long
1.2 dia
1967 Nov 22.3
1968 Feb 7.8
70.96
70.96
92.16
90.47
6760
6676
267
235
497
360
0.017
0.009
84
-
D
Cosmos 191
2nd stage
1967-115 B
[03044]
1967 Nov 21.6O
53.42 days
1968 Jan 14.02
Cylinder
1500?
8 long
1.65 dia
1967 Nov 22.3
1967 Dec 23.5
70.97
70.97
91.95
90.96
6749
6700
270
258
472
386
0.015
0.010
84
-
Cosmos 192
[Kosmos 11K65M]
1967-116 A
[03047]
PLE-132
1967 Nov 23.62
80 years
Cylinder
+ boom
75O?
1.4 long?
2.0 dia?
1967 Nov 23.9
2001 Feb 13.68
73.98
74.02
99.85
99.15
7132
7097
747
713
761
723
0.001
0.0007
179
202
Cosmos 192
2nd stage
1967-116 B
[03048]
1967 Nov 23.62
80 years
Cylinder
2200?
7.4 long
2.4 dia
1967 Nov 25.4
2001 Feb 13.92
74.01
74.01
99.84
99.95
7131
7087
746
704
760
712
0.001
0.0006
260
109
D
R
Cosmos 193
[Voskhod 11A57]
1967-117 A
[03052]
PLE-LC41/1
1967 Nov 25.48
7.74 days
1967 Dec 3.22
Spherecylinder
5530?
5 long?
2.4 dia
1967 Nov 25.8
65.63
89.85
6647
202
335
0.010
52
D
Cosmos 193
Block I 3rd stage
1967-117 B
[03053]
1967 Nov 25.48
6.18 days
1967 Dec 1.66
Cylinder
2500?
7.5 long
2.6 dia
1967 Nov 27.3
65.64
89.50
6628
184
316
0.010
39
D
Wresat 1 *
[SPARTA 2029
/SV-10]
1967-118 A
[03054]
WMR-LA8
1967 Nov 29.20
42.28 days
1968 Jan l0.48
Cone 73
(payload 45)
2.2 long
0.76) dia
1967 Nov 29.2
1967 Dec 23.5
83.35
83.2
99.27
95.24
7l04
6908
193
167
1259
893
0.075
0.053
340
-
D
R
Cosmos 194
[Voskhod 11A57]
1967-119 A
[03055]
PLE
1967 Dec 3.50
7.78 days
1967 Dec 11.28
Spherecylinder
5530?
5 long?
2.4 dia
1967 Dec 3.7
65.66
89.55
6632
201
307
0.008
39
D
p
Cosmos 194
Block I 3rd stage
1967-119 B
[03056]
1967 Dec 3.50
6.12 days
1967 Dec 9.62
Cylinder
2500?
7.5 long
2.6 dia
1967 Dec 3.8
65.65
89.55
6632
201
307
0.008
48
* Originally listed on page 152.
** Weapons Research Establishment Satellite (Australia).
2004 December 31 – version 1.01
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
154
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
OV3-6
(Atcos 2)*
[Scout B S158C]
1967-120 A
[03057]
VDB-SLC5
1967 Dec 5.04
460.14 days
1969 Mar 9.18
Octagonalcylinder
95
0.53 long
0.73 dia
1967 Dec 7.2
1968 Apr 30.5
1968 Sep 30.5
90.67
90.6
90.6
93.14
92.58
91.99
6804
6777
6748
412
384
358
439
413
381
0.002
0.002
0.002
242
-
D
OV3-6
Scout 4th stage
1967-120 B
[03059]
1967 Dec 5.04
125.40 days
1968 Apr 8.44
Cylinder
24
1.50 long
0.46 dia
1967 Dec 15.5
1968 Feb 22.5
90.6
90.6
93.O2
92.07
6798
6752
404
364
436
383
0.002
0.001
-
D
Fragments
1967-12O C-E 3 pieces, all have decayed
D
KH 8-10
[Titan 3B-12
Agena D]
1967-121 A
[03058]
VDB-SLC4W
1967 Dec 5.78
11.18 days
1967 Dec 16.96
Cylinder
3000?
8 long?
1.5 dia
1967 Dec 7.8
109.55
90.16
6662
137
430
0.022
138
D
Discoverer 120
KH 4B-07
[Thor 2L 514
Agena D 1642]
1967-122 A
[03063]
VDB-SLC1W
1967 Dec 9.93
15 days
1967 Dec 25
Cylinder
1350
8 long?
1.5 dia
1967 Dec 10.5
1967 Dec 22.7
81.65
81.74
88.45
88.46
6576
6577
158
146
237
251
0.006
0.008
165
132
Pioneer 8
[Thor Delta E1
489 #55]
1967-123 A
[03066]
CC-LC17B
1967 Dec 13.59
Indefinitely
Cylinder
66
0.89 high
0.94 dia
Solar orbit
Reached aphelion
0.06
386 days
on 1968 Jun 23?
0.990
1.087
0.047
D
TTS 1*
ERS 30
1967-123 B
[03067]
1967 Dec 13.59
137.4 days
1968 Apr 29.0
Octahedron
20
0.27 side
1967 Dec 14.9
1968 Mar 8.0
32.90
32.90
92.l8
90.99
6767
6708
287
271
490
388
0.015
0.009
71
-
D
Pioneer 8
Delta 2nd stage
1967-123 C
[03068]
1967 Dec 13.59
110.0 days
1968 Apr 1.6
Cylinder
400?
4.9 long
1.43 dia
1967 Dec 19.4
1968 Feb 22.5
32.91
32.85
92.15
90.94
6765
6705
293
272
479
332
0.0l4
0.008
117
-
D
Fragments
1967-123 D
1967-123 E
[03069]
[03070]
1968 Feb 12
1968 Feb 12
61 days
61 days
Pioneer 8
Altair stage
1967-123 F
[NNA]
1967 Dec 13.59
Indefinitely
Cylinder
24
1.5 long
0.46 dia
Orbit probably similar to 1967-123 A
D
R
Cosmos 195
[Voskhod 11A57]
1967-124 A
[03071]
PLE-LC41/1
1967 Dec 16.50
7.76 days
1967 Dec 24.26
Spherecylinder
5530?
5 long?
2.4 dia
1967 Dec 16.7
65.65
90.l0
6658
207
353
0.011
59
D
Cosmos 195
Block I 3rd stage
1967-124 B
[03072]
1967 Dec 16.50
7.31 days
1967 Dec 23.81
Cylinder
2500?
7.5 long
2.6 dia
1967 Dec 18.1
65.64
89.76
6642
197
330
0.010
47
D
Fragment
1967-124 C
[03073]
1967 Dec 18
2 days
* Atmospheric composition satellite.
** Test and Training Satellite.
2004 December 31 – version 1.01
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1967
Name
[Launcher]
Fragments
Cospar ID
[Norad #] Launchsite
Cospar ID
(Revised 2001)
Launchdate
Lifetime + Descent date
[Norad]
Shape and
weight (kg)
Descent date
Size
(m)
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
Nodal
period
(min)
Semi
major axis
(km)
Page
155
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
D
Cosmos 196
[Kosmos 11K63]
1967-125 A
[03074]
KY-LC86/1
1967 Dec 19.27
202.85 days
1968 Jul 7.12
Ellipsoid
400?
1.8 long
1.2 dia
1967 Dec 21.7
1968 Feb 29.8
48.80
48.73
95.42
94.09
6920
6854
223
217
860
735
0.046
0.038
117
-
D
Cosmos 196
2nd stage
1967-125 B
[03075]
1967 Dec 19.27
63.54 days
1968 Feb 20.81
Cylinder
1500?
8 long
1.65 dia
1967 Dec 22.6
1968 Feb 7.5
48.81
48.77
95.20
91.86
6908
6749
219
200
841
542
0.045
0.025
119
-
D
Fragments
1967-125 C
1967-125 D
1967-125 E
[03076]
[03077]
[03078]
1968 Jan 7
1968 Jan 7
1968 Jan 7
19 days
19 days
19 days
D
Cosmos 197
[Kosmos 11K63]
1967-126 A
[03079]
KY-LC86/4
1967 Dec 26.38
34.80 days
1968 Jan 30.18
Ellipsoid
400?
1.8 long
1.2 dia
1967 Dec 26.6
48.42
91.51
6730
217
486
0.020
95
D
Cosmos 197
2nd stage
1967-126 B
[03080]
1967 Dec 26.38
12.80 days
1968 Jan 8.18
Cylinder
1500 ?
8 long*
1.65 dia
1967 Dec 26.6
48.44
91.40
6724
218
473
0.019
99
D
Fragments
1967-126 C-J 7 pieces, all have decayed
Cosmos 198**
[Tsyklon]
1967-127 A
[03081]
BAI-LC90
1967 Dec 27.48
500 years
Conecylinder
6 long?
2 dia?
1967 Dec 27.5
1967 Dec 29.7
2001 Feb 13.99
65.14
65.15
65.14
89.70
103.43
103.37
6638
7301
7296
249
894
888
270
952
947
0.002
0.004
0.004
275
307
238
D
Cosmos 198
platform
1967-127 B
[03082]
1967 Dec 27.48
211.74 days
1968 Jan 21.22
Irregular
-
1967 Dec 27.5
65.10
89.63
6635
241
273
0.002
305
D
Cosmos 198
1967-127 C
[03088]
1967 Dec 27.48
3.99 days
1967 Dec 31.47
Cylinder
1500?
8 long?
2.5 dia?
1967 Dec 30.1
65.09
89.12
6610
224
239
0.001
224
* Before explosion.
** 1967-127 B and 127 C attached to 1967-127 A until orbit change.
Engineering test of Rorsat - Radar ocean reconnaissance satellite.
2004 December 31 – version 1.01
For orbital information see extra pages at the end of the year
RAE Table of Earth Satellites
Year of Launch 1967
Cospar ID
[Norad number]
Descent date
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
(Revised 2001)
Nodal
period
(min)
Semi
major axis
(km)
Extra Page 1967- 1
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
Text in box is from "History of on-orbit satellite fragmentations", 13th edition, May 2004.
Orbital Debris Program Office, Johnson Space Centre, NASA, Houston, TX 77058.
Intelsat 2-2 fragments, 39 pieces, 21 have decayed
Analyses indicate that the Intelsat-2 2 payload is the most likely debris source.
The orbital information for the reassigned objects is for the last TLE with the 1967-01 designation
D 1967-01 C
[02641]
1967 Feb 24
44 days
D 1967-01 E
[04901]
1971 Feb 9
1490 days
D 1967-01 F
[05122]
1972 Apr 30
1936 days
D 1967-01 G
[05123]
1971 Oct 6
1729 days
D 1967-01 H
[05245]
1971 Jun 17
1618 days
D 1967-01 J
[05269]
1978 Oct 29
4309 days
D 1967-01 K
[05333]
1971 Oct 14
1737 days
D 1967-01 L
[05735]
1973 Mar 9
2249 days
D 1967-01 M
[05766]
1972 Jan 20
1835 days
D 1967-01 N
[05951]
1973 Jun 26
2358 days
D 1967-01 P
[05960]
1973 Jun 26
2358 days
D 1967-01 Q
[05961]
1973 Jun 26
2358 days
D 1967-01 R
[05969]
1975 Sep 14
3168 days
D? 1967-01 S
[05987]
1973 Jun 26?
2358 days?
2001 Apr 5.99
26.30
D 1967-01 T
[05988]
1993 Jan 29
9515 days
D 1967-01 U
[05989]
1976 Nov 7
3588 days
D 1967-01 V
[05990]
1992 Oct 14
9408 days
1967-01 W
[R05998]
= 1965-108 BH
1999 Aug 5.08
29.68
1967-01 X
[R06779]
= 1971-116 B
Intelsat 4-3 Centaur 26
1992 Mar 30.25
27.96
1967-01 Y
[R13904]
= 1981-88 G
Cosmos 1305 SL-06
1999 Aug 4.95
27.57
D 1967-01 Z
[13905]
1992 Sep 20
9384 days
1967-01 AA
[R13906]
= 1965-108 L
1967-01 AB
[R13907]
= 1977-108 D
Meteosat 5 AKM
1998 Sep 30.05
24.39
1967-01 AC
[R13908]
= 1981-88 H
Cosmos 1305 SL-06
1999 Aug 12.67
28.52
1967-01 AD
[R13909]
= 1981-88 J
Cosmos 1305 SL-06
1999 Jul 30.09
26.14
1967-01 AE
[R13910]
= 1981-88 K
Cosmos 1305 SL-06
1999 Jul 29.54
26.12
1967-01 AF
[R13911]
= 1981-88 L
Cosmos 1305 SL-06
1999 Jul 27.96
27.89
1967-01 AG
[R13912]
= 1965-108 M
D 1967-01 AH
[R13939]
1990 May 28
8538 days
1990 May 27.75
26.17
=1973-23 C?
1967-01 AJ
[R21692]
= 1965-108 V
1967-01 AK
[R13957]
= 1965-108 N
1967-01 AL
[R13958]
= 1965-108 BQ
1999 Sep 23.44
26.95
1967-01 AM
[R14756]
= 1965-108 P
1967-01 AN
[R19518]
= 1965-108 Q
1967-01 AP
[R19592]
= 1965-108 R
1967-01 AQ
[R19595]
= 1965-108 S
1967-01 AR
[R20102]
= 1965-108 T
1967-01 AS
[R20469]
= 1990-65 T
1967-01 AT
[20672]
2000 Oct 21.85
26.65
Diademe 1 Diamant 3rd stage fragments, 13 pieces, all have decayed
2004 December 31 – version 1.01
509.42
21129
434
29067
0.678
285
311.07
656.25
368.52
15208
25016
17027
245
690
258
17414
36584
21039
0.564
0.717
0.610
111
90
331
319.42
532.07
472.55
345.37
340.30
15479
21751
20097
16306
16146
292
330
355
274
257
17909
30415
27082
19581
19278
0.569
0.692
0.665
0.592
0.589
2
28
262
132
237
89.35
6621
119
366
0.019
15
425.28
18734
302
24408
0.643
240
534.78
21825
590
30302
0.681
231
RAE Table of Earth Satellites
Year of Launch 1967
Cospar ID
[Norad number]
Analyses indicate that the Diamant
D 1967-11 C
[02673]
D 1967-11 D
[02675]
D 1967-11 E
[02676]
D 1967-11 F
[02677]
D 1967-11 G
[02688]
D 1967-11 H
[02689]
D 1967-11 J
[02690]
D 1967-11 K
[02691]
D 1967-11 L
[02692]
D 1967-11 M
[02900]
D 1967-11 N
[02990]
D 1967-11 P
[03742]
D 1967-11 Q
[04009]
Descent date
3rd stage
1967 Dec
1968 Jan
1967 Dec
1968 Feb
1980 Jun
1990 Jun
1968 May
1967 Oct
1989 Apr
1980 May
1980 Feb
1980 Aug
1982 Nov
Lifetime
Orbital
Inclination
(deg)
Nodal
period
(min)
2001 Feb 18.26
39.97
105.08
2001 Feb 17.90
38.94
2001 Feb 14.26
2001 Feb 14.59
Semi
major axis
(km)
Extra Page 1967- 2
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
7377
561
1436
0.059
344
101.17
7334
553
1358
0.055
85
38.78
99.42
7109
522
939
0.029
276
38.82
105.73
7407
558
1499
0.063
67
is the most likely debris source.
13
308 days
3
329 days
5
300 days
12
369 days
22
7883 days
20
8533 days
8
455 days
29
263 days
21
8108 days
23 A
4853 days
7
4747 days
27
4949 days
12 A
5756 days
Diademe 2 fragments, 12 pieces, 8 have decayed
1967-14 C
[02684]
D 1967-14 D
[02681]
1968 Sep 16
D 1967-14 E
[02683]
1982 Nov 12
1967-14 F
[02685]
D 1967-14 G
[03589]
1979 Nov 20
D 1967-14 H
[03935]
1981 Aug 2
1967-14 J
[14505]
D 1967-14 K
[14633]
1991 Aug 30
D 1967-14 L
[15531]
1991 Aug 19
1967-14 M
[18911]
D 1967-14 N
[18928]
1991 Sep 20
D 1967-14 P
[18929]
1991 Nov 10
579 days
5749 days
4661 days
5282 days
8962 days
8951 days
8983 days
9034 days
Cosmos 149 Cosmos 2 2nd stage fragments, 16 pieces, all have decayed
Analyses indicate that the Cosmos 2 2nd stage is the most likely debris source.
D 1967-24 C
[02724]
1967 Mar 25
4 days
D 1967-24 D
[02725]
1967 Mar 26
5 days
D 1967-24 E
[02726]
1967 Mar 27
6 days
D 1967-24 F
[02727]
1967 Mar 27
6 days
D 1967-24 G
[02728]
1967 Mar 27
6 days
D 1967-24 H
[02729]
1967 Apr 12
22 days
D 1967-24 J
[02730]
1967 Apr 3
13 days
D 1967-24 K
[02731]
1967 Apr 3
13 days
D 1967-24 L
[02732]
1967 Apr 9
19 days
D 1967-24 M
[02733]
1967 Mar 28
7 days
D 1967-24 N
[02734]
1967 Mar 28
7 days
D 1967-24 P
[02737]
1967 Mar 27
6 days
D 1967-24 Q
[02738]
1967 Mar 27
6 days
D 1967-24 R
[02739]
1967 Mar 27
6 days
D 1967-24 S
[02748]
1967 Mar 31
10 days
D 1967-24 T
[02749]
1967 Apr 4
14 days
2004 December 31 – version 1.01
(Revised 2001)
Date of
orbital
determination
RAE Table of Earth Satellites
Year of Launch 1967
Cospar ID
[Norad number]
Descent date
Lifetime
Date of
orbital
determination
Orbital
Inclination
(deg)
(Revised 2001)
Nodal
period
(min)
Semi
major axis
(km)
Perigee
height
(km)
Extra Page 1967- 3
Apogee
height
(km)
Transit 0-12 fragments, 6 pieces, 2 have decayed
Event most likely happened around 28 September 1992 based on element data near the event time and analysis using the COMBO algorithm in the
Astrodynamics Toolkit. One of several Transit-class satellites involved in anomalous events.
1967-34 C
[02777]
2001 Feb 18.32
90.30
103.10
7284
805
1005
1967-34 D
[02778]
2001 Feb 16.78
90.04
108.07
7516
1042
1232
1967-34 E
[04843]
2001 Feb 18.25
90.36
106.60
7448
1047
1091
D 1967-34 F
[06718]
1980 Mar 6
4710 days
D 1967-34 G
[07670]
1981 May 2
5132 days
1967-34 H
[22172]
2001 Feb 15.47
90.11
101.47
7207
814
842
Orbital
Argument
eccentricity of perigee
(deg)
SATRAK
0.014
0.013
0.003
95
68
298
0.002
44
Transit 0-13 fragments, 4 pieces, 2 have decayed
One piece of debris liberated 1995 Feb 11-12. One of several Transit-class satellites involved in anomalous events.
D 1967-48 C
[17723]
1992 Feb 3
9027 days
D 1967-48 D
[19222]
1993 Jan 9
9368 days
1967-48 E
[23562]
2001 Feb 15
89.53
104.45
1967-48 F
[26531]
2000 Sep 19.64
89.58
105.71
Cosmos 169 fragments, 2 pieces, all have decayed
D 1967-69 D
[02881]
1967 Jul 18
D 1967-69 E
[02882]
1967 Jul 18
1 day
1 day
Ferret 17 fragments, 3 pieces, all have decayed.
D 1967-71 B
[02891]
1967 Aug 21
D 1967-71 C
[02892]
1967 Oct 16
D 1967-71 D
[02978]
1967 Oct 17
27 days
83 days
84 days
7347
7406
952
995
984
1061
0.002
0.004
312
91
7306
7550
857
1029
998
1314
0.010
0.019
188
223
Cosmos 176, 10 pieces, all have decayed
Analyses indicate that the Cosmos 176 payload is the most likely debris source.
D 1967-86 C
[02944]
1967 Oct 4
22 days
D 1967-86 D
[02956]
1967 Sep 21
9 days
D 1967-86 E
[02957]
1968 Apr 6
207 days
D 1967-86 F
[02958]
1975 Mar 12
2738 days
D 1967-86 G
[02959]
1968 Apr 2
203 days
D 1967-86 H
[02960]
1967 Oct 3
21 days
D 1967-86 J
[02961]
1967 Oct 6
24 days
D 1967-86 K
[02979]
1968 Jan 13
123 days
D 1967-86 L
[02983]
1967 Nov 4
43 days
D 1967-86 M
[02984]
1967 Oct 31
39 days
Transit O-14 fragments, 9 pieces, 6 have decayed
First event occurred 1981 Apr.
Second event observed in August 1986. One of several known Transits involved in anomalous events.
1967-92 C
[02994]
2001 Feb 18.38
1967-92 D
[03122]
2001 Feb 17.41
D 1967-92 E
[12554]
1989 Mar 20
7847 days
D 1967-92 F
[12555]
1989 Feb 2 A
7801 days
D 1967-92 G
[17176]
1991 Oct 3
8409 days
2004 December 31 – version 1.01
89.46
89.11
103.57
108.80
RAE Table of Earth Satellites
Year of Launch 1967
Cospar ID
D
D
D
1967-92
1967-92
1967-92
1967-92
[Norad number]
H
J
K
L
[20009]
[20652]
[24807]
[25408]
Descent date
Lifetime
1991 Sep 12
1991 Sep 26
2004 Jun 26
8388 days
8402 days
13424 days
Orbital
Inclination
(deg)
Nodal
period
(min)
2001 Feb 15.80
2001 Feb 17.28
89.21
89.21
104.40
104.70
Cosmos 189 fragments, 9 pieces, all have decayed
Fragments designated 1967-108F to 108L possibly belong
D 1967-108 C
[03028]
1968 Jun 18
D 1967-108 D
[03041]
1967 Dec 23
D 1967-108 E
[03042]
1968 Jun 24
D 1967-108 F
[06362]
1974 Feb 27
D 1967-108 G
[06696]
1974 Feb 27
D 1967-108 H
[06697]
1977 Mar 29
D 1967-108 J
[06698]
1974 May 13
D 1967-108 K
[06699]
1974 Mar 29
D 1967-108 L
[06701]
1974 Feb 10
to the 1972-88, 1973-03 and 1973-10 launches.
232 days
54 days
238 days
2312 days
2312 days
3438 days
2387 days
2342 days
2295 days
OV3-6 fragments, 3 pieces, all have decayed
D 1967-120 C
[03060]
1968 Jun 18
D 1967-120 D
[03061]
1967 Dec 25
D 1967-120 E
[03062]
1968 Mar 27
196 days
20 days
113 days
Cosmos 197 2nd stage fragments, 7 pieces, all have decayed
D 1967-126 C
[03083]
1968 Jan 10
15 days
D 1967-126 D
[03084]
1968 Jan 5
10 days
D 1967-126 E
[03085]
1968 Jan 18
23 days
D 1967-126 F
[03086]
1968 Jan 26
31 days
D 1967-126 G
[03087]
1968 Jan 3
8 days
D 1967-126 H
[03089]
1967 Dec 30
4 days
D 1967-126 J
[03090]
1967 Dec 30
4 days
2004 December 31 – version 1.01
(Revised 2001)
Date of
orbital
determination
Semi
major axis
(km)
7345
7359
Extra Page 1967- 4
Perigee
height
(km)
Apogee
height
(km)
Orbital
Argument
eccentricity of perigee
(deg)
941
960
991
1001
0.003
0.003
203
219
