Friday, May 12, 1989
Thursday, May 11, 1989
Tuesday, May 9, 1989
Monday, May 8, 1989
Meteor 203
1977-117A
The third Meteor-2 was launched in Dec 1977.
Object 14950, cataloged in 1984 May, shows a decay pattern identical to the Blok E stage, and may be a duplicate catalog entry.
| Meteor-2 (F3) | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1977 Dec 14 | 0930 | Launch by Vostok 8A92M | PL |
| 0934? | Blok E burn | ||
| 0940? | Blok E sep | ||
| 102.5 856 x 894 x 81.2 | |||
| 1980s | End of ops | ||
Gambit-3 46
1976-027A
KH-8 flight 46 (GAMBIT 4346) was launched on 1976 Mar 27 by Titan 23B Agena D from Vandenberg. The mission lasted 57 days (56 days photo), and again used the new 125 km perigee and 96.4 deg inclination.
| KH-8 46 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1976 Mar 22 | 1814? | Launch by Titan 23B Agena D | V SLC4W |
| 1816? | Titan stage 1 sep | ||
| 1819 | Titan stage 2 sep | ||
| 1819 | Agena burn | ||
| 1824? | Agena MECO | ||
| 89.3 125 x 347 x 96.4 | |||
| 1976 Apr 7 | 89.21 125 x 344 x 96.4 | ||
| 1976 Apr 18 | 89.21 124 x 346 x 96.4 | ||
| 1976 Apr 18 | 2029? | SRV-1 deorbit opp | |
| 1976 Apr 19 | 0921 | 89.22 128 x 343 x 96.4 | |
| 1976 Apr 19 | 2114 | Orbit raise | 89.42 123 x 367 x 96.4 |
| 1976 Apr 25 | 89.29 121 x 356 x 96.4 | ||
| 1976 May 7 | 89.18 128 x 339 x 96.4 | ||
| 1976 May 9 | 89.27 128 x 348 x 96.5 | ||
| 1976 May 10 | 2011 | Last orbit raise | 89.34 132 x 351 x 96.4 |
| 1976 May 11 | 2129 | 89.25 127 x 347 x 96.4 | |
| 1976 May 15 | 1013 | 88.96 127 x 318 x 96.4 | |
| 1976 May 16 | 0659 | 88.85 127 x 307 x 96.4 | |
| 1976 May 17 | 2030? | SRV-2 deorbit after 56 days | |
| 1976 May 18 | 1214 | 88.51 124 x 277 x 96.4 | |
| 1976 May 18 | 2233 | 87.38 65 x 223 x 96.4 | |
| 1976 May 18 | 2302? | reentered | |
Kosmos 1973
1988-088A
Two-tone telemetry; Medium res satellite
| Kosmos-1973 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Sep 22 | 1020:00 | Launch by Soyuz | PL |
| 1024 | Blok I burn | ||
| 1028 | Blok I MECO | ||
| 1988 Sep 22 | 90.14 194x368x72.9 | ||
| 1988 Sep 23 | 92.26 368x403x72.9 | ||
| 1988 Oct 4 | 92.26 356x415x72.9 | ||
| 1988 Oct 9 | 92.25 356x413x72.9 | ||
| 1988 Oct 10 | |||
| 0335? | Deorbit | ||
| 0345? | PO sep | -80 x 405 x 72.86 | |
| 0403? | Entry | ||
| 0415? | Landed | ||
Sunday, May 7, 1989
CAT-1
1979-104A
CAT, the Capsule Ariane Technologique, was a cylinder containing a ballast Al alloy sphere. CAT carried instruments to measure accelerations, noise levels, temperature, pressure and stress during launch of the first Ariane rocket.
| CAT 1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1979 Dec 24 | 1414:41 | Launch by Ariane LO1 | CSG |
| 1417:11 | Stage 1 sep 51 km (T+2:30) | -6130 x 81 x 14 | |
| 1417:41 | T+3:00 L140 LOS | ||
| 1418:49 | Fairing sep (T+4:08) | -5489 x 130 x 14.9 | |
| T+4:48 L33 MECO | |||
| 1419:34 | Stage 2 sep (T+4:53) | -4028 x 199 x 17 | |
| 1423:49 | T+4:57 St 3 burn 9:08 | ||
| 1428:46 | T+14:05 St 3 burnout | ||
| 1429:53 | CAT sep (T+912s) | ||
| 635.3 201 x 36003 x 17.6 | |||
| 1979 Dec 27 | end of ops? | ||
| 1982 Nov 14 | Reentered | ||
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