1965-097A
The Zenit-2 No. 31 satellite was launched in Nov 1965 by 8A92 from Baikonur. The Blok-E third stage appears to have overburned, leaving the satellite in an orbit with an unusually high apogee. However, the Zenit reentry vehicle was deorbited after the usual 8 day flight.
| Kosmos-98 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1965 Nov 27 | 0820 | Launch by Vostok 8A92 | KB |
| 0825? | Blok-E burn | ||
| 0830? | Blok-E sep | ||
| 92 216 x 570 x 65.0 (TASS) | |||
| 1965 Nov 28 | 1200 | 92.1 205 x 547 x 65.0 (RAE) | |
| 1965 Dec 5 | 0800? | Landed | |
1971-078A
Gektor mission 22, Kosmos-439, was launched on 1971 Sep 21 by 11A57 from Plesetsk and flew an 11 day mission.
| Kosmos-439 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1971 Sep 21 | 1200:00 | Launch by 11A57 | PL |
| 1204 | Blok-I burn | ||
| 1208 | Blok-I sep | ||
| 1743 | 89.48 207 x 289 x 65.4 | ||
| 1971 Sep 24 | 2014 | 89.39 207 x 281 x 65.4 | |
| 1971 Sep 30 | 1314 | 89.30 207 x 272 x 65.4 | |
| 1971 Oct 2 | 0520? | Retrofire | |
| 0530? | PO sep | ||
| 0537? | Entry | ||
| 0552? | Landed | ||
1985-113A
| Kosmos-1707 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1985 Dec 12 | 1551 | Launch by 11K68 | Plesetsk |
| T+2:00 St 1 sep | |||
| T+3:33? GO sep | |||
| T+4:38? St 2 sep | |||
| T+5:20? S5M burn 1 | |||
| 1557 | T+6:48 S5M MECO1 km | 60? x 650 x 82.5 | |
| T+40:58? S5M burn 2 | |||
| T+41:08? S5M MECO2 | |||
| 1631? | T+41:38? S5M sep | ||
| 1985 Dec 12 | 598x654x82.6 Node=345 at 85346 | ||
| 1985 Dec 20 | 634x664x82.6 | ||
1987-041A
| Kosmos-1844 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1987 May 13 | 0540:00 | Launch by Zenit-2 | KB |
| 0542:23 | T+2:23 St 1 MECO | ||
| 0542:25 | T+2:25 Stage 1 sep | ||
| 0542:25 | T+2:25 Stage 2 burn | ||
| 0542:40 | T+2:40 GO sep | ||
| 0546:42 | T+6:42 Stage 2 MECO | 150? x 850? x 71.0 | |
| 0555? | T+15m? Stage 2 VECO | ||
| 0555? | Stage 2 sep motor covers | ||
| 0555? | T+15m? Stage 2 sep | ||
| 1987 May 18 | 101.94 848x853x71.0 | ||
1965-039A
Apollo-Saturn 105 (AS-105) was launched at 0735 on 1965 May 25. It reached a 97.0 min, 502 x 740 km x 31.7 deg orbit at 0746 and delivered Apollo BP-26 to orbit. It reentered on 1979 Nov 3. Pegasus II was attached to the Saturn S-4-8 rocket stage.
| SA-8 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1965 May 25 | 0735:01 | Launch by Saturn I | |
| 0737:23 | IECO | ||
| 0737:29 | OECO | ||
| 0737:30 | SI sep | ||
| 0737:31 | S4 MES | ||
| 0737:41 | Ullage sep | ||
| 0737:41 | LES sep | ||
| 0745:25 | S4 MECO | ||
| 0745:35 | Insertion | 506 x 748 x 31.78 (MPR) | |
| 0748:26 | Apollo BP-26 sep | ||
| 0749:26 | Pegasus wing deploy | ||
| 0750:07 | Pegasus deploy complete | ||
| 0820 | C-band beacon end tx | ||
| 1000? | End of tx | ||
1990-023A
| Kosmos-2061 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1990 Mar 20 | 0025:22 | Launch by Kosmos from Plesetsk | |
| T+2:10 St 1 MECO | |||
| T+2:12 St 1 sep | |||
| T+2:12 St 2 burn 59km | |||
| T+2:27 Fairing sep 76km | |||
| 0033? | T+8:03 St 2 MECO 150 km | 150 x 1003? x 83 | |
| T+1:02:19 St 2 MES2 | |||
| T+1:02:30 St 2 MECO2 | |||
| 0128? | T+1:02:50 St 2 sep | ||
| 1990 Mar 20 | 105.0 971x1018x82.9 | ||
