1990-066A
Geo-IK 3?. GEOS geodetic transponder.
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1990 Jul 30 | 0006:00 | Launch by 11K68 | PL |
| T+2:00 St 1 sep | |||
| T+3:33 GO sep | |||
| T+4:38 St 2 sep, alt 126 km | -2400? x 170? x 73.6 | ||
| T+5:19 S5M burn 1, alt 143 km | -2400? x 170? x 73.6 | ||
| 0012 | T+6:48 S5M MECO-1, alt 173 km | 90 x 1502 x 73.6 | |
| T+49:37 BOZ burn | |||
| T+51:15 S5M MES2 | 90 x 1502 x 73.6 | ||
| T+51:33 S5M MECO2 | |||
| 0058 | T+52:03 S5M sep | ||
| 1990 Jul 30 | 116.1 1484x1526x73.6 | ||
1986-059A
RCS was 40m2; 3 debris tracked, all small.
| Kosmos-1769 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1986 Aug 4 | 0508 | Launch by 11K69 | Baykonur |
| 0510 | Stage 1 sep | ||
| 0512 | Stage 2 sep | ||
| 0556? | AKM burn | ||
| 1986 Aug 4 | 111x365x65.0 | ||
| 1986 Aug 4 | 427x444x65.0 | ||
| 1986 Aug 5 | 429x444x65.0 | ||
| 1987 Jul 14 | 93.30 426x446x65.0 | ||
| 1987 Aug 5 | 93.30 426 x 445 x 65.0 | ||
| 1987 Aug 6 | Orbit lower | 92.52 377 x 417 x 65.0 | |
| 1987 Aug 6 | 92.08 308 x 444 x 65.0 | ||
| 1987 Oct 29 | 91.79 297x419x65.0 | ||
| 1988 Feb 10 | 89.31 218x255x65.0 | ||
| 1988 Feb 18 | reentered | ||
1972-060A
Kosmos-513 was launched in Aug 1972 from Baikonur. The Zenit-4M satellite was recovered 14 days later.
| Kosmos-513 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1972 Aug 2 | 0815:00 | Launch by 11A57 | KB |
| 0819 | Blok-I burn | ||
| 0823 | Blok-I sep | ||
| 1972 Aug 2 | 1835 | 89.73 204 x 318 x 65.0 | |
| 1972 Aug 3 | 1200 | 89.73 203 x 320 x 64.97 (RAE) | |
| 1232 | 89.72 202 x 318 x 65.0 | ||
| Orbit lower | |||
| 1972 Aug 4 | 0329 | 89.35 173 x 311 x 65.0 | |
| 1972 Aug 10 | 2135 | 89.11 169 x 291 x 65.0 | |
| Orbit adjust | |||
| 1972 Aug 12 | 0445 | 89.06 171 x 284 x 65.0 | |
| Orbit raise apogee | |||
| 1043 | 89.93 169 x 372 x 65.0 | ||
| 1972 Aug 14 | Engine sep (60E) | ||
| 1972 Aug 15 | 0439 | 89.86 169 x 365 x 65.0 | |
| 1972 Aug 15 | 0434? | Retrofire | |
| 0444? | PO sep | ||
| 0449? | Entry | ||
| 0506? | Landed | ||
1969-065A
Ferret 14 was launched in 1969. The second STRAWMAN carried the standard THRESHER and REAPER payloads and the second CONVOY ABM study payload. CONVOY II (Mission 7239) was targeted at TI (technical intelligence) on DOG HOUSE, HEN HOUSE and the still-classified advanced ABM signal.
| OPS 8285 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1969 Jul 31 | 1019 | Launch by LTTA Thor Agena D | V |
| 1020? | Castor II SRMs sep (T+1:42?) | ||
| 1022? | Thor MECO (T+3:37?) | ||
| 1022? | Thor VECO (T+3:46?) | ||
| 1022? | Thor sep (T+3:52?) | ||
| 1022? | Agena burn (T+3:58?) | ||
| 1027? | Agena MECO (T+8:00?) | -100? x 483 x 75.0 | |
| 1049? | Agena MES-2 | ||
| 1049? | Agena MECO-2 | ||
| 1969 Aug 1 | 1058 | 94.63 460 x 540 x 75.0 | |
| 1969 Oct 13 | Wideband recorder failed, EOB mode only | ||
| 1970 Feb 1 | 94.40 454 x 524 x 75.0 | ||
| 1970 Aug 23 | THRESHER and REAPER turned off | ||
| In caretaker status | |||
| 1971 Jul 26 | Battery 2 failed | ||
| 1971 Jul 27 | Switched off by command from Guam after 725 days | ||
| 1973 Jan 3 | 88.41 190 x 201 x 75.0 | ||
