1992-050A
Molniya-1T (F90, N84) was launched in Aug 1992.
| Molniya-1T F90 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1992 Aug 6 | 1930:59 | Launch by 8K78M | PL |
| BVGD sep | |||
| GO sep | |||
| T+4:46 Blok A sep | |||
| T+4:56 KhO sep | |||
| T+8:46 Blok-I MECO | |||
| 1939 | T+8:50 Blok-I sep | ||
| T+53:16 BOZ burn | |||
| 2024 | T+53:56 BOZ sep | ||
| ML burn | |||
| T+56:46 ML MECO | |||
| 2027 | T+56:54 ML sep | ||
| 1992 Aug 8 | 737.01 620 x 40679 x 62.9 | ||
| 1992 Aug 12 | 716.98 626 x 39687 x 62.9 | ||
| 1992 Aug 15 | 716.95 630 x 39683 x 62.9 | ||
1969-033A
The 20th DS-P1-Yu was a standard Subgroup 1 mission.
| Kosmos-277 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1969 Apr 4 | 1300 | Launch by 11K63 | GTsP4 |
| 1302 | Stage 2 burn | ||
| 1307? | Stage 2 sep | ||
| 1969 Apr 6 | 0500? | 91.90 268 x 466 x 70.95 | |
| 1969 May 18 | 0516? | Stage 2 reentered | |
| 1969 Jun 10 | End of operations | ||
| 1969 Jul 6 | 0238? | Reentered | |
1988-026A
The long delayed NASA/CRA San Marco D/L satellite finally left the pad in Mar 1988, becoming San Marco 5. The satellite, with a mass of 237 kg, carried more sophisticated instruments than its predecessors. A companion spacecraft, San Marco D/M, was never launched. L stood for 'low orbit' and M for 'medium orbit'.
| San Marco 5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Mar 25 | 1950 | Launch by Scout G-1 | SMLC |
| T+1:24 Stage 1 burnout | |||
| T+1:27 Stage 2 burn | |||
| T+2:08 Stage 2 burnout | |||
| T+2:23 Fairing sep | |||
| 1952 | Stage 3 burn (T+2:24), 85 km | ||
| T+3:13 Stage 3 burnout | |||
| T+7:28 Stage 3 sep | |||
| 1957 | Stage 4 burn (T+7:33), 276 km | ||
| 1958 | T+8:07 Stage 4 burnout | ||
| 2001 | T+11:38 Stage 4 sep | 262 x 619 x 3.0 | |
| 1988 Dec 6 | Reentered | ||
