1974-091A
DS-P1-Yu No. 73 was launched in Nov 1974.
| Kosmos-695 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1974 Nov 20 | 1200 | Launch by 11K63 | NIIP-53 LC133/1 |
| 1202 | Stage 2 burn | ||
| 1206? | Stage 2 sep | ||
| 1974 Nov 20 | 92.0 273 x 468 x 71.0 | ||
| 1975 May 10 | End of ops | ||
| 1975 Jul 15 | Reentered | ||
1974-091A
DS-P1-Yu No. 73 was launched in Nov 1974.
| Kosmos-695 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1974 Nov 20 | 1200 | Launch by 11K63 | NIIP-53 LC133/1 |
| 1202 | Stage 2 burn | ||
| 1206? | Stage 2 sep | ||
| 1974 Nov 20 | 92.0 273 x 468 x 71.0 | ||
| 1975 May 10 | End of ops | ||
| 1975 Jul 15 | Reentered | ||
1968-050A
The third and final IDCSP Initial Defense Communications Satellite Program cluster was launched by Titan IIIC on 1968 Jun 13. It had initially been planned as a replenishment launch but most of the previous IDCSP satellites were still operating well. The first satellite of the eight in the cluster was IDCSP 20,.
| IDCSP 20 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1968 Jun 13 | 1403:50 | Launch by Titan IIIC (3C-16) | CC LC41 |
| T+0:02:01 SRM sep | |||
| T+0:02? St 1 burn | |||
| T+0:04:17 St 1 sep | |||
| T+0:04:41 Fairing | |||
| T+0:07:38 Titan Stage 2 MECO | |||
| 1411:41 | T+7:51 Transtage burn 1 14s | ||
| 1411:55 | T+8:05 MECO-1 | 148 x 176 km x 28.6 | |
| 1509:32 | T+1:05:42 Transtage burn 2 | ||
| 1514:35 | T+1:10:45 MECO-2 | 250 x 33700 x 26.4 | |
| 2005 | T+6:02:52 MES-3 | ||
| 2008 | T+6:04:38 MECO-3 | ||
| 2010? | IDCSP sep | ||
| 1335.7 33758 x 33841 x 0.2 | |||
1973-076A
Molniya-2 F7 was launched on 1973 Oct 19 into a 62.8 degree orbit, the first Molniya-2 to enter such an orbit. It was located in the D plane.
| Molniya-2 F7 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1973 Oct 19 | 1026:01 | 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 | |||
| 1034 | T+8:50 Blok-I sep | ||
| T+53:16 BOZ burn | |||
| 1119 | T+53:56 BOZ sep | ||
| ML burn | |||
| T+56:46 ML MECO | |||
| 1122 | T+56:54 ML sep | ||
| 1973 Oct 19 | 1140 | (approx?) | 722.96 555 x 40055 x 62.9 |
| 1973 Oct 22 | 1315 | 735.87 616 x 40626 x 62.8 | |
| Lower orbit | |||
| 1973 Oct 25 | 1415 | 717.94 502 x 39859 x 62.8 | |
| 1973 Dec 19 | 1016 | 717.81 608 x 39747 x 62.9 | |
| 1975 May 21 | 717.67 511 x 39837 x 63.8 | ||
| Orbit raise | |||
| 1975 May 27 | 732.61 496 x 40587 x 63.9 | ||
| 1975 Oct 3 | 732.58 488 x 40593 x 64.1 | ||
| 1975 Oct 7 | End of ops | ||
| 1978 Jan 19 | 732.63 1141 x 39943 x 65.0 | ||
| 1983 May 23 | 687.25 111 x 38726 x 64.1 | ||
| 1983 Jul 8 | Reentered | ||
1963-012A
Zenit-2 No. 10 was launched the day after the landing of Zenit-2 No. 8, the first time this had happened in the Zenit program. The spacecraft flew a 10 day mission, a record which would stand for five years.
| Kosmos-16 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1963 Apr 28 | 0849:56 | Launch by Vostok 8A92 | KB |
| 0855? | Blok-E burn | ||
| 0859? | Blok-E sep | ||
| 90.4 207 x 401 x 65 (TASS) | |||
| 90.38 194 x 388 x 65.0 (RAE) | |||
| 1963 Apr 28 | 90.33 198 x 383 x 65.1 | ||
| 1963 May 7 | 90.22 190 x 379 x 65.0 | ||
| 1963 May 8 | 0630? | Retrofire | |
| 1963 May 8 | 0650? | Landed after 9.9d | |
1966-092A
Molniya-1 No. 7 was the last OKB-1 built Molniya and the first to achieve a stabilized 12-hour period ground track, in Nov 1966. Improvements to the solar panels made it longer lived, operating for more than a year.
| Molniya-1 7 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1966 Oct 20 | 0750 | Launch by 8K78M | KB |
| 0754? | Blok-I | ||
| 0759? | Blok-I MECO | ||
| 0850? | BOZ burn | ||
| 0851? | Blok L burn | ||
| 0855? | Blok L sep | ||
| 1966 Nov 8 | 713.23 454 x 39675 x 64.6 | ||
| 1966 Nov | Ground track stabilized | ||
| 1966 Dec 1 | 718.12 464 x 39907 x 64.7 | ||
| 1967 Jan 27 | 717.87 480 x 39878 x 64.8 | ||
| 1968 Jan 29 | End of ops | ||
| 1968 Jul 3 | 712.48 181 x 39911 x 65.0 | ||
| 1968 Sep 11 | Reentered | ||
1965-072A
Vehicle 1 in the Block 2 series was orbited on 1965 Sep 10, using a Thor Burner 1 with an FW4 upper stage. It operated on its primary mission for 341 days. The satellite carried a 1.3cm video camera, the medium resolution `C' IR camera system with 16 sensors in the 0.2-5 micron band and the 5-30 micron bands, and a high resolution radiometer (HRR) in the 7-14 micron bands.
| DSAP 01213 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1965 Sep 10 | 0441:38 | Launch by Thor Burner 1 | V 4300B6 |
| 0444:16 | Thor MECO (T+2:38) | ||
| 0444:24 | Thor VECO (T+2:46) | ||
| 0444:35 | Heatshield sep (T+2:57) | ||
| 0452:03 | FW4 spinup (T+10:25) | ||
| 0452:04 | Thor sep (T+10:26) | ||
| 0452:10 | FW4 burn (T+10:32) | ||
| 0452:43 | FW4 burnout (T+11:05) | ||
| 0452 | FW4 sep | ||
| 1430 | 101.93 649 x 1054 x 98.7 (RAE) | ||
| 1966 Aug 17 | end of primary mission | ||
| 1966 Sep 22 | end of ops | ||
Summary: The chapters within are outlines for both future stories I’ve got planned (in the case that I never get around to writing them) a...