1981-099A
Two-tone telemetry; Hi res satellite
| Kosmos-1313 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1981 Oct 1 | 0900 | Launch by Soyuz-U | Baykonur |
| 0904 | Blok-I burn | ||
| 0908 | Blok-I sep | ||
| 1981 Oct 1 | 89.48 207x291x70.4 | ||
| 1981 Oct 2 | 89.64 233x280x70.4 | ||
| 1981 Oct 15 | 89.50 228x272x70.4 | ||
| 1981 Oct 17 | |||
| 0535? | Deorbit | ||
| 0545? | PO sep | ||
| 0551? | Entry | ||
| 0607? | Landed | ||
1964-005A
The first Block II Saturn I was SA-5. SA-5 carried a live S-IV stage with 4 LOX/LH2 RL10 engines, the same engines as carried by Centaur. It was topped by the first Saturn Instrument Unit, S-IU-5, a dummy S-V stage and a Jupiter nosecone.
The Saturn I launch vehicle took off at 1625 on 1964 Jan 29 from pad 37B at Cape Kennedy. The S-1-5 stage cut off at T+2:27 and the Saturn S-4-5 second stage ignited, entering orbit at 1635. It was the heaviest satellite to date at 17190 kg. SA-5 was in a 264 x 760 km x 31.4 deg orbit. It reentered on 1966 Apr 30.
| SA-5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1964 Jan 29 | 1625:01 | Launch by SA-5 | |
| 1627:21 | IECO | ||
| 1627:26 | OECO | ||
| 1627:28 | T+2:27 Sep 75 km | -5940 x 176 x 30.6 | |
| 1627:29 | T+2:28 S-IV MES | ||
| 1627 | T+2:54 8 camera capsules ejected from S-I | ||
| 1635? | S-I impact | ||
| 1635:31 | T+10:30 S-IV MECO | ||
| 1639 | End of LH2 venting | ||
| 1640 | LOS from Antigua | ||
| 1711 | LOS from Pretoria | ||
| 1964 Jan 30 | 1405 | 94.86 265 x 757 x 31.4 | |
| 1964 Jun 13 | 94.28 263 x 703 x 31.4 | ||
| 1965 Oct 1 | 92.13 254 x 503 x 31.4 | ||
| 1966 Apr 28 | 88.08 174 x 184 x 31.4 | ||
| 1966 Apr 30 | Reentered near Rio Negro, Brazil | ||
1966-093A
Zenit-4 No. 25 resumed Zenit-4 flights after a two month gap.
| Kosmos-130 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1966 Oct 20 | 0846 | Launch by 11A57 | KB |
| 0850? | Blok-I burn | ||
| 0856? | Blok-I sep | 89.7 208 x 314 x 65.0 | |
| 1966 Oct 28 | 0625? | Retrofire | |
| 0645? | Landed after 7.9d | ||
