1967-049A
Zenit-4 No. 31 was launched in May 1967 from Plesetsk and it was the second Zenit-4 flight at 65.6 degrees.
| Kosmos-161 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1967 May 22 | 1400:00 | Launch by 11A57 | PL |
| 1404 | Blok-I burn | ||
| 1409 | Blok-I sep | 89.71 201 x 321 x 65.64 (RAE) | |
| 1967 May 23 | 0743 | 89.73 200 x 321 x 65.6 | |
| 1967 May 29 | 1131 | 89.60 196 x 312 x 65.6 | |
| 1967 May 30 | 0834? | Deorbit | |
| 0856? | Landed | ||
1967-019A
DS-U2-M No. 2 carried a maser clock like that on the first DS-U2-M satellite (Kosmos-97). It was used to measure the gravitational redshift predicted by Einstein's general theory.
| Kosmos-145 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1967 Mar 3 | 0645 | Launch by 11K63 | GTsP4 |
| 0647 | Stage 2 burn | ||
| 0652? | Stage 2 sep, orbit insertion | 108.60 215 x 2116 x 48.4 | |
| 1967 Aug 30 | End of ops | ||
| 1968 Mar 8 | Reentered | ||
1966-068A
Zenit-4 No. 21 was launched from Baikonur into a 51.8 degree orbit in Jul 1966, beginning a rapid series of Zenit-4 launches over the next several months.
| Kosmos-126 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1966 Jul 28 | 1050 | Launch by 11A57 | KB |
| 1054? | Blok-I burn | ||
| 1059? | Blok-I sep | 90.0 204 x 350 x 51.8 | |
| 1966 Jul 28 | 1808 | 90.05 207 x 346 x 51.8 | |
| 1966 Jul 29 | 2238 | 90.05 209 x 343 x 51.8 | |
| 1966 Aug 5 | 1803 | 89.97 207 x 338 x 51.8 | |
| 1966 Aug 6 | 0600? | Retrofire | |
| 0601? | PO sep | ||
| 0620? | Landed after 8.9d | ||
1966-019A
GATV 5003 comprised Agena 5003 mated with the TDA 3 payload. After the Gemini 8 mission the Agena propulsion systems were used for several orbit-changing burns.
| TDA 3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1966 Mar 16 | 1500:03 | Launch from LC14 | |
| 1502:12 | T+2:09 BECO | ||
| 1502:14 | T+2:11 58 km booster sep | -5954 x 124 x 28.8 | |
| 1504:46 | T+4:43 SECO | ||
| 1505:07 | T+5:04 VECO | ||
| 1505:11 | T+5:08 Atlas sep | -4398 x 293 x 29.0 | |
| -4406 x 288 x 28.85 (SR6) | |||
| 1506:01 | T+5:58 Agena SPS burn | ||
| 1506:20 | T+6:17 Agena PPS burn | -4401 x 294 x 29.0 | |
| 1506:21 | T+6:18 SPS shutdown | ||
| 1506:29 | T+6:26 Fairing | ||
| 1509:23 | T+9:20 PPS MECO, Orbit insertion | 298 x 298 x 28.9 | |
| Rendezvous by Gemini 8 | |||
| 2315:24 | Docking by Gemini 8 | ||
| 2357:14 | Undocking | ||
| 291 x 298 x 29.02 | |||
| 1966 Mar 17 | 1423:49 | PPS-1 Orbit raise | 298 x 407 x 28.86 |
| 1966 Mar 17 | 1944:37 | PPS-2 Orbit raise 31m/s | 407 x 407 x 28.88 |
| 1966 Mar 18 | 0757:28 | PPS-3 Plane change 488m/s | 407 x 618 x 30.6 |
| 1242:25 | PPS-4 Min impulse 29m/s | 407 x 515 x 30.6 | |
| 1620:21 | PPS-5 Plane change | 477 x 710 x 29.0 | |
| 1927:54 | PPS-6 HA | 410 x 476 x 29.0 | |
| 2320:10 | PPS-7 HA | 410 x 753 x 29.0 | |
| 1966 Mar 19 | 0409:01 | PPS-8 HA | 410 x 413 x 29.0 |
| 0911:49 | SPS-II-1 Cal burn 21s | ||
| 1966 Mar 19 | 1120 | 407 x 411 x 28.9 | |
| 1219:50 | SPS-II-2 Inc adjust 50s | ||
| 1966 Mar 25 | 0300? | End of transmissions | |
| 1966 Jul 20 | 2220? | Rendezvous by Gemini 10 | |
| EVA contact by Collins | |||
| 1966 Nov 4 | 1127 | 92.31 382 x 392 x 28.9 | |
| 1967 Jul 23 | 90.60 303 x 304 x 28.9 | ||
| 1967 Sep 14 | 88.33 188 x 195 x 28.9 | ||
| 1967 Sep 15 | 2010? | Reentered | |
