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 | |
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