1970-099A
T2K No. 1 was launched in Nov 1970 as Kosmos-379. The modified 11A511L Soyuz-L launch vehicle placed the spacecraft in a typical Soyuz-type parking orbit. The T2K consisted of the cabin, including the Blok E propulsion system, and a lower section containing the landing gear.
| Kosmos 379 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1970 Nov 24 | 0515:01 | Launch by 11A511L | KB |
| 0520? | Blok-I burn | ||
| 0524? | Blok-I sep | ||
| 0700 | 88.61 189 x 222 x 51.67 (TLE) | ||
| 0930 | 88.78 191 x 237 x 51.61 (TLE) | ||
| 2130 | 88.67 192 x 232 x 51.62 (RAE) | ||
| 1970 Nov 25 | 1430? | LK Blok-E burn | 98.79 196 x 1206 x 51.65 |
| Simulated lunar descent and hover | |||
| 1970 Nov 26 | Ion flux meter turned on | ||
| 1970 Nov 27 | 0805? | Landing gear jettison | 98.63 188 x 1198 x 51.59 |
| 1970 Nov 28 | 0515? | Blok-E burn 2 (LOI simulation) | 259.80 177 x 14041 x 51.72 |
| 1970 Nov 28 | Simulated passive rendezvous phase | ||
| 1970 Dec 5 | End of transmissions | ||
| 1970 Dec 21 | 94.1 179 x 766 x 51.6 | ||
| 1983 Sep 21 | Reentered over 51S, 22W | ||
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