Kosmos 133
Soyuz 7K-OK spacecraft with an active docking unit. | |
| Mission type | Test Flight |
|---|---|
| Operator | Experimental Design Bureau (OKB-1) |
| COSPAR ID | 1966-107A |
| SATCAT no. | 02601 |
| Mission duration | 1 day, 23 hours and 19 minutes |
| Spacecraft properties | |
| Spacecraft | Soyuz 7K-OK No.2 |
| Spacecraft type | Soyuz 7K-OK |
| Manufacturer | Experimental Design Bureau (OKB-1) |
| Launch mass | 6450 kg |
| Landing mass | 2500 kg |
| Dimensions | 7.13 m long 2.72 m wide |
| Start of mission | |
| Launch date | 28 November 1966 11:02:00 GMT |
| Rocket | Soyuz 11A511 s/n U15000-02 |
| Launch site | Baikonour, Site 31/6 |
| Contractor | Experimental Design Bureau (OKB-1) |
| End of mission | |
| Disposal | Exploded: on the self-destruct command of ground |
| Landing date | 30 November 1966, 10:21 GMT (exploded) |
| Landing site | Kazakh Steppe of Kazakhstan (planned) |
| Orbital parameters | |
| Reference system | Geocentric orbit |
| Regime | Low Earth orbit |
| Perigee altitude | 171.0 km |
| Apogee altitude | 223.0 km |
| Inclination | 51.9° |
| Period | 88.4 minutes |
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Kosmos 133 (Russian: Космос 133, meaning "Kosmos 133"), Soyuz 7K-OK No.2, was the first uncrewed test flight of the Soyuz spacecraft, and first mission of the Soyuz programme, as part of the Soviet space programme.