Mission type | Test flight |
---|---|
Operator | Experimental Design Bureau (OKB-1) |
COSPAR ID | 1968-093A |
SATCAT no. | 03511 |
Mission duration | 3 days |
Orbits completed | 48 |
Spacecraft properties | |
Spacecraft | Soyuz 7K-OK No.11 |
Spacecraft type | Soyuz 7K-OK (passive) |
Manufacturer | Experimental Design Bureau (OKB-1) |
Launch mass | 6,520 kg (14,370 lb) [1] |
Landing mass | 2,800 kg (6,200 lb) |
Dimensions | 7.13 m (23.4 ft) long 2.72 m (8 ft 11 in) wide |
Start of mission | |
Launch date | 25 October 1968, 09:00 GMT |
Rocket | Soyuz |
Launch site | Baikonur, Site 1/5[2] |
Contractor | Experimental Design Bureau (OKB-1) |
End of mission | |
Landing date | 28 October 1968, 07:51 GMT |
Landing site | Kazakh Steppe, Kazakhstan |
Orbital parameters | |
Reference system | Geocentric orbit[3] |
Regime | Low Earth orbit |
Perigee altitude | 196.0 km (121.8 mi) |
Apogee altitude | 200.0 km (124.3 mi) |
Inclination | 51.70° |
Period | 88.50 minutes |
Soyuz 2 (Russian: Союз 2, Union 2) was an uncrewed spacecraft (capsule number 7K-OK-P No. 11)[4] in the Soyuz family, intended to be the target of a docking maneuver by the crewed Soyuz 3 spacecraft. It was intended to be the first docking of a crewed spacecraft in the Soviet space program. Although the two craft approached closely, the docking did not take place and the first successful Soviet docking of crewed spacecraft took place in the joint Soyuz 4 and Soyuz 5 mission. It served for the radio search and as a target vehicle for docking by the crewed Soyuz 3. Soyuz 2 soft-landed in a predetermined area of the Soviet Union,[1] near the village of Maiburnak, southwest of the city of Karaganda.[4]
Trajectory
was invoked but never defined (see the help page).