Kosmos 133

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
	Soyuz programme Soyuz 7K-OK No.1 →

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.

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