Contents

Kosmos 105

Kosmos 105

A Zenit reentry capsule
Names	Zenit 2-34
Mission type	Optical imaging reconnaissance
Operator	OKB-1
COSPAR ID	1966-003A
SATCAT no.	1945
Mission duration	8 days
Spacecraft properties
Spacecraft type	Zenit-2
Manufacturer	OKB-1
Launch mass	4730 kg[1]
Start of mission
Launch date	22 January 1966 08:38:00 GMT
Rocket	Vostok-2
Launch site	Baikonur 31/6
Contractor	OKB-1
End of mission
Disposal	Recovered
Landing date	30 January 1966
Orbital parameters
Reference system	Geocentric[2]
Regime	Low Earth
Perigee altitude	204 km
Apogee altitude	310 km
Inclination	65.0°
Period	89.7 minutes
Epoch	22 January 1966
Zenit programme Zenit-2 ← Zenit 2-33 Zenit 2-35 →   Kosmos (satellites) ← Kosmos 104 Kosmos 106 →

Kosmos 105 (Russian: Космос 105 meaning Cosmos 105) or Zenit-2 No.34 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1966. A Zenit-2 spacecraft, Kosmos 105 was the thirty-fourth of eighty-one such satellites to be launched^[3] and had a mass of 4,730 kilograms (10,430 lb).

Kosmos 105 was launched by a Vostok-2 rocket^[4] flying from Site 31/6 at the Baikonur Cosmodrome. The launch took place at 08:38 GMT on 22 January 1966,^[5] and following its successful arrival in orbit the spacecraft received its Kosmos designation, along with the International Designator 1966-003A and the Satellite Catalog Number 01945.^[6]

Kosmos 105 was operated in a low Earth orbit; at an epoch of 22 January 1966 it had a perigee of 204 kilometres (127 mi), an apogee of 310 kilometres (190 mi), an inclination of 65.0° and an orbital period of 89.7 minutes.^[7] On 30 January 1966, after eight days in orbit, the satellite was deorbited with its return capsule descending by parachute for recovery by Soviet force.^[8]

References[edit]

This article about one or more spacecraft of the Soviet Union is a stub. You can help Wikipedia by expanding it.