Mission type | Optical imaging reconnaissance |
---|---|
Operator | OKB-1 |
COSPAR ID | 1966-106A |
SATCAT no. | 02599 |
Mission duration | 8 days |
Spacecraft properties | |
Spacecraft type | Zenit-2 |
Manufacturer | OKB-1 |
Launch mass | 4730 kg[1] |
Start of mission | |
Launch date | 19 November 1966 08:09:00 GMT[2] |
Rocket | Vostok-2 s/n N15001-08 |
Launch site | Baikonur, Site 31/6 |
Contractor | OKB-1 |
End of mission | |
Disposal | Recovered |
Landing date | 27 November 1966 07:12 GMT[3] |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Low Earth |
Perigee altitude | 210 km |
Apogee altitude | 276 km |
Inclination | 65.0° |
Period | 89.3 minutes |
Epoch | 19 November 1966 |
Kosmos 132 (Russian: Космос 132 meaning Cosmos 132) or Zenit-2 No.46 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1966. A Zenit-2 spacecraft, Kosmos 132 was the forty-third of eighty-one such satellites to be launched[4][5] and had a mass of 4,730 kilograms (10,430 lb).[1]
Kosmos 132 was launched by a Vostok-2 rocket, serial number N15001-08,[6] flying from Site 31/6 at the Baikonur Cosmodrome. The launch took place at 08:09 GMT on 19 November 1966, and following its successful arrival in orbit the spacecraft received its Kosmos designation, along with the International Designator 1966-106A and the Satellite Catalog Number 02599.[1]
Kosmos 132 was operated in a low Earth orbit, at an epoch of 19 November 1966, it had a perigee of 210 kilometres (130 mi), an apogee of 276 kilometres (171 mi), an inclination of 65.0°, and an orbital period of 89.3 minutes.[2] After spending eight days in orbit, Kosmos 132 was deorbited with its return capsule descending under parachute, landing at 07:12 GMT on 27 November 1966, and recovered by Soviet force.[3]