Kosmos 132
| 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 |
| Start of mission | |
| Launch date | 19 November 1966 08:09:00 GMT |
| 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 |
| Orbital parameters | |
| Reference system | Geocentric |
| 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 and had a mass of 4,730 kilograms (10,430 lb).
Kosmos 132 was launched by a Vostok-2 rocket, serial number N15001-08, 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.
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. 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.