Kosmos 147
| Mission type | Optical imaging reconnaissance |
|---|---|
| Operator | OKB-1 |
| COSPAR ID | 1967-022A |
| SATCAT no. | 02710 |
| Mission duration | 8 days |
| Spacecraft properties | |
| Spacecraft type | Zenit-2 |
| Manufacturer | OKB-1 |
| Launch mass | 4000 kg |
| Start of mission | |
| Launch date | 13 March 1967, 12:10:23 GMT |
| Rocket | Vostok-2 s/n N15001-06 |
| Launch site | Plesetsk, Site 41/1 |
| Contractor | OKB-1 |
| End of mission | |
| Disposal | Recovered |
| Landing date | 21 March 1967, 06:29 GMT |
| Landing site | Steppe du Kazakhstan |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 195 km |
| Apogee altitude | 301 km |
| Inclination | 65.0° |
| Period | 89.5 minutes |
| Epoch | 13 March 1967 |
Kosmos 147 (Russian: Космос 147 meaning Cosmos 147) or Zenit-2 No.44 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1967. A Zenit-2 spacecraft, Kosmos 147 was the forty-seventh of eighty-one such satellites to be launched. and had a mass of 4,000 kilograms (8,800 lb).
Kosmos 147 was launched by a Vostok-2 rocket, serial number N15001-06, flying from Site 41/1 at the Plesetsk Cosmodrome. The launch took place at 12:10:23 GMT on 13 March 1967, and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1967-022A and the Satellite Catalog Number 02710.
Kosmos 147 was operated in a low Earth orbit, at an epoch of 13 March 1967, it had a perigee of 195 kilometres (121 mi), an apogee of 301 kilometres (187 mi), an inclination of 65.0°, and an orbital period of 89.5 minutes. After eight days in orbit, Kosmos 147 was deorbited, with its return capsule descending under parachute and landing at 06:29 GMT on 21 March 1967, and recovered by the Soviet forces. An unspecified problem with the satellite resulted in the mission being considered a partial failure.