Kosmos 136
| Mission type | Optical imaging reconnaissance |
|---|---|
| Operator | OKB-1 |
| COSPAR ID | 1966-115A |
| SATCAT no. | 02624 |
| Mission duration | 8 days |
| Spacecraft properties | |
| Spacecraft type | Zenit-2 |
| Manufacturer | OKB-1 |
| Launch mass | 4730 kg |
| Start of mission | |
| Launch date | 19 December 1966 12:00:01 GMT |
| Rocket | Vostok-2 s/n N15001-09 |
| Launch site | Plesetsk, Site 41/1 |
| Contractor | OKB-1 |
| End of mission | |
| Disposal | Recovered |
| Landing date | 27 December 1966 06:00 GMT |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 188 km |
| Apogee altitude | 280 km |
| Inclination | 64.6° |
| Period | 89.4 minutes |
| Epoch | 19 December 1966 |
Kosmos 136 (Russian: Космос 136 meaning Cosmos 136) or Zenit-2 No.47 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1966. A Zenit-2 spacecraft, Kosmos 136 was the forty-fourth of eighty-one such satellites to be launched and had a mass of 4,730 kilograms (10,430 lb). In addition to its reconnaissance mission, the satellite was also used for scientific research.
Kosmos 136 was launched by a Vostok-2 rocket, serial number N15001-09, flying from Site 41/1 at the Plesetsk Cosmodrome. The launch took place at 12:00:01 GMT on 19 December 1966, and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1966-115A and the Satellite Catalog Number 02624.
Kosmos 136 was operated in a low Earth orbit, at an epoch of 19 December 1966, it had a perigee of 188 kilometres (117 mi), an apogee of 280 kilometres (170 mi), an inclination of 64.6°, and an orbital period of 89.4 minutes. After eight days in orbit, Kosmos 136 was deorbited, with its return capsule descending under parachute, landing at 06:00 GMT on 27 December 1966, and recovered by Soviet force.