![]() A Zenit reentry capsule | |
Names | Zenit 2-26 |
---|---|
Mission type | Optical imaging reconnaissance |
Operator | OKB-1 |
COSPAR ID | 1965-025A |
SATCAT no. | 1305 |
Mission duration | 8 days |
Spacecraft properties | |
Spacecraft type | Zenit-2 |
Manufacturer | OKB-1 |
Launch mass | 4720 kg [1] |
Start of mission | |
Launch date | 25 March 1965, 10:04:00 GMT [1] |
Rocket | Vostok-2 |
Launch site | Baikonur 31/6 |
Contractor | OKB-1 |
End of mission | |
Disposal | Recovered |
Landing date | 2 April 1965 |
Orbital parameters | |
Reference system | Geocentric [2] |
Regime | Low Earth |
Perigee altitude | 201 km |
Apogee altitude | 267 km |
Inclination | 65.0° |
Period | 89.2 minutes |
Epoch | 25 March 1965 |
Zenit programme Zenit-2 |
Kosmos 64 ( Russian: Космос 64 meaning Cosmos 64) or Zenit-2 No.26 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1965. A Zenit-2 satellite, Kosmos 64 was the twenty-sixth of eighty-one such spacecraft to be launched [3] [4] and had a mass of 4,720 kilograms (10,410 lb).
Kosmos 64 was launched by a Vostok-2 rocket, serial number G15001-06, [5] flying from Site 31/6 at the Baikonur Cosmodrome. The launch took place at 10:04 GMT on 25 March 1965, and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1965-025A and the Satellite Catalog Number 01305. [1]
Kosmos 64 was operated in a low Earth orbit, on 25 March 1965 it had a perigee of 201 kilometres (125 mi), an apogee of 267 kilometres (166 mi), an inclination of 65.0° and an orbital period of 89.2 minutes. On 2 April 1965, after eight days in orbit, Kosmos 64 was deorbited with its return capsule descending by parachute for recovery by Soviet forces. [4]
![]() A Zenit reentry capsule | |
Names | Zenit 2-26 |
---|---|
Mission type | Optical imaging reconnaissance |
Operator | OKB-1 |
COSPAR ID | 1965-025A |
SATCAT no. | 1305 |
Mission duration | 8 days |
Spacecraft properties | |
Spacecraft type | Zenit-2 |
Manufacturer | OKB-1 |
Launch mass | 4720 kg [1] |
Start of mission | |
Launch date | 25 March 1965, 10:04:00 GMT [1] |
Rocket | Vostok-2 |
Launch site | Baikonur 31/6 |
Contractor | OKB-1 |
End of mission | |
Disposal | Recovered |
Landing date | 2 April 1965 |
Orbital parameters | |
Reference system | Geocentric [2] |
Regime | Low Earth |
Perigee altitude | 201 km |
Apogee altitude | 267 km |
Inclination | 65.0° |
Period | 89.2 minutes |
Epoch | 25 March 1965 |
Zenit programme Zenit-2 |
Kosmos 64 ( Russian: Космос 64 meaning Cosmos 64) or Zenit-2 No.26 was a Soviet, first generation, low resolution, optical film-return reconnaissance satellite launched in 1965. A Zenit-2 satellite, Kosmos 64 was the twenty-sixth of eighty-one such spacecraft to be launched [3] [4] and had a mass of 4,720 kilograms (10,410 lb).
Kosmos 64 was launched by a Vostok-2 rocket, serial number G15001-06, [5] flying from Site 31/6 at the Baikonur Cosmodrome. The launch took place at 10:04 GMT on 25 March 1965, and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1965-025A and the Satellite Catalog Number 01305. [1]
Kosmos 64 was operated in a low Earth orbit, on 25 March 1965 it had a perigee of 201 kilometres (125 mi), an apogee of 267 kilometres (166 mi), an inclination of 65.0° and an orbital period of 89.2 minutes. On 2 April 1965, after eight days in orbit, Kosmos 64 was deorbited with its return capsule descending by parachute for recovery by Soviet forces. [4]