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Mission type | Optical imaging reconnaissance |
---|---|
Operator | OKB-1 |
COSPAR ID | 1968-032A |
SATCAT no. | 03203 |
Mission duration | 100 days |
Spacecraft properties | |
Spacecraft type | Zenit-4 |
Manufacturer | OKB-1 |
Launch mass | 4000 kg |
Start of mission | |
Launch date | 18 April 1968, 10:33:00 GMT |
Rocket | Voskhod 11A57 s/n V15001-12 |
Launch site | Plesetsk, Site 41/1 |
Contractor | OKB-1 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 200 km |
Apogee altitude | 373 km |
Inclination | 81.4° |
Period | 90.3 minutes |
Epoch | 18 April 1968 |
Kosmos 214 (Template:Lang-ru meaning Cosmos 214) or Zenit-4 No.45 was a Soviet, second generation, high resolution, optical film-return reconnaissance satellite launched in 1968. A Zenit-4 spacecraft, Kosmos 214 was the forty-seventh of eighty-one such satellites to be launched. and had a mass of 4,000 kilograms (8,800 lb). "Cosmos 214: Display 1968-032A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 20 April 2020.{{cite web}}
: CS1 maint: url-status (link) This article incorporates text from this source, which is in the public domain.
Kosmos 214 was launched by a Voskhod 11A57 rocket, serial number V15001-12, flying from Site 41/1 at the Plesetsk Cosmodrome. The launch took place at 10:33:00 GMT on 18 April 1968, and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1968-032A and the Satellite Catalog Number 03203.
Kosmos 214 was operated in a low Earth orbit, at an epoch of 18 April 1968, it had a perigee of 200 kilometres (121 mi), an apogee of 373 kilometres (187 mi), an inclination of 81.4°, and an orbital period of 90.3 minutes."Cosmos 214: Trajectory 1968-032A".nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 20 April 2020. This article incorporates text from this source, which is in the public domain.
This article incorporates text from this source, which is in the public domain.
See also
References
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