This is an old revision of this page, as edited by CRS-20 (talk | contribs) at 23:26, 19 April 2020. The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.
Revision as of 23:26, 19 April 2020 by CRS-20 (talk | contribs)(diff) ← Previous revision | Latest revision (diff) | Newer revision → (diff)| 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. .
See also
