Back Cosmos 314 Spanish ماهواره کاسموس 314 Persian Kosmos 314 Galician Koszmosz–314 Hungarian Космос-314 Macedonian Kosmos 314 Portuguese Kosmos-314 Serbo-Croatian Космос-314 Serbian
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1969-106A |
| SATCAT no. | 04266 |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 325 kilograms (717 lb) |
| Start of mission | |
| Launch date | 11 December 1969, 12:58:59 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 22 March 1970 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 263 kilometres (163 mi) |
| Apogee altitude | 426 kilometres (265 mi) |
| Inclination | 71 degrees |
| Period | 91.4 minutes |
Kosmos 314 (Russian: Космос 314 meaning Cosmos 314), known before launch as DS-P1-Yu No.30, was a Soviet satellite which was launched in 1969 as part of the Dnepropetrovsk Sputnik programme. It was a 325-kilogram (717 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used as a radar calibration target for anti-ballistic missile tests.[1]
- ^ Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Archived from the original on 2 June 2012. Retrieved 14 August 2009.
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