Kosmos 580
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1973-057A |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 400 kilograms (880 lb) |
| Start of mission | |
| Launch date | 22 August 1973, 11:24:55 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 1 April 1974 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee | 268 kilometres (167 mi) |
| Apogee | 472 kilometres (293 mi) |
| Inclination | 71 degrees |
| Period | 91.9 minutes |
Kosmos 580 (Russian: Космос 580 meaning Cosmos 580), known before launch as DS-P1-Yu No.59, was a Soviet satellite which was launched in 1973 as part of the Dnepropetrovsk Sputnik programme. It was a 400-kilogram (880 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used as a radar calibration target for anti-ballistic missile tests.[1]
Contents
Launch
Kosmos 580 was successfully launched into low Earth orbit at 11:24:55 UTC on 22 August 1973.[2] The launch took place from Site 133/1 at the Plesetsk Cosmodrome,[3] and used a Kosmos-2I 63SM carrier rocket.
Orbit
Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1973-057A.[4] The North American Aerospace Defense Command assigned it the catalogue number 06793.
Kosmos 580 was the sixty-fourth of seventy nine DS-P1-Yu satellites to be launched,[1] and the fifty-eighth of seventy two to successfully reach orbit.[5] It was operated in an orbit with a perigee of 268 kilometres (167 mi), an apogee of 472 kilometres (293 mi), 71 degrees of inclination, and an orbital period of 91.9 minutes.[6] It remained in orbit until it decayed and reentered the atmosphere on 1 April 1974.[6]
See also
References
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