Kosmos 608
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1973-091A |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 400 kilograms (880 lb) |
| Start of mission | |
| Launch date | 20 November 1973, 12:29:58 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 10 July 1974 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 265 kilometres (165 mi) |
| Apogee altitude | 486 kilometres (302 mi) |
| Inclination | 70.9 degrees |
| Period | 92.1 minutes |
Kosmos 608 (Russian: Космос 608 meaning Cosmos 608), known before launch as DS-P1-Yu No.69, 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]
Launch
[edit | edit source]Kosmos 608 was successfully launched into low Earth orbit at 12:29:58 UTC on 20 November 1973.[2] The launch took place from Site 133/1 at the Plesetsk Cosmodrome,[3] and used a Kosmos-2I 63SM carrier rocket.
Orbit
[edit | edit source]Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1973-091A.[4] The North American Aerospace Defense Command assigned it the catalogue number 06941.
Kosmos 608 was the sixty-sixth of seventy nine DS-P1-Yu satellites to be launched,[1] and the sixtieth of seventy two to successfully reach orbit.[5] It was operated in an orbit with a perigee of 265 kilometres (165 mi), an apogee of 486 kilometres (302 mi), 70.9 degrees of inclination, and an orbital period of 92.1 minutes.[6] It remained in orbit until it decayed and reentered the atmosphere on 10 July 1974.[6]
See also
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References
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