Kosmos 261
| Mission type | Aeronomy Auroral |
|---|---|
| COSPAR ID | 1968-117A |
| Spacecraft properties | |
| Spacecraft type | DS-U2-GK |
| Manufacturer | Yuzhnoye |
| Launch mass | 347 kilograms (765 lb)[1] |
| Start of mission | |
| Launch date | 19 December 1968, 23:55:00 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 12 February 1969 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee | 201 kilometres (125 mi) |
| Apogee | 611 kilometres (380 mi) |
| Inclination | 71 degrees |
| Period | 92.68 minutes |
Kosmos 261 (Russian: Космос 261 meaning Cosmos 261), also known as DS-U2-GK No.1, was a Soviet satellite which was launched in 1968 as part of the Dnepropetrovsk Sputnik programme. It was a 347-kilogram (765 lb) spacecraft,[1] which was built by the Yuzhnoye Design Bureau, and was used to study the density of air in the upper atmosphere, and investigate aurorae.[1]
A Kosmos-2I 63SM carrier rocket was used to launch Kosmos 261 into low Earth orbit from Site 133/1 at the Plesetsk Cosmodrome.[2] The launch occurred at 23:55:00 UTC on 19 December 1968, and resulted in the successful insertion of the satellite into orbit.[3] Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1968-117A.[4] The North American Aerospace Defense Command assigned it the catalogue number 03624.
Kosmos 261 was the first of two DS-U2-GK satellites to be launched.[1][5] It was operated in an orbit with a perigee of 201 kilometres (125 mi), an apogee of 611 kilometres (380 mi), 71 degrees of inclination, and an orbital period of 92.68 minutes.[6] It decayed from orbit and reentered the atmosphere on 12 February 1969.[6]
See also
References
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