Mission type | Technology |
---|---|
COSPAR ID | 1965-084A |
SATCAT no. | 01629 |
Mission duration | 76 days |
Spacecraft properties | |
Spacecraft type | DS-U2-V |
Manufacturer | Yuzhnoye |
Launch mass | 305 kg[1] |
Start of mission | |
Launch date | 19 October 1965, 05:45:00 GMT |
Rocket | Kosmos-2M 63S1M |
Launch site | Kapustin Yar, Site 86/1 |
Contractor | Yuzhnoye |
End of mission | |
Decay date | 3 January 1966 |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Low Earth |
Perigee altitude | 216 km |
Apogee altitude | 513 km |
Inclination | 48.4° |
Period | 91.7 minutes |
Epoch | 19 October 1965 |
Kosmos 93 (Russian: Космос 93 meaning Cosmos 93), also known as DS-U2-V No.1, was a Soviet satellite which was launched in 1965 as part of the Dnepropetrovsk Sputnik programme. It was a 305 kilograms (672 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used to conduct classified technology development experiments for the Soviet armed forces.[3]
A Kosmos-2M 63S1M[4] carrier rocket was used to launch Kosmos 93 into low Earth orbit. The launch took place from Site 86/1 at Kapustin Yar.[5] The launch occurred at 05:45 GMT on 19 October 1965, and resulted in the successful insertion of the satellite into orbit.[6] Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1965-084A.[7] The North American Air Defense Command assigned it the catalogue number 01629.
Kosmos 93 was the first of four DS-U2-V satellites to be launched.[8] It was operated in an orbit with a perigee of 216 kilometres (134 mi), an apogee of 513 kilometres (319 mi), an 48.4° of inclination, and an orbital period of 91.7 minutes. On 3 January 1966, it decayed from orbit and reentered the atmosphere.[9][10]