Mission type | Micrometeoroid research |
---|---|
COSPAR ID | 1967-056A |
SATCAT no. | 02832 |
Mission duration | 128 days |
Spacecraft properties | |
Spacecraft type | DS-U2-MP |
Manufacturer | Yuzhnoye |
Launch mass | 357 kg[1] |
Start of mission | |
Launch date | 5 June 1967, 05:03:00 GMT |
Rocket | Kosmos-2I 63SM |
Launch site | Kapustin Yar, Site 86/1 |
Contractor | Yuzhnoye |
End of mission | |
Decay date | 11 October 1967 |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Low Earth |
Perigee altitude | 244 km |
Apogee altitude | 611 km |
Inclination | 48.4° |
Period | 93.1 minutes |
Epoch | 5 June 1967 |
Kosmos 163 (Russian: Космос 163 meaning Cosmos 163), also known as DS-U2-MP No.2, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 357 kilograms (787 lb) spacecraft, which was built by the Yuzhnoye Design Office, and was used to investigate micrometeoroids and cosmic dust particles in near-Earth space.[3]
A Kosmos-2I 63SM carrier rocket was used to launch Kosmos 163 into low Earth orbit. The launch took place from Site 86/1 at Kapustin Yar.[4] The launch occurred at 05:03:00 GMT on 5 June 1967, and resulted in the successful insertion of the satellite into orbit.[5] Upon reaching orbit, the satellite was assigned its Kosmos designation, and received the International Designator 1967-056A.[1] The North American Air Defense Command assigned it the catalogue number 02832.[1]
Kosmos 163 was the second of two DS-U2-MP satellites to be launched, after Kosmos 135.[5][6] It was operated in an orbit with a perigee of 244 kilometres (152 mi), an apogee of 611 kilometres (380 mi), an inclination of 48.4°, and an orbital period of 93.1 minutes.[2] It decayed from its orbit and reentered the atmosphere on 11 October 1967.[7]