Mission type | Ionosphere |
---|---|
COSPAR ID | 1967-013A |
SATCAT no. | 02678 |
Mission duration | 142 days |
Spacecraft properties | |
Spacecraft type | DS-U2-I |
Manufacturer | Yuzhnoye |
Launch mass | 315 kg[1] |
Start of mission | |
Launch date | 14 February 1967, 10:04:56 GMT |
Rocket | Kosmos-2I 63SM |
Launch site | Kapustin Yar, Site 86/1 |
Contractor | Yuzhnoye |
End of mission | |
Decay date | 6 July 1967 |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Low Earth |
Perigee altitude | 207 km |
Apogee altitude | 1336 km |
Inclination | 48.4° |
Period | 100.3 minutes |
Epoch | 14 February 1967 |
Kosmos 142 (Russian: Космос 142 meaning Cosmos 142), also known as DS-U2-I No.2, was a Soviet satellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 315 kilograms (694 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used to study the effects on radio waves of passing through the ionosphere.[3]
A Kosmos-2I 63SM carrier rocket was used to launch Kosmos 142 into low Earth orbit. The launch took place from Site 86/1 at Kapustin Yar.[4] The launch occurred at 10:04:56 GMT on 14 February 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 1967-013A.[1] The North American Air Defense Command assigned it the catalogue number 02678.
Kosmos 142 was the second of three DS-U2-I satellites to be launched.[6] It was operated in an orbit with a perigee of 207 kilometres (129 mi), an apogee of 1,336 kilometres (830 mi), an inclination of 48.4°, and an orbital period of 100.3 minutes.[2] On 6 July 1967, it decayed from orbit and reentered the atmosphere.[7]