Mission type | ABM radar target |
---|---|
COSPAR ID | 1966-061A |
SATCAT no. | 02295 |
Mission duration | 155 days |
Spacecraft properties | |
Spacecraft type | DS-P1-Yu |
Manufacturer | Yuzhnoye |
Launch mass | 325 kg[1] |
Start of mission | |
Launch date | 8 July 1966, 05:31:00 GMT |
Rocket | Kosmos-2I 63S1 |
Launch site | Kapustin Yar, Site 86/1 |
Contractor | Yuzhnoye |
End of mission | |
Decay date | 10 December 1966 |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Low Earth |
Perigee altitude | 256 km |
Apogee altitude | 512 km |
Inclination | 48.8° |
Period | 92.2 minutes |
Epoch | 8 July 1966 |
Kosmos 123 (Russian: Космос 123 meaning Cosmos 123), also known as DS-P1-Yu No.5 was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles.[3] It was built by the Yuzhnoye Design Bureau, and launched in 1966 as part of the Dnepropetrovsk Sputnik programme.[4]
A Kosmos-2I 63S1 carrier rocket was used to launch Kosmos 123.[5] The launch occurred from Site 86/1 at Kapustin Yar, at 05:31 GMT on 8 July 1966.[6] and following its successful arrival in orbit the spacecraft received its Kosmos designation; along with the International Designator 1966-061A[1] and the Satellite Catalog Number 02295.
Kosmos 123 separated from the carrier rocket into a low Earth orbit with a perigee of 256 kilometres (159 mi), an apogee of 512 kilometres (318 mi), an inclination of 48.8°, and an orbital period of 92.2 minutes.[2] It decayed from orbit on 10 December 1966.[7] Kosmos 123 was the sixth of seventy-nine DS-P1-Yu satellites to be launched,[4] and the fifth of seventy-two to successfully reach orbit.