Kosmos 152
Appearance
Mission type | ABM Radar target |
---|---|
COSPAR ID | 1967-028A |
SATCAT no. | 02722 |
Mission duration | 133 days |
Spacecraft properties | |
Spacecraft type | Yuzhnoye |
Launch mass | 325 kg[1] |
Start of mission | |
Launch date | 25 March 1967, 06:57:00 GMT |
Rocket | Yuzhnoye |
End of mission | |
Decay date | 5 August 1967 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 272 km |
Apogee altitude | 488 km |
Inclination | 71.0° |
Period | 92.2 minutes |
Epoch | 25 March 1967 |
Kosmos 152 (
Yuzhnoye Design Bureau, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme,[3] and had a mass of 325 kilograms (717 lb).[1]
Kosmos 152 was launched using a
Kosmos-2I 63SM carrier rocket, which flew from Site 133/3 at Plesetsk Cosmodrome.[4] The launch occurred at 06:57 GMT on 25 March 1967.[5]
Kosmos 152 separated from its carrier rocket into a
inclination of 71.0°, and an orbital period of 92.2 minutes.[6] It decayed from orbit on 5 August 1967.[7] Kosmos 152 was the seventh of seventy nine DS-P1-Yu satellites to be launched,[3]
and the sixth of seventy two to successfully reach orbit.
See also
References
- ^ a b "Cosmos 152: Display 1967-028A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 13 April 2020.
This article incorporates text from this source, which is in the public domain.
- ^ Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 9 August 2009.
- ^ a b Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Archived from the original on 2 June 2012. Retrieved 9 August 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 August 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 9 August 2009.
- ^ "Cosmos 152: Trajectory 1967-028A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 13 April 2020.
- ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 9 August 2009.