Kosmos 148
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1967-023A |
| SATCAT no. | 02712 |
| Spacecraft properties | |
| Spacecraft type | DS-P1-I |
| Manufacturer | Yuzhnoye |
| Launch mass | 325 kilograms (717 lb) |
| Start of mission | |
| Launch date | 16 March 1967, 17:30 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 7 May 1967 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 270 kilometres (170 mi) |
| Apogee altitude | 404 kilometres (251 mi) |
| Inclination | 71 degrees |
| Period | 91.3 minutes |
Kosmos 148 (Russian: Космос 148 meaning Cosmos 148), also known as DS-P1-I No.2 was a satellite which was used as a radar target for anti-ballistic missile tests. It was launched by the Soviet Union in 1967 as part of the Dnepropetrovsk Sputnik programme.[1]
It was launched aboard a Kosmos-2I 63SM rocket,[2] from Site 133/1 at Plesetsk. The launch occurred at 17:30 UTC on 16 March 1967.[3] This was the first DS-P1-I launch to use the Kosmos-2I 63SM, which replaced the earlier 63S1 model. It was also the first launch from Site 133 at the Plesetsk Cosmodrome.
Kosmos 148 was placed into a low Earth orbit with a perigee of 270 kilometres (170 mi), an apogee of 404 kilometres (251 mi), 71 degrees of inclination, and an orbital period of 91.3 minutes.[1] It decayed from orbit on 7 May 1967.[4]
Kosmos 148 was the second of nineteen DS-P1-I satellites to be launched.[1] Of these, all reached orbit successfully except the seventh.[5]
See also
References
- ^ a b c Wade, Mark. "DS-P1-I". Encyclopedia Astronautica. Retrieved 28 May 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 28 May 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Retrieved 28 May 2009.
- ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 28 May 2009.
- ^ Wade, Mark. "DS". Encyclopedia Astronautica. Retrieved 28 May 2009.
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