Engineering:Kosmos 327
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1970-020A |
| Spacecraft properties | |
| Spacecraft type | DS-P1-I |
| Manufacturer | Yuzhnoye |
| Launch mass | 300 kilograms (660 lb) |
| Start of mission | |
| Launch date | 18 March 1970, 14:39:56 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 19 January 1971 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 280 kilometres (170 mi) |
| Apogee altitude | 819 kilometres (509 mi) |
| Inclination | 71 degrees |
| Period | 95.7 minutes |
Kosmos 327 (Russian: Космос 327 meaning Cosmos 327), also known as DS-P1-I No.8 was a satellite which was used as a radar target for anti-ballistic missile tests. It was launched by the Soviet Union in 1970 as part of the Dnepropetrovsk Sputnik programme.[1]
Launch
It was launched aboard a Kosmos-2I 63SM rocket,[2] from Site 133/1 at Plesetsk. The launch occurred at 14:39:56 UTC on 18 March 1970.[3]
Orbit
Kosmos 327 was placed into a low Earth orbit with a perigee of 280 kilometres (170 mi), an apogee of 819 kilometres (509 mi), 71 degrees of inclination, and an orbital period of 95.7 minutes.[1] It decayed from orbit on 19 January 1971.[4]
Kosmos 327 was the eighth of nineteen DS-P1-I satellites to be launched.[1] Of these, all reached orbit successfully except the seventh.[5]
References
- ↑ 1.0 1.1 1.2 Wade, Mark. "DS-P1-I". Encyclopedia Astronautica. http://www.astronautix.com/craft/dsp1i.htm.
- ↑ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. http://planet4589.org/space/log/launchlog.txt.
- ↑ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. http://www.astronautix.com/lvs/kosmos2.htm.
- ↑ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. http://www.planet4589.org/space/log/satcat.txt.
- ↑ Wade, Mark. "DS". Encyclopedia Astronautica. http://www.astronautix.com/project/ds.htm.
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