Kosmos 204
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1968-015A |
| SATCAT no. |
03139 |
| Spacecraft properties | |
| Spacecraft type | DS-P1-I |
| Manufacturer | Yuzhnoye |
| Launch mass | 300 kilograms (660 lb) |
| Start of mission | |
| Launch date | 5 March 1968, 11:20 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 2 March 1969 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee | 485 kilometres (301 mi) |
| Apogee | 626 kilometres (389 mi) |
| Inclination | 70.9 degrees |
| Period | 95.7 minutes |
Kosmos 204 (Russian: Космос 204 meaning Cosmos 204), also known as DS-P1-I No.3 was a satellite which was used as a radar target for anti-ballistic missile tests. It was launched by the Soviet Union in 1968 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 11:20 UTC on 5 March 1968.[3]
Kosmos 204 was placed into a low Earth orbit with a perigee of 485 kilometres (301 mi), an apogee of 626 kilometres (389 mi), 70.9 degrees of inclination, and an orbital period of 95.7 minutes.[1] It decayed from orbit on 2 March 1969.[4]
Kosmos 204 was the third of nineteen DS-P1-I satellites to be launched.[1] Of these, all reached orbit successfully except the seventh.[5]
See also
References
- 1 2 3 Wade, Mark. "DS-P1-I". Encyclopedia Astronautica. Archived from the original on 30 November 2009. Retrieved 28 May 2009.
- ↑ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 28 May 2009.
- ↑ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 8 July 2012. Retrieved 28 May 2009.
- ↑ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 28 May 2009.
- ↑ Wade, Mark. "DS". Encyclopedia Astronautica. Archived from the original on 31 March 2009. Retrieved 28 May 2009.