Kosmos 165
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1967-059A |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 250 kilograms (550 lb) |
| Start of mission | |
| Launch date | 12 June 1967, 18:06 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 15 January 1968 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee | 198 kilometres (123 mi) |
| Apogee | 1,399 kilometres (869 mi) |
| Inclination | 81.9 degrees |
| Period | 100.84 minutes |
Kosmos 165 (Russian: Космос 165 meaning Cosmos 165), also known as DS-P1-Yu No.11 was a radar calibration target satellite which was used by the Soviet Union for tests of anti-ballistic missiles. It was built by the Yuzhnoye Design Bureau, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme.[1]
Kosmos 165 was launched using a Kosmos-2I 63SM carrier rocket, which flew from Site 133/1 at Plesetsk Cosmodrome.[2] The launch occurred at 18:06 UTC on 12 June 1967.[3]
Kosmos 165 separated from its carrier rocket into a low Earth orbit with a perigee of 198 kilometres (123 mi), an apogee of 1,399 kilometres (869 mi), 81.9 degrees of inclination, and an orbital period of 100.84 minutes.[1][4] It decayed from orbit on 15 January 1968.[4] Kosmos 165 was the eighth of seventy nine DS-P1-Yu satellites to be launched,[1] and the seventh of seventy two to successfully reach orbit.[5]
See also
References
- ↑ 1.0 1.1 1.2 Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Retrieved 9 August 2009.
- ↑ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 August 2009.
- ↑ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Retrieved 9 August 2009.
- ↑ 4.0 4.1 McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 9 August 2009.
- ↑ Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 9 August 2009.
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