Kosmos 36
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1964-042A |
| SATCAT no. | 00844 |
| Mission duration | 213 days |
| Spacecraft properties | |
| Spacecraft type | Yuzhnoye |
| Launch mass | 325 kg[1] |
| Start of mission | |
| Launch date | 30 July 1964, 03:36:00 GMT |
| Rocket | Yuzhnoye |
| End of mission | |
| Decay date | 28 February 1965 |
| Orbital parameters | |
| Reference system | Geocentric[2] |
| Regime | Low Earth |
| Perigee altitude | 261 km |
| Apogee altitude | 477 km |
| Inclination | 49.0° |
| Period | 91.9 minutes |
| Epoch | 30 July 1964 |
Kosmos 36 (
Yuzhnoye Design Bureau
.
Kosmos 36 was launched using a
Kosmos-2I 63S1 carrier rocket,[4] which flew from Mayak-2 at Kapustin Yar. The launch occurred at 03:36 GMT on 30 July 1964.[5]
After separating from its carrier rocket, Kosmos 36 was in a
inclination, and an orbital period of 91.9 minutes. It decayed from orbit on 28 February 1965.[6] Kosmos 36 was the first of seventy nine DS-P1-Yu satellites to be launched,[7]
of which all but seven were successful. The next launch of a DS-P1-Yu satellite, the DS-P1-Yu #2 will be on 12 February 1965, failed due to a second stage malfunction.
See also
References
- ^ https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1964-042A - 27 February 2020
- ^ https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=1964-042A - 27 February 2020
- ^ Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 8 August 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 8 August 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 8 August 2009.
- ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 8 August 2009.
- ^ Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Archived from the original on 2 June 2012. Retrieved 8 August 2009.
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