Kosmos 601
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1973-075A |
| SATCAT no. | 06875 |
| Spacecraft properties | |
| Spacecraft type | Yuzhnoye |
| Launch mass | 400 kilograms (880 lb) |
| Start of mission | |
| Launch date | 16 October 1973, 14:00:01 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 15 August 1974 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 197 kilometres (122 mi) |
| Apogee altitude | 1,404 kilometres (872 mi) |
| Inclination | 81.8 degrees |
| Period | 100.9 minutes |
Kosmos 601 (
Yuzhnoye Design Bureau, and was used as a radar calibration target for anti-ballistic missile tests.[1]
Launch
Kosmos 601 was successfully launched into
carrier rocket
.
Orbit
Upon reaching orbit, the satellite was assigned its
North American Aerospace Defense Command assigned it the catalogue number
06875.
Kosmos 601 was the sixty-fifth of seventy nine
inclination, and an orbital period of 100.9 minutes.[6] It remained in orbit until it decayed and reentered the atmosphere on 15 August 1974.[6]
See also
References
- ^ a b Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Archived from the original on 2 June 2012. Retrieved 1 September 2009.
- ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 1 September 2009.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 1 September 2009.
- ^ "Cosmos 601". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 1 September 2009.
- ^ Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 1 September 2009.
- ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 1 September 2009.
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