Kosmos 611

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Kosmos 611
Mission typeABM radar target
COSPAR ID1973-094A Edit this at Wikidata
SATCAT no.06952Edit this on Wikidata
Spacecraft properties
Spacecraft type
Yuzhnoye
Launch mass400 kilograms (880 lb)
Start of mission
Launch date28 November 1973, 09:29:58 (1973-11-28UTC09:29:58Z) UTC
Rocket
Kosmos-2I 63SM
Launch sitePlesetsk 133/1
End of mission
Decay date19 June 1974 (1974-06-20)
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude264 kilometres (164 mi)
Apogee altitude466 kilometres (290 mi)
Inclination70.9 degrees
Period91.8 minutes
 

Kosmos 611 (

Yuzhnoye Design Bureau, and was used as a radar calibration target for anti-ballistic missile tests.[1]

Launch

Kosmos 611 was successfully launched into

carrier rocket
.

Orbit

Upon reaching orbit, the satellite was assigned its

06952.

Kosmos 611 was the sixty-seventh of seventy nine

inclination, and an orbital period of 91.8 minutes.[6] It remained in orbit until it decayed and reentered the atmosphere on 19 June 1974.[6]

See also

References

  1. ^ a b Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Archived from the original on 2 June 2012. Retrieved 1 September 2009.
  2. ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 1 September 2009.
  3. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 1 September 2009.
  4. ^ "Cosmos 611". NSSDC Master Catalog. US National Space Science Data Center. Retrieved 1 September 2009.
  5. ^ Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 1 September 2009.
  6. ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 1 September 2009.