Kosmos 119

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Kosmos 119
Mission typeIonospheric
COSPAR ID1966-043A Edit this at Wikidata
SATCAT no.02182
Mission duration100 days
Spacecraft properties
Spacecraft type
Yuzhnoye
Launch mass250 kg[1]
Start of mission
Launch date24 May 1966, 05:30:59 GMT
Rocket
Yuzhnoye
End of mission
Decay date30 November 1966
Orbital parameters
Reference systemGeocentric[2]
RegimeLow Earth
Perigee altitude208 km
Apogee altitude1292 km
Inclination48.5°
Period99.8 minutes
Epoch24 May 1966
 

Kosmos 119 (

Yuzhnoye Design Bureau, and was used to study the effects on radio waves of passing through the ionosphere.[3]

A

Kosmos 119 was the first of three

reentered the atmosphere.[7]

See also

References

  1. ^ a b "Cosmos 119: Display 1966-043A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 29 March 2020. Public Domain This article incorporates text from this source, which is in the public domain.
  2. ^ a b "Cosmos 119: Trajectory 1966-043A". nssdc.gsfc.nasa.gov. NASA. 27 February 2020. Retrieved 29 March 2020.
  3. ^ Wade, Mark. "DS-U2-I". Encyclopedia Astronautica. Archived from the original on 8 January 2010. Retrieved 23 December 2009.
  4. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 23 December 2009.
  5. ^ Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Archived from the original on 18 June 2012. Retrieved 23 December 2009.
  6. ^ Krebs, Gunter. "DS-U2-I". Gunter's Space Page. Retrieved 23 December 2009.
  7. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 23 December 2009.