Neha Patil (Editor)

Kosmos 265

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Mission type
  
ABM radar target

Spacecraft type
  
DS-P1-Yu

Rocket
  
Kosmos-2I 63SM

Launch date
  
7 February 1969

Decay date
  
1 May 1969

COSPAR ID
  
1969-012A

Launch mass
  
325 kg (717 lb)

Launch site
  
Plesetsk 133/1

Manufacturer
  
Yuzhnoye Design Office

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Kosmos 265 (Russian: Космос 265 meaning Cosmos 265), known before launch as DS-P1-Yu No.21, was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles. It was built by the Yuzhnoye Design Bureau, and launched in 1969 as part of the Dnepropetrovsk Sputnik programme. It had a mass of 325 kg (717 lb).

Kosmos 265 was launched from Plesetsk Cosmodrome Site 133/1, atop a Kosmos-2I 63SM carrier rocket. The launch occurred on 7 February 1969 at 13:59 UTC, and resulted in Kosmos 265's successful deployment into low Earth orbit. Upon reaching orbit, it was assigned its Kosmos designation, and received the International Designator 1969-012A.

Kosmos 265 was operated in an orbit with a perigee of 261 kilometres (162 mi), an apogee of 413 kilometres (257 mi), 70.9 degrees of inclination, and an orbital period of 91.3 minutes. It remained in orbit until it decayed and reentered the atmosphere on 1 May 1969. It was the eighteenth of seventy nine DS-P1-Yu satellites to be launched, and the seventeenth of seventy two to successfully reach orbit.

References

Kosmos 265 Wikipedia