Kosmos 919

Kosmos 919

Mission type	ABM radar target
COSPAR ID	1977-051A
Spacecraft properties
Spacecraft type	DS-P1-I
Manufacturer	Yuzhnoye
Launch mass	400 kilograms (880 lb)
Start of mission
Launch date	18 June 1977, 10:30 UTC
Rocket	Kosmos-2I 63SM
Launch site	Plesetsk 133/1
End of mission
Decay date	28 August 1978
Orbital parameters
Reference system	Geocentric
Regime	Low Earth
Perigee	269 kilometres (167 mi)
Apogee	822 kilometres (511 mi)
Inclination	71 degrees
Period	95.6 minutes

Kosmos 919 (Russian: Космос 919 meaning Cosmos 919), also known as DS-P1-I No.19 was a satellite which was used as a radar target for anti-ballistic missile tests. It was launched by the Soviet Union in 1977 as part of the Dnepropetrovsk Sputnik programme.^[1]

It was launched aboard a Kosmos-2I 63SM rocket,^[2] from Site 133/1 at Plesetsk. The launch occurred at 10:30 UTC on 18 June 1977.^[3] It was the final flight of the Kosmos-2I carrier rocket, and the final flight of an R-12 family rocket. Kosmos launches continued using the R-14-derived Kosmos-3M. It also marked the last launch from Plesetsk Site 133/1 until it was rebuilt as Site 133/3 in 1985.

Kosmos 919 was placed into a low Earth orbit with a perigee of 269 kilometres (167 mi), an apogee of 822 kilometres (511 mi), 71 degrees of inclination, and an orbital period of 95.6 minutes.^[1] It decayed from orbit on 28 August 1978.^[4]

Kosmos 919 was the last of nineteen DS-P1-I satellites to be launched.^[1] Of these, all reached orbit successfully except the seventh.^[5]

See also

• 1977 in spaceflight

References

1. Wade, Mark. "DS-P1-I". Encyclopedia Astronautica. Retrieved 28 May 2009.
2. McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 28 May 2009.
3. Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Retrieved 28 May 2009.
4. McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 28 May 2009.
5. Wade, Mark. "DS". Encyclopedia Astronautica. Retrieved 28 May 2009.