Mission type | ABM radar target |
---|---|
COSPAR ID | 1970-004A |
SATCAT no. | 04299 |
Spacecraft properties | |
Spacecraft type | DS-P1-Yu |
Manufacturer | Yuzhnoye |
Launch mass | 250 kilograms (550 lb) |
Start of mission | |
Launch date | 15 January 1970, 13:39:59 | UTC
Rocket | Kosmos-2I 63SM |
Launch site | Plesetsk 133/1 |
End of mission | |
Decay date | 1 July 1970 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 196 kilometres (122 mi) |
Apogee altitude | 1,371 kilometres (852 mi) |
Inclination | 81.9 degrees |
Period | 100.5 minutes |
Kosmos 319 ( Russian: Космос 319 meaning Cosmos 319), known before launch as DS-P1-Yu No.25, was a Soviet satellite which was launched in 1970 as part of the Dnepropetrovsk Sputnik programme. It was a 250-kilogram (550 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used as a radar calibration target for anti-ballistic missile tests. [1]
Kosmos 319 was launched from Site 133/1 at the Plesetsk Cosmodrome, [2] atop a Kosmos-2I 63SM carrier rocket. The launch occurred on 15 January 1970 at 13:39:59 UTC, and resulted in the successful deployment of Kosmos 319 into low Earth orbit. [3] Upon reaching orbit, it was assigned its Kosmos designation, and received the International Designator 1970-004A.
Kosmos 319 was operated in an orbit with a perigee of 196 kilometres (122 mi), an apogee of 1,371 kilometres (852 mi), 81.9 degrees of inclination, and an orbital period of 100.5 minutes. [1] [4] It remained in orbit until it decayed and reentered the atmosphere on 1 July 1970. [4] It was the twenty-ninth of seventy nine DS-P1-Yu satellites to be launched, [1] and the twenty-seventh of seventy two to successfully reach orbit. [5]
Mission type | ABM radar target |
---|---|
COSPAR ID | 1970-004A |
SATCAT no. | 04299 |
Spacecraft properties | |
Spacecraft type | DS-P1-Yu |
Manufacturer | Yuzhnoye |
Launch mass | 250 kilograms (550 lb) |
Start of mission | |
Launch date | 15 January 1970, 13:39:59 | UTC
Rocket | Kosmos-2I 63SM |
Launch site | Plesetsk 133/1 |
End of mission | |
Decay date | 1 July 1970 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 196 kilometres (122 mi) |
Apogee altitude | 1,371 kilometres (852 mi) |
Inclination | 81.9 degrees |
Period | 100.5 minutes |
Kosmos 319 ( Russian: Космос 319 meaning Cosmos 319), known before launch as DS-P1-Yu No.25, was a Soviet satellite which was launched in 1970 as part of the Dnepropetrovsk Sputnik programme. It was a 250-kilogram (550 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used as a radar calibration target for anti-ballistic missile tests. [1]
Kosmos 319 was launched from Site 133/1 at the Plesetsk Cosmodrome, [2] atop a Kosmos-2I 63SM carrier rocket. The launch occurred on 15 January 1970 at 13:39:59 UTC, and resulted in the successful deployment of Kosmos 319 into low Earth orbit. [3] Upon reaching orbit, it was assigned its Kosmos designation, and received the International Designator 1970-004A.
Kosmos 319 was operated in an orbit with a perigee of 196 kilometres (122 mi), an apogee of 1,371 kilometres (852 mi), 81.9 degrees of inclination, and an orbital period of 100.5 minutes. [1] [4] It remained in orbit until it decayed and reentered the atmosphere on 1 July 1970. [4] It was the twenty-ninth of seventy nine DS-P1-Yu satellites to be launched, [1] and the twenty-seventh of seventy two to successfully reach orbit. [5]