Kosmos 369
| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1970-081A |
| SATCAT no. | 04573 |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 325 kilograms (717 lb) |
| Start of mission | |
| Launch date | 8 October 1970, 15:10:03 UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk 133/1 |
| End of mission | |
| Decay date | 22 January 1971 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 256 kilometres (159 mi) |
| Apogee altitude | 454 kilometres (282 mi) |
| Inclination | 70.9 degrees |
| Period | 91.6 minutes |
Kosmos 369 (Russian: Космос 369 meaning Cosmos 369), known before launch as DS-P1-Yu No.42, was a Soviet satellite which was launched in 1970 as part of the Dnepropetrovsk Sputnik programme. It was a 325-kilogram (717 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and was used as a radar calibration target for anti-ballistic missile tests.