Kosmos 6
| Mission type | ABM radar target Technology |
|---|---|
| Harvard designation | 1962 Alpha Delta 1 |
| COSPAR ID | 1962-028A |
| SATCAT no. | 00338 |
| Mission duration | 39 days |
| Spacecraft properties | |
| Spacecraft type | DS-P1 |
| Manufacturer | Yuzhnoye |
| Launch mass | 355 kg |
| Start of mission | |
| Launch date | 30 June 1962, 16:00:00 GMT |
| Rocket | Kosmos-2I 63S1 |
| Launch site | Kapustin Yar, Mayak-2 |
| Contractor | Yuzhnoye |
| End of mission | |
| Decay date | 8 August 1962 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 264 km |
| Apogee altitude | 344 km |
| Inclination | 49.0° |
| Period | 90.6 minutes |
| Epoch | 30 June 1962 |
Kosmos 6 (Russian: Космос 6 meaning Cosmos 6), also known as DS-P1 No.1 as part of the Dnepropetrovsk Sputnik programme and occasionally in the West as Sputnik 16 was a prototype radar target satellite for anti-ballistic missile tests, which was launched by the Soviet Union in 1962.