| Mission type | ABM radar target |
|---|---|
| COSPAR ID | 1969-020A  |
| SATCAT no. | 03773 |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 250 kilograms (550 lb) |
| Start of mission | |
| Launch date | 5 March 1969, 13:04:55 (1969-03-05UTC13:04:55Z) UTC |
| Rocket | Kosmos-2I 63SM |
| Launch site | Kapustin Yar 86/4 |
| End of mission | |
| Decay date | 9 May 1970 (1970-05-10) |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 212 kilometres (132 mi) |
| Apogee altitude | 2,063 kilometres (1,282 mi) |
| Inclination | 48.4 degrees |
| Period | 108 minutes |
Kosmos 268 (Russian: Космос 268 meaning Cosmos 268), known before launch as DS-P1-Yu No.18, was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles. It was a 250-kilogram (550 lb) spacecraft, which was built by the Yuzhnoye Design Bureau, and launched in 1969 as part of the Dnepropetrovsk Sputnik programme.[1]
Kosmos 268 was launched from Site 86/4atKapustin Yar,[2] atop a Kosmos-2I 63SM carrier rocket. The launch occurred on 5 March 1969 at 13:04:55 UTC, and resulted in Kosmos 268's successful deployment into low Earth orbit.[3] Upon reaching orbit, it was assigned its Kosmos designation, and received the International Designator 1969-020A.
Kosmos 268 was operated in an orbit with a perigee of 212 kilometres (132 mi), an apogee of 2,063 kilometres (1,282 mi), 48.4 degrees of inclination, and an orbital period of 108 minutes.[1][4] It remained in orbit until it decayed and reentered the atmosphere on 9 May 1970.[4] It was the nineteenth of seventy nine DS-P1-Yu satellites to be launched,[1] and the eighteenth of seventy two to successfully reach orbit.[5]
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Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |
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