Kosmos 163 (Russian: Космос 163 meaning Cosmos 163), also known as DS-U2-MP No.2, was a Sovietsatellite which was launched in 1967 as part of the Dnepropetrovsk Sputnik programme. It was a 357 kilograms (787 lb) spacecraft, which was built by the Yuzhnoye Design Office, and was used to investigate micrometeoroids and cosmic dust particles in near-Earth space.[3]
Kosmos 163 was the second of two DS-U2-MP satellites to be launched, after Kosmos 135.[5][6] It was operated in an orbit with a perigee of 244 kilometres (152 mi), an apogee of 611 kilometres (380 mi), an inclination of 48.4°, and an orbital period of 93.1 minutes.[2] It decayed from its orbit and reentered the atmosphere on 11 October 1967.[7]
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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