In this article, we will explore Kosmos 165 from different perspectives and in various contexts. We will delve into its history, its origins, its influence on society and its relevance today. We will analyze Kosmos 165 from a multidisciplinary approach, addressing cultural, social, political, economic and scientific aspects. Through this journey, we aim to offer a comprehensive and complete vision of Kosmos 165, providing the reader with a deep and enriching understanding of this topic.
Mission type | ABM radar target |
---|---|
COSPAR ID | 1967-059A |
SATCAT no. | 02842 |
Mission duration | 217 days |
Spacecraft properties | |
Spacecraft type | DS-P1-Yu |
Manufacturer | Yuzhnoye |
Launch mass | 400 kg[1] |
Start of mission | |
Launch date | 12 June 1967, 18:06:00 GMT |
Rocket | Kosmos-2I 63SM |
Launch site | Plesetsk, Site 133/3 |
Contractor | Yuzhnoye |
End of mission | |
Decay date | 15 January 1968 |
Orbital parameters | |
Reference system | Geocentric[2] |
Regime | Low Earth |
Perigee altitude | 198 km |
Apogee altitude | 1515 km |
Inclination | 81.9° |
Period | 102.1 minutes |
Epoch | 12 June 1967 |
Kosmos 165 (Russian: Космос 165 meaning Cosmos 165), also known as DS-P1-Yu No.11 was a radar calibration target satellite which was used by the Soviet Union for tests of anti-ballistic missiles. It was a 400 kilograms (880 lb) spacecraft,[1] which was built by the Yuzhnoye Design Office, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme.[3]
Kosmos 165 was launched using a Kosmos-2I 63SM carrier rocket, which flew from Site 133/3 at Plesetsk Cosmodrome.[4] The launch occurred at 18:06:00 GMT on 12 June 1967.[5]
Kosmos 165 separated from its carrier rocket into a low Earth orbit with a perigee of 198 kilometres (123 mi), an apogee of 1,515 kilometres (941 mi), an inclination of 81.9°, and an orbital period of 102.1 minutes.[2] It decayed from orbit on 15 January 1968.[6] Kosmos 165 was the eighth of seventy nine DS-P1-Yu satellites to be launched,[3] and the seventh of seventy two to successfully reach orbit.[7]