| Mission type | ABM Radar target |
|---|---|
| COSPAR ID | 1967-028A  |
| SATCAT no. | 02722 |
| Mission duration | 133 days |
| Spacecraft properties | |
| Spacecraft type | DS-P1-Yu |
| Manufacturer | Yuzhnoye |
| Launch mass | 325 kg[1] |
| Start of mission | |
| Launch date | 25 March 1967, 06:57:00 GMT |
| Rocket | Kosmos-2I 63SM |
| Launch site | Plesetsk, Site 133/3 |
| Contractor | Yuzhnoye |
| End of mission | |
| Decay date | 5 August 1967 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Perigee altitude | 272 km |
| Apogee altitude | 488 km |
| Inclination | 71.0° |
| Period | 92.2 minutes |
| Epoch | 25 March 1967 |
Kosmos 152 (Russian: Космос 152 meaning Cosmos 152), also known as DS-P1-Yu No.7 was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles.[2] It was built by the Yuzhnoye Design Bureau, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme,[3] and had a mass of 325 kilograms (717 lb).[1]
Kosmos 152 was launched using a Kosmos-2I 63SM carrier rocket, which flew from Site 133/3atPlesetsk Cosmodrome.[4] The launch occurred at 06:57 GMT on 25 March 1967.[5]
Kosmos 152 separated from its carrier rocket into a low Earth orbit with a perigee of 272 kilometres (169 mi), an apogee of 488 kilometres (303 mi), an inclination of 71.0°, and an orbital period of 92.2 minutes.[6]Itdecayed from orbit on 5 August 1967.[7] Kosmos 152 was the seventh of seventy nine DS-P1-Yu satellites to be launched,[3] and the sixth of seventy two to successfully reach orbit.
This article incorporates text from this source, which is in the public domain.
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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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