|Mission type||ABM radar target|
|Launch mass||250 kilograms (550 lb)|
|Start of mission|
|Launch date||12 September 1967, 17:00UTC|
|Launch site||Plesetsk 133/1|
|End of mission|
|Decay date||3 March 1968|
|Perigee||193 kilometres (120 mi)|
|Apogee||1,395 kilometres (867 mi)|
Kosmos 176 (Russian: Космос 176 meaning Cosmos 176), also known as DS-P1-Yu No.10 was a Soviet satellite which was used as a radar calibration target for tests of anti-ballistic missiles. It was built by the Yuzhnoye Design Bureau, and launched in 1967 as part of the Dnepropetrovsk Sputnik programme.
A Kosmos-2I 63SM carrier rocket was used to launch Kosmos 176 from Site 133/1 at Plesetsk Cosmodrome. The launch occurred at 17:00 UTC on 12 September 1967, and resulted in Kosmos 176's successful deployment into Low earth orbit.
Kosmos 176 was operated in an orbit with a perigee of 193 kilometres (120 mi), an apogee of 1,395 kilometres (867 mi), 81.9 degrees of inclination, and an orbital period of 100.74 minutes. It remained in orbit until it decayed and reentered the atmosphere on 3 March 1968. It was the tenth of seventy nine DS-P1-Yu satellites to be launched, and the ninth of seventy two to successfully reach orbit.
- Wade, Mark. "DS-P1-Yu". Encyclopedia Astronautica. Retrieved 9 August 2009.
- McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 August 2009.
- Wade, Mark. "Kosmos 2". Encyclopedia Astronautica. Retrieved 9 August 2009.
- McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 9 August 2009.
- Krebs, Gunter. "DS-P1-Yu (11F618)". Gunter's Space Page. Retrieved 9 August 2009.
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