![]() Progress M-MIM2 and Poisk as seen by Expedition 21.
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Mission type | ISS resupply |
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Operator | Roskosmos |
COSPAR ID | 2009-060A |
SATCAT № | 36086 |
Spacecraft properties | |
Spacecraft type | Progress-M (modified) |
Manufacturer | RKK Energia |
Launch mass | 7,102 kilograms (15,657 lb) |
Start of mission | |
Launch date | 10 November 2009, 14:22:04 | UTC
Rocket | Soyuz-U |
Launch site | Baikonur Site 1/5 |
End of mission | |
Disposal | Deorbited |
Decay date | 8 December 2009, 05:27 | UTC
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee | 336 kilometres (209 mi) |
Apogee | 344 kilometres (214 mi) |
Inclination | 51.6 degrees |
Period | 91.33 minutes |
Epoch | November 18, 2009 |
Docking with ISS | |
Docking port | Zvezda zenith (Poisk) |
Docking date | 12 November 2009, 15:41 UTC |
Undocking date | 8 December 2009, 00:16 UTC |
Time docked | 25 1⁄2 days |
Payload | |
Poisk | |
Mass | 3,670 kilograms (8,090 lb) |
Progress M-MIM2 (Russian: Прогресс М-МИМ2), or Progress M-MRM2, originally designated Progress M-SO2, was a modified Progress-M spacecraft which was used to deliver the Poisk module to the International Space Station. It was based on the Progress-M 11F615A55 spacecraft, with the pressurised cargo module removed to accommodate Poisk, and had the serial number 302. It was similar to the Progress M-SO1 spacecraft which was used to deliver the Pirs module to the station in 2001.
Progress M-MIM2 and Poisk were launched by a Soyuz-U carrier rocket flying from Site 1/5 at the Baikonur Cosmodrome. The launch occurred at 14:22 GMT on 10 November 2009. At launch, Progress M-MIM2 had a total mass of 7,102 kilograms (15,657 lb), including the 3,670-kilogram (8,090 lb) Poisk module.
The spacecraft docked with the zenith port of the International Space Station's Zvezda module on 12 November. Capture occurred at 15:41 GMT, and initial docking was completed successfully at 15:44. At 00:16 GMT on 8 December, Progress M-MIM2 was undocked from Poisk, and at 04:48 GMT its engines ignited to begin a 38-second deorbit burn. It reentered the atmosphere over the Pacific Ocean at 05:27, and had broken up by 05:32.