| Progress M-MIM2 | |
| Mission Type: | ISS assembly |
| Operator: | Roskosmos |
| Cospar Id: | 2009-060A |
| Satcat: | 36086 |
| Spacecraft Type: | Progress-M (modified) |
| Manufacturer: | RKK Energia |
| Launch Mass: | 7102kg (15,657lb) |
| Launch Date: | UTC[1] |
| Launch Rocket: | Soyuz-U |
| Launch Site: | Baikonur Site 1/5 |
| Disposal Type: | Deorbited |
| Decay Date: | UTC |
| Orbit Epoch: | November 18, 2009[2] |
| Orbit Reference: | Geocentric |
| Orbit Regime: | Low Earth |
| Orbit Periapsis: | 336km (209miles) |
| Orbit Apoapsis: | 344km (214miles) |
| Orbit Inclination: | 51.6 degrees |
| Orbit Period: | 91.33 minutes |
| Apsis: | gee |
| Docking: | |
| Payload Items: | Poisk |
| Cargo Mass: | 3670kg (8,090lb) |
| Programme: | Progress ISS assembly |
| Previous Mission: | Progress M-03M |
| Next Mission: | Progress M-04M |
Progress M-MIM2 (Russian: Прогресс М-МИМ2), or Progress M-MRM2, originally designated Progress M-SO2, was a modified Progress-M 11F615A55, Russian production No. 302, which was used to deliver the Poisk module to the International Space Station.[3] It has the pressurised cargo module removed to accommodate Poisk.[4] 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.[3] At launch, Progress M-MIM2 had a total mass of, including the 3670kg (8,090lb) Poisk module.[4] [5]
The spacecraft docked with the zenith port of the International Space Station's Zvezda module on 12 November. Capture occurred at 15:41 GMT,[6] and initial docking was completed successfully at 15:44.[7]
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.[8]