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 Progress M-MIM2 and Poisk as seen by Expedition 21. | |
| Mission type | ISS assembly |
|---|---|
| Operator | Roskosmos |
| COSPAR ID | 2009-060A |
| SATCAT no. | 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[1] |
| 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 altitude | 336 kilometres (209 mi) |
| Apogee altitude | 344 kilometres (214 mi) |
| Inclination | 51.6 degrees |
| Period | 91.33 minutes |
| Epoch | November 18, 2009[2] |
| 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 ISS assembly | |
Progress M-MIM2 (Russian: Прогресс М-МИМ2), or Progress M-MRM2, originally designated Progress M-SO2,[3] was a modified Progress-M 11F615A55, Russian production No. 302, which was used to deliver the Poisk module to the International Space Station.[4] It has the pressurised cargo module removed to accommodate Poisk.[3] It was similar to the Progress M-SO1 spacecraft which was used to deliver the Pirs module to the station in 2001.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 22 January 2014.
- ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 22 January 2014.
- ^ a b McDowell, Jonathan. "Issue 618". Jonathan's Space Report. Jonathan's Space Page. Retrieved 2009-11-13.
- ^ "Russia Launches Scientific Module To ISS". Space-Travel.com. 2009-11-10. Retrieved 2009-11-13.