Progress M-MIM2

Progress M-MIM2
Progress M-MIM2 and Poisk as seen by Expedition 21.
Mission typeISS assembly
OperatorRoskosmos
COSPAR ID2009-060A Edit this at Wikidata
SATCAT no.36086
Spacecraft properties
Spacecraft typeProgress-M (modified)
ManufacturerRKK Energia
Launch mass7,102 kilograms (15,657 lb)
Start of mission
Launch date10 November 2009, 14:22:04 (2009-11-10UTC14:22:04Z) UTC[1]
RocketSoyuz-U
Launch siteBaikonur Site 1/5
End of mission
DisposalDeorbited
Decay date8 December 2009, 05:27 (2009-12-08UTC05:28Z) UTC
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude336 kilometres (209 mi)
Apogee altitude344 kilometres (214 mi)
Inclination51.6 degrees
Period91.33 minutes
EpochNovember 18, 2009[2]
Docking with ISS
Docking portZvezda zenith (Poisk)
Docking date12 November 2009, 15:41 UTC
Undocking date8 December 2009, 00:16 UTC
Time docked25+12 days
Payload
Poisk
Mass3,670 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.

  1. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 22 January 2014.
  2. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 22 January 2014.
  3. ^ a b McDowell, Jonathan. "Issue 618". Jonathan's Space Report. Jonathan's Space Page. Retrieved 2009-11-13.
  4. ^ "Russia Launches Scientific Module To ISS". Space-Travel.com. 2009-11-10. Retrieved 2009-11-13.