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Meteor-M No.1

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2009 Russian weather satellite
Meteor-M No.1
Mission typeWeather
OperatorRoscosmos/Roshydromet
COSPAR ID2009-049A Edit this at Wikidata
SATCAT no.35865
Mission durationPlanned: 5 years
Actual: 5 years, 2 months
Spacecraft properties
ManufacturerVNIIEM
Launch mass2,930 kilograms (6,460 lb)
Payload mass700 kilograms (1,500 lb)
Power1400 watts
Start of mission
Launch date17 September 2009 15:55:07 (2009-09-17UTC15:55:07Z) UTC
RocketSoyuz-2.1b/Fregat
Launch siteBaikonur Site 31/6
End of mission
Last contactNovember 2014 (2014-12)
Orbital parameters
Reference systemGeocentric
RegimeSun-synchronous
Perigee altitude827.3 kilometres (514.1 mi)
Apogee altitude823.8 kilometres (511.9 mi)
Inclination98.5 degrees
Period101.3 minutes
Meteor← Meteor-3M No.1Meteor-M No.2 →

Meteor-M No.1 was the first of the Russian Meteor-M series of polar-orbiting weather satellites. It was launched on a Soyuz-2.1b rocket with a Fregat upper stage on 17 September 2009. Meteor-M No.1 was the designated replacement for Meteor-3M No.1, and had a design life of 5 years. In November 2014, Russian officials announced the termination of the mission after a failure of the onboard attitude control system.

Since its termination, the satellite has been heard on radio by amateur radio operators, even transmitting pictures of the Earth.

See also

References

  1. ^ Administrator. "Основные характеристики КА "Метеор-М" №1". www.vniiem.ru. Retrieved 2016-04-03.
  2. ^ Zak, Anatoly (4 July 2019). "Russia begins rebuilding its weather satellite network with Meteor M1". RussianSpaceWeb. Retrieved 24 March 2021.
  3. ^ "Technical details for satellite METEOR-M". N2YO.com - Real Time Satellite Tracking and Predictions. Retrieved 2016-04-03.
  4. Clark, Stephen (17 September 2009). "Soyuz rocket launches Russian weather satellite". Spaceflight Now. Retrieved 24 March 2021.
  5. "Meteor M-N1 Satellite Wakes up from the Dead". RTL-SDR.com. November 9, 2015. Retrieved 2024-02-02.
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