Mission type | Weather |
---|---|
Operator | Roscosmos/Roshydromet |
COSPAR ID | 2009-049A |
SATCAT no. | 35865 |
Mission duration | Planned: 5 years[1] Actual: 5 years, 2 months[2] |
Spacecraft properties | |
Manufacturer | VNIIEM |
Launch mass | 2,930 kilograms (6,460 lb)[1] |
Payload mass | 700 kilograms (1,500 lb)[1] |
Power | 1400 watts[1] |
Start of mission | |
Launch date | 17 September 2009 15:55:07 | UTC
Rocket | Soyuz-2.1b/Fregat |
Launch site | Baikonur Site 31/6 |
End of mission | |
Last contact | November 2014 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-synchronous |
Perigee altitude | 827.3 kilometres (514.1 mi)[3] |
Apogee altitude | 823.8 kilometres (511.9 mi)[3] |
Inclination | 98.5 degrees[3] |
Period | 101.3 minutes[3] |
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,[4] 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.[2]
Since its termination, the satellite has been heard on radio by amateur radio operators, even transmitting pictures of the Earth.[5]