2006 - ...

MetOp-A

MetOp-A

ESA and EUMETSAT jointly developed the MetOp-A satellite, which was launched in October 2006 and defines the space segment of the EUMETSAT Polar System (EPS). Two additional platforms of the MetOp series are to follow at 4-5 year intervals, thereby assuring high-quality data until at least 2020. This is also facilitated because the MetOp series satellites are equipped with almost identical instruments. Together with the NOAA-18 satellite, which circles the earth in an afternoon polar orbit—the local overflight time in the descending node is 2 pm—MetOp-A makes it possible to comprehensively monitor the weather worldwide from earth orbit.

Table: MetOp-A Mission Parameters

  
Dimensions
17.6 m × 6.7 m × 5.4 m
Total mass
4.1 t
Payload
930 kg
Number of instruments
8 (5 Europa / 3 USA)
Launcher
Soyuz-ST Fregat
Launch
19. Oktober 2006

Table: MetOp-A Orbit Parameters

  
Semi-major axis
7189 km
Orbit altitude (mean)
817 km
Inclination angle
98.7°
Orbital period
101.3 min
Orbit
polar, sun synchronous
Overflight time
09:30 am
Orbits per day
14.2
Revisit
29 days

Link

Contact

Dr. Diego Loyola

Head of Department
German Aerospace Center (DLR)
Remote Sensing Technology Institute (IMF)
Atmospheric Processors
Oberpfaffenhofen, 82234 Weßling
Tel: +49 8153 28-1367