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    MetOp at a glance

    MetOp MetOp launch MetOp-A satellite Level-1 products from AVHRR
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    ESA > Our Activities > Observing the Earth

    MetOp overview

    MetOp orbital path
    MetOp in polar orbit

    MetOp is Europe's first polar-orbiting satellite dedicated to operational meteorology. It represents the European contribution to a new co-operative venture with the United States providing data to monitor climate and improve weather forecasting. MetOp is a series of three satellites to be launched sequentially over 14 years, forming the space segment of EUMETSAT's Polar System (EPS).

    The first satellite, MetOp-A, was launched on 19 October 2006. MetOp-B, the second in the series, is set for launch on 19 September 2012.

    MetOp carries a set of 'heritage' instruments provided by the United States and a new generation of European instruments that offer improved remote sensing capabilities to both meteorologists and climatologists. The new instruments will augment the accuracy of temperature humidity measurements, readings of wind speed and direction, and atmospheric ozone profiles.

    MetOp flies in a polar orbit corresponding to local 'morning' while the US will be responsible for 'afternoon' coverage. The series will provide data for both operational meteorology and climate studies. The combination of instruments on board MetOp has remote sensing capabilities to observe the Earth by day and night as well as under cloudy conditions.

    Dimensions 6.2 x 3.4 x 3.4 metres (under the launcher fairing)
    17.6 x 6.5 x 5.2 metres (deployed in orbit)
    Orbit Sun-synchronous orbit
    09.30 mean local solar time (Equator crossing, descending node)
    Inclination 98.7 degrees to the Equator
    Time for one orbit 101 minutes
    Repeat cycle 29 days
    Mean altitude Approximately 817 km
    Mass 4093 Kg
    Payload mass 931 Kg
    Power 1812 W average power consumption (end-of-life)
    Launch MetOp-A: 19 October 2006
    MetOp-B: 19 September 2012
    from Baikonur Space Centre in Kazakhstan
    Launch vehicle Soyuz-ST Fregat
    Mission duration Six months of commissioning followed by 4.5 years operational mission

    Last update: 6 August 2012

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