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GRACE - Gravity Recovery And Climate Experiment



GRACE Satelliten, Artist View

The GRACE mission is a joint German-American project. The primary objective of the GRACE mission is to obtain accurate global models for the mean and time variable components of the earth´s gravity field. This goal will be achieved by measurements of the inter-satellite range between 2 co-planar, low altitude near-polar orbiting satellites. In addition, each satellite carries a high accuracy accelerometer and a geodetic qualified GPS receiver to perform precise orbit determination, recover gravity data and to estimate the gravity field. The secondary task of the GRACE mission is to keep a daily record of several hundred globally distributed profiles of the delay or inclination angle of GPS measurements. Both can be converted into a total electron or refractivity by applying Atmospheric- and Ionospheric-Profiling. The German Space Operations Center configured the Ground Operations System and prepared and executed the GRACE mission operations.

Launch Date: 17 March 2002
Orbit Altitude: 450-500 km
Orbit Inclination 89°
Mass: 2x 487 kg
Length: 2x 3.1 m
Launch Site: Plesetsk, Russia
Launcher: Rockot
Mission Lifetime: 5 years (planned)
Control Center: DLR / GSOC
Ground Stations: Weilheim, Neustrelitz

Further information about GRACE can be found on the homepage of the University of Texas at Austin


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