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Improved kHz-SLR tracking techniques and orbit quality analysis for LEO missions
Authors:W Hausleitner  G Kirchner  S Krauss  J Weingrill  R Pail  H Goiginger  D Rieser
Institution:1. Austrian Academy of Sciences, Space Research Institute, 8042 Graz, Austria;2. Graz University of Technology, Institute of Navigation and Satellite Geodesy, 8010 Graz, Austria
Abstract:Satellite gravity field missions such as CHAMP, GRACE and GOCE are designed as low Earth orbiting spacecraft (LEO) with orbit heights of about 250–500 km. The challenging mission objectives require a very precise knowledge of the satellite orbit position in space. For these missions precise orbit information is typically provided by GPS satellite-to-satellite tracking (SST) observations supported by satellite laser ranging (SLR).
Keywords:Satellite laser ranging  Low earth orbit  Orbit determination
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