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Determining Precise Orbits for TOPEX/POSEIDON Within One Day of Real Time: Results and Implications

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dc.contributor.author Haines, B. en_US
dc.contributor.author Lichten, S. en_US
dc.contributor.author Lough, M. en_US
dc.contributor.author Muellerschoen, R. en_US
dc.contributor.author Vigue-Rodi, Y. en_US
dc.date.accessioned 2004-09-23T22:58:24Z
dc.date.available 2004-09-23T22:58:24Z
dc.date.issued 1999-02-07 en_US
dc.identifier.citation Space Flight Mechanics - AAS/AIAA en_US
dc.identifier.citation Breckenridge, CO, USA en_US
dc.identifier.clearanceno 99-0199 en_US
dc.identifier.uri http://hdl.handle.net/2014/16796
dc.description.abstract Radar altimeter missions require precise estimates of the satellite radial orbit position in order to support measurement of surface heights. en_US
dc.format.extent 973215 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other TOPEX/POSEIDON GPS Precise Orbit Determination en_US
dc.title Determining Precise Orbits for TOPEX/POSEIDON Within One Day of Real Time: Results and Implications en_US


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