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Using Anomalous Along-Track Forces for Topex/Poseidon Ground Track Control

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dc.contributor.author Shapiro, B. en_US
dc.contributor.author Bhat, R. en_US
dc.contributor.author Frauenholz, R. en_US
dc.date.accessioned 2004-10-06T05:41:33Z
dc.date.available 2004-10-06T05:41:33Z
dc.date.issued 1993-02 en_US
dc.identifier.citation Cocoa Beach, Florida, USA en_US
dc.identifier.clearanceno 93-1789 en_US
dc.identifier.uri http://hdl.handle.net/2014/36056
dc.description.abstract The TOPES/POSEIDON satellite is maintained in a nearly circular, frozen orbit at an altitude of =1336 km. and an inclination of i = 66.4, which provides an exact repeat ground track every 127 revolutions and overflies two altimetry verifications sites. en_US
dc.format.extent 1051403 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other luni-solar gravity solar array curling thermal imbalances radiative forces outgassing en_US
dc.title Using Anomalous Along-Track Forces for Topex/Poseidon Ground Track Control en_US


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