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NASA NTRS · 20060039506

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

Shapiro, B.·Bhat, R.·Frauenholz, R.
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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.

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Shapiro, B., Bhat, R., Frauenholz, R.. 1993-02-01. Using Anomalous Along-Track Forces for Topex/Poseidon Ground Track Control. https://ntrs.nasa.gov/citations/20060039506

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