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Orbit accuracy assessment for SeasatLaser range measurements are used to determine the orbit of Seasat during the period from July 28, 1978, to Aug. 14, 1978, and the influence of the gravity field, atmospheric drag, and solar radiation pressure on the orbit accuracy is investigated. It is noted that for the orbits of three-day duration, little distinction can be made between the influence of different atmospheric models. It is found that the special Seasat gravity field PGS-S3 is most consistent with the data for three-day orbits, but an unmodeled systematic effect in radiation pressure is noted. For orbits of 18-day duration, little distinction can be made between the results derived from the PGS gravity fields. It is also found that the geomagnetic field is an influential factor in the atmospheric modeling during this time period. Seasat altimeter measurements are used to determine the accuracy of the altimeter measurement time tag and to evaluate the orbital accuracy.
Document ID
19810040393
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Schutz, B. E.
(Texas Univ. Austin, TX, United States)
Tapley, B. D.
(Texas, University Austin, Tex., United States)
Date Acquired
August 11, 2013
Publication Date
December 1, 1980
Publication Information
Publication: Journal of the Astronautical Sciences
Volume: 28
Subject Category
Astrodynamics
Accession Number
81A24797
Funding Number(s)
CONTRACT_GRANT: NOAA-MO-A01-78-00-4325
CONTRACT_GRANT: JPL-954703
Distribution Limits
Public
Copyright
Other

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