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Mean elements of GEOS-1 and GEOS-2A combined analytical-numerical procedure for determining precise mean orbital elements is presented and applied to the orbits of GEOS-1 and GEOS-2. The precision of the mean semi-major axes of these orbits is a few tens of centimeters when optical flash data is used to determine two-day orbital arcs. Four-day Minitrack orbits give mean semi-major axes of a few meters precision. The mean orientation parameters are obtained to a precision of about 0.1 sec (about 3m) or better from the optical orbits. This precision is adequate for determinations of tidal parameters, particularly in the case of GEOS-2, where the tidal perturbation of the inclination is 10 sec.
Document ID
19720016240
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Douglas, B. C.
(Wolf Res. and Develop. Corp. Riverdale, Md., United States)
Marsh, J. G.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Mullins, N. E.
(Wolf Res. and Develop. Corp. Riverdale, Md., United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-65870
X-553-72-85
Report Number: NASA-TM-X-65870
Report Number: X-553-72-85
Accession Number
72N23890
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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