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Anticipated orbital perturbations of satellite 1959 delta twoNumerical integration of equations of motion for Explorer VI satellite - lunar, solar, oblateness, and atmospheric drag perturbations
Document ID
19650012365
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Kozai, Y. (Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Whitney, C. A. (Smithsonian Astrophysical Observatory Cambridge, MA, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Space Sciences
Accession Number
65N21966
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NUMERICAL INTEGRATION
ORBIT PERTURBATION
EXPLORER VI SATELLITE
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