The calculation of orbital positioning using standard orbital parameters.

Details The calculation of orbital positioning using standard orbital parameters. The calculation of orbital positioning using standard orbital parameters.

Aug 1999

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1999ijsc...17..303p&link_type=abstract

International Journa l of Satell. Commun. (UK), Vol. 17, No. 4, p. 303 - 304

Other

Orbit Theory: Celestial Mechanics, Orbit Theory: Artificial Satellites

Scientific paper

Practical difficulties arise solving the deceptively simple Kepler's equation. Kepler's equation can be solved easily using the method Newton developed for doing so. The authors recommend that this method be used in any general approach to orbital calculations. Another practical point to be reckoned with, is the variation in true orbital parameters. It is important to note that inclined orbits, eccentric orbits, and low orbits all suffer from rapid changes in their parameters. They can be ignored only for simple calculations for just a few orbits. Any calculation covering a longer period of time must take these changes into account.

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