A simple intermediary orbit for the J{2} problem

Details A simple intermediary orbit for the J{2} problem A simple intermediary orbit for the J{2} problem

Jul 2005

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2005a%26a...437..333o&link_type=abstract

Astronomy and Astrophysics, Volume 437, Issue 1, July I 2005, pp.333-338

Astronomy and Astrophysics

Astrophysics

Planets And Satellites: General, Celestial Mechanics

Scientific paper

A simple precessing ellipse suitable for satellites with moderate
eccentricities and inclinations is built in the Hamiltonian context of
the J2 problem. Easy to use as a first intermediary orbit, it
provides a substantially closer starting point for series expansions
than the regular Keplerian ellipse.

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