Physics
Scientific paper
Sep 2002
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2002cosre..40..501n&link_type=abstract
Cosmic Research, v. 40, Issue 5, p. 501-516 (2002).
Physics
Scientific paper
We consider the applied aspects of the geometrical analysis of solutions in a restricted circular double-averaged three-body problem that are concerned with the design of high-apogee satellite orbits. Based on the analysis of the long-term evolution and the ballistic lifetime for orbit families of the Prognoz satellites launched into their orbits in the period 1972-1995, we suggest some practical suggestions for choosing long-lived high-apogee orbits with taking into account various requirements for the domain of evolution of the orbital elements.
Nazirov R. R.
Prokhorenko V. I.
Sheikhet A. I.
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