A high-fidelity satellite ephemeris program for Earth satellites in eccentric orbits

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Computer Programming, Computer Programs, Eccentric Orbits, Ephemerides, Program Verification (Computers), Celestial Mechanics, Ephemeris Time, Fortran, Nasa Programs, Project Planning, University Program

Scientific paper

A program for mission planning called the Analytic Satellite Ephemeris Program (ASEP), produces projected data for orbits that remain fairly close to the Earth. ASEP does not take into account lunar and solar perturbations. These perturbations are accounted for in another program called GRAVE, which incorporates more flexible means of input for initial data, provides additional kinds of output information, and makes use of structural programming techniques to make the program more understandable and reliable. GRAVE was revised, and a new program called ORBIT was developed. It is divided into three major phases: initialization, integration, and output. Results of the program development are presented.

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