The Short-Period Drag Perturbations of the Orbits of Artificial Satellites

Statistics – Computation

Scientific paper

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Scientific paper

The aim of this paper is the computation of short-period perturbations of the elements of the orbits of artificial satellites, caused by atmospheric drag. The density function of the earth's atmosphere includes the effect of the atmospheric bulge, described by a formula given by Jacchia. The method of the solution is in essence the method of construction of the disturbing function on an electronic computer; the formulas needed for such computations and some numerical results are given.

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