The Satellite Orbital Eccentricity Perturbations Under the Influence of a Drag
Publications of the Department of Astronomy, Tome 16 (1988) no. 1.

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By a procedure like that in the previous paper (Šegan, 1987) is developed a special FORTRAN program for the computation of perturbation of the satellite orbital eccentricity. Comparison with observed values is given, too.
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S. Šegan. The Satellite Orbital Eccentricity Perturbations Under the Influence of a Drag. Publications of the Department of Astronomy, Tome 16 (1988) no. 1. http://geodesic.mathdoc.fr/item/PDA_1988_16_1_a2/