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.
@article{PDA_1988_16_1_a2,
author = {S. \v{S}egan},
title = {The {Satellite} {Orbital} {Eccentricity} {Perturbations} {Under} the {Influence} of a {Drag}},
journal = {Publications of the Department of Astronomy},
pages = {23 - 30},
publisher = {mathdoc},
volume = {16},
number = {1},
year = {1988},
url = {http://geodesic.mathdoc.fr/item/PDA_1988_16_1_a2/}
}
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/