Annotation
The differential equations for the elements of an intermediate orbit are integrated on the basis of the solution of the generalized problem of two fixed centers. The right side of these equations contain the components of the perturbing acceleration caused by atmospheric drag. Equations are derived for the perturbations in the orbital elements with the atmospheric drag.
© 2016 Publisher M.V.Lomonosov Moscow State University
Authors
B.N. Noskov
P.K. Shternberg State Astronomical Institute
P.K. Shternberg State Astronomical Institute
Science News of the Faculty of Physics, Lomonosov Moscow State University
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