Annotation
Equations are derived for the second-order secular perturbations in the orbital elements for remote earth satellites under the condition that the perturbing function contains terms of third degree in the Lagrange variables.
© 2016 Publisher M.V.Lomonosov Moscow State University
Authors
V.P. Dolgachev
Department of Stellar Mechanics and Gravimetry
Department of Stellar Mechanics and Gravimetry
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