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Second-order secular perturbations in the motion of a remote satellite

V.P. Dolgachev

Moscow University Physics Bulletin 1970. 25. N 3. P. 57

  • Article
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.

Authors
V.P. Dolgachev
Department of Stellar Mechanics and Gravimetry
Issue 3, 1970

Moscow University Physics Bulletin

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