Note on Expressions for Second-Order Short-Periodic Perturbations

Physics

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Scientific paper

Expressions for second-order short-periodic perturbations for satellite motion are derived by assuming that J4 = 1.4 J22. The expressions consist of terms for which amplitudes are larger than 10-7 when the parameter of the ellipse is equal to the equatorial radius of the earth and the eccentricity is 0.15. The expressions for the J3 term are also given.

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