Celestial Mechanics and Dynamical Astronomy

, Volume 113, Issue 4, pp 435–452

On the third-body perturbations of high-altitude orbits

  • Martin Lara
  • Juan F. San-Juan
  • Luis M. López
  • Paul J. Cefola
Original Article

DOI: 10.1007/s10569-012-9433-z

Cite this article as:
Lara, M., San-Juan, J.F., López, L.M. et al. Celest Mech Dyn Astr (2012) 113: 435. doi:10.1007/s10569-012-9433-z


The long-term effects of a distant third-body on a massless satellite that is orbiting an oblate body are studied for a high order expansion of the third-body disturbing function. This high order may be required, for instance, for Earth artificial satellites in the so-called MEO region. After filtering analytically the short-period angles via averaging, the evolution of the orbital elements is efficiently integrated numerically with very long step-sizes. The necessity of retaining higher orders in the expansion of the third-body disturbing function becomes apparent when recovering the short-periodic effects required in the computation of reliable osculating elements.


Third-body perturbation Lie transforms Averaging High-altitude orbits 

Copyright information

© Springer Science+Business Media B.V. 2012

Authors and Affiliations

  • Martin Lara
    • 1
  • Juan F. San-Juan
    • 2
  • Luis M. López
    • 3
  • Paul J. Cefola
    • 4
  1. 1.Columnas de Hercules 1San FernandoSpain
  2. 2.Departamento de Matemáticas y ComputaciónUniversidad de La RiojaLogroñoSpain
  3. 3.Departamento de Ingeniería MecánicaUniversidad de La RiojaLogroñoSpain
  4. 4.University at Buffalo, The State University of New YorkAmherstUSA

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