Abstract
The motion of artificial satellites in the gravitational field of an oblate body is discussed in the parametrized-post-Newtonian (PPN) framework with parameters β and γ. Analytical expressions for first order post-Newtonian short periodic, long periodic and secular perturbations of orbital elements are given.
| Original language | English |
|---|---|
| Pages (from-to) | 81-89 |
| Number of pages | 9 |
| Journal | Celestial Mechanics |
| Volume | 42 |
| Issue number | 1-4 |
| DOIs | |
| State | Published - Mar 1987 |
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