On the equinoctial orbit elements
- 1 May 1972
- journal article
- Published by Springer Nature in Celestial Mechanics and Dynamical Astronomy
- Vol. 5 (3) , 303-310
- https://doi.org/10.1007/bf01228432
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- The main problem of artificial satellite theory for small and moderate eccentricitiesCelestial Mechanics and Dynamical Astronomy, 1970
- Orbit determination using analytic partial derivatives of perturbed motionAIAA Journal, 1970
- Perturbations in rectangular coordinates by iterationCelestial Mechanics and Dynamical Astronomy, 1969
- Completely general closed-form solution for coordinates and partial derivative of the two-body problemThe Astronomical Journal, 1965