Satellite motion in a non-singular gravitational potential
Ioannis Haranas, Spiros Pagiatakis

TL;DR
This paper investigates how a non singular gravitational potential affects satellite orbits by deriving orbital element changes and evaluating their magnitudes, finding effects too small for current detection capabilities.
Contribution
It introduces a second-order expansion of a non singular potential and analyzes its impact on satellite orbital elements using the Lagrange planetary equations.
Findings
Secular effects on perigee and mean anomaly are extremely small.
Low and high frequency effects are negligible for current observational technology.
The study provides a framework for assessing non singular gravitational influences on satellites.
Abstract
We study the effects of a non singular gravitational potential on satellite orbits by deriving the corresponding time rates of change of its orbital elements. This is achieved by expanding the non singular potential into power series up to second order. This series contains three terms, the first being the Newtonian potential and the other two, (first order term)and (second order term), express deviations of the singular potential from the Newtonian. These deviations from the Newtonian potential are taken as disturbing potential terms in the Lagrange planetary equations that provide the time rates of change of the orbital elements of a satellite in a non singular gravitational field. We split these effects into secular, low and high frequency components and we evaluate them numerically using the low Earth orbiting mission Gravity Recovery and Climate Experiment (GRACE). We show that the…
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Taxonomy
TopicsGeophysics and Gravity Measurements · Cosmology and Gravitation Theories · Pulsars and Gravitational Waves Research
