From order to chaos in Earth satellite orbits
Ioannis Gkolias, Jerome Daquin, Fabien Gachet, Aaron J. Rosengren

TL;DR
This paper investigates the long-term dynamical behavior of Earth satellite orbits in MEO and GEO, revealing a transition from order to chaos influenced by secular resonances and inclination, with implications for space debris management.
Contribution
It applies a Hamiltonian model and chaos indicators to characterize the transition to chaos in satellite orbits, especially near secular resonances, using a novel statistical approach with FLI maps.
Findings
Transition from order to chaos near critical inclinations
Highly inclined GEO orbits are particularly unstable
Rich dynamical behaviors observed in satellite orbits
Abstract
We consider Earth satellite orbits in the range of semi-major axes where the perturbing effects of Earth's oblateness and lunisolar gravity are of comparable order. This range covers the medium-Earth orbits (MEO) of the Global Navigation Satellite Systems and the geosynchronous orbits (GEO) of the communication satellites. We recall a secular and quadrupolar model, based on the Milankovitch vector formulation of perturbation theory, which governs the long-term orbital evolution subject to the predominant gravitational interactions. We study the global dynamics of this two-and-a-half degrees-of-freedom Hamiltonian system by means of the fast Lyapunov indicator (FLI), used in a statistical sense. Specifically, we characterize the degree of chaoticity of the action space using angle-averaged normalized FLI maps, thereby overcoming the angle dependencies of the conventional stability maps.…
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