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Recent works demonstrated that the dynamics caused by the planetaryoblateness coupled with the solar radiation pressure can be described through amodel based on singly-averaged equations of motion. The coupled perturbationsaffect the evolution of the eccentricity, inclination and orientation of theorbit with respect to the Sun--Earth line. Resonant interactions lead tonon-trivial orbital evolution that can be exploited in mission design.Moreover, the dynamics in the vicinity of each resonance can be analyticallydescribed by a resonant model that provides the location of the central andhyperbolic invariant manifolds which drive the phase space evolution. Theclassical tools of the dynamical systems theory can be applied to perform apreliminary mission analysis for practical applications. On this basis, in thiswork we provide a detailed derivation of the resonant dynamics, also innon-singular variables, and discuss its properties, by studying the mainbifurcation phenomena associated to each resonance. Last, the analytical modelwill provide a simple analytical expression to obtain the area-to-mass ratiorequired for a satellite to deorbit from a given altitude in a feasibletimescale.

Dynamical taxonomy of the coupled solar radiation pressure and oblateness problem and analytical deorbiting configurations