Anjali Rawat, Bhanu Kumar, Aaron J. Rosengren, Shane D. Ross
Lunar mean-motion resonances (MMRs) significantly shape cislunar dynamics beyond geosynchronous orbit, forming stable/unstable orbit pairs with corresponding intermingled chaotic and regular regions. The resonance zone is rigorously defined using the separatrices of unstable resonant periodic orbits surrounding stable quasi-periodic regions. Our study leverages the planar circular restricted three-body problem to estimate the (stable) resonance widths and (unstable) chaotic resonance zones of influence of the 2:1 and 3:1 MMRs across various Jacobi constants, employing a Poincaré map at perigee and presenting findings in easily interpretable geocentric orbital elements. An analysis of the semi-major axis versus eccentricity plane reveals broader regions of resonance influence than those predicted by semi-analytical models based on the perturbed Kepler problem. A comparison with high-fidelity three-dimensional ephemeris propagation of several spacecraft (TESS, IBEX, and Spektr-R) in these regions is made, which shows good agreement with the simplified circular restricted three-body problem model.