Initial Parameter Analysis about Resonant Orbits in Earth-Moon System

Table 2

Simulation results for 1:2 resonant orbits when the initial parameters define the closest distance as and temporary Kepler energy H₂ 0.

Initial Phase	Eccentricity e	Closest Distances r1	Kepler Energy H2	Simulation Results
5°	0.26	0.1908	-0.0636	Resonance transition
	0.485	0.1715	-0.0033	Resonance transition
10°	0.26	0.2303	-0.0489	Resonance transition
	0.32	0.1961	-0.0587	Resonance transition
15°	0.36	0.2210	-0.0360	Resonance transition
	0.38	0.1821	-0.0325	Resonance transition
20°	0.41	0.2033	-0.0111	Resonance transition