Research Article

Planetary Satellite Orbiters: Applications for the Moon

Figure 9

𝑒 versus 𝑔 -degree. Model LP165P. Initial conditions: 𝑖 = 9 0 °, 𝑎 = 1 8 6 1  km. Perturbations: 𝐽 2 𝐽 5 , 𝐽 7 , and 𝐶 2 2 .
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