Planetary Satellite Orbiters: Applications for the Moon

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<g transform="translate(72,-66.25)">
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<tspan style="font-size: 12.50px; " x="0" y="0">𝑒</tspan>
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</svg> versus <svg height="9.9375" id="M303" style="vertical-align:-2.34499pt" version="1.1" viewbox="0 0 8.4375 9.9375" width="8.4375" xmlns="http://www.w3.org/2000/svg">
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<tspan style="font-size: 12.50px; " x="0" y="0">𝑔</tspan>
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</svg>-degree. Model LP165P. Initial conditions: <svg height="11.0375" id="M304" style="vertical-align:-0.27588pt" version="1.1" viewbox="0 0 40 11.0375" width="40" xmlns="http://www.w3.org/2000/svg">
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<tspan style="font-size: 12.50px; " x="28.031727" y="0">8</tspan>
<tspan style="font-size: 12.50px; " x="34.283226" y="0">6</tspan>
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</svg> km. Perturbations: <svg height="14.2375" id="M306" style="vertical-align:-3.13504pt" version="1.1" viewbox="0 0 14.6625 14.2375" width="14.6625" xmlns="http://www.w3.org/2000/svg">
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<tspan style="font-size: 12.50px; " x="0" y="0">𝐽</tspan>
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<tspan style="font-size: 12.50px; " x="0" y="0">𝐽</tspan>
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Mathematical Problems in Engineering

Planetary Satellite Orbiters: Applications for the Moon

Figure 11