Geomagnetic Energy Approach to Space Debris Deorbiting in a Low Earth Orbit

<div>Main angular momentum accumulation (orbital coordinates) in the elliptical orbit with an inclination of 0°/90° (300 km to 950 km) under equations (<a href="https://static.hindawi.com/articles/ijae/volume-2019/5876861/figures/#EEq10">11</a>) and (<a href="https://static.hindawi.com/articles/ijae/volume-2019/5876861/figures/#EEq9">10</a>) (example 4).</div>

International Journal of Aerospace Engineering

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Figure 8

Figure 8: Geomagnetic Energy Approach to Space Debris Deorbiting in a Low Earth Orbit 