4. Application example
We consider a list of 21 pieces of debris in circular orbits at altitudes between 700 and 900 km, inclinations between 97 and 99 degrees, and initial RAANs between 0 and 360 degrees. The altitudes, inclinations and initial RAANs are uniformly distributed within their respective ranges. Table 1 gives the orbital parameters of the debris, with their nodal precession velocity in the last column.
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