Mention the apogee and perigee height.

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Apogee (A) means the furthest distance a satellite gets from Earth in its orbit. A is related to the semi-major axis and eccentricity. A=a(1+e).

Perigee (P) means the closest distance the satellite gets to Earth in its orbit. P is related to the semi-major axis and eccentricity P=a(1−e).


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