An earth satellite has a perigee of 300km and an apogee of 3,500 km above the Earth’s surface. How far is the satellite above earth When (a) It has rotation 90° around Earth from perigee and (b) It has moved halfway from perigee to apogee?

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An earth satellite has a perigee of 300km and an apogee of 3,500 km above the Earth’s
surface. How far is the satellite above earth When (a) It has rotation 90° around Earth
from perigee and (b) It has moved halfway from perigee to apogee?

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