A satellite is in Earth orbit with an altitude at perigee of 500 km and an altitude at apogee of 700 km.

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A satellite is in Earth orbit with an altitude at perigee of 500 km and an altitude at apogee of 700 km.

What is the semimajor axis of the orbit?

Please only submit a number in the answer box (do not include units). I will assume the answer you submit is in kilometers.

science Advanced-Physics

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Answer 1

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Answer 2

Answer #2

elliptic orbit of satelite ae Apogee Perigee a Centre of the earth At perigee and apogee the altitude of the satelite is 500k

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A satellite is in Earth orbit with an altitude at perigee of 500 km and an altitude at apogee of 700 km.

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