What is the semi major axis of the orbit


A satellite is in Earth orbit with an altitude at perigee of 555.0 km and an altitude at apogee of 1200.0 km.

a. What is the semi-major axis of the orbit?

b. What is the eccentricity? c. If the true anomaly is 160 degrees, what is the satellite's altitude? 

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Mechanical Engineering: What is the semi major axis of the orbit
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