A satellite is in earth orbit with an altitude at perigee

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Reference no: EM13344081

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? 

Reference no: EM13344081

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