1. A satellite is in Earth orbit with an altitude at perigee of 750 km and an altitude at apogee of 8000 km. a. What is the semi-major axis of the

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1.     A satellite is in Earth orbit with an altitude at perigee of 750 km and an altitude at apogee of 8000 km. a. What is the semi-major axis of the orbit? b. What is the eccentricity? c. If the true anomaly is 175 degrees, what is the satellite’s altitude?

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