The Russian Spektr-R satellite was recently placed in an Earth orbit with an altitude at perigee of 6,000 km and an altitude at apogee of 390,000 km. a. What is the semi-major axis of the orbit? b. What is the eccentricity? c. If the true anomaly is 180 deg, what is the satellite’s altitude

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The Russian Spektr-R satellite was recently placed in an Earth orbit with an altitude at perigee of 6,000 km and an altitude at apogee of 390,000 km. a. What is the semi-major axis of the orbit? b. What is the eccentricity? c. If the true anomaly is 180 deg, what is the satellite’s altitude?
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Step 1 To determine,

Part(a)

What is the semi-major axis of the orbit.

(b) What is the eccentricity.

(c) If the true anomaly is 180 degree, what is the satellite’s altitude.

Given,

Perigee distancerp=6000 km=6000×103 mapogee distancera=390000 km=390000×103 m 

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