Explanation 1) Concept: As the satellite is revolving around earth, using Kepler’s 3 rd law, we can first find the orbital radius of the satellite from the center of the earth. To find the height of the orbit, we have to subtract the radius of the earth from the orbital radius to get the required answer. 2) Formula: T 2 = 4 π 2 G M a 3 3) Given: i) T s a t e l l i t e = T e a r t h = 86400 s a s t h e s t a t e l l i t e i s G e o s t a t i o n a r y s a t e l l i t e . ii) G = 6.67 × 10 - 11 N . m 2 k g 2 iii) M e a r t h = 5.98 × 10 24 k g iv) R e a r t h = 6

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Author: David Halliday, Robert Resnick, Jearl Walker

Publisher: Wiley, John & Sons, Incorporated

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Central Force

Central force is the force that acts along the center of mass of one body to the center of mass of another body. Its direction from or away from a point on a body to another is called the center of the force. Such forces include gravitational force betwe…

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Chapter 13, Problem 50P

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Altitude of the orbit.

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Chapter 13, Problem 49P

Chapter 13, Problem 51P

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Fundamentals of Physics Extended

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Altitude of the orbit.

Solution Summary: The author explains how to find the orbital radius of the satellite using Kepler's 3 rd law.

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To Find: Altitude of the orbit.

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Chapter 13 Solutions

To Find:

Altitude of the orbit.