A 500 kg satellite remains at the same location relative to a location on a Planet Mars that rotates on its axis. The distance from the center of the Planet Mars to the satellite is r = 3.03 x 107 m. (M Mars = 6.42 x 1023 kg, G 6.67 x 1011 kg1 m³/s?) (a) What is the equation used to calculate the orbital period, T of the satellite? 472 %3D GMMars 472 T2 = GMMars 47 T = GM Satellite (b) Calculate the orbital period, T of the satellite (your answer must be in 2 decimal places) Your answer is x 105 s c) What is the equation used to calculate the speed of satellite?

A 500 kg satellite remains at the same location relative to a location on a Planet Mars that rotates on its axis. The distance from the center of the Planet Mars to the satellite is r = 3.03 x 107 m. (M Mars = 6.42 x 1023 kg, G 6.67 x 1011 kg1 m³/s?) (a) What is the equation used to calculate the orbital period, T of the satellite? 472 %3D GMMars 472 T2 = GMMars 47 T = GM Satellite (b) Calculate the orbital period, T of the satellite (your answer must be in 2 decimal places) Your answer is x 105 s c) What is the equation used to calculate the speed of satellite?

Principles of Physics: A Calculus-Based Text

5th Edition

ISBN:9781133104261

Author:Raymond A. Serway, John W. Jewett

Publisher:Raymond A. Serway, John W. Jewett

Chapter3: Motion In Two Dimensions

Section: Chapter Questions

Problem 27P: The astronaut orbiting the Earth in Figure P3.27 is preparing to dock with a Westar VI satellite....

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