A Satellite in an elliptical orbit is moving from position A, where its Kinetic energy is 15 MJ and its total mechanical energy is 27 MJ, to a new position B, where its kinetic energy is 12 Mj. What is the work done (if any) by the net force acting on the satellite, when it moves from A to B? Is the satellite getting closer or going away from the planet it is orbiting around? What is the total mechanical energy of the satellite at point B?

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Chapter13: Universal Gravitation
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. A Satellite in an elliptical orbit is moving from position A, where its Kinetic energy is 15 MJ and its total mechanical energy is 27 MJ, to a new position B, where its kinetic energy is 12 Mj.

  1. What is the work done (if any) by the net force acting on the satellite, when it moves from A to B?
  2. Is the satellite getting closer or going away from the planet it is orbiting around?
  3. What is the total mechanical energy of the satellite at point B?

 

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