Derive expression for total energy of orbiting satellite

1.	Derive expression for total energy of orbiting satellite
Answer» ETIC ENERGY or total energy of an object in orbit can be found from the following equations: We know that,The Centripetal force on a satellite of mass 'm' moving at VELOCITY ' v ' in an orbit of radius r isF = mv^2/r But this is equal to the gravitational force ' F ' between the planet mass of M and the satellite. So, we get,F =GMm/r^2 and mv^2= GMm/r But, kinetic energy = ½mv^2So, Satellite's kinetic energy = ½ GMm/r Orbit's kinetic energy = ½ mv^2 = + ½GMm/r All SATELLITES have to be given a tangential velocity ' v ' to maintain their orbit position by the process that is CALLED orbit injection. Total energy of satellite in orbit = -GMm/2r know more:https://brainly.com/question/1358919 Derive the relationship between g and g

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Derive expression for total energy of orbiting satellite

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