A 981-kg satellite orbits the Earth at a constant altitude of 103-km.
How much energy must be added to the system to move the satellite into a circular orbit with altitude 199 km?

I need answer in MJ

please tell me what formula

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  1. find the original PE+KE
    find the new PE+KE

    what is the difference?

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  2. You need to do work against gravity to move it to a higher orbit, but you get some back because the kinetic energy will be less at the higher orbit. You have to consider the total energy required.

    The total energy (kinetic + potential) for a circular orbit at radius R is
    Etotal = (1/2) m V^2 - G M m/R

    where G is the universal constant of gravity and M is the mass of the Earth. Since
    V^2/R = GM/R^2,
    Etotal = (1/2)m*GM/R -GmM/R
    = -(1/2)GmM/R

    Compute this quantity at R = 103 km and at R = 199 km and take the difference. The work required will be positive.

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  3. ok sir is the formula

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