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Ratio of energy to raise a satellite to height h to energy to put it in orbit there

The same question, asked 2 times: 2 May 2023 S2, 11 May 2024 S2. Every wording below, oldest first.

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  1. Question 1

    2 May 2023 S2

    39
    The gravitational potential energy required to raise a satellite of mass 'm' to height 'h' above the earth's surface is 'E1_1'. Let the energy required to put this satellite into the orbit at the same height be 'E2_2'. If M and R are the mass and radius of the earth respectively, then E1:E2E_1:E_2 is

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  2. Question 2

    11 May 2024 S2

    45
    The ratio of energy required to raise a satellite to a height 'h' above the earth's surface to that required to put it into the orbit at the same height is (R=R = radius of earth)

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