The energy required to take a satellite
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The energy required to take a satellite to a height 'h' above earth surface (radius of earth = 6.4 × 10³ km) is E1 and kinetic energy required for the satellite to be in a circular orbit at this height is E2. The value of h for which E1 and E2 are equal is :- a) 1.28 × 10⁴ kmb) 6.4 × 10³ kmc) 3.2 × 10³ kmd) 1.6 × 10³ km