A satellite of 200 kg revolves around the earth at a height of 1000 km from the surface of the earth. Calculate (i) escape energy (ii) escape speed of this satellite. Take G = 6.67 × 10⁻¹¹ Nm²/kg², radius of the earth = 6400 km and mass of the earth = 6 × 10²⁴ kg.
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