A low orbiting satellite is launched at the height of 3.0 × 105 m above the surface of the Earth. If the mass of the Earth is taken as 6.0 × 1024 kg, radius as 6.4 × 106 m and gravitational constant as 6.67 × 10–11 Nm2 /kg2 , then the orbital speed of the satellite is
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Ans should be 0.77×10^4 m/s
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