At an altitude where the acceleration due to gravity is

PHYSICS · Single correct · A Level · Physics · Fields and their consequences · Fields and their consequences

Problem

At an altitude where the acceleration due to gravity is 3.0 m s−23.0\,\text{m\,s}^{-2}, a satellite moves in a circular orbit around Earth. Using g=9.8 m s−2g = 9.8\,\text{m\,s}^{-2} and Earth’s radius R=6400 kmR = 6400\,\text{km}, determine the orbital speed of the satellite. (a) 7.9 km s−17.9\,\text{km\,s}^{-1} (b) 5.9 km s−15.9\,\text{km\,s}^{-1} (c) 11.2 km s−111.2\,\text{km\,s}^{-1} (d) 4.4 km s−14.4\,\text{km\,s}^{-1}

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