here,
the height of satellite , h = 4810 km
h = 4.81 * 10^6 m
the radius of Earth , r = 6.37 * 10^6 m
the speed of satellite , v = sqrt( G * M /(r + h))
v = sqrt( 6.67 * 10^-11 * 5.98 * 10^24 /(6.37 * 10^6 + 4.81 * 10^6))
v = 5973 m/s
the speed of satellite is 5973 m/s
Problem 5.46 Part A Calculate the speed of a satelite moving in a stable circular orbit...
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