a satellite which is at a height h from earths surface complete one revolution of the earth in 90 minute. if the radius of the earth be 6370 km and acceleration due to gravity 9.8 ms^-2 , then find the value of h.
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R = radius of earth = 6370 km = 6370,000 m
h = height of satellite above the earth's surface
g = acceleration due to gravity = 9.8 m/s²
T = time period of the satellite for one revolution around earth = 90 min = 90 x 60 sec = 5400 sec
time period of the satellite for one revolution around earth is given as
T = (2π) √(R + h)³/(gR²)
taking square both side
T² = (2π)² (R + h)³/(gR²)
T² (gR²)/ (2π)² = (R + h)³
inserting the values
(5400)² ((9.8) (6370,000)²)/ (2(3.14))² = ((6370,000) + h)³
h = 279532 m = 279.532 km
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