A satellite of mass 290 kg is orbiting in a circular orbit of radius 1150 km (measured from the center of the planet). The mass of the planet is 5.78×1024 kg.
Part A
What is the angular momentum of the satellite with respect to the point at the center of the planet?
Gravitational constant = G = 6.67 x 10-11 N.m2/kg2
Mass of the planet = M = 5.78 x 1024 kg
Mass of the satellite = m = 290 kg
Radius of orbit = R = 1150 km = 1150 x 103 m = 1.15 x 106 m
Orbital speed of the satellite = V
The gravitational force between the planet and the satellite provides the necessary centripetal force for the circular motion of the satellite.
V = 1.831 x 104 m/s
Angular momentum of the satellite with respect to the point at the center of the planet = L
L = mVR
L = (290)(1.831x104)(1.15x106)
L = 6.106 x 1012 kg.m2/s
A) Angular momentum of the satellite with respect to the point at the center of the planet = 6.106 x 1012 kg.m2/s
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