(a) Determine the satellite's altitude above the surface of Earth.
_______m
(b) Determine the period of the satellite's orbit.
______h
_______m
(b) Determine the period of the satellite's orbit.
______h
-
a)
Ro = G*Me/V² = 24.257E6 m
A = Ro - Re = 17.88E6 m
b)
T = 2π√[Ro^3/(G*Me)] = 37585.6 sec = 10.44 hr
Ro = G*Me/V² = 24.257E6 m
A = Ro - Re = 17.88E6 m
b)
T = 2π√[Ro^3/(G*Me)] = 37585.6 sec = 10.44 hr