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the_d
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A satellite moves in a circular orbit around
the Earth at a speed of 6.7 km/s.
Determine the satellite's altitude above the
surface of the Earth. Assume the Earth
is a homogeneous sphere of radius Rearth =
6370 km and mass Mearth = 5.98 x 10^24 kg .
You will need G = 6:67259 x 10^-11 N m^2/kg2
the Earth at a speed of 6.7 km/s.
Determine the satellite's altitude above the
surface of the Earth. Assume the Earth
is a homogeneous sphere of radius Rearth =
6370 km and mass Mearth = 5.98 x 10^24 kg .
You will need G = 6:67259 x 10^-11 N m^2/kg2