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A satellite moves in a circular orbit around the Earth at a speed of 6.3 km/s. Determine the satellite’s altitude above the surface of the Earth. Assume the Earth is a homogeneous sphere of radius 6370 km and mass 5.98 × 1024 kg. The value of the universal gravitational constant is 6.67259 × 10−11 N · m2/kg2. Answer in units of km
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you can start from thinking that the gravitational force equals centrifugal force. Then you can solve distance from there.
centrifugal force?
\[F=\frac{ m*v ^{2} }{ r } \]
I got 3.67953*10^6 but I think its wrong
you got the right answer except unit.. check the unit.
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Hmm how do I change the units?
what you got is unit in meter. If you turn it into km, you have to divide it by 1000.
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u r welcome !
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