Satellite X moves around Earth in a circular orbit radius R. Satellite Y is also in a circular orbit around earth, and it completes one orbit for every eight orbits completed by satellite X. What is the orbital radius of satellite Y?
First of all, we know the difference in the period of the orbits:\[T _{Y}=8T _{X}\]We also know that the velocity of each satellite is determined by the equation which treated gives out:\[v =\frac{ 2 \pi R }{ T }\rightarrow R=\frac{ vT }{ 2\pi } \rightarrow R _{Y}=\frac{ v _{Y}T _{Y} }{ 2\pi }=\frac{ v _{Y}4T _{X} }{ \pi }\]The problem is that we don't know the velocity of satellite Y which is absolutely necessary since for what we know the radius of Y may be a 100 time bigger than the radius of X if satellite Y has a velocity 25 times bigger than tha of satellite X. There maybe a orbit equation that I am not aware about? Maybe one that includes masses that cancel of since we can assume that the satellites have the same mass.
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