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## Homework Statement

I have to find the orbital height of a satellite with a specific g force (ie. the acceleration due to gravity). g=5.7(ms)2

## Homework Equations

So far I have been using the equation g=Gm/(r+h)2 to find the acceleration due to gravity, where G= gravitational constant, m=mass of the Earth ,r=radius of the earth and h= the orbital height from the Earth

except now I am given a specific g force and have been asked to find the height.