The velocity of a satellite rotating around the Earth

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yashboi123
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Homework Statement
A satellite travels at an altitude of 6580 km where gravity is 9.2 m/s^2.
Relevant Equations
v^2/r = a
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Not sure what r would be in this scenario. I tried adding the radius of the earth to the altitude but that wasn't correct either.
 
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The confusion is in the question itself.

If gravity is 9.2 m/s^2 (as stated in the question), then satellite distance from earth center is 6580km (verify yourself!). And that distance should not be called altitude :-(

If altitude is really 6580km, g is about 2.38 m/s^2.
 
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