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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yashboi123 said:
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.
Please show your work. We cannot help you if you don't tell us what you did.
 
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.