How Can You Calculate the Altitude of a Satellite Using Gravitational Equations?

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chewtoy929
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how can I calculate the distance something is above the earth? as an example a 1750 kg satellite orbits the earth. it has a gravitational potential energy of 1.69*10^10 J. Its free fall accel is 6.44 m/s^2 how high is it.

How would I solve this? thanks.
 
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Welcome to the PF, chewtoy. On homework and coursework questions, you must show us the relevant equations and also your initial attempt at a solution, before we can offer much in the way of tutorial help.

You appear to be studying uniform circular motion and gravitational forces. Show us the relevant equations from your textbook for this subject matter, and tell us your thoughts on how you might use those equations to approach this question.
 
tnutty said:
Use this formula :

F_g = GMm/r^2

or

mg = GMm/r^2

dont you mean use a = GM/R^2? If a satellite is way above Earth's surface, using little g(9.81) for any calculation would be wrong. the point of that equation is the gravitational pull ISN'T 9.81.

the force one mass pulls on the other mass is equal to gravitational constant 6.67...something * mass of object 1 * mass of object 2 divided by the distance from the centers of the objects squared:
GMm/r^2 = F

you know by now that f = ma

substitute for f, use your given a, and solve for r.