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F= G (m1m2)/(r2)

F= the gravitational force

G= gravitational constant

m1= mass of the first object (the satellite)

m2= mass of the second object (earth)

r= the radius

Plug in the values and solve for r:

690 N= 6.67 X 10-11 ((124kg) X (5.98 X 1024)/(r2)

690r2= 6.67 X10-11 (7.41 X 1026)

690r2= 4.94 X 1016

r2= (4.94 X 1016)/(690)

r= square root of (7.16 x 1013)

r= 8.46 x 106 m, or 846,000 Km

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