I did a little research, and I came up with this answer. Please correct me if I'm wrong guys!
We know that the circumference of the earth is 24,934 miles. We also know that gravity at sea level is 9.81 meters per second. Every meter above sea level you increase, gravity decreases by .0003086 cm squared.. I think. Also, if you are at an altitude of 100 miles above earth, that would mean that the circumference is now 25,214 miles.
So, (25,214 x 100) / 24,934 = 1.123% more circumference distance that the satellite is traveling than it would be if it were on the surface of Earth.
If we were to increase this height by 1 meter, then we are increasing the height 1/1609.344ths of a single mile. This would mean that 25,214 would turn into 25,214.2 about. 1.124% So we can say that increasing the height of the satellite by one meter would increase it by 1 thousandths of a percent in circumference.
Now for gravitational pull~
If gravity is 9.81 meters per second at sea level, and it decreases by .3 x 10^-3cm, than we can say that; Gravity at 100 meters above sea level would be 9.81 - (160,934.4 x .000003)
This means that the force of gravity at 100 miles above sea level is 9.3271968.
If we increase the height of the satellite by 1 meter, than the equation would become: 9.81 - (160,935.4 x .000003)
So the force of gravity 100miles + 1 meter above sea level is 9.3271938.
(9.3271938 x 100) / 9.3271968 = .000043
This means that Gravity would have went down .000043% due to the height increase of the satellite by 1 meter. or 4 billionths of a meter.
wow... lots of math. Break time. Brb, food.