Please help!! circular motion 1. The problem statement, all variables and given/known data At what height above teh earths surface would a satellite have to orbit in order that it be stationary in reference to a point on the earth? b. what would be it's speed? c. How would you describe the general location of that point in relation to the earth's surface? 2. Relevant equations Fg= (G)(M1M2) r2 G=6.67x10-11Nm2/kg2 Fw=Mg Fc=M v2 r a=v2 r Earth mass=6x1024kg Earth radius=6.4x106m 3. The attempt at a solution Can someone help me and let me know where to start? I know how to find the velocity, but seems like i dont have enough information? is there something i'm missing?? please help!!!