Here's what should make it a little clearer. According to the current model, objects with great enough velocities can orbit the earth because the object is "trying" to get away from the earth, but it is pulled back by gravity. The force acts perpendicular to the object's trajectory, causing it to circle the earth instead of just crash down onto it.<br /><br />Now, -according to your own theory-, as soon as an object leaves the earth, whether it's rock or a rocket, no other force is acting on it. The only thing the object has to go on is it's own velocity (once the fuel has been used).<br /><br />Now, I've calculated (if you want to see them, just ask, but trust me, they're right). That if an object shoots straight up into the air from the ground with initial velocity v, then (on earth) the amount of time it takes for the object to come back down is about t = .204v, that is, if something pops up from the ground at 5 m/s, after about a second it will hit the ground. Now, I don't care how big v is, if no other forces are acting on the object it WILL come back down after (.204)v seconds.<br /><br />If the initial velocity is directed -anywhere except straight up- the amount of time will lessen, no matter what. I can show you this with calculus if you wish. Just ask.<br /><br />Now, if you're right, we can figure out long the sattelites will stay up where they are. We can assume there is no initial expansion velocity, because if there is, then it's the same for both the sattelite and the earth. So all we need to do is figure out if the earth accelerates at 9.8 m/s^2, how long will it take till it overtakes the average sattelite. Since this calculation is rather simple, I'll show it.<br /><br />1. With no inital velocity, d = 1/2 x a x t^2 right? Rearranging, we get:<br />t = sqr. root (2d/a).<br /><br />2. The average sattelite is up about 100 miles, and that's about 161,000 meters.<br /><br />3. a = 9.8. So we plug this into the equation.<br /><br />I got 181 seconds. In oth