Hey REB
Hi All
REB... below you pointed to a link with useful orbit equations, which I have checked and they're only half-right. Here's the original link...
http://web.mit.edu/12.000/www/finalpresentation/traj/free.html
First mistake - they calculated time as theta/2*pi, which is only half-way to finding t. It's true for a circular orbit, but for an ellipse you need the area enclosed by the angle. Second mistake - all the distances used are too small by x10. Hence all velocities are inflated.
A more useful set of equations can be found here...
http://www.gdnordley.com/Kepler.doc
...hope you find them useful
Adam
