morbit

This is a solution for the keplar problem for orbit insertion.

This is a solution for the keplar problem for orbit insertion. Given a burn out velocity and a flight path angle, what is the apogee of the orbit, and the circular orbit that can be achived with one burn at apogee? The delta-velocity for circularization is also plotted. Several other planets , besides earth, are also included and the user can simple adjust the initial parameters to preform orbital analysis of several planets in our home solar system.