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| | Global Space Initiative (Site not responding. Last check: 2007-10-17) |
 | | At the beginning of each iteration, the orbiting body is regarded as having a momentary position and velocity, and the gravitational force, acting upon it, is calculated from its mass, the central body's mass, and the distance between these bodies. |
 | | If the graph does not show the orbit as expected, or at all, this may be because the scaling of the graph axes has resulted in the orbit's being outside the display range. |
 | | If, for example, you are trying to generate a parabolic orbit, and you see only half a parabola, it may be because you have defined the True Anomaly as being zero, which is at periapsis; so, all you see is the orbit after periapsis. |
| orbiter.vidmar.org /orbit-simulation.php (810 words) |
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