==Formulas== To find the position of the object in an elliptic Kepler orbit at a given time t, the mean anomaly is found by multiplying the time and the mean motion, then it is used to find the eccentric anomaly by solving Kepler`s equation. Again n is the mean motion. However, t, in this instance, is the time since epoch, which is how much time ....
Found on
http://en.wikipedia.org/wiki/Mean_anomaly
(from the article `anomaly`) ...anomaly is the angle, V, between lines drawn from the centre of mass (near the centre of the Sun, S), to a planet P, and to the perihelion point ... ...The angle , called the eccentric anomaly, also locates relative to but with the centre of the ellipse as the origin rather than the focus . An ... [2...
Found on
http://www.britannica.com/eb/a-z/m/60
No exact match found.
