CELESTIAL MECHANICS A  B  C  D  E  F  G  H  I  J  K  L  M  N  O  P  Q  R  S  T  U  V  W  X  Y  Z                    HOME ABOUT CATEGORIES SITE MAP COPYRIGHT ADVERTISE CONTACT entire Web this site Kepler's equation One of the important formulae that enables the position of a body in an elliptical orbit to calculated at any given time from its orbital elements. It relates the mean anomaly, M, of the body to its eccentric anomaly, E, by the following: M = E - e sin E where e is the eccentricity of the orbit. Related category    • CELESTIAL MECHANICS Also on this site: Encyclopedia of Alternative Energy & Sustainable Living Encyclopedia of History Transport Concepts & Designs (partner site) BACK TO TOP