Kepler's equation
Kepler's equation, M = E − e sin E, relates mean anomaly M to eccentric anomaly E for an orbit with eccentricity e. Solving it yields a body's position along an elliptical orbit at a given time.
Kepler's equation, M = E − e sin E, relates mean anomaly M to eccentric anomaly E for an orbit with eccentricity e. Solving it yields a body's position along an elliptical orbit at a given time.