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The eccentric anomaly is the angle between the direction of periapsis and the current position of an object on its orbit, projected onto the ellipse's circumscribing circle perpendicularly to the major axis, measured at the centre of the ellipse. In the diagram below, it is E (the angle zcx). [edit] CalculationIn astrodynamics eccentric anomaly E can be calculated as follows: where:
The relation between E and M, the mean anomaly, is: This equation can be solved iteratively, starting from E0 = M and using the relation The equation can also be expanded in powers of e, as long as e < 0.6627434. The first few terms of the expansion are:
For references on details of this derivation, as well as other more efficient methods of solution, see Murray and Dermott (1999, p.35). For a derivation of the limiting value of e see Plummer (1960, section 46). The relation between E and ν, the true anomaly, is: or equivalently The relations between the radius (position vector magnitude) and the anomalies are: and [edit] See also[edit] References
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