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Kepler's Equation

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on

Jul 24, 2020, 6:28:07 PM

Created by

on

Jul 5, 2016, 3:02:24 PM

M = E - e sin E

$M = E-esinE$

(E) Eccentric anomaly

$(E)"Eccentric anomaly"$

(e) Eccentricity

$(e)"Eccentricity"$

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In orbital mechanics, Kepler's Equation relates various geometric properties of the orbit of a body subject to a central force. The equation is $M = E - e sin E$ $M=E-esinE$ , where:

$E$ $E$ = eccentric anomaly
$e$ $e$ = eccentricity
$M$ $M$ = mean anomaly

References

The formula and definition are from Wikipedia(https://en.wikipedia.org/wiki/Kepler%27s_equation).

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