A transcendental equation of the form
The case $0\leq c<1$ is important for applications; here $y$ is uniquely determined from a given $c$ and $x$. This equation was first considered by J. Kepler (1609) in connection with the problem of planetary motion: Let the ellipse $AQB$ (see Fig.) with focal point $D$ be a planetary orbit, with circumscribed circle $APB$.
Then the Kepler equation gives the relation between the eccentric anomaly $y=\angle POA$ and the mean anomaly $x$, $c$ being the eccentricity of the ellipse.
The Kepler equation plays an important role in astronomy in determining the sections of elliptic orbits of planets.
|||M.F. Subbotin, "A course in celestial mechanics" , 1 , Leningrad-Moscow (1941) (In Russian)|
The mean anomaly is a linear function of the time of the planet's passage at the point $Q$. For more details, including the corresponding equations for hyperbolic and parabolic motion, see e.g. [a1].
|[a1]||P.M. Fitzpatrick, "Principles of celestial mechanics" , Acad. Press (1970)|
Kepler equation. Encyclopedia of Mathematics. URL: http://www.encyclopediaofmath.org/index.php?title=Kepler_equation&oldid=43516