Difference between revisions of "Semi-major axis"
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<math>a = (Q + q)/2</math> | <math>a = (Q + q)/2</math> | ||
| − | The semi-major axis, together with the [[orbital eccentricity]], can predict the periapsis and apoapsis | + | For this reason the semi-major axis is often cited as a "mean orbital radius." |
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| + | The semi-major axis, together with the [[orbital eccentricity]] (''e''), can predict the periapsis and apoapsis: | ||
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| + | <math>Q = a(1+e)</math> | ||
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| + | <math>q = a(1-e)</math> | ||
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| + | See [[orbital eccentricity]] for a detailed derviation | ||
[[Category:Astronomy]] | [[Category:Astronomy]] | ||
Latest revision as of 20:15, February 20, 2008
The semi-major axis of any ellipse is the axis of symmetry that passes through the foci of that ellipse.
In astrophysics, the semi-major axis of an orbit is the distance between the geometric center of the orbit and either apsis. It is a commonly reported orbital element that can determine the size and shape of an orbit.
Calculations
The semi-major axis, usually labeled a, is the arithmetic mean of the two apsides:
For this reason the semi-major axis is often cited as a "mean orbital radius."
The semi-major axis, together with the orbital eccentricity (e), can predict the periapsis and apoapsis:
See orbital eccentricity for a detailed derviation