Difference between revisions of "Semi-major axis"

From Conservapedia
Jump to navigation Jump to search
(New page)
 
(→‎Calculations: More formulas)
 
Line 8: Line 8:
 
<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. See [[orbital eccentricity]] for details.
+
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:
 +
 
 +
<math>Q = a(1+e)</math>
 +
 
 +
<math>q = a(1-e)</math>
 +
 
 +
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