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Apsis-Pericenter (minimum distance)

Last modified by
on
Jul 24, 2020, 6:28:07 PM
Created by
on
Aug 1, 2016, 6:08:50 PM
rper=(1-e)a
(a)semi-major axis
(e)eccentricity
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The Apsis-Pericenter Minimum Distance calculator computes the minimum distance from the center of gravity in an orbit at perigee based on the semi-major axis (a) and eccentricity (e).

INSTRUCTION: Choose units and enter the following:

  • (a) This is the semi-major axis of the orbit
  • (e) This is the eccentricity of the the orbit

Minimum Distance (rper): The calculator returns the distance in meters.  However this can be automatically converted to compatible units via the pull-down menu.

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The Math / Science

The Apsis-Pericenter (minimum distance) is an extreme point in an object's orbit. For elliptical orbits about a larger body, there are two apsides. The pericenter is the point closest to the object being orbited. 

The formula for the Apsis-Pericenter minimum distance is:

rper=(1-e)a

where:

References

Wikipedia (https://en.wikipedia.org/wiki/Apsis)


This equation, Apsis-Pericenter (minimum distance), is used in 1 page
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