Quantcast
Loading [MathJax]/jax/output/CommonHTML/jax.js

Apsis-Pericenter (maximum speed)

Last modified by
on
Jul 24, 2020, 6:28:07 PM
Created by
on
Aug 1, 2016, 6:04:33 PM
vper=(1+e)MG(1-e)a
(M)Mass of the primary body
(a)semi-major axis
(e)eccentricity
Tags
UUID
669ecc83-5812-11e6-9770-bc764e2038f2

The Apsis-Pericenter Maximum Speed calculator computes the maximum speed in an orbit at perigee based on the semi-major axis (a), eccentricity (e), the mass of the primary body (M), and the Universal Gravitational Constant (G).

INSTRUCTION: Choose units and enter the following:

  • (M) This is the mass of the primary body.
  • (a) This is the semi-major axis of the orbit
  • (e) This is the eccentricity of the the orbit

Maximum Orbital Speed(Vper): The calculator returns the velocity in meters per second.  However this can be automatically converted to compatible units via the pull-down menu.

Related Calculators

The Math / Science

The Apsis-Pericenter (maximum speed) 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 maximum speed is:

vper=(1+e)μ(1-e)a

where:

References

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


This equation, Apsis-Pericenter (maximum speed), references 1 page
This equation, Apsis-Pericenter (maximum speed), is used in 1 page
  • Comments
  • Attachments
  • Stats
No comments
This site uses cookies to give you the best, most relevant experience. By continuing to browse the site you are agreeing to our use of cookies.