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Eccentricity Vector

Last modified by
on
Mar 4, 2021, 12:50:36 PM
Created by
on
May 25, 2014, 3:16:46 AM
e=(1μ)[(v2-μr)r-(rv)v]
(v)vector v
(r)vector r
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UUID
011767c1-e3bb-11e3-b7aa-bc764e2038f2

The Eccentricity Vector calculator computes the orbital eccentricity vector based on the velocity vector (V) and the position vector (R).

INSTRUCTIONS: Enter the following:

  • (v) Velocity Vector in meters per second (comma separated values)
  • (r) Position Vector in meters (comma separated values)

Eccentricity Vector (e): The calculator returns the eccentricity vector. 

The Math / Science

This equation produces the three components of the Eccentricity Vecotor, e

/attachments/011767c1-e3bb-11e3-b7aa-bc764e2038f2/EccentrictyVectorvece-illustration.png

Notes

The orbits and trajectories that can be characterized by eccentricity are:

elliptical:

circular: e = 1

parabolic trajectory

hyperbolic trajectory

0 < e < 1

e = 1

e = 1

e> 1

3D Vector Functions


This equation, Eccentricity Vector, references 2 pages
This equation, Eccentricity Vector, is used in 1 page
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