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Eccentricity

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Revision as of 09:54, 3 November 2011 by 120.203.1.250 (talk) (Definition)


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For the love of God, keep wtrinig these articles.

Calculation

For elliptic orbits, eccentricity can be calculated from distance at periapsis and apoapsis:

e=dadpda+dp
=12(da/dp)+1

where:

  • dp is distance at periapsis (closest approach),
  • da is distance at apoapsis (farthest approach).

References