Fundamental Technologies Voyager LECP Pages

Figure E-1. Earth Mean Ecliptic and Equinox of 1950.0 (ECL50), Jupiter Encounter State Vectors

Nomenclature --> S refers to State Vector (position and velocity components) with the subscripts AB, where A is the reference or "from" body and B is the "to" body. The following body definitions are used: S - Sun; P - S/C or Probe; E - Earth; 5 - Jupiter; I - Io; U - Europa; G - Ganymede; C - Callisto.

Return to Voyager LECP Data Analysis Handbook Table of Contents.
Return to Fundamental Technologies Home Page.

Last modified 12/6/02, Tizby Hunt-Ward
tizby@ftecs.com