Path: SCPro/ProEphemeris
% Low precision orbits of the four major Galilean satellites.
Uses orbital elements which ignores all perturbations.
The satellites are 'Io' 'Europa' 'Ganymede' 'Callisto'.
The outputs are
r[Io 3xn; Europa 3xn; Ganymeded 3xn; Callisto 3xn];
v[Io 3xn; Europa 3xn; Ganymeded 3xn; Callisto 3xn];
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Form:
[r,v,name] = GalileanSatelliteOrbits( jD )
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Inputs
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jD (1,:) Julian day numbers
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Outputs
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r (12,:) [x;y;z;x;y;z...]
v (12,:) [x;y;z;x;y;z...]
name {4} Corresponding name
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