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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Orbit: OrbitCoord/SLR Orbit: OrbitMechanics/RVOrbGen SC: BasicOrbit/CP2I SC: BasicOrbit/E2M SC: BasicOrbit/E2Nu SC: BasicOrbit/M2E SC: BasicOrbit/M2EApp SC: BasicOrbit/M2EEl SC: BasicOrbit/M2EHy SC: BasicOrbit/Nu2E SC: BasicOrbit/Nu2M SC: SCMat/EarthMR SC: Visualization/PlotPlanet Common: CommonData/SwooshWatermark Common: General/CellToMat Common: General/DeBlankLT Common: General/MatToCell Common: General/Watermark Common: Graphics/Axis3D Common: Graphics/Ellipsd Common: Graphics/Map Common: Graphics/Mesh2 Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle Common: Graphics/TimeLabl Common: Graphics/TitleS Common: Graphics/XLabelS Common: Graphics/YLabelS Common: Graphics/ZLabelS Common: Time/DTSToDTA Common: Time/Date2JD Math: Linear/DupVect
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