Path: Orbit/Visualization

% Plot an orbit track in the Earth/Moon Rotating System.
   The input vectors are in the ECI frame. Has a built-in demo for an orbit  
   with an apogee of 400,000 km, a perigee of 7000 km, and a duration of 5 days.
   EarthMoonRotFrame( r, jD, scale, lagrange, lunarCone )

   r                (3,:) ECI position vectors (km) or
                    (1,6) elements
   jD               (:)   Julian dates
   scale            (1,2) Planet scale (optional, default is [1 1])
   lagrange         (1,1) If entered draw lagrange points
   lunarCone        (1,3) [lat, lon, angle]




AC: ACData/ACTConstants
AerospaceUtils: Coord/LatLonToR
Orbit: OrbitCoord/RPRA2AE
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: Ephem/LagrangePointsL1ToL5
SC: Ephem/MoonEl
SC: Ephem/MoonV1
SC: SCData/sCTConstants
Common: CommonData/Constants
Common: CommonData/SwooshWatermark
Common: CommonData/xSplashSmall
Common: ComponentModels/Box
Common: ComponentModels/Cone
Common: ComponentModels/Frustrum
Common: Database/Constant
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/DeleteCell
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Axis3D
Common: Graphics/DrawVertices
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: Quaternion/QForm
Common: Quaternion/QTForm
Common: Quaternion/U2Q
Common: Time/DTSToDTA
Common: Time/Date2JD
Common: Time/JD2000
Common: Time/JD2T
Math: Geometry/Perpendicular
Math: Linear/Cross
Math: Linear/Dot
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/Unit
Math: Trigonometry/CosD
Math: Trigonometry/SinD

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