Path: Orbit/OrbitCoord

% Computes closest orbit point to points on the earth. 

 You can input any number of orbits to check. The function propagates
 the orbit with a Kepler propagator. The Earth rotation is found using

 Type OrbitClosestPoint for a demo.
   [rMin, dMin, jDMin] = OrbitClosestPoint( rEFTarget, el, jDEpoch, n, nOrbits )

   rEFTarget   (3,m)   Target vectors to check
   el          (1,6)   Keplerian elements [a i Lon Arg e M]
   jDEpoch     (1,1)   Julian date epoch of elements
   n           (1,1)   Number of points to check
   nOrbits     (1,1)   Number of orbits to check

   rMin        (3,m)   Nearest orbital point
   dMin        (1,m)   Distance to each point
   jDMin       (1,m)   Julian date for each point (days)



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: BasicOrbit/Period
SC: Ephem/EOfE
SC: Ephem/EarthNut
SC: Ephem/EarthPre
SC: Ephem/EarthRot
SC: Ephem/GMSTime
SC: Ephem/MSidDay
SC: Ephem/NutDelta
SC: Ephem/ObOfE
SC: Ephem/TruEarth
Common: CommonData/SwooshWatermark
Common: General/CellToMat
Common: General/DeBlankLT
Common: General/MatToCell
Common: General/Watermark
Common: Graphics/Axis3D
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
Common: Time/JD2000
Common: Time/JD2T
Common: Time/JDToMidnight
Math: Linear/DupVect
Math: Linear/Mag
Math: MathUtils/R2P5
Math: Trigonometry/CosD
Math: Trigonometry/SinD

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