PlotOrbit:

Path: CubeSat/Visualization

% Plot the state in 3D with an Earth map. 

 Note that the location relative to the map is only accurate for
 Earth-fixed frame input. Enter time and Julian date to compute the
 Earth-fixed positions from ECI data automatically.

 Since version 8.
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   Form:
   h = PlotOrbit( rEF )
   h = PlotOrbit( rECI, t, jD0 )
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   ------
   Inputs
   ------
   r         (3,m)  Position vectors (km)
           or
              {n}   Cell array of position matrices for multiple satellites
   t         (1,:)  Time array (sec)
   jD0       (1,1)  Epoch Julian date

   ------
   Output
   ------
   h         (1,1)  Figure handle
   l         (1,n)  Handle to orbit lines

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   See also: LoadEarthMap
--------------------------------------------------------------------------

Children:

AeroUtils: Coord/ECIToEF
Common: Time/JD2T
SC: Visualization/LoadEarthMap

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