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.

--------------------------------------------------------------------------
   Form:
   [h, l] = PlotOrbit( rEF )
   [h, l] = PlotOrbit( rECI, t, jD0 )
--------------------------------------------------------------------------

   ------
   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

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

Children:

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

Back to the CubeSat Module page