Overload List

  NameDescription
Public methodStatic memberOrbitTrack(Satellite, DateTime, DateTime, Double)
Returns the equidistant Earth Centered Inertial coordinates of a satellite orbit track.
Public methodStatic memberOrbitTrack(Satellite, DateTime, DateTime, TimeSpan)
Returns the equal time-spaced Earth Centered Inertial coordinates of a satellite orbit track.
Public methodStatic memberOrbitTrack(Satellite, Double, Double, Double)
Returns the equidistant Earth Centered Inertial coordinates of a satellite orbit track.
Public methodStatic memberOrbitTrack(Satellite, Double, Double, TimeSpan)
Returns the equal time-spaced Earth Centered Inertial coordinates of a satellite orbit track.

See Also