orbitx.TLE
==========

.. currentmodule:: orbitx

.. autoclass:: TLE

   
   .. automethod:: __init__

   
   .. rubric:: Methods

   .. autosummary::
   
      ~TLE.__init__
      ~TLE.from_filepath
      ~TLE.from_sat_shortname
   
   

   
   
   .. rubric:: Attributes

   .. autosummary::
   
      ~TLE.argument_perigee
      ~TLE.ballistic_coefficient
      ~TLE.classification
      ~TLE.creation_date
      ~TLE.drag_term
      ~TLE.eccentricity
      ~TLE.element_set_number
      ~TLE.end_date
      ~TLE.end_date_seconds_since
      ~TLE.inclination
      ~TLE.launch_number
      ~TLE.launch_piece
      ~TLE.launch_year
      ~TLE.mean_anomaly
      ~TLE.mean_motion
      ~TLE.reference_date
      ~TLE.reference_date_seconds_since1970
      ~TLE.revolution_number
      ~TLE.right_ascension
      ~TLE.satellite_catalog_number
      ~TLE.satellite_name
      ~TLE.satellite_shortname
      ~TLE.second_derivative
      ~TLE.start_date
      ~TLE.start_date_seconds_since
      ~TLE.tle_date
      ~TLE.tle_date_seconds_since
      ~TLE.tle_line_1
      ~TLE.tle_line_2
      ~TLE.tle_xarray
      ~TLE.version