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        "author": "Sean Herron",
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        "description": "===========\nOrbit\n===========\n\nOrbit provides an easy way to get a number of values, such as current latitude and longitude, from objects in space. Currently, any object with a corresponding Two Line Element (TLE) can be tracked. A list of supported objects is available from Celestrack at <http://www.celestrak.com/NORAD/elements/master.asp>. Usage looks like:\n\n    from orbit import satellite\n    \n    # 25544 is the idenfier for the International Space Station\n    # See http://www.celestrak.com/NORAD/elements/master.asp for an index\n    # of identifiers.\n    \n    iss = satellite(25544)\n    \n    # Get the current lat/long of the satellite\n    iss_current_latitude = iss.lat()\n    iss_current_longitude = iss.long()\n    \n    # Get the proper name of the satellite\n    iss_name = iss.name()\n    \n    # Get the elsat classificiation of the satellite\n    iss_elsat_classification = iss.elsat_classification()\n    \n    # Get the year the satellite launched\n    iss_launch_year = iss.launch_year()\n    \n    # Get the current TLE for the satellite\n    iss_tle = iss.tle()\n    \n    # Get the current elevation of the satellite\n    iss_elevation = iss.elevation()\n    \n    # True if the satellite is currently in the earth's shadow\n    iss_eclipsed = iss.eclipsed()",
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