original_docstring: First order kepler equation solver derived using taylor series
          expansion.
          e is orbit eccentricity.
          M is mean anomaly,
          x is previous Eccentric Anomaly
          returns E eccentric anomaly
docstring: First order kepler equation solver derived using taylor series
  expansion.
  e is orbit eccentricity.
  M is mean anomaly,
  x is previous Eccentric Anomaly
  returns E eccentric anomaly
docstring_tokens: First order kepler equation solver derived using taylor series expansion . e is orbit eccentricity . M is mean anomaly x is previous Eccentric Anomaly returns E eccentric anomaly
code: def kepler1order(self, M, x):
          """First order kepler equation solver derived using taylor series
          expansion.
          e is orbit eccentricity.
          M is mean anomaly,
          x is previous Eccentric Anomaly
          returns E eccentric anomaly"""
          return (x- self.e * sin(x)-M)/(1.0 - self.e * cos(x))
code_tokens: def kepler1order ( self , M , x ) : return ( x - self . e * sin ( x ) - M ) / ( 1.0 - self . e * cos ( x ) )
short_docstring: First order kepler equation solver derived using taylor series
  expansion.
short_docstring_tokens: First order kepler equation solver derived using taylor series expansion .
comment: """First order kepler equation solver derived using taylor series
          expansion.
          e is orbit eccentricity.
          M is mean anomaly,
          x is previous Eccentric Anomaly
          returns E eccentric anomaly"""