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
docstring: First order kepler equation solver derived using taylor series
  expansion.
  e is orbit eccentricity.
  M is mean anomaly,
  x is previous 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
code: def kepler1order(e, 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"""
      return (x-e*sin(x)-M)/(1.0-e*cos(x))
code_tokens: def kepler1order ( e , M , x ) : return ( x - e * sin ( x ) - M ) / ( 1.0 - 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"""