original_docstring: Second order kepler equation solver derived using taylor series
      expansion.
      e is orbit eccentricity.
      M is mean anomaly,
      x is previous Eccentric Anomaly
docstring: Second order kepler equation solver derived using taylor series
  expansion.
  e is orbit eccentricity.
  M is mean anomaly,
  x is previous Eccentric Anomaly
docstring_tokens: Second order kepler equation solver derived using taylor series expansion . e is orbit eccentricity . M is mean anomaly x is previous Eccentric Anomaly
code: def kepler2order(e, M, x):
      """Second order kepler equation solver derived using taylor series
      expansion.
      e is orbit eccentricity.
      M is mean anomaly,
      x is previous Eccentric Anomaly"""
      t1 = -1 + e*cos(x)
      t2 = e*sin(x)
      t3 = -x+t2+M
      return t3/(0.5*t3*t2/t1 + t1)
code_tokens: def kepler2order ( e , M , x ) : t1 = - 1 + e * cos ( x ) t2 = e * sin ( x ) t3 = - x + t2 + M return t3 / ( 0.5 * t3 * t2 / t1 + t1 )
short_docstring: Second order kepler equation solver derived using taylor series
  expansion.
short_docstring_tokens: Second order kepler equation solver derived using taylor series expansion .
comment: """Second order kepler equation solver derived using taylor series
      expansion.
      e is orbit eccentricity.
      M is mean anomaly,
      x is previous Eccentric Anomaly"""