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Text File  |  1991-02-26  |  503b  |  10 lines
  1. Kepler's equation solved by Newton method 
  2.  --Beware of e very close to 1!-- 
  3. Initial eccentric anom           =      280.0000000000000000 
  4. Input mean anom                  =      286.8792980000000000 
  5. Input maximum its                =      15 
  6. Input stop tolerance             =        0.0000010000000000 
  7. Input eccentricity               =        0.1000000000000000 
  8. Final eccentric anom             =      281.2600076068777000 
  9. Mean anom computed from solution =      286.8792979999999000 
  10.