Orbital parameters of (99942) Apophis, solution A


  improved coordinates (AU) and velocities (AU/day)

  2455600.500000000000000 
   4.732916106086960D-001   6.896970329621680D-001  2.687090344441910D-001 
  -1.366808487165656D-002   1.218481485089794D-002  4.182080123361198D-003

  mean errors of coordinates and velocities 

  0.1744625011D-06          0.1456622166D-06        0.5366439414D-07   
  0.2538718092D-08          0.3563550979D-08        0.1403304296D-08   


   
  covariance matrix for coordinates and velocities (DSIG=  9.692542295080200D-001)

   .32398789D-13 -.26923066D-13 -.96386917D-14  .47119950D-15  .65809804D-15  .25534335D-15
  -.26923066D-13  .22584913D-13  .79878887D-14 -.39230662D-15 -.55235513D-15 -.21331152D-15
  -.96386917D-14  .79878887D-14  .30654699D-14 -.14009470D-15 -.19604688D-15 -.78858435D-16
   .47119950D-15 -.39230662D-15 -.14009470D-15  .68604649D-17  .95935504D-17  .37244746D-17
   .65809804D-15 -.55235513D-15 -.19604688D-15  .95935504D-17  .13517318D-16  .52255962D-17
   .25534335D-15 -.21331152D-15 -.78858435D-16  .37244746D-17  .52255962D-17  .20961787D-17

  

  elements M,Peri,Node,Incl,e,n   
  (degrees with the exception of e)

  2455600.500000000000000 
  65.030524581169000        126.424999255817300      204.431297971423600 
  3.331901677567745         1.911152687318415D-001     1.112755711713546

  mean errors of elements 

  1.305061494250017D-005    2.097279426367224D-005   2.099915584962974D-005
  4.631713865484807D-007    1.643845069533824D-008   5.873444407951790D-009