The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory. Take special note that while the original Bernstein software works with barycentric coordinates, we convert these results into a heliocentric coordinate system.
# Object: 02FV6 # Created Thu May 24 01:37:11 2012 # Orbit generated from Bernstein formalism # Fitting 13 observations of 16 # Arc: 2.97y # First observation: 2002/03/20 # Last observation: 2005/03/10 Preliminary a, adot, b, bdot, g, gdot: -0.000010 0.015391 0.000000 -0.000677 0.018967 0.000000 # Chi-squared of fit: 10.03 DOF: 20 RMS: 0.16 # Min/Max residuals: -0.47 0.22 # Exact a, adot, b, bdot, g, gdot: 1.283237E-05 1.542941E-02 -7.391254E-07 -6.792145E-04 1.922095E-02 1.376696E-03 # Covariance matrix: 2.5518E-13 -2.3091E-13 -2.1085E-15 5.4057E-15 2.9410E-13 -2.6024E-12 -2.3091E-13 1.1261E-12 7.0346E-15 -4.3615E-14 6.4773E-13 2.2805E-11 -2.1085E-15 7.0346E-15 1.8024E-13 -8.4629E-14 -3.4052E-15 1.4362E-13 5.4057E-15 -4.3615E-14 -8.4629E-14 1.0868E-13 -3.3929E-14 -9.8662E-13 2.9410E-13 6.4773E-13 -3.4052E-15 -3.3929E-14 3.1916E-12 1.9349E-11 -2.6024E-12 2.2805E-11 1.4362E-13 -9.8662E-13 1.9349E-11 5.1867E-10 # lat0 lon0 xBary yBary zBary JD0 -1.828801 168.054261 -0.202676 -0.031210 -0.975410 2452353.790823 # Heliocentric elements and errors Epoch: 2452350.5000 = 2002/03/17 Mean Anomaly: 136.89483 +/- 0.408 Argument of Peri: 68.14975 +/- 0.396 Long of Asc Node: 312.63415 +/- 0.013 Inclination: 3.07929 +/- 0.001 Eccentricity: 0.15589044 +/- 0.0007 Semi-Major Axis: 47.17874452 +/- 0.0155 Time of Perihelion: 2407341.1706 +/- 132.3 Perihelion: 39.82402916 +/- 0.0363 Aphelion: 54.53345987 +/- 0.0383 Period (y) 324.0617 +/- 0.16 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -51.86993924 +/- 0.0047 Ecliptic Y 10.77183962 +/- 0.0010 Ecliptic Z -1.66037043 +/- 0.0002 Ecliptic XDOT -0.00065205 +/- 0.0000 Ecliptic YDOT -0.00211141 +/- 0.0000 Ecliptic ZDOT -0.00010274 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 53.00264103 +/- 0.0046 Geocenter to KBO 52.02655986 +/- 0.0048 # Hcoef: 6.81
The following table shows the complete astrometric record for 02FV6. The first three columns show the date of observation. The next six columns are RA and DEC. The next column (when provided) is the observed magnitude and filter. The next column is the object name (02FV6) followed by the observatory code and reference code for the source of the astrometry.
2002 03 20.29008 11 13 11.99 +03 02 19.7 24.0R 02FV6 568 Cf5861 2002 03 20.32480 11 13 11.87 +03 02 20.5 24.2R 02FV6 568 Cf5861 2002 03 20.35929 11 13 11.74 +03 02 21.3 23.9R 02FV6 568 Cf5861 2002 03 22.32156 11 13 04.70 +03 03 05.7 23.1R 02FV6 568 Cf5861 2002 03 22.35862 11 13 04.57 +03 03 06.6 23.2R 02FV6 568 Cf5861 2002 03 22.41437 11 13 04.35 +03 03 08.0 02FV6 568 Cf5861 2002 06 03.17224 11 10 38.89 +03 19 57.9 24. R 02FV6 675 Cf8969 2002 06 04.20833 11 10 39.12 +03 19 57.4 02FV6 675 Cf8969 2002 06 07.20417 11 10 40.22 +03 19 57.0 02FV6 675 Cf8969 2002 06 08.23045 11 10 40.69 +03 19 55.5 24. R 02FV6 675 Cf8969 2003 03 30.19290 11 15 50.16 +02 43 06.9 23.7R 02FV6 695 Ch8263 2003 03 30.28934 11 15 49.82 +02 43 09.1 02FV6 695 Ch8263 2003 03 31.29162 11 15 46.39 +02 43 31.5 02FV6 695 Ch8263 2003 03 31.33598 11 15 46.28 +02 43 32.2 02FV6 695 Ch8263 2005 03 10.31173 11 23 22.39 +01 50 05.5 23.3R 02FV6 695 Cn0182 2005 03 10.44558 11 23 21.90 +01 50 08.7 02FV6 695 Cn0182
The following table shows the residuals to the orbit fit. The first coumn is the point number. The second column is the time, in years, measured from the first observation. The third and fifth columns are the regularized positions used in the orbit fit. The fourth and sixth columns are the residuals, in arc seconds, for RA and Dec respectively.
1 0.0000 0.00 -0.03 0.00 0.04 2 0.0001 -1.97 0.07 0.04 0.08 3 0.0002 -4.07 0.01 0.01 0.07 4 0.0056 -118.49 0.05 -0.19 -0.26 5 0.0057 -120.63 0.09 -0.12 -0.18 6 0.0058 -124.21 -0.20 -0.11 -0.16 7 0.2050 -2524.16 ( -0.41) 81.72 ( 1.00) 8 0.2079 -2520.79 0.01 82.60 0.13 9 0.2161 -2505.46 ( 0.00) 88.64 ( 1.07) 10 0.2189 -2498.39 ( -0.47) 90.00 ( 0.69) 11 1.0264 2631.65 0.18 -137.45 0.00 12 1.0267 2626.10 0.08 -137.41 0.03 13 1.0294 2570.03 -0.47 -136.84 0.20 14 1.0296 2568.24 0.22 -136.84 0.20 15 2.9734 10121.96 -0.04 -416.63 -0.16 16 2.9737 10113.93 0.04 -416.56 0.00
The following table comes from a 10My integration of the orbit of the object. Three columns are shown. The first column is the result of integrating the nominal orbit. The other two columns are based on clones of the nominal orbit that are +/- 3 sigma from the nominal orbit. If all three types agree then the classificiation is deemed secure. The basis for these calculations is described in more detail in AJ, 129, 1117 (2005). Any use made of these calculations should refer to and credit this publication and the Deep Ecliptic Survey Team.
02FV6 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 46.879 46.925 46.834 ecceobj 0.161 0.162 0.161 incobj 3.091 3.091 3.091 qmin 39.260 39.250 39.263 qmax 54.957 55.064 54.837 amean 47.037 47.083 46.991 amin 46.998 47.041 46.945 amax 47.117 47.166 47.071 emean 0.158 0.159 0.157 emin 0.150 0.150 0.149 emax 0.167 0.168 0.165 imean 4.456 4.450 4.462 imin 3.890 3.898 3.892 imax 5.002 4.999 4.999 excite_mean 0.176 0.177 0.176 fracstop 1.000 1.000 1.000 cjmean 3.101 3.101 3.100 libcent 0 -180.0 -180.0 -180.0 libamp 0 -180.0 -180.0 -180.0 libcent 1 -180.0 -180.0 -180.0 libamp 1 -180.0 -180.0 -180.0 libcent 2 -180.0 -180.0 -180.0 libamp 2 -180.0 -180.0 -180.0 libcent 3 -180.0 -180.0 -180.0 libamp 3 -180.0 -180.0 -180.0 libcent 4 -180.0 -180.0 -180.0 libamp 4 -180.0 -180.0 -180.0 kozaimean 178.0 178.0 178.0 kozaiamp 180.0 180.0 180.0