The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory.
# Object: 00AD255 # Created Fri May 2 02:36:30 2008 # Orbit generated from Bernstein formalism # Fitting 18 observations of 18 # Arc: 1.09d # First observation: 2000/01/01 # Last observation: 2000/01/02 # WARNING Fitting with energy constraint # WARNING and with gdot fixed = 0 # Chi-squared of fit: 8.97 DOF: 32 RMS: 0.12 # Min/Max residuals: -0.32 0.22 # Exact a, adot, b, bdot, g, gdot: 1.322243E-05 2.247722E-02 8.322136E-06 1.138874E-02 2.524150E-02 0.000000E+00 # Covariance matrix: 6.4123E-11 1.0133E-07 -9.2799E-12 -1.4944E-08 1.7193E-08 0.0000E+00 1.0133E-07 1.6043E-04 -1.4684E-08 -2.3647E-05 2.7205E-05 0.0000E+00 -9.2799E-12 -1.4684E-08 1.4267E-12 2.1599E-09 -2.4913E-09 0.0000E+00 -1.4944E-08 -2.3647E-05 2.1599E-09 3.5741E-06 -4.0120E-06 0.0000E+00 1.7193E-08 2.7205E-05 -2.4913E-09 -4.0120E-06 4.6157E-06 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 2.1163E-04 # lat0 lon0 xBary yBary zBary JD0 -20.789792 78.328221 -0.372514 -0.322650 -0.849271 2451544.812233 # Heliocentric elements and errors Epoch: 2451540.5000 = 1999/12/28 Mean Anomaly: 26.25372 +/- 334.286 Argument of Peri: 292.96182 +/- 35.339 Long of Asc Node: 113.12196 +/- 19.239 Inclination: 33.36413 +/- 13.006 Eccentricity: 0.03030664 +/- 0.5881 Semi-Major Axis: 41.59614897 +/- 21.7837 Time of Perihelion: 2444394.4441 +/- 286913.5 Perihelion: 40.33550964 +/- 32.3213 Aphelion: 42.85678830 +/- 33.1993 Period (y) 268.2797 +/- 210.74 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 7.31855356 +/- 0.6380 Ecliptic Y 37.24001067 +/- 3.0872 Ecliptic Z -14.06147450 +/- 1.1968 Ecliptic XDOT -0.00230428 +/- 0.0012 Ecliptic YDOT 0.00093002 +/- 0.0015 Ecliptic ZDOT 0.00115496 +/- 0.0006 # Distances at JD0 (AU) Heliocenter to KBO 40.47350598 +/- 2.8732 Geocenter to KBO 39.61729417 +/- 3.3720 # Hcoef: 8.89
The following table shows the complete astrometric record for 00AD255. 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 (00AD255) followed by the observatory code and reference code for the source of the astrometry.
2000 01 01.31149 05 16 21.51 +02 12 30.7 24.5R 00AD255 568 Cb9120 2000 01 01.33118 05 16 21.38 +02 12 31.2 00AD255 568 Cb9120 2000 01 01.34422 05 16 21.35 +02 12 31.2 24.8R 00AD255 568 Cb9120 2000 01 01.35739 05 16 21.26 +02 12 31.6 24.5R 00AD255 568 Cb9120 2000 01 01.37054 05 16 21.20 +02 12 31.6 24.4R 00AD255 568 Cb9120 2000 01 01.38365 05 16 21.15 +02 12 31.9 24.7R 00AD255 568 Cb9120 2000 01 01.39682 05 16 21.08 +02 12 31.9 00AD255 568 Cb9120 2000 01 01.40336 05 16 21.04 +02 12 32.2 24.7R 00AD255 568 Cb9120 2000 01 01.41649 05 16 20.98 +02 12 32.3 24.8R 00AD255 568 Cb9120 2000 01 01.42969 05 16 20.89 +02 12 32.4 00AD255 568 Cb9120 2000 01 01.44281 05 16 20.85 +02 12 32.6 00AD255 568 Cb9120 2000 01 01.45652 05 16 20.78 +02 12 32.8 00AD255 568 Cb9120 2000 01 01.46976 05 16 20.70 +02 12 33.0 00AD255 568 Cb9120 2000 01 01.49018 05 16 20.62 +02 12 33.3 24.5R 00AD255 568 Cb9120 2000 01 01.50972 05 16 20.52 +02 12 33.6 24.6R 00AD255 568 Cb9120 2000 01 02.28652 05 16 16.77 +02 12 43.5 24.9R 00AD255 568 Cb9120 2000 01 02.34594 05 16 16.47 +02 12 44.3 00AD255 568 Cb9120 2000 01 02.40519 05 16 16.18 +02 12 45.1 00AD255 568 Cb9120
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 0.18 0.00 -0.24 2 0.0001 -1.90 -0.29 0.66 0.04 3 0.0001 -2.35 0.22 0.69 -0.16 4 0.0001 -3.66 -0.13 1.20 0.10 5 0.0002 -4.56 -0.07 1.27 -0.07 6 0.0002 -5.28 0.17 1.63 0.04 7 0.0002 -6.33 0.08 1.72 -0.12 8 0.0003 -6.90 -0.01 2.06 0.11 9 0.0003 -7.79 0.06 2.23 0.03 10 0.0003 -9.13 -0.32 2.44 0.00 11 0.0004 -9.71 0.06 2.69 0.00 12 0.0004 -10.74 0.03 2.97 0.03 13 0.0004 -11.92 -0.19 3.27 0.08 14 0.0005 -13.09 0.13 3.67 0.09 15 0.0005 -14.56 0.08 4.09 0.15 16 0.0027 -69.79 0.07 18.48 -0.04 17 0.0028 -74.20 -0.04 19.64 -0.02 18 0.0030 -78.47 -0.02 20.79 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.
00AD255 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 42.794 42.794 42.794 ecceobj 0.058 0.058 0.058 incobj 32.707 32.707 32.707 qmin 39.383 39.383 39.383 qmax 45.903 45.900 45.907 amean 42.556 42.556 42.556 amin 42.232 42.229 42.233 amax 42.897 42.897 42.897 emean 0.055 0.055 0.055 emin 0.039 0.039 0.039 emax 0.071 0.071 0.071 imean 31.127 31.127 31.127 imin 30.835 30.835 30.835 imax 31.416 31.417 31.415 fracstop 1.000 1.000 1.000 cjmean 2.741 2.741 2.741 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 173.4 173.4 173.3 kozaiamp 180.0 180.0 180.0