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: 00CL105
# Created Fri May 2 02:36:30 2008
# Orbit generated from Bernstein formalism
# Fitting 19 observations of 19
# Arc: 8.16y
# First observation: 2000/02/06
# Last observation: 2008/04/04
Preliminary a, adot, b, bdot, g, gdot:
0.000034 0.020697 -0.000005 0.001415 0.022823 0.000000
# Chi-squared of fit: 131.29 DOF: 32 RMS: 0.46
# Min/Max residuals: -2.02 0.66
# Exact a, adot, b, bdot, g, gdot:
1.429731E-05 2.072367E-02 -1.744180E-06 1.414998E-03 2.270751E-02 -3.804707E-05
# Covariance matrix:
2.7484E-13 -1.5445E-13 8.8546E-15 -1.0089E-14 1.2928E-13 -9.2290E-13
-1.5445E-13 1.8375E-13 -1.0210E-14 1.2365E-14 8.5793E-14 1.0880E-12
8.8546E-15 -1.0210E-14 1.3645E-13 -2.8948E-14 2.8794E-16 -6.8546E-14
-1.0089E-14 1.2365E-14 -2.8948E-14 1.4546E-14 2.3547E-15 8.1402E-14
1.2928E-13 8.5793E-14 2.8794E-16 2.3547E-15 8.6495E-13 5.7388E-14
-9.2290E-13 1.0880E-12 -6.8546E-14 8.1402E-14 5.7388E-14 7.2518E-12
# lat0 lon0 xBary yBary zBary JD0
1.516677 134.375288 -0.048774 0.025935 -0.987561 2451580.793733
# Heliocentric elements and errors
Epoch: 2451580.5000 = 2000/02/06
Mean Anomaly: 176.53027 +/- 0.159
Argument of Peri: 203.99337 +/- 0.154
Long of Asc Node: 113.65074 +/- 0.002
Inclination: 4.17503 +/- 0.000
Eccentricity: 0.04643756 +/- 0.0001
Semi-Major Axis: 43.02842209 +/- 0.0064
Time of Perihelion: 2504120.9121 +/- 44.3
Perihelion: 41.03028695 +/- 0.0078
Aphelion: 45.02655723 +/- 0.0082
Period (y) 282.2548 +/- 0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -31.50688918 +/- 0.0013
Ecliptic Y 32.14105267 +/- 0.0013
Ecliptic Z 1.16553543 +/- 0.0001
Ecliptic XDOT -0.00178529 +/- 0.0000
Ecliptic YDOT -0.00174682 +/- 0.0000
Ecliptic ZDOT 0.00017053 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 45.02321407 +/- 0.0013
Geocenter to KBO 44.03829803 +/- 0.0018
# Hcoef: 6.34
The following table shows the complete astrometric record for 00CL105. 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 (00CL105) followed by the observatory code and reference code for the source of the astrometry.
2000 02 06.29299 09 09 12.91 +17 58 09.0 22.4R 00CL105 695 Cb1115 2000 02 06.42211 09 09 12.29 +17 58 11.6 00CL105 695 Cb1115 2000 02 27.13600 09 07 38.81 +18 05 05.1 22.8R 00CL105 695 Cb1115 2000 02 27.23388 09 07 38.39 +18 05 07.2 00CL105 695 Cb1115 2001 02 03.33464 09 14 15.38 +17 40 55.1 00CL105 568 Cc6636 2001 02 03.35658 09 14 15.27 +17 40 55.8 00CL105 568 Cc6636 2001 02 04.42686 09 14 10.27 +17 41 19.1 00CL105 568 Cc6636 2001 02 04.44906 09 14 10.16 +17 41 19.3 00CL105 568 Cc6636 2001 03 24.13664 09 10 57.48 +17 55 29.0 22.9R 00CL105 695 Cc7839 2001 03 24.31185 09 10 56.98 +17 55 31.1 00CL105 695 Cc7839 2001 03 26.07167 09 10 52.11 +17 55 49.4 21.0 00CL105 304 Ce8743 2001 03 26.09589 09 10 51.97 +17 55 49.3 00CL105 304 Ce8743 2002 02 04.50305 09 19 02.81 +17 24 20.7 22.8R 00CL105 568 Cf1711 2002 02 04.56093 09 19 02.52 +17 24 22.0 00CL105 568 Cf1711 2002 02 05.49569 09 18 58.20 +17 24 42.4 00CL105 568 Cf1711 2004 03 18.19922 09 25 45.00 +17 03 17.3 23.5R 00CL105 688 Ck2009 2004 03 18.28374 09 25 44.72 +17 03 18.9 00CL105 688 Ck2009 2008 04 04.14119 09 43 59.39 +15 53 33.7 23.6R 00CL105 688 Cy5651 2008 04 04.23319 09 43 59.14 +15 53 34.9 00CL105 688 Cy5651
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 0.56 2 0.0004 -9.22 -0.04 -0.10 0.42 3 0.0571 -1405.23 -0.23 6.86 0.29 4 0.0573 -1411.57 -0.31 7.13 0.58 5 0.9940 4432.49 0.21 289.48 -0.09 6 0.9940 4430.78 0.05 289.68 0.09 7 0.9969 4355.59 -0.13 290.56 0.14 8 0.9970 4354.03 -0.11 290.28 -0.14 9 1.1276 1473.47 0.04 285.13 0.16 10 1.1280 1466.03 0.15 285.04 0.28 11 1.1329 1394.22 0.66 282.05 -1.36 12 1.1329 1392.34 -0.23 281.36 -2.02 13 1.9965 8656.19 0.19 582.86 0.32 14 1.9966 8651.84 -0.06 582.83 0.27 15 1.9992 8586.61 0.16 583.41 0.12 16 4.1120 14545.74 -0.27 1163.68 -0.05 17 4.1122 14541.41 -0.17 1163.95 0.32 18 8.1584 31000.83 0.10 2320.77 -0.01 19 8.1586 30996.94 -0.03 2320.69 0.11
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.
00CL105 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 43.019 43.019 43.019 ecceobj 0.047 0.047 0.047 incobj 4.175 4.175 4.175 qmin 40.186 40.185 40.187 qmax 46.136 46.139 46.135 amean 43.069 43.069 43.069 amin 42.739 42.739 42.739 amax 43.422 43.422 43.422 emean 0.046 0.046 0.046 emin 0.025 0.025 0.025 emax 0.063 0.063 0.063 imean 2.870 2.870 2.870 imin 1.864 1.864 1.864 imax 3.833 3.834 3.832 fracstop 1.000 1.000 1.000 cjmean 3.085 3.085 3.085 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 175.9 176.0 176.0 kozaiamp 180.0 180.0 180.0