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: 00CO104
# Created Fri May 2 02:36:30 2008
# Orbit generated from Bernstein formalism
# Fitting 12 observations of 12
# Arc: 4.04y
# First observation: 2000/02/06
# Last observation: 2004/02/22
Preliminary a, adot, b, bdot, g, gdot:
-0.000729 0.075726 0.000032 -0.003626 0.050974 0.000000
# Chi-squared of fit: 9.33 DOF: 18 RMS: 0.16
# Min/Max residuals: -0.32 0.31
# Exact a, adot, b, bdot, g, gdot:
2.367660E-05 7.488284E-02 -2.638295E-06 -3.596490E-03 5.077123E-02 3.143834E-03
# Covariance matrix:
4.5985E-13 -2.6428E-13 -3.4802E-15 8.3940E-15 4.9384E-13 -6.1876E-13
-2.6428E-13 4.6911E-13 8.5324E-15 -2.0282E-14 1.0948E-13 1.4910E-12
-3.4802E-15 8.5324E-15 3.0691E-13 -1.0837E-13 1.1595E-15 3.1405E-14
8.3940E-15 -2.0282E-14 -1.0837E-13 6.3783E-14 -2.0580E-15 -7.4710E-14
4.9384E-13 1.0948E-13 1.1595E-15 -2.0580E-15 3.1188E-12 1.4161E-13
-6.1876E-13 1.4910E-12 3.1405E-14 -7.4710E-14 1.4161E-13 5.4931E-12
# lat0 lon0 xBary yBary zBary JD0
1.459819 146.806046 0.164484 0.024633 -0.975031 2451580.824873
# Heliocentric elements and errors
Epoch: 2451580.5000 = 2000/02/06
Mean Anomaly: 11.99774 +/- 0.012
Argument of Peri: 136.81235 +/- 0.016
Long of Asc Node: 353.24780 +/- 0.001
Inclination: 3.07078 +/- 0.000
Eccentricity: 0.14649598 +/- 0.0001
Semi-Major Axis: 24.09177740 +/- 0.0041
Time of Perihelion: 2450141.0428 +/- 1.4
Perihelion: 20.56242875 +/- 0.0045
Aphelion: 27.62112605 +/- 0.0055
Period (y) 118.2528 +/- 0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -17.19631621 +/- 0.0006
Ecliptic Y 11.45395789 +/- 0.0004
Ecliptic Z 0.50173849 +/- 0.0000
Ecliptic XDOT -0.00236238 +/- 0.0000
Ecliptic YDOT -0.00327653 +/- 0.0000
Ecliptic ZDOT -0.00018946 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 20.66780550 +/- 0.0005
Geocenter to KBO 19.69619450 +/- 0.0007
# Hcoef: 10.08
The following table shows the complete astrometric record for 00CO104. 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 (00CO104) followed by the observatory code and reference code for the source of the astrometry.
2000 02 06.32413 09 58 09.33 +13 57 00.2 22.8R 00CO104 695 Cb1114 2000 02 06.46317 09 58 08.07 +13 57 06.2 00CO104 695 Cb1114 2000 02 27.14883 09 55 01.34 +14 12 48.8 23.0R 00CO104 695 Cb1114 2000 02 27.24084 09 55 00.50 +14 12 52.7 00CO104 695 Cb1114 2002 02 06.33930 10 30 04.45 +10 31 39.3 22.7R 00CO104 695 Ch5665 2002 02 06.43463 10 30 03.65 +10 31 43.7 00CO104 695 Ch5665 2002 02 08.32953 10 29 47.96 +10 33 13.2 22.9R 00CO104 695 Ch5665 2002 02 08.42655 10 29 47.11 +10 33 17.9 00CO104 695 Ch5665 2002 03 08.49706 10 25 42.73 +10 55 53.9 22.5R 00CO104 568 Ch5665 2002 03 08.52618 10 25 42.49 +10 55 54.8 00CO104 568 Ch5665 2004 02 22.34020 10 58 46.74 +07 10 18.0 23.3R 00CO104 695 Ck0849 2004 02 22.37546 10 58 46.42 +07 10 19.6 00CO104 695 Ck0849
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 -0.07 0.00 0.31 2 0.0004 -19.29 0.04 -0.65 -0.05 3 0.0570 -2894.82 0.08 -42.25 0.11 4 0.0573 -2907.63 -0.03 -42.73 -0.07 5 2.0014 30845.35 -0.04 -1482.62 -0.26 6 2.0017 30832.48 -0.02 -1482.90 -0.32 7 2.0069 30578.91 0.22 -1485.40 -0.02 8 2.0071 30565.23 -0.15 -1485.67 -0.05 9 2.0840 26643.40 -0.19 -1552.26 0.19 10 2.0841 26639.72 0.15 -1552.72 -0.15 11 4.0438 60469.03 0.10 -3027.74 0.28 12 4.0439 60463.58 -0.09 -3028.12 0.01
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.
00CO104 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 24.086 24.086 24.086 ecceobj 0.146 0.146 0.146 incobj 3.071 3.071 3.071 qmin 18.171 20.401 20.282 qmax 32.272 31.058 30.369 amean 24.291 25.692 24.790 amin 23.728 23.740 23.790 amax 25.519 27.881 27.403 emean 0.168 0.094 0.131 emin 0.125 0.002 0.090 emax 0.268 0.192 0.177 imean 4.028 4.158 3.575 imin 3.029 2.625 2.052 imax 4.761 6.816 4.499 fracstop 0.009 0.104 0.023 cjmean 3.004 3.006 3.011 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 171.8 168.2 200.9 kozaiamp 178.4 179.8 179.2