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: 00CJ105
# Created Fri May 2 02:36:30 2008
# Orbit generated from Bernstein formalism
# Fitting 18 observations of 18
# Arc: 7.03y
# First observation: 2000/02/05
# Last observation: 2007/02/15
Preliminary a, adot, b, bdot, g, gdot:
-0.000114 0.018232 0.000011 0.003699 0.021056 0.000000
# Chi-squared of fit: 37.96 DOF: 30 RMS: 0.26
# Min/Max residuals: -0.69 0.56
# Exact a, adot, b, bdot, g, gdot:
1.434813E-05 1.832689E-02 2.597699E-06 3.723850E-03 2.142764E-02 1.573152E-03
# Covariance matrix:
3.2054E-13 -8.3046E-14 4.0034E-15 -6.2352E-15 2.0156E-13 -2.5891E-13
-8.3046E-14 1.9349E-13 -2.6414E-14 3.9244E-14 2.2252E-13 1.5773E-12
4.0034E-15 -2.6414E-14 2.0299E-13 -4.3719E-14 -3.8438E-14 -2.3303E-13
-6.2352E-15 3.9244E-14 -4.3719E-14 2.0891E-14 5.6438E-14 3.4587E-13
2.0156E-13 2.2252E-13 -3.8438E-14 5.6438E-14 8.7239E-13 2.2490E-12
-2.5891E-13 1.5773E-12 -2.3303E-13 3.4587E-13 2.2490E-12 1.3891E-11
# lat0 lon0 xBary yBary zBary JD0
1.553383 162.170509 0.431150 0.023902 -0.889599 2451579.921233
# Heliocentric elements and errors
Epoch: 2451570.5000 = 2000/01/27
Mean Anomaly: 131.01216 +/- 0.076
Argument of Peri: 227.78813 +/- 0.069
Long of Asc Node: 154.20503 +/- 0.000
Inclination: 11.61428 +/- 0.000
Eccentricity: 0.11108563 +/- 0.0002
Semi-Major Axis: 44.06312408 +/- 0.0055
Time of Perihelion: 2412691.0197 +/- 21.2
Perihelion: 39.16834418 +/- 0.0084
Aphelion: 48.95790398 +/- 0.0092
Period (y) 292.4968 +/- 0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -45.11937731 +/- 0.0019
Ecliptic Y 14.96935101 +/- 0.0006
Ecliptic Z 1.26525057 +/- 0.0001
Ecliptic XDOT -0.00090166 +/- 0.0000
Ecliptic YDOT -0.00216448 +/- 0.0000
Ecliptic ZDOT 0.00048118 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 47.55460585 +/- 0.0018
Geocenter to KBO 46.66868683 +/- 0.0020
# Hcoef: 5.86
The following table shows the complete astrometric record for 00CJ105. 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 (00CJ105) followed by the observatory code and reference code for the source of the astrometry.
2000 02 05.42049 10 56 37.95 +08 25 52.0 21.9R 00CJ105 695 Cb1115 2000 02 05.52549 10 56 37.57 +08 25 54.5 00CJ105 695 Cb1115 2000 03 01.30425 10 55 00.83 +08 36 58.6 21.9R 00CJ105 695 Cb1115 2000 03 01.38808 10 55 00.52 +08 37 00.8 00CJ105 695 Cb1115 2000 03 01.39586 10 55 00.45 +08 37 01.2 00CJ105 695 Cb1115 2001 03 25.17406 10 57 42.23 +08 35 02.5 22.8R 00CJ105 695 Ch1183 2002 02 08.37609 11 04 53.91 +08 02 29.8 22.2R 00CJ105 695 Cg5554 2002 02 08.50852 11 04 53.42 +08 02 33.2 00CJ105 695 Cg5554 2002 04 11.20322 11 00 58.78 +08 28 51.4 21.3R 00CJ105 695 Cg5554 2002 04 11.26419 11 00 58.60 +08 28 52.5 00CJ105 695 Cg5554 2004 03 19.20061 11 10 46.49 +07 54 50.0 23.0R 00CJ105 688 Ck2009 2004 03 19.29196 11 10 46.12 +07 54 52.5 00CJ105 688 Ck2009 2006 01 16.28522 11 22 46.153 +07 02 23.33 22.2R 00CJ105 500 2006 01 16.28962 11 22 46.140 +07 02 23.44 00CJ105 500 2006 01 16.29402 11 22 46.131 +07 02 23.51 00CJ105 500 2006 01 16.35114 11 22 46.013 +07 02 24.58 00CJ105 500 2007 02 15.40023 11 25 28.27 +07 00 53.6 23.1R 00CJ105 688 Cu2276 2007 02 15.47470 11 25 27.95 +07 00 55.6 00CJ105 688 Cu2276
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 -0.17 0.00 0.03 2 0.0003 -6.17 -0.10 0.15 -0.10 3 0.0681 -1586.14 0.00 65.13 -0.09 4 0.0684 -1591.23 0.56 65.41 0.04 5 0.0684 -1592.35 -0.03 65.39 0.00 6 1.1328 669.92 0.42 873.85 0.10 7 2.0095 7337.82 -0.36 1542.89 -0.06 8 2.0098 7329.79 -0.44 1543.20 -0.11 9 2.1787 3504.57 -0.41 1652.25 0.06 10 2.1789 3501.68 -0.19 1652.24 0.04 11 4.1171 12353.69 0.37 3161.53 0.21 12 4.1174 12347.63 0.26 3161.68 0.28 13 5.9462 23520.15 0.25 4501.07 -0.20 14 5.9463 23519.93 0.19 4501.09 -0.20 15 5.9463 23519.77 0.19 4501.10 -0.21 16 5.9464 23517.71 0.20 4501.38 -0.20 17 7.0280 25804.37 -0.02 5388.53 0.34 18 7.0282 25799.12 -0.69 5388.46 0.06
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.
00CJ105 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 44.063 44.063 44.063 ecceobj 0.111 0.111 0.111 incobj 11.616 11.616 11.616 qmin 38.561 38.549 38.537 qmax 50.173 50.197 50.238 amean 44.221 44.220 44.221 amin 43.864 43.862 43.860 amax 44.600 44.622 44.627 emean 0.112 0.111 0.112 emin 0.098 0.099 0.098 emax 0.126 0.126 0.126 imean 10.918 10.917 10.916 imin 10.337 10.337 10.337 imax 11.532 11.531 11.530 fracstop 1.000 1.000 1.000 cjmean 3.046 3.046 3.046 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 187.8 187.6 187.8 kozaiamp 180.0 179.9 180.0