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: 00CG105
# Created Fri May 2 02:36:30 2008
# Orbit generated from Bernstein formalism
# Fitting 16 observations of 16
# Arc: 2.01y
# First observation: 2000/02/05
# Last observation: 2002/02/07
Preliminary a, adot, b, bdot, g, gdot:
-0.000054 0.017855 0.000033 -0.009474 0.021891 0.000000
# Chi-squared of fit: 18.84 DOF: 26 RMS: 0.19
# Min/Max residuals: -0.39 0.44
# Exact a, adot, b, bdot, g, gdot:
1.137020E-05 1.787916E-02 -7.007226E-06 -9.503204E-03 2.199617E-02 7.844253E-04
# Covariance matrix:
3.3077E-13 -3.5258E-13 -2.1967E-14 8.5629E-14 -6.7531E-14 -4.6613E-12
-3.5258E-13 9.6237E-13 1.1015E-13 -4.3049E-13 5.9111E-13 2.3424E-11
-2.1967E-14 1.1015E-13 3.1064E-13 -2.6932E-13 8.3549E-14 3.4391E-12
8.5629E-14 -4.3049E-13 -2.6932E-13 4.5771E-13 -3.2788E-13 -1.3438E-11
-6.7531E-14 5.9111E-13 8.3549E-14 -3.2788E-13 7.5707E-13 1.7828E-11
-4.6613E-12 2.3424E-11 3.4391E-12 -1.3438E-11 1.7828E-11 7.3121E-10
# lat0 lon0 xBary yBary zBary JD0
0.189011 133.668777 -0.041451 0.003050 -0.987915 2451579.677003
# Heliocentric elements and errors
Epoch: 2451570.5000 = 2000/01/27
Mean Anomaly: 89.95876 +/- 0.217
Argument of Peri: 84.69153 +/- 0.198
Long of Asc Node: 314.05896 +/- 0.000
Inclination: 28.00051 +/- 0.001
Eccentricity: 0.04305592 +/- 0.0013
Semi-Major Axis: 46.36238608 +/- 0.0066
Time of Perihelion: 2422757.5277 +/- 69.2
Perihelion: 44.36621113 +/- 0.0617
Aphelion: 48.35856104 +/- 0.0618
Period (y) 315.6871 +/- 0.07
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -32.09668258 +/- 0.0012
Ecliptic Y 33.57346807 +/- 0.0013
Ecliptic Z 0.14966216 +/- 0.0000
Ecliptic XDOT -0.00168552 +/- 0.0000
Ecliptic YDOT -0.00145603 +/- 0.0000
Ecliptic ZDOT -0.00118243 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 46.44778994 +/- 0.0013
Geocenter to KBO 45.46245328 +/- 0.0018
# Hcoef: 6.47
The following table shows the complete astrometric record for 00CG105. 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 (00CG105) followed by the observatory code and reference code for the source of the astrometry.
2000 02 05.17626 09 04 46.05 +16 54 11.3 22.6R 00CG105 695 Cb1115 2000 02 05.29149 09 04 45.48 +16 54 13.1 00CG105 695 Cb1115 2000 02 27.11346 09 03 06.31 +16 59 14.6 22.6R 00CG105 695 Cb1115 2000 02 27.20388 09 03 05.91 +16 59 16.0 00CG105 695 Cb1115 2000 12 21.63597 09 11 18.70 +15 55 43.8 00CG105 568 Cc3758 2000 12 22.56729 09 11 15.75 +15 55 51.6 23.1R 00CG105 568 Cc3758 2000 12 22.62420 09 11 15.57 +15 55 52.0 00CG105 568 Cc3758 2001 03 12.05788 09 05 38.54 +16 13 07.3 22.5 00CG105 304 Ce8743 2001 03 12.12751 09 05 38.28 +16 13 08.1 00CG105 304 Ce8743 2001 03 25.16397 09 04 56.61 +16 15 01.2 24.6R 00CG105 695 Cd0020 2001 03 25.25215 09 04 56.33 +16 15 01.7 00CG105 695 Cd0020 2001 04 26.25592 09 04 07.89 +16 15 51.6 23.0R 00CG105 568 Cd0809 2001 04 27.25990 09 04 07.78 +16 15 47.4 00CG105 568 Cd0809 2002 02 06.19986 09 11 29.45 +15 16 24.2 22.5R 00CG105 695 Ce8743 2002 02 06.28876 09 11 29.07 +15 16 25.6 00CG105 695 Ce8743 2002 02 07.22347 09 11 24.67 +15 16 39.5 00CG105 695 Ce8743
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 0.31 0.00 0.04 2 0.0003 -8.35 0.01 -0.62 0.05 3 0.0601 -1458.13 0.02 -118.76 -0.01 4 0.0603 -1464.03 -0.21 -119.05 0.20 5 0.8774 6427.91 0.03 -1712.50 -0.15 6 0.8799 6384.91 -0.19 -1717.58 -0.05 7 0.8801 6382.31 -0.08 -1717.97 -0.09 8 1.0976 1431.49 -0.03 -2142.98 -0.08 9 1.0977 1427.67 -0.11 -2143.29 -0.03 10 1.1334 820.33 0.44 -2207.61 0.22 11 1.1337 816.32 0.05 -2208.29 0.00 12 1.2213 133.72 -0.39 -2360.55 -0.29 13 1.2240 133.41 -0.01 -2365.02 -0.11 14 2.0042 7273.48 -0.11 -3923.29 0.15 15 2.0044 7267.80 0.43 -3923.57 0.35 16 2.0070 7202.78 -0.18 -3929.04 -0.20
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.
00CG105 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 46.350 46.350 46.350 ecceobj 0.043 0.043 0.043 incobj 28.005 28.005 28.005 qmin 43.899 43.893 43.907 qmax 49.031 49.021 49.036 amean 46.384 46.384 46.383 amin 46.018 46.022 46.017 amax 46.742 46.744 46.746 emean 0.039 0.039 0.039 emin 0.029 0.029 0.029 emax 0.049 0.049 0.049 imean 29.380 29.380 29.380 imin 29.180 29.178 29.180 imax 29.581 29.581 29.583 fracstop 1.000 1.000 1.000 cjmean 2.810 2.810 2.810 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 184.1 183.9 184.2 kozaiamp 180.0 180.0 180.0