The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory. Take special note that while the original Bernstein software works with barycentric coordinates, we convert these results into a heliocentric coordinate system.
# Object: 612802
# Created Sun Dec 22 02:07:47 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 56 observations of 56
# Arc: 10.01y
# First observation: 2004/08/17
# Last observation: 2014/08/22
# Chi-squared of fit: 129.54 DOF: 106 RMS: 0.27
# Min/Max residuals: -0.77 0.43
# Exact a, adot, b, bdot, g, gdot:
2.312456E-05 7.039413E-02 8.248489E-06 2.723990E-02 4.976380E-02 -2.578223E-04
# Covariance matrix:
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00
# lat0 lon0 xBary yBary zBary JD0
4.592009 -153.010164 -0.900054 -0.037760 0.470860 2453234.745969
# Heliocentric elements and errors
Epoch: 2453234.5000 = 2004/08/17
Mean Anomaly: 13.04251 +/- 0.000
Argument of Peri: 355.05474 +/- 0.000
Long of Asc Node: 197.52992 +/- 0.000
Inclination: 21.42538 +/- 0.000
Eccentricity: 0.15321876 +/- 0.0000
Semi-Major Axis: 23.05358094 +/- 0.0000
Time of Perihelion: 2451769.7456 +/- 0.0
Perihelion: 19.52133988 +/- 0.0000
Aphelion: 26.58582201 +/- 0.0000
Period (y) 110.6919 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -17.02334927 +/- 0.0000
Ecliptic Y -9.67723707 +/- 0.0000
Ecliptic Z 1.60899566 +/- 0.0000
Ecliptic XDOT 0.00187524 +/- 0.0000
Ecliptic YDOT -0.00339720 +/- 0.0000
Ecliptic ZDOT 0.00149282 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 19.64768259 +/- 0.0000
Geocenter to KBO 20.09496237 +/- 0.0000
# Hcoef: 9.55
The following table shows the complete astrometric record for 612802. 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 (612802) followed by the observatory code and reference code for the source of the astrometry.
2004 08 17.245226 13 46 49.990 -06 06 47.11 22.5R 612802 568 Cr7042 2004 08 17.250818 13 46 50.035 -06 06 47.43 22.5R 612802 568 Cr7042 2004 08 17.256398 13 46 50.080 -06 06 47.66 22.5R 612802 568 Cr7042 2004 08 19.239096 13 47 05.745 -06 08 10.03 23.0 612802 568 Cr7042 2004 08 19.249891 13 47 05.830 -06 08 10.70 23.7 612802 568 Cr7042 2004 08 19.260848 13 47 05.903 -06 08 11.11 23.4 612802 568 Cr7042 2004 08 21.250134 13 47 22.254 -06 09 36.48 23.7 612802 568 Cr7042 2004 08 21.261069 13 47 22.334 -06 09 37.06 612802 568 Cr7042 2004 08 23.248911 13 47 39.236 -06 11 05.62 612802 568 Cr7042 2004 08 23.253883 13 47 39.290 -06 11 05.81 23.3 612802 568 Cr7042 2004 08 23.258984 13 47 39.345 -06 11 05.97 612802 568 Cr7042 2006 04 29.561584 14 26 57.863 -06 23 49.57 21.9R 612802 568 Ct2200 2006 04 29.588941 14 26 57.615 -06 23 47.89 21.9R 612802 568 Ct2200 2006 04 30.533561 14 26 49.229 -06 22 50.80 22.0R 612802 568 Ct2200 2006 04 30.575337 14 26 48.853 -06 22 48.31 22.1R 612802 568 Ct2200 2006 07 27.300962 14 20 01.883 -05 49 01.03 22.0R 612802 568 Ct2200 2006 07 27.319348 14 20 01.917 -05 49 01.42 22.0R 612802 568 Ct2200 2006 07 27.339338 14 20 01.963 -05 49 01.90 22.0R 612802 568 Ct2200 2007 04 15.288727 14 47 28.90 -06 30 42.6 22.7V 612802 645 C~1rRC 2007 04 15.289549 14 47 28.89 -06 30 42.6 612802 645 C~1rRC 2007 04 15.292037 14 47 28.88 -06 30 42.4 612802 645 C~1rRC 2007 04 20.31546 14 46 46.64 -06 25 24.9 21.6r 612802 705 C~0nKE 2007 04 20.315802 14 46 46.64 -06 25 25.1 22.3V 612802 645 C~1rRC 2007 04 20.31629 14 46 46.64 -06 25 24.7 612802 705 C~0nKE 2007 04 20.316631 14 46 46.63 -06 25 25.0 22.2V 612802 645 C~1rRC 2007 04 20.31878 14 46 46.62 -06 25 24.5 612802 705 C~0nKE 2007 04 20.319119 14 46 46.61 -06 25 24.9 23.1V 612802 645 C~1rRC 2007 06 14.22069 14 39 20.59 -05 42 44.6 23.1R 612802 688 Cv1058 2007 06 14.25391 14 39 20.38 -05 42 43.8 612802 688 Cv1058 2007 06 15.295645 14 39 14.293 -05 42 19.94 22.2R 612802 568 Cv1058 2007 06 15.297767 14 39 14.280 -05 42 19.88 22.2R 612802 568 Cv1058 2008 04 21.500124 15 04 41.834 -06 12 39.50 612802 568 Cy9806 2008 04 21.501656 15 04 41.831 -06 12 39.22 612802 568 Cy9806 2008 04 21.502874 15 04 41.818 -06 12 39.29 612802 568 Cy9806 2008 04 21.504058 15 04 41.808 -06 12 39.14 612802 568 Cy9806 2008 04 21.505084 15 04 41.788 -06 12 39.03 22.8R 612802 568 Cy9806 2008 04 21.506279 15 04 41.787 -06 12 39.11 612802 568 Cy9806 2008 04 21.507338 15 04 41.785 -06 12 39.15 612802 568 Cy9806 2008 04 21.508413 15 04 41.759 -06 12 39.07 612802 568 Cy9806 2008 04 21.509656 15 04 41.747 -06 12 39.05 612802 568 Cy9806 2008 04 21.510815 15 04 41.745 -06 12 39.01 612802 568 Cy9806 2009 06 02.416704 15 16 35.942 -05 26 18.13 22.3R 612802 568 C~0Dov 2009 06 02.420601 15 16 35.911 -05 26 18.06 22.4R 612802 568 C~0Dov 2010 01 21.97894 15 41 10.16 -06 58 12.1 612802 250 S~0M4R 2010 01 21.98132 15 41 10.18 -06 58 12.0 612802 250 S~0M4R 2010 01 21.98413 15 41 10.21 -06 58 12.0 612802 250 S~0M4R 2010 01 21.98652 15 41 10.23 -06 58 12.0 612802 250 S~0M4R 2010 01 21.99160 15 41 10.23 -06 58 12.0 612802 250 S~0M4R 2010 01 21.99715 15 41 10.28 -06 58 11.8 612802 250 S~0M4R 2010 01 22.03505 15 41 10.57 -06 58 11.1 612802 250 S~0M4R 2010 01 22.04060 15 41 10.62 -06 58 11.1 612802 250 S~0M4R 2010 02 20.581937 15 43 40.047 -06 41 52.77 23.4R 612802 568 C~0Dov 2010 07 14.359088 15 29 52.029 -05 04 53.17 22.4R 612802 568 C~0M4R 2011 04 23.578571 15 57 29.496 -05 26 10.93 22.9G 612802 T12 C~4Yrf 2014 08 22.314405 16 34 54.786 -04 13 42.72 22.9R 612802 568 C~17jp 2014 08 22.357948 16 34 54.804 -04 13 44.59 22.9R 612802 568 C~17jp
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 -0.12 0.00 0.13
2 0.0000 0.00 -0.08 0.00 0.04
3 0.0000 0.00 -0.05 0.00 0.04
4 0.0055 0.00 -0.03 0.00 0.03
5 0.0055 0.00 -0.04 0.00 -0.19
6 0.0055 0.00 -0.25 0.00 -0.14
7 0.0110 0.00 0.10 0.00 0.09
8 0.0110 0.00 -0.05 0.00 -0.01
9 0.0164 0.00 -0.18 0.00 -0.21
10 0.0165 0.00 -0.01 0.00 -0.17
11 0.0165 0.00 0.16 0.00 -0.10
12 1.6983 0.00 -0.21 0.00 0.17
13 1.6984 0.00 -0.24 0.00 0.18
14 1.7010 0.00 -0.15 0.00 0.06
15 1.7011 0.00 -0.14 0.00 0.02
16 1.9413 0.00 -0.01 0.00 0.08
17 1.9413 0.00 -0.10 0.00 0.08
18 1.9414 0.00 -0.08 0.00 0.02
19 2.6586 0.00 0.32 0.00 0.18
20 2.6586 0.00 0.27 0.00 0.13
21 2.6586 0.00 0.43 0.00 0.17
22 2.6723 0.00 -0.03 0.00 -0.12
23 2.6723 0.00 0.01 0.00 -0.34
24 2.6723 0.00 0.08 0.00 0.03
25 2.6723 0.00 -0.03 0.00 -0.29
26 2.6723 0.00 0.10 0.00 0.07
27 2.6723 0.00 -0.00 0.00 -0.35
28 2.8227 0.00 -0.01 0.00 0.06
29 2.8227 0.00 -0.13 0.00 0.08
30 2.8256 0.00 0.10 0.00 0.06
31 2.8256 0.00 0.09 0.00 0.07
32 3.6776 0.00 0.19 0.00 0.17
33 3.6776 0.00 0.35 0.00 0.36
34 3.6776 0.00 0.31 0.00 0.21
35 3.6776 0.00 0.31 0.00 0.29
36 3.6776 0.00 0.14 0.00 0.34
37 3.6776 0.00 0.28 0.00 0.19
38 3.6777 0.00 0.39 0.00 0.08
39 3.6777 0.00 0.14 0.00 0.10
40 3.6777 0.00 0.12 0.00 0.04
41 3.6777 0.00 0.24 0.00 0.01
42 4.7917 0.00 0.11 0.00 0.18
43 4.7917 0.00 0.13 0.00 0.13
44 5.4312 0.00 -0.35 0.00 -0.49
45 5.4312 0.00 -0.32 0.00 -0.44
46 5.4312 0.00 -0.20 0.00 -0.50
47 5.4312 0.00 -0.18 0.00 -0.55
48 5.4312 0.00 -0.77 0.00 -0.65
49 5.4312 0.00 -0.67 0.00 -0.56
50 5.4313 0.00 -0.73 0.00 -0.62
51 5.4313 0.00 -0.63 0.00 -0.73
52 5.5122 0.00 -0.01 0.00 0.24
53 5.9059 0.00 0.19 0.00 0.26
54 6.6813 0.00 0.27 0.00 0.10
55 10.0125 0.00 0.30 0.00 0.21
56 10.0126 0.00 0.30 0.00 0.22
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.
612802 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 22.840 22.840 22.840 ecceobj 0.146 0.146 0.146 incobj 21.498 21.498 21.498 qmin 19.033 18.869 18.314 qmax 26.838 26.660 30.028 amean 22.809 21.582 22.806 amin 22.072 20.144 22.008 amax 23.609 23.256 24.601 emean 0.102 0.081 0.146 emin 0.041 0.001 0.111 emax 0.164 0.167 0.238 imean 20.257 19.782 20.396 imin 19.738 16.736 19.307 imax 21.550 21.550 21.550 excite_mean 0.362 0.350 0.379 fracstop 0.110 0.077 0.034 cjmean 2.943 2.983 2.935 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 182.5 165.9 172.8 kozaiamp 179.7 179.1 178.2