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: 00CK105
# Created Fri Nov 22 02:08:04 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 35 observations of 35
# Arc: 23.04y
# First observation: 2000/02/06
# Last observation: 2023/02/20
# Chi-squared of fit: 86.69 DOF: 64 RMS: 0.28
# Min/Max residuals: -0.80 0.59
# Exact a, adot, b, bdot, g, gdot:
1.352041E-05 1.652699E-02 -3.039034E-06 -2.282600E-03 2.106168E-02 6.055086E-04
# Covariance matrix:
1.3279E-13 -2.4875E-14 -5.2544E-15 2.6623E-15 5.8874E-14 -5.3880E-14
-2.4875E-14 9.2923E-15 2.4364E-15 -1.1898E-15 -9.9177E-15 2.3957E-14
-5.2544E-15 2.4364E-15 8.3400E-14 -5.6751E-15 -1.0792E-15 6.8010E-15
2.6623E-15 -1.1898E-15 -5.6751E-15 8.4570E-16 1.1356E-15 -3.3132E-15
5.8874E-14 -9.9177E-15 -1.0792E-15 1.1356E-15 2.4093E-13 -2.4579E-14
-5.3880E-14 2.3957E-14 6.8010E-15 -3.3132E-15 -2.4579E-14 6.6690E-14
# lat0 lon0 xBary yBary zBary JD0
2.131200 131.636154 -0.095696 0.036398 -0.983788 2451580.780463
# Heliocentric elements and errors
Epoch: 2451580.5000 = 2000/02/06
Mean Anomaly: 167.40964 +/- 0.018
Argument of Peri: 353.17586 +/- 0.004
Long of Asc Node: 326.49925 +/- 0.000
Inclination: 8.14463 +/- 0.000
Eccentricity: 0.23245715 +/- 0.0001
Semi-Major Axis: 39.43888785 +/- 0.0027
Time of Perihelion: 2409511.3844 +/- 6.2
Perihelion: 30.27103624 +/- 0.0030
Aphelion: 48.60673946 +/- 0.0040
Period (y) 247.6824 +/- 0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -32.24265942 +/- 0.0007
Ecliptic Y 36.13551970 +/- 0.0008
Ecliptic Z 1.76553033 +/- 0.0000
Ecliptic XDOT -0.00167092 +/- 0.0000
Ecliptic YDOT -0.00135321 +/- 0.0000
Ecliptic ZDOT -0.00029348 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 48.46111358 +/- 0.0008
Geocenter to KBO 47.47960559 +/- 0.0011
# Hcoef: 6.27
The following table shows the complete astrometric record for 00CK105. 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 (00CK105) followed by the observatory code and reference code for the source of the astrometry.
2000 02 06.27972 08 58 53.00 +19 20 30.7 22.7R 00CK105 695 Cb1115 2000 02 06.40899 08 58 52.40 +19 20 32.7 00CK105 695 Cb1115 2000 02 26.16705 08 57 26.66 +19 25 44.4 23.0R 00CK105 695 Cb1115 2000 02 26.25132 08 57 26.32 +19 25 45.6 00CK105 695 Cb1115 2001 02 03.32739 09 02 44.38 +18 56 16.3 00CK105 568 Cc6636 2001 02 03.34939 09 02 44.28 +18 56 16.4 00CK105 568 Cc6636 2001 02 04.41973 09 02 39.45 +18 56 34.9 00CK105 568 Cc6636 2001 02 04.44081 09 02 39.33 +18 56 35.5 00CK105 568 Cc6636 2001 03 13.04359 09 00 09.80 +19 05 37.8 22.7 00CK105 304 Ce8743 2001 03 13.06549 09 00 09.77 +19 05 38.2 00CK105 304 Ce8743 2001 04 26.26970 08 58 51.75 +19 08 23.7 23.2R 00CK105 568 Cd0809 2001 04 27.25118 08 58 51.77 +19 08 19.4 00CK105 568 Cd0809 2001 04 27.36001 08 58 51.78 +19 08 18.9 00CK105 568 Cd0809 2002 02 04.49351 09 06 20.75 +18 32 40.8 22.2R 00CK105 568 Cf1711 2002 02 05.44656 09 06 16.48 +18 32 57.9 00CK105 568 Cf1711 2002 02 05.50379 09 06 16.23 +18 32 59.0 00CK105 568 Cf1711 2005 02 04.223221 09 17 15.77 +17 19 36.5 22.8V 00CK105 645 C~1S6l 2005 02 04.224050 09 17 15.77 +17 19 36.6 22.7V 00CK105 645 C~1S6l 2005 02 04.226538 09 17 15.76 +17 19 36.6 24.6V 00CK105 645 C~1S6l 2005 02 09.20385 09 16 53.60 +17 21 10.0 22.9R 00CK105 688 Cm6694 2005 02 09.32529 09 16 53.07 +17 21 12.4 00CK105 688 Cm6694 2006 12 21.37570 09 27 15.97 +16 16 57.8 22.8R 00CK105 695 Ct5419 2006 12 21.51592 09 27 15.63 +16 16 59.9 00CK105 695 Ct5419 2013 03 13.18565 09 42 57.97 +14 07 36.1 23.0R 00CK105 695 C~0uco 2013 03 14.17857 09 42 54.29 +14 07 53.1 00CK105 695 C~0uco 2013 03 14.26612 09 42 53.97 +14 07 54.9 00CK105 695 C~0uco 2016 01 11.302737 09 57 32.63 +12 27 28.7 00CK105 W84 C~3i9V 2016 01 11.303773 09 57 32.65 +12 27 29.0 00CK105 W84 C~3i9V 2016 01 11.305006 09 57 32.64 +12 27 29.1 00CK105 W84 C~3i9V 2016 01 11.306076 09 57 32.63 +12 27 29.0 00CK105 W84 C~3i9V 2017 03 03.044994 09 57 32.57 +12 17 37.6 00CK105 W84 C~3i9V 2017 03 03.046487 09 57 32.57 +12 17 37.7 00CK105 W84 C~3i9V 2023 02 20.277870 10 18 56.119 +09 27 19.26 23.0G 00CK105 G37 C~6EkO 2023 02 20.329820 10 18 55.882 +09 27 20.40 00CK105 G37 C~6EkO 2023 02 20.382790 10 18 55.649 +09 27 21.22 00CK105 G37 C~6EkO
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 -0.15 0.00 0.33
2 0.0004 0.00 -0.26 0.00 0.13
3 0.0544 0.00 -0.21 0.00 0.15
4 0.0547 0.00 -0.10 0.00 0.16
5 0.9940 0.00 0.08 0.00 -0.20
6 0.9940 0.00 0.09 0.00 -0.49
7 0.9970 0.00 0.14 0.00 -0.80
8 0.9970 0.00 -0.21 0.00 -0.57
9 1.0972 0.00 -0.61 0.00 0.06
10 1.0973 0.00 0.06 0.00 0.22
11 1.2183 0.00 0.44 0.00 0.59
12 1.2210 0.00 0.24 0.00 0.21
13 1.2213 0.00 0.36 0.00 0.19
14 1.9965 0.00 -0.04 0.00 0.11
15 1.9991 0.00 0.09 0.00 0.19
16 1.9992 0.00 0.26 0.00 0.28
17 4.9964 0.00 0.20 0.00 -0.46
18 4.9964 0.00 0.26 0.00 -0.38
19 4.9964 0.00 0.28 0.00 -0.43
20 5.0101 0.00 -0.53 0.00 -0.11
21 5.0104 0.00 -0.29 0.00 0.02
22 6.8723 0.00 -0.43 0.00 0.02
23 6.8727 0.00 0.12 0.00 0.38
24 13.0976 0.00 0.00 0.00 -0.04
25 13.1003 0.00 -0.24 0.00 0.07
26 13.1006 0.00 -0.14 0.00 0.39
27 15.9289 0.00 -0.11 0.00 -0.21
28 15.9289 0.00 0.24 0.00 0.08
29 15.9289 0.00 0.16 0.00 0.16
30 15.9289 0.00 0.06 0.00 0.04
31 17.0699 0.00 0.14 0.00 0.17
32 17.0699 0.00 0.23 0.00 0.24
33 23.0390 0.00 0.07 0.00 0.01
34 23.0392 0.00 -0.13 0.00 -0.03
35 23.0393 0.00 -0.21 0.00 -0.41
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.
00CK105 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.430 39.430 39.430 ecceobj 0.233 0.233 0.233 incobj 8.146 8.146 8.146 qmin 28.201 28.202 28.201 qmax 51.293 51.294 51.292 amean 39.455 39.455 39.455 amin 39.118 39.117 39.118 amax 39.908 39.908 39.907 emean 0.229 0.229 0.229 emin 0.180 0.180 0.180 emax 0.285 0.285 0.285 imean 9.677 9.677 9.677 imin 5.240 5.240 5.239 imax 12.050 12.050 12.050 excite_mean 0.286 0.286 0.286 fracstop 1.000 1.000 1.000 cjmean 2.958 2.958 2.958 libcent 0 179.8 179.8 179.8 libamp 0 20.0 20.1 20.0 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 208.0 208.0 208.0 kozaiamp 180.0 180.0 180.0