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: 06HT122
# Created Fri Nov 22 02:08:51 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 52 observations of 52
# Arc: 16.00y
# First observation: 2006/04/26
# Last observation: 2022/04/26
# Chi-squared of fit: 36.76 DOF: 98 RMS: 0.15
# Min/Max residuals: -0.87 0.46
# Exact a, adot, b, bdot, g, gdot:
1.595724E-05 2.678806E-02 -2.779521E-07 2.153079E-03 2.663150E-02 4.425860E-03
# Covariance matrix:
3.9572E-13 -6.2750E-14 7.9917E-15 -2.6020E-15 2.7104E-14 -8.9592E-14
-6.2750E-14 1.7695E-14 -2.5452E-15 1.1404E-15 9.6708E-15 4.0518E-14
7.9917E-15 -2.5452E-15 2.9493E-13 -3.0039E-14 2.3813E-15 -6.9069E-15
-2.6020E-15 1.1404E-15 -3.0039E-14 3.4896E-15 8.1637E-16 3.2354E-15
2.7104E-14 9.6708E-15 2.3813E-15 8.1637E-16 1.0154E-13 3.4509E-14
-8.9592E-14 4.0518E-14 -6.9069E-15 3.2354E-15 3.4509E-14 1.1537E-13
# lat0 lon0 xBary yBary zBary JD0
5.675307 -138.260271 0.104377 0.098639 -0.991407 2453851.734594
# Heliocentric elements and errors
Epoch: 2453852.5000 = 2006/04/27
Mean Anomaly: 71.51419 +/- 0.009
Argument of Peri: 320.28515 +/- 0.012
Long of Asc Node: 171.56670 +/- 0.001
Inclination: 7.19896 +/- 0.000
Eccentricity: 0.16168179 +/- 0.0000
Semi-Major Axis: 39.58533943 +/- 0.0019
Time of Perihelion: 2435781.1880 +/- 2.6
Perihelion: 33.18511096 +/- 0.0016
Aphelion: 45.98556790 +/- 0.0022
Period (y) 249.0633 +/- 0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -28.69724805 +/- 0.0003
Ecliptic Y -25.46472900 +/- 0.0003
Ecliptic Z 3.71329625 +/- 0.0000
Ecliptic XDOT 0.00151572 +/- 0.0000
Ecliptic YDOT -0.00234750 +/- 0.0000
Ecliptic ZDOT 0.00026523 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 38.54562977 +/- 0.0003
Geocenter to KBO 37.54945586 +/- 0.0004
# Hcoef: 7.60
The following table shows the complete astrometric record for 06HT122. 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 (06HT122) followed by the observatory code and reference code for the source of the astrometry.
2006 04 26.23384 14 44 17.83 -09 57 00.4 22.4R 06HT122 807 Cr3609 2006 04 26.31833 14 44 17.40 -09 56 58.6 06HT122 807 Cr3609 2006 04 28.09587 14 44 08.51 -09 56 12.9 06HT122 807 Cr3609 2006 06 20.01100 14 40 12.41 -09 39 30.5 23.5R 06HT122 304 Cr4858 2006 06 20.10534 14 40 12.10 -09 39 29.6 06HT122 304 Cr4858 2006 08 21.03029 14 39 48.70 -09 45 17.5 22.3R 06HT122 807 Cs2782 2006 08 22.02907 14 39 51.32 -09 45 37.9 06HT122 807 Cs2782 2006 08 23.03145 14 39 54.06 -09 45 57.1 06HT122 807 Cs2782 2014 05 30.38156 15 28 59.213 -12 12 12.73 23.5r 06HT122 568 C~2lRz 2014 05 30.43011 15 28 58.982 -12 12 11.88 23.2r 06HT122 568 C~2lRz 2014 05 30.43466 15 28 58.948 -12 12 11.61 22.9r 06HT122 568 C~2lRz 2014 05 31.42022 15 28 54.201 -12 11 56.24 23.8r 06HT122 568 C~2lRz 2014 06 01.30833 15 28 49.942 -12 11 42.27 23.6r 06HT122 568 C~2lRz 2014 06 01.35165 15 28 49.731 -12 11 41.62 23.8r 06HT122 568 C~2lRz 2014 06 01.39455 15 28 49.518 -12 11 40.92 23.4r 06HT122 568 C~2lRz 2014 06 22.34880 15 27 18.247 -12 07 23.30 23.6r 06HT122 568 C~2lRz 2014 07 19.32186 15 26 01.587 -12 05 46.54 23.5r 06HT122 568 C~2lRz 2015 02 23.63194 15 40 10.270 -12 56 44.15 23.5r 06HT122 568 C~2lRz 2015 03 19.59128 15 39 47.587 -12 51 13.42 23.6r 06HT122 568 C~2lRz 2015 03 22.51359 15 39 41.060 -12 50 22.84 23.7r 06HT122 568 C~2lRz 2015 04 12.50860 15 38 33.995 -12 43 37.99 23.8r 06HT122 568 C~2lRz 2015 04 12.54955 15 38 33.833 -12 43 37.14 23.7r 06HT122 568 C~2lRz 2015 04 18.53176 15 38 09.266 -12 41 33.65 23.6r 06HT122 568 C~2lRz 2015 05 17.40428 15 35 51.479 -12 31 52.71 23.5r 06HT122 568 C~2lRz 2015 05 17.44599 15 35 51.267 -12 31 51.86 23.5r 06HT122 568 C~2lRz 2015 05 17.49805 15 35 51.004 -12 31 50.66 23.8r 06HT122 568 C~2lRz 2015 05 24.38965 15 35 16.460 -12 29 47.62 23.9r 06HT122 568 C~2lRz 2015 05 24.43575 15 35 16.226 -12 29 46.80 23.9r 06HT122 568 C~2lRz 2015 05 24.47682 15 35 16.015 -12 29 46.15 23.5r 06HT122 568 C~2lRz 2015 05 26.46493 15 35 06.131 -12 29 12.22 22.8r 06HT122 568 C~2lRz 2015 06 18.36386 15 33 20.362 -12 24 00.09 23.7r 06HT122 568 C~2lRz 2015 06 18.40481 15 33 20.196 -12 23 59.66 23.9r 06HT122 568 C~2lRz 2015 06 21.37946 15 33 08.118 -12 23 31.01 23.8r 06HT122 568 C~2lRz 2015 07 10.41516 15 32 04.454 -12 21 43.61 23.5r 06HT122 568 C~2lRz 2015 07 18.33993 15 31 46.083 -12 21 39.59 23.7r 06HT122 568 C~2lRz 2016 02 06.62104 15 45 25.525 -13 13 08.30 24.0w 06HT122 568 C~2lRz 2016 02 12.60658 15 45 36.677 -13 12 39.74 23.9w 06HT122 568 C~2lRz 2016 03 15.60417 15 45 34.087 -13 06 43.89 23.8w 06HT122 568 C~2lRz 2016 03 15.61316 15 45 34.071 -13 06 43.80 23.9w 06HT122 568 C~2lRz 2016 04 03.55069 15 44 46.548 -13 01 11.25 24.1w 06HT122 568 C~2lRz 2016 04 08.60024 15 44 29.046 -12 59 33.44 24.0w 06HT122 568 C~2lRz 2016 04 29.50143 15 43 00.608 -12 52 34.55 23.9w 06HT122 568 C~2lRz 2016 05 04.47406 15 42 36.826 -12 50 56.06 23.9w 06HT122 568 C~2lRz 2016 05 30.46201 15 40 27.653 -12 43 14.53 23.8w 06HT122 568 C~2lRz 2016 07 04.29818 15 38 02.162 -12 37 24.32 23.8w 06HT122 568 C~2lRz 2016 07 05.36646 15 37 58.813 -12 37 20.07 23.9w 06HT122 568 C~2lRz 2017 03 30.57261 15 50 39.912 -13 16 41.98 23.9w 06HT122 568 C~2lRz 2017 08 20.25685 15 42 43.045 -12 55 38.26 23.9w 06HT122 568 C~2lRz 2017 08 26.26800 15 42 50.253 -12 56 59.56 24.2w 06HT122 568 C~2lRz 2022 04 26.381770 16 17 01.237 -14 11 36.85 23.5G 06HT122 G37 C~5ZW5 2022 04 26.429290 16 17 01.023 -14 11 35.92 06HT122 G37 C~5ZW5 2022 04 26.454640 16 17 00.956 -14 11 35.19 06HT122 G37 C~5ZW5
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 0.09 0.00 0.31
2 0.0002 0.00 0.07 0.00 -0.07
3 0.0051 0.00 -0.05 0.00 0.01
4 0.1500 0.00 0.04 0.00 0.43
5 0.1502 0.00 -0.04 0.00 0.46
6 0.3198 0.00 -0.14 0.00 -0.32
7 0.3225 0.00 -0.12 0.00 -0.87
8 0.3253 0.00 0.15 0.00 0.23
9 8.0935 0.00 -0.04 0.00 -0.04
10 8.0936 0.00 0.09 0.00 0.03
11 8.0936 0.00 -0.09 0.00 0.23
12 8.0963 0.00 0.05 0.00 -0.08
13 8.0988 0.00 -0.03 0.00 -0.02
14 8.0989 0.00 -0.03 0.00 -0.04
15 8.0990 0.00 -0.09 0.00 -0.00
16 8.1564 0.00 -0.03 0.00 -0.04
17 8.2302 0.00 -0.01 0.00 -0.01
18 8.8307 0.00 0.00 0.00 -0.05
19 8.8963 0.00 0.13 0.00 -0.04
20 8.9043 0.00 -0.02 0.00 -0.01
21 8.9617 0.00 -0.13 0.00 0.02
22 8.9619 0.00 -0.08 0.00 0.03
23 8.9782 0.00 0.15 0.00 0.03
24 9.0573 0.00 0.02 0.00 -0.14
25 9.0574 0.00 0.04 0.00 -0.06
26 9.0575 0.00 0.09 0.00 0.17
27 9.0764 0.00 0.09 0.00 -0.01
28 9.0765 0.00 0.09 0.00 0.02
29 9.0766 0.00 0.05 0.00 -0.04
30 9.0821 0.00 -0.06 0.00 0.22
31 9.1448 0.00 -0.05 0.00 -0.00
32 9.1449 0.00 0.06 0.00 0.01
33 9.1530 0.00 -0.04 0.00 0.01
34 9.2052 0.00 -0.01 0.00 -0.09
35 9.2268 0.00 -0.06 0.00 -0.03
36 9.7834 0.00 -0.02 0.00 0.01
37 9.7998 0.00 0.04 0.00 -0.02
38 9.8874 0.00 -0.10 0.00 0.05
39 9.8874 0.00 -0.11 0.00 -0.00
40 9.9393 0.00 -0.06 0.00 -0.03
41 9.9531 0.00 0.01 0.00 -0.03
42 10.0103 0.00 -0.00 0.00 -0.01
43 10.0239 0.00 -0.01 0.00 -0.04
44 10.0951 0.00 -0.04 0.00 -0.11
45 10.1905 0.00 -0.01 0.00 -0.15
46 10.1934 0.00 -0.01 0.00 -0.14
47 10.9277 0.00 -0.02 0.00 -0.05
48 11.3183 0.00 0.07 0.00 -0.03
49 11.3348 0.00 -0.04 0.00 -0.05
50 16.0004 0.00 -0.07 0.00 -0.06
51 16.0005 0.00 -0.24 0.00 0.08
52 16.0006 0.00 0.37 0.00 0.38
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.
06HT122 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.096 39.096 39.096 ecceobj 0.160 0.160 0.160 incobj 7.222 7.222 7.222 qmin 32.391 32.392 32.391 qmax 46.651 46.660 46.641 amean 39.455 39.455 39.455 amin 39.065 39.064 39.066 amax 39.780 39.781 39.784 emean 0.160 0.160 0.160 emin 0.143 0.143 0.143 emax 0.176 0.176 0.176 imean 6.985 6.984 6.985 imin 6.400 6.400 6.400 imax 7.738 7.738 7.738 excite_mean 0.201 0.201 0.201 fracstop 1.000 1.000 1.000 cjmean 3.006 3.006 3.006 libcent 0 179.5 179.5 179.6 libamp 0 58.6 58.5 58.7 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 180.8 180.8 180.7 kozaiamp 179.9 180.0 180.0