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: 13TP145
# Created Fri Nov 22 02:09:40 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 52 observations of 52
# Arc: 14.35y
# First observation: 2009/10/10
# Last observation: 2024/02/15
# Chi-squared of fit: 97.44 DOF: 98 RMS: 0.24
# Min/Max residuals: -0.98 0.66
# Exact a, adot, b, bdot, g, gdot:
2.309636E-05 1.006792E-01 1.331472E-05 5.714751E-02 6.696385E-02 -3.842344E-02
# Covariance matrix:
9.7988E-11 9.8974E-09 -8.0553E-11 1.3874E-08 -4.3510E-09 -4.8182E-08
9.8974E-09 1.8352E-06 -8.2106E-09 1.6096E-06 -4.4156E-07 -6.4278E-06
-8.0553E-11 -8.2106E-09 6.7036E-11 -1.1497E-08 3.5947E-09 3.9818E-08
1.3874E-08 1.6096E-06 -1.1497E-08 2.0485E-06 -6.1874E-07 -7.2306E-06
-4.3510E-09 -4.4156E-07 3.5947E-09 -6.1874E-07 1.9417E-07 2.1471E-06
-4.8182E-08 -6.4278E-06 3.9818E-08 -7.2306E-06 2.1471E-06 2.6707E-05
# lat0 lon0 xBary yBary zBary JD0
5.106861 -26.518754 -0.686919 0.064217 -0.718755 2455114.641237
# Heliocentric elements and errors
Epoch: 2455114.5000 = 2009/10/10
Mean Anomaly: 335.51375 +/- 0.001
Argument of Peri: 68.62976 +/- 0.000
Long of Asc Node: 327.25331 +/- 0.000
Inclination: 29.24835 +/- 0.001
Eccentricity: 0.41544605 +/- 0.0000
Semi-Major Axis: 23.03723716 +/- 0.0000
Time of Perihelion: 2457861.5327 +/- 0.1
Perihelion: 13.46650796 +/- 0.0001
Aphelion: 32.60796636 +/- 0.0001
Period (y) 110.5742 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 14.26522150 +/- 0.0000
Ecliptic Y -6.35176814 +/- 0.0000
Ecliptic Z 1.32949486 +/- 0.0000
Ecliptic XDOT 0.00025538 +/- 0.0000
Ecliptic YDOT 0.00447983 +/- 0.0000
Ecliptic ZDOT 0.00218731 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 15.67203893 +/- 0.0000
Geocenter to KBO 14.93360580 +/- 0.0000
# Hcoef: 9.23
The following table shows the complete astrometric record for 13TP145. 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 (13TP145) followed by the observatory code and reference code for the source of the astrometry.
2009 10 10.140471 22 14 11.44 -05 27 52.5 21.1r 13TP145 645 C~3xqn 2009 10 10.141300 22 14 11.43 -05 27 52.5 20.8i 13TP145 645 C~3xqn 2009 10 10.143788 22 14 11.41 -05 27 52.7 21.7g 13TP145 645 C~3xqn 2009 10 15.120122 22 13 36.47 -05 29 42.9 21.5r 13TP145 645 C~3xqn 2009 10 15.120951 22 13 36.47 -05 29 43.0 20.9i 13TP145 645 C~3xqn 2009 10 15.123439 22 13 36.44 -05 29 43.0 21.9g 13TP145 645 C~3xqn 2010 09 15.29609 22 35 59.64 +00 09 39.5 21.0V 13TP145 G96 C~3xqn 2010 09 15.30460 22 35 59.56 +00 09 39.6 20.8V 13TP145 G96 C~3xqn 2010 09 15.31306 22 35 59.49 +00 09 39.2 20.9V 13TP145 G96 C~3xqn 2010 09 15.32156 22 35 59.38 +00 09 39.0 20.8V 13TP145 G96 C~3xqn 2013 10 08.02964 23 33 27.781 +18 05 08.80 20.7R 13TP145 809 C~0wdY 2013 10 08.03221 23 33 27.708 +18 05 07.54 21.1R 13TP145 809 C~0wdY 2013 10 08.10051 23 33 26.858 +18 05 04.16 20.8R 13TP145 809 C~0wdY 2013 10 08.10307 23 33 26.865 +18 05 02.97 20.9R 13TP145 809 C~0wdY 2013 10 08.16743 23 33 26.052 +18 04 59.62 20.9R 13TP145 809 C~0wdY 2013 10 08.16999 23 33 26.023 +18 04 58.80 21.2R 13TP145 809 C~0wdY 2013 10 29.00791 23 29 45.962 +17 39 42.73 20.8R 13TP145 809 C~0wdY 2013 10 29.06256 23 29 45.534 +17 39 38.66 20.7R 13TP145 809 C~0wdY 2013 10 29.06512 23 29 45.495 +17 39 38.80 20.3R 13TP145 809 C~0wdY 2013 10 29.12050 23 29 45.010 +17 39 34.23 20.9R 13TP145 809 C~0wdY 2020 11 14.382760 03 58 13.643 +52 06 53.13 20.9G 13TP145 G37 C~4Nkp 2020 11 14.443650 03 58 12.421 +52 06 52.10 13TP145 G37 C~4Nkp 2023 10 09.589223 06 29 52.206 +48 32 04.52 21.4w 13TP145 F52 C~7Axc 2023 10 09.601581 06 29 52.235 +48 32 05.32 21.4w 13TP145 F52 C~7Axc 2023 10 09.613921 06 29 52.261 +48 32 06.37 21.5w 13TP145 F52 C~7Axc 2023 10 09.626279 06 29 52.282 +48 32 07.20 21.6w 13TP145 F52 C~7Axc 2023 10 22.574109 06 29 47.510 +48 48 44.29 21.3w 13TP145 F52 C~7Mj1 2023 10 22.587586 06 29 47.470 +48 48 45.35 21.4w 13TP145 F52 C~7Mj1 2023 10 22.614490 06 29 47.378 +48 48 47.35 21.3w 13TP145 F52 C~7Mj1 2023 11 11.479441 06 27 31.739 +49 11 49.59 21.3w 13TP145 F52 C~7RAY 2023 11 11.491067 06 27 31.618 +49 11 50.23 21.2w 13TP145 F52 C~7RAY 2023 11 11.502738 06 27 31.478 +49 11 50.94 21.3w 13TP145 F52 C~7RAY 2023 11 11.514352 06 27 31.362 +49 11 51.69 21.2w 13TP145 F52 C~7RAY 2023 12 08.502748 06 21 01.000 +49 30 45.28 21.2w 13TP145 F52 C~7bID 2023 12 08.515047 06 21 00.770 +49 30 45.45 21.3w 13TP145 F52 C~7bID 2023 12 08.527344 06 21 00.548 +49 30 45.85 21.5w 13TP145 F52 C~7bID 2023 12 08.539664 06 21 00.354 +49 30 46.27 21.2w 13TP145 F52 C~7bID 2023 12 15.485726 06 18 54.872 +49 32 10.40 21.2w 13TP145 F52 C~7bID 2023 12 15.496818 06 18 54.664 +49 32 10.49 21.0w 13TP145 F52 C~7bID 2023 12 15.507838 06 18 54.456 +49 32 10.71 21.0w 13TP145 F52 C~7bID 2023 12 15.518902 06 18 54.228 +49 32 10.74 21.0w 13TP145 F52 C~7bID 2024 02 04.302461 06 04 41.818 +48 52 58.73 21.2w 13TP145 F52 C~7mvP 2024 02 04.314816 06 04 41.684 +48 52 57.69 21.3w 13TP145 F52 C~7mvP 2024 02 04.327140 06 04 41.531 +48 52 56.63 21.2w 13TP145 F52 C~7mvP 2024 02 04.339444 06 04 41.380 +48 52 55.59 21.3w 13TP145 F52 C~7mvP 2024 02 13.279473 06 03 13.146 +48 38 36.51 21.2w 13TP145 F52 C~7mvP 2024 02 13.290525 06 03 13.038 +48 38 35.37 21.2w 13TP145 F52 C~7mvP 2024 02 13.301561 06 03 12.942 +48 38 34.43 21.4w 13TP145 F52 C~7mvP 2024 02 13.312613 06 03 12.834 +48 38 33.19 21.4w 13TP145 F52 C~7mvP 2024 02 15.236117 06 02 57.677 +48 35 17.63 21.1w 13TP145 F52 C~7mvP 2024 02 15.252933 06 02 57.561 +48 35 15.64 21.1w 13TP145 F52 C~7mvP 2024 02 15.261341 06 02 57.443 +48 35 14.86 21.3w 13TP145 F52 C~7mvP
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 0.08
2 0.0000 0.00 0.06 0.00 0.10
3 0.0000 0.00 0.05 0.00 -0.03
4 0.0136 0.00 -0.04 0.00 0.04
5 0.0136 0.00 0.05 0.00 -0.04
6 0.0136 0.00 -0.15 0.00 0.01
7 0.9313 0.00 -0.74 0.00 -0.27
8 0.9313 0.00 -0.42 0.00 0.19
9 0.9313 0.00 0.05 0.00 0.15
10 0.9314 0.00 -0.07 0.00 0.32
11 3.9942 0.00 0.21 0.00 0.11
12 3.9942 0.00 -0.40 0.00 -0.98
13 3.9944 0.00 -0.38 0.00 0.15
14 3.9944 0.00 0.20 0.00 -0.87
15 3.9946 0.00 0.05 0.00 0.07
16 3.9946 0.00 0.09 0.00 -0.58
17 4.0517 0.00 -0.15 0.00 0.26
18 4.0518 0.00 0.66 0.00 0.31
19 4.0518 0.00 0.42 0.00 0.65
20 4.0520 0.00 0.46 0.00 0.27
21 11.0972 0.00 -0.10 0.00 0.16
22 11.0973 0.00 -0.19 0.00 0.04
23 13.9971 0.00 -0.07 0.00 0.16
24 13.9972 0.00 0.00 0.00 -0.01
25 13.9972 0.00 0.04 0.00 0.08
26 13.9972 0.00 -0.00 0.00 -0.06
27 14.0327 0.00 -0.08 0.00 -0.03
28 14.0327 0.00 -0.00 0.00 -0.00
29 14.0328 0.00 -0.04 0.00 -0.04
30 14.0872 0.00 0.01 0.00 0.06
31 14.0872 0.00 0.08 0.00 -0.02
32 14.0872 0.00 -0.12 0.00 -0.04
33 14.0873 0.00 0.03 0.00 -0.01
34 14.1612 0.00 -0.01 0.00 -0.15
35 14.1612 0.00 -0.15 0.00 -0.21
36 14.1612 0.00 -0.17 0.00 -0.04
37 14.1613 0.00 0.23 0.00 0.16
38 14.1803 0.00 0.10 0.00 -0.10
39 14.1803 0.00 0.12 0.00 -0.07
40 14.1803 0.00 0.11 0.00 0.11
41 14.1804 0.00 -0.18 0.00 0.09
42 14.3194 0.00 -0.05 0.00 -0.02
43 14.3194 0.00 0.12 0.00 0.06
44 14.3195 0.00 0.00 0.00 0.12
45 14.3195 0.00 -0.09 0.00 0.20
46 14.3440 0.00 0.22 0.00 -0.05
47 14.3440 0.00 0.03 0.00 -0.08
48 14.3440 0.00 0.02 0.00 0.10
49 14.3441 0.00 -0.18 0.00 -0.02
50 14.3493 0.00 0.11 0.00 0.21
51 14.3494 0.00 0.36 0.00 -0.06
52 14.3494 0.00 -0.41 0.00 0.02
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.
13TP145 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 22.924 22.924 22.925 ecceobj 0.415 0.415 0.415 incobj 29.266 29.266 29.266 qmin 13.260 13.260 13.260 qmax 32.604 32.605 32.603 amean 22.661 22.885 22.916 amin 22.290 22.672 22.727 amax 23.015 23.193 23.139 emean 0.403 0.407 0.409 emin 0.385 0.391 0.401 emax 0.417 0.417 0.417 imean 30.965 30.858 30.812 imin 30.496 30.496 30.496 imax 31.712 31.430 31.100 excite_mean 0.653 0.655 0.655 fracstop 0.004 0.004 0.004 cjmean 2.685 2.677 2.676 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 77.4 76.8 78.7 kozaiamp 8.4 7.4 9.9