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: 679995 # Created Fri Nov 22 02:07:51 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 96 observations of 96 # Arc: 14.06y # First observation: 2009/09/27 # Last observation: 2023/10/20 # Chi-squared of fit: 62.36 DOF: 186 RMS: 0.14 # Min/Max residuals: -0.45 0.55 # Exact a, adot, b, bdot, g, gdot: 2.237661E-05 8.715799E-02 4.774187E-06 2.282015E-02 6.289525E-02 -2.054806E-02 # 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 -9.148178 6.410696 0.031450 -0.158765 -0.985909 2455102.010114 # Heliocentric elements and errors Epoch: 2455102.5000 = 2009/09/28 Mean Anomaly: 263.83996 +/- 0.000 Argument of Peri: 90.34982 +/- 0.000 Long of Asc Node: 35.87243 +/- 0.000 Inclination: 17.04726 +/- 0.000 Eccentricity: 0.23246362 +/- 0.0000 Semi-Major Axis: 15.71329128 +/- 0.0000 Time of Perihelion: 2461179.5291 +/- 0.0 Perihelion: 12.06052266 +/- 0.0000 Aphelion: 19.36605991 +/- 0.0000 Period (y) 62.2887 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 16.59833761 +/- 0.0000 Ecliptic Y 1.82983501 +/- 0.0000 Ecliptic Z -2.52775091 +/- 0.0000 Ecliptic XDOT -0.00114045 +/- 0.0000 Ecliptic YDOT 0.00369436 +/- 0.0000 Ecliptic ZDOT 0.00112286 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 16.88920855 +/- 0.0000 Geocenter to KBO 15.89956630 +/- 0.0000 # Hcoef: 10.96
The following table shows the complete astrometric record for 679995. 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 (679995) followed by the observatory code and reference code for the source of the astrometry.
2009 09 27.509348 00 38 02.711 -05 51 19.86 22.4G 679995 F51 C~6BDQ 2010 09 27.440621 00 54 44.533 -02 35 04.39 22.4G 679995 F51 C~6BDQ 2010 10 04.415915 00 53 26.867 -02 41 43.22 23.1G 679995 F51 C~6BDQ 2010 10 04.444703 00 53 26.543 -02 41 45.24 23.3G 679995 F51 C~6BDQ 2011 09 26.434581 01 12 16.572 +00 51 21.55 21.9G 679995 F51 C~6BDQ 2011 09 26.449484 01 12 16.400 +00 51 20.16 21.7G 679995 F51 C~6BDQ 2011 09 26.483361 01 12 16.035 +00 51 18.43 23.8G 679995 F51 C~6BDQ 2012 10 17.394249 01 26 16.226 +04 06 06.81 22.9G 679995 F51 C~6BDQ 2012 10 17.407644 01 26 16.067 +04 06 05.88 22.6G 679995 F51 C~6BDQ 2012 10 17.421064 01 26 15.913 +04 06 05.37 22.0G 679995 F51 C~6BDQ 2012 10 17.434603 01 26 15.754 +04 06 04.58 22.3G 679995 F51 C~6BDQ 2012 11 05.288796 01 22 39.131 +03 51 28.28 22.9G 679995 F51 C~6BDQ 2012 11 05.303933 01 22 38.969 +03 51 27.71 22.7G 679995 F51 C~6BDQ 2012 11 05.319003 01 22 38.803 +03 51 26.93 22.8G 679995 F51 C~6BDQ 2012 11 05.334141 01 22 38.635 +03 51 26.40 23.2G 679995 F51 C~6BDQ 2013 11 25.242112 01 38 12.844 +07 22 49.46 22.9G 679995 F51 C~6BDQ 2013 11 25.257185 01 38 12.708 +07 22 49.02 23.0G 679995 F51 C~6BDQ 2013 11 25.272212 01 38 12.571 +07 22 48.79 23.0G 679995 F51 C~6BDQ 2013 11 25.287217 01 38 12.430 +07 22 48.28 23.0G 679995 F51 C~6BDQ 2014 10 02.389499 02 09 08.821 +11 53 03.20 22.6G 679995 F51 C~6BDQ 2014 10 02.401676 02 09 08.675 +11 53 02.42 21.7G 679995 F51 C~6BDQ 2014 10 02.413916 02 09 08.551 +11 53 01.98 22.6G 679995 F51 C~6BDQ 2014 10 02.426117 02 09 08.415 +11 53 01.67 22.0G 679995 F51 C~6BDQ 2014 11 18.288444 01 59 36.147 +11 17 51.09 22.9G 679995 F51 C~6BDQ 2014 11 21.416799 01 59 01.274 +11 15 51.02 22.9G 679995 F51 C~6BDQ 2014 11 21.428357 01 59 01.135 +11 15 50.30 22.9G 679995 F51 C~6BDQ 2014 11 21.439973 01 59 01.011 +11 15 50.55 23.4G 679995 F51 C~6BDQ 2014 11 21.451646 01 59 00.885 +11 15 49.71 22.9G 679995 F51 C~6BDQ 2014 11 28.416767 01 57 48.517 +11 11 50.39 23.0G 679995 F51 C~6BDQ 2014 12 16.321195 01 55 23.772 +11 05 19.02 23.2G 679995 F51 C~6BDQ 2015 09 09.473844 02 34 43.560 +15 55 13.53 22.8G 679995 F51 C~6BDQ 2015 09 09.486130 02 34 43.483 +15 55 13.33 22.9G 679995 F51 C~6BDR 2015 09 09.498385 02 34 43.413 +15 55 13.10 23.0G 679995 F51 C~6BDR 2015 09 09.510687 02 34 43.336 +15 55 13.09 22.7G 679995 F51 C~6BDR 2015 12 04.254778 02 18 35.374 +15 07 10.55 22.7G 679995 F51 C~6BDR 2015 12 04.265385 02 18 35.230 +15 07 10.45 22.4G 679995 F51 C~6BDR 2015 12 04.275944 02 18 35.153 +15 07 09.98 22.4G 679995 F51 C~6BDR 2015 12 04.286625 02 18 35.036 +15 07 09.76 22.4G 679995 F51 C~6BDR 2016 01 04.296678 02 15 04.979 +14 57 51.01 22.4G 679995 F51 C~6BDR 2016 01 04.309672 02 15 04.948 +14 57 50.83 22.4G 679995 F51 C~6BDR 2016 01 04.322657 02 15 04.905 +14 57 51.08 22.4G 679995 F51 C~6BDR 2016 01 04.335625 02 15 04.863 +14 57 50.77 22.6G 679995 F51 C~6BDR 2016 01 24.224278 02 15 02.810 +15 02 22.63 22.2G 679995 F51 C~6BDR 2016 01 24.261595 02 15 02.897 +15 02 23.62 22.1G 679995 F51 C~6BDR 2016 10 25.551938 02 51 08.400 +19 36 59.76 21.7G 679995 F51 C~6BDR 2017 10 28.554965 03 17 41.516 +23 38 05.74 22.4G 679995 F51 C~6BDR 2017 10 28.567376 03 17 41.337 +23 38 05.47 22.4G 679995 F51 C~6BDR 2017 10 28.579749 03 17 41.162 +23 38 05.18 22.3G 679995 F51 C~6BDR 2017 10 28.592072 03 17 40.997 +23 38 04.96 22.1G 679995 F51 C~6BDR 2017 11 17.493765 03 12 51.729 +23 28 24.43 21.4G 679995 F51 C~6BDR 2017 11 17.505820 03 12 51.533 +23 28 23.98 22.3G 679995 F51 C~6BDR 2017 11 17.517858 03 12 51.368 +23 28 23.67 21.9G 679995 F51 C~6BDR 2017 11 17.529968 03 12 51.179 +23 28 23.28 22.9G 679995 F51 C~6BDR 2017 12 08.277245 03 08 02.437 +23 15 14.47 21.9G 679995 F51 C~6BDR 2017 12 08.291976 03 08 02.249 +23 15 13.83 21.8G 679995 F51 C~6BDR 2017 12 08.306656 03 08 02.052 +23 15 13.35 22.3G 679995 F51 C~6BDR 2017 12 08.321478 03 08 01.862 +23 15 12.76 22.2G 679995 F51 C~6BDR 2017 12 09.262832 03 07 50.053 +23 14 36.30 22.2G 679995 F51 C~6BDR 2017 12 09.276572 03 07 49.873 +23 14 35.87 22.2G 679995 F51 C~6BDR 2017 12 09.290166 03 07 49.683 +23 14 35.43 21.6G 679995 F51 C~6BDR 2018 01 08.321843 03 03 15.159 +22 58 36.00 23.1G 679995 F51 C~6BDR 2018 11 05.414193 03 46 20.905 +27 32 31.38 22.2G 679995 F52 C~6BDR 2018 11 05.426294 03 46 20.722 +27 32 31.55 22.2G 679995 F52 C~6BDR 2018 11 05.438677 03 46 20.543 +27 32 31.22 22.2G 679995 F52 C~6BDR 2018 11 14.506622 03 44 02.676 +27 30 06.13 22.4G 679995 F52 C~6BDR 2019 01 07.223411 03 32 11.326 +27 00 22.93 22.7G 679995 F51 C~6BDR 2019 01 07.232504 03 32 11.249 +27 00 22.73 22.4G 679995 F51 C~6BDR 2019 01 07.241635 03 32 11.186 +27 00 22.27 22.5G 679995 F51 C~6BDR 2019 01 07.250859 03 32 11.122 +27 00 21.78 22.5G 679995 F51 C~6BDR 2019 01 23.338681 03 30 45.024 +26 52 56.24 22.3G 679995 F51 C~6BDR 2019 01 27.306415 03 30 36.638 +26 51 37.50 22.5G 679995 F52 C~6BDR 2019 08 08.593542 04 23 01.621 +29 55 31.00 22.0G 679995 F52 C~6BDR 2019 08 08.598019 04 23 01.681 +29 55 31.35 22.5G 679995 F52 C~6BDR 2019 08 08.602516 04 23 01.725 +29 55 32.02 22.2G 679995 F52 C~6BDR 2019 09 06.596108 04 26 58.986 +30 31 35.78 22.5G 679995 F51 C~6BDR 2019 09 06.604842 04 26 58.998 +30 31 36.32 21.9G 679995 F51 C~6BDR 2019 09 06.613526 04 26 59.032 +30 31 36.90 22.5G 679995 F51 C~6BDR 2019 09 06.622247 04 26 59.074 +30 31 37.51 22.5G 679995 F51 C~6BDR 2022 12 22.300290 06 18 28.843 +39 08 28.57 21.8G 679995 V00 C~6BDR 2022 12 22.305252 06 18 28.753 +39 08 28.61 21.7G 679995 V00 C~6BDR 2022 12 22.310296 06 18 28.652 +39 08 28.72 22.0G 679995 V00 C~6BDR 2022 12 22.315258 06 18 28.562 +39 08 28.86 21.7G 679995 V00 C~6BDR 2022 12 22.421080 06 18 26.525 +39 08 31.81 21.4G 679995 V00 C~6BDR 2022 12 22.427108 06 18 26.410 +39 08 31.85 21.7G 679995 V00 C~6BDR 2022 12 22.433105 06 18 26.305 +39 08 32.03 21.5G 679995 V00 C~6BDR 2022 12 22.439133 06 18 26.183 +39 08 32.14 21.5G 679995 V00 C~6BDR 2022 12 27.254271 06 16 55.240 +39 10 25.00 21.8G 679995 V06 C~6BDR 2022 12 27.264722 06 16 55.050 +39 10 25.80 20.9G 679995 V06 C~6BDR 2022 12 27.285404 06 16 54.620 +39 10 25.60 21.3G 679995 V06 C~6BDR 2022 12 27.295869 06 16 54.420 +39 10 25.80 22.3G 679995 V06 C~6BDR 2022 12 31.464812 06 15 35.768 +39 11 31.54 21.0G 679995 T12 C~6BDR 2022 12 31.473082 06 15 35.611 +39 11 31.65 20.4G 679995 T12 C~6BDR 2023 10 20.606223 07 18 54.902 +38 13 28.25 21.8w 679995 F52 C~7Mvc 2023 10 20.613917 07 18 54.932 +38 13 29.04 21.9w 679995 F52 C~7Mvc 2023 10 20.621609 07 18 54.933 +38 13 29.63 21.8w 679995 F52 C~7Mvc 2023 10 20.629344 07 18 54.985 +38 13 30.50 22.0w 679995 F52 C~7Mvc
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 -0.17 0.00 0.14
2 0.9991 0.00 -0.39 0.00 -0.08
3 1.0182 0.00 -0.07 0.00 0.19
4 1.0183 0.00 0.02 0.00 -0.23
5 1.9957 0.00 0.17 0.00 0.37
6 1.9957 0.00 0.08 0.00 -0.17
7 1.9958 0.00 0.25 0.00 0.03
8 3.0551 0.00 -0.14 0.00 0.23
9 3.0552 0.00 -0.10 0.00 -0.01
10 3.0552 0.00 0.02 0.00 0.18
11 3.0552 0.00 0.09 0.00 0.09
12 3.1069 0.00 0.01 0.00 0.04
13 3.1069 0.00 0.09 0.00 0.07
14 3.1069 0.00 0.10 0.00 -0.12
15 3.1070 0.00 0.09 0.00 -0.05
16 4.1608 0.00 -0.10 0.00 0.06
17 4.1608 0.00 -0.03 0.00 0.02
18 4.1609 0.00 0.03 0.00 0.18
19 4.1609 0.00 0.01 0.00 0.07
20 5.0127 0.00 -0.04 0.00 0.09
21 5.0127 0.00 -0.17 0.00 -0.20
22 5.0127 0.00 0.04 0.00 -0.15
23 5.0128 0.00 0.07 0.00 0.02
24 5.1411 0.00 0.11 0.00 -0.21
25 5.1496 0.00 -0.05 0.00 -0.04
26 5.1497 0.00 -0.20 0.00 -0.33
27 5.1497 0.00 -0.12 0.00 0.36
28 5.1497 0.00 -0.06 0.00 -0.04
29 5.1688 0.00 0.13 0.00 0.12
30 5.2178 0.00 -0.06 0.00 -0.19
31 5.9493 0.00 -0.06 0.00 0.27
32 5.9493 0.00 -0.09 0.00 0.12
33 5.9493 0.00 -0.02 0.00 -0.06
34 5.9494 0.00 -0.04 0.00 -0.01
35 6.1841 0.00 0.05 0.00 -0.22
36 6.1841 0.00 -0.45 0.00 0.03
37 6.1842 0.00 0.05 0.00 -0.09
38 6.1842 0.00 -0.03 0.00 0.04
39 6.2691 0.00 0.03 0.00 -0.09
40 6.2691 0.00 0.17 0.00 -0.27
41 6.2692 0.00 0.13 0.00 -0.01
42 6.2692 0.00 0.10 0.00 -0.32
43 6.3237 0.00 -0.17 0.00 0.22
44 6.3238 0.00 -0.24 0.00 0.21
45 7.0775 0.00 0.07 0.00 -0.27
46 8.0850 0.00 0.09 0.00 -0.02
47 8.0850 0.00 0.04 0.00 -0.01
48 8.0851 0.00 0.03 0.00 -0.02
49 8.0851 0.00 0.17 0.00 0.04
50 8.1396 0.00 0.10 0.00 -0.15
51 8.1396 0.00 -0.13 0.00 -0.16
52 8.1397 0.00 0.09 0.00 -0.03
53 8.1397 0.00 -0.03 0.00 0.02
54 8.1965 0.00 0.11 0.00 0.09
55 8.1965 0.00 0.14 0.00 0.01
56 8.1966 0.00 0.03 0.00 0.09
57 8.1966 0.00 0.05 0.00 0.07
58 8.1992 0.00 0.12 0.00 0.00
59 8.1992 0.00 0.04 0.00 0.09
60 8.1993 0.00 -0.21 0.00 0.17
61 8.2815 0.00 -0.09 0.00 0.04
62 9.1058 0.00 -0.03 0.00 -0.16
63 9.1059 0.00 -0.03 0.00 0.14
64 9.1059 0.00 0.08 0.00 -0.05
65 9.1307 0.00 0.13 0.00 0.21
66 9.2778 0.00 0.05 0.00 -0.08
67 9.2778 0.00 0.00 0.00 0.02
68 9.2778 0.00 0.17 0.00 -0.15
69 9.2779 0.00 0.34 0.00 -0.34
70 9.3219 0.00 0.12 0.00 -0.03
71 9.3328 0.00 0.05 0.00 0.10
72 9.8620 0.00 0.14 0.00 -0.08
73 9.8620 0.00 0.21 0.00 -0.09
74 9.8620 0.00 0.04 0.00 0.21
75 9.9414 0.00 0.05 0.00 0.01
76 9.9414 0.00 -0.20 0.00 -0.05
77 9.9414 0.00 -0.11 0.00 -0.06
78 9.9414 0.00 0.09 0.00 -0.04
79 13.2342 0.00 -0.07 0.00 0.12
80 13.2342 0.00 0.01 0.00 0.02
81 13.2342 0.00 -0.05 0.00 -0.01
82 13.2342 0.00 0.03 0.00 -0.01
83 13.2345 0.00 -0.10 0.00 0.10
84 13.2345 0.00 -0.10 0.00 -0.02
85 13.2346 0.00 0.05 0.00 0.01
86 13.2346 0.00 -0.06 0.00 -0.04
87 13.2478 0.00 0.00 0.00 -0.04
88 13.2478 0.00 0.17 0.00 0.55
89 13.2478 0.00 -0.30 0.00 -0.06
90 13.2479 0.00 -0.28 0.00 -0.06
91 13.2593 0.00 -0.00 0.00 0.02
92 13.2593 0.00 0.02 0.00 0.04
93 14.0619 0.00 0.15 0.00 -0.11
94 14.0619 0.00 0.19 0.00 0.04
95 14.0619 0.00 -0.20 0.00 -0.02
96 14.0619 0.00 0.17 0.00 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.
679995 quality flag:3 Type: CENTAURR CENTAURR CENTAURR axisobj 15.712 15.712 15.712 ecceobj 0.232 0.232 0.232 incobj 17.030 17.030 17.030 qmin 11.635 10.817 11.882 qmax 19.889 20.467 19.654 amean 15.849 15.882 15.813 amin 15.486 14.818 14.885 amax 16.157 16.386 16.131 emean 0.171 0.179 0.172 emin 0.108 0.120 0.102 emax 0.252 0.307 0.234 imean 17.120 17.172 16.907 imin 16.054 14.895 16.138 imax 17.974 18.040 17.891 excite_mean 0.342 0.347 0.339 fracstop 0.068 0.049 0.063 cjmean 3.265 3.260 3.269 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 184.6 183.1 180.8 kozaiamp 179.2 179.0 179.4