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: 14KE113 # Created Wed Dec 25 02:09:51 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 95 observations of 95 # Arc: 8.15y # First observation: 2012/04/27 # Last observation: 2020/06/22 # Chi-squared of fit: 74.29 DOF: 184 RMS: 0.16 # Min/Max residuals: -0.62 0.53 # Exact a, adot, b, bdot, g, gdot: 1.753473E-05 2.762922E-02 -6.984586E-06 -1.080303E-02 2.511343E-02 -1.539927E-03 # Covariance matrix: 1.7964E-13 -7.2979E-14 -3.2573E-14 2.3019E-14 5.4469E-15 -2.6935E-13 -7.2979E-14 4.4112E-14 2.6321E-14 -1.6871E-14 1.6139E-14 1.9399E-13 -3.2573E-14 2.6321E-14 1.0556E-13 -2.9516E-14 1.7421E-14 1.2926E-13 2.3019E-14 -1.6871E-14 -2.9516E-14 1.1838E-14 -7.5577E-15 -8.2872E-14 5.4469E-15 1.6139E-14 1.7421E-14 -7.5577E-15 5.3526E-14 7.9027E-14 -2.6935E-13 1.9399E-13 1.2926E-13 -8.2872E-14 7.9027E-14 9.5292E-13 # lat0 lon0 xBary yBary zBary JD0 27.706940 -122.662790 0.342621 0.441705 -0.841161 2456045.062196 # Heliocentric elements and errors Epoch: 2456044.5000 = 2012/04/27 Mean Anomaly: 356.30359 +/- 0.002 Argument of Peri: 135.75707 +/- 0.006 Long of Asc Node: 106.39458 +/- 0.000 Inclination: 33.88398 +/- 0.000 Eccentricity: 0.43891596 +/- 0.0000 Semi-Major Axis: 72.09888472 +/- 0.0054 Time of Perihelion: 2458340.4830 +/- 24.8 Perihelion: 40.45353372 +/- 0.0040 Aphelion: 103.74423572 +/- 0.0082 Period (y) 612.2109 +/- 0.07 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -19.82409840 +/- 0.0002 Ecliptic Y -30.29219527 +/- 0.0003 Ecliptic Z 18.51377649 +/- 0.0002 Ecliptic XDOT 0.00231547 +/- 0.0000 Ecliptic YDOT -0.00195789 +/- 0.0000 Ecliptic ZDOT -0.00112065 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 40.66171734 +/- 0.0002 Geocenter to KBO 39.81940857 +/- 0.0004 # Hcoef: 6.66
The following table shows the complete astrometric record for 14KE113. 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 (14KE113) followed by the observatory code and reference code for the source of the astrometry.
2012 04 27.56143 16 04 45.591 +07 28 32.76 22.0G 14KE113 F51 C~346Z 2012 05 14.36357 16 03 28.573 +07 33 34.08 22.6G 14KE113 F51 C~346Z 2012 05 14.37616 16 03 28.493 +07 33 34.12 23.0G 14KE113 F51 C~346Z 2012 05 14.38879 16 03 28.433 +07 33 34.16 22.6G 14KE113 F51 C~346Z 2012 05 14.40144 16 03 28.370 +07 33 34.28 22.7G 14KE113 F51 C~346Z 2013 03 08.63091 16 12 31.363 +06 05 59.18 22.2G 14KE113 F51 C~346Z 2013 06 17.42717 16 06 28.768 +06 37 08.05 22.9G 14KE113 F51 C~346Z 2014 05 09.45069 16 15 16.611 +05 37 45.73 22.1G 14KE113 F51 C~346Z 2014 05 21.49311 16 14 19.242 +05 40 15.26 23.0G 14KE113 F51 C~346Z 2014 05 21.50450 16 14 19.173 +05 40 15.08 22.0G 14KE113 F51 C~346Z 2014 05 21.51583 16 14 19.125 +05 40 15.25 22.4G 14KE113 F51 C~346Z 2014 05 21.52716 16 14 19.063 +05 40 15.38 22.7G 14KE113 F51 C~346Z 2014 05 27.42528 16 13 50.308 +05 40 54.30 22.5G 14KE113 F51 C~346Z 2014 05 27.44816 16 13 50.199 +05 40 54.34 22.7G 14KE113 F51 C~346Z 2014 05 27.45967 16 13 50.119 +05 40 54.27 21.9G 14KE113 F51 C~346Z 2014 06 18.44570 16 12 05.981 +05 39 46.23 23.0G 14KE113 F51 C~346Z 2014 06 28.37435 16 11 23.933 +05 37 22.51 22.7G 14KE113 F51 C~346Z 2014 06 28.38590 16 11 23.890 +05 37 22.57 23.2G 14KE113 F51 C~346Z 2014 06 28.39745 16 11 23.829 +05 37 22.28 22.7G 14KE113 F51 C~346Z 2014 06 28.40900 16 11 23.782 +05 37 22.02 22.9G 14KE113 F51 C~346Z 2014 07 31.32201 16 09 48.574 +05 21 48.57 22.1G 14KE113 F51 C~346Z 2014 07 31.33413 16 09 48.526 +05 21 48.09 22.9G 14KE113 F51 C~346Z 2014 07 31.34623 16 09 48.515 +05 21 47.72 22.4G 14KE113 F51 C~346Z 2014 08 20.25403 16 09 34.781 +05 07 53.60 22.6G 14KE113 F51 C~346Z 2014 08 20.26612 16 09 34.771 +05 07 53.15 22.4G 14KE113 F51 C~346Z 2014 08 20.27822 16 09 34.785 +05 07 53.02 22.7G 14KE113 F51 C~346Z 2014 08 20.29033 16 09 34.775 +05 07 52.11 23.4G 14KE113 F51 C~346a 2014 08 21.25167 16 09 35.063 +05 07 08.17 22.7G 14KE113 F51 C~346a 2014 08 21.26382 16 09 35.067 +05 07 07.78 22.5G 14KE113 F51 C~346a 2014 08 21.27590 16 09 35.081 +05 07 07.22 22.3G 14KE113 F51 C~346a 2014 08 21.28800 16 09 35.079 +05 07 06.39 22.6G 14KE113 F51 C~346a 2015 04 12.61975 16 22 44.644 +04 29 49.09 22.8G 14KE113 F51 C~346a 2015 06 20.31214 16 17 39.482 +04 41 51.21 22.6G 14KE113 F51 C~346a 2015 06 20.32477 16 17 39.424 +04 41 50.96 22.6G 14KE113 F51 C~346a 2015 06 20.33745 16 17 39.368 +04 41 50.85 22.5G 14KE113 F51 C~346a 2015 06 20.35015 16 17 39.310 +04 41 50.48 22.6G 14KE113 F51 C~346a 2015 08 17.31099 16 15 09.044 +04 13 43.05 23.3G 14KE113 F51 C~346a 2016 03 19.61848 16 29 11.848 +03 20 41.29 22.2G 14KE113 F51 C~346a 2016 03 19.62507 16 29 11.842 +03 20 41.45 23.1G 14KE113 F51 C~346a 2016 03 19.62714 16 29 11.841 +03 20 41.49 22.9G 14KE113 F51 C~346a 2016 03 19.63385 16 29 11.842 +03 20 41.63 22.6G 14KE113 F51 C~346a 2016 04 02.57930 16 28 48.673 +03 27 37.88 22.4G 14KE113 F51 C~346a 2016 04 10.59033 16 28 27.740 +03 31 23.63 22.7G 14KE113 F51 C~346a 2016 04 10.60223 16 28 27.699 +03 31 24.19 22.6G 14KE113 F51 C~346a 2016 04 10.61411 16 28 27.662 +03 31 24.73 22.7G 14KE113 F51 C~346a 2016 04 10.62594 16 28 27.619 +03 31 24.97 23.0G 14KE113 F51 C~346a 2016 04 20.55126 16 27 54.935 +03 35 40.78 22.8G 14KE113 F51 C~346a 2016 05 06.55374 16 26 49.741 +03 41 12.67 22.1G 14KE113 F51 C~346a 2016 05 13.49929 16 26 17.925 +03 42 56.99 23.0G 14KE113 F51 C~346a 2016 05 13.51206 16 26 17.879 +03 42 57.31 22.3G 14KE113 F51 C~346a 2016 05 13.52474 16 26 17.775 +03 42 57.45 21.2G 14KE113 F51 C~346a 2016 05 13.53744 16 26 17.755 +03 42 57.55 22.4G 14KE113 F51 C~346a 2016 05 27.47505 16 25 10.619 +03 45 03.44 22.2G 14KE113 F51 C~346a 2016 05 27.48718 16 25 10.553 +03 45 03.24 22.1G 14KE113 F51 C~346a 2016 05 27.49934 16 25 10.473 +03 45 03.37 22.9G 14KE113 F51 C~346a 2016 06 23.41421 16 23 03.349 +03 43 10.25 22.8G 14KE113 F51 C~346a 2016 07 01.41838 16 22 30.031 +03 41 03.12 22.3G 14KE113 F51 C~346a 2016 07 05.40166 16 22 14.693 +03 39 44.64 22.8G 14KE113 F51 C~346a 2016 07 05.40244 16 22 14.665 +03 39 44.70 23.5G 14KE113 F51 C~346a 2016 07 05.41371 16 22 14.642 +03 39 44.33 23.0G 14KE113 F51 C~346a 2016 07 05.41448 16 22 14.632 +03 39 44.43 22.8G 14KE113 F51 C~346a 2016 07 05.42582 16 22 14.597 +03 39 44.06 22.4G 14KE113 F51 C~346a 2016 07 05.42660 16 22 14.598 +03 39 44.19 22.8G 14KE113 F51 C~346a 2016 07 28.32491 16 21 07.206 +03 29 06.63 23.4G 14KE113 F51 C~346a 2017 04 27.53072 16 33 09.758 +02 40 03.28 22.3G 14KE113 F51 C~346a 2017 04 27.54334 16 33 09.703 +02 40 03.48 22.6G 14KE113 F51 C~346a 2017 04 27.55595 16 33 09.645 +02 40 03.89 22.0G 14KE113 F51 C~346a 2017 04 27.56853 16 33 09.607 +02 40 04.17 22.7G 14KE113 F51 C~346a 2017 05 18.54137 16 31 36.825 +02 45 36.03 22.6G 14KE113 F51 C~346a 2017 05 30.51459 16 30 38.650 +02 46 56.94 22.5G 14KE113 F51 C~346a 2017 05 30.52699 16 30 38.568 +02 46 57.60 21.8G 14KE113 F51 C~346a 2017 06 25.34274 16 28 36.874 +02 44 43.00 22.5G 14KE113 F51 C~346a 2017 06 25.35547 16 28 36.821 +02 44 42.84 22.6G 14KE113 F51 C~346a 2017 06 25.36821 16 28 36.756 +02 44 42.54 22.8G 14KE113 F51 C~346a 2017 06 25.38092 16 28 36.698 +02 44 42.42 22.3G 14KE113 F51 C~346a 2018 04 13.59697 16 39 38.861 +01 36 26.97 22.5G 14KE113 F51 C~346a 2018 04 13.60595 16 39 38.818 +01 36 27.09 23.1G 14KE113 F51 C~346a 2018 04 13.61500 16 39 38.808 +01 36 27.39 22.6G 14KE113 F51 C~346a 2018 04 13.62401 16 39 38.770 +01 36 27.61 22.6G 14KE113 F51 C~346a 2018 05 22.49473 16 37 00.696 +01 47 46.61 21.4G 14KE113 F51 C~346a 2018 05 22.50776 16 37 00.610 +01 47 46.62 22.7G 14KE113 F51 C~346a 2018 05 22.54944 16 37 00.402 +01 47 47.18 22.5G 14KE113 F51 C~346a 2018 06 13.36104 16 35 14.198 +01 48 20.91 22.5G 14KE113 F51 C~346a 2018 06 13.37312 16 35 14.098 +01 48 21.03 22.5G 14KE113 F51 C~346a 2018 06 13.38519 16 35 14.064 +01 48 21.19 22.9G 14KE113 F51 C~346a 2018 06 13.39731 16 35 13.992 +01 48 20.93 21.8G 14KE113 F51 C~346a 2018 06 21.35293 16 34 36.762 +01 47 19.47 23.2G 14KE113 F51 C~346a 2018 07 05.35151 16 33 37.006 +01 43 55.48 22.8G 14KE113 F51 C~346a 2018 07 05.36384 16 33 36.945 +01 43 55.16 22.2G 14KE113 F51 C~346a 2018 07 13.32339 16 33 07.510 +01 41 05.87 23.0G 14KE113 F51 C~346a 2018 07 13.33514 16 33 07.482 +01 41 05.52 22.5G 14KE113 F51 C~346a 2018 07 13.34683 16 33 07.434 +01 41 05.26 22.8G 14KE113 F51 C~346a 2020 06 22.38303 16 45 51.625 -00 09 29.95 22.4w 14KE113 F52 C~3xr2 2020 06 22.39422 16 45 51.582 -00 09 30.48 22.2w 14KE113 F52 C~3xr2 2020 06 22.41656 16 45 51.500 -00 09 30.40 22.4w 14KE113 F52 C~3xr2
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 -0.02 0.00 0.04
2 0.0460 0.00 0.27 0.00 0.28
3 0.0460 0.00 -0.01 0.00 0.16
4 0.0461 0.00 0.02 0.00 0.04
5 0.0461 0.00 -0.00 0.00 0.00
6 0.8626 0.00 -0.22 0.00 -0.07
7 1.1386 0.00 -0.10 0.00 -0.32
8 2.0312 0.00 -0.11 0.00 0.07
9 2.0642 0.00 0.02 0.00 0.21
10 2.0642 0.00 -0.17 0.00 -0.07
11 2.0642 0.00 -0.05 0.00 0.00
12 2.0642 0.00 -0.14 0.00 0.03
13 2.0804 0.00 0.46 0.00 -0.05
14 2.0805 0.00 0.53 0.00 -0.12
15 2.0805 0.00 0.19 0.00 -0.24
16 2.1407 0.00 0.18 0.00 0.41
17 2.1679 0.00 0.14 0.00 -0.18
18 2.1679 0.00 0.21 0.00 0.08
19 2.1679 0.00 -0.00 0.00 0.00
20 2.1680 0.00 -0.00 0.00 -0.05
21 2.2581 0.00 0.25 0.00 -0.17
22 2.2581 0.00 -0.16 0.00 -0.19
23 2.2581 0.00 -0.02 0.00 -0.10
24 2.3126 0.00 0.00 0.00 -0.16
25 2.3127 0.00 -0.18 0.00 -0.06
26 2.3127 0.00 0.00 0.00 0.36
27 2.3127 0.00 -0.18 0.00 0.00
28 2.3154 0.00 -0.14 0.00 -0.08
29 2.3154 0.00 -0.12 0.00 0.09
30 2.3154 0.00 0.04 0.00 0.08
31 2.3155 0.00 -0.04 0.00 -0.20
32 2.9570 0.00 -0.19 0.00 0.08
33 3.1451 0.00 -0.02 0.00 0.16
34 3.1451 0.00 -0.03 0.00 0.05
35 3.1452 0.00 -0.01 0.00 0.09
36 3.1452 0.00 -0.02 0.00 -0.14
37 3.3039 0.00 -0.03 0.00 0.13
38 3.8934 0.00 -0.04 0.00 -0.04
39 3.8934 0.00 -0.02 0.00 -0.08
40 3.8934 0.00 -0.00 0.00 -0.11
41 3.8934 0.00 0.12 0.00 -0.17
42 3.9316 0.00 -0.05 0.00 0.07
43 3.9535 0.00 0.08 0.00 -0.31
44 3.9536 0.00 0.01 0.00 -0.07
45 3.9536 0.00 -0.01 0.00 0.15
46 3.9536 0.00 -0.12 0.00 0.06
47 3.9808 0.00 -0.14 0.00 0.11
48 4.0246 0.00 0.02 0.00 0.37
49 4.0436 0.00 -0.19 0.00 -0.16
50 4.0437 0.00 0.03 0.00 -0.00
51 4.0437 0.00 -0.62 0.00 -0.03
52 4.0437 0.00 -0.01 0.00 -0.10
53 4.0819 0.00 0.18 0.00 0.17
54 4.0819 0.00 0.09 0.00 -0.09
55 4.0820 0.00 -0.20 0.00 -0.01
56 4.1557 0.00 0.02 0.00 0.03
57 4.1776 0.00 0.09 0.00 -0.20
58 4.1885 0.00 0.10 0.00 0.01
59 4.1885 0.00 -0.28 0.00 0.09
60 4.1885 0.00 0.02 0.00 -0.04
61 4.1885 0.00 -0.08 0.00 0.08
62 4.1885 0.00 0.04 0.00 -0.06
63 4.1885 0.00 0.10 0.00 0.09
64 4.2512 0.00 -0.16 0.00 -0.36
65 4.9992 0.00 -0.04 0.00 -0.02
66 4.9993 0.00 -0.10 0.00 -0.09
67 4.9993 0.00 -0.20 0.00 0.06
68 4.9993 0.00 -0.01 0.00 0.08
69 5.0568 0.00 0.08 0.00 -0.00
70 5.0895 0.00 0.36 0.00 -0.23
71 5.0896 0.00 0.05 0.00 0.39
72 5.1603 0.00 0.04 0.00 0.06
73 5.1603 0.00 0.09 0.00 0.07
74 5.1603 0.00 -0.03 0.00 -0.05
75 5.1604 0.00 -0.06 0.00 0.00
76 5.9604 0.00 0.10 0.00 0.05
77 5.9604 0.00 -0.14 0.00 -0.05
78 5.9604 0.00 0.12 0.00 0.03
79 5.9605 0.00 -0.04 0.00 0.02
80 6.0669 0.00 0.34 0.00 0.06
81 6.0669 0.00 0.01 0.00 -0.04
82 6.0670 0.00 -0.04 0.00 0.19
83 6.1268 0.00 0.35 0.00 -0.17
84 6.1268 0.00 -0.27 0.00 0.01
85 6.1268 0.00 0.11 0.00 0.23
86 6.1269 0.00 -0.09 0.00 0.03
87 6.1486 0.00 -0.08 0.00 -0.03
88 6.1870 0.00 0.08 0.00 0.24
89 6.1870 0.00 -0.09 0.00 0.16
90 6.2088 0.00 -0.08 0.00 -0.06
91 6.2088 0.00 0.12 0.00 -0.13
92 6.2089 0.00 0.02 0.00 -0.11
93 8.1528 0.00 -0.27 0.00 0.14
94 8.1529 0.00 -0.12 0.00 -0.27
95 8.1529 0.00 0.22 0.00 0.03
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.
14KE113 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 71.740 71.740 71.741 ecceobj 0.436 0.436 0.436 incobj 33.874 33.874 33.874 qmin 39.346 39.292 39.558 qmax 107.817 107.773 107.431 amean 72.674 72.674 72.674 amin 71.740 71.735 71.741 amax 73.924 73.889 73.890 emean 0.443 0.443 0.442 emin 0.432 0.431 0.433 emax 0.458 0.459 0.454 imean 32.246 32.233 32.285 imin 31.845 31.809 31.994 imax 32.636 32.645 32.565 excite_mean 0.694 0.694 0.694 fracstop 1.000 1.000 1.000 cjmean 2.770 2.770 2.770 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 216.6 218.6 208.9 kozaiamp 85.8 87.0 79.6