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: 14JQ92 # Created Fri Nov 22 02:09:54 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 114 observations of 114 # Arc: 12.34y # First observation: 2010/02/28 # Last observation: 2022/07/04 # Chi-squared of fit: 95.54 DOF: 222 RMS: 0.16 # Min/Max residuals: -0.46 0.57 # Exact a, adot, b, bdot, g, gdot: 1.941288E-05 5.466209E-02 3.116575E-06 7.447245E-03 3.877333E-02 1.084081E-03 # Covariance matrix: 2.3780E-13 -6.2870E-14 1.7449E-14 -7.7869E-15 6.1265E-15 -7.6513E-14 -6.2870E-14 2.2878E-14 -1.0124E-14 3.2141E-15 1.0367E-14 3.0877E-14 1.7449E-14 -1.0124E-14 1.0623E-13 -1.6288E-14 -1.3094E-14 -1.4367E-14 -7.7869E-15 3.2141E-15 -1.6288E-14 2.9846E-15 1.3794E-15 4.8950E-15 6.1265E-15 1.0367E-14 -1.3094E-14 1.3794E-15 4.3059E-14 1.1145E-14 -7.6513E-14 3.0877E-14 -1.4367E-14 4.8950E-15 1.1145E-14 4.7279E-14 # lat0 lon0 xBary yBary zBary JD0 22.938862 -128.862992 0.943518 0.123347 -0.291525 2455256.097976 # Heliocentric elements and errors Epoch: 2455256.5000 = 2010/03/01 Mean Anomaly: 358.09687 +/- 0.000 Argument of Peri: 74.25207 +/- 0.001 Long of Asc Node: 160.48167 +/- 0.000 Inclination: 24.17033 +/- 0.000 Eccentricity: 0.33826633 +/- 0.0000 Semi-Major Axis: 39.41524970 +/- 0.0014 Time of Perihelion: 2455734.3151 +/- 4.8 Perihelion: 26.08239773 +/- 0.0012 Aphelion: 52.74810166 +/- 0.0020 Period (y) 247.4598 +/- 0.01 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -15.83203787 +/- 0.0001 Ecliptic Y -18.15134328 +/- 0.0001 Ecliptic Z 10.05207256 +/- 0.0001 Ecliptic XDOT 0.00309220 +/- 0.0000 Ecliptic YDOT -0.00231137 +/- 0.0000 Ecliptic ZDOT 0.00051406 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 26.09922207 +/- 0.0001 Geocenter to KBO 25.79093997 +/- 0.0001 # Hcoef: 8.37
The following table shows the complete astrometric record for 14JQ92. 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 (14JQ92) followed by the observatory code and reference code for the source of the astrometry.
2010 02 28.59721 15 38 22.672 +04 08 56.67 21.4G 14JQ92 F51 C~346Y 2010 02 28.60780 15 38 22.644 +04 08 57.45 21.5G 14JQ92 F51 C~346Y 2010 04 19.55065 15 35 42.385 +04 56 44.59 22.1G 14JQ92 F51 C~346Y 2011 03 15.64329 15 50 49.515 +04 00 46.76 22.5G 14JQ92 F51 C~346Y 2011 04 28.59505 15 47 41.455 +04 40 45.69 22.4G 14JQ92 F51 C~346Y 2012 04 14.56168 16 01 48.526 +04 06 27.67 22.8G 14JQ92 F51 C~346Y 2012 04 27.55954 16 00 35.240 +04 16 55.76 22.8G 14JQ92 F51 C~346Y 2012 04 27.56995 16 00 35.179 +04 16 56.28 22.1G 14JQ92 F51 C~346Y 2012 04 27.58204 16 00 35.091 +04 16 57.13 22.0G 14JQ92 F51 C~346Y 2012 04 27.59326 16 00 35.039 +04 16 57.27 22.9G 14JQ92 F51 C~346Y 2013 06 18.33773 16 07 38.854 +04 10 40.11 22.9G 14JQ92 F51 C~346Y 2013 06 18.34881 16 07 38.809 +04 10 40.52 22.2G 14JQ92 F51 C~346Y 2013 06 18.36041 16 07 38.745 +04 10 40.09 22.4G 14JQ92 F51 C~346Y 2013 06 18.37057 16 07 38.688 +04 10 40.19 21.5G 14JQ92 F51 C~346Y 2014 04 23.56992 16 26 34.790 +03 24 18.10 22.0G 14JQ92 F51 C~346Y 2014 05 09.41168 16 25 00.305 +03 35 12.39 22.2G 14JQ92 F51 C~346Y 2014 05 09.41244 16 25 00.314 +03 35 12.63 22.0G 14JQ92 F51 C~346Y 2014 05 09.42492 16 25 00.230 +03 35 12.75 22.5G 14JQ92 F51 C~346Y 2014 05 09.43666 16 25 00.146 +03 35 13.26 22.6G 14JQ92 F51 C~346Y 2014 05 09.43743 16 25 00.158 +03 35 13.35 22.1G 14JQ92 F51 C~346Y 2014 05 09.44918 16 25 00.055 +03 35 13.60 22.1G 14JQ92 F51 C~346Y 2014 05 09.44995 16 25 00.057 +03 35 13.58 22.8G 14JQ92 F51 C~346Y 2014 05 09.53633 16 24 59.493 +03 35 16.83 22.3G 14JQ92 F51 C~346Y 2014 05 09.53699 16 24 59.493 +03 35 16.72 22.4G 14JQ92 F51 C~346Y 2014 05 09.54846 16 24 59.405 +03 35 17.34 23.1G 14JQ92 F51 C~346Y 2014 05 09.54912 16 24 59.402 +03 35 17.13 22.6G 14JQ92 F51 C~346Y 2014 05 09.56055 16 24 59.313 +03 35 17.97 22.1G 14JQ92 F51 C~346Y 2014 05 09.56121 16 24 59.351 +03 35 17.34 23.0G 14JQ92 F51 C~346Y 2014 05 09.57267 16 24 59.239 +03 35 17.98 22.5G 14JQ92 F51 C~346Y 2014 05 09.57333 16 24 59.254 +03 35 18.12 22.4G 14JQ92 F51 C~346Y 2014 05 21.49244 16 23 38.646 +03 41 15.32 22.5G 14JQ92 F51 C~346Y 2014 05 21.50384 16 23 38.556 +03 41 15.12 22.2G 14JQ92 F51 C~346Y 2014 06 28.37501 16 19 25.251 +03 44 29.95 22.4G 14JQ92 F51 C~346Y 2014 06 28.38656 16 19 25.171 +03 44 29.81 22.8G 14JQ92 F51 C~346Y 2014 06 28.39810 16 19 25.117 +03 44 29.70 22.6G 14JQ92 F51 C~346Y 2014 06 28.40966 16 19 25.065 +03 44 29.48 22.4G 14JQ92 F51 C~346Y 2014 08 21.25167 16 16 56.776 +03 10 07.58 22.0G 14JQ92 F51 C~346Y 2014 08 21.26382 16 16 56.795 +03 10 06.60 22.1G 14JQ92 F51 C~346Y 2014 08 21.27590 16 16 56.791 +03 10 06.02 22.5G 14JQ92 F51 C~346Y 2014 08 21.28800 16 16 56.825 +03 10 05.64 22.6G 14JQ92 F51 C~346Y 2015 03 23.55337 16 40 53.139 +02 31 35.76 22.3G 14JQ92 F51 C~346Y 2015 03 23.58031 16 40 53.105 +02 31 38.03 23.3G 14JQ92 F51 C~346Y 2015 05 14.51261 16 37 12.273 +03 12 29.37 23.1G 14JQ92 F51 C~346Y 2015 06 20.31479 16 32 58.958 +03 20 47.51 22.0G 14JQ92 F51 C~346Y 2015 06 20.32741 16 32 58.877 +03 20 47.36 22.0G 14JQ92 F51 C~346Y 2015 06 20.34010 16 32 58.793 +03 20 47.25 22.0G 14JQ92 F51 C~346Y 2015 06 20.35278 16 32 58.712 +03 20 47.27 22.1G 14JQ92 F51 C~346Y 2015 08 17.32580 16 29 17.350 +02 49 43.77 22.6G 14JQ92 F51 C~346Y 2016 04 02.54767 16 53 00.405 +02 16 08.44 23.0G 14JQ92 F51 C~346Y 2016 04 02.56077 16 53 00.372 +02 16 09.23 23.0G 14JQ92 F51 C~346Y 2016 04 02.57393 16 53 00.319 +02 16 09.86 22.6G 14JQ92 F51 C~346Y 2016 04 02.58726 16 53 00.317 +02 16 10.64 23.0G 14JQ92 F51 C~346Y 2016 04 10.58569 16 52 38.549 +02 23 11.21 23.2G 14JQ92 F51 C~346Y 2016 04 10.59759 16 52 38.518 +02 23 11.91 22.4G 14JQ92 F51 C~346Y 2016 04 10.60946 16 52 38.468 +02 23 12.41 22.8G 14JQ92 F51 C~346Y 2016 04 10.62133 16 52 38.446 +02 23 13.22 22.5G 14JQ92 F51 C~346Y 2016 05 06.52447 16 50 36.120 +02 42 38.62 21.3G 14JQ92 F51 C~346Y 2016 05 06.53651 16 50 36.046 +02 42 39.29 21.4G 14JQ92 F51 C~346Y 2016 05 06.54835 16 50 35.961 +02 42 39.77 21.7G 14JQ92 F51 C~346Y 2016 05 06.56024 16 50 35.898 +02 42 40.08 22.0G 14JQ92 F51 C~346Y 2016 05 13.50674 16 49 52.781 +02 46 37.16 22.5G 14JQ92 F51 C~346Y 2016 05 13.51943 16 49 52.702 +02 46 37.53 22.5G 14JQ92 F51 C~346Y 2016 05 13.53211 16 49 52.625 +02 46 38.11 22.7G 14JQ92 F51 C~346Y 2016 05 13.54493 16 49 52.530 +02 46 38.42 22.3G 14JQ92 F51 C~346Y 2016 05 27.46642 16 48 18.681 +02 52 28.85 22.0G 14JQ92 F51 C~346Y 2016 06 03.47127 16 47 29.523 +02 54 16.06 22.4G 14JQ92 F51 C~346Y 2016 06 03.48246 16 47 29.434 +02 54 16.29 22.2G 14JQ92 F51 C~346Y 2016 06 03.49364 16 47 29.361 +02 54 16.36 22.2G 14JQ92 F51 C~346Y 2016 06 03.50483 16 47 29.270 +02 54 16.63 22.4G 14JQ92 F51 C~346Y 2016 06 10.50818 16 46 40.110 +02 55 14.44 22.3G 14JQ92 F51 C~346Y 2016 06 23.40880 16 45 12.797 +02 54 50.44 22.1G 14JQ92 F51 C~346Y 2016 07 01.42162 16 44 22.746 +02 53 09.63 22.9G 14JQ92 F51 C~346Y 2016 07 05.39641 16 43 59.556 +02 51 56.16 22.0G 14JQ92 F51 C~346Y 2016 07 05.40846 16 43 59.489 +02 51 56.37 20.8G 14JQ92 F51 C~346Y 2016 07 05.42052 16 43 59.420 +02 51 55.49 22.3G 14JQ92 F51 C~346Y 2016 07 05.43262 16 43 59.334 +02 51 55.40 22.7G 14JQ92 F51 C~346Y 2016 07 28.30733 16 42 15.600 +02 40 09.07 22.7G 14JQ92 F51 C~346Y 2017 03 29.58728 17 05 26.327 +01 46 58.13 22.6G 14JQ92 F51 C~346Y 2017 03 29.59938 17 05 26.317 +01 46 58.69 22.5G 14JQ92 F51 C~346Y 2017 03 29.61148 17 05 26.301 +01 46 59.46 22.7G 14JQ92 F51 C~346Y 2017 03 29.62360 17 05 26.290 +01 46 59.79 22.5G 14JQ92 F51 C~346Y 2017 04 20.57514 17 04 27.480 +02 05 28.94 23.1G 14JQ92 F51 C~346Y 2017 05 04.48322 17 03 20.107 +02 15 20.91 22.6G 14JQ92 F51 C~346Y 2017 05 06.48903 17 03 08.839 +02 16 35.69 22.7G 14JQ92 F51 C~346Y 2017 05 18.58269 17 01 54.586 +02 23 03.52 21.9G 14JQ92 F51 C~346Y 2017 05 30.49475 17 00 33.868 +02 27 22.41 23.1G 14JQ92 F51 C~346Y 2017 05 30.50704 17 00 33.774 +02 27 23.08 22.1G 14JQ92 F51 C~346Y 2017 06 25.34856 16 57 35.192 +02 28 51.70 22.6G 14JQ92 F51 C~346Y 2017 06 25.36134 16 57 35.087 +02 28 51.75 22.5G 14JQ92 F51 C~346Y 2017 06 25.37412 16 57 35.026 +02 28 51.36 22.4G 14JQ92 F51 C~346Y 2017 06 25.38681 16 57 34.952 +02 28 51.49 22.3G 14JQ92 F51 C~346Y 2018 05 23.49192 17 13 50.552 +01 59 02.91 22.7G 14JQ92 F51 C~346Y 2018 05 23.50421 17 13 50.486 +01 59 03.26 22.3G 14JQ92 F51 C~346Y 2018 05 23.51641 17 13 50.408 +01 59 03.61 22.9G 14JQ92 F51 C~346Y 2018 05 23.52875 17 13 50.314 +01 59 03.86 22.7G 14JQ92 F51 C~346Y 2018 06 08.46122 17 12 00.943 +02 03 11.48 22.1G 14JQ92 F51 C~346Y 2018 06 08.47255 17 12 00.854 +02 03 11.57 22.2G 14JQ92 F51 C~346Y 2018 06 08.48329 17 12 00.793 +02 03 11.80 22.9G 14JQ92 F51 C~346Y 2018 06 08.49403 17 12 00.710 +02 03 11.99 22.6G 14JQ92 F51 C~346Y 2018 06 15.42419 17 11 12.127 +02 03 43.47 22.5G 14JQ92 F51 C~346Y 2018 06 15.43620 17 11 12.038 +02 03 43.64 22.7G 14JQ92 F51 C~346Y 2018 06 15.44816 17 11 11.947 +02 03 43.57 22.5G 14JQ92 F51 C~346Y 2018 06 15.46008 17 11 11.864 +02 03 43.41 22.7G 14JQ92 F51 C~346Y 2018 07 08.40047 17 08 41.246 +01 59 50.05 22.4G 14JQ92 F51 C~346Y 2018 07 08.41235 17 08 41.173 +01 59 49.75 22.8G 14JQ92 F51 C~346Y 2018 07 08.42423 17 08 41.107 +01 59 49.65 22.6G 14JQ92 F51 C~346Y 2018 07 08.43608 17 08 41.035 +01 59 49.34 23.0G 14JQ92 F51 C~346Y 2018 08 03.31788 17 06 38.868 +01 45 52.07 22.0G 14JQ92 F51 C~346Y 2018 08 03.32996 17 06 38.824 +01 45 51.07 22.2G 14JQ92 F51 C~346Y 2018 08 03.34198 17 06 38.785 +01 45 51.18 22.5G 14JQ92 F51 C~346Y 2018 08 03.35402 17 06 38.733 +01 45 50.50 21.9G 14JQ92 F51 C~346Y 2018 08 13.29115 17 06 12.285 +01 38 17.50 23.0G 14JQ92 F51 C~346Y 2022 07 04.315450 17 57 28.543 +00 19 58.67 22.7G 14JQ92 G37 C~5i37 2022 07 04.381170 17 57 28.103 +00 19 57.74 14JQ92 G37 C~5i37
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 0.57 0.00 -0.16
2 0.0000 0.00 0.14 0.00 0.01
3 0.1368 0.00 0.37 0.00 0.30
4 1.0405 0.00 -0.12 0.00 -0.32
5 1.1608 0.00 -0.18 0.00 0.23
6 2.1245 0.00 -0.03 0.00 0.00
7 2.1601 0.00 -0.21 0.00 -0.09
8 2.1601 0.00 -0.14 0.00 -0.02
9 2.1601 0.00 -0.33 0.00 0.29
10 2.1602 0.00 -0.05 0.00 -0.06
11 3.3011 0.00 -0.46 0.00 -0.20
12 3.3012 0.00 -0.08 0.00 0.26
13 3.3012 0.00 0.07 0.00 -0.11
14 3.3012 0.00 0.19 0.00 0.05
15 4.1478 0.00 0.23 0.00 0.24
16 4.1911 0.00 -0.24 0.00 0.02
17 4.1911 0.00 -0.03 0.00 0.23
18 4.1912 0.00 -0.05 0.00 -0.09
19 4.1912 0.00 -0.14 0.00 0.01
20 4.1912 0.00 0.11 0.00 0.07
21 4.1912 0.00 -0.26 0.00 -0.10
22 4.1912 0.00 -0.16 0.00 -0.14
23 4.1915 0.00 -0.01 0.00 0.06
24 4.1915 0.00 0.05 0.00 -0.07
25 4.1915 0.00 -0.13 0.00 0.15
26 4.1915 0.00 -0.10 0.00 -0.09
27 4.1915 0.00 -0.30 0.00 0.35
28 4.1916 0.00 0.33 0.00 -0.30
29 4.1916 0.00 -0.21 0.00 -0.06
30 4.1916 0.00 0.08 0.00 0.05
31 4.2242 0.00 0.11 0.00 0.26
32 4.2242 0.00 -0.03 0.00 -0.22
33 4.3279 0.00 -0.03 0.00 -0.12
34 4.3280 0.00 -0.21 0.00 -0.09
35 4.3280 0.00 0.00 0.00 -0.03
36 4.3280 0.00 0.25 0.00 -0.08
37 4.4754 0.00 -0.06 0.00 0.14
38 4.4755 0.00 0.09 0.00 -0.16
39 4.4755 0.00 -0.11 0.00 -0.05
40 4.4755 0.00 0.26 0.00 0.25
41 5.0622 0.00 0.03 0.00 -0.23
42 5.0622 0.00 -0.01 0.00 0.54
43 5.2044 0.00 -0.05 0.00 -0.03
44 5.3052 0.00 -0.08 0.00 -0.00
45 5.3052 0.00 -0.03 0.00 -0.08
46 5.3053 0.00 -0.02 0.00 -0.13
47 5.3053 0.00 0.03 0.00 -0.04
48 5.4640 0.00 0.21 0.00 0.16
49 6.0916 0.00 0.11 0.00 -0.17
50 6.0916 0.00 0.07 0.00 -0.08
51 6.0917 0.00 -0.27 0.00 -0.16
52 6.0917 0.00 0.16 0.00 -0.09
53 6.1136 0.00 0.00 0.00 -0.11
54 6.1136 0.00 0.14 0.00 -0.02
55 6.1137 0.00 -0.01 0.00 -0.13
56 6.1137 0.00 0.27 0.00 0.07
57 6.1846 0.00 0.02 0.00 -0.16
58 6.1846 0.00 0.01 0.00 0.07
59 6.1847 0.00 -0.18 0.00 0.11
60 6.1847 0.00 -0.04 0.00 -0.02
61 6.2037 0.00 -0.03 0.00 -0.16
62 6.2038 0.00 0.04 0.00 -0.18
63 6.2038 0.00 0.13 0.00 -0.00
64 6.2038 0.00 -0.03 0.00 -0.09
65 6.2419 0.00 -0.01 0.00 0.11
66 6.2611 0.00 0.08 0.00 -0.12
67 6.2612 0.00 -0.05 0.00 -0.02
68 6.2612 0.00 0.06 0.00 -0.08
69 6.2612 0.00 -0.10 0.00 0.06
70 6.2804 0.00 0.01 0.00 -0.18
71 6.3157 0.00 -0.37 0.00 0.28
72 6.3376 0.00 0.22 0.00 -0.12
73 6.3485 0.00 -0.03 0.00 -0.01
74 6.3486 0.00 0.01 0.00 0.45
75 6.3486 0.00 0.03 0.00 -0.19
76 6.3486 0.00 -0.21 0.00 -0.03
77 6.4113 0.00 0.29 0.00 -0.16
78 7.0801 0.00 -0.07 0.00 0.07
79 7.0801 0.00 0.02 0.00 -0.02
80 7.0801 0.00 0.01 0.00 0.11
81 7.0802 0.00 0.08 0.00 -0.20
82 7.1403 0.00 0.24 0.00 0.20
83 7.1783 0.00 0.18 0.00 0.25
84 7.1838 0.00 0.04 0.00 -0.05
85 7.2169 0.00 0.08 0.00 0.19
86 7.2495 0.00 0.08 0.00 -0.25
87 7.2496 0.00 -0.03 0.00 0.22
88 7.3203 0.00 -0.13 0.00 0.04
89 7.3204 0.00 -0.42 0.00 0.21
90 7.3204 0.00 -0.05 0.00 -0.06
91 7.3204 0.00 0.11 0.00 0.20
92 8.2297 0.00 -0.19 0.00 -0.17
93 8.2297 0.00 0.06 0.00 -0.10
94 8.2298 0.00 0.13 0.00 -0.03
95 8.2298 0.00 -0.04 0.00 -0.06
96 8.2734 0.00 0.03 0.00 -0.11
97 8.2734 0.00 -0.09 0.00 -0.11
98 8.2735 0.00 0.14 0.00 0.04
99 8.2735 0.00 0.05 0.00 0.14
100 8.2925 0.00 0.12 0.00 0.00
101 8.2925 0.00 0.07 0.00 0.16
102 8.2925 0.00 -0.02 0.00 0.08
103 8.2926 0.00 0.01 0.00 -0.10
104 8.3554 0.00 -0.07 0.00 -0.03
105 8.3554 0.00 -0.08 0.00 -0.08
106 8.3554 0.00 0.01 0.00 0.08
107 8.3555 0.00 0.00 0.00 0.02
108 8.4263 0.00 0.08 0.00 0.07
109 8.4264 0.00 0.04 0.00 -0.42
110 8.4264 0.00 0.08 0.00 0.20
111 8.4264 0.00 -0.08 0.00 0.03
112 8.4536 0.00 0.21 0.00 0.03
113 12.3442 0.00 -0.24 0.00 0.09
114 12.3444 0.00 -0.15 0.00 0.16
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.
14JQ92 quality flag:3 Type: 3:2E 3:2E 3:2E Type: 6:4II 6:4II 6:4II axisobj 39.103 39.103 39.103 ecceobj 0.333 0.333 0.333 incobj 24.188 24.188 24.188 qmin 25.296 25.295 25.297 qmax 54.188 54.184 54.192 amean 39.453 39.453 39.453 amin 39.098 39.098 39.098 amax 39.933 39.930 39.936 emean 0.286 0.286 0.286 emin 0.165 0.165 0.165 emax 0.357 0.357 0.357 imean 25.228 25.228 25.229 imin 22.547 22.547 22.546 imax 28.851 28.851 28.851 excite_mean 0.517 0.517 0.517 fracstop 1.000 1.000 1.000 cjmean 2.743 2.743 2.743 libcent 0 178.7 178.8 178.7 libamp 0 31.3 31.3 31.2 libcent 1 178.3 178.7 178.2 libamp 1 163.5 164.4 163.3 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 94.4 94.4 94.4 kozaiamp 67.5 67.5 67.5