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: 19UE174 # Created Mon Apr 28 01:11:19 2025 # Orbit generated from Bernstein formalism # Fitting 54 observations of 54 # Arc: 33.86d # First observation: 2019/09/29 # Last observation: 2019/11/02 Preliminary a, adot, b, bdot, g, gdot: 0.000000 0.030368 0.000000 0.012679 0.028325 0.000000 # Chi-squared of fit: 34.15 DOF: 102 RMS: 0.14 # Min/Max residuals: -0.47 0.29 # Exact a, adot, b, bdot, g, gdot: 1.654403E-05 3.056009E-02 7.438515E-06 1.266378E-02 2.830526E-02 1.061048E-03 # Covariance matrix: 1.2831E-13 3.0187E-11 1.9254E-14 1.6476E-12 5.8357E-12 3.6599E-10 3.0187E-11 7.3547E-08 4.4095E-11 3.2321E-09 1.2332E-08 2.0849E-07 1.9254E-14 4.4095E-11 1.1737E-13 7.8853E-13 7.4071E-12 1.3031E-10 1.6476E-12 3.2321E-09 7.8853E-13 1.6601E-10 5.4861E-10 1.2275E-08 5.8357E-12 1.2332E-08 7.4071E-12 5.4861E-10 2.0825E-09 4.1641E-08 3.6599E-10 2.0849E-07 1.3031E-10 1.2275E-08 4.1641E-08 3.7856E-06 # lat0 lon0 xBary yBary zBary JD0 -17.039016 31.045734 0.420126 -0.265818 -0.867336 2458755.958091 # Heliocentric elements and errors Epoch: 2458750.5000 = 2019/09/24 Mean Anomaly: 4.29975 +/- 9.374 Argument of Peri: 314.38826 +/- 16.454 Long of Asc Node: 65.16947 +/- 0.237 Inclination: 27.58849 +/- 0.142 Eccentricity: 0.25320784 +/- 0.0198 Semi-Major Axis: 48.38894949 +/- 0.9525 Time of Perihelion: 2457282.0535 +/- 3200.9 Perihelion: 36.13648831 +/- 1.1951 Aphelion: 60.64141067 +/- 1.5320 Period (y) 336.6104 +/- 9.94 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 29.93646819 +/- 0.0467 Ecliptic Y 17.52110807 +/- 0.0281 Ecliptic Z -10.35198931 +/- 0.0167 Ecliptic XDOT -0.00112437 +/- 0.0002 Ecliptic YDOT 0.00276917 +/- 0.0001 Ecliptic ZDOT 0.00114084 +/- 0.0001 # Distances at JD0 (AU) Heliocenter to KBO 36.19868835 +/- 0.0412 Geocenter to KBO 35.32912217 +/- 0.0570 # Hcoef: 8.90
The following table shows the complete astrometric record for 19UE174. 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 (19UE174) followed by the observatory code and reference code for the source of the astrometry.
2019 09 29.45729 02 19 07.82 -04 10 09.8 24.7r 19UE174 T09 C~7xXE 2019 09 29.46287 02 19 07.78 -04 10 10.0 24.8r 19UE174 T09 C~7xXE 2019 09 29.49462 02 19 07.63 -04 10 10.8 24.6i 19UE174 T09 C~7xXE 2019 09 29.51293 02 19 07.56 -04 10 11.5 24.2i 19UE174 T09 C~7xXE 2019 09 29.53122 02 19 07.46 -04 10 11.8 24.4i 19UE174 T09 C~7xXE 2019 09 29.55335 02 19 07.37 -04 10 12.7 24.5i 19UE174 T09 C~7xXE 2019 09 29.59096 02 19 07.19 -04 10 13.9 23.7z 19UE174 T09 C~7xXE 2019 09 29.59862 02 19 07.13 -04 10 14.2 23.7z 19UE174 T09 C~7xXE 2019 09 29.61677 02 19 07.07 -04 10 14.7 23.9z 19UE174 T09 C~7xXE 2019 09 29.62059 02 19 07.07 -04 10 14.7 24.5z 19UE174 T09 C~7xXE 2019 10 04.59083 02 18 43.74 -04 12 41.1 24.4z 19UE174 T09 C~7xXE 2019 10 04.59466 02 18 43.72 -04 12 41.1 24.0z 19UE174 T09 C~7xXE 2019 10 04.60998 02 18 43.65 -04 12 41.6 24.2z 19UE174 T09 C~7xXE 2019 10 04.61764 02 18 43.61 -04 12 41.7 24.9z 19UE174 T09 C~7xXE 2019 10 04.62530 02 18 43.58 -04 12 42.1 24.2z 19UE174 T09 C~7xXE 2019 10 04.62913 02 18 43.55 -04 12 42.3 24.3z 19UE174 T09 C~7xXE 2019 10 04.63296 02 18 43.54 -04 12 42.1 24.1z 19UE174 T09 C~7xXE 2019 10 04.63679 02 18 43.50 -04 12 42.4 23.9z 19UE174 T09 C~7xXE 2019 10 23.49622 02 17 05.81 -04 20 51.1 23.7z 19UE174 T09 C~7xXE 2019 10 23.50004 02 17 05.78 -04 20 51.1 23.9z 19UE174 T09 C~7xXE 2019 10 23.51827 02 17 05.68 -04 20 51.4 24.0z 19UE174 T09 C~7xXE 2019 10 23.52592 02 17 05.65 -04 20 51.6 23.4z 19UE174 T09 C~7xXE 2019 10 23.54029 02 17 05.56 -04 20 52.1 24.1z 19UE174 T09 C~7xXE 2019 10 23.54411 02 17 05.55 -04 20 52.1 24.1z 19UE174 T09 C~7xXE 2019 10 23.54794 02 17 05.50 -04 20 52.2 23.9z 19UE174 T09 C~7xXE 2019 10 23.56228 02 17 05.45 -04 20 52.4 23.7z 19UE174 T09 C~7xXE 2019 10 27.28540 02 16 45.18 -04 22 11.7 24.3r 19UE174 T09 C~7xXE 2019 10 27.29655 02 16 45.11 -04 22 11.7 24.5r 19UE174 T09 C~7xXE 2019 10 27.30773 02 16 45.05 -04 22 12.1 24.4r 19UE174 T09 C~7xXE 2019 10 27.31891 02 16 44.99 -04 22 12.2 24.5r 19UE174 T09 C~7xXE 2019 10 27.41777 02 16 44.44 -04 22 14.2 24.3i 19UE174 T09 C~7xXE 2019 10 27.42160 02 16 44.41 -04 22 14.2 24.6i 19UE174 T09 C~7xXE 2019 10 27.43602 02 16 44.33 -04 22 14.4 24.2i 19UE174 T09 C~7xXE 2019 10 27.43985 02 16 44.32 -04 22 14.6 24.0i 19UE174 T09 C~7xXE 2019 10 27.45429 02 16 44.23 -04 22 14.7 24.3i 19UE174 T09 C~7xXE 2019 10 27.45813 02 16 44.20 -04 22 14.9 24.2i 19UE174 T09 C~7xXE 2019 10 27.47257 02 16 44.14 -04 22 15.1 23.9i 19UE174 T09 C~7xXE 2019 10 27.47640 02 16 44.13 -04 22 15.4 24.1i 19UE174 T09 C~7xXE 2019 10 31.52506 02 16 21.94 -04 23 32.8 24.1z 19UE174 T09 C~7xXE 2019 10 31.52889 02 16 21.91 -04 23 33.0 24.0z 19UE174 T09 C~7xXE 2019 10 31.54707 02 16 21.81 -04 23 33.1 24.0z 19UE174 T09 C~7xXE 2019 10 31.55090 02 16 21.81 -04 23 33.1 23.9z 19UE174 T09 C~7xXE 2019 11 01.35249 02 16 17.43 -04 23 47.6 25.6g 19UE174 T09 C~7xXE 2019 11 01.36371 02 16 17.34 -04 23 47.6 26.0g 19UE174 T09 C~7xXE 2019 11 01.43281 02 16 16.98 -04 23 48.8 25.5g 19UE174 T09 C~7xXE 2019 11 01.44414 02 16 16.92 -04 23 49.1 25.5g 19UE174 T09 C~7xXE 2019 11 01.52311 02 16 16.45 -04 23 50.8 24.9g 19UE174 T09 C~7xXE 2019 11 01.53430 02 16 16.42 -04 23 50.9 25.6g 19UE174 T09 C~7xXE 2019 11 02.28153 02 16 12.35 -04 24 03.5 24.5i 19UE174 T09 C~7xXE 2019 11 02.28536 02 16 12.34 -04 24 03.7 24.0i 19UE174 T09 C~7xXE 2019 11 02.29968 02 16 12.25 -04 24 03.7 24.3i 19UE174 T09 C~7xXE 2019 11 02.30351 02 16 12.24 -04 24 03.9 24.4i 19UE174 T09 C~7xXE 2019 11 02.31783 02 16 12.16 -04 24 04.0 24.2i 19UE174 T09 C~7xXE 2019 11 02.32166 02 16 12.11 -04 24 04.0 24.9i 19UE174 T09 C~7xXE
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 0.11 0.00 -0.08
2 0.0000 -0.63 -0.10 0.02 -0.03
3 0.0001 -3.01 -0.09 0.03 0.12
4 0.0002 -4.24 0.07 -0.27 -0.10
5 0.0002 -5.74 -0.05 -0.04 0.21
6 0.0003 -7.32 0.05 -0.43 -0.07
7 0.0004 -10.26 -0.05 -0.63 -0.12
8 0.0004 -11.20 -0.42 -0.61 -0.06
9 0.0004 -12.22 -0.07 -0.77 -0.14
10 0.0004 -12.22 0.22 -0.77 -0.12
11 0.0141 -390.25 0.04 -19.13 0.01
12 0.0141 -390.53 0.06 -19.02 0.12
13 0.0141 -391.69 0.11 -19.14 0.04
14 0.0141 -392.28 0.12 -19.02 0.17
15 0.0141 -392.84 0.16 -19.25 -0.04
16 0.0142 -393.33 -0.03 -19.28 -0.07
17 0.0142 -393.40 0.20 -19.04 0.18
18 0.0142 -394.07 -0.16 -19.12 0.11
19 0.0658 -1934.44 -0.05 20.31 -0.13
20 0.0658 -1934.86 -0.15 20.46 -0.00
21 0.0659 -1936.37 -0.11 20.69 0.09
22 0.0659 -1936.86 0.06 20.65 -0.00
23 0.0659 -1938.29 -0.16 20.64 -0.12
24 0.0659 -1938.44 0.03 20.69 -0.10
25 0.0660 -1939.17 -0.39 20.86 0.04
26 0.0660 -1939.94 0.06 20.92 -0.00
27 0.0762 -2252.02 0.06 49.77 -0.25
28 0.0762 -2253.00 0.02 50.13 0.01
29 0.0763 -2253.98 -0.02 50.06 -0.16
30 0.0763 -2254.86 0.06 50.27 -0.05
31 0.0766 -2263.27 0.05 51.19 -0.04
32 0.0766 -2263.70 -0.04 51.35 0.07
33 0.0766 -2264.89 -0.01 51.57 0.16
34 0.0766 -2265.10 0.11 51.43 -0.01
35 0.0767 -2266.40 0.04 51.79 0.21
36 0.0767 -2266.89 -0.12 51.76 0.14
37 0.0767 -2267.80 0.19 51.88 0.13
38 0.0767 -2268.04 0.28 51.64 -0.14
39 0.0878 -2606.47 0.03 92.03 -0.03
40 0.0878 -2606.96 -0.14 91.99 -0.11
41 0.0879 -2608.40 -0.05 92.41 0.10
42 0.0879 -2608.40 0.27 92.41 0.05
43 0.0901 -2674.94 0.03 101.10 -0.13
44 0.0901 -2676.21 -0.29 101.56 0.20
45 0.0903 -2681.68 0.06 102.27 0.08
46 0.0903 -2682.62 0.07 102.29 -0.03
47 0.0905 -2689.81 -0.47 103.09 -0.18
48 0.0906 -2690.27 0.01 103.15 -0.25
49 0.0926 -2751.80 0.01 112.05 0.03
50 0.0926 -2752.01 0.12 111.91 -0.15
51 0.0927 -2753.27 0.05 112.37 0.13
52 0.0927 -2753.48 0.17 112.24 -0.05
53 0.0927 -2754.64 0.21 112.55 0.09
54 0.0927 -2755.34 -0.18 112.80 0.29
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.
19UE174 quality flag:1 Type: SCATNEAR SCATNEAR SCATEXTD axisobj 48.872 56.770 45.158 ecceobj 0.260 0.400 0.196 incobj 27.524 27.161 27.996 qmin 34.874 33.497 34.952 qmax 62.711 79.889 55.017 amean 48.419 56.210 44.807 amin 47.847 55.413 44.422 amax 49.019 57.108 45.257 emean 0.256 0.382 0.198 emin 0.233 0.363 0.180 emax 0.280 0.401 0.217 imean 26.171 26.581 26.565 imin 25.598 25.872 26.019 imax 26.782 27.400 27.072 excite_mean 0.510 0.588 0.489 fracstop 1.000 1.000 1.000 cjmean 2.822 2.794 2.811 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 171.0 168.5 169.6 kozaiamp 179.9 180.0 180.0