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: 09JE19 # Created Fri Apr 19 01:13:10 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 52 observations of 52 # Arc: 20.97y # First observation: 2003/03/31 # Last observation: 2024/03/18 # Chi-squared of fit: 21.80 DOF: 98 RMS: 0.11 # Min/Max residuals: -0.29 0.27 # Exact a, adot, b, bdot, g, gdot: 1.541554E-05 2.987764E-02 5.388123E-06 1.040697E-02 2.940653E-02 -9.429645E-03 # Covariance matrix: 1.7040E-07 -2.3175E-05 1.8105E-07 2.4097E-06 -4.2989E-07 -4.7348E-05 -2.3175E-05 2.4256E-02 -2.4515E-05 -2.5423E-03 5.8264E-05 4.9620E-02 1.8105E-07 -2.4515E-05 1.9236E-07 2.5489E-06 -4.5675E-07 -5.0085E-05 2.4097E-06 -2.5423E-03 2.5489E-06 2.6754E-04 -6.0580E-06 -5.2009E-03 -4.2989E-07 5.8264E-05 -4.5675E-07 -6.0580E-06 1.0845E-06 1.1904E-04 -4.7348E-05 4.9620E-02 -5.0085E-05 -5.2009E-03 1.1904E-04 1.0151E-01 # lat0 lon0 xBary yBary zBary JD0 12.023535 174.467881 -0.272391 0.199948 -0.938818 2452729.716854 # Heliocentric elements and errors Epoch: 2452730.5000 = 2003/04/01 Mean Anomaly: 308.93890 +/- 0.001 Argument of Peri: 116.56640 +/- 0.002 Long of Asc Node: 144.32723 +/- 0.000 Inclination: 22.13422 +/- 0.002 Eccentricity: 0.30045755 +/- 0.0000 Semi-Major Axis: 39.61940636 +/- 0.0000 Time of Perihelion: 2465650.0690 +/- 0.1 Perihelion: 27.71545640 +/- 0.0006 Aphelion: 51.52335631 +/- 0.0006 Period (y) 249.3849 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -34.08875143 +/- 0.0000 Ecliptic Y 3.03166817 +/- 0.0000 Ecliptic Z 7.08411724 +/- 0.0000 Ecliptic XDOT 0.00078104 +/- 0.0000 Ecliptic YDOT -0.00287575 +/- 0.0000 Ecliptic ZDOT 0.00076497 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 34.94896869 +/- 0.0000 Geocenter to KBO 34.00626111 +/- 0.0000 # Hcoef: 6.55
The following table shows the complete astrometric record for 09JE19. 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 (09JE19) followed by the observatory code and reference code for the source of the astrometry.
2003 03 31.216111 11 59 08.50 +13 12 59.1 22.2r 09JE19 645 C~4qBt 2003 03 31.216940 11 59 08.49 +13 12 59.2 21.4i 09JE19 645 C~4qBt 2003 03 31.218598 11 59 08.47 +13 12 59.4 21.1z 09JE19 645 C~4qBt 2003 03 31.219428 11 59 08.46 +13 12 59.5 23.1g 09JE19 645 C~4qBt 2009 04 23.349341 12 44 00.27 +12 12 50.6 23.6u 09JE19 568 C~4qBt 2009 04 23.393327 12 44 00.04 +12 12 51.7 23.5u 09JE19 568 C~4qBt 2009 05 15.469581 12 42 21.517 +12 18 39.25 21.7i 09JE19 568 C~0aRU 2009 05 20.331222 12 42 04.590 +12 18 59.90 21.9i 09JE19 568 C~0aRU 2009 05 20.364003 12 42 04.480 +12 19 00.00 21.9i 09JE19 568 C~0aRU 2009 05 20.401995 12 42 04.350 +12 19 00.10 21.8i 09JE19 568 C~0aRU 2009 05 26.258739 12 41 46.739 +12 18 57.25 23.0g 09JE19 568 C~0aRU 2009 05 26.306652 12 41 46.599 +12 18 57.03 23.1g 09JE19 568 C~0aRU 2009 05 26.354612 12 41 46.466 +12 18 56.86 23.1g 09JE19 568 C~0aRU 2009 07 20.249242 12 41 55.91 +11 56 40.2 21.6r 09JE19 568 C~4qBt 2009 07 20.263887 12 41 55.96 +11 56 39.5 21.6r 09JE19 568 C~4qBt 2016 03 02.328704 13 49 23.51 +09 17 40.2 21.3z 09JE19 W84 C~4qBt 2016 03 02.331192 13 49 23.49 +09 17 40.4 21.3z 09JE19 W84 C~4qBt 2016 06 08.049595 13 41 13.97 +10 06 30.2 09JE19 W84 C~4qBt 2016 06 08.052280 13 41 13.96 +10 06 30.4 21.1z 09JE19 W84 C~4qBt 2022 02 09.581897 14 46 58.529 +06 11 11.76 21.6w 09JE19 F52 C~5RrD 2022 02 09.592691 14 46 58.545 +06 11 12.29 21.7w 09JE19 F52 C~5RrD 2022 02 09.603538 14 46 58.560 +06 11 12.86 21.5w 09JE19 F52 C~5RrD 2022 02 09.614403 14 46 58.564 +06 11 13.31 21.6w 09JE19 F52 C~5RrD 2022 04 29.514587 14 42 18.832 +07 14 11.04 21.5w 09JE19 F52 C~5aXL 2022 04 29.526624 14 42 18.763 +07 14 11.21 21.4w 09JE19 F52 C~5aXL 2022 04 29.538719 14 42 18.693 +07 14 11.75 21.4w 09JE19 F52 C~5aXL 2022 06 05.288514 14 38 43.741 +07 24 30.12 21.6w 09JE19 F52 C~5few 2022 06 05.300095 14 38 43.674 +07 24 30.18 21.6w 09JE19 F52 C~5few 2022 06 05.311674 14 38 43.627 +07 24 30.23 21.5w 09JE19 F52 C~5few 2023 03 17.558078 14 56 07.743 +06 09 00.09 21.5w 09JE19 F51 C~6V4w 2023 03 17.570027 14 56 07.705 +06 09 00.72 21.4w 09JE19 F51 C~6V4w 2023 03 17.581997 14 56 07.665 +06 09 01.46 21.4w 09JE19 F51 C~6V4w 2023 03 27.533593 14 55 28.980 +06 17 41.52 21.5w 09JE19 F51 C~6hJ6 2023 03 27.554922 14 55 28.880 +06 17 42.51 21.6w 09JE19 F51 C~6hJ6 2023 03 27.565559 14 55 28.829 +06 17 43.20 21.6w 09JE19 F51 C~6hJ6 2023 05 09.313396 14 51 25.988 +06 46 53.20 21.2w 09JE19 F51 C~6mzI 2023 05 09.336554 14 51 25.831 +06 46 53.63 21.4w 09JE19 F51 C~6mzI 2023 05 09.353775 14 51 25.732 +06 46 54.01 21.4w 09JE19 F51 C~6mzI 2023 05 14.426667 14 50 54.041 +06 48 54.85 21.4w 09JE19 F51 C~6o8S 2023 05 14.437344 14 50 53.975 +06 48 55.21 21.5w 09JE19 F51 C~6o8S 2023 05 14.447977 14 50 53.904 +06 48 55.34 21.4w 09JE19 F51 C~6o8S 2023 05 14.458708 14 50 53.835 +06 48 55.63 21.4w 09JE19 F51 C~6o8S 2023 05 25.310808 14 49 48.177 +06 51 54.33 21.4w 09JE19 F51 C~6pjY 2023 05 25.322602 14 49 48.103 +06 51 54.49 21.4w 09JE19 F51 C~6pjY 2023 05 25.335985 14 49 48.017 +06 51 54.66 21.6w 09JE19 F51 C~6pjY 2023 05 25.347907 14 49 47.954 +06 51 54.77 21.3w 09JE19 F51 C~6pjY 2024 03 16.585918 15 06 17.175 +05 35 20.76 21.5w 09JE19 F51 C~7wKa 2024 03 16.612207 15 06 17.089 +05 35 22.42 21.2w 09JE19 F51 C~7wKa 2024 03 16.625313 15 06 17.036 +05 35 22.95 21.4w 09JE19 F51 C~7wKa 2024 03 18.572443 15 06 10.818 +05 37 05.25 21.5w 09JE19 F51 C~7wKa 2024 03 18.583933 15 06 10.791 +05 37 05.74 21.4w 09JE19 F51 C~7wKa 2024 03 18.595411 15 06 10.750 +05 37 06.41 21.5w 09JE19 F51 C~7wKa
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 0.14 0.00 -0.02
2 0.0000 0.00 0.06 0.00 0.06
3 0.0000 0.00 -0.11 0.00 0.20
4 0.0000 0.00 -0.19 0.00 0.27
5 6.0647 0.00 -0.21 0.00 -0.29
6 6.0648 0.00 -0.22 0.00 -0.28
7 6.1253 0.00 0.13 0.00 0.02
8 6.1386 0.00 0.24 0.00 -0.03
9 6.1387 0.00 0.25 0.00 0.01
10 6.1388 0.00 0.22 0.00 0.03
11 6.1548 0.00 -0.07 0.00 0.03
12 6.1549 0.00 -0.13 0.00 -0.04
13 6.1551 0.00 -0.09 0.00 -0.06
14 6.3054 0.00 0.01 0.00 0.01
15 6.3054 0.00 0.09 0.00 -0.07
16 12.9230 0.00 0.01 0.00 0.02
17 12.9230 0.00 -0.15 0.00 0.09
18 13.1905 0.00 -0.05 0.00 -0.22
19 13.1905 0.00 -0.07 0.00 0.00
20 18.8648 0.00 -0.14 0.00 -0.03
21 18.8648 0.00 -0.02 0.00 0.02
22 18.8649 0.00 0.09 0.00 0.11
23 18.8649 0.00 0.03 0.00 0.08
24 19.0809 0.00 0.00 0.00 0.11
25 19.0809 0.00 0.11 0.00 -0.12
26 19.0810 0.00 0.20 0.00 0.02
27 19.1816 0.00 -0.03 0.00 0.02
28 19.1816 0.00 -0.15 0.00 0.08
29 19.1816 0.00 0.03 0.00 0.14
30 19.9626 0.00 -0.00 0.00 -0.04
31 19.9626 0.00 0.05 0.00 -0.05
32 19.9627 0.00 0.08 0.00 0.06
33 19.9899 0.00 0.08 0.00 -0.03
34 19.9900 0.00 0.02 0.00 -0.13
35 19.9900 0.00 -0.02 0.00 0.01
36 20.1070 0.00 0.15 0.00 0.23
37 20.1071 0.00 0.01 0.00 0.05
38 20.1072 0.00 0.17 0.00 -0.02
39 20.1210 0.00 0.05 0.00 -0.11
40 20.1211 0.00 0.07 0.00 0.02
41 20.1211 0.00 0.02 0.00 -0.08
42 20.1211 0.00 -0.00 0.00 -0.02
43 20.1508 0.00 -0.04 0.00 -0.06
44 20.1509 0.00 -0.09 0.00 -0.04
45 20.1509 0.00 -0.19 0.00 -0.02
46 20.1509 0.00 -0.06 0.00 -0.04
47 20.9620 0.00 -0.05 0.00 -0.13
48 20.9621 0.00 -0.08 0.00 0.15
49 20.9621 0.00 -0.24 0.00 -0.01
50 20.9674 0.00 -0.01 0.00 0.03
51 20.9675 0.00 0.18 0.00 -0.08
52 20.9675 0.00 0.16 0.00 -0.01
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.
09JE19 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.253 39.253 39.253 ecceobj 0.299 0.299 0.299 incobj 22.201 22.201 22.201 qmin 26.753 26.736 26.767 qmax 52.850 52.797 52.697 amean 39.454 39.454 39.454 amin 39.007 39.008 38.993 amax 39.996 39.999 40.013 emean 0.260 0.260 0.260 emin 0.185 0.185 0.183 emax 0.322 0.321 0.319 imean 22.734 22.735 22.744 imin 20.437 20.395 20.501 imax 25.251 25.249 25.252 excite_mean 0.468 0.468 0.468 fracstop 1.000 1.000 1.000 cjmean 2.799 2.799 2.799 libcent 0 180.2 179.8 179.6 libamp 0 88.3 88.1 89.4 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 95.6 95.8 95.5 kozaiamp 57.8 57.6 57.8