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: 524747 # Created Wed Apr 24 01:08:30 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 54 observations of 54 # Arc: 14.22y # First observation: 2003/10/24 # Last observation: 2018/01/12 # Chi-squared of fit: 50.75 DOF: 102 RMS: 0.17 # Min/Max residuals: -0.47 0.43 # Exact a, adot, b, bdot, g, gdot: 1.692804E-05 2.775422E-02 -2.843357E-06 -5.426071E-03 2.552956E-02 -4.647798E-03 # 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 -0.607947 17.332941 -0.219698 -0.010271 -0.971289 2452936.715923 # Heliocentric elements and errors Epoch: 2452936.5000 = 2003/10/24 Mean Anomaly: 340.02610 +/- 0.000 Argument of Peri: 222.26898 +/- 0.000 Long of Asc Node: 194.62050 +/- 0.000 Inclination: 11.07608 +/- 0.000 Eccentricity: 0.31779883 +/- 0.0000 Semi-Major Axis: 55.64910947 +/- 0.0000 Time of Perihelion: 2461349.4057 +/- 0.0 Perihelion: 37.96388766 +/- 0.0000 Aphelion: 73.33433127 +/- 0.0000 Period (y) 415.1409 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 38.24790278 +/- 0.0000 Ecliptic Y 12.17210636 +/- 0.0000 Ecliptic Z -0.41571203 +/- 0.0000 Ecliptic XDOT -0.00137314 +/- 0.0000 Ecliptic YDOT 0.00268490 +/- 0.0000 Ecliptic ZDOT -0.00057642 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 40.14030263 +/- 0.0000 Geocenter to KBO 39.17043234 +/- 0.0000 # Hcoef: 6.81
The following table shows the complete astrometric record for 524747. 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 (524747) followed by the observatory code and reference code for the source of the astrometry.
2003 10 24.21518 01 04 51.01 +06 14 39.0 21.8R 524747 695 Cj5825 2003 10 24.31417 01 04 50.54 +06 14 36.0 524747 695 Cj5825 2003 11 20.12158 01 03 05.30 +06 02 30.6 21.9R 524747 695 Cj5825 2003 11 20.20624 01 03 05.01 +06 02 28.9 524747 695 Cj5825 2010 10 07.41581 01 52 25.025 +08 32 43.62 22.8w 524747 F51 C~1w3e 2010 10 07.43328 01 52 24.946 +08 32 43.24 23.3w 524747 F51 C~1w3e 2010 10 15.35532 01 51 48.141 +08 28 44.64 23.0G 524747 F51 C~343k 2010 11 02.42699 01 50 22.181 +08 19 48.45 23.5w 524747 F51 C~1w3e 2010 11 02.44186 01 50 22.119 +08 19 47.86 23.5w 524747 F51 C~1w3e 2010 11 02.45796 01 50 22.008 +08 19 47.26 23.3w 524747 F51 C~1w3e 2010 11 02.47060 01 50 21.979 +08 19 47.07 23.1w 524747 F51 C~1w3e 2012 09 26.56997 02 06 56.589 +09 12 16.78 22.6G 524747 F51 C~343k 2012 10 08.42449 02 06 05.620 +09 06 38.96 22.2r 524747 F51 C~1w3e 2012 10 08.43659 02 06 05.560 +09 06 38.45 22.1G 524747 F51 C~343k 2012 10 08.51511 02 06 05.187 +09 06 36.34 21.8i 524747 F51 C~1w3e 2012 10 17.40350 02 05 23.687 +09 02 13.86 22.4w 524747 F51 C~1w3e 2012 10 17.41692 02 05 23.617 +09 02 13.51 22.3w 524747 F51 C~1w3e 2012 10 17.43034 02 05 23.564 +09 02 13.13 22.4w 524747 F51 C~1w3e 2012 10 17.44387 02 05 23.487 +09 02 12.84 22.5w 524747 F51 C~1w3e 2012 11 06.29497 02 03 47.968 +08 52 38.97 22.6G 524747 F51 C~343k 2013 02 09.23675 02 01 20.392 +08 41 31.09 22.5w 524747 F51 C~1w3e 2013 02 09.24512 02 01 20.422 +08 41 30.82 22.2G 524747 F51 C~343k 2013 07 19.58019 02 15 16.355 +09 45 50.60 22.8G 524747 F51 C~343k 2013 10 03.46384 02 13 26.724 +09 25 51.65 22.6w 524747 F51 C~1w3e 2013 11 25.25047 02 09 21.007 +09 01 45.18 22.7w 524747 F51 C~1w3e 2013 11 25.26553 02 09 20.947 +09 01 45.12 22.5w 524747 F51 C~1w3e 2013 11 25.28051 02 09 20.891 +09 01 44.55 22.5w 524747 F51 C~1w3e 2013 11 25.29554 02 09 20.822 +09 01 44.31 22.8w 524747 F51 C~1w3e 2014 10 02.42744 02 20 32.514 +09 42 40.73 22.7G 524747 F51 C~343k 2014 11 17.50087 02 16 55.187 +09 21 17.66 22.6G 524747 F51 C~343k 2015 01 16.25804 02 14 18.307 +09 09 44.12 23.2G 524747 F51 C~343k 2015 01 22.27389 02 14 20.365 +09 10 16.99 23.4G 524747 F51 C~343k 2015 10 10.38939 02 27 02.020 +09 54 49.99 21.9G 524747 F51 C~343k 2015 10 10.40163 02 27 01.970 +09 54 49.64 23.1G 524747 F51 C~343k 2015 10 10.41387 02 27 01.921 +09 54 49.49 21.7G 524747 F51 C~343k 2015 10 10.42622 02 27 01.853 +09 54 49.12 22.1G 524747 F51 C~343k 2016 01 04.29530 02 21 20.700 +09 25 30.04 22.5G 524747 F51 C~343k 2016 01 04.30829 02 21 20.673 +09 25 30.12 23.0G 524747 F51 C~343k 2016 01 04.32124 02 21 20.669 +09 25 30.00 22.1G 524747 F51 C~343k 2016 01 04.33424 02 21 20.648 +09 25 29.72 23.2G 524747 F51 C~343k 2016 01 26.24169 02 21 14.818 +09 26 32.08 22.4G 524747 F51 C~343k 2016 02 01.25851 02 21 21.825 +09 27 34.05 21.8G 524747 F51 C~343k 2017 01 23.27489 02 28 07.400 +09 41 32.05 23.2G 524747 F51 C~343k 2017 08 03.57770 02 43 16.761 +10 45 17.51 23.1G 524747 F51 C~343k 2017 09 23.47066 02 42 18.833 +10 31 57.72 22.7G 524747 F51 C~343k 2017 09 27.59836 02 42 04.308 +10 30 14.57 22.0G 524747 F51 C~343k 2017 11 21.42789 02 37 48.994 +10 06 03.99 22.3G 524747 F51 C~343k 2017 11 21.43945 02 37 48.943 +10 06 03.83 22.8G 524747 F51 C~343k 2017 11 21.45101 02 37 48.897 +10 06 03.47 22.6G 524747 F51 C~343k 2017 11 21.46260 02 37 48.828 +10 06 03.32 22.3G 524747 F51 C~343k 2018 01 12.29263 02 35 07.897 +09 55 40.01 22.8G 524747 F51 C~343k 2018 01 12.30331 02 35 07.877 +09 55 40.23 23.0G 524747 F51 C~343k 2018 01 12.31396 02 35 07.849 +09 55 40.40 22.9G 524747 F51 C~343k 2018 01 12.32467 02 35 07.856 +09 55 40.43 23.1G 524747 F51 C~343k
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 0.09 0.00 -0.08
2 0.0003 0.00 -0.25 0.00 -0.07
3 0.0737 0.00 0.14 0.00 -0.08
4 0.0739 0.00 -0.01 0.00 0.13
5 6.9547 0.00 0.06 0.00 -0.09
6 6.9547 0.00 0.09 0.00 0.05
7 6.9764 0.00 0.08 0.00 -0.06
8 7.0259 0.00 0.14 0.00 0.30
9 7.0259 0.00 0.28 0.00 0.13
10 7.0260 0.00 -0.23 0.00 -0.00
11 7.0260 0.00 0.24 0.00 0.17
12 8.9264 0.00 -0.11 0.00 -0.47
13 8.9588 0.00 0.02 0.00 -0.07
14 8.9589 0.00 -0.04 0.00 -0.23
15 8.9591 0.00 -0.17 0.00 -0.04
16 8.9834 0.00 -0.22 0.00 0.04
17 8.9834 0.00 -0.29 0.00 0.09
18 8.9835 0.00 -0.11 0.00 0.10
19 8.9835 0.00 -0.28 0.00 0.22
20 9.0379 0.00 -0.02 0.00 -0.08
21 9.2978 0.00 -0.14 0.00 0.43
22 9.2978 0.00 -0.04 0.00 0.02
23 9.7368 0.00 0.30 0.00 0.04
24 9.9446 0.00 0.30 0.00 -0.00
25 10.0891 0.00 -0.23 0.00 -0.15
26 10.0891 0.00 -0.18 0.00 0.12
27 10.0892 0.00 -0.07 0.00 -0.12
28 10.0892 0.00 -0.15 0.00 -0.04
29 10.9410 0.00 0.10 0.00 0.03
30 11.0672 0.00 0.09 0.00 -0.10
31 11.2308 0.00 0.28 0.00 0.33
32 11.2473 0.00 0.07 0.00 -0.33
33 11.9621 0.00 -0.07 0.00 -0.15
34 11.9622 0.00 0.02 0.00 -0.15
35 11.9622 0.00 0.12 0.00 0.04
36 11.9622 0.00 -0.05 0.00 0.02
37 12.1973 0.00 0.15 0.00 -0.12
38 12.1974 0.00 0.03 0.00 0.00
39 12.1974 0.00 0.25 0.00 -0.08
40 12.1975 0.00 0.22 0.00 -0.31
41 12.2574 0.00 0.22 0.00 0.07
42 12.2739 0.00 -0.41 0.00 0.07
43 13.2514 0.00 -0.26 0.00 0.09
44 13.7779 0.00 -0.02 0.00 0.04
45 13.9172 0.00 0.01 0.00 0.06
46 13.9285 0.00 0.14 0.00 -0.15
47 14.0786 0.00 -0.07 0.00 -0.17
48 14.0786 0.00 -0.01 0.00 -0.07
49 14.0787 0.00 0.14 0.00 -0.16
50 14.0787 0.00 -0.06 0.00 -0.04
51 14.2206 0.00 0.16 0.00 -0.03
52 14.2206 0.00 0.02 0.00 0.18
53 14.2207 0.00 -0.24 0.00 0.34
54 14.2207 0.00 0.02 0.00 0.37
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.
524747 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 56.452 56.452 56.452 ecceobj 0.326 0.326 0.326 incobj 11.029 11.029 11.029 qmin 36.687 36.698 36.370 qmax 75.777 75.714 76.018 amean 55.684 55.480 55.600 amin 54.641 54.593 54.577 amax 56.547 56.479 56.562 emean 0.322 0.320 0.324 emin 0.303 0.299 0.304 emax 0.341 0.341 0.344 imean 11.092 11.322 11.146 imin 10.201 10.581 10.310 imax 11.938 12.020 12.125 excite_mean 0.375 0.375 0.377 fracstop 1.000 1.000 1.000 cjmean 3.067 3.064 3.064 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 181.0 182.6 185.0 kozaiamp 180.0 180.0 180.0