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: 602572 # Created Thu Apr 25 01:09:03 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 55 observations of 55 # Arc: 13.24y # First observation: 2010/06/19 # Last observation: 2023/09/14 # Chi-squared of fit: 34.41 DOF: 104 RMS: 0.14 # Min/Max residuals: -0.37 0.35 # Exact a, adot, b, bdot, g, gdot: 1.730821E-05 3.232096E-02 1.324949E-06 7.849537E-05 2.768203E-02 -3.980483E-04 # 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 -11.097467 -30.184960 0.895379 -0.091799 -0.467696 2455367.114666 # Heliocentric elements and errors Epoch: 2455366.5000 = 2010/06/19 Mean Anomaly: 354.45524 +/- 0.000 Argument of Peri: 279.32102 +/- 0.000 Long of Asc Node: 59.11095 +/- 0.000 Inclination: 10.94987 +/- 0.000 Eccentricity: 0.27147376 +/- 0.0000 Semi-Major Axis: 50.08502066 +/- 0.0000 Time of Perihelion: 2457360.5689 +/- 0.0 Perihelion: 36.48825173 +/- 0.0000 Aphelion: 63.68178959 +/- 0.0000 Period (y) 354.4622 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 30.60862128 +/- 0.0000 Ecliptic Y -18.83853636 +/- 0.0000 Ecliptic Z -6.95310019 +/- 0.0000 Ecliptic XDOT 0.00157653 +/- 0.0000 Ecliptic YDOT 0.00278797 +/- 0.0000 Ecliptic ZDOT 0.00001516 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 36.60772553 +/- 0.0000 Geocenter to KBO 36.12454109 +/- 0.0000 # Hcoef: 6.96
The following table shows the complete astrometric record for 602572. 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 (602572) followed by the observatory code and reference code for the source of the astrometry.
2010 06 19.61390 22 24 20.959 -21 53 30.59 22.2G 602572 F51 C~2rY7 2010 08 18.42665 22 20 35.059 -22 24 41.32 23.0G 602572 F51 C~2rY7 2010 09 16.41727 22 18 02.037 -22 36 40.22 21.9G 602572 F51 C~2rY7 2011 08 01.49185 22 29 33.325 -21 33 14.67 22.6w 602572 F51 C~1vXb 2011 08 01.50438 22 29 33.253 -21 33 14.96 22.7w 602572 F51 C~1vXb 2011 08 01.51692 22 29 33.192 -21 33 15.40 22.7w 602572 F51 C~1vXb 2011 09 18.42732 22 25 25.978 -21 55 42.10 21.9G 602572 F51 C~2rY7 2011 09 18.43854 22 25 25.944 -21 55 42.27 22.4G 602572 F51 C~2rY7 2011 10 14.35567 22 23 37.248 -22 00 11.20 23.1G 602572 F51 C~2rY7 2013 09 09.43204 22 41 03.236 -20 25 33.99 23.1G 602572 F51 C~2rY7 2013 09 22.36538 22 39 57.468 -20 30 19.38 23.3G 602572 F51 C~2rY7 2013 09 23.36743 22 39 52.645 -20 30 37.42 20.9G 602572 F51 C~2rY7 2014 06 28.56287 22 53 19.719 -19 01 46.60 22.5w 602572 F51 C~1vXb 2014 06 28.57475 22 53 19.706 -19 01 46.85 22.8w 602572 F51 C~1vXb 2014 06 28.58661 22 53 19.683 -19 01 46.89 22.5w 602572 F51 C~1vXb 2014 07 08.54979 22 53 00.439 -19 06 23.29 22.5w 602572 F51 C~1vXb 2014 07 08.56159 22 53 00.405 -19 06 23.70 22.5w 602572 F51 C~1vXb 2014 07 08.57339 22 53 00.377 -19 06 24.19 22.7w 602572 F51 C~1vXb 2014 07 27.53581 22 51 59.788 -19 16 31.27 22.5G 602572 F51 C~2rY7 2014 07 30.52562 22 51 47.765 -19 18 12.75 22.5w 602572 F51 C~1vXb 2014 07 30.53689 22 51 47.704 -19 18 13.39 22.6w 602572 F51 C~1vXb 2014 07 30.55935 22 51 47.625 -19 18 13.80 22.4w 602572 F51 C~1vXb 2014 08 28.38032 22 49 29.020 -19 34 15.48 22.7G 602572 F51 C~2rY7 2014 08 28.39086 22 49 28.954 -19 34 15.79 22.2G 602572 F51 C~2rY7 2014 09 18.39770 22 47 39.061 -19 43 41.50 22.5G 602572 F51 C~2rY7 2015 06 17.58058 23 00 35.227 -18 11 03.29 22.5w 602572 F51 C~1vXb 2015 06 17.59135 23 00 35.227 -18 11 03.32 22.6w 602572 F51 C~1vXb 2015 06 17.60204 23 00 35.221 -18 11 03.31 22.7w 602572 F51 C~1vXb 2015 06 20.58334 23 00 34.441 -18 12 03.29 21.8G 602572 F51 C~2rY7 2015 08 10.47016 22 58 15.332 -18 37 26.06 22.1G 602572 F51 C~2rY7 2015 08 10.48203 22 58 15.284 -18 37 26.30 22.1G 602572 F51 C~2rY7 2015 08 10.49394 22 58 15.222 -18 37 26.76 22.9G 602572 F51 C~2rY7 2015 08 10.50584 22 58 15.180 -18 37 27.13 22.8G 602572 F51 C~2rY7 2015 08 11.48589 22 58 10.644 -18 38 00.87 22.7G 602572 F51 C~2rY7 2015 08 11.49780 22 58 10.583 -18 38 01.57 22.2G 602572 F51 C~2rY7 2015 08 11.50967 22 58 10.529 -18 38 01.85 22.4G 602572 F51 C~2rY7 2015 08 12.46751 22 58 06.061 -18 38 34.73 22.5G 602572 F51 C~2rY7 2016 08 07.52714 23 05 35.785 -17 48 15.94 23.1G 602572 F51 C~2rY7 2016 08 07.53752 23 05 35.740 -17 48 16.29 22.2G 602572 F51 C~2rY7 2016 08 07.54786 23 05 35.679 -17 48 16.75 22.7G 602572 F51 C~2rY7 2016 08 07.55823 23 05 35.644 -17 48 17.15 22.4G 602572 F51 C~2rY7 2016 08 08.50121 23 05 31.512 -17 48 49.57 22.7G 602572 F51 C~2rY7 2016 08 10.47866 23 05 22.665 -17 49 57.68 22.6G 602572 F51 C~2rY7 2016 08 26.49907 23 04 05.024 -17 58 59.36 22.5G 602572 F51 C~2rY7 2016 09 25.37789 23 01 31.093 -18 12 38.82 22.4G 602572 F51 C~2rY7 2016 09 25.38887 23 01 31.051 -18 12 39.31 22.7G 602572 F51 C~2rY7 2016 09 25.41079 23 01 30.932 -18 12 39.85 22.6G 602572 F51 C~2rY7 2017 09 13.43263 23 09 42.033 -17 19 14.08 23.2G 602572 F51 C~2rY7 2017 09 21.44535 23 09 00.849 -17 22 41.84 22.5G 602572 F51 C~2rY7 2021 10 03.145120 23 36 02.196 -14 05 05.98 22.7G 602572 G37 C~55QU 2021 10 03.198070 23 36 01.935 -14 05 07.28 602572 G37 C~55QU 2021 10 03.251050 23 36 01.665 -14 05 08.40 602572 G37 C~55QU 2023 09 14.435073 23 51 16.008 -12 11 10.74 22.6w 602572 F51 C~7MUY 2023 09 14.446773 23 51 15.936 -12 11 11.28 22.6w 602572 F51 C~7MUY 2023 09 14.458484 23 51 15.863 -12 11 11.51 22.5w 602572 F51 C~7MUY
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 0.34 0.00 -0.16
2 0.1638 0.00 0.02 0.00 -0.01
3 0.2431 0.00 -0.29 0.00 -0.02
4 1.1167 0.00 0.12 0.00 0.00
5 1.1167 0.00 -0.07 0.00 0.14
6 1.1168 0.00 -0.10 0.00 0.12
7 1.2479 0.00 -0.02 0.00 -0.07
8 1.2480 0.00 0.31 0.00 -0.04
9 1.3189 0.00 -0.12 0.00 0.13
10 3.2247 0.00 -0.14 0.00 0.10
11 3.2601 0.00 -0.37 0.00 -0.21
12 3.2628 0.00 0.13 0.00 0.10
13 4.0245 0.00 -0.15 0.00 -0.09
14 4.0245 0.00 -0.07 0.00 -0.03
15 4.0246 0.00 -0.14 0.00 0.23
16 4.0518 0.00 0.06 0.00 -0.05
17 4.0519 0.00 -0.00 0.00 -0.11
18 4.0519 0.00 0.02 0.00 -0.26
19 4.1038 0.00 -0.01 0.00 0.05
20 4.1120 0.00 0.09 0.00 0.15
21 4.1120 0.00 -0.11 0.00 -0.11
22 4.1121 0.00 0.13 0.00 0.25
23 4.1910 0.00 0.09 0.00 0.02
24 4.1910 0.00 -0.06 0.00 0.03
25 4.2486 0.00 0.14 0.00 -0.12
26 4.9937 0.00 -0.12 0.00 -0.04
27 4.9938 0.00 -0.09 0.00 0.13
28 4.9938 0.00 -0.15 0.00 0.35
29 5.0020 0.00 0.04 0.00 -0.34
30 5.1413 0.00 -0.01 0.00 -0.06
31 5.1413 0.00 0.10 0.00 0.11
32 5.1414 0.00 0.01 0.00 0.06
33 5.1414 0.00 0.22 0.00 0.10
34 5.1441 0.00 0.08 0.00 0.03
35 5.1441 0.00 0.01 0.00 -0.26
36 5.1441 0.00 0.04 0.00 -0.13
37 5.1468 0.00 0.04 0.00 -0.15
38 6.1353 0.00 0.17 0.00 0.10
39 6.1353 0.00 0.19 0.00 0.11
40 6.1353 0.00 -0.03 0.00 0.00
41 6.1354 0.00 0.14 0.00 -0.04
42 6.1380 0.00 0.08 0.00 0.06
43 6.1434 0.00 -0.31 0.00 0.14
44 6.1872 0.00 -0.08 0.00 -0.20
45 6.2690 0.00 -0.05 0.00 0.19
46 6.2691 0.00 0.14 0.00 -0.07
47 6.2691 0.00 0.00 0.00 -0.16
48 7.2356 0.00 -0.15 0.00 0.19
49 7.2576 0.00 0.09 0.00 0.07
50 11.2896 0.00 0.10 0.00 -0.02
51 11.2898 0.00 0.10 0.00 -0.13
52 11.2899 0.00 -0.02 0.00 -0.06
53 13.2370 0.00 0.13 0.00 0.09
54 13.2371 0.00 -0.05 0.00 -0.08
55 13.2371 0.00 -0.24 0.00 0.06
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.
602572 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 49.837 49.837 49.837 ecceobj 0.269 0.269 0.269 incobj 10.960 10.960 10.960 qmin 35.915 35.736 35.935 qmax 64.195 64.458 64.294 amean 49.746 49.779 49.815 amin 49.244 49.240 49.262 amax 50.370 50.404 50.434 emean 0.261 0.264 0.263 emin 0.247 0.248 0.249 emax 0.277 0.280 0.277 imean 9.913 9.722 9.815 imin 9.332 8.950 9.096 imax 10.550 10.539 10.528 excite_mean 0.312 0.314 0.313 fracstop 1.000 1.000 1.000 cjmean 3.050 3.049 3.050 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 179.0 178.8 180.8 kozaiamp 180.0 180.0 180.0