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: 06WS195 # Created Sat Apr 27 01:12:53 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 34 observations of 34 # Arc: 18.13y # First observation: 2004/09/12 # Last observation: 2022/10/29 # Chi-squared of fit: 30.54 DOF: 62 RMS: 0.17 # Min/Max residuals: -0.64 0.41 # Exact a, adot, b, bdot, g, gdot: 1.427246E-05 2.467787E-02 9.967830E-06 1.300018E-02 2.727481E-02 6.962787E-03 # Covariance matrix: 2.3004E-13 -2.3836E-14 1.2133E-14 -8.3425E-15 1.3405E-13 -3.8374E-14 -2.3836E-14 3.7364E-14 -3.1364E-14 1.9564E-14 4.4850E-14 8.6017E-14 1.2133E-14 -3.1364E-14 9.6230E-14 -2.3832E-14 -4.2665E-14 -7.5874E-14 -8.3425E-15 1.9564E-14 -2.3832E-14 1.2539E-14 2.5825E-14 4.7310E-14 1.3405E-13 4.4850E-14 -4.2665E-14 2.5825E-14 2.1506E-13 1.1182E-13 -3.8374E-14 8.6017E-14 -7.5874E-14 4.7310E-14 1.1182E-13 2.0798E-13 # lat0 lon0 xBary yBary zBary JD0 -19.260799 31.482918 0.668749 -0.249838 -0.715274 2453261.072743 # Heliocentric elements and errors Epoch: 2453260.5000 = 2004/09/12 Mean Anomaly: 65.16838 +/- 0.008 Argument of Peri: 231.45376 +/- 0.011 Long of Asc Node: 62.53819 +/- 0.000 Inclination: 32.73336 +/- 0.000 Eccentricity: 0.23335114 +/- 0.0000 Semi-Major Axis: 39.24629605 +/- 0.0025 Time of Perihelion: 2437003.8584 +/- 2.5 Perihelion: 30.08812832 +/- 0.0020 Aphelion: 48.40446378 +/- 0.0031 Period (y) 245.8704 +/- 0.02 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 30.50773121 +/- 0.0005 Ecliptic Y 17.90272416 +/- 0.0003 Ecliptic Z -12.09391202 +/- 0.0002 Ecliptic XDOT -0.00036562 +/- 0.0000 Ecliptic YDOT 0.00267486 +/- 0.0000 Ecliptic ZDOT 0.00100147 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 37.38290402 +/- 0.0004 Geocenter to KBO 36.66375104 +/- 0.0006 # Hcoef: 7.50
The following table shows the complete astrometric record for 06WS195. 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 (06WS195) followed by the observatory code and reference code for the source of the astrometry.
2004 09 12.57200 02 23 44.70 -06 06 57.1 23.8V 06WS195 568 C~0CfG 2004 09 12.61894 02 23 44.55 -06 06 58.8 06WS195 568 C~0CfG 2004 09 13.53563 02 23 41.36 -06 07 28.4 06WS195 568 C~0CfG 2004 09 13.56745 02 23 41.24 -06 07 29.3 06WS195 568 C~0CfG 2004 09 14.53884 02 23 37.80 -06 08 00.8 06WS195 568 C~0CfG 2004 09 14.57000 02 23 37.66 -06 08 02.0 06WS195 568 C~0CfG 2006 11 14.37555 02 27 13.47 -04 11 33.2 23.4i 06WS195 568 Ct2571 2006 11 14.39538 02 27 13.37 -04 11 33.5 23.4i 06WS195 568 Ct2571 2006 11 14.41916 02 27 13.24 -04 11 33.7 23.2i 06WS195 568 Ct2571 2006 11 17.34995 02 26 57.89 -04 11 59.7 22.9i 06WS195 568 Ct2571 2006 11 17.36013 02 26 57.84 -04 11 59.8 22.5i 06WS195 568 Ct2571 2006 11 17.36965 02 26 57.79 -04 11 59.8 22.8i 06WS195 568 Ct2571 2006 11 21.34729 02 26 37.36 -04 12 26.1 21.9i 06WS195 568 Ct2571 2006 11 21.36708 02 26 37.27 -04 12 26.3 22.4i 06WS195 568 Ct2571 2006 11 21.39287 02 26 37.13 -04 12 26.3 22.8i 06WS195 568 Ct2571 2006 11 24.39131 02 26 22.14 -04 12 38.7 22.9i 06WS195 568 Ct2571 2006 11 24.40090 02 26 22.09 -04 12 38.7 22.8i 06WS195 568 Ct2571 2006 12 12.30031 02 25 02.52 -04 11 38.7 23.2i 06WS195 568 Ct2571 2006 12 12.32011 02 25 02.44 -04 11 38.5 23.2i 06WS195 568 Ct2571 2006 12 12.33990 02 25 02.36 -04 11 38.4 23.3i 06WS195 568 Ct2571 2006 12 20.20344 02 24 34.31 -04 09 57.5 23.3i 06WS195 568 Ct2571 2006 12 20.22328 02 24 34.25 -04 09 57.2 22.9i 06WS195 568 Ct2571 2006 12 20.24309 02 24 34.17 -04 09 56.9 23.0i 06WS195 568 Ct2571 2006 12 23.26236 02 24 24.74 -04 09 05.9 22.5I 06WS195 568 Ct2571 2006 12 23.27186 02 24 24.72 -04 09 05.7 22.6I 06WS195 568 Ct2571 2006 12 23.28133 02 24 24.69 -04 09 05.5 22.6I 06WS195 568 Ct2571 2006 12 26.21815 02 24 16.30 -04 08 09.8 23.7I 06WS195 568 Ct2571 2006 12 26.23805 02 24 16.24 -04 08 09.5 23.1I 06WS195 568 Ct2571 2006 12 26.25796 02 24 16.19 -04 08 09.1 23.2I 06WS195 568 Ct2571 2014 10 22.34551 03 01 27.56 +04 45 27.8 22.9R 06WS195 G37 C~1BxO 2014 10 22.43875 03 01 27.08 +04 45 25.8 06WS195 G37 C~1BxO 2022 10 29.394690 03 30 45.678 +12 39 59.07 23.5G 06WS195 G37 C~5yqi 2022 10 29.443120 03 30 45.439 +12 39 57.99 06WS195 G37 C~5yqi 2022 10 29.490970 03 30 45.219 +12 39 57.39 06WS195 G37 C~5yqi
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 0.18 0.00 -0.47
2 0.0001 0.00 0.41 0.00 -0.64
3 0.0026 0.00 0.14 0.00 -0.26
4 0.0027 0.00 0.05 0.00 -0.12
5 0.0054 0.00 0.08 0.00 0.14
6 0.0055 0.00 -0.30 0.00 -0.04
7 2.1706 0.00 -0.14 0.00 0.20
8 2.1706 0.00 -0.04 0.00 0.10
9 2.1707 0.00 -0.07 0.00 0.13
10 2.1787 0.00 0.00 0.00 0.18
11 2.1787 0.00 0.06 0.00 0.16
12 2.1788 0.00 0.07 0.00 0.24
13 2.1897 0.00 -0.15 0.00 0.07
14 2.1897 0.00 0.03 0.00 -0.03
15 2.1898 0.00 -0.07 0.00 0.10
16 2.1980 0.00 -0.08 0.00 0.11
17 2.1980 0.00 -0.10 0.00 0.14
18 2.2470 0.00 0.08 0.00 -0.03
19 2.2471 0.00 0.06 0.00 -0.03
20 2.2471 0.00 0.04 0.00 -0.12
21 2.2687 0.00 0.12 0.00 -0.00
22 2.2687 0.00 0.21 0.00 -0.01
23 2.2688 0.00 0.00 0.00 -0.03
24 2.2770 0.00 -0.11 0.00 0.14
25 2.2771 0.00 0.03 0.00 0.17
26 2.2771 0.00 0.02 0.00 0.20
27 2.2851 0.00 -0.06 0.00 0.10
28 2.2852 0.00 -0.12 0.00 0.00
29 2.2852 0.00 -0.03 0.00 0.00
30 10.1075 0.00 -0.10 0.00 -0.07
31 10.1078 0.00 -0.25 0.00 -0.24
32 18.1268 0.00 -0.03 0.00 0.23
33 18.1270 0.00 0.01 0.00 -0.18
34 18.1271 0.00 0.28 0.00 -0.11
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.
06WS195 quality flag:3 Type: 3:2E 3:2E 3:2E Type: 6:4II 6:4II 6:4II axisobj 39.689 39.689 39.689 ecceobj 0.236 0.236 0.236 incobj 32.649 32.649 32.649 qmin 25.311 25.312 25.311 qmax 54.027 54.027 54.028 amean 39.453 39.453 39.453 amin 39.068 39.069 39.067 amax 39.954 39.954 39.955 emean 0.289 0.289 0.289 emin 0.179 0.179 0.179 emax 0.357 0.357 0.357 imean 29.875 29.875 29.875 imin 27.810 27.811 27.810 imax 32.515 32.515 32.515 excite_mean 0.578 0.578 0.578 fracstop 1.000 1.000 1.000 cjmean 2.660 2.660 2.660 libcent 0 181.8 181.8 181.6 libamp 0 50.3 50.4 50.3 libcent 1 179.0 179.1 178.8 libamp 1 155.6 156.2 155.5 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 267.2 267.2 267.2 kozaiamp 47.5 47.5 47.5