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: 363401 # Created Fri Nov 1 01:06:59 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 53 observations of 53 # Arc: 14.87y # First observation: 2003/06/01 # Last observation: 2018/04/12 # Chi-squared of fit: 72.62 DOF: 100 RMS: 0.21 # Min/Max residuals: -1.00 0.42 # Exact a, adot, b, bdot, g, gdot: 1.678062E-05 2.681618E-02 8.517661E-07 -1.074624E-03 2.555824E-02 1.186786E-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 -0.103998 -128.286312 -0.324743 -0.001717 -0.963840 2452791.557413 # Heliocentric elements and errors Epoch: 2452792.5000 = 2003/06/02 Mean Anomaly: 21.10154 +/- 0.000 Argument of Peri: 154.98042 +/- 0.000 Long of Asc Node: 49.63942 +/- 0.000 Inclination: 2.29449 +/- 0.000 Eccentricity: 0.13275134 +/- 0.0000 Semi-Major Axis: 45.61179689 +/- 0.0000 Time of Perihelion: 2446197.3313 +/- 0.0 Perihelion: 39.55676980 +/- 0.0000 Aphelion: 51.66682397 +/- 0.0000 Period (y) 308.0520 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -24.58641487 +/- 0.0000 Ecliptic Y -31.66523082 +/- 0.0000 Ecliptic Z -0.07099276 +/- 0.0000 Ecliptic XDOT 0.00217022 +/- 0.0000 Ecliptic YDOT -0.00188461 +/- 0.0000 Ecliptic ZDOT -0.00011516 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 40.08965988 +/- 0.0000 Geocenter to KBO 39.12633435 +/- 0.0000 # Hcoef: 6.64
The following table shows the complete astrometric record for 363401. 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 (363401) followed by the observatory code and reference code for the source of the astrometry.
2003 06 01.05667 15 17 03.41 -18 17 37.7 21.4R 363401 807 Ci2139 2003 06 02.11348 15 16 58.40 -18 17 19.1 363401 807 Ci2139 2003 06 02.17650 15 16 58.11 -18 17 18.0 363401 807 Ci2139 2003 07 06.38128 15 14 48.08 -18 09 15.5 22.7R 363401 568 Ci2707 2003 07 07.26876 15 14 45.88 -18 09 07.0 363401 568 Ci2707 2003 07 07.37572 15 14 45.58 -18 09 05.8 363401 568 Ci2707 2004 03 15.42155 15 28 42.41 -19 03 35.9 21.8 363401 695 Ck9037 2004 03 15.49541 15 28 42.23 -19 03 35.0 363401 695 Ck9037 2004 05 24.36996 15 23 49.10 -18 46 44.1 23.0g 363401 568 C74769 2004 05 24.39504 15 23 48.97 -18 46 43.8 23.1g 363401 568 C74769 2004 05 24.41756 15 23 48.86 -18 46 43.3 23.0g 363401 568 C74769 2004 05 25.37886 15 23 44.07 -18 46 26.3 363401 568 C74769 2004 05 26.02356 15 23 40.90 -18 46 14.7 22.3R 363401 304 Ck9037 2004 05 26.05308 15 23 40.75 -18 46 14.4 363401 304 Ck9037 2004 06 09.33018 15 22 33.04 -18 42 12.3 22.5R 363401 568 Ck9037 2004 06 09.39737 15 22 32.73 -18 42 11.2 363401 568 Ck9037 2004 06 10.31129 15 22 28.67 -18 41 56.5 22.4i 363401 568 C~0VDh 2004 06 10.38265 15 22 28.34 -18 41 55.4 22.3i 363401 568 C~0VDh 2005 05 14.40147 15 30 54.39 -19 15 54.1 22.5r 363401 568 C74769 2005 05 14.43516 15 30 54.22 -19 15 53.5 22.6r 363401 568 C74769 2005 05 14.47384 15 30 54.01 -19 15 52.8 22.7r 363401 568 C74769 2005 05 17.38240 15 30 39.17 -19 15 02.4 22.3r 363401 568 C~0VDh 2005 05 17.38453 15 30 39.16 -19 15 02.4 22.5r 363401 568 C74769 2007 05 08.26398 15 43 58.18 -20 07 16.0 22.0R 363401 304 Cu8878 2007 05 08.30686 15 43 57.96 -20 07 15.3 363401 304 Cu8878 2010 06 04.420227 16 00 26.094 -21 08 17.06 20.5G 363401 F51 C~42o9 2010 06 04.432301 16 00 26.057 -21 08 16.92 20.6G 363401 F51 C~42o9 2010 06 07.376298 16 00 11.306 -21 07 36.32 22.1G 363401 F51 C~42o9 2011 06 07.391251 16 06 28.194 -21 28 31.75 23.0G 363401 F51 C~42o9 2011 06 07.405463 16 06 28.124 -21 28 31.31 22.6G 363401 F51 C~42o9 2011 06 07.419606 16 06 28.051 -21 28 31.34 22.8G 363401 F51 C~42o9 2011 06 07.433799 16 06 27.977 -21 28 30.92 23.0G 363401 F51 C~42o9 2013 06 06.03587 16 19 04.51 -22 07 32.8 22.3R 363401 304 C~0sni 2013 06 06.21182 16 19 03.60 -22 07 30.8 363401 304 C~0sni 2013 06 06.32392 16 19 02.99 -22 07 29.6 363401 304 C~0sni 2013 06 07.03221 16 18 59.39 -22 07 21.0 363401 304 C~0sni 2013 06 07.09774 16 18 59.05 -22 07 20.1 363401 304 C~0sni 2013 06 07.32461 16 18 57.87 -22 07 17.4 363401 304 C~0sni 2013 06 08.07794 16 18 54.03 -22 07 08.6 363401 304 C~0sni 2013 06 08.21490 16 18 53.33 -22 07 06.9 363401 304 C~0sni 2013 06 08.30207 16 18 52.88 -22 07 06.0 363401 304 C~0sni 2014 08 22.264568 16 21 24.590 -22 16 14.95 22.4G 363401 F51 C~42o9 2015 05 20.477152 16 33 06.304 -22 45 24.86 23.0G 363401 F51 C~42o9 2015 05 21.472656 16 33 01.192 -22 45 15.17 22.9G 363401 F51 C~42o9 2015 06 11.366650 16 31 12.636 -22 41 40.91 23.2G 363401 F51 C~42o9 2015 07 12.352110 16 28 52.304 -22 36 42.67 23.4G 363401 F51 C~42o9 2015 08 06.287490 16 27 45.576 -22 34 07.01 22.7G 363401 F51 C~42o9 2017 05 04.532660 16 46 54.177 -23 17 54.03 22.9G 363401 F51 C~42o9 2017 05 27.410881 16 45 02.292 -23 15 00.01 23.3G 363401 F51 C~42o9 2017 05 27.421949 16 45 02.242 -23 14 59.95 23.2G 363401 F51 C~42o9 2017 05 27.433032 16 45 02.174 -23 14 59.89 22.9G 363401 F51 C~42o9 2017 05 27.444096 16 45 02.109 -23 14 59.59 22.9G 363401 F51 C~42oA 2018 04 12.580166 16 54 30.097 -23 33 01.37 23.1G 363401 F51 C~42oA
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 -0.13 0.00 -0.29 2 0.0029 0.00 -0.10 0.00 -0.25 3 0.0031 0.00 0.10 0.00 -0.26 4 0.0967 0.00 -1.00 0.00 -0.43 5 0.0991 0.00 0.19 0.00 -0.36 6 0.0994 0.00 -0.10 0.00 -0.18 7 0.7895 0.00 0.29 0.00 -0.11 8 0.7897 0.00 -0.05 0.00 0.32 9 0.9810 0.00 0.03 0.00 0.19 10 0.9811 0.00 -0.01 0.00 0.04 11 0.9811 0.00 0.06 0.00 0.14 12 0.9838 0.00 0.06 0.00 0.08 13 0.9855 0.00 0.42 0.00 0.06 14 0.9856 0.00 0.40 0.00 -0.15 15 1.0247 0.00 0.09 0.00 0.03 16 1.0249 0.00 0.04 0.00 0.05 17 1.0274 0.00 -0.08 0.00 0.17 18 1.0276 0.00 -0.20 0.00 0.14 19 1.9530 0.00 -0.03 0.00 0.23 20 1.9531 0.00 0.05 0.00 0.24 21 1.9532 0.00 -0.08 0.00 0.27 22 1.9612 0.00 0.18 0.00 0.20 23 1.9612 0.00 0.19 0.00 0.17 24 3.9349 0.00 -0.02 0.00 -0.12 25 3.9350 0.00 -0.04 0.00 -0.09 26 7.0099 0.00 -0.73 0.00 -0.15 27 7.0099 0.00 -0.35 0.00 -0.18 28 7.0180 0.00 0.03 0.00 -0.22 29 8.0173 0.00 -0.03 0.00 -0.04 30 8.0174 0.00 0.01 0.00 0.22 31 8.0174 0.00 0.01 0.00 0.00 32 8.0175 0.00 -0.01 0.00 0.23 33 10.0150 0.00 0.15 0.00 0.11 34 10.0155 0.00 0.29 0.00 0.04 35 10.0158 0.00 -0.11 0.00 -0.12 36 10.0177 0.00 0.09 0.00 0.08 37 10.0179 0.00 0.09 0.00 0.22 38 10.0185 0.00 0.09 0.00 0.21 39 10.0206 0.00 -0.02 0.00 0.10 40 10.0210 0.00 0.13 0.00 0.18 41 10.0212 0.00 0.15 0.00 0.03 42 11.2258 0.00 0.10 0.00 0.04 43 11.9683 0.00 0.01 0.00 0.00 44 11.9710 0.00 -0.11 0.00 -0.03 45 12.0282 0.00 -0.10 0.00 -0.13 46 12.1131 0.00 -0.00 0.00 -0.24 47 12.1813 0.00 0.26 0.00 -0.37 48 13.9260 0.00 -0.02 0.00 -0.24 49 13.9886 0.00 0.01 0.00 0.04 50 13.9887 0.00 0.14 0.00 0.01 51 13.9887 0.00 0.00 0.00 -0.02 52 13.9887 0.00 -0.09 0.00 0.18 53 14.8652 0.00 -0.31 0.00 -0.09
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.
363401 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 45.279 45.279 45.279 ecceobj 0.126 0.126 0.126 incobj 2.302 2.302 2.302 qmin 39.008 39.007 39.012 qmax 52.622 52.629 52.575 amean 45.644 45.644 45.644 amin 45.257 45.257 45.270 amax 46.070 46.072 46.066 emean 0.128 0.128 0.128 emin 0.114 0.114 0.114 emax 0.142 0.142 0.142 imean 1.680 1.680 1.679 imin 0.994 0.994 0.994 imax 2.251 2.251 2.251 excite_mean 0.131 0.131 0.131 fracstop 1.000 1.000 1.000 cjmean 3.100 3.100 3.100 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 178.5 178.7 178.7 kozaiamp 180.0 179.9 180.0