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: 13RT155 # Created Tue Apr 1 01:09:36 2025 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 16 observations of 16 # Arc: 11.08y # First observation: 2013/09/01 # Last observation: 2024/10/01 # Chi-squared of fit: 4.68 DOF: 26 RMS: 0.10 # Min/Max residuals: -0.30 0.22 # Exact a, adot, b, bdot, g, gdot: 1.461532E-05 1.822995E-02 -4.482757E-06 -7.545502E-03 2.043695E-02 -1.060672E-02 # Covariance matrix: 4.6420E-13 1.3645E-14 4.8381E-14 -2.4263E-15 1.1148E-12 2.9302E-14 1.3645E-14 6.7626E-14 1.9376E-14 -2.5831E-14 1.8198E-13 2.8154E-13 4.8381E-14 1.9376E-14 1.3531E-13 -2.1100E-14 1.8206E-13 7.5900E-14 -2.4263E-15 -2.5831E-14 -2.1100E-14 1.6326E-14 -4.6721E-14 -1.1948E-13 1.1148E-12 1.8198E-13 1.8206E-13 -4.6721E-14 3.7951E-12 5.1825E-13 2.9302E-14 2.8154E-13 7.5900E-14 -1.1948E-13 5.1825E-13 1.3014E-12 # lat0 lon0 xBary yBary zBary JD0 13.510898 -36.837681 -0.268386 0.227648 -0.947110 2456536.659628 # Heliocentric elements and errors Epoch: 2456536.5000 = 2013/09/01 Mean Anomaly: 345.09528 +/- 0.022 Argument of Peri: 222.39263 +/- 0.023 Long of Asc Node: 172.27213 +/- 0.000 Inclination: 26.05440 +/- 0.000 Eccentricity: 0.65391209 +/- 0.0003 Semi-Major Axis: 102.99089100 +/- 0.1029 Time of Perihelion: 2472342.3556 +/- 548.9 Perihelion: 35.64390206 +/- 0.0458 Aphelion: 170.33787995 +/- 0.1726 Period (y) 1045.2169 +/- 1.57 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 39.01826316 +/- 0.0036 Ecliptic Y -28.89089269 +/- 0.0027 Ecliptic Z 11.43155016 +/- 0.0011 Ecliptic XDOT 0.00054128 +/- 0.0000 Ecliptic YDOT 0.00264025 +/- 0.0000 Ecliptic ZDOT -0.00131470 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 49.87813591 +/- 0.0033 Geocenter to KBO 48.93143013 +/- 0.0047 # Hcoef: 6.30
The following table shows the complete astrometric record for 13RT155. 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 (13RT155) followed by the observatory code and reference code for the source of the astrometry.
2013 09 01.15885 21 24 25.420 -01 00 17.18 23.6g 13RT155 W84 C~52RK 2013 09 10.16600 21 23 54.972 -01 04 26.96 23.5r 13RT155 W84 C~52RK 2013 09 10.16736 21 23 54.968 -01 04 27.10 23.2i 13RT155 W84 C~52RK 2013 09 13.11802 21 23 45.639 -01 05 50.73 22.8i 13RT155 W84 C~52RK 2013 09 13.12082 21 23 45.623 -01 05 50.87 22.9z 13RT155 W84 C~52RK 2013 09 23.03700 21 23 17.103 -01 10 34.07 24.1g 13RT155 W84 C~52RK 2013 09 24.03670 21 23 14.489 -01 11 02.45 23.7g 13RT155 W84 C~52RK 2013 09 29.11050 21 23 02.119 -01 13 26.56 23.5r 13RT155 W84 C~52RK 2013 09 29.11609 21 23 02.108 -01 13 26.77 23.5i 13RT155 W84 C~52RK 2013 10 10.07773 21 22 40.700 -01 18 29.41 23.6r 13RT155 W84 C~52RK 2013 10 11.05883 21 22 39.174 -01 18 55.68 23.5z 13RT155 W84 C~52RK 2017 10 11.00195 21 41 15.591 -01 38 57.91 22.9r 13RT155 W84 C~52RK 2017 10 11.04610 21 41 15.511 -01 38 59.18 23.8g 13RT155 W84 C~52RK 2018 09 18.20554 21 47 11.980 -01 32 52.76 22.8z 13RT155 W84 C~52RL 2024 10 01.104980 22 18 32.891 -02 11 05.25 20.8G 13RT155 G37 C~8GyC 2024 10 01.190140 22 18 32.611 -02 11 08.35 13RT155 G37 C~8GyC
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 -0.01 0.00 -0.30
2 0.0247 0.00 0.04 0.00 0.12
3 0.0247 0.00 0.04 0.00 0.02
4 0.0327 0.00 0.11 0.00 0.03
5 0.0328 0.00 0.01 0.00 -0.03
6 0.0599 0.00 -0.03 0.00 -0.03
7 0.0626 0.00 -0.16 0.00 0.11
8 0.0765 0.00 0.02 0.00 0.06
9 0.0765 0.00 0.05 0.00 0.00
10 0.1066 0.00 -0.03 0.00 0.03
11 0.1092 0.00 0.02 0.00 -0.00
12 4.1091 0.00 -0.07 0.00 0.02
13 4.1092 0.00 0.02 0.00 -0.03
14 5.0460 0.00 0.05 0.00 0.02
15 11.0827 0.00 0.05 0.00 0.22
16 11.0829 0.00 -0.06 0.00 -0.23
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.
13RT155 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 104.276 104.274 104.278 ecceobj 0.658 0.658 0.658 incobj 25.989 25.989 25.989 qmin 34.904 34.904 34.903 qmax 176.264 176.002 176.298 amean 103.219 103.097 103.108 amin 101.143 101.106 101.019 amax 106.482 106.201 106.281 emean 0.649 0.649 0.648 emin 0.633 0.633 0.627 emax 0.661 0.661 0.661 imean 25.982 25.917 26.002 imin 25.175 25.175 25.175 imax 27.567 27.198 27.816 excite_mean 0.783 0.783 0.783 fracstop 1.000 1.000 1.000 cjmean 2.824 2.824 2.824 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 271.6 270.2 274.4 kozaiamp 58.8 55.1 62.9