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: 16EB367 # Created Tue Apr 1 01:10:44 2025 # Orbit generated from Bernstein formalism # Fitting 13 observations of 13 # Arc: 38.92d # First observation: 2016/03/07 # Last observation: 2016/04/15 Preliminary a, adot, b, bdot, g, gdot: 0.000001 0.018790 -0.000002 -0.000706 0.020818 0.000000 # WARNING Fitting with energy constraint # Chi-squared of fit: 4.85 DOF: 21 RMS: 0.11 # Min/Max residuals: -0.28 0.22 # Exact a, adot, b, bdot, g, gdot: 1.298041E-05 1.692695E-02 -2.838334E-07 -5.773426E-04 2.040750E-02 7.105815E-04 # Covariance matrix: 5.0172E-13 1.7736E-10 -1.8775E-13 -1.2337E-11 3.9711E-11 4.4919E-09 1.7736E-10 2.4734E-07 -2.2536E-10 -1.7254E-08 5.0149E-08 3.8906E-06 -1.8775E-13 -2.2536E-10 4.2181E-13 1.3283E-11 -4.6195E-11 -3.7972E-09 -1.2337E-11 -1.7254E-08 1.3283E-11 1.2622E-09 -3.4950E-09 -2.6931E-07 3.9711E-11 5.0149E-08 -4.6195E-11 -3.4950E-09 1.0237E-08 8.2323E-07 4.4919E-09 3.8906E-06 -3.7972E-09 -2.6931E-07 8.2323E-07 7.8704E-05 # lat0 lon0 xBary yBary zBary JD0 10.975969 -152.479365 0.641857 0.143478 -0.739036 2457455.094829 # Heliocentric elements and errors Epoch: 2457450.5000 = 2016/03/03 Mean Anomaly: 164.72703 +/- 202.115 Argument of Peri: 291.30804 +/- 201.804 Long of Asc Node: 107.17885 +/- 0.321 Inclination: 10.95856 +/- 0.011 Eccentricity: 0.12923703 +/- 0.0533 Semi-Major Axis: 44.19580593 +/- 2.7401 Time of Perihelion: 2408344.7460 +/- 60078.0 Perihelion: 38.48407137 +/- 3.3534 Aphelion: 49.90754049 +/- 3.8893 Period (y) 293.8189 +/- 27.32 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -43.62954562 +/- 0.2115 Ecliptic Y -22.00894269 +/- 0.1102 Ecliptic Z 9.32977459 +/- 0.0463 Ecliptic XDOT 0.00095310 +/- 0.0010 Ecliptic YDOT -0.00207098 +/- 0.0006 Ecliptic ZDOT -0.00005788 +/- 0.0002 # Distances at JD0 (AU) Heliocenter to KBO 49.74912565 +/- 0.1920 Geocenter to KBO 49.00158805 +/- 0.2429 # Hcoef: 6.67
The following table shows the complete astrometric record for 16EB367. 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 (16EB367) followed by the observatory code and reference code for the source of the astrometry.
2016 03 07.59404 13 57 52.17 -00 19 46.4 24.6g 16EB367 T09 C~89TC 2016 03 07.60489 13 57 52.12 -00 19 46.1 24.4g 16EB367 T09 C~89TC 2016 03 07.62696 13 57 52.09 -00 19 45.4 24.4g 16EB367 T09 C~89TC 2016 03 07.64195 13 57 52.05 -00 19 45.3 24.6g 16EB367 T09 C~89TC 2016 03 16.46294 13 57 26.81 -00 16 07.4 23.3z 16EB367 T09 C~89TC 2016 03 16.51602 13 57 26.64 -00 16 05.9 23.3z 16EB367 T09 C~89TC 2016 03 16.54079 13 57 26.57 -00 16 05.4 23.5z 16EB367 T09 C~89TC 2016 03 16.62672 13 57 26.30 -00 16 03.2 23.5z 16EB367 T09 C~89TC 2016 03 16.63751 13 57 26.26 -00 16 03.0 23.3z 16EB367 T09 C~89TC 2016 04 15.46969 13 55 38.94 -00 03 55.0 23.2y 16EB367 T09 C~89TC 2016 04 15.48536 13 55 38.86 -00 03 54.7 22.9y 16EB367 T09 C~89TC 2016 04 15.49884 13 55 38.80 -00 03 54.2 23.0y 16EB367 T09 C~89TC 2016 04 15.51502 13 55 38.74 -00 03 54.0 23.0y 16EB367 T09 C~89TC
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 0.03 0.00 -0.03
2 0.0000 -0.81 -0.28 0.02 -0.11
3 0.0001 -1.48 0.08 0.51 0.20
4 0.0001 -2.07 0.17 0.39 -0.05
5 0.0243 -433.20 -0.00 70.73 -0.08
6 0.0244 -436.11 -0.10 71.23 0.07
7 0.0245 -437.27 0.06 71.33 -0.00
8 0.0247 -441.84 0.05 71.96 0.05
9 0.0248 -442.47 -0.01 71.93 -0.05
10 0.1064 -2205.67 0.22 185.20 0.06
11 0.1065 -2206.90 -0.01 185.06 -0.08
12 0.1065 -2207.92 -0.17 185.21 0.07
13 0.1066 -2208.83 -0.05 185.08 -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.
16EB367 quality flag:0 Type: ERR2LARGE ERR2LARGE ERR2LARGE axisobj 0.000 0.000 0.000 ecceobj -1.000 -1.000 -1.000 incobj -1.000 -1.000 -1.000 qmin 0.000 0.000 0.000 qmax 0.000 0.000 0.000 amean 0.000 0.000 0.000 amin 0.000 0.000 0.000 amax 0.000 0.000 0.000 emean 0.000 0.000 0.000 emin 0.000 0.000 0.000 emax 0.000 0.000 0.000 imean 0.000 0.000 0.000 imin 0.000 0.000 0.000 imax 0.000 0.000 0.000 excite_mean 0.000 0.000 0.000 fracstop 0.000 0.000 0.000 cjmean 0.000 0.000 0.000 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 0.0 0.0 0.0 kozaiamp 0.0 0.0 0.0