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: 14TF116 # Created Fri May 3 01:16:30 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 12 observations of 12 # Arc: 7.16y # First observation: 2014/10/02 # Last observation: 2021/12/01 # Chi-squared of fit: 15.68 DOF: 18 RMS: 0.20 # Min/Max residuals: -0.47 0.40 # Exact a, adot, b, bdot, g, gdot: 1.487220E-05 2.193184E-02 -2.917502E-07 -6.156578E-04 2.382234E-02 5.433898E-03 # Covariance matrix: 1.1412E-12 -4.1978E-14 -1.4952E-14 -1.3719E-16 1.4226E-12 -6.0344E-13 -4.1978E-14 8.9838E-13 4.4682E-15 -2.5800E-14 5.1585E-13 6.3452E-12 -1.4952E-14 4.4682E-15 1.9016E-13 -3.3129E-14 -1.9751E-14 4.0735E-14 -1.3719E-16 -2.5800E-14 -3.3129E-14 2.1222E-14 -1.5762E-14 -1.8625E-13 1.4226E-12 5.1585E-13 -1.9751E-14 -1.5762E-14 2.4465E-12 2.9199E-12 -6.0344E-13 6.3452E-12 4.0735E-14 -1.8625E-13 2.9199E-12 4.6166E-11 # lat0 lon0 xBary yBary zBary JD0 -3.327877 19.213618 0.183120 -0.057092 -0.984703 2456932.768638 # Heliocentric elements and errors Epoch: 2456932.5000 = 2014/10/02 Mean Anomaly: 82.28090 +/- 0.089 Argument of Peri: 134.07742 +/- 0.051 Long of Asc Node: 135.83554 +/- 0.005 Inclination: 3.64403 +/- 0.000 Eccentricity: 0.23551511 +/- 0.0003 Semi-Major Axis: 41.97718715 +/- 0.0116 Time of Perihelion: 2434227.8435 +/- 26.3 Perihelion: 32.09092532 +/- 0.0140 Aphelion: 51.86344898 +/- 0.0180 Period (y) 271.9745 +/- 0.11 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 40.56135538 +/- 0.0026 Ecliptic Y 13.94466790 +/- 0.0009 Ecliptic Z -2.43682891 +/- 0.0002 Ecliptic XDOT -0.00024925 +/- 0.0000 Ecliptic YDOT 0.00257936 +/- 0.0000 Ecliptic ZDOT -0.00010678 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 42.96047980 +/- 0.0025 Geocenter to KBO 41.97727883 +/- 0.0028 # Hcoef: 6.44
The following table shows the complete astrometric record for 14TF116. 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 (14TF116) followed by the observatory code and reference code for the source of the astrometry.
2014 10 02.26786 01 15 58.921 +04 26 25.96 22.8i 14TF116 W84 C~55SP 2014 11 14.05317 01 12 56.457 +04 08 23.39 22.0i 14TF116 W84 C~55SP 2014 11 15.07745 01 12 52.704 +04 08 03.08 23.0r 14TF116 W84 C~55SP 2014 11 15.07884 01 12 52.701 +04 08 02.98 23.0z 14TF116 W84 C~55SP 2014 11 18.12715 01 12 41.880 +04 07 05.63 22.3z 14TF116 W84 C~55SP 2014 11 27.07245 01 12 13.325 +04 04 38.93 22.0z 14TF116 W84 C~55SP 2015 11 07.11459 01 18 05.553 +04 37 11.94 22.9i 14TF116 W84 C~55SP 2015 11 07.11595 01 18 05.542 +04 37 11.69 22.4r 14TF116 W84 C~55SP 2015 12 18.07071 01 16 07.191 +04 27 31.08 22.3z 14TF116 W84 C~55SP 2021 12 01.097230 01 43 52.891 +06 59 04.70 23.5G 14TF116 G37 C~5J6T 2021 12 01.148620 01 43 52.765 +06 59 04.73 14TF116 G37 C~5J6T 2021 12 01.200550 01 43 52.555 +06 59 03.85 14TF116 G37 C~5J6T
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 -0.05 0.00 -0.05
2 0.1171 0.00 0.22 0.00 0.14
3 0.1199 0.00 0.00 0.00 0.01
4 0.1199 0.00 0.04 0.00 -0.06
5 0.1283 0.00 -0.24 0.00 0.23
6 0.1528 0.00 -0.01 0.00 -0.10
7 1.0975 0.00 0.07 0.00 0.17
8 1.0975 0.00 -0.01 0.00 -0.05
9 1.2096 0.00 0.05 0.00 -0.31
10 7.1645 0.00 -0.18 0.00 -0.47
11 7.1646 0.00 0.40 0.00 0.31
12 7.1648 0.00 -0.25 0.00 0.18
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.
14TF116 quality flag:3 Type: 5:3EE 5:3EE 5:3EE axisobj 42.338 42.339 42.338 ecceobj 0.236 0.236 0.236 incobj 3.638 3.638 3.638 qmin 31.448 31.443 31.453 qmax 54.069 54.135 54.069 amean 42.328 42.328 42.328 amin 41.715 41.710 41.745 amax 43.010 43.014 43.003 emean 0.243 0.243 0.243 emin 0.228 0.227 0.228 emax 0.258 0.259 0.258 imean 2.811 3.087 2.960 imin 1.913 1.968 1.968 imax 3.778 4.447 4.122 excite_mean 0.248 0.249 0.249 fracstop 1.000 1.000 1.000 cjmean 3.008 3.008 3.008 libcent 0 181.2 179.3 179.6 libamp 0 135.7 135.3 137.5 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 195.1 199.2 164.1 kozaiamp 179.8 180.0 180.0