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: 14TA116 # Created Fri Apr 26 01:16:26 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 15 observations of 15 # Arc: 8.07y # First observation: 2014/10/03 # Last observation: 2022/10/29 # Chi-squared of fit: 12.71 DOF: 24 RMS: 0.16 # Min/Max residuals: -0.35 0.43 # Exact a, adot, b, bdot, g, gdot: 1.720921E-05 2.892517E-02 -4.106978E-06 -6.956329E-03 2.700184E-02 -3.602282E-04 # Covariance matrix: 3.8381E-13 -8.1539E-14 -8.8636E-15 1.4982E-14 3.6084E-13 -2.3211E-13 -8.1539E-14 2.6217E-13 5.1764E-14 -6.2585E-14 3.6747E-13 1.0333E-12 -8.8636E-15 5.1764E-14 1.9746E-13 -4.3680E-14 7.9595E-14 2.1305E-13 1.4982E-14 -6.2585E-14 -4.3680E-14 2.7002E-14 -8.6296E-14 -2.5812E-13 3.6084E-13 3.6747E-13 7.9595E-14 -8.6296E-14 1.5525E-12 1.4603E-12 -2.3211E-13 1.0333E-12 2.1305E-13 -2.5812E-13 1.4603E-12 4.2597E-12 # lat0 lon0 xBary yBary zBary JD0 -23.700188 34.279660 0.415728 -0.366666 -0.835712 2456933.880368 # Heliocentric elements and errors Epoch: 2456934.5000 = 2014/10/04 Mean Anomaly: 352.34128 +/- 0.018 Argument of Peri: 251.62913 +/- 0.026 Long of Asc Node: 155.67139 +/- 0.000 Inclination: 26.76830 +/- 0.000 Eccentricity: 0.16645106 +/- 0.0001 Semi-Major Axis: 45.31986294 +/- 0.0097 Time of Perihelion: 2459305.2471 +/- 35.3 Perihelion: 37.77632363 +/- 0.0104 Aphelion: 52.86340224 +/- 0.0130 Period (y) 305.0992 +/- 0.10 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 29.00602868 +/- 0.0013 Ecliptic Y 19.27211085 +/- 0.0009 Ecliptic Z -14.88623320 +/- 0.0007 Ecliptic XDOT -0.00191838 +/- 0.0000 Ecliptic YDOT 0.00224025 +/- 0.0000 Ecliptic ZDOT -0.00063106 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 37.87301423 +/- 0.0011 Geocenter to KBO 37.03454422 +/- 0.0017 # Hcoef: 7.73
The following table shows the complete astrometric record for 14TA116. 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 (14TA116) followed by the observatory code and reference code for the source of the astrometry.
2014 10 03.37959 02 39 40.669 -09 25 05.00 23.1i 14TA116 W84 C~55SP 2014 10 21.33806 02 38 18.787 -09 36 32.03 23.6r 14TA116 W84 C~55SP 2014 10 21.34079 02 38 18.782 -09 36 32.16 23.5i 14TA116 W84 C~55SP 2014 10 23.33268 02 38 08.969 -09 37 38.60 23.2i 14TA116 W84 C~55SP 2014 10 28.31273 02 37 44.022 -09 40 13.57 23.1r 14TA116 W84 C~55SP 2016 09 24.30614 02 53 55.997 -08 56 56.17 23.2r 14TA116 W84 C~55SP 2016 10 26.31829 02 51 38.017 -09 17 46.82 23.0r 14TA116 W84 C~55SP 2016 11 03.21230 02 50 58.056 -09 21 33.56 22.6i 14TA116 W84 C~55SP 2016 11 04.21319 02 50 52.910 -09 21 59.39 23.4r 14TA116 W84 C~55SP 2016 11 25.15088 02 49 07.402 -09 28 02.31 24.5g 14TA116 W84 C~55SP 2016 12 02.13300 02 48 34.802 -09 28 43.55 23.5i 14TA116 W84 C~55SP 2016 12 02.14268 02 48 34.768 -09 28 43.68 24.1g 14TA116 W84 C~55SP 2022 10 29.372040 03 32 39.048 -08 02 09.01 24.0G 14TA116 G37 C~5z2t 2022 10 29.420000 03 32 38.829 -08 02 10.24 14TA116 G37 C~5z2t 2022 10 29.468380 03 32 38.591 -08 02 12.31 14TA116 G37 C~5z2t
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 -0.06 0.00 -0.01
2 0.0492 0.00 -0.12 0.00 0.09
3 0.0492 0.00 0.01 0.00 0.05
4 0.0546 0.00 0.17 0.00 -0.12
5 0.0683 0.00 -0.01 0.00 0.03
6 1.9765 0.00 -0.04 0.00 0.08
7 2.0642 0.00 -0.35 0.00 -0.22
8 2.0858 0.00 0.43 0.00 0.05
9 2.0885 0.00 0.18 0.00 -0.04
10 2.1458 0.00 0.08 0.00 0.21
11 2.1650 0.00 -0.20 0.00 0.02
12 2.1650 0.00 -0.04 0.00 -0.09
13 8.0712 0.00 -0.18 0.00 -0.00
14 8.0713 0.00 0.08 0.00 0.27
15 8.0714 0.00 0.08 0.00 -0.28
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.
14TA116 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 45.709 45.709 45.709 ecceobj 0.173 0.173 0.173 incobj 26.709 26.709 26.709 qmin 37.208 37.208 37.150 qmax 53.782 53.788 53.889 amean 45.315 45.317 45.312 amin 44.934 44.934 44.923 amax 45.747 45.746 45.737 emean 0.161 0.161 0.162 emin 0.146 0.146 0.146 emax 0.176 0.176 0.179 imean 25.895 25.900 25.878 imin 25.502 25.515 25.495 imax 26.243 26.251 26.221 excite_mean 0.465 0.466 0.466 fracstop 1.000 1.000 1.000 cjmean 2.843 2.843 2.843 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 180.6 180.7 180.5 kozaiamp 180.0 180.0 179.9