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: 14YH92 # Created Thu Apr 25 01:16:48 2024 # Orbit generated from Bernstein formalism # Fitting 13 observations of 13 # Arc: 3.93y # First observation: 2014/12/23 # Last observation: 2018/11/29 Preliminary a, adot, b, bdot, g, gdot: -0.000019 0.026816 -0.000071 0.006979 0.027373 0.000000 # Chi-squared of fit: 5.50 DOF: 20 RMS: 0.11 # Min/Max residuals: -0.20 0.22 # Exact a, adot, b, bdot, g, gdot: 1.666590E-05 2.639337E-02 3.320364E-06 6.813893E-03 2.656084E-02 -2.560240E-03 # Covariance matrix: 3.0488E-13 -2.2273E-13 1.4656E-14 -3.3479E-14 -8.4182E-14 -1.3923E-12 -2.2273E-13 1.1774E-12 -1.0818E-13 2.0888E-13 -1.7876E-13 1.1398E-11 1.4656E-14 -1.0818E-13 2.7006E-13 -1.2138E-13 8.6485E-15 -1.1222E-12 -3.3479E-14 2.0888E-13 -1.2138E-13 1.1016E-13 1.0062E-16 2.1884E-12 -8.4182E-14 -1.7876E-13 8.6485E-15 1.0062E-16 3.6576E-13 -1.4033E-12 -1.3923E-12 1.1398E-11 -1.1222E-12 2.1884E-12 -1.4033E-12 1.1760E-10 # lat0 lon0 xBary yBary zBary JD0 -26.342007 19.205787 -0.932343 -0.137716 -0.278588 2457014.580398 # Heliocentric elements and errors Epoch: 2457010.5000 = 2014/12/19 Mean Anomaly: 288.72026 +/- 0.082 Argument of Peri: 17.42734 +/- 0.128 Long of Asc Node: 79.22825 +/- 0.001 Inclination: 29.92245 +/- 0.000 Eccentricity: 0.07309667 +/- 0.0004 Semi-Major Axis: 38.65390397 +/- 0.0039 Time of Perihelion: 2474390.5912 +/- 19.8 Perihelion: 35.82843244 +/- 0.0151 Aphelion: 41.47937550 +/- 0.0153 Period (y) 240.3246 +/- 0.04 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 31.84590012 +/- 0.0007 Ecliptic Y 12.08335801 +/- 0.0003 Ecliptic Z -16.70606636 +/- 0.0004 Ecliptic XDOT -0.00082803 +/- 0.0000 Ecliptic YDOT 0.00258871 +/- 0.0000 Ecliptic ZDOT 0.00074663 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 37.93760072 +/- 0.0006 Geocenter to KBO 37.64941588 +/- 0.0009 # Hcoef: 8.07
The following table shows the complete astrometric record for 14YH92. 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 (14YH92) followed by the observatory code and reference code for the source of the astrometry.
2014 12 23.07962 01 51 21.998 -16 50 55.64 23.9r 14YH92 W84 C~55TR 2014 12 24.14669 01 51 19.767 -16 50 18.10 24.5r 14YH92 W84 C~55TR 2015 01 12.09103 01 50 59.205 -16 36 48.81 23.2i 14YH92 W84 C~55TR 2015 01 12.09242 01 50 59.208 -16 36 48.69 23.9r 14YH92 W84 C~55TR 2015 01 16.08166 01 50 59.701 -16 33 28.71 23.9r 14YH92 W84 C~55TR 2016 09 30.24057 02 08 05.082 -14 49 15.72 22.8i 14YH92 W84 C~55TR 2016 09 30.24194 02 08 05.061 -14 49 16.07 23.7r 14YH92 W84 C~55TR 2016 10 02.23745 02 07 55.511 -14 50 26.06 23.0i 14YH92 W84 C~55TR 2016 10 02.23883 02 07 55.485 -14 50 26.24 23.9r 14YH92 W84 C~55TR 2016 10 02.24020 02 07 55.491 -14 50 26.12 24.5g 14YH92 W84 C~55TR 2017 12 14.07451 02 07 09.450 -14 00 26.30 24.2r 14YH92 W84 C~55TR 2017 12 22.14266 02 06 45.431 -13 56 52.76 24.1r 14YH92 W84 C~55TR 2018 11 29.22351 02 13 15.219 -13 04 22.79 24.3r 14YH92 W84 C~55TR
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 -0.20 0.00 0.15
2 0.0029 -14.73 0.05 47.10 -0.13
3 0.0548 31.00 0.01 907.40 0.01
4 0.0548 31.09 0.07 907.49 0.04
5 0.0657 116.01 0.08 1088.69 0.01
6 1.7718 16220.89 0.14 870.16 0.22
7 1.7718 16220.47 -0.17 869.97 0.03
8 1.7773 16064.51 0.13 862.97 -0.16
9 1.7773 16064.09 -0.18 862.96 -0.17
10 1.7773 16064.22 0.05 863.03 -0.09
11 2.9760 16689.19 0.12 3883.61 0.13
12 2.9981 16456.24 -0.05 4222.52 -0.03
13 3.9347 22995.90 -0.03 4760.07 0.01
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.
14YH92 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 38.970 38.983 38.957 ecceobj 0.073 0.072 0.073 incobj 29.923 29.923 29.923 qmin 35.208 35.173 35.189 qmax 42.449 42.531 42.455 amean 38.729 38.743 38.715 amin 38.444 38.452 38.424 amax 39.040 39.061 39.018 emean 0.074 0.075 0.074 emin 0.061 0.062 0.061 emax 0.088 0.090 0.088 imean 28.265 28.252 28.264 imin 27.783 27.774 27.776 imax 28.817 28.817 28.827 excite_mean 0.479 0.479 0.479 fracstop 1.000 1.000 1.000 cjmean 2.771 2.771 2.771 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 171.6 171.7 171.4 kozaiamp 179.9 180.0 180.0