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: 14RY86 # Created Thu Apr 25 01:16:08 2024 # Orbit generated from Bernstein formalism # Fitting 13 observations of 13 # Arc: 4.01y # First observation: 2014/09/12 # Last observation: 2018/09/15 Preliminary a, adot, b, bdot, g, gdot: 0.000070 0.031026 -0.000085 0.004094 0.029142 0.000000 # Chi-squared of fit: 3.88 DOF: 20 RMS: 0.10 # Min/Max residuals: -0.23 0.14 # Exact a, adot, b, bdot, g, gdot: 1.871795E-05 3.136106E-02 3.104626E-06 4.175333E-03 2.819934E-02 2.539036E-03 # Covariance matrix: 3.2364E-13 -1.5958E-14 -7.2280E-14 -9.1535E-15 1.0209E-12 3.6101E-13 -1.5958E-14 8.4389E-13 -1.7050E-13 8.7542E-14 2.2482E-12 6.9854E-12 -7.2280E-14 -1.7050E-13 3.0684E-13 -8.2058E-14 -1.0567E-12 -1.3971E-12 -9.1535E-15 8.7542E-14 -8.2058E-14 5.9355E-14 9.8068E-14 7.9266E-13 1.0209E-12 2.2482E-12 -1.0567E-12 9.8068E-14 1.4585E-11 1.8311E-11 3.6101E-13 6.9854E-12 -1.3971E-12 7.9266E-13 1.8311E-11 6.1473E-11 # lat0 lon0 xBary yBary zBary JD0 -27.542238 -59.496199 -0.755375 -0.309303 -0.593374 2456912.558638 # Heliocentric elements and errors Epoch: 2456910.5000 = 2014/09/10 Mean Anomaly: 27.71667 +/- 0.084 Argument of Peri: 245.76626 +/- 0.126 Long of Asc Node: 14.26371 +/- 0.001 Inclination: 28.17181 +/- 0.000 Eccentricity: 0.18315940 +/- 0.0003 Semi-Major Axis: 42.56137070 +/- 0.0259 Time of Perihelion: 2449102.1292 +/- 22.6 Perihelion: 34.76585556 +/- 0.0247 Aphelion: 50.35688584 +/- 0.0332 Period (y) 277.6717 +/- 0.25 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 16.94902392 +/- 0.0022 Ecliptic Y -27.28252110 +/- 0.0037 Ecliptic Z -16.39753874 +/- 0.0022 Ecliptic XDOT 0.00282476 +/- 0.0000 Ecliptic YDOT 0.00119122 +/- 0.0000 Ecliptic ZDOT 0.00024557 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 36.06223296 +/- 0.0031 Geocenter to KBO 35.46182764 +/- 0.0048 # Hcoef: 8.06
The following table shows the complete astrometric record for 14RY86. 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 (14RY86) followed by the observatory code and reference code for the source of the astrometry.
2014 09 12.05786 20 44 10.106 -46 43 46.92 24.2g 14RY86 W84 C~52Tx 2014 09 12.05921 20 44 10.115 -46 43 46.68 23.9r 14RY86 W84 C~52Tx 2014 09 19.99209 20 43 30.553 -46 40 27.29 23.2r 14RY86 W84 C~52Tx 2014 09 20.01434 20 43 30.428 -46 40 26.52 24.8g 14RY86 W84 C~52Tx 2014 09 26.99952 20 43 02.028 -46 36 47.70 23.2i 14RY86 W84 C~52Tx 2014 10 01.01545 20 42 48.652 -46 34 24.77 23.4i 14RY86 W84 C~52Tx 2016 10 02.04643 21 01 08.015 -44 58 58.59 23.6r 14RY86 W84 C~52Tx 2016 10 02.04780 21 01 08.012 -44 58 58.65 24.0i 14RY86 W84 C~52Tx 2016 10 02.04919 21 01 08.024 -44 58 58.53 24.8g 14RY86 W84 C~52Tx 2017 10 13.06273 21 09 21.379 -44 01 43.45 24.4g 14RY86 W84 C~52Tx 2017 10 15.10289 21 09 17.205 -44 00 21.27 23.9r 14RY86 W84 C~52Tx 2018 09 15.20625 21 19 42.003 -43 21 24.79 23.4r 14RY86 W84 C~52Tx 2018 09 15.20763 21 19 42.012 -43 21 24.61 22.2i 14RY86 W84 C~52Tx
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 -0.23 0.00 -0.16
2 0.0000 0.16 -0.01 0.20 -0.01
3 0.0217 -330.35 0.07 310.28 -0.11
4 0.0218 -331.35 -0.10 311.39 0.09
5 0.0409 -547.22 0.13 606.04 0.04
6 0.0519 -637.58 0.14 782.89 0.11
7 2.0561 12099.22 -0.03 2556.58 0.09
8 2.0561 12099.16 -0.05 2556.54 -0.02
9 2.0561 12099.33 0.14 2556.61 -0.01
10 3.0856 18290.34 0.02 3890.41 0.02
11 3.0912 18278.73 -0.11 3983.79 -0.01
12 4.0086 25516.25 -0.10 3550.72 -0.06
13 4.0086 25516.41 0.14 3550.85 0.02
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.
14RY86 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 42.596 42.675 42.517 ecceobj 0.183 0.184 0.182 incobj 28.178 28.178 28.178 qmin 34.077 34.267 34.171 qmax 51.768 51.875 51.596 amean 42.751 42.867 42.686 amin 42.381 42.474 42.308 amax 43.166 43.326 43.116 emean 0.181 0.178 0.177 emin 0.160 0.158 0.158 emax 0.200 0.200 0.197 imean 28.189 28.276 28.243 imin 27.647 27.731 27.694 imax 28.752 28.791 28.684 excite_mean 0.506 0.506 0.505 fracstop 1.000 1.000 1.000 cjmean 2.769 2.770 2.769 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 181.8 183.6 184.7 kozaiamp 180.0 180.0 180.0