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: 14TY115 # Created Sat Apr 20 01:16:30 2024 # Orbit generated from Bernstein formalism # Fitting 11 observations of 11 # Arc: 4.12y # First observation: 2014/10/03 # Last observation: 2018/11/15 Preliminary a, adot, b, bdot, g, gdot: 0.000311 0.032801 -0.000057 -0.007867 0.027206 0.000000 # Chi-squared of fit: 5.13 DOF: 16 RMS: 0.12 # Min/Max residuals: -0.15 0.36 # Exact a, adot, b, bdot, g, gdot: 1.998117E-05 3.324302E-02 -4.906190E-06 -7.966473E-03 2.711589E-02 3.152290E-03 # Covariance matrix: 1.0201E-12 4.2255E-14 -1.1919E-13 -2.3807E-14 9.8057E-13 1.0354E-12 4.2255E-14 6.9300E-13 -7.1167E-15 -1.6531E-13 4.3887E-13 6.0152E-12 -1.1919E-13 -7.1167E-15 3.2962E-13 -9.2643E-14 -1.5806E-13 -2.7657E-14 -2.3807E-14 -1.6531E-13 -9.2643E-14 9.2305E-14 -9.8653E-14 -1.5492E-12 9.8057E-13 4.3887E-13 -1.5806E-13 -9.8653E-14 1.4560E-12 3.8098E-12 1.0354E-12 6.0152E-12 -2.7657E-14 -1.5492E-12 3.8098E-12 5.6315E-11 # lat0 lon0 xBary yBary zBary JD0 -22.881971 21.268081 0.201059 -0.381882 -0.905271 2456933.793808 # Heliocentric elements and errors Epoch: 2456930.5000 = 2014/09/30 Mean Anomaly: 3.49130 +/- 0.009 Argument of Peri: 226.37848 +/- 0.035 Long of Asc Node: 143.63735 +/- 0.001 Inclination: 25.98606 +/- 0.000 Eccentricity: 0.53643829 +/- 0.0002 Semi-Major Axis: 80.70716508 +/- 0.0354 Time of Perihelion: 2454362.1707 +/- 6.3 Perihelion: 37.41275113 +/- 0.0227 Aphelion: 124.00157902 +/- 0.0565 Period (y) 725.0640 +/- 0.48 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 32.64839359 +/- 0.0014 Ecliptic Y 12.49542215 +/- 0.0005 Ecliptic Z -14.33992217 +/- 0.0006 Ecliptic XDOT -0.00124030 +/- 0.0000 Ecliptic YDOT 0.00311617 +/- 0.0000 Ecliptic ZDOT -0.00086471 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 37.78473960 +/- 0.0013 Geocenter to KBO 36.87875095 +/- 0.0016 # Hcoef: 7.93
The following table shows the complete astrometric record for 14TY115. 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 (14TY115) followed by the observatory code and reference code for the source of the astrometry.
2014 10 03.29303 01 52 59.496 -12 55 59.74 24.0r 14TY115 W84 C~55SO 2014 11 21.22583 01 49 10.749 -13 15 07.68 23.2r 14TY115 W84 C~55SO 2014 11 21.23130 01 49 10.759 -13 15 07.52 24.4g 14TY115 W84 C~55SO 2014 12 23.07137 01 47 37.048 -13 09 54.48 23.7i 14TY115 W84 C~55SO 2014 12 24.11955 01 47 35.431 -13 09 29.51 24.3r 14TY115 W84 C~55SO 2016 11 25.11500 02 04 34.477 -12 38 47.64 23.6r 14TY115 W84 C~55SO 2017 11 01.15617 02 14 10.432 -12 14 16.65 22.9z 14TY115 W84 C~55SO 2017 12 15.10462 02 11 08.327 -12 17 25.26 23.7r 14TY115 W84 C~55SO 2017 12 23.14087 02 10 48.316 -12 14 59.86 23.6i 14TY115 W84 C~55SO 2018 11 15.25765 02 20 44.407 -11 58 05.48 23.7r 14TY115 W84 C~55SO 2018 11 15.25902 02 20 44.399 -11 58 05.43 23.5i 14TY115 W84 C~55SP
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 -0.12 0.00 0.05
2 0.1340 -3528.18 -0.15 202.81 0.05
3 0.1340 -3527.99 0.36 202.90 0.04
4 0.2212 -4678.71 -0.04 1007.89 -0.12
5 0.2240 -4691.23 -0.02 1039.91 0.03
6 2.1460 9786.05 -0.13 -2969.35 -0.13
7 3.0797 18160.09 0.23 -4959.56 -0.10
8 3.2000 15617.55 -0.12 -4065.69 0.09
9 3.2220 15404.41 0.07 -3815.05 0.01
10 4.1176 23905.47 -0.04 -6407.58 -0.00
11 4.1176 23905.38 -0.03 -6407.49 0.07
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.
14TY115 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 82.309 82.423 82.195 ecceobj 0.546 0.546 0.545 incobj 25.943 25.943 25.943 qmin 36.310 35.940 35.965 qmax 128.258 128.402 128.536 amean 80.847 80.826 80.854 amin 79.697 79.620 79.555 amax 82.605 82.662 82.670 emean 0.536 0.539 0.539 emin 0.523 0.520 0.521 emax 0.553 0.555 0.555 imean 24.796 24.495 24.518 imin 24.060 23.732 23.751 imax 25.433 25.728 25.669 excite_mean 0.680 0.680 0.680 fracstop 1.000 1.000 1.000 cjmean 2.884 2.884 2.884 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 211.6 178.1 183.0 kozaiamp 180.0 180.0 180.0