Orbit Fit and Astrometric record for 13TJ187

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: 13TJ187   
# Created Sun Nov 24 02:09:39 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     36 observations of     36
# Arc:   6.07y
# First observation: 2013/09/02
#  Last observation: 2019/09/27
# Chi-squared of fit:    10.83 DOF:     66 RMS:  0.10
# Min/Max residuals:    -0.23    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.481558E-05  2.220195E-02  3.481047E-06  3.449474E-03  2.369995E-02  2.475965E-03
# Covariance matrix:
  2.9248E-13 -7.8272E-14  1.7052E-15 -6.2822E-15  1.6754E-13 -3.6154E-13
 -7.8272E-14  8.1103E-14 -8.6156E-15  1.2436E-14  9.5830E-15  6.5840E-13
  1.7052E-15 -8.6156E-15  1.2927E-13 -3.2539E-14 -6.5840E-15 -8.3540E-14
 -6.2822E-15  1.2436E-14 -3.2539E-14  1.3275E-14  4.4831E-15  1.1818E-13
  1.6754E-13  9.5830E-15 -6.5840E-15  4.4831E-15  2.2994E-13  1.9933E-13
 -3.6154E-13  6.5840E-13 -8.3540E-14  1.1818E-13  1.9933E-13  6.2389E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
   -6.344502    3.536312    0.408015   -0.102015   -0.918327  2456537.840508
# Heliocentric elements and errors
Epoch:              2456538.5000  =  2013/09/03
Mean Anomaly:           88.79145 +/-     0.053
Argument of Peri:      224.35542 +/-     0.041
Long of Asc Node:       38.11887 +/-     0.001
Inclination:            10.70672 +/-     0.000
Eccentricity:         0.09863370 +/-    0.0001
Semi-Major Axis:     42.78891247 +/-    0.0037
Time of Perihelion: 2431323.2107 +/-      15.3
Perihelion:          38.56848391 +/-    0.0056
Aphelion:            47.00934104 +/-    0.0061
Period (y)              279.9014 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           42.80302704 +/-    0.0008
Ecliptic Y            2.23950179 +/-    0.0000
Ecliptic Z           -4.66259173 +/-    0.0001
Ecliptic XDOT         0.00016330 +/-    0.0000
Ecliptic YDOT         0.00257907 +/-    0.0000
Ecliptic ZDOT         0.00036458 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   43.11436974 +/-    0.0008
Geocenter to KBO     42.19414194 +/-    0.0009
# Hcoef:  7.08

The following table shows the complete astrometric record for 13TJ187. 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 (13TJ187) followed by the observatory code and reference code for the source of the astrometry.

2013 09  02.33973  00 23 04.311  -04 24 58.64  24.5g 13TJ187   W84  C~4yRD      
2013 10  13.15746  00 20 08.590  -04 42 50.72  23.2i 13TJ187   W84  C~4yRD      
2013 10  13.15746  00 20 08.59   -04 42 50.7   23.4i 13TJ187   W84  C~3clQ      
2013 10  13.15883  00 20 08.591  -04 42 50.64  23.1z 13TJ187   W84  C~4yRD      
2013 10  13.15883  00 20 08.59   -04 42 50.6   23.0z 13TJ187   W84  C~3clQ      
2013 11  23.13213  00 17 49.616  -04 52 16.63  23.6r 13TJ187   W84  C~4yRD      
2013 11  23.13496  00 17 49.611  -04 52 16.63  23.2i 13TJ187   W84  C~4yRD      
2013 12  02.11033  00 17 33.558  -04 52 22.34  22.9r 13TJ187   W84  C~4yRD      
2013 12  02.11033  00 17 33.56   -04 52 22.4   23.0r 13TJ187   W84  C~3clQ      
2014 10  02.24072  00 25 19.17   -03 57 07.6   23.2i 13TJ187   W84  C~3clQ      
2014 11  14.12260  00 22 32.693  -04 10 30.80  22.8i 13TJ187   W84  C~4yRD      
2014 11  15.10699  00 22 29.906  -04 10 39.85  23.0z 13TJ187   W84  C~4yRD      
2016 09  09.16734  00 35 33.988  -02 24 59.26  22.8i 13TJ187   W84  C~4yRD      
2016 09  09.16734  00 35 33.99   -02 24 59.2   23.1i 13TJ187   W84  C~3clQ      
2016 09  09.16872  00 35 33.981  -02 24 59.45  22.7z 13TJ187   W84  C~4yRD      
2016 09  09.16872  00 35 33.98   -02 24 59.4   22.7z 13TJ187   W84  C~3clQ      
2016 09  09.27089  00 35 33.562  -02 25 01.97  23.7r 13TJ187   W84  C~4yRD      
2016 09  09.27089  00 35 33.56   -02 25 02.0   23.7r 13TJ187   W84  C~3clQ      
2016 10  01.19983  00 33 59.707  -02 34 48.97  23.1r 13TJ187   W84  C~4yRD      
2016 10  01.19983  00 33 59.70   -02 34 48.9   23.5r 13TJ187   W84  C~3clQ      
2016 10  01.20122  00 33 59.684  -02 34 49.10  23.1i 13TJ187   W84  C~4yRD      
2016 11  18.07307  00 30 55.032  -02 49 49.68  23.4r 13TJ187   W84  C~4yRD      
2016 11  18.07307  00 30 55.03   -02 49 49.7   23.6r 13TJ187   W84  C~3clQ      
2016 11  18.07445  00 30 55.024  -02 49 49.50  24.1g 13TJ187   W84  C~4yRD      
2017 09  18.24293  00 39 13.871  -01 48 07.06  23.1i 13TJ187   W84  C~4yRD      
2017 09  18.24430  00 39 13.873  -01 48 07.16  23.5r 13TJ187   W84  C~4yRD      
2017 09  18.24567  00 39 13.862  -01 48 07.15  24.3g 13TJ187   W84  C~4yRD      
2017 10  22.15797  00 36 46.716  -02 02 13.73  22.8z 13TJ187   W84  C~4yRD      
2017 10  28.17095  00 36 22.418  -02 04 14.84  22.1z 13TJ187   W84  C~4yRD      
2018 09  09.34244  00 44 06.375  -01 03 23.75  23.2r 13TJ187   W84  C~4yRD      
2018 11  08.17671  00 39 57.408  -01 26 43.69  23.4r 13TJ187   W84  C~4yRD      
2018 11  08.17810  00 39 57.408  -01 26 43.43  22.7i 13TJ187   W84  C~4yRD      
2018 11  27.08173  00 39 02.222  -01 30 01.81  23.9g 13TJ187   W84  C~4yRD      
2019 09  27.30586  00 47 07.08   -00 30 36.0   25.1g 13TJ187   T09  C~85E0      
2019 09  27.50183  00 47 06.21   -00 30 41.2   24.6g 13TJ187   T09  C~85E0      
2019 09  27.56948  00 47 05.91   -00 30 42.8   25.2g 13TJ187   T09  C~85E0      

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     0.10       0.00    -0.22
     2   0.1118      0.00    -0.10       0.00    -0.01
     3   0.1118      0.00    -0.10       0.00    -0.03
     4   0.1118      0.00    -0.02       0.00     0.12
     5   0.1118      0.00    -0.00       0.00     0.08
     6   0.2239      0.00     0.01       0.00     0.02
     7   0.2239      0.00     0.03       0.00     0.03
     8   0.2485      0.00     0.03       0.00     0.04
     9   0.2485      0.00     0.06       0.00    -0.02
    10   1.0812      0.00    -0.04       0.00     0.01
    11   1.1986      0.00    -0.22       0.00     0.21
    12   1.2013      0.00     0.03       0.00     0.07
    13   3.0194      0.00     0.09       0.00     0.04
    14   3.0194      0.00     0.06       0.00    -0.02
    15   3.0194      0.00     0.04       0.00    -0.17
    16   3.0194      0.00     0.03       0.00    -0.12
    17   3.0197      0.00    -0.01       0.00     0.01
    18   3.0197      0.00     0.02       0.00     0.04
    19   3.0797      0.00     0.13       0.00     0.02
    20   3.0797      0.00     0.23       0.00    -0.05
    21   3.0797      0.00    -0.02       0.00    -0.15
    22   3.2108      0.00    -0.03       0.00     0.03
    23   3.2108      0.00    -0.00       0.00     0.05
    24   3.2108      0.00    -0.07       0.00     0.24
    25   4.0435      0.00    -0.06       0.00    -0.05
    26   4.0435      0.00     0.05       0.00    -0.12
    27   4.0435      0.00    -0.02       0.00    -0.07
    28   4.1364      0.00     0.02       0.00    -0.03
    29   4.1529      0.00    -0.00       0.00    -0.13
    30   5.0185      0.00     0.04       0.00     0.02
    31   5.1823      0.00    -0.02       0.00    -0.09
    32   5.1823      0.00     0.06       0.00     0.20
    33   5.2341      0.00     0.04       0.00    -0.23
    34   6.0670      0.00    -0.02       0.00     0.10
    35   6.0675      0.00    -0.08       0.00     0.05
    36   6.0677      0.00    -0.10       0.00     0.23

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.

13TJ187    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.022    43.022    43.021
ecceobj         0.100     0.100     0.100
incobj         10.692    10.692    10.692
qmin           37.790    37.801    37.732
qmax           48.103    48.086    48.148
amean          42.828    42.828    42.828
amin           42.476    42.474    42.478
amax           43.208    43.206    43.192
emean           0.095     0.095     0.095
emin            0.078     0.077     0.078
emax            0.115     0.115     0.115
imean           9.448     9.448     9.448
imin            8.572     8.576     8.570
imax           10.380    10.380    10.377
excite_mean     0.190     0.190     0.189
fracstop        1.000     1.000     1.000
cjmean          3.045     3.045     3.045

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       180.7     180.7     180.7
kozaiamp        180.0     180.0     179.9