Orbit Fit and Astrometric record for 13RJ109

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: 13RJ109   
# Created Sun Dec 22 02:09:31 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     65 observations of     65
# Arc:   7.04y
# First observation: 2013/09/08
#  Last observation: 2020/09/21
# Chi-squared of fit:    16.02 DOF:    124 RMS:  0.09
# Min/Max residuals:    -0.31    0.29
# Exact a, adot, b, bdot, g, gdot:
  1.452432E-05  2.196320E-02 -5.266953E-06 -7.834740E-03  2.412890E-02 -3.053416E-03
# Covariance matrix:
  9.1071E-14 -3.7840E-14 -5.3433E-15  7.3432E-15  2.4013E-14 -1.6564E-13
 -3.7840E-14  3.3155E-14  7.6808E-15 -1.0124E-14 -4.3228E-15  2.2784E-13
 -5.3433E-15  7.6808E-15  7.4367E-14 -2.0888E-14  6.5756E-16  6.5937E-14
  7.3432E-15 -1.0124E-14 -2.0888E-14  1.0312E-14  6.4351E-16 -8.6611E-14
  2.4013E-14 -4.3228E-15  6.5756E-16  6.4351E-16  1.0520E-13 -1.6365E-14
 -1.6564E-13  2.2784E-13  6.5937E-14 -8.6611E-14 -1.6365E-14  1.9489E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
    5.343636  -11.747045    0.051067    0.093876   -1.002753  2456543.662238
# Heliocentric elements and errors
Epoch:              2456544.5000  =  2013/09/09
Mean Anomaly:          286.24372 +/-     0.013
Argument of Peri:      253.83780 +/-     0.019
Long of Asc Node:      182.47513 +/-     0.000
Inclination:            20.30295 +/-     0.000
Eccentricity:         0.13390254 +/-    0.0001
Semi-Major Axis:     43.31920864 +/-    0.0024
Time of Perihelion: 2477880.6316 +/-       7.9
Perihelion:          37.51865670 +/-    0.0033
Aphelion:            49.11976058 +/-    0.0037
Period (y)              285.1208 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           41.37524457 +/-    0.0005
Ecliptic Y           -8.65296746 +/-    0.0001
Ecliptic Z            3.85941898 +/-    0.0001
Ecliptic XDOT         0.00024451 +/-    0.0000
Ecliptic YDOT         0.00249215 +/-    0.0000
Ecliptic ZDOT        -0.00091725 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.44628341 +/-    0.0005
Geocenter to KBO     41.44420118 +/-    0.0006
# Hcoef:  6.94

The following table shows the complete astrometric record for 13RJ109. 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 (13RJ109) followed by the observatory code and reference code for the source of the astrometry.

2013 09  08.16146  23 08 27.152  +00 16 32.57  24.0g 13RJ109   W84  C~4yQp      
2013 09  13.18754  23 08 05.324  +00 13 49.61  22.5i 13RJ109   W84  C~4yQp      
2013 09  30.097315 23 06 54.41   +00 04 30.4   22.7r 13RJ109   W84  C~35bW      
2013 09  30.09784  23 06 54.411  +00 04 30.38  22.9r 13RJ109   W84  C~4yQp      
2013 09  30.098785 23 06 54.41   +00 04 30.3   22.8i 13RJ109   W84  C~35bW      
2013 09  30.09931  23 06 54.404  +00 04 30.31  22.6i 13RJ109   W84  C~4yQp      
2013 09  30.109363 23 06 54.36   +00 04 29.9   23.0r 13RJ109   W84  C~35bW      
2013 09  30.10989  23 06 54.364  +00 04 29.93  23.0r 13RJ109   W84  C~4yQp      
2013 09  30.113843 23 06 54.35   +00 04 29.8   22.7i 13RJ109   W84  C~35bW      
2013 09  30.11437  23 06 54.346  +00 04 29.79  22.6i 13RJ109   W84  C~4yQp      
2013 10  11.09647  23 06 12.963  -00 01 25.08  22.4z 13RJ109   W84  C~4yQp      
2013 10  12.06808  23 06 09.569  -00 01 55.49  22.4i 13RJ109   W84  C~4yQp      
2013 10  12.06945  23 06 09.565  -00 01 55.37  22.3z 13RJ109   W84  C~4yQp      
2013 10  13.039225 23 06 06.22   -00 02 25.8   22.4z 13RJ109   W84  C~36Su      
2013 10  13.03975  23 06 06.217  -00 02 25.76  22.7z 13RJ109   W84  C~4yQp      
2013 10  13.12418  23 06 05.925  -00 02 28.28  22.9i 13RJ109   W84  C~4yQp      
2013 11  23.06358  23 04 43.173  -00 18 57.30  23.2r 13RJ109   W84  C~4yQp      
2016 07  29.54398  23 27 07.30   +00 48 07.8   22.6z 13RJ109   T09  C~8Af5      
2016 07  29.55844  23 27 07.24   +00 48 07.5   22.8z 13RJ109   T09  C~8Af5      
2016 07  29.57290  23 27 07.20   +00 48 07.0   23.0z 13RJ109   T09  C~8Af5      
2016 07  29.58728  23 27 07.17   +00 48 06.8   22.8z 13RJ109   T09  C~8Af5      
2016 08  01.48420  23 26 58.69   +00 47 10.8   23.7z 13RJ109   T09  C~7gpU      
2016 08  01.51671  23 26 58.60   +00 47 10.2   23.1z 13RJ109   T09  C~7gpU      
2016 08  01.54112  23 26 58.52   +00 47 09.7   23.5z 13RJ109   T09  C~7gpU      
2016 08  01.54931  23 26 58.49   +00 47 09.5   23.3z 13RJ109   T09  C~7gpU      
2016 08  01.56281  23 26 58.45   +00 47 09.2   23.2z 13RJ109   T09  C~7gpU      
2016 08  09.43274  23 26 32.90   +00 44 17.4   23.3y 13RJ109   T09  C~7gpU      
2016 08  09.44578  23 26 32.86   +00 44 17.0   23.4y 13RJ109   T09  C~7gpU      
2016 08  09.45746  23 26 32.81   +00 44 16.9   23.2y 13RJ109   T09  C~7gpU      
2016 08  09.47657  23 26 32.76   +00 44 16.4   23.9y 13RJ109   T09  C~7gpU      
2016 08  09.50679  23 26 32.66   +00 44 15.7   24.0y 13RJ109   T09  C~7gpU      
2016 08  09.52904  23 26 32.57   +00 44 15.0   23.8y 13RJ109   T09  C~7gpU      
2016 08  09.54843  23 26 32.49   +00 44 14.7   23.4y 13RJ109   T09  C~7gpU      
2016 09  07.37087  23 24 37.00   +00 30 32.9   23.3r 13RJ109   T09  C~7gpU      
2016 09  07.39898  23 24 36.88   +00 30 32.1   23.4r 13RJ109   T09  C~7gpU      
2016 09  07.44284  23 24 36.68   +00 30 30.8   23.0r 13RJ109   T09  C~7gpU      
2016 09  07.44502  23 24 36.67   +00 30 30.7   23.0r 13RJ109   T09  C~7gpU      
2016 09  07.47602  23 24 36.54   +00 30 29.7   23.1r 13RJ109   T09  C~7gpU      
2016 09  26.13353  23 23 15.624  +00 20 10.45  23.0r 13RJ109   W84  C~4yQp      
2016 09  26.13489  23 23 15.614  +00 20 10.36  22.8i 13RJ109   W84  C~4yQp      
2016 09  26.13627  23 23 15.613  +00 20 10.43  23.2g 13RJ109   W84  C~4yQp      
2016 09  30.12434  23 22 58.915  +00 17 56.91  22.8z 13RJ109   W84  C~4yQp      
2016 10  05.13613  23 22 38.569  +00 15 10.93  22.8r 13RJ109   W84  C~4yQp      
2016 10  05.13751  23 22 38.561  +00 15 10.85  22.8i 13RJ109   W84  C~4yQp      
2016 10  05.13890  23 22 38.553  +00 15 10.81  23.9g 13RJ109   W84  C~4yQp      
2017 09  13.36589  23 29 38.36   +00 31 59.9   22.8y 13RJ109   T09  C~85Dt      
2017 09  13.38015  23 29 38.30   +00 31 59.8   23.1y 13RJ109   T09  C~85Dt      
2017 09  13.39746  23 29 38.22   +00 31 59.1   22.8y 13RJ109   T09  C~85Dt      
2017 09  13.40105  23 29 38.20   +00 31 58.9   22.7y 13RJ109   T09  C~85Dt      
2017 09  13.41178  23 29 38.14   +00 31 58.8   23.0y 13RJ109   T09  C~85Dt      
2017 09  13.41536  23 29 38.14   +00 31 58.4   23.1y 13RJ109   T09  C~85Dt      
2017 10  11.18778  23 27 41.481  +00 16 34.26  22.7i 13RJ109   W84  C~4yQp      
2017 11  08.06827  23 26 16.577  +00 03 28.51  23.7g 13RJ109   W84  C~4yQp      
2017 11  08.069120 23 26 16.57   +00 03 28.7   23.2r 13RJ109   W84  C~35bW      
2017 11  08.06964  23 26 16.577  +00 03 28.60  23.2r 13RJ109   W84  C~4yQp      
2017 11  09.04198  23 26 14.552  +00 03 06.22  23.9g 13RJ109   W84  C~4yQp      
2017 11  09.042836 23 26 14.56   +00 03 06.3   23.1r 13RJ109   W84  C~35bW      
2017 11  09.04336  23 26 14.556  +00 03 06.32  23.1r 13RJ109   W84  C~4yQp      
2018 09  17.26605  23 34 51.029  +00 34 35.26  22.4i 13RJ109   W84  C~4yQp      
2018 09  17.26746  23 34 51.026  +00 34 35.31  22.9r 13RJ109   W84  C~4yQp      
2018 09  17.26884  23 34 51.023  +00 34 35.24  23.9g 13RJ109   W84  C~4yQp      
2018 10  01.22900  23 33 50.606  +00 26 44.90  22.3z 13RJ109   W84  C~4yQp      
2020 09  21.158990 23 45 36.272  +00 41 28.73  22.8G 13RJ109   G37  C~49w4      
2020 09  21.195910 23 45 36.110  +00 41 27.45        13RJ109   G37  C~49w4      
2020 09  21.264720 23 45 35.807  +00 41 25.18        13RJ109   G37  C~49w4      

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    -0.04       0.00     0.01
     2   0.0138      0.00     0.00       0.00     0.02
     3   0.0601      0.00    -0.02       0.00     0.06
     4   0.0601      0.00     0.03       0.00     0.06
     5   0.0601      0.00     0.07       0.00     0.01
     6   0.0601      0.00     0.01       0.00     0.04
     7   0.0601      0.00    -0.03       0.00    -0.04
     8   0.0601      0.00     0.06       0.00     0.00
     9   0.0601      0.00     0.09       0.00     0.00
    10   0.0601      0.00     0.06       0.00     0.01
    11   0.0902      0.00     0.01       0.00    -0.09
    12   0.0928      0.00     0.01       0.00    -0.04
    13   0.0928      0.00     0.03       0.00     0.13
    14   0.0955      0.00    -0.06       0.00    -0.09
    15   0.0955      0.00    -0.08       0.00    -0.04
    16   0.0957      0.00    -0.04       0.00     0.06
    17   0.2078      0.00    -0.05       0.00    -0.11
    18   2.8895      0.00     0.08       0.00     0.20
    19   2.8895      0.00    -0.19       0.00     0.17
    20   2.8896      0.00    -0.16       0.00    -0.06
    21   2.8896      0.00     0.02       0.00     0.01
    22   2.8975      0.00    -0.06       0.00     0.02
    23   2.8976      0.00     0.11       0.00     0.07
    24   2.8977      0.00     0.04       0.00     0.06
    25   2.8977      0.00    -0.03       0.00     0.02
    26   2.8977      0.00     0.00       0.00    -0.01
    27   2.9193      0.00    -0.04       0.00     0.03
    28   2.9193      0.00     0.05       0.00    -0.06
    29   2.9194      0.00    -0.08       0.00     0.11
    30   2.9194      0.00     0.19       0.00     0.06
    31   2.9195      0.00     0.29       0.00     0.08
    32   2.9196      0.00     0.13       0.00    -0.10
    33   2.9196      0.00    -0.04       0.00     0.06
    34   2.9985      0.00    -0.07       0.00    -0.16
    35   2.9986      0.00    -0.00       0.00    -0.05
    36   2.9987      0.00    -0.09       0.00     0.06
    37   2.9987      0.00    -0.09       0.00     0.03
    38   2.9988      0.00     0.02       0.00     0.03
    39   3.0499      0.00     0.06       0.00    -0.03
    40   3.0499      0.00    -0.00       0.00    -0.08
    41   3.0499      0.00     0.07       0.00     0.04
    42   3.0608      0.00     0.08       0.00    -0.03
    43   3.0745      0.00     0.07       0.00    -0.03
    44   3.0745      0.00     0.04       0.00    -0.07
    45   3.0745      0.00     0.00       0.00    -0.06
    46   4.0142      0.00    -0.09       0.00    -0.26
    47   4.0143      0.00    -0.03       0.00     0.12
    48   4.0143      0.00    -0.07       0.00    -0.01
    49   4.0143      0.00    -0.13       0.00    -0.09
    50   4.0144      0.00    -0.31       0.00     0.16
    51   4.0144      0.00    -0.07       0.00    -0.12
    52   4.0904      0.00     0.07       0.00    -0.17
    53   4.1668      0.00     0.03       0.00    -0.09
    54   4.1668      0.00    -0.05       0.00     0.12
    55   4.1668      0.00     0.08       0.00     0.04
    56   4.1694      0.00     0.01       0.00    -0.08
    57   4.1694      0.00     0.16       0.00     0.02
    58   4.1694      0.00     0.11       0.00     0.05
    59   5.0242      0.00     0.04       0.00    -0.04
    60   5.0242      0.00     0.09       0.00     0.05
    61   5.0243      0.00     0.14       0.00     0.03
    62   5.0625      0.00    -0.11       0.00     0.09
    63   7.0363      0.00    -0.06       0.00     0.01
    64   7.0364      0.00    -0.02       0.00    -0.02
    65   7.0366      0.00     0.06       0.00     0.05

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.

13RJ109    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        43.527    43.527    43.528
ecceobj         0.134     0.134     0.134
incobj         20.246    20.246    20.246
qmin           36.950    36.967    36.916
qmax           50.143    50.134    50.161
amean          43.388    43.388    43.388
amin           43.036    43.046    43.045
amax           43.769    43.773    43.777
emean           0.130     0.130     0.130
emin            0.116     0.117     0.117
emax            0.146     0.145     0.146
imean          20.335    20.335    20.335
imin           19.824    19.823    19.824
imax           20.828    20.832    20.825
excite_mean     0.371     0.371     0.371
fracstop        1.000     1.000     1.000
cjmean          2.926     2.926     2.926

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       179.3     179.4     179.4
kozaiamp        179.9     179.9     180.0