Orbit Fit and Astrometric record for 13SN106

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: 13SN106   
# Created Wed Jul 17 01:10:02 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     37 observations of     37
# Arc:  21.94y
# First observation: 2000/09/19
#  Last observation: 2022/08/27
# Chi-squared of fit:    14.83 DOF:     68 RMS:  0.11
# Min/Max residuals:    -0.38    0.32
# Exact a, adot, b, bdot, g, gdot:
  1.390315E-05  2.049498E-02 -1.307494E-06 -1.375619E-03  2.247565E-02 -6.299046E-04
# Covariance matrix:
  7.0223E-13 -7.5000E-14 -2.3536E-14  3.4990E-15 -1.3505E-13 -8.7058E-14
 -7.5000E-14  1.1619E-14  5.0321E-15 -7.1188E-16  4.3678E-14  1.7719E-14
 -2.3536E-14  5.0321E-15  4.1887E-13 -2.4679E-14  2.6330E-14  8.9304E-15
  3.4990E-15 -7.1188E-16 -2.4679E-14  1.5706E-15 -3.2741E-15 -1.2534E-15
 -1.3505E-13  4.3678E-14  2.6330E-14 -3.2741E-15  4.1271E-13  8.1594E-14
 -8.7058E-14  1.7719E-14  8.9304E-15 -1.2534E-15  8.1594E-14  3.1200E-14
#      lat0       lon0       xBary       yBary       zBary        JD0
    5.293558  -30.880956   -0.455226    0.081869   -0.885855  2451806.640883
# Heliocentric elements and errors
Epoch:              2451806.5000  =  2000/09/19
Mean Anomaly:          213.36842 +/-     0.005
Argument of Peri:      275.97812 +/-     0.001
Long of Asc Node:      202.89761 +/-     0.001
Inclination:             6.47154 +/-     0.000
Eccentricity:         0.04512273 +/-    0.0000
Semi-Major Axis:     43.71057825 +/-    0.0003
Time of Perihelion: 2494800.0472 +/-       1.7
Perihelion:          41.73823770 +/-    0.0005
Aphelion:            45.68291881 +/-    0.0005
Period (y)              288.9935 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           39.02519067 +/-    0.0004
Ecliptic Y          -22.79963491 +/-    0.0002
Ecliptic Z            4.10480247 +/-    0.0000
Ecliptic XDOT         0.00122165 +/-    0.0000
Ecliptic YDOT         0.00217903 +/-    0.0000
Ecliptic ZDOT        -0.00017378 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.38325303 +/-    0.0004
Geocenter to KBO     44.49264527 +/-    0.0005
# Hcoef:  6.87

The following table shows the complete astrometric record for 13SN106. 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 (13SN106) followed by the observatory code and reference code for the source of the astrometry.

2000 09  19.14014  21 57 33.63   -06 48 50.1   22.9R 13SN106   695  C~3clH      
2000 09  19.23656  21 57 33.26   -06 48 52.2         13SN106   695  C~3clH      
2013 09  08.15869  22 57 30.116  -02 13 45.60  23.2g 13SN106   W84  C~4yR3      
2013 09  11.24870  22 57 17.292  -02 15 10.19  24.0g 13SN106   W84  C~4yR3      
2013 09  29.20758  22 56 05.562  -02 23 23.26  23.9r 13SN106   W84  C~4yR3      
2013 09  29.20758  22 56 05.56   -02 23 23.2   24.3r 13SN106   W84  C~3clH      
2013 09  29.21040  22 56 05.550  -02 23 23.25  22.9i 13SN106   W84  C~4yR3      
2013 09  29.21040  22 56 05.55   -02 23 23.3   22.9i 13SN106   W84  C~3clH      
2013 10  12.07796  22 55 20.522  -02 28 56.13  23.2i 13SN106   W84  C~4yR3      
2013 10  12.07796  22 55 20.52   -02 28 56.1   23.3i 13SN106   W84  C~3clH      
2013 10  12.07934  22 55 20.531  -02 28 56.22  22.5z 13SN106   W84  C~4yR3      
2013 10  12.07934  22 55 20.53   -02 28 56.2   22.7z 13SN106   W84  C~3clH      
2015 11  01.04855  23 03 32.028  -01 53 17.72  22.9i 13SN106   W84  C~4yR3      
2015 11  01.04855  23 03 32.03   -01 53 17.7   23.1i 13SN106   W84  C~3clH      
2015 11  01.04992  23 03 32.028  -01 53 17.58  23.5r 13SN106   W84  C~4yR3      
2015 11  01.04992  23 03 32.03   -01 53 17.6   23.6r 13SN106   W84  C~3clH      
2015 11  01.05129  23 03 32.043  -01 53 17.78  24.5g 13SN106   W84  C~4yR3      
2016 09  29.12214  23 09 45.431  -01 18 44.75  23.8r 13SN106   W84  C~4yR3      
2016 09  29.12214  23 09 45.43   -01 18 44.7   23.7r 13SN106   W84  C~3clH      
2016 09  29.12352  23 09 45.420  -01 18 44.91  22.8i 13SN106   W84  C~4yR3      
2016 09  29.12352  23 09 45.42   -01 18 44.9   22.8i 13SN106   W84  C~3clH      
2016 09  30.12020  23 09 41.572  -01 19 12.27  22.6z 13SN106   W84  C~4yR3      
2016 09  30.12020  23 09 41.57   -01 19 12.3   22.7z 13SN106   W84  C~3clH      
2016 10  29.04759  23 08 08.933  -01 31 05.39  23.5r 13SN106   W84  C~4yR3      
2016 10  29.04759  23 08 08.93   -01 31 05.4   23.6r 13SN106   W84  C~3clH      
2016 10  29.04895  23 08 08.927  -01 31 05.39  23.0i 13SN106   W84  C~4yR3      
2016 10  29.04895  23 08 08.93   -01 31 05.4   23.0i 13SN106   W84  C~3clH      
2017 10  26.05120  23 12 49.670  -01 08 23.18  22.6z 13SN106   W84  C~4yR3      
2018 09  17.25775  23 19 44.618  -00 29 27.47  23.0r 13SN106   W84  C~4yR3      
2018 09  17.25914  23 19 44.603  -00 29 27.43  22.9i 13SN106   W84  C~4yR3      
2019 11  02.21365  23 21 39.66   -00 27 24.8   23.2i 13SN106   T09  C~7bIA      
2019 11  02.22767  23 21 39.63   -00 27 25.0   23.1i 13SN106   T09  C~7bIA      
2019 11  02.24174  23 21 39.58   -00 27 25.5   24.2i 13SN106   T09  C~7bIA      
2019 11  02.25586  23 21 39.56   -00 27 25.5   23.8i 13SN106   T09  C~7bIA      
2022 08  27.366240 23 39 37.012  +01 07 48.26  23.3G 13SN106   G37  C~5nHc      
2022 08  27.399210 23 39 36.883  +01 07 47.42        13SN106   G37  C~5nHc      
2022 08  27.433790 23 39 36.750  +01 07 46.56        13SN106   G37  C~5nHc      

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     0.08       0.00     0.10
     2   0.0003      0.00    -0.20       0.00     0.32
     3  12.9693      0.00    -0.38       0.00    -0.08
     4  12.9777      0.00     0.21       0.00    -0.00
     5  13.0269      0.00     0.04       0.00    -0.17
     6  13.0269      0.00     0.01       0.00    -0.11
     7  13.0269      0.00     0.02       0.00    -0.08
     8  13.0269      0.00     0.02       0.00    -0.13
     9  13.0621      0.00    -0.05       0.00    -0.03
    10  13.0621      0.00    -0.02       0.00    -0.06
    11  13.0621      0.00     0.17       0.00    -0.10
    12  13.0621      0.00     0.18       0.00    -0.12
    13  15.1154      0.00    -0.03       0.00    -0.06
    14  15.1154      0.00    -0.06       0.00    -0.08
    15  15.1154      0.00    -0.02       0.00     0.08
    16  15.1154      0.00     0.01       0.00     0.06
    17  15.1154      0.00     0.26       0.00    -0.09
    18  16.0273      0.00     0.10       0.00     0.03
    19  16.0273      0.00     0.11       0.00    -0.02
    20  16.0273      0.00     0.03       0.00    -0.13
    21  16.0273      0.00     0.03       0.00    -0.14
    22  16.0301      0.00    -0.02       0.00    -0.07
    23  16.0301      0.00     0.01       0.00    -0.04
    24  16.1093      0.00    -0.02       0.00     0.02
    25  16.1093      0.00     0.03       0.00     0.03
    26  16.1093      0.00     0.04       0.00     0.05
    27  16.1093      0.00    -0.01       0.00     0.06
    28  17.1004      0.00    -0.02       0.00    -0.04
    29  17.9935      0.00     0.08       0.00     0.02
    30  17.9935      0.00    -0.06       0.00     0.09
    31  19.1186      0.00    -0.07       0.00     0.03
    32  19.1187      0.00     0.00       0.00     0.12
    33  19.1187      0.00    -0.23       0.00    -0.09
    34  19.1187      0.00    -0.00       0.00     0.20
    35  21.9363      0.00    -0.06       0.00     0.18
    36  21.9364      0.00    -0.06       0.00     0.15
    37  21.9365      0.00    -0.02       0.00     0.14

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.

13SN106    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.808    43.808    43.808
ecceobj         0.043     0.043     0.043
incobj          6.470     6.470     6.470
qmin           39.893    39.931    39.912
qmax           47.853    47.876    47.819
amean          43.722    43.711    43.708
amin           43.332    43.331    43.334
amax           44.130    44.133    44.128
emean           0.062     0.058     0.059
emin            0.034     0.034     0.034
emax            0.085     0.085     0.085
imean           7.382     7.388     7.382
imin            6.656     6.657     6.661
imax            8.205     8.174     8.165
excite_mean     0.143     0.141     0.142
fracstop        1.000     1.000     1.000
cjmean          3.074     3.074     3.074

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       179.1     184.0     184.5
kozaiamp        180.0     180.0     180.0