Orbit Fit and Astrometric record for 13SF112

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: 13SF112   
# Created Tue Apr  1 01:09:43 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     37 observations of     37
# Arc:   8.91y
# First observation: 2013/09/29
#  Last observation: 2022/08/27
# Chi-squared of fit:    19.47 DOF:     68 RMS:  0.13
# Min/Max residuals:    -0.38    0.28
# Exact a, adot, b, bdot, g, gdot:
  1.522488E-05  2.183564E-02  1.053344E-06 -5.101774E-05  2.316109E-02  6.512211E-05
# Covariance matrix:
  1.9361E-13 -8.2943E-14 -5.8383E-16  1.6698E-16 -4.9625E-14 -3.0780E-13
 -8.2943E-14  5.4438E-14  1.0480E-16 -1.1323E-16  7.3715E-15  2.3275E-13
 -5.8383E-16  1.0480E-16  1.0086E-13 -2.2039E-14  1.3922E-15  6.2341E-16
  1.6698E-16 -1.1323E-16 -2.2039E-14  7.9507E-15 -7.5360E-17 -5.7104E-16
 -4.9625E-14  7.3715E-15  1.3922E-15 -7.5360E-17  1.2429E-13  4.5744E-14
 -3.0780E-13  2.3275E-13  6.2341E-16 -5.7104E-16  4.5744E-14  1.1659E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
    3.837669  -10.989188   -0.290795    0.064276   -0.956654  2456564.703928
# Heliocentric elements and errors
Epoch:              2456564.5000  =  2013/09/29
Mean Anomaly:          137.68585 +/-     0.287
Argument of Peri:      313.70977 +/-     0.284
Long of Asc Node:      257.14535 +/-     0.004
Inclination:             3.75726 +/-     0.000
Eccentricity:         0.01108686 +/-    0.0000
Semi-Major Axis:     43.77142001 +/-    0.0027
Time of Perihelion: 2416109.5956 +/-      84.3
Perihelion:          43.28613236 +/-    0.0032
Aphelion:            44.25670766 +/-    0.0032
Period (y)              289.5971 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           43.28549579 +/-    0.0006
Ecliptic Y           -8.10610743 +/-    0.0001
Ecliptic Z            2.88977802 +/-    0.0000
Ecliptic XDOT         0.00049380 +/-    0.0000
Ecliptic YDOT         0.00253098 +/-    0.0000
Ecliptic ZDOT        -0.00000536 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.13268087 +/-    0.0006
Geocenter to KBO     43.17590629 +/-    0.0007
# Hcoef:  7.34

The following table shows the complete astrometric record for 13SF112. 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 (13SF112) followed by the observatory code and reference code for the source of the astrometry.

2013 09  29.20315  23 13 35.054  -00 48 59.12  23.4r 13SF112   W84  C~52RU      
2013 09  30.10989  23 13 31.448  -00 49 23.72  23.5r 13SF112   W84  C~52RU      
2013 09  30.11437  23 13 31.437  -00 49 23.84  22.7i 13SF112   W84  C~52RU      
2013 10  11.10657  23 12 49.984  -00 54 14.39  23.3z 13SF112   W84  C~52RU      
2013 10  12.08494  23 12 46.552  -00 54 39.33  23.3i 13SF112   W84  C~52RU      
2013 10  12.08781  23 12 46.558  -00 54 39.43  23.0z 13SF112   W84  C~52RU      
2013 10  28.02795  23 11 57.589  -01 00 50.37  23.7r 13SF112   W84  C~52RU      
2015 07  20.57390  23 27 09.03   +00 35 10.8   23.8i 13SF112   T09  C~8cPT      
2015 07  20.58838  23 27 09.00   +00 35 10.8   23.8i 13SF112   T09  C~8cPT      
2015 07  20.60288  23 27 08.96   +00 35 10.4   23.8i 13SF112   T09  C~8cPT      
2015 07  22.54647  23 27 04.60   +00 34 51.3   23.8z 13SF112   T09  C~8cPT      
2015 07  22.56103  23 27 04.58   +00 34 51.3   23.7z 13SF112   T09  C~8cPT      
2015 07  22.57560  23 27 04.53   +00 34 51.1   24.0z 13SF112   T09  C~8cPT      
2015 07  22.59009  23 27 04.51   +00 34 50.9   23.9z 13SF112   T09  C~8cPT      
2015 07  22.60458  23 27 04.46   +00 34 50.9   23.7z 13SF112   T09  C~8cPT      
2016 08  01.47069  23 31 10.64   +01 01 28.6   24.3z 13SF112   T09  C~85Dw      
2016 08  01.49230  23 31 10.56   +01 01 28.3   23.6z 13SF112   T09  C~85Dw      
2016 08  01.49500  23 31 10.59   +01 01 28.1   23.6z 13SF112   T09  C~85Dw      
2016 08  01.55200  23 31 10.41   +01 01 27.3   23.4z 13SF112   T09  C~85Dw      
2016 08  01.57640  23 31 10.33   +01 01 26.9   23.6z 13SF112   T09  C~85Dw      
2016 09  07.37372  23 28 53.87   +00 48 14.5   24.4r 13SF112   T09  C~7bIA      
2016 09  07.44502  23 28 53.57   +00 48 12.3   23.9r 13SF112   T09  C~7bIA      
2016 09  07.44719  23 28 53.56   +00 48 12.3   24.0r 13SF112   T09  C~7bIA      
2016 09  07.47817  23 28 53.41   +00 48 11.6   24.1r 13SF112   T09  C~7bIB      
2016 09  07.48918  23 28 53.37   +00 48 11.3   24.7r 13SF112   T09  C~7bIB      
2016 09  26.14177  23 27 34.581  +00 39 37.95  23.5i 13SF112   W84  C~52RU      
2016 09  26.14314  23 27 34.577  +00 39 37.91  23.8r 13SF112   W84  C~52RU      
2016 09  30.12844  23 27 18.237  +00 37 46.77  22.9z 13SF112   W84  C~52RU      
2016 10  05.11964  23 26 58.341  +00 35 29.21  23.3i 13SF112   W84  C~52RU      
2016 10  05.12101  23 26 58.334  +00 35 29.07  23.6r 13SF112   W84  C~52RU      
2017 11  09.04336  23 29 44.911  +00 50 43.09  23.6r 13SF112   W84  C~52RU      
2017 11  15.05477  23 29 33.609  +00 48 59.86  23.7g 13SF112   W84  C~52RU      
2017 11  15.05615  23 29 33.632  +00 49 00.18  23.9r 13SF112   W84  C~52RU      
2017 11  15.05752  23 29 33.621  +00 48 59.94  23.4i 13SF112   W84  C~52RU      
2022 08  27.388110 23 57 19.861  +03 46 42.29  23.3G 13SF112   G37  C~5nHc      
2022 08  27.421980 23 57 19.725  +03 46 41.61        13SF112   G37  C~5nHc      
2022 08  27.457270 23 57 19.600  +03 46 40.67        13SF112   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     0.03       0.00    -0.23
     2   0.0025      0.00    -0.07       0.00    -0.16
     3   0.0025      0.00     0.04       0.00    -0.15
     4   0.0326      0.00    -0.17       0.00     0.10
     5   0.0353      0.00     0.02       0.00     0.04
     6   0.0353      0.00     0.26       0.00     0.01
     7   0.0789      0.00     0.10       0.00    -0.15
     8   1.8053      0.00    -0.03       0.00     0.06
     9   1.8053      0.00     0.01       0.00     0.20
    10   1.8053      0.00    -0.10       0.00    -0.07
    11   1.8107      0.00    -0.14       0.00    -0.02
    12   1.8107      0.00     0.08       0.00     0.13
    13   1.8107      0.00    -0.15       0.00     0.08
    14   1.8108      0.00     0.07       0.00     0.03
    15   1.8108      0.00    -0.16       0.00     0.18
    16   2.8399      0.00    -0.14       0.00     0.10
    17   2.8399      0.00    -0.38       0.00     0.12
    18   2.8400      0.00     0.19       0.00    -0.04
    19   2.8401      0.00     0.04       0.00     0.01
    20   2.8402      0.00    -0.07       0.00    -0.03
    21   2.9409      0.00     0.18       0.00     0.18
    22   2.9411      0.00     0.28       0.00    -0.13
    23   2.9411      0.00     0.27       0.00    -0.07
    24   2.9412      0.00     0.02       0.00     0.06
    25   2.9412      0.00     0.13       0.00     0.05
    26   2.9923      0.00    -0.01       0.00     0.02
    27   2.9923      0.00     0.02       0.00     0.01
    28   3.0032      0.00     0.03       0.00    -0.04
    29   3.0169      0.00     0.08       0.00     0.10
    30   3.0169      0.00     0.05       0.00    -0.00
    31   4.1118      0.00     0.07       0.00     0.05
    32   4.1283      0.00    -0.35       0.00    -0.22
    33   4.1283      0.00     0.03       0.00     0.12
    34   4.1283      0.00    -0.10       0.00    -0.10
    35   8.9095      0.00     0.03       0.00    -0.04
    36   8.9096      0.00    -0.07       0.00     0.03
    37   8.9097      0.00     0.08       0.00    -0.13

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.

13SF112    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.005    44.005    44.005
ecceobj         0.008     0.008     0.008
incobj          3.760     3.760     3.760
qmin           42.684    42.677    42.690
qmax           45.221    45.222    45.219
amean          43.861    43.861    43.861
amin           43.531    43.532    43.531
amax           44.195    44.196    44.195
emean           0.010     0.010     0.010
emin            0.000     0.000     0.000
emax            0.023     0.023     0.023
imean           5.502     5.502     5.502
imin            4.879     4.879     4.879
imax            6.061     6.061     6.061
excite_mean     0.097     0.097     0.097
fracstop        1.000     1.000     1.000
cjmean          3.089     3.089     3.089

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       181.0     181.1     181.0
kozaiamp        180.0     179.9     179.9