Orbit Fit and Astrometric record for 612167

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: 612167    
# Created Wed Dec 25 02:07:38 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     80 observations of     80
# Arc:  20.95y
# First observation: 2000/07/29
#  Last observation: 2021/07/09
# Chi-squared of fit:   102.52 DOF:    154 RMS:  0.20
# Min/Max residuals:    -0.89    0.68
# Exact a, adot, b, bdot, g, gdot:
  1.611734E-05  2.499319E-02 -7.913551E-07 -1.444542E-03  2.493808E-02 -2.588138E-04
# Covariance matrix:
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
#      lat0       lon0       xBary       yBary       zBary        JD0
   -3.018173  -61.206721   -0.124707   -0.053232   -1.006222  2451754.574243
# Heliocentric elements and errors
Epoch:              2451754.5000  =  2000/07/29
Mean Anomaly:          348.26681 +/-     0.000
Argument of Peri:      234.63529 +/-     0.000
Long of Asc Node:       77.34754 +/-     0.000
Inclination:             4.42711 +/-     0.000
Eccentricity:         0.04794909 +/-    0.0000
Semi-Major Axis:     43.12514651 +/-    0.0000
Time of Perihelion: 2455125.8830 +/-       0.0
Perihelion:          41.05733479 +/-    0.0000
Aphelion:            45.19295823 +/-    0.0000
Period (y)              283.2071 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           19.88808336 +/-    0.0000
Ecliptic Y          -35.91132023 +/-    0.0000
Ecliptic Z           -2.11137218 +/-    0.0000
Ecliptic XDOT         0.00237985 +/-    0.0000
Ecliptic YDOT         0.00135938 +/-    0.0000
Ecliptic ZDOT        -0.00015673 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.10495355 +/-    0.0000
Geocenter to KBO     40.09936269 +/-    0.0000
# Hcoef:  6.76

The following table shows the complete astrometric record for 612167. 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 (612167) followed by the observatory code and reference code for the source of the astrometry.

2000 07  29.07350  20 06 22.73   -23 21 16.8   22.0R 612167    807  Cd1702      
2000 07  29.18080  20 06 22.17   -23 21 18.5         612167    807  Cd1702      
2000 09  20.11778  20 02 51.66   -23 29 58.7   23.2R 612167    695  Cd1702      
2000 09  20.20143  20 02 51.49   -23 29 59.2         612167    695  Cd1702      
2001 05  23.28180  20 17 09.99   -22 50 08.0   22.2R 612167    807  Cd7641      
2001 05  23.36202  20 17 09.82   -22 50 08.9         612167    807  Cd7641      
2001 06  12.28897  20 16 12.89   -22 54 37.5   21.5  612167    304  Ce6494      
2001 06  12.36625  20 16 12.61   -22 54 38.6         612167    304  Ce6494      
2001 08  19.08332  20 10 50.54   -23 12 46.9   21.1R 612167    807  Cd7641      
2001 08  19.15838  20 10 50.20   -23 12 47.9         612167    807  Cd7641      
2001 08  20.08816  20 10 46.00   -23 12 58.6         612167    807  Cd7641      
2002 06  06.53543  20 22 37.55   -22 38 17.9         612167    568  Cf8835      
2002 06  06.54045  20 22 37.52   -22 38 17.8         612167    568  Cf8835      
2002 06  06.55689  20 22 37.49   -22 38 18.1         612167    568  Cf8835      
2002 06  06.56615  20 22 37.45   -22 38 18.3         612167    568  Cf8835      
2002 06  06.57338  20 22 37.44   -22 38 18.3         612167    568  Cf8835      
2002 06  18.36185  20 21 56.16   -22 41 22.2   22.6R 612167    695  Cf8835      
2002 06  18.38773  20 21 56.06   -22 41 22.7         612167    695  Cf8835      
2004 07  17.32674  20 31 52.00   -22 18 20.3   22.8R 612167    688  Cl0684      
2004 07  17.40589  20 31 51.54   -22 18 22.2         612167    688  Cl0684      
2011 07  26.44851  21 13 13.260  -20 04 19.76  22.5G 612167    F51  C~2rXd      
2011 07  26.46230  21 13 13.185  -20 04 20.09  22.4G 612167    F51  C~2rXd      
2012 07  28.45799  21 18 53.501  -19 42 50.87  21.9G 612167    F51  C~2rXd      
2012 08  21.38425  21 16 56.528  -19 51 45.69  22.0G 612167    F51  C~2rXd      
2012 08  21.41224  21 16 56.418  -19 51 46.13  23.0G 612167    F51  C~2rXd      
2012 08  21.42607  21 16 56.350  -19 51 46.39  22.2G 612167    F51  C~2rXd      
2013 06  09.22552  21 27 39.96   -19 02 40.8   22.6R 612167    304  C~0snV      
2013 06  09.30361  21 27 39.79   -19 02 42.2         612167    304  C~0snV      
2013 06  09.37646  21 27 39.65   -19 02 43.2         612167    304  C~0snV      
2013 07  14.48789  21 25 49.103  -19 14 04.09  23.1G 612167    F51  C~2rXd      
2013 07  14.50394  21 25 49.028  -19 14 04.87  23.0G 612167    F51  C~2rXd      
2013 07  14.51939  21 25 48.990  -19 14 05.19  23.0G 612167    F51  C~2rXd      
2013 07  14.53483  21 25 48.920  -19 14 05.30  22.7G 612167    F51  C~2rXd      
2013 08  04.44795  21 24 12.365  -19 22 18.72  22.9G 612167    F51  C~2rXd      
2013 08  24.43628  21 22 35.004  -19 29 46.73  22.8G 612167    F51  C~2rXd      
2013 08  29.35240  21 22 11.912  -19 31 25.80  21.9G 612167    F51  C~2rXd      
2013 08  29.36624  21 22 11.838  -19 31 26.31  22.2G 612167    F51  C~2rXd      
2013 09  21.31822  21 20 37.462  -19 37 35.09  22.5G 612167    F51  C~2rXd      
2013 10  20.19789  21 19 30.414  -19 40 26.31  21.7G 612167    F51  C~2rXd      
2014 06  27.51447  21 32 40.325  -18 43 54.54  23.3G 612167    F51  C~2rXd      
2014 06  27.52621  21 32 40.284  -18 43 54.40  22.7G 612167    F51  C~2rXd      
2014 06  27.53791  21 32 40.249  -18 43 54.97  22.9G 612167    F51  C~2rXd      
2014 06  27.54956  21 32 40.197  -18 43 55.40  23.3G 612167    F51  C~2rXd      
2014 07  03.56601  21 32 20.212  -18 45 58.73  23.3G 612167    F51  C~2rXd      
2014 07  25.47580  21 30 50.098  -18 54 22.78  23.0G 612167    F51  C~2rXd      
2014 07  25.48705  21 30 50.047  -18 54 22.78  22.6G 612167    F51  C~2rXd      
2014 07  25.49831  21 30 49.990  -18 54 23.13  23.0G 612167    F51  C~2rXd      
2014 07  25.50955  21 30 49.951  -18 54 23.33  23.2G 612167    F51  C~2rXd      
2014 07  28.44743  21 30 36.325  -18 55 34.51  22.9G 612167    F51  C~2rXd      
2014 08  15.43958  21 29 09.481  -19 02 43.86  22.3G 612167    F51  C~2rXd      
2014 08  25.41034  21 28 21.266  -19 06 25.81  22.5G 612167    F51  C~2rXd      
2014 08  25.42091  21 28 21.209  -19 06 26.24  23.5G 612167    F51  C~2rXd      
2014 08  25.43149  21 28 21.142  -19 06 26.15  22.9G 612167    F51  C~2rXd      
2014 08  25.44208  21 28 21.110  -19 06 26.55  23.1G 612167    F51  C~2rXd      
2014 09  11.34890  21 27 05.259  -19 11 49.60  23.1G 612167    F51  C~2rXd      
2015 07  18.54018  21 37 08.548  -18 26 56.09  23.8G 612167    F51  C~2rXd      
2015 07  25.41778  21 36 38.455  -18 29 42.15  22.4G 612167    F51  C~2rXd      
2015 08  10.42173  21 35 22.979  -18 36 14.45  22.1G 612167    F51  C~2rXd      
2015 08  10.43273  21 35 22.921  -18 36 14.72  21.9G 612167    F51  C~2rXd      
2015 08  10.45478  21 35 22.820  -18 36 15.18  21.9G 612167    F51  C~2rXd      
2015 08  11.43580  21 35 18.057  -18 36 39.12  23.3G 612167    F51  C~2rXd      
2015 09  08.45744  21 33 06.020  -18 46 49.72  22.8G 612167    F51  C~2rXd      
2015 10  03.26966  21 31 35.400  -18 52 35.33  22.4G 612167    F51  C~2rXd      
2015 10  03.28064  21 31 35.376  -18 52 35.24  22.4G 612167    F51  C~2rXd      
2015 10  03.29162  21 31 35.348  -18 52 35.53  23.0G 612167    F51  C~2rXd      
2015 10  03.30259  21 31 35.324  -18 52 35.69  23.1G 612167    F51  C~2rXd      
2017 06  21.58999  21 50 01.741  -17 26 29.44  22.7G 612167    F51  C~2rXd      
2017 07  04.55110  21 49 25.511  -17 30 42.87  22.8G 612167    F51  C~2rXd      
2017 07  25.46621  21 48 04.606  -17 38 53.84  23.7G 612167    F51  C~2rXd      
2017 07  29.50604  21 47 46.611  -17 40 35.31  23.7G 612167    F51  C~2rXd      
2017 08  18.43248  21 46 12.402  -17 48 56.19  22.9G 612167    F51  C~2rXd      
2017 09  15.36004  21 44 04.727  -17 58 55.94  23.3G 612167    F51  C~2rXd      
2017 11  02.28185  21 42 09.205  -18 04 42.42  23.1G 612167    F51  C~2rXd      
2017 12  12.22194  21 43 14.186  -17 55 27.57  23.4G 612167    F51  C~2rXd      
2020 08  19.47951  22 03 11.214  -16 28 44.15  22.5w 612167    F51  C~43p4      
2020 08  19.48853  22 03 11.169  -16 28 44.36  22.6w 612167    F51  C~43p4      
2020 08  19.49758  22 03 11.118  -16 28 44.70  22.4w 612167    F51  C~43p4      
2021 07  09.343970 22 11 41.108  -15 43 06.81  22.8G 612167    G37  C~4unQ      
2021 07  09.390680 22 11 40.944  -15 43 06.92        612167    G37  C~4unQ      
2021 07  09.435650 22 11 40.780  -15 43 08.07        612167    G37  C~4unQ      

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    -0.05       0.00    -0.04
     2   0.0003      0.00    -0.07       0.00    -0.08
     3   0.1452      0.00    -0.12       0.00     0.21
     4   0.1455      0.00     0.08       0.00    -0.06
     5   0.8164      0.00     0.12       0.00    -0.09
     6   0.8167      0.00     0.09       0.00    -0.08
     7   0.8712      0.00     0.25       0.00    -0.22
     8   0.8714      0.00     0.35       0.00    -0.14
     9   1.0568      0.00    -0.16       0.00    -0.30
    10   1.0570      0.00    -0.06       0.00    -0.36
    11   1.0596      0.00    -0.26       0.00     0.36
    12   1.8548      0.00     0.22       0.00     0.22
    13   1.8548      0.00     0.00       0.00     0.40
    14   1.8548      0.00     0.33       0.00     0.34
    15   1.8549      0.00     0.17       0.00     0.27
    16   1.8549      0.00     0.36       0.00     0.37
    17   1.8872      0.00    -0.18       0.00    -0.03
    18   1.8872      0.00    -0.14       0.00    -0.10
    19   3.9678      0.00    -0.01       0.00    -0.03
    20   3.9681      0.00    -0.89       0.00    -0.42
    21  10.9908      0.00     0.10       0.00    -0.21
    22  10.9908      0.00    -0.02       0.00    -0.22
    23  11.9983      0.00     0.23       0.00     0.13
    24  12.0638      0.00    -0.34       0.00    -0.15
    25  12.0639      0.00     0.07       0.00    -0.01
    26  12.0639      0.00     0.06       0.00     0.02
    27  12.8628      0.00     0.10       0.00     0.31
    28  12.8631      0.00    -0.26       0.00     0.05
    29  12.8633      0.00    -0.28       0.00     0.10
    30  12.9594      0.00    -0.04       0.00     0.23
    31  12.9594      0.00    -0.13       0.00    -0.18
    32  12.9595      0.00     0.31       0.00    -0.15
    33  12.9595      0.00     0.26       0.00     0.10
    34  13.0168      0.00     0.05       0.00    -0.21
    35  13.0715      0.00     0.36       0.00    -0.07
    36  13.0850      0.00    -0.08       0.00     0.07
    37  13.0850      0.00    -0.21       0.00    -0.17
    38  13.1478      0.00    -0.42       0.00     0.00
    39  13.2269      0.00    -0.00       0.00    -0.08
    40  13.9122      0.00     0.03       0.00    -0.14
    41  13.9123      0.00    -0.02       0.00     0.23
    42  13.9123      0.00     0.02       0.00    -0.11
    43  13.9123      0.00    -0.20       0.00    -0.31
    44  13.9288      0.00     0.01       0.00    -0.05
    45  13.9888      0.00     0.01       0.00    -0.18
    46  13.9888      0.00     0.03       0.00     0.10
    47  13.9888      0.00    -0.03       0.00     0.02
    48  13.9889      0.00     0.17       0.00     0.09
    49  13.9969      0.00     0.02       0.00    -0.07
    50  14.0462      0.00     0.11       0.00    -0.02
    51  14.0735      0.00     0.10       0.00     0.06
    52  14.0735      0.00     0.02       0.00    -0.14
    53  14.0735      0.00    -0.22       0.00     0.17
    54  14.0736      0.00     0.07       0.00    -0.00
    55  14.1199      0.00     0.07       0.00     0.00
    56  14.9691      0.00     0.18       0.00    -0.06
    57  14.9879      0.00     0.24       0.00     0.08
    58  15.0318      0.00    -0.06       0.00     0.10
    59  15.0318      0.00    -0.11       0.00     0.10
    60  15.0318      0.00     0.01       0.00     0.18
    61  15.0345      0.00     0.01       0.00    -0.02
    62  15.1112      0.00     0.19       0.00    -0.04
    63  15.1792      0.00    -0.18       0.00     0.08
    64  15.1792      0.00    -0.07       0.00     0.26
    65  15.1792      0.00    -0.01       0.00     0.07
    66  15.1793      0.00     0.11       0.00     0.01
    67  16.8967      0.00    -0.25       0.00    -0.05
    68  16.9322      0.00    -0.15       0.00    -0.35
    69  16.9894      0.00    -0.04       0.00     0.10
    70  17.0005      0.00    -0.04       0.00     0.21
    71  17.0551      0.00    -0.03       0.00    -0.05
    72  17.1315      0.00     0.02       0.00    -0.18
    73  17.2627      0.00     0.68       0.00     0.14
    74  17.3721      0.00     0.27       0.00     0.07
    75  20.0586      0.00     0.01       0.00     0.11
    76  20.0586      0.00    -0.00       0.00     0.13
    77  20.0587      0.00    -0.11       0.00     0.02
    78  20.9453      0.00     0.17       0.00    -0.63
    79  20.9454      0.00    -0.05       0.00     0.30
    80  20.9456      0.00    -0.35       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.

612167    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.208    43.208    43.208
ecceobj         0.050     0.050     0.050
incobj          4.426     4.426     4.426
qmin           40.425    40.426    40.424
qmax           46.302    46.302    46.302
amean          43.252    43.252    43.252
amin           42.921    42.918    42.922
amax           43.602    43.603    43.602
emean           0.044     0.044     0.044
emin            0.023     0.024     0.023
emax            0.062     0.062     0.062
imean           2.476     2.476     2.476
imin            1.597     1.597     1.598
imax            3.279     3.279     3.280
excite_mean     0.063     0.063     0.063
fracstop        1.000     1.000     1.000
cjmean          3.088     3.088     3.088

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       180.2     180.1     180.2
kozaiamp        180.0     180.0     180.0