Orbit Fit and Astrometric record for 613619

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: 613619    
# Created Fri Mar 29 01:09:32 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting    110 observations of    110
# Arc:  12.08y
# First observation: 2005/12/06
#  Last observation: 2018/01/03
# Chi-squared of fit:   165.29 DOF:    214 RMS:  0.22
# Min/Max residuals:    -0.91    1.11
# Exact a, adot, b, bdot, g, gdot:
  1.775872E-05  5.586535E-02  1.409915E-05  3.777191E-02  4.504109E-02 -1.983713E-02
# 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
  -16.023897   15.779683   -0.839489   -0.143903   -0.501485  2453710.719936
# Heliocentric elements and errors
Epoch:              2453710.5000  =  2005/12/06
Mean Anomaly:          343.20278 +/-     0.000
Argument of Peri:       21.03811 +/-     0.000
Long of Asc Node:       39.42840 +/-     0.000
Inclination:            37.45743 +/-     0.000
Eccentricity:         0.45902859 +/-    0.0000
Semi-Major Axis:     37.72568849 +/-    0.0000
Time of Perihelion: 2457659.5173 +/-       0.0
Perihelion:          20.40851902 +/-    0.0000
Aphelion:            55.04285797 +/-    0.0000
Period (y)              231.7202 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           20.80494788 +/-    0.0000
Ecliptic Y            6.75108829 +/-    0.0000
Ecliptic Z           -6.12828595 +/-    0.0000
Ecliptic XDOT        -0.00142637 +/-    0.0000
Ecliptic YDOT         0.00311867 +/-    0.0000
Ecliptic ZDOT         0.00253964 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   22.71530551 +/-    0.0000
Geocenter to KBO     22.20214032 +/-    0.0000
# Hcoef:  8.76

The following table shows the complete astrometric record for 613619. 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 (613619) followed by the observatory code and reference code for the source of the astrometry.

2005 12  06.219193 01 22 49.39   -08 35 09.2         613619    645  C~1SLC      
2005 12  06.220022 01 22 49.38   -08 35 09.2         613619    645  C~1SLC      
2005 12  06.222510 01 22 49.37   -08 35 09.1         613619    645  C~1SLC      
2006 10  22.90898  01 37 02.70   -05 18 30.6   21.4R 613619    950  Cs4401      
2006 10  22.91478  01 37 02.66   -05 18 30.7   21.1R 613619    950  Cs4401      
2006 10  22.91990  01 37 02.61   -05 18 30.8   21.2R 613619    950  Cs4401      
2006 10  22.98699  01 37 02.00   -05 18 32.2   21.3R 613619    950  Cs4401      
2006 10  23.03509  01 37 01.56   -05 18 33.2   21.2R 613619    950  Cs4401      
2006 10  23.06363  01 37 01.30   -05 18 33.8   21.3R 613619    950  Cs4401      
2006 10  23.09828  01 37 00.99   -05 18 34.5   21.2R 613619    950  Cs4401      
2006 10  23.14178  01 37 00.60   -05 18 35.4   20.9R 613619    950  Cs4401      
2006 10  23.95247  01 36 53.42   -05 18 52.2   21.4R 613619    950  Cs4401      
2006 10  24.01036  01 36 52.90   -05 18 53.5   21.6R 613619    950  Cs4401      
2006 10  24.08181  01 36 52.25   -05 18 54.9   21.5R 613619    950  Cs4401      
2006 10  24.14089  01 36 51.72   -05 18 56.0   21.2R 613619    950  Cs4401      
2006 10  27.09845  01 36 25.56   -05 19 51.6   21.9R 613619    950  Ct2368      
2006 11  13.99403  01 33 55.25   -05 22 27.3   22.7V 613619    493  Ct2368      
2006 11  14.87927  01 33 48.35   -05 22 26.1   22.5V 613619    493  Ct2368      
2006 11  14.96109  01 33 47.72   -05 22 26.0   22.7V 613619    493  Ct2368      
2006 11  18.92789  01 33 17.76   -05 22 09.3   22.4V 613619    620  Ct2368      
2006 12  16.87218  01 30 40.35   -05 11 13.3   22.0V 613619    J86  Ct2368      
2006 12  16.88631  01 30 40.32   -05 11 12.8   22.0V 613619    J86  Ct2368      
2006 12  17.85983  01 30 36.88   -05 10 32.9   22.1V 613619    J86  Ct2368      
2006 12  17.87396  01 30 36.81   -05 10 32.2   22.1V 613619    J86  Ct2368      
2007 10  11.37897  01 47 51.75   -01 43 58.4   21.1R 613619    688  C~02IB      
2007 10  11.44061  01 47 51.15   -01 43 59.6         613619    688  C~02IB      
2008 09  06.427928 02 01 28.38   +02 08 27.8         613619    645  C~1rRG      
2008 09  06.428762 02 01 28.38   +02 08 27.8         613619    645  C~1rRG      
2008 09  06.431250 02 01 28.36   +02 08 27.8         613619    645  C~1rRG      
2008 10  03.302556 01 58 16.70   +01 56 00.4   22.0V 613619    645  C~1SLC      
2008 10  03.303385 01 58 16.70   +01 56 00.3   21.7V 613619    645  C~1SLC      
2008 10  03.305873 01 58 16.68   +01 56 00.3   22.8V 613619    645  C~1SLC      
2008 10  23.38105  01 55 17.21   +01 47 08.4   21.0r 613619    695  C~02IB      
2008 10  23.43177  01 55 16.75   +01 47 07.2   21.2r 613619    695  C~02IB      
2008 10  24.33484  01 55 08.45   +01 46 46.8   21.3r 613619    695  C~02IB      
2008 10  24.43488  01 55 07.54   +01 46 44.7   21.1r 613619    695  C~02IB      
2008 12  01.14601  01 49 53.54   +01 41 24.0   21.6R 613619    688  C~02Mi      
2008 12  01.19151  01 49 53.23   +01 41 24.7         613619    688  C~02Mi      
2010 09  17.35962  02 20 08.40   +09 30 30.7   22.2R 613619    688  C~0NHX      
2010 09  17.40992  02 20 08.06   +09 30 31.1         613619    688  C~0NHX      
2010 10  07.44460  02 17 34.136  +09 24 42.40  21.8G 613619    F51  C~2kJo      
2010 10  08.55990  02 17 24.360  +09 24 19.63  21.8G 613619    F51  C~2kJo      
2010 10  08.58452  02 17 24.132  +09 24 19.30  22.2G 613619    F51  C~2kJo      
2010 10  15.34667  02 16 23.198  +09 21 56.23  22.4G 613619    F51  C~2kJo      
2010 10  15.35730  02 16 23.102  +09 21 55.97  22.1G 613619    F51  C~2kJo      
2010 11  02.43304  02 13 31.458  +09 15 37.31  22.0w 613619    F51  C~1vVe      
2010 11  02.44830  02 13 31.318  +09 15 36.87  22.2w 613619    F51  C~1vVe      
2010 11  02.46357  02 13 31.160  +09 15 36.71  22.0w 613619    F51  C~1vVe      
2010 11  02.47617  02 13 31.048  +09 15 36.49  22.0w 613619    F51  C~1vVe      
2010 12  04.40181  02 08 53.707  +09 09 14.24  22.4G 613619    F51  C~2kJo      
2011 01  30.26505  02 06 28.115  +09 32 18.83  22.5w 613619    F51  C~1vVe      
2011 01  30.26903  02 06 28.132  +09 32 19.02  22.4w 613619    F51  C~1vVe      
2011 01  30.27366  02 06 28.138  +09 32 19.26  22.5w 613619    F51  C~1vVe      
2011 01  30.27764  02 06 28.151  +09 32 19.49  22.5w 613619    F51  C~1vVe      
2011 09  07.63623  02 31 36.269  +13 19 57.45  21.6G 613619    F51  C~2kJo      
2011 11  14.31452  02 22 10.667  +13 05 21.65  21.8G 613619    F51  C~2kJo      
2011 11  14.32680  02 22 10.521  +13 05 21.60  21.9G 613619    F51  C~2kJo      
2011 11  24.29910  02 20 38.860  +13 02 49.53  21.9G 613619    F51  C~2kJo      
2011 11  24.31032  02 20 38.772  +13 02 49.59  22.1G 613619    F51  C~2kJo      
2011 12  02.26196  02 19 31.775  +13 01 19.47  22.3G 613619    F51  C~2kJo      
2012 10  19.52097  02 37 23.639  +17 08 41.36  21.9w 613619    F51  C~1vVe      
2012 10  19.53522  02 37 23.497  +17 08 41.19  21.7w 613619    F51  C~1vVe      
2012 10  19.54946  02 37 23.343  +17 08 40.92  22.0w 613619    F51  C~1vVe      
2012 10  19.56373  02 37 23.225  +17 08 40.79  21.7G 613619    F51  C~2kJo      
2012 11  02.32951  02 35 06.038  +17 05 07.74  21.9G 613619    F51  C~2kJo      
2012 11  02.34169  02 35 05.886  +17 05 07.76  22.2G 613619    F51  C~2kJo      
2012 11  17.06461  02 32 38.55   +17 00 47.9         613619    I17  C~0li5      
2012 11  17.09459  02 32 38.26   +17 00 47.9         613619    I17  C~0li5      
2012 11  17.12540  02 32 37.94   +17 00 47.9         613619    I17  C~0li5      
2013 10  25.52368  02 48 15.250  +21 04 37.03  22.6G 613619    F51  C~2kJo      
2013 10  25.53626  02 48 15.125  +21 04 36.95  22.2G 613619    F51  C~2kJo      
2013 10  30.48254  02 47 24.384  +21 03 40.12  21.6G 613619    F51  C~2kJo      
2013 10  30.49689  02 47 24.232  +21 03 40.07  21.9G 613619    F51  C~2kJo      
2014 10  25.57617  03 00 52.146  +25 01 17.93  22.2w 613619    F51  C~1vVe      
2014 10  25.58808  03 00 52.007  +25 01 18.00  22.1w 613619    F51  C~1vVe      
2014 10  25.59996  03 00 51.906  +25 01 18.27  21.8w 613619    F51  C~1vVe      
2014 10  25.61182  03 00 51.744  +25 01 17.88  21.8w 613619    F51  C~1vVe      
2014 10  28.53554  03 00 21.367  +25 01 03.56  22.8G 613619    F51  C~2kJo      
2014 10  28.54756  03 00 21.254  +25 01 03.67  22.8G 613619    F51  C~2kJo      
2014 11  17.30594  02 56 49.184  +24 57 16.70  21.9w 613619    F51  C~1vVe      
2014 11  17.31785  02 56 49.053  +24 57 16.40  22.1w 613619    F51  C~1vVe      
2014 11  17.32984  02 56 48.927  +24 57 16.28  22.1w 613619    F51  C~1vVe      
2014 11  19.26303  02 56 28.333  +24 56 44.09  21.6G 613619    F51  C~2kJo      
2014 11  19.27580  02 56 28.193  +24 56 44.09  22.0w 613619    F51  C~1vVe      
2014 11  19.28906  02 56 28.042  +24 56 43.67  21.8w 613619    F51  C~1vVe      
2014 11  19.30100  02 56 27.925  +24 56 43.83  21.9w 613619    F51  C~1vVe      
2014 11  27.40795  02 55 03.633  +24 54 17.12  22.0w 613619    F51  C~1vVe      
2014 11  27.42021  02 55 03.492  +24 54 16.84  21.9w 613619    F51  C~1vVe      
2014 11  27.43247  02 55 03.364  +24 54 16.27  21.6G 613619    F51  C~2kJo      
2014 11  27.44474  02 55 03.251  +24 54 16.31  21.8w 613619    F51  C~1vVe      
2014 12  27.32662  02 50 52.784  +24 44 59.46  21.3G 613619    F51  C~2kJo      
2015 01  12.28949  02 49 39.158  +24 41 59.29  21.3G 613619    F51  C~2kJo      
2015 01  12.30219  02 49 39.120  +24 41 59.14  22.1G 613619    F51  C~2kJo      
2015 01  12.31474  02 49 39.076  +24 41 58.96  22.1G 613619    F51  C~2kJo      
2015 01  12.32734  02 49 39.047  +24 41 58.88  22.3G 613619    F51  C~2kJo      
2015 12  28.24731  03 03 43.187  +28 39 27.43  22.4G 613619    F51  C~2kJo      
2015 12  30.40522  03 03 28.948  +28 38 41.07  22.1G 613619    F51  C~2kJo      
2016 01  02.24601  03 03 11.573  +28 37 42.10  22.2G 613619    F51  C~2kJo      
2016 01  05.38858  03 02 54.102  +28 36 39.87  22.0G 613619    F51  C~2kJo      
2016 01  15.39049  03 02 12.068  +28 33 49.45  22.6G 613619    F51  C~2kJo      
2016 01  26.35610  03 01 50.821  +28 31 47.33  21.9G 613619    F51  C~2kJo      
2016 11  28.48531  03 22 22.796  +32 42 05.93  21.4G 613619    F51  C~2kJo      
2016 11  28.48595  03 22 22.806  +32 42 05.73  21.8G 613619    F51  C~2kJo      
2016 11  28.49711  03 22 22.632  +32 42 05.84  21.6G 613619    F51  C~2kJo      
2016 11  28.50905  03 22 22.490  +32 42 05.49  21.9G 613619    F51  C~2kJo      
2016 11  28.50969  03 22 22.489  +32 42 05.40  22.2G 613619    F51  C~2kJo      
2016 11  28.52085  03 22 22.369  +32 42 05.38  22.3G 613619    F51  C~2kJo      
2016 11  28.52149  03 22 22.366  +32 42 05.36  22.1G 613619    F51  C~2kJo      
2018 01  03.28612  03 31 57.034  +36 12 42.54  22.5G 613619    F51  C~2kJo      
2018 01  03.30889  03 31 56.870  +36 12 41.97  22.4G 613619    F51  C~2kJo      

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     0.42       0.00    -0.01
     2   0.0000      0.00     0.34       0.00    -0.04
     3   0.0000      0.00     0.37       0.00    -0.03
     4   0.8780      0.00    -0.08       0.00    -0.03
     5   0.8780      0.00     0.11       0.00    -0.01
     6   0.8780      0.00     0.05       0.00     0.00
     7   0.8782      0.00    -0.02       0.00     0.03
     8   0.8783      0.00    -0.09       0.00     0.04
     9   0.8784      0.00    -0.12       0.00     0.04
    10   0.8785      0.00    -0.08       0.00     0.07
    11   0.8786      0.00    -0.04       0.00     0.08
    12   0.8809      0.00    -0.08       0.00     0.02
    13   0.8810      0.00    -0.05       0.00    -0.10
    14   0.8812      0.00    -0.12       0.00    -0.06
    15   0.8814      0.00    -0.09       0.00     0.03
    16   0.8895      0.00     0.00       0.00     0.18
    17   0.9385      0.00     0.19       0.00    -0.20
    18   0.9409      0.00    -0.25       0.00    -0.17
    19   0.9411      0.00    -0.04       0.00    -0.23
    20   0.9520      0.00    -0.16       0.00    -0.24
    21   1.0285      0.00    -0.38       0.00     0.05
    22   1.0285      0.00    -0.03       0.00    -0.02
    23   1.0312      0.00     0.12       0.00    -0.09
    24   1.0312      0.00    -0.16       0.00     0.02
    25   1.8457      0.00     0.14       0.00     0.38
    26   1.8459      0.00    -0.58       0.00     0.97
    27   2.7521      0.00     0.13       0.00    -0.07
    28   2.7521      0.00     0.20       0.00    -0.05
    29   2.7521      0.00     0.11       0.00     0.01
    30   2.8257      0.00     0.28       0.00    -0.38
    31   2.8257      0.00     0.38       0.00    -0.46
    32   2.8257      0.00     0.40       0.00    -0.39
    33   2.8807      0.00    -0.40       0.00     0.25
    34   2.8808      0.00    -0.21       0.00     0.21
    35   2.8833      0.00    -0.25       0.00     0.21
    36   2.8835      0.00     0.10       0.00     0.35
    37   2.9868      0.00    -0.03       0.00    -0.12
    38   2.9869      0.00    -0.04       0.00     0.19
    39   4.7807      0.00    -0.22       0.00     0.05
    40   4.7808      0.00    -0.31       0.00     1.11
    41   4.8357      0.00     0.04       0.00    -0.32
    42   4.8387      0.00    -0.04       0.00    -0.14
    43   4.8388      0.00    -0.17       0.00     0.05
    44   4.8573      0.00     0.07       0.00    -0.08
    45   4.8573      0.00     0.12       0.00    -0.11
    46   4.9068      0.00     0.02       0.00    -0.03
    47   4.9069      0.00     0.14       0.00    -0.17
    48   4.9069      0.00     0.00       0.00    -0.03
    49   4.9069      0.00     0.16       0.00    -0.01
    50   4.9943      0.00    -0.00       0.00    -0.08
    51   5.1500      0.00    -0.12       0.00    -0.04
    52   5.1500      0.00    -0.01       0.00    -0.06
    53   5.1500      0.00    -0.10       0.00    -0.05
    54   5.1501      0.00    -0.05       0.00    -0.03
    55   5.7534      0.00    -0.18       0.00    -0.07
    56   5.9387      0.00     0.07       0.00    -0.18
    57   5.9387      0.00    -0.34       0.00    -0.02
    58   5.9660      0.00     0.02       0.00    -0.06
    59   5.9660      0.00     0.22       0.00     0.15
    60   5.9878      0.00     0.03       0.00    -0.14
    61   6.8701      0.00     0.02       0.00    -0.00
    62   6.8701      0.00    -0.00       0.00     0.02
    63   6.8702      0.00    -0.21       0.00    -0.06
    64   6.8702      0.00     0.13       0.00     0.01
    65   6.9079      0.00     0.15       0.00    -0.16
    66   6.9079      0.00    -0.25       0.00     0.07
    67   6.9482      0.00     0.52       0.00    -0.91
    68   6.9483      0.00     0.61       0.00    -0.40
    69   6.9484      0.00     0.38       0.00     0.13
    70   7.8858      0.00    -0.09       0.00    -0.11
    71   7.8859      0.00    -0.02       0.00    -0.05
    72   7.8994      0.00    -0.05       0.00    -0.15
    73   7.8995      0.00    -0.06       0.00    -0.01
    74   8.8853      0.00    -0.00       0.00     0.02
    75   8.8853      0.00    -0.22       0.00     0.14
    76   8.8854      0.00     0.13       0.00     0.47
    77   8.8854      0.00    -0.44       0.00     0.13
    78   8.8934      0.00     0.27       0.00    -0.20
    79   8.8934      0.00     0.50       0.00    -0.02
    80   8.9475      0.00    -0.11       0.00     0.15
    81   8.9476      0.00    -0.14       0.00     0.04
    82   8.9476      0.00    -0.07       0.00     0.11
    83   8.9529      0.00    -0.07       0.00     0.01
    84   8.9529      0.00    -0.11       0.00     0.21
    85   8.9530      0.00    -0.23       0.00     0.01
    86   8.9530      0.00    -0.05       0.00     0.36
    87   8.9752      0.00     0.21       0.00     0.17
    88   8.9752      0.00    -0.01       0.00     0.12
    89   8.9753      0.00    -0.03       0.00    -0.21
    90   8.9753      0.00     0.17       0.00     0.07
    91   9.0571      0.00     0.14       0.00    -0.02
    92   9.1008      0.00    -0.05       0.00     0.11
    93   9.1008      0.00    -0.01       0.00     0.04
    94   9.1009      0.00    -0.07       0.00    -0.05
    95   9.1009      0.00     0.10       0.00    -0.04
    96  10.0589      0.00    -0.32       0.00     0.13
    97  10.0648      0.00    -0.07       0.00     0.05
    98  10.0726      0.00    -0.05       0.00     0.01
    99  10.0812      0.00    -0.13       0.00     0.10
   100  10.1086      0.00    -0.01       0.00     0.12
   101  10.1386      0.00     0.05       0.00    -0.05
   102  10.9795      0.00     0.28       0.00    -0.07
   103  10.9795      0.00     0.54       0.00    -0.26
   104  10.9795      0.00    -0.16       0.00     0.05
   105  10.9796      0.00    -0.24       0.00    -0.08
   106  10.9796      0.00    -0.14       0.00    -0.16
   107  10.9796      0.00    -0.03       0.00     0.02
   108  10.9796      0.00     0.04       0.00     0.01
   109  12.0768      0.00    -0.13       0.00    -0.11
   110  12.0769      0.00    -0.01       0.00     0.03

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.

613619    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        38.252    38.252    38.252
ecceobj         0.465     0.465     0.465
incobj         37.348    37.348    37.348
qmin           20.243    20.222    19.133
qmax           57.719    56.731    62.050
amean          38.448    37.912    38.477
amin           37.708    36.517    37.773
amax           39.344    38.626    40.751
emean           0.396     0.380     0.364
emin            0.274     0.226     0.243
emax            0.474     0.470     0.523
imean          39.057    39.295    39.837
imin           36.669    36.716    34.537
imax           42.284    42.873    42.734
excite_mean     0.746     0.742     0.741
fracstop        0.107     0.111     0.380
cjmean          2.384     2.389     2.388

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        43.3      41.8      91.6
kozaiamp         15.9      15.2      67.7