Orbit Fit and Astrometric record for 532039

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: 532039    
# Created Sat Apr 20 01:08:42 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     64 observations of     64
# Arc:  11.31y
# First observation: 2011/01/29
#  Last observation: 2022/05/23
# Chi-squared of fit:    67.56 DOF:    122 RMS:  0.18
# Min/Max residuals:    -0.70    0.78
# Exact a, adot, b, bdot, g, gdot:
  1.947306E-05  3.644789E-02 -7.021577E-07 -1.666672E-03  3.031349E-02  3.038775E-03
# 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
    1.553075 -167.337326    0.882872    0.012008   -0.443408  2455591.100416
# Heliocentric elements and errors
Epoch:              2455590.5000  =  2011/01/29
Mean Anomaly:           10.28822 +/-     0.000
Argument of Peri:      132.14364 +/-     0.000
Long of Asc Node:       41.87663 +/-     0.000
Inclination:             2.99675 +/-     0.000
Eccentricity:         0.23758032 +/-    0.0000
Semi-Major Axis:     43.48782756 +/-    0.0000
Time of Perihelion: 2452596.9414 +/-       0.0
Perihelion:          33.15597538 +/-    0.0000
Aphelion:            53.81967975 +/-    0.0000
Period (y)              286.7872 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -32.79645553 +/-    0.0000
Ecliptic Y           -6.46579621 +/-    0.0000
Ecliptic Z            0.89406335 +/-    0.0000
Ecliptic XDOT         0.00044889 +/-    0.0000
Ecliptic YDOT        -0.00326678 +/-    0.0000
Ecliptic ZDOT        -0.00014302 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   33.43966185 +/-    0.0000
Geocenter to KBO     32.98858831 +/-    0.0000
# Hcoef:  7.31

The following table shows the complete astrometric record for 532039. 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 (532039) followed by the observatory code and reference code for the source of the astrometry.

2011 01  29.59965  12 49 00.893  -03 34 18.31  21.9G 532039    F51  C~2rXx      
2011 03  10.53252  12 46 42.081  -03 18 53.54  21.8G 532039    F51  C~2rXx      
2011 03  14.55684  12 46 21.968  -03 16 45.11  22.6r 532039    F51  C~1w3t      
2011 04  01.34020  12 44 47.211  -03 06 51.96  22.8w 532039    F51  C~1w3t      
2011 04  01.41448  12 44 46.784  -03 06 50.31  22.9w 532039    F51  C~1w3t      
2012 02  28.54955  12 55 07.043  -04 18 20.36  23.0w 532039    F51  C~1w3t      
2012 02  28.56398  12 55 06.967  -04 18 19.80  23.0w 532039    F51  C~1w3t      
2012 04  12.34584  12 51 23.369  -03 55 09.86  22.8G 532039    F51  C~2rXx      
2012 04  12.35976  12 51 23.311  -03 55 09.16  22.4G 532039    F51  C~2rXx      
2012 04  12.37376  12 51 23.199  -03 55 08.92  22.3G 532039    F51  C~2rXx      
2012 04  12.38773  12 51 23.146  -03 55 08.20  22.5G 532039    F51  C~2rXx      
2012 12  22.62192  13 03 29.565  -05 18 29.95  22.6w 532039    F51  C~1w3t      
2012 12  22.62652  13 03 29.575  -05 18 30.16  22.6w 532039    F51  C~1w3t      
2012 12  22.62718  13 03 29.575  -05 18 30.09  22.3w 532039    F51  C~1w3t      
2013 01  21.61547  13 04 09.856  -05 21 48.83  23.0G 532039    F51  C~2rXx      
2013 03  19.49171  13 01 12.062  -05 02 35.88  22.7w 532039    F51  C~1w3t      
2013 03  19.50712  13 01 11.944  -05 02 35.49  22.4w 532039    F51  C~1w3t      
2013 03  19.52253  13 01 11.854  -05 02 35.02  22.7w 532039    F51  C~1w3t      
2013 03  19.53796  13 01 11.786  -05 02 34.69  22.3w 532039    F51  C~1w3t      
2013 04  11.37957  12 59 09.057  -04 50 07.61  22.1w 532039    F51  C~1w3t      
2013 04  11.39321  12 59 08.990  -04 50 07.19  22.3w 532039    F51  C~1w3t      
2013 04  11.42067  12 59 08.845  -04 50 06.29  22.4w 532039    F51  C~1w3t      
2013 04  19.47564  12 58 25.635  -04 45 49.63  22.8G 532039    F51  C~2rXx      
2014 02  28.49990  13 10 17.158  -06 05 07.66  22.4w 532039    F51  C~1w3t      
2014 02  28.51117  13 10 17.116  -06 05 07.50  22.8w 532039    F51  C~1w3t      
2014 02  28.52240  13 10 17.076  -06 05 07.42  22.5w 532039    F51  C~1w3t      
2014 02  28.53368  13 10 17.029  -06 05 07.01  22.5w 532039    F51  C~1w3t      
2014 05  04.38302  13 04 49.430  -05 32 24.43  22.3G 532039    F51  C~2rXx      
2014 05  18.28043  13 03 49.143  -05 26 45.82  21.5G 532039    F51  C~2rXx      
2015 03  21.49938  13 16 19.074  -06 48 15.14  22.4G 532039    F51  C~2rXx      
2015 03  22.48754  13 16 14.090  -06 47 45.43  22.7G 532039    F51  C~2rXx      
2015 04  20.38119  13 13 39.104  -06 32 31.34  22.6G 532039    F51  C~2rXx      
2016 01  15.61809  13 26 26.072  -07 55 58.02  22.0G 532039    F51  C~2rXx      
2016 02  09.63341  13 26 17.407  -07 54 42.63  22.6G 532039    F51  C~2rXx      
2016 02  09.64140  13 26 17.384  -07 54 42.40  22.7G 532039    F51  C~2rXx      
2016 02  09.64940  13 26 17.381  -07 54 42.35  23.2G 532039    F51  C~2rXx      
2016 02  09.65736  13 26 17.367  -07 54 42.18  23.5G 532039    F51  C~2rXx      
2016 03  11.52325  13 24 38.503  -07 44 40.77  23.1G 532039    F51  C~2rXx      
2016 03  14.44182  13 24 25.270  -07 43 21.86  22.8G 532039    F51  C~2rXx      
2016 04  02.41710  13 22 49.358  -07 33 57.80  22.6G 532039    F51  C~2rXx      
2016 04  02.44097  13 22 49.194  -07 33 57.12  21.7G 532039    F51  C~2rXx      
2016 04  03.43990  13 22 43.850  -07 33 25.85  22.6G 532039    F51  C~2rXx      
2016 04  03.45226  13 22 43.774  -07 33 25.49  22.4G 532039    F51  C~2rXx      
2016 04  03.46463  13 22 43.705  -07 33 25.14  22.5G 532039    F51  C~2rXx      
2016 04  03.47701  13 22 43.636  -07 33 24.68  22.8G 532039    F51  C~2rXx      
2016 04  28.38476  13 20 29.440  -07 20 32.62  22.5G 532039    F51  C~2rXx      
2017 02  02.59706  13 33 53.416  -08 45 52.09  22.8G 532039    F51  C~2rXx      
2017 03  21.44437  13 31 27.746  -08 31 27.97  22.4G 532039    F51  C~2rXx      
2017 12  23.65270  13 40 08.133  -09 28 46.02  22.2G 532039    F51  C~2rXx      
2018 03  17.55718  13 39 20.582  -09 23 39.45  21.0G 532039    F51  C~2rXx      
2018 06  16.99297  13 32 24.93   -08 45 50.9   23.4V 532039    W84  C~30LZ      
2018 06  17.01892  13 32 24.88   -08 45 50.7   23.3V 532039    W84  C~30LZ      
2018 06  17.07826  13 32 24.75   -08 45 50.1         532039    W84  C~30LZ      
2018 06  17.09033  13 32 24.72   -08 45 49.9         532039    W84  C~30LZ      
2018 06  18.00131  13 32 22.96   -08 45 42.0         532039    W84  C~30LZ      
2018 06  18.05203  13 32 22.86   -08 45 41.4         532039    W84  C~30LZ      
2018 06  18.06409  13 32 22.84   -08 45 41.4         532039    W84  C~30LZ      
2018 06  18.11297  13 32 22.74   -08 45 40.9         532039    W84  C~30LZ      
2020 05  19.16601  13 48 57.69   -10 32 18.1         532039    G37  C~5Rhe      
2020 05  19.19248  13 48 57.56   -10 32 17.5         532039    G37  C~5Rhe      
2020 05  19.22555  13 48 57.40   -10 32 16.7         532039    G37  C~5Rhe      
2020 05  19.28370  13 48 57.13   -10 32 15.1         532039    G37  C~5Rhe      
2022 05  23.197450 14 03 35.262  -12 05 12.11  23.0G 532039    G37  C~5hPU      
2022 05  23.291270 14 03 34.845  -12 05 09.73        532039    G37  C~5hPU      

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    -0.10       0.00     0.01
     2   0.1093      0.00    -0.03       0.00    -0.01
     3   0.1203      0.00     0.17       0.00     0.28
     4   0.1690      0.00    -0.05       0.00     0.15
     5   0.1692      0.00    -0.25       0.00    -0.70
     6   1.0813      0.00     0.16       0.00    -0.11
     7   1.0814      0.00    -0.05       0.00     0.06
     8   1.2012      0.00     0.01       0.00    -0.11
     9   1.2013      0.00     0.28       0.00     0.14
    10   1.2013      0.00    -0.25       0.00    -0.07
    11   1.2013      0.00     0.11       0.00     0.19
    12   1.8974      0.00     0.29       0.00     0.08
    13   1.8974      0.00     0.23       0.00    -0.05
    14   1.8974      0.00     0.20       0.00     0.03
    15   1.9795      0.00     0.19       0.00     0.27
    16   2.1352      0.00     0.24       0.00     0.07
    17   2.1353      0.00    -0.32       0.00    -0.03
    18   2.1353      0.00    -0.46       0.00    -0.05
    19   2.1354      0.00    -0.27       0.00    -0.21
    20   2.1979      0.00     0.05       0.00     0.23
    21   2.1979      0.00     0.18       0.00     0.20
    22   2.1980      0.00     0.28       0.00     0.21
    23   2.2201      0.00    -0.28       0.00    -0.08
    24   3.0825      0.00     0.05       0.00     0.14
    25   3.0826      0.00     0.09       0.00     0.03
    26   3.0826      0.00     0.17       0.00    -0.17
    27   3.0826      0.00     0.15       0.00    -0.03
    28   3.2602      0.00    -0.23       0.00    -0.14
    29   3.2982      0.00    -0.36       0.00    -0.39
    30   4.1394      0.00     0.02       0.00     0.14
    31   4.1421      0.00     0.24       0.00    -0.12
    32   4.2212      0.00     0.07       0.00    -0.23
    33   4.9610      0.00    -0.18       0.00     0.42
    34   5.0295      0.00    -0.02       0.00    -0.19
    35   5.0295      0.00    -0.15       0.00    -0.05
    36   5.0296      0.00     0.03       0.00    -0.09
    37   5.0296      0.00     0.04       0.00    -0.01
    38   5.1141      0.00    -0.01       0.00    -0.12
    39   5.1221      0.00    -0.03       0.00     0.09
    40   5.1740      0.00     0.09       0.00     0.08
    41   5.1741      0.00    -0.41       0.00     0.02
    42   5.1768      0.00     0.05       0.00    -0.03
    43   5.1769      0.00    -0.07       0.00    -0.06
    44   5.1769      0.00    -0.09       0.00    -0.10
    45   5.1769      0.00    -0.10       0.00    -0.03
    46   5.2451      0.00     0.14       0.00     0.02
    47   6.0123      0.00     0.14       0.00    -0.07
    48   6.1406      0.00    -0.11       0.00     0.01
    49   6.8995      0.00    -0.09       0.00     0.78
    50   7.1292      0.00    -0.07       0.00     0.10
    51   7.3796      0.00     0.01       0.00    -0.02
    52   7.3797      0.00     0.08       0.00    -0.05
    53   7.3798      0.00    -0.01       0.00    -0.00
    54   7.3799      0.00    -0.08       0.00     0.09
    55   7.3823      0.00     0.04       0.00    -0.11
    56   7.3825      0.00     0.06       0.00     0.05
    57   7.3825      0.00     0.12       0.00    -0.06
    58   7.3827      0.00     0.07       0.00     0.02
    59   9.3020      0.00     0.06       0.00    -0.13
    60   9.3021      0.00    -0.03       0.00    -0.16
    61   9.3022      0.00    -0.10       0.00    -0.15
    62   9.3024      0.00    -0.05       0.00     0.05
    63  11.3117      0.00    -0.15       0.00    -0.07
    64  11.3120      0.00     0.26       0.00     0.12

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.

532039    quality flag:3

Type:         7:4EEE    7:4EEE    7:4EEE

axisobj        43.477    43.477    43.477
ecceobj         0.237     0.237     0.237
incobj          2.996     2.996     2.996
qmin           32.438    32.438    32.438
qmax           55.438    55.438    55.438
amean          43.726    43.726    43.726
amin           43.342    43.342    43.342
amax           44.196    44.196    44.196
emean           0.243     0.243     0.243
emin            0.231     0.231     0.231
emax            0.255     0.255     0.255
imean           1.809     1.809     1.809
imin            0.987     0.985     0.988
imax            2.758     2.758     2.758
excite_mean     0.245     0.245     0.245
fracstop        1.000     1.000     1.000
cjmean          3.025     3.025     3.025

libcent 0       178.5     178.5     178.5
libamp  0        26.6      26.6      26.5
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       170.9     170.8     170.9
kozaiamp        163.7     164.5     162.7