Orbit Fit and Astrometric record for 13XU33

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: 13XU33    
# Created Sat Apr 27 01:15:42 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     36 observations of     36
# Arc:   9.07y
# First observation: 2013/11/03
#  Last observation: 2022/11/28
# Chi-squared of fit:     6.26 DOF:     66 RMS:  0.07
# Min/Max residuals:    -0.16    0.15
# Exact a, adot, b, bdot, g, gdot:
  1.476761E-05  2.622172E-02  5.431949E-06  9.321284E-03  2.675624E-02 -2.451282E-03
# Covariance matrix:
  1.2552E-13 -6.3961E-14  1.7469E-14 -1.7961E-14  3.6979E-15 -2.1784E-13
 -6.3961E-14  5.8926E-14 -1.8490E-14  1.9589E-14 -1.3913E-14  2.3808E-13
  1.7469E-14 -1.8490E-14  8.6994E-14 -2.2273E-14 -8.5939E-16 -8.2881E-14
 -1.7961E-14  1.9589E-14 -2.2273E-14  1.3241E-14 -5.1341E-15  8.8104E-14
  3.6979E-15 -1.3913E-14 -8.5939E-16 -5.1341E-15  1.0375E-13 -6.7488E-14
 -2.1784E-13  2.3808E-13 -8.2881E-14  8.8104E-14 -6.7488E-14  1.0711E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
  -12.275109   24.394504   -0.274364   -0.202338   -0.930527  2456599.559968
# Heliocentric elements and errors
Epoch:              2456600.5000  =  2013/11/04
Mean Anomaly:          310.54090 +/-     0.023
Argument of Peri:       26.66966 +/-     0.029
Long of Asc Node:       54.98374 +/-     0.000
Inclination:            22.87835 +/-     0.000
Eccentricity:         0.10018832 +/-    0.0000
Semi-Major Axis:     40.69700798 +/-    0.0023
Time of Perihelion: 2469628.7430 +/-       9.1
Perihelion:          36.61964312 +/-    0.0024
Aphelion:            44.77437285 +/-    0.0028
Period (y)              259.6282 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           34.01275059 +/-    0.0004
Ecliptic Y           15.72947829 +/-    0.0002
Ecliptic Z           -7.94587233 +/-    0.0001
Ecliptic XDOT        -0.00115289 +/-    0.0000
Ecliptic YDOT         0.00242448 +/-    0.0000
Ecliptic ZDOT         0.00098547 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   38.30697598 +/-    0.0004
Geocenter to KBO     37.37455599 +/-    0.0004
# Hcoef:  7.39

The following table shows the complete astrometric record for 13XU33. 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 (13XU33) followed by the observatory code and reference code for the source of the astrometry.

2013 11  03.05919  01 48 17.34   -01 58 43.6   23.8r 13XU33    W84  C~3clm      
2013 11  03.12180  01 48 17.02   -01 58 44.7         13XU33    W84  C~3clm      
2013 11  03.20695  01 48 16.58   -01 58 46.2         13XU33    W84  C~3clm      
2013 12  01.18002  01 46 10.993  -02 03 09.62  23.4r 13XU33    W84  C~4yRo      
2013 12  01.18002  01 46 10.99   -02 03 09.6   23.5r 13XU33    W84  C~3clm      
2013 12  01.18139  01 46 10.987  -02 03 09.68  22.8i 13XU33    W84  C~4yRo      
2013 12  01.18139  01 46 10.99   -02 03 09.7   22.7i 13XU33    W84  C~3clm      
2013 12  20.12539  01 45 14.519  -02 01 22.88  22.7i 13XU33    W84  C~4yRo      
2014 08  18.37835  01 58 20.607  -00 24 07.10  23.2i 13XU33    W84  C~4yRo      
2014 08  18.37835  01 58 20.61   -00 24 07.1   23.3i 13XU33    W84  C~3clm      
2014 10  01.33657  01 55 54.460  -00 43 04.83  23.0r 13XU33    W84  C~4yRo      
2014 10  01.33657  01 55 54.46   -00 43 04.8   23.1r 13XU33    W84  C~3clm      
2014 10  21.29028  01 54 14.753  -00 51 35.49  22.8r 13XU33    W84  C~4yRo      
2014 10  21.29028  01 54 14.76   -00 51 35.5   23.2r 13XU33    W84  C~3clm      
2014 12  25.08913  01 49 50.746  -00 58 37.45  22.8z 13XU33    W84  C~4yRo      
2015 01  15.04625  01 49 33.380  -00 51 29.07  23.0z 13XU33    W84  C~4yRo      
2015 01  16.04263  01 49 33.671  -00 51 02.22  23.1z 13XU33    W84  C~4yRo      
2015 09  04.32065  02 02 31.521  +00 31 52.77  23.0z 13XU33    W84  C~4yRo      
2015 11  20.13475  01 56 37.493  +00 02 54.46  22.7z 13XU33    W84  C~4yRo      
2015 12  29.13643  01 54 30.196  +00 04 14.45  22.9z 13XU33    W84  C~4yRo      
2016 01  12.05868  01 54 17.204  +00 08 39.98  23.7r 13XU33    W84  C~4yRo      
2016 01  12.05868  01 54 17.21   +00 08 40.0   23.9r 13XU33    W84  C~3clm      
2016 08  26.34885  02 07 42.467  +01 37 39.99  23.2r 13XU33    W84  C~4yRo      
2016 08  26.34885  02 07 42.47   +01 37 40.0   23.5r 13XU33    W84  C~3clm      
2016 09  09.40021  02 07 04.109  +01 32 16.79  23.1i 13XU33    W84  C~4yRo      
2016 09  10.38751  02 07 00.812  +01 31 52.35  22.5z 13XU33    W84  C~4yRo      
2016 10  22.23427  02 03 51.238  +01 14 07.27  22.5z 13XU33    W84  C~4yRo      
2017 09  18.33522  02 11 25.610  +02 31 47.65  23.3r 13XU33    W84  C~4yRo      
2018 09  11.32738  02 16 45.634  +03 37 57.78  22.7i 13XU33    W84  C~4yRo      
2018 09  11.32877  02 16 45.623  +03 37 57.80  23.7r 13XU33    W84  C~4yRo      
2018 10  20.21247  02 13 53.749  +03 22 16.57  22.4z 13XU33    W84  C~4yRo      
2018 11  28.04459  02 10 37.702  +03 11 23.35  22.6r 13XU33    W84  C~4yRo      
2018 11  29.17618  02 10 32.730  +03 11 14.36  24.3g 13XU33    W84  C~4yRo      
2022 11  28.100710 02 30 36.540  +07 27 07.92  23.2G 13XU33    G37  C~675t      
2022 11  28.151890 02 30 36.291  +07 27 07.42        13XU33    G37  C~675t      
2022 11  28.204040 02 30 36.035  +07 27 06.85        13XU33    G37  C~675t      

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     0.13       0.00     0.07
     2   0.0002      0.00     0.14       0.00     0.06
     3   0.0004      0.00     0.09       0.00     0.03
     4   0.0770      0.00    -0.08       0.00     0.01
     5   0.0770      0.00    -0.03       0.00    -0.01
     6   0.0770      0.00    -0.00       0.00    -0.09
     7   0.0770      0.00    -0.05       0.00    -0.07
     8   0.1289      0.00     0.04       0.00     0.05
     9   0.7894      0.00    -0.01       0.00     0.02
    10   0.7894      0.00     0.04       0.00     0.02
    11   0.9097      0.00    -0.15       0.00    -0.07
    12   0.9097      0.00    -0.15       0.00    -0.10
    13   0.9644      0.00    -0.04       0.00     0.02
    14   0.9644      0.00    -0.15       0.00     0.03
    15   1.1418      0.00     0.02       0.00    -0.15
    16   1.1991      0.00    -0.16       0.00     0.13
    17   1.2019      0.00     0.03       0.00    -0.03
    18   1.8351      0.00    -0.02       0.00     0.10
    19   2.0454      0.00     0.10       0.00     0.03
    20   2.1522      0.00    -0.02       0.00     0.04
    21   2.1903      0.00     0.15       0.00    -0.02
    22   2.1903      0.00     0.06       0.00    -0.04
    23   2.8126      0.00     0.06       0.00     0.01
    24   2.8126      0.00     0.02       0.00    -0.00
    25   2.8510      0.00     0.14       0.00     0.03
    26   2.8537      0.00     0.07       0.00     0.04
    27   2.9683      0.00     0.08       0.00    -0.07
    28   3.8748      0.00     0.02       0.00     0.02
    29   4.8549      0.00     0.03       0.00    -0.07
    30   4.8549      0.00    -0.06       0.00    -0.02
    31   4.9614      0.00    -0.14       0.00     0.10
    32   5.0677      0.00    -0.04       0.00     0.02
    33   5.0708      0.00    -0.04       0.00     0.03
    34   9.0679      0.00     0.04       0.00    -0.07
    35   9.0680      0.00     0.02       0.00     0.00
    36   9.0682      0.00    -0.03       0.00     0.02

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.

13XU33    quality flag:3

Type:       SCATEXTD  SCATEXTD  SCATEXTD

axisobj        40.910    40.910    40.910
ecceobj         0.101     0.101     0.101
incobj         22.860    22.860    22.860
qmin           35.878    35.783    35.882
qmax           45.813    45.916    45.776
amean          40.697    40.697    40.698
amin           40.344    40.327    40.339
amax           41.085    41.078    41.073
emean           0.100     0.100     0.101
emin            0.085     0.085     0.088
emax            0.116     0.119     0.115
imean          21.547    21.536    21.529
imin           20.842    20.853    20.878
imax           22.113    22.137    22.122
excite_mean     0.381     0.381     0.381
fracstop        1.000     1.000     1.000
cjmean          2.891     2.892     2.891

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       173.3     173.3     175.8
kozaiamp        179.9     179.9     179.9