Orbit Fit and Astrometric record for 13FL28

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: 13FL28    
# Created Fri Apr 26 01:14:21 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     65 observations of     65
# Arc:  11.15y
# First observation: 2011/01/30
#  Last observation: 2022/03/27
# Chi-squared of fit:    81.78 DOF:    124 RMS:  0.20
# Min/Max residuals:    -0.51    0.68
# Exact a, adot, b, bdot, g, gdot:
  2.387598E-05  4.759494E-02 -4.514375E-06 -1.042428E-02  3.187959E-02 -1.967546E-03
# Covariance matrix:
  9.6729E-14 -2.8953E-14 -6.1665E-15  4.5506E-15  3.8588E-15 -4.0361E-14
 -2.8953E-14  1.9706E-14  4.8112E-15 -4.0012E-15  1.1003E-14  3.5023E-14
 -6.1665E-15  4.8112E-15  6.9914E-14 -9.7370E-15  6.4621E-16  9.4722E-15
  4.5506E-15 -4.0012E-15 -9.7370E-15  2.5281E-15 -2.2670E-15 -7.7679E-15
  3.8588E-15  1.1003E-14  6.4621E-16 -2.2670E-15  5.5254E-14  1.8258E-14
 -4.0361E-14  3.5023E-14  9.4722E-15 -7.7679E-15  1.8258E-14  6.8094E-14
#      lat0       lon0       xBary       yBary       zBary        JD0
  -10.107104  152.714223    0.379126   -0.160144   -0.898416  2455591.907796
# Heliocentric elements and errors
Epoch:              2455592.5000  =  2011/01/31
Mean Anomaly:          359.87287 +/-     0.000
Argument of Peri:      224.99359 +/-     0.001
Long of Asc Node:      294.38349 +/-     0.000
Inclination:            15.82764 +/-     0.000
Eccentricity:         0.90786317 +/-    0.0000
Semi-Major Axis:    349.19076614 +/-    0.1520
Time of Perihelion: 2456434.1837 +/-    1555.2
Perihelion:          32.17333027 +/-    0.0196
Aphelion:           666.20820201 +/-    0.2902
Period (y)             6525.3277 +/-      4.26
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -28.07852795 +/-    0.0002
Ecliptic Y           14.91094256 +/-    0.0001
Ecliptic Z           -5.50489554 +/-    0.0000
Ecliptic XDOT        -0.00158744 +/-    0.0000
Ecliptic YDOT        -0.00377488 +/-    0.0000
Ecliptic ZDOT        -0.00085169 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   32.26524989 +/-    0.0002
Geocenter to KBO     31.36808915 +/-    0.0002
# Hcoef:  8.02

The following table shows the complete astrometric record for 13FL28. 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 (13FL28) followed by the observatory code and reference code for the source of the astrometry.

2011 01  30.407030 10 04 13.329  +01 03 39.19  23.2G 13FL28    F51  C~5Xcq      
2011 01  30.421791 10 04 13.239  +01 03 39.38  22.9G 13FL28    F51  C~5Xcq      
2011 01  30.437865 10 04 13.169  +01 03 39.56  22.4G 13FL28    F51  C~5Xcq      
2011 01  30.452644 10 04 13.099  +01 03 39.90  23.1G 13FL28    F51  C~5Xcq      
2011 02  04.453345 10 03 46.389  +01 05 01.67  23.2G 13FL28    F51  C~5Xcq      
2011 02  04.467611 10 03 46.341  +01 05 02.19  23.2G 13FL28    F51  C~5Xcq      
2011 02  04.482069 10 03 46.239  +01 05 02.15  23.1G 13FL28    F51  C~5Xcq      
2011 02  04.496500 10 03 46.161  +01 05 02.81  22.6G 13FL28    F51  C~5Xcq      
2011 02  05.455724 10 03 40.929  +01 05 19.64  22.7G 13FL28    F51  C~5Xcq      
2011 06  02.244549 09 58 34.38   +01 44 15.2   22.7i 13FL28    568  C~5Xcq      
2011 06  04.245211 09 58 40.64   +01 44 07.1   22.6z 13FL28    568  C~5Xcq      
2011 10  27.621935 10 14 39.636  +00 04 41.86  22.2G 13FL28    F51  C~5Xcq      
2012 01  19.458548 10 14 29.021  -00 29 40.49  22.2G 13FL28    F51  C~5Xcq      
2012 01  19.481358 10 14 28.902  -00 29 40.89  22.5G 13FL28    F51  C~5Xcq      
2012 01  19.495365 10 14 28.852  -00 29 40.41  22.3G 13FL28    F51  C~5Xcq      
2012 01  19.509507 10 14 28.779  -00 29 40.63  23.1G 13FL28    F51  C~5Xcq      
2012 03  21.297876 10 09 04.428  -00 06 53.40  22.7G 13FL28    F51  C~5Xcq      
2013 03  16.03362  10 18 55.393  -01 41 31.46  23.1r 13FL28    807  C~1M7X      
2013 03  16.10813  10 18 55.012  -01 41 28.96  23.2r 13FL28    807  C~1M7X      
2013 03  16.17826  10 18 54.641  -01 41 27.00        13FL28    807  C~1M7X      
2013 03  17.03265  10 18 50.364  -01 41 00.09        13FL28    807  C~1M7X      
2013 04  01.098495 10 17 41.91   -01 33 08.8         13FL28    W84  C~55Mp      
2013 04  01.099653 10 17 41.90   -01 33 08.7         13FL28    W84  C~55Mp      
2013 04  03.148519 10 17 33.83   -01 32 05.8         13FL28    W84  C~55Mp      
2013 04  03.149676 10 17 33.82   -01 32 05.8         13FL28    W84  C~55Mp      
2014 03  26.007308 10 27 34.18   -03 08 09.9   23.1V 13FL28    W84  C~5Xcq      
2014 03  28.006398 10 27 25.06   -03 07 04.8   22.9V 13FL28    W84  C~5Xcq      
2015 02  20.425449 10 40 01.377  -04 56 13.12  23.0G 13FL28    F51  C~5Xcq      
2015 12  13.602501 10 53 04.193  -06 21 06.40  22.5G 13FL28    F51  C~5Xcq      
2015 12  13.615270 10 53 04.215  -06 21 06.77  23.6G 13FL28    F51  C~5Xcq      
2015 12  13.628083 10 53 04.218  -06 21 07.27  22.9G 13FL28    F51  C~5Xcq      
2016 01  12.544643 10 52 23.559  -06 31 37.94  22.8G 13FL28    F51  C~5Xcq      
2016 01  17.528286 10 52 07.573  -06 32 09.43  22.8G 13FL28    F51  C~5Xcq      
2016 01  17.541599 10 52 07.533  -06 32 09.47  23.4G 13FL28    F51  C~5Xcq      
2016 01  17.568245 10 52 07.407  -06 32 09.45  23.0G 13FL28    F51  C~5Xcq      
2016 03  30.361525 10 46 05.006  -06 07 27.65  23.3G 13FL28    F51  C~5Xcq      
2016 04  30.264742 10 44 20.792  -05 50 34.75  23.0G 13FL28    F51  C~5Xcq      
2016 04  30.275884 10 44 20.778  -05 50 34.45  23.6G 13FL28    F51  C~5Xcr      
2016 04  30.287007 10 44 20.743  -05 50 34.30  22.9G 13FL28    F51  C~5Xcr      
2016 04  30.298143 10 44 20.716  -05 50 33.99  23.1G 13FL28    F51  C~5Xcr      
2017 01  26.574313 11 00 53.973  -08 00 47.86  23.9G 13FL28    F51  C~5Xcr      
2017 03  02.188525 10 58 01.20   -07 52 07.4   22.7r 13FL28    W84  C~5Xcr      
2017 03  02.189547 10 58 01.19   -07 52 07.4   23.2g 13FL28    W84  C~5Xcr      
2018 05  18.050752 11 02 34.64   -08 38 37.6   23.4g 13FL28    W84  C~5Xcr      
2019 01  04.654144 11 20 33.878  -10 48 10.74  22.9G 13FL28    F51  C~5Xcr      
2019 01  12.544326 11 20 19.725  -10 50 41.79  23.0G 13FL28    F51  C~5Xcr      
2019 01  12.557693 11 20 19.677  -10 50 42.21  23.0G 13FL28    F51  C~5Xcr      
2019 02  05.562042 11 18 59.087  -10 52 42.19  23.6G 13FL28    F51  C~5Xcr      
2019 04  08.341431 11 13 42.704  -10 26 37.61  23.0G 13FL28    F51  C~5Xcr      
2019 05  01.346767 11 12 19.189  -10 12 45.47  22.2G 13FL28    F51  C~5Xcr      
2019 06  02.298343 11 11 48.158  -09 58 15.26  23.0G 13FL28    F51  C~5Xcr      
2020 01  01.648403 11 29 48.648  -12 08 45.41  22.6G 13FL28    F51  C~5Xcr      
2020 04  17.347838 11 22 21.915  -11 44 52.37  23.5G 13FL28    F51  C~5Xcr      
2020 05  11.278359 11 21 11.154  -11 30 43.51  23.9G 13FL28    F51  C~5Xcr      
2020 12  17.592856 11 38 50.221  -13 19 46.17  24.1G 13FL28    F51  C~5Xcr      
2020 12  21.599985 11 38 54.322  -13 22 23.09  23.6G 13FL28    F51  C~5Xcr      
2020 12  22.629953 11 38 55.062  -13 23 01.60  23.0G 13FL28    F52  C~5Xcr      
2021 02  11.498405 11 37 07.942  -13 36 16.11  23.4G 13FL28    F51  C~5Xcr      
2021 02  17.526601 11 36 40.099  -13 35 20.68  22.9G 13FL28    F51  C~5Xcr      
2021 03  04.109453 11 35 25.85   -13 31 09.1         13FL28    W84  C~5Xcr      
2021 03  04.194388 11 35 25.38   -13 31 06.9         13FL28    W84  C~5Xcr      
2021 04  09.393988 11 32 15.697  -13 12 02.51  23.5G 13FL28    F51  C~5Xcr      
2021 05  09.321114 11 30 28.344  -12 53 30.72  21.9G 13FL28    F51  C~5Xcr      
2022 02  26.455554 11 45 12.871  -14 51 56.06  23.8G 13FL28    F52  C~5Xcr      
2022 03  27.353127 11 42 38.888  -14 39 26.16  23.2G 13FL28    F52  C~5Xcr      

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    -0.11
     2   0.0000      0.00    -0.27       0.00    -0.14
     3   0.0001      0.00    -0.03       0.00    -0.20
     4   0.0001      0.00     0.10       0.00    -0.08
     5   0.0138      0.00    -0.13       0.00    -0.21
     6   0.0139      0.00     0.34       0.00     0.06
     7   0.0139      0.00     0.01       0.00    -0.24
     8   0.0139      0.00     0.04       0.00     0.17
     9   0.0166      0.00    -0.19       0.00    -0.30
    10   0.3363      0.00     0.22       0.00    -0.09
    11   0.3418      0.00    -0.31       0.00     0.13
    12   0.7398      0.00    -0.31       0.00     0.33
    13   0.9693      0.00     0.07       0.00     0.29
    14   0.9694      0.00    -0.16       0.00    -0.25
    15   0.9694      0.00     0.04       0.00     0.15
    16   0.9695      0.00    -0.09       0.00    -0.16
    17   1.1386      0.00     0.07       0.00     0.04
    18   2.1235      0.00     0.45       0.00     0.44
    19   2.1238      0.00     0.48       0.00     0.63
    20   2.1239      0.00     0.33       0.00     0.40
    21   2.1263      0.00     0.34       0.00     0.68
    22   2.1675      0.00     0.03       0.00    -0.05
    23   2.1675      0.00    -0.04       0.00     0.02
    24   2.1731      0.00    -0.04       0.00    -0.16
    25   2.1731      0.00    -0.13       0.00    -0.19
    26   3.1502      0.00    -0.09       0.00    -0.15
    27   3.1556      0.00    -0.10       0.00    -0.28
    28   4.0575      0.00     0.01       0.00    -0.21
    29   4.8684      0.00    -0.10       0.00    -0.18
    30   4.8685      0.00     0.18       0.00    -0.12
    31   4.8685      0.00     0.17       0.00    -0.20
    32   4.9504      0.00    -0.04       0.00     0.00
    33   4.9641      0.00     0.04       0.00    -0.10
    34   4.9641      0.00     0.14       0.00    -0.08
    35   4.9642      0.00    -0.33       0.00     0.05
    36   5.1635      0.00    -0.20       0.00    -0.03
    37   5.2481      0.00    -0.06       0.00     0.07
    38   5.2481      0.00     0.08       0.00     0.05
    39   5.2481      0.00    -0.11       0.00    -0.12
    40   5.2482      0.00    -0.17       0.00    -0.13
    41   5.9909      0.00    -0.21       0.00     0.24
    42   6.0856      0.00    -0.08       0.00    -0.01
    43   6.0856      0.00    -0.14       0.00    -0.04
    44   7.2954      0.00     0.05       0.00    -0.07
    45   7.9295      0.00    -0.20       0.00     0.19
    46   7.9511      0.00     0.18       0.00    -0.05
    47   7.9511      0.00    -0.08       0.00    -0.26
    48   8.0169      0.00     0.04       0.00     0.04
    49   8.1860      0.00    -0.12       0.00     0.06
    50   8.2490      0.00     0.16       0.00     0.03
    51   8.3365      0.00    -0.01       0.00    -0.12
    52   8.9206      0.00     0.12       0.00    -0.08
    53   9.2127      0.00    -0.18       0.00     0.19
    54   9.2782      0.00    -0.19       0.00    -0.03
    55   9.8814      0.00     0.10       0.00    -0.13
    56   9.8924      0.00     0.24       0.00     0.05
    57   9.8952      0.00     0.22       0.00     0.03
    58  10.0345      0.00     0.13       0.00    -0.03
    59  10.0510      0.00    -0.51       0.00    -0.06
    60  10.0909      0.00     0.06       0.00    -0.02
    61  10.0911      0.00    -0.09       0.00     0.28
    62  10.1902      0.00     0.26       0.00    -0.25
    63  10.2722      0.00     0.34       0.00     0.23
    64  11.0747      0.00    -0.04       0.00     0.04
    65  11.1539      0.00    -0.16       0.00     0.04

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.

13FL28    quality flag:3

Type:       CENTAURS  CENTAURS  CENTAURS

axisobj       358.317   358.297   358.336
ecceobj         0.910     0.910     0.910
incobj         15.816    15.816    15.816
qmin           28.704    28.677    28.635
qmax          904.052   936.477   838.806
amean         385.770   388.756   370.590
amin          343.354   345.563   337.409
amax          468.069   484.335   435.320
emean           0.917     0.917     0.913
emin            0.902     0.901     0.900
emax            0.932     0.934     0.927
imean          16.744    16.762    16.743
imin           15.921    16.043    15.894
imax           17.962    17.939    17.949
excite_mean     0.961     0.962     0.958
fracstop        1.000     1.000     1.000
cjmean          2.812     2.812     2.813

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       239.8     239.3     240.2
kozaiamp         17.7      16.2      18.3