Orbit Fit and Astrometric record for 23XQ45

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: 23XQ45    
# Created Wed May 21 01:11:40 2025
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     80 observations of     80
# Arc:   6.32y
# First observation: 2019/01/09
#  Last observation: 2025/05/04
# Chi-squared of fit:    66.46 DOF:    154 RMS:  0.16
# Min/Max residuals:    -0.68    0.77
# Exact a, adot, b, bdot, g, gdot:
  3.425601E-05  2.021860E-01  5.609022E-06  3.546248E-02  9.339774E-02 -5.642973E-02
# Covariance matrix:
  3.6686E-13 -5.8925E-11  1.6935E-14 -9.4413E-12 -2.2368E-12 -2.0289E-11
 -5.8925E-11  1.1518E-07 -9.5347E-12  1.8294E-08  1.2960E-08  3.8539E-08
  1.6935E-14 -9.5347E-12  3.2667E-13 -2.9354E-12  1.5868E-12 -3.7641E-12
 -9.4413E-12  1.8294E-08 -2.9354E-12  3.5278E-09  2.0175E-09  6.1640E-09
 -2.2368E-12  1.2960E-08  1.5868E-12  2.0175E-09  2.4068E-09  4.1624E-09
 -2.0289E-11  3.8539E-08 -3.7641E-12  6.1640E-09  4.1624E-09  1.3004E-08
#      lat0       lon0       xBary       yBary       zBary        JD0
   30.685701  128.413560    0.336580    0.475612   -0.801292  2458492.979082
# Heliocentric elements and errors
Epoch:              2458492.5000  =  2019/01/09
Mean Anomaly:          348.16726 +/-     0.000
Argument of Peri:      120.52581 +/-     0.000
Long of Asc Node:       57.51189 +/-     0.000
Inclination:            29.99292 +/-     0.000
Eccentricity:         0.57516949 +/-    0.0000
Semi-Major Axis:     23.71921721 +/-    0.0000
Time of Perihelion: 2459879.3569 +/-       0.0
Perihelion:          10.07664725 +/-    0.0000
Aphelion:            37.36178717 +/-    0.0000
Period (y)              115.5204 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           -6.03574410 +/-    0.0000
Ecliptic Y            8.14622117 +/-    0.0000
Ecliptic Z            5.46404507 +/-    0.0000
Ecliptic XDOT        -0.00342256 +/-    0.0000
Ecliptic YDOT        -0.00521478 +/-    0.0000
Ecliptic ZDOT         0.00004961 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   11.51735846 +/-    0.0000
Geocenter to KBO     10.70703082 +/-    0.0000
# Hcoef: 11.79

The following table shows the complete astrometric record for 23XQ45. 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 (23XQ45) followed by the observatory code and reference code for the source of the astrometry.

2019 01  09.478281 09 28 35.769  +47 24 47.47  22.9G 23XQ45    F51  C~8rAn      
2019 01  09.491915 09 28 35.539  +47 24 49.40  22.3G 23XQ45    F51  C~8rAn      
2019 01  09.505585 09 28 35.342  +47 24 51.33  22.7G 23XQ45    F51  C~8rAn      
2019 01  09.519267 09 28 35.102  +47 24 53.31  22.6G 23XQ45    F51  C~8rAn      
2019 01  14.468565 09 27 13.066  +47 36 37.08  21.9G 23XQ45    F51  C~8rAn      
2021 02  13.544003 11 33 54.377  +38 45 05.07  22.5G 23XQ45    F51  C~8rAn      
2021 02  13.556184 11 33 54.232  +38 45 07.02  22.3G 23XQ45    F51  C~8rAn      
2021 02  13.568353 11 33 54.062  +38 45 09.53  22.7G 23XQ45    F51  C~8rAn      
2021 02  13.580532 11 33 53.849  +38 45 10.50  22.5G 23XQ45    F51  C~8rAn      
2022 02  06.505526 12 33 03.235  +29 38 12.05  21.8G 23XQ45    F52  C~8rAn      
2022 02  06.516286 12 33 03.157  +29 38 13.74  21.8G 23XQ45    F52  C~8rAn      
2022 02  06.527126 12 33 03.052  +29 38 15.00  22.1G 23XQ45    F52  C~8rAn      
2023 03  25.526563 13 13 03.501  +20 47 39.83  21.5G 23XQ45    F52  C~8rAn      
2023 03  30.521455 13 11 38.624  +20 52 54.48  21.8G 23XQ45    F52  C~8rAn      
2023 03  30.534310 13 11 38.401  +20 52 55.63  22.0G 23XQ45    F52  C~8rAn      
2023 03  30.547135 13 11 38.158  +20 52 56.22  22.0G 23XQ45    F52  C~8rAn      
2023 03  30.560084 13 11 37.949  +20 52 56.81  21.7G 23XQ45    F52  C~8rAn      
2023 04  24.297536 13 04 30.851  +20 59 49.48  21.6w 23XQ45    F52  C~8rAn      
2023 04  24.309613 13 04 30.640  +20 59 48.83  21.7w 23XQ45    F52  C~8rAn      
2023 04  24.321745 13 04 30.450  +20 59 48.51  21.8w 23XQ45    F52  C~8rAn      
2023 04  24.333848 13 04 30.231  +20 59 48.54  21.8w 23XQ45    F52  C~8rAn      
2023 12  11.526310 13 52 25.352  +09 05 12.62  22.8G 23XQ45    V00  C~8rAn      
2023 12  11.531198 13 52 25.468  +09 05 12.19  22.8G 23XQ45    V00  C~8rAn      
2023 12  11.536085 13 52 25.547  +09 05 11.44  23.2G 23XQ45    V00  C~8rAn      
2023 12  11.540969 13 52 25.651  +09 05 11.29  22.3G 23XQ45    V00  C~8rAn      
2024 01  22.610954 14 02 06.938  +08 49 55.14  22.0G 23XQ45    F51  C~8rAn      
2024 01  22.624196 14 02 07.025  +08 49 55.39  22.2G 23XQ45    F51  C~8rAn      
2024 01  22.637427 14 02 07.111  +08 49 55.88  21.9G 23XQ45    F51  C~8rAn      
2024 01  22.650742 14 02 07.190  +08 49 56.13  22.1G 23XQ45    F51  C~8rAn      
2024 03  17.589359 13 58 51.444  +09 49 30.93  21.8G 23XQ45    F52  C~8rAn      
2024 03  17.599744 13 58 51.294  +09 49 31.43  21.3G 23XQ45    F52  C~8rAn      
2024 03  17.610129 13 58 51.189  +09 49 32.33  21.2G 23XQ45    F52  C~8rAn      
2024 03  17.620550 13 58 51.024  +09 49 33.11  21.4G 23XQ45    F52  C~8rAn      
2024 03  19.543770 13 58 26.020  +09 51 55.91  21.8G 23XQ45    F51  C~8rAn      
2024 03  19.544591 13 58 26.009  +09 51 55.87  21.6G 23XQ45    F51  C~8rAn      
2024 04  01.371680 13 55 18.802  +10 06 05.87  21.8G 23XQ45    F52  C~8rAn      
2024 04  01.384035 13 55 18.608  +10 06 06.65  21.6G 23XQ45    F52  C~8rAn      
2024 04  01.396413 13 55 18.408  +10 06 07.35  21.6G 23XQ45    F52  C~8rAn      
2024 04  01.408778 13 55 18.219  +10 06 08.13  21.8G 23XQ45    F52  C~8rAn      
2024 04  10.377705 13 52 51.984  +10 13 32.49  22.0G 23XQ45    F51  C~8rAn      
2024 04  10.388224 13 52 51.794  +10 13 32.85  21.8G 23XQ45    F51  C~8rAn      
2024 04  10.398735 13 52 51.607  +10 13 33.19  21.3G 23XQ45    F51  C~8rAn      
2024 04  10.409331 13 52 51.441  +10 13 33.67  21.7G 23XQ45    F51  C~8rAn      
2024 04  28.312001 13 47 49.007  +10 19 31.46  22.0G 23XQ45    F51  C~8rAn      
2024 04  28.324968 13 47 48.788  +10 19 31.18  21.9G 23XQ45    F51  C~8rAn      
2024 04  28.337978 13 47 48.561  +10 19 31.39  21.7G 23XQ45    F51  C~8rAn      
2024 04  28.350951 13 47 48.350  +10 19 31.02  22.0G 23XQ45    F51  C~8rAn      
2024 04  28.399076 13 47 47.520  +10 19 30.78  21.3G 23XQ45    F51  C~8rAn      
2024 05  03.359439 13 46 26.368  +10 18 43.56  21.7G 23XQ45    V00  C~8rAn      
2024 05  03.365072 13 46 26.260  +10 18 43.70  21.8G 23XQ45    V00  C~8rAn      
2024 05  03.370679 13 46 26.173  +10 18 43.52  21.5G 23XQ45    V00  C~8rAn      
2024 05  03.376294 13 46 26.080  +10 18 43.42  21.7G 23XQ45    V00  C~8rAn      
2024 05  28.398653 13 40 40.516  +09 57 00.88  21.7G 23XQ45    F51  C~8rAn      
2024 05  28.409364 13 40 40.390  +09 56 59.73  21.9G 23XQ45    F51  C~8rAn      
2024 06  01.358495 13 39 59.604  +09 50 53.00  21.9G 23XQ45    F51  C~8rAn      
2024 06  01.370083 13 39 59.490  +09 50 51.98  22.0G 23XQ45    F51  C~8rAn      
2024 06  01.381612 13 39 59.376  +09 50 50.61  22.3G 23XQ45    F51  C~8rAn      
2025 02  25.563267 14 39 37.420  -00 41 42.66  22.2G 23XQ45    F52  C~8rAn      
2025 02  25.575494 14 39 37.357  -00 41 42.32  22.3G 23XQ45    F52  C~8rAn      
2025 02  25.587675 14 39 37.327  -00 41 41.95  22.6G 23XQ45    F52  C~8rAn      
2025 03  03.629454 14 39 11.363  -00 38 20.04  21.8G 23XQ45    F51  C~8rAn      
2025 03  03.637636 14 39 11.311  -00 38 19.83  22.3G 23XQ45    F51  C~8rAn      
2025 03  03.645772 14 39 11.264  -00 38 19.49  22.0G 23XQ45    F51  C~8rAn      
2025 03  08.536917 14 38 40.892  -00 35 13.07  22.1G 23XQ45    F52  C~8rAn      
2025 03  08.549100 14 38 40.790  -00 35 12.93  21.7G 23XQ45    F52  C~8rAn      
2025 03  08.561331 14 38 40.713  -00 35 12.02  21.8G 23XQ45    F52  C~8rAn      
2025 04  07.506305 14 33 00.521  -00 13 45.46  21.3G 23XQ45    F51  C~8rAn      
2025 04  07.518110 14 33 00.342  -00 13 44.79  21.7G 23XQ45    F51  C~8rAn      
2025 04  24.410856 14 28 32.148  -00 04 52.36  21.5w 23XQ45    F51  C~8rAn      
2025 04  24.423381 14 28 31.934  -00 04 52.01  21.9w 23XQ45    F51  C~8rAn      
2025 04  24.435954 14 28 31.720  -00 04 51.86  21.8w 23XQ45    F51  C~8rAn      
2025 04  24.522050 14 28 30.281  -00 04 49.97  21.8G 23XQ45    F51  C~8rAn      
2025 04  24.522690 14 28 30.256  -00 04 49.88  21.7G 23XQ45    F51  C~8rAn      
2025 05  02.396757 14 26 19.518  -00 02 44.69  21.6w 23XQ45    F51  C~8sxk      
2025 05  02.409757 14 26 19.278  -00 02 44.61  21.7w 23XQ45    F51  C~8sxk      
2025 05  02.422759 14 26 19.076  -00 02 44.69  21.7w 23XQ45    F51  C~8sxk      
2025 05  02.435757 14 26 18.852  -00 02 44.53  21.8w 23XQ45    F51  C~8sxk      
2025 05  04.394140 14 25 46.492  -00 02 28.86  21.8w 23XQ45    F51  C~8sxk      
2025 05  04.407435 14 25 46.264  -00 02 28.73  21.7w 23XQ45    F51  C~8sxk      
2025 05  04.420854 14 25 46.038  -00 02 28.72  21.6w 23XQ45    F51  C~8sxk      

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     0.04       0.00     0.08
     2   0.0000      0.00    -0.09       0.00    -0.01
     3   0.0001      0.00     0.29       0.00    -0.10
     4   0.0001      0.00     0.03       0.00    -0.14
     5   0.0137      0.00    -0.15       0.00     0.05
     6   2.0974      0.00    -0.68       0.00    -0.41
     7   2.0974      0.00     0.07       0.00    -0.10
     8   2.0974      0.00     0.45       0.00     0.77
     9   2.0975      0.00     0.18       0.00     0.11
    10   3.0774      0.00    -0.12       0.00    -0.13
    11   3.0774      0.00     0.04       0.00    -0.03
    12   3.0775      0.00    -0.20       0.00    -0.37
    13   4.2055      0.00     0.06       0.00    -0.17
    14   4.2191      0.00     0.04       0.00    -0.17
    15   4.2192      0.00     0.08       0.00     0.27
    16   4.2192      0.00    -0.18       0.00     0.16
    17   4.2193      0.00     0.10       0.00     0.04
    18   4.2870      0.00     0.07       0.00     0.13
    19   4.2870      0.00    -0.06       0.00    -0.22
    20   4.2870      0.00     0.13       0.00    -0.23
    21   4.2871      0.00    -0.11       0.00     0.10
    22   4.9200      0.00    -0.07       0.00     0.22
    23   4.9201      0.00     0.22       0.00     0.15
    24   4.9201      0.00    -0.04       0.00    -0.23
    25   4.9201      0.00     0.08       0.00    -0.02
    26   5.0353      0.00     0.04       0.00     0.08
    27   5.0353      0.00     0.07       0.00    -0.05
    28   5.0353      0.00     0.10       0.00     0.06
    29   5.0354      0.00     0.01       0.00    -0.07
    30   5.1858      0.00     0.24       0.00     0.23
    31   5.1858      0.00     0.04       0.00    -0.05
    32   5.1859      0.00     0.50       0.00     0.08
    33   5.1859      0.00     0.07       0.00     0.08
    34   5.1911      0.00     0.05       0.00     0.03
    35   5.1911      0.00     0.05       0.00    -0.07
    36   5.2263      0.00    -0.14       0.00    -0.06
    37   5.2263      0.00    -0.08       0.00     0.00
    38   5.2263      0.00    -0.10       0.00    -0.02
    39   5.2264      0.00     0.05       0.00     0.05
    40   5.2509      0.00     0.12       0.00     0.07
    41   5.2510      0.00    -0.04       0.00    -0.00
    42   5.2510      0.00    -0.15       0.00    -0.10
    43   5.2510      0.00     0.08       0.00    -0.05
    44   5.3000      0.00    -0.01       0.00     0.20
    45   5.3001      0.00    -0.00       0.00    -0.05
    46   5.3001      0.00    -0.10       0.00     0.19
    47   5.3001      0.00     0.03       0.00    -0.16
    48   5.3003      0.00    -0.18       0.00    -0.27
    49   5.3138      0.00     0.19       0.00    -0.15
    50   5.3139      0.00    -0.04       0.00     0.08
    51   5.3139      0.00     0.03       0.00    -0.00
    52   5.3139      0.00     0.01       0.00    -0.01
    53   5.3824      0.00     0.11       0.00     0.06
    54   5.3824      0.00     0.01       0.00    -0.15
    55   5.3932      0.00    -0.10       0.00     0.11
    56   5.3933      0.00    -0.05       0.00     0.23
    57   5.3933      0.00    -0.02       0.00     0.00
    58   6.1303      0.00     0.10       0.00     0.23
    59   6.1303      0.00    -0.19       0.00     0.20
    60   6.1303      0.00     0.00       0.00     0.19
    61   6.1469      0.00     0.15       0.00     0.03
    62   6.1469      0.00     0.07       0.00    -0.06
    63   6.1469      0.00     0.06       0.00    -0.01
    64   6.1603      0.00    -0.04       0.00    -0.01
    65   6.1604      0.00    -0.22       0.00    -0.35
    66   6.1604      0.00    -0.02       0.00     0.07
    67   6.2424      0.00    -0.10       0.00    -0.35
    68   6.2424      0.00    -0.09       0.00    -0.14
    69   6.2887      0.00     0.00       0.00    -0.08
    70   6.2887      0.00    -0.03       0.00    -0.00
    71   6.2887      0.00    -0.05       0.00    -0.12
    72   6.2890      0.00     0.19       0.00    -0.11
    73   6.2890      0.00    -0.02       0.00    -0.03
    74   6.3105      0.00     0.13       0.00     0.21
    75   6.3106      0.00    -0.18       0.00     0.16
    76   6.3106      0.00     0.09       0.00    -0.05
    77   6.3106      0.00     0.03       0.00    -0.01
    78   6.3160      0.00     0.01       0.00    -0.02
    79   6.3160      0.00    -0.06       0.00     0.03
    80   6.3161      0.00    -0.06       0.00    -0.05

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.

23XQ45    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        23.834    23.833    23.834
ecceobj         0.573     0.573     0.573
incobj         29.887    29.887    29.887
qmin           10.053    10.053    10.053
qmax           39.017    39.011    39.016
amean          24.038    24.119    24.187
amin           23.517    23.715    23.639
amax           24.645    24.627    24.644
emean           0.571     0.570     0.577
emin            0.548     0.558     0.563
emax            0.587     0.587     0.587
imean          29.710    30.186    29.430
imin           28.898    28.898    28.898
imax           30.661    31.266    29.956
excite_mean     0.756     0.760     0.758
fracstop        0.002     0.005     0.001
cjmean          2.520     2.512     2.513

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       130.5     132.6     127.4
kozaiamp         10.4      10.2       7.3