Orbit Fit and Astrometric record for 15BX603

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: 15BX603   
# Created Thu Apr 25 01:16:54 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     67 observations of     67
# Arc:   9.22y
# First observation: 2015/01/25
#  Last observation: 2024/04/14
# Chi-squared of fit:   172.89 DOF:    128 RMS:  0.28
# Min/Max residuals:    -1.13    0.85
# Exact a, adot, b, bdot, g, gdot:
  1.780230E-05  4.694972E-02 -1.385438E-06 -9.748990E-04  4.017525E-02 -5.938791E-03
# Covariance matrix:
  1.4603E-13 -6.4119E-14 -1.6338E-15  1.5047E-15  6.0991E-14 -1.3364E-13
 -6.4119E-14  4.0879E-14  1.1465E-15 -9.4538E-16 -1.2803E-14  8.8331E-14
 -1.6338E-15  1.1465E-15  4.8357E-14 -1.1481E-14 -3.2189E-16  2.8014E-15
  1.5047E-15 -9.4538E-16 -1.1481E-14  4.8711E-15  5.8648E-16 -2.3444E-15
  6.0991E-14 -1.2803E-14 -3.2189E-16  5.8648E-16  9.0762E-14 -4.0627E-14
 -1.3364E-13  8.8331E-14  2.8014E-15 -2.3444E-15 -4.0627E-14  2.1753E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
    5.687079  149.133891    0.404972    0.088842   -0.890460  2457047.924843
# Heliocentric elements and errors
Epoch:              2457048.5000  =  2015/01/26
Mean Anomaly:          245.39354 +/-     0.009
Argument of Peri:      231.91630 +/-     0.006
Long of Asc Node:       46.60468 +/-     0.001
Inclination:             5.60287 +/-     0.000
Eccentricity:         0.16615147 +/-    0.0000
Semi-Major Axis:     23.66731047 +/-    0.0006
Time of Perihelion: 2470436.8914 +/-       1.6
Perihelion:          19.73495215 +/-    0.0007
Aphelion:            27.59966880 +/-    0.0009
Period (y)              115.1414 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -21.82398359 +/-    0.0002
Ecliptic Y           13.51410507 +/-    0.0001
Ecliptic Z            2.46651829 +/-    0.0000
Ecliptic XDOT        -0.00130525 +/-    0.0000
Ecliptic YDOT        -0.00295500 +/-    0.0000
Ecliptic ZDOT        -0.00010612 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   25.78767839 +/-    0.0001
Geocenter to KBO     24.89103766 +/-    0.0002
# Hcoef:  8.93

The following table shows the complete astrometric record for 15BX603. 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 (15BX603) followed by the observatory code and reference code for the source of the astrometry.

2015 01  25.424065 10 13 20.033  +17 05 48.45  22.7G 15BX603   F51  C~436r      
2015 01  25.435959 10 13 19.928  +17 05 48.92  22.9G 15BX603   F51  C~436r      
2015 01  25.447884 10 13 19.847  +17 05 48.97  22.5G 15BX603   F51  C~436r      
2015 01  25.459800 10 13 19.771  +17 05 49.64  22.9G 15BX603   F51  C~436r      
2015 03  14.266187 10 07 24.531  +17 37 33.18  23.9G 15BX603   F51  C~436r      
2015 03  14.279702 10 07 24.477  +17 37 33.01  22.8G 15BX603   F51  C~436r      
2015 03  14.293943 10 07 24.357  +17 37 34.13  22.8G 15BX603   F51  C~436r      
2015 03  15.260004 10 07 17.663  +17 38 03.63  23.6G 15BX603   F51  C~436r      
2015 03  15.272790 10 07 17.592  +17 38 03.54  22.6G 15BX603   F51  C~436r      
2016 02  06.561549 10 22 25.690  +16 12 13.01  22.8G 15BX603   F51  C~436r      
2016 02  06.574233 10 22 25.602  +16 12 13.56  22.1G 15BX603   F51  C~436r      
2016 02  06.586970 10 22 25.501  +16 12 14.20  22.9G 15BX603   F51  C~436r      
2016 02  06.599727 10 22 25.417  +16 12 14.86  22.8G 15BX603   F51  C~436r      
2016 02  11.378426 10 21 50.060  +16 15 46.28  23.0G 15BX603   F51  C~436r      
2016 02  11.390425 10 21 49.969  +16 15 46.87  23.7G 15BX603   F51  C~436r      
2016 02  11.402076 10 21 49.867  +16 15 47.14  22.7G 15BX603   F51  C~436r      
2016 02  11.413689 10 21 49.768  +16 15 47.80  22.7G 15BX603   F51  C~436r      
2016 03  06.326852 10 18 47.224  +16 32 18.81  22.5G 15BX603   F51  C~436r      
2016 03  06.338550 10 18 47.157  +16 32 19.33  21.9G 15BX603   F51  C~436r      
2016 03  06.350197 10 18 47.076  +16 32 19.66  22.7G 15BX603   F51  C~436r      
2016 03  06.361948 10 18 46.970  +16 32 19.94  23.0G 15BX603   F51  C~436r      
2016 04  03.246324 10 15 44.154  +16 45 36.21  22.7G 15BX603   F51  C~436r      
2016 04  03.257955 10 15 44.097  +16 45 36.32  22.9G 15BX603   F51  C~436r      
2016 04  03.269659 10 15 44.042  +16 45 36.76  23.2G 15BX603   F51  C~436r      
2016 04  03.281403 10 15 43.974  +16 45 36.71  22.5G 15BX603   F51  C~436r      
2016 05  05.310049 10 13 59.624  +16 48 18.79  23.2G 15BX603   F51  C~436r      
2016 05  05.322192 10 13 59.583  +16 48 19.02  23.2G 15BX603   F51  C~436r      
2016 05  06.311923 10 13 58.679  +16 48 09.82  23.7G 15BX603   F51  C~436r      
2016 05  06.323799 10 13 58.623  +16 48 09.65  23.0G 15BX603   F51  C~436r      
2016 05  06.335638 10 13 58.626  +16 48 09.27  23.7G 15BX603   F51  C~436r      
2017 01  27.581018 10 34 00.430  +15 00 29.21  23.2G 15BX603   F51  C~436r      
2017 01  27.581822 10 34 00.426  +15 00 29.05  22.6G 15BX603   F51  C~436r      
2017 01  27.593311 10 34 00.353  +15 00 29.42  22.9G 15BX603   F51  C~436r      
2017 01  27.594086 10 34 00.387  +15 00 29.55  22.9G 15BX603   F51  C~436r      
2017 01  27.605594 10 34 00.275  +15 00 30.20  22.9G 15BX603   F51  C~436r      
2017 01  27.606362 10 34 00.286  +15 00 30.30  22.4G 15BX603   F51  C~436r      
2017 01  27.617967 10 34 00.207  +15 00 30.48  22.5G 15BX603   F51  C~436r      
2017 01  27.618765 10 34 00.194  +15 00 31.48  22.4G 15BX603   F51  C~436r      
2017 03  05.362276 10 29 29.657  +15 27 21.16  22.5G 15BX603   F51  C~436s      
2017 03  05.372262 10 29 29.618  +15 27 21.85  22.6G 15BX603   F51  C~436s      
2017 03  19.423358 10 27 47.227  +15 35 51.88  22.7G 15BX603   F51  C~436s      
2017 03  19.435688 10 27 47.134  +15 35 51.97  21.8G 15BX603   F51  C~436s      
2017 03  28.248363 10 26 49.260  +15 40 10.91  22.4G 15BX603   F51  C~436s      
2017 03  28.258703 10 26 49.186  +15 40 11.04  23.3G 15BX603   F51  C~436s      
2017 03  28.279326 10 26 49.074  +15 40 11.94  23.0G 15BX603   F51  C~436s      
2018 01  15.474425 10 45 41.203  +13 44 24.36  22.7G 15BX603   F51  C~436s      
2018 01  15.486744 10 45 41.141  +13 44 24.79  23.1G 15BX603   F51  C~436s      
2018 01  15.499089 10 45 41.081  +13 44 25.27  22.7G 15BX603   F51  C~436s      
2018 01  15.511560 10 45 41.020  +13 44 25.69  23.6G 15BX603   F51  C~436s      
2018 03  07.298190 10 39 52.766  +14 21 31.71  23.3G 15BX603   F51  C~436s      
2018 03  07.308527 10 39 52.675  +14 21 32.38  22.6G 15BX603   F51  C~436s      
2018 03  07.318848 10 39 52.641  +14 21 32.58  22.4G 15BX603   F51  C~436s      
2018 03  07.329172 10 39 52.523  +14 21 33.28  22.4G 15BX603   F51  C~436s      
2018 03  18.303166 10 38 31.360  +14 28 36.71  21.7G 15BX603   F51  C~436s      
2018 03  18.329360 10 38 31.148  +14 28 37.65  21.5G 15BX603   F51  C~436s      
2018 03  18.342546 10 38 31.059  +14 28 38.01  22.8G 15BX603   F51  C~436s      
2019 01  11.514766 10 56 29.538  +12 31 51.33  23.4G 15BX603   F51  C~436s      
2019 01  11.525934 10 56 29.453  +12 31 51.70  23.2G 15BX603   F51  C~436s      
2019 01  11.537099 10 56 29.450  +12 31 52.21  22.8G 15BX603   F51  C~436s      
2019 01  11.548267 10 56 29.403  +12 31 52.47  23.1G 15BX603   F51  C~436s      
2019 02  04.419436 10 54 20.557  +12 48 05.53  22.0G 15BX603   F51  C~436s      
2019 02  04.431074 10 54 20.496  +12 48 05.68  22.5G 15BX603   F51  C~436s      
2019 02  04.442743 10 54 20.396  +12 48 06.03  22.8G 15BX603   F51  C~436s      
2019 02  04.454551 10 54 20.326  +12 48 06.45  22.2G 15BX603   F51  C~436s      
2024 04  14.16968  11 40 14.058  +07 10 48.92  22.6G 15BX603   G37              
2024 04  14.21146  11 40 13.776  +07 10 50.38        15BX603   G37              
2024 04  14.25198  11 40 13.514  +07 10 51.87        15BX603   G37              

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     0.21       0.00     0.14
     2   0.0000      0.00    -0.14       0.00     0.10
     3   0.0001      0.00    -0.13       0.00    -0.36
     4   0.0001      0.00    -0.05       0.00    -0.20
     5   0.1310      0.00    -0.39       0.00     0.09
     6   0.1310      0.00     0.24       0.00    -0.50
     7   0.1311      0.00    -0.05       0.00     0.18
     8   0.1337      0.00    -0.07       0.00     0.37
     9   0.1337      0.00     0.21       0.00    -0.11
    10   1.0325      0.00    -0.06       0.00     0.06
    11   1.0326      0.00     0.03       0.00     0.05
    12   1.0326      0.00    -0.07       0.00     0.13
    13   1.0327      0.00     0.09       0.00     0.23
    14   1.0457      0.00     0.09       0.00     0.02
    15   1.0458      0.00     0.10       0.00     0.08
    16   1.0458      0.00    -0.10       0.00    -0.17
    17   1.0458      0.00    -0.25       0.00    -0.02
    18   1.1113      0.00    -0.22       0.00     0.01
    19   1.1113      0.00     0.11       0.00     0.09
    20   1.1114      0.00     0.22       0.00    -0.01
    21   1.1114      0.00    -0.03       0.00    -0.17
    22   1.1877      0.00    -0.18       0.00     0.07
    23   1.1878      0.00    -0.09       0.00    -0.04
    24   1.1878      0.00     0.05       0.00     0.18
    25   1.1878      0.00    -0.01       0.00    -0.09
    26   1.2755      0.00     0.28       0.00    -0.09
    27   1.2756      0.00    -0.12       0.00     0.25
    28   1.2783      0.00     0.10       0.00     0.18
    29   1.2783      0.00    -0.56       0.00     0.12
    30   1.2783      0.00    -0.35       0.00    -0.14
    31   2.0073      0.00    -0.44       0.00     0.22
    32   2.0073      0.00    -0.42       0.00     0.02
    33   2.0073      0.00    -0.38       0.00    -0.11
    34   2.0073      0.00     0.21       0.00    -0.01
    35   2.0073      0.00    -0.33       0.00     0.14
    36   2.0073      0.00    -0.09       0.00     0.21
    37   2.0074      0.00    -0.13       0.00    -0.11
    38   2.0074      0.00    -0.25       0.00     0.85
    39   2.1080      0.00    -0.48       0.00    -0.37
    40   2.1080      0.00     0.09       0.00    -0.08
    41   2.1465      0.00    -0.18       0.00    -0.10
    42   2.1465      0.00    -0.27       0.00    -0.40
    43   2.1706      0.00    -0.12       0.00     0.08
    44   2.1707      0.00    -0.25       0.00    -0.06
    45   2.1707      0.00     0.03       0.00     0.29
    46   2.9734      0.00    -0.27       0.00     0.18
    47   2.9735      0.00    -0.28       0.00     0.14
    48   2.9735      0.00    -0.25       0.00     0.14
    49   2.9735      0.00    -0.22       0.00     0.08
    50   3.1126      0.00    -0.33       0.00    -0.21
    51   3.1126      0.00    -0.50       0.00     0.03
    52   3.1126      0.00     0.18       0.00    -0.20
    53   3.1127      0.00    -0.40       0.00     0.08
    54   3.1427      0.00    -0.08       0.00     0.04
    55   3.1428      0.00    -0.40       0.00     0.04
    56   3.1428      0.00    -0.29       0.00    -0.08
    57   3.9619      0.00    -0.18       0.00     0.08
    58   3.9619      0.00    -0.76       0.00     0.06
    59   3.9620      0.00    -0.12       0.00     0.18
    60   3.9620      0.00    -0.13       0.00     0.06
    61   4.0274      0.00    -0.54       0.00     0.56
    62   4.0274      0.00    -0.28       0.00     0.17
    63   4.0274      0.00    -0.61       0.00    -0.01
    64   4.0275      0.00    -0.46       0.00    -0.13
    65   9.2176      0.00    -1.01       0.00     0.15
    66   9.2178      0.00    -1.13       0.00     0.24
    67   9.2179      0.00    -1.07       0.00     0.41

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.

15BX603    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        23.600    23.602    23.598
ecceobj         0.166     0.166     0.166
incobj          5.598     5.598     5.598
qmin           17.818    18.826    18.636
qmax           30.467    28.339    27.753
amean          24.418    23.358    22.435
amin           23.138    22.682    20.057
amax           25.704    23.887    23.673
emean           0.151     0.173     0.125
emin            0.101     0.162     0.054
emax            0.259     0.186     0.172
imean           5.357     5.419     6.477
imin            3.965     4.976     4.955
imax            6.977     5.845     7.403
excite_mean     0.178     0.197     0.170
fracstop        0.036     0.002     0.007
cjmean          3.004     3.014     3.044

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       182.8     273.7     218.7
kozaiamp        178.8      33.9     179.5