Orbit Fit and Astrometric record for 24RU155

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: 24RU155   
# Created Tue Jan 21 02:11:45 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc: 112.76d
# First observation: 2024/09/09
#  Last observation: 2024/12/31
Preliminary a, adot, b, bdot, g, gdot:
  -0.000095   0.460228  -0.000380   0.037404   0.163726   0.000000
# Chi-squared of fit:    13.87 DOF:     34 RMS:  0.15
# Min/Max residuals:    -0.30    0.36
# Exact a, adot, b, bdot, g, gdot:
  3.752716E-05  3.373505E-01  2.470164E-06  3.014945E-02  1.423467E-01 -9.776901E-02
# Covariance matrix:
  3.6500E-13 -3.0616E-12 -9.6048E-16  9.0494E-14  8.6899E-13  6.4809E-11
 -3.0616E-12  1.7557E-08 -6.2343E-11  9.3506E-10  2.4466E-09 -8.2281E-08
 -9.6048E-16 -6.2343E-11  3.4889E-13 -4.0226E-12 -8.7390E-12  2.9019E-10
  9.0494E-14  9.3506E-10 -4.0226E-12  5.8980E-11  1.3146E-10 -4.3354E-09
  8.6899E-13  2.4466E-09 -8.7390E-12  1.3146E-10  3.4715E-10 -1.1200E-08
  6.4809E-11 -8.2281E-08  2.9019E-10 -4.3354E-09 -1.1200E-08  3.9793E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
    5.249945   10.986214    0.414511    0.083239   -0.908293  2460562.915141
# Heliocentric elements and errors
Epoch:              2460560.5000  =  2024/09/07
Mean Anomaly:          324.95442 +/-     0.118
Argument of Peri:      116.21686 +/-     0.053
Long of Asc Node:      326.69743 +/-     0.008
Inclination:             7.00405 +/-     0.001
Eccentricity:         0.39755673 +/-    0.0021
Semi-Major Axis:     10.43582452 +/-    0.0217
Time of Perihelion: 2461759.2245 +/-       1.5
Perihelion:           6.28699220 +/-    0.0253
Aphelion:            14.58465683 +/-    0.0372
Period (y)               33.7131 +/-      0.10
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X            7.84826103 +/-    0.0009
Ecliptic Y            1.10476509 +/-    0.0002
Ecliptic Z            0.64284726 +/-    0.0001
Ecliptic XDOT        -0.00313343 +/-    0.0000
Ecliptic YDOT         0.00600746 +/-    0.0000
Ecliptic ZDOT         0.00040549 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO    7.95166395 +/-    0.0009
Geocenter to KBO      7.02510376 +/-    0.0009
# Hcoef: 13.36

The following table shows the complete astrometric record for 24RU155. 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 (24RU155) followed by the observatory code and reference code for the source of the astrometry.

2024 09  09.414340 00 32 04.557  +09 10 27.34  22.3w 24RU155   F52  C~8Mqc      
2024 09  09.426927 00 32 04.346  +09 10 26.31  22.2w 24RU155   F52  C~8Mqc      
2024 09  09.439514 00 32 04.111  +09 10 25.28  22.0w 24RU155   F52  C~8Mqc      
2024 09  09.452156 00 32 03.864  +09 10 24.17  22.4w 24RU155   F52  C~8Mqc      
2024 09  28.341715 00 25 58.734  +08 41 09.03  22.7w 24RU155   F51  C~8Mqc      
2024 09  28.354250 00 25 58.491  +08 41 07.66  22.1w 24RU155   F51  C~8Mqc      
2024 09  28.366192 00 25 58.240  +08 41 06.44  22.1w 24RU155   F51  C~8Mqc      
2024 09  28.379956 00 25 57.956  +08 41 04.99  22.1w 24RU155   F51  C~8Mqc      
2024 10  01.13970  00 25 01.802  +08 36 03.73  22.2G 24RU155   309  C~8Mqc      
2024 10  01.14093  00 25 01.739  +08 36 03.72  22.1G 24RU155   309  C~8Mqc      
2024 10  01.14216  00 25 01.702  +08 36 03.61  22.1G 24RU155   309  C~8Mqc      
2024 10  01.14341  00 25 01.722  +08 36 03.34  21.9G 24RU155   309  C~8Mqc      
2024 10  01.14465  00 25 01.656  +08 36 03.41  22.1G 24RU155   309  C~8Mqc      
2024 10  01.14588  00 25 01.645  +08 36 03.16  22.1G 24RU155   309  C~8Mqc      
2024 10  01.14710  00 25 01.608  +08 36 03.12  21.9G 24RU155   309  C~8Mqc      
2024 10  01.14955  00 25 01.552  +08 36 02.85  22.1G 24RU155   309  C~8Mqc      
2024 10  01.15078  00 25 01.547  +08 36 02.78  22.2G 24RU155   309  C~8Mqc      
2024 12  31.07679  00 14 00.608  +07 05 12.05  22.4G 24RU155   G37              
2024 12  31.12800  00 14 01.236  +07 05 14.76        24RU155   G37              
2024 12  31.17901  00 14 01.888  +07 05 17.66        24RU155   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    -0.01       0.00     0.18
     2   0.0000     -3.28     0.19       0.29    -0.01
     3   0.0001     -6.88     0.07       0.72    -0.06
     4   0.0001    -10.68    -0.23       1.15    -0.12
     5   0.0518  -5674.54    -0.20     541.24     0.03
     6   0.0519  -5678.40     0.03     541.42    -0.10
     7   0.0519  -5682.30     0.01     541.79    -0.02
     8   0.0519  -5686.74     0.06     542.14    -0.01
     9   0.0595  -6571.28     0.36     598.83    -0.30
    10   0.0595  -6572.14    -0.10     599.19     0.04
    11   0.0595  -6572.69    -0.25     599.31     0.13
    12   0.0595  -6572.52     0.33     598.95    -0.26
    13   0.0595  -6573.39    -0.14     599.40     0.16
    14   0.0595  -6573.64     0.02     599.24    -0.03
    15   0.0595  -6574.16    -0.10     599.42     0.13
    16   0.0595  -6575.03    -0.17     599.51     0.16
    17   0.0595  -6575.13     0.14     599.47     0.10
    18   0.3085 -17801.68     0.04    -433.84     0.05
    19   0.3086 -17791.96    -0.13    -435.16    -0.02
    20   0.3087 -17781.84     0.09    -436.45    -0.03

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.

24RU155    quality flag:1

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        10.384    11.074     9.734
ecceobj         0.395     0.391     0.401
incobj          7.011     7.016     7.006
qmin            6.282     6.745     5.828
qmax           21.897    18.441    16.191
amean          13.106    12.217    10.295
amin           10.384    11.074     8.913
amax           14.766    12.741    11.367
emean           0.445     0.429     0.387
emin            0.395     0.391     0.318
emax            0.485     0.456     0.436
imean           9.175     6.827     6.347
imin            6.291     6.352     5.445
imax           11.958     8.304     8.287
excite_mean     0.474     0.446     0.403
fracstop        0.003     0.001     0.001
cjmean          3.482     3.610     4.013

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       222.9     212.4     184.0
kozaiamp        173.8      82.8     151.6