Orbit Fit and Astrometric record for 24FV24

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: 24FV24    
# Created Wed Jun 11 01:13:44 2025
# Orbit generated from Bernstein formalism
# Fitting     23 observations of     23
# Arc:   1.22y
# First observation: 2024/03/07
#  Last observation: 2025/05/27
Preliminary a, adot, b, bdot, g, gdot:
   0.000023   0.522496   0.000003   0.274204   0.176302   0.000000
# Chi-squared of fit:    15.73 DOF:     40 RMS:  0.15
# Min/Max residuals:    -0.35    0.28
# Exact a, adot, b, bdot, g, gdot:
  4.634549E-05  5.021667E-01  2.473982E-05  2.643074E-01  1.697650E-01  5.911018E-02
# Covariance matrix:
  2.0637E-13 -6.1148E-14 -2.5596E-15 -1.1729E-13  2.4089E-13 -3.1249E-13
 -6.1148E-14  4.1513E-11 -2.6438E-12  2.7929E-11  8.1300E-12  7.9434E-11
 -2.5596E-15 -2.6438E-12  2.5218E-13 -1.9124E-12 -5.2370E-13 -5.1284E-12
 -1.1729E-13  2.7929E-11 -1.9124E-12  1.9771E-11  5.2646E-12  5.4645E-11
  2.4089E-13  8.1300E-12 -5.2370E-13  5.2646E-12  2.0425E-12  1.5013E-11
 -3.1249E-13  7.9434E-11 -5.1284E-12  5.4645E-11  1.5013E-11  1.5535E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
   11.933930 -148.126328    0.697150    0.147831   -0.700555  2460377.280974
# Heliocentric elements and errors
Epoch:              2460370.5000  =  2024/03/01
Mean Anomaly:          359.98758 +/-     0.000
Argument of Peri:       21.11328 +/-     0.002
Long of Asc Node:      187.30073 +/-     0.000
Inclination:            30.62034 +/-     0.000
Eccentricity:         0.89141406 +/-    0.0000
Semi-Major Axis:     60.97664714 +/-    0.0168
Time of Perihelion: 2460376.5013 +/-       0.0
Perihelion:           6.62120641 +/-    0.0026
Aphelion:           115.33208786 +/-    0.0319
Period (y)              476.1607 +/-      0.20
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           -5.86253217 +/-    0.0000
Ecliptic Y           -2.82613740 +/-    0.0000
Ecliptic Z            1.21822105 +/-    0.0000
Ecliptic XDOT         0.00422757 +/-    0.0000
Ecliptic YDOT        -0.00689796 +/-    0.0000
Ecliptic ZDOT         0.00436762 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO    6.62120824 +/-    0.0000
Geocenter to KBO      5.89049541 +/-    0.0000
# Hcoef: 13.49

The following table shows the complete astrometric record for 24FV24. 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 (24FV24) followed by the observatory code and reference code for the source of the astrometry.

2024 03  07.780173 14 15 12.515  -00 54 16.12  22.1r 24FV24    O18  C~892S      
2024 03  07.787152 14 15 12.488  -00 54 14.09  22.0r 24FV24    O18  C~892S      
2024 03  07.828217 14 15 12.326  -00 54 02.89  22.3g 24FV24    O18  C~892S      
2024 03  19.578774 14 13 56.097  +00 01 21.86  21.8w 24FV24    F51  C~892S      
2024 03  19.591699 14 13 55.960  +00 01 25.98  21.8w 24FV24    F51  C~892S      
2024 03  19.604065 14 13 55.829  +00 01 29.37  21.9w 24FV24    F51  C~892S      
2024 03  29.722361 14 12 03.150  +00 50 54.71  21.4r 24FV24    O18  C~89Xl      
2024 03  29.760914 14 12 02.641  +00 51 06.20  21.2r 24FV24    O18  C~89Xl      
2024 04  06.688344 14 10 10.643  +01 29 39.04  22.4g 24FV24    O18  C~892S      
2024 04  06.793888 14 10 09.002  +01 30 09.73  21.3r 24FV24    O18  C~892S      
2024 04  06.878993 14 10 07.648  +01 30 33.94  21.0r 24FV24    O18  C~892S      
2024 04  11.690949 14 08 52.201  +01 53 24.52  21.5r 24FV24    O18  C~892S      
2024 04  11.801620 14 08 50.364  +01 53 55.55  22.4g 24FV24    O18  C~892S      
2024 05  06.431547 14 01 59.954  +03 35 56.66  21.9w 24FV24    F51  C~892S      
2024 05  06.446260 14 01 59.709  +03 35 59.66  21.6w 24FV24    F51  C~892S      
2024 05  06.460951 14 01 59.444  +03 36 02.45  21.8w 24FV24    F51  C~892S      
2024 05  06.475672 14 01 59.198  +03 36 05.48  21.6w 24FV24    F51  C~892S      
2024 05  08.316355 14 01 30.513  +03 42 19.50  21.9w 24FV24    F51  C~892S      
2024 05  08.327444 14 01 30.340  +03 42 21.91  21.9w 24FV24    F51  C~892S      
2024 05  08.338618 14 01 30.154  +03 42 24.09  22.0w 24FV24    F51  C~892S      
2024 05  08.349789 14 01 29.975  +03 42 26.37  21.9w 24FV24    F51  C~892S      
2025 05  27.36373  16 02 00.300  +08 17 34.68  22.2G 24FV24    G37              
2025 05  27.40236  16 01 59.568  +08 17 38.78        24FV24    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     0.09       0.00    -0.03
     2   0.0000     -1.07     0.06       1.77     0.10
     3   0.0001     -7.14     0.13      11.49     0.12
     4   0.0323  -2206.83     0.01    2754.68    -0.25
     5   0.0323  -2210.16    -0.27    2757.87     0.03
     6   0.0324  -2213.15    -0.35    2760.39    -0.21
     7   0.0601  -4807.41    -0.01    4981.87    -0.06
     8   0.0602  -4818.49     0.06    4990.12     0.13
     9   0.0819  -7184.27     0.24    6602.58     0.14
    10   0.0822  -7217.86     0.02    6623.21     0.28
    11   0.0824  -7245.20    -0.14    6639.18    -0.12
    12   0.0956  -8776.60     0.10    7550.06    -0.04
    13   0.0959  -8813.11     0.18    7570.05    -0.08
    14   0.1633 -16710.32     0.15   11286.04     0.21
    15   0.1634 -16714.82     0.11   11287.65     0.15
    16   0.1634 -16719.54    -0.15   11288.96    -0.20
    17   0.1634 -16724.06    -0.21   11290.60    -0.24
    18   0.1685 -17259.16     0.04   11500.85    -0.11
    19   0.1685 -17262.44     0.04   11502.27     0.10
    20   0.1685 -17265.83    -0.05   11503.40     0.02
    21   0.1686 -17269.15    -0.06   11504.66     0.07
    22   1.2199  85399.65     0.12   69970.21     0.10
    23   1.2200  85385.41    -0.12   69969.15    -0.10

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.

24FV24    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        62.215    62.296    62.134
ecceobj         0.892     0.892     0.892
incobj         30.521    30.521    30.521
qmin            6.472     6.538    -8.366
qmax          160.751   117.890  ********
amean          59.610    27.564  1698.814
amin           37.120    22.846    62.134
amax           83.762    62.296  5952.814
emean           0.878     0.722     0.988
emin            0.817     0.644     0.892
emax            0.919     0.892     1.009
imean          33.405    34.679    33.516
imin           30.026    30.047    16.810
imax           37.120    38.699   139.965
excite_mean     1.036     0.921     1.127
fracstop        0.036     0.026     0.213
cjmean          1.637     2.197     0.000

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        34.7      40.7      33.9
kozaiamp         12.0      14.1      27.9