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 Sun Dec 22 02:11:26 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:  61.57d
# First observation: 2024/03/07
#  Last observation: 2024/05/08
Preliminary a, adot, b, bdot, g, gdot:
   0.000026   0.521095  -0.000068   0.275096   0.176058   0.000000
# Chi-squared of fit:    14.76 DOF:     36 RMS:  0.15
# Min/Max residuals:    -0.35    0.31
# Exact a, adot, b, bdot, g, gdot:
  4.635263E-05  5.021427E-01  2.487879E-05  2.643062E-01  1.697603E-01  5.905974E-02
# Covariance matrix:
  4.1900E-13 -2.6717E-11  1.3772E-14  3.4994E-12 -3.5857E-12  3.6915E-11
 -2.6717E-11  7.1700E-09 -2.7365E-11 -2.0457E-10  1.2420E-09  3.7276E-09
  1.3772E-14 -2.7365E-11  3.8920E-13 -2.9571E-12 -5.3329E-12 -5.2054E-11
  3.4994E-12 -2.0457E-10 -2.9571E-12  9.4168E-11 -1.5834E-11  1.1728E-09
 -3.5857E-12  1.2420E-09 -5.3329E-12 -1.5834E-11  2.2108E-10  1.0009E-09
  3.6915E-11  3.7276E-09 -5.2054E-11  1.1728E-09  1.0009E-09  2.4929E-08
#      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:          359.98732 +/-     0.001
Argument of Peri:       21.12249 +/-     0.032
Long of Asc Node:      187.30162 +/-     0.003
Inclination:            30.62141 +/-     0.004
Eccentricity:         0.89138814 +/-    0.0001
Semi-Major Axis:     60.96360506 +/-    0.0396
Time of Perihelion: 2460376.6248 +/-       0.4
Perihelion:           6.62137060 +/-    0.0063
Aphelion:           115.30583952 +/-    0.0750
Period (y)              476.0079 +/-      0.46
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           -5.86266879 +/-    0.0004
Ecliptic Y           -2.82622240 +/-    0.0003
Ecliptic Z            1.21825589 +/-    0.0001
Ecliptic XDOT         0.00422815 +/-    0.0000
Ecliptic YDOT        -0.00689740 +/-    0.0000
Ecliptic ZDOT         0.00436756 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO    6.62137190 +/-    0.0004
Geocenter to KBO      5.89066004 +/-    0.0005
# Hcoef: 13.47

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      

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    -0.05
     2   0.0000     -1.07     0.06       1.77     0.07
     3   0.0001     -7.14     0.13      11.49     0.09
     4   0.0323  -2206.83     0.02    2754.68    -0.25
     5   0.0323  -2210.16    -0.26    2757.87     0.04
     6   0.0324  -2213.15    -0.35    2760.39    -0.21
     7   0.0601  -4807.41    -0.01    4981.87    -0.04
     8   0.0602  -4818.49     0.06    4990.12     0.15
     9   0.0819  -7184.27     0.24    6602.58     0.17
    10   0.0822  -7217.86     0.02    6623.21     0.31
    11   0.0824  -7245.20    -0.15    6639.18    -0.09
    12   0.0956  -8776.60     0.09    7550.06    -0.01
    13   0.0959  -8813.11     0.17    7570.05    -0.05
    14   0.1633 -16710.32     0.15   11286.04     0.20
    15   0.1634 -16714.82     0.11   11287.65     0.14
    16   0.1634 -16719.54    -0.15   11288.96    -0.21
    17   0.1634 -16724.06    -0.21   11290.60    -0.25
    18   0.1685 -17259.16     0.04   11500.85    -0.13
    19   0.1685 -17262.44     0.04   11502.27     0.08
    20   0.1685 -17265.83    -0.04   11503.40     0.00
    21   0.1686 -17269.15    -0.06   11504.66     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.

24FV24    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        62.201    63.171    61.261
ecceobj         0.892     0.894     0.891
incobj         30.522    30.518    30.525
qmin            6.042    -8.339     6.474
qmax          629.883  ********   140.442
amean         146.084  3888.949    59.507
amin           52.383    59.699    42.368
amax          318.333  ********    73.911
emean           0.941     0.992     0.883
emin            0.842     0.886     0.846
emax            0.980     1.004     0.903
imean          32.453    39.772    33.136
imin           29.066    12.176    30.241
imax           38.804   161.765    36.650
excite_mean     1.083     1.140     1.038
fracstop        0.114     0.237     0.033
cjmean          1.391     0.000     1.620

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        37.7      29.3      41.5
kozaiamp         14.8      35.7      14.9