Orbit Fit and Astrometric record for 23FY54

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: 23FY54    
# Created Wed Dec 25 02:11:20 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:   0.97y
# First observation: 2023/03/21
#  Last observation: 2024/03/08
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.013927  -0.000001   0.001139   0.017470   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     0.86 DOF:      7 RMS:  0.07
# Min/Max residuals:    -0.13    0.11
# Exact a, adot, b, bdot, g, gdot:
  1.260807E-05  1.397381E-02  5.072084E-07  1.143927E-03  1.768302E-02  6.876151E-03
# Covariance matrix:
  7.4498E-13  5.2416E-12 -3.2094E-14  4.6689E-13  3.8666E-12  4.0232E-10
  5.2416E-12  4.5733E-09 -2.2002E-11  3.4037E-10  2.0049E-09  2.9458E-07
 -3.2094E-14 -2.2002E-11  5.4662E-13 -2.1546E-12 -9.6683E-12 -1.4181E-09
  4.6689E-13  3.4037E-10 -2.1546E-12  2.6728E-11  1.4944E-10  2.1936E-08
  3.8666E-12  2.0049E-09 -9.6683E-12  1.4944E-10  8.8526E-10  1.2932E-07
  4.0232E-10  2.9458E-07 -1.4181E-09  2.1936E-08  1.2932E-07  1.8984E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.290501  150.872839   -0.490068   -0.004667   -0.877319  2460024.738791
# Heliocentric elements and errors
Epoch:              2460020.5000  =  2023/03/17
Mean Anomaly:           48.01609 +/-    27.595
Argument of Peri:      254.28346 +/-     7.268
Long of Asc Node:      154.82199 +/-     0.007
Inclination:             4.72322 +/-     0.010
Eccentricity:         0.46590651 +/-    0.2746
Semi-Major Axis:     66.09915399 +/-   21.4562
Time of Perihelion: 2433840.0830 +/-    7992.6
Perihelion:          35.30312788 +/-   21.4665
Aphelion:            96.89518009 +/-   36.3148
Period (y)              537.4054 +/-    261.67
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -50.39573298 +/-    0.0831
Ecliptic Y           27.52496563 +/-    0.0463
Ecliptic Z           -0.28669141 +/-    0.0005
Ecliptic XDOT        -0.00198579 +/-    0.0006
Ecliptic YDOT        -0.00136261 +/-    0.0003
Ecliptic ZDOT         0.00017169 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   57.42330387 +/-    0.0762
Geocenter to KBO     56.55144214 +/-    0.0952
# Hcoef:  7.52

The following table shows the complete astrometric record for 23FY54. 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 (23FY54) followed by the observatory code and reference code for the source of the astrometry.

2023 03  21.23799  10 11 16.217  +10 53 32.30  25.0r 23FY54    568  C~7xZo      
2023 03  21.43473  10 11 15.612  +10 53 35.53  25.1r 23FY54    568  C~7xZo      
2023 05  15.97864  10 09 46.184  +11 02 45.54  25.1r 23FY54    304  C~7xZo      
2023 05  18.98344  10 09 46.674  +11 02 45.74  24.9r 23FY54    304  C~7xZo      
2024 03  07.23577  10 15 05.440  +10 36 08.62  25.1r 23FY54    304  C~7xZo      
2024 03  08.22684  10 15 02.135  +10 36 28.09  25.2r 23FY54    304  C~7xZo      

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    -0.02       0.00     0.11
     2   0.0005     -9.48     0.02      -0.13    -0.13
     3   0.1526  -1435.80     0.03      49.20     0.04
     4   0.1608  -1429.12    -0.03      51.93    -0.02
     5   0.9637   3528.78    -0.08     224.69    -0.05
     6   0.9664   3476.30     0.08     225.50     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.

23FY54    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0