Orbit Fit and Astrometric record for 23FB55

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: 23FB55    
# Created Sun Nov 24 02:11:14 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   0.021829   0.000003  -0.000840   0.022841   0.000000
# Chi-squared of fit:     2.97 DOF:      6 RMS:  0.12
# Min/Max residuals:    -0.28    0.26
# Exact a, adot, b, bdot, g, gdot:
  1.531272E-05  2.180129E-02  7.708450E-07 -8.397295E-04  2.309590E-02  2.033277E-03
# Covariance matrix:
  7.5212E-13  1.5101E-11  6.1048E-14 -5.8198E-13  6.3700E-12  6.6591E-10
  1.5101E-11  1.6565E-08  5.6300E-11 -5.9362E-10  5.6472E-09  6.8655E-07
  6.1048E-14  5.6300E-11  6.2967E-13 -2.5294E-12  1.9223E-11  2.3341E-09
 -5.8198E-13 -5.9362E-10 -2.5294E-12  2.2646E-11 -2.0246E-10 -2.4606E-08
  6.3700E-12  5.6472E-09  1.9223E-11 -2.0246E-10  1.9290E-09  2.3413E-07
  6.6591E-10  6.8655E-07  2.3341E-09 -2.4606E-08  2.3413E-07  2.8458E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.413584  163.797007   -0.283131    0.023563   -0.963980  2460024.839821
# Heliocentric elements and errors
Epoch:              2460020.5000  =  2023/03/17
Mean Anomaly:           82.32319 +/-    33.403
Argument of Peri:       54.16135 +/-    11.134
Long of Asc Node:       16.03790 +/-     0.067
Inclination:             2.61766 +/-     0.005
Eccentricity:         0.10108514 +/-    0.2428
Semi-Major Axis:     44.40094025 +/-    2.2554
Time of Perihelion: 2435308.5865 +/-    9848.5
Perihelion:          39.91266514 +/-   10.9711
Aphelion:            48.88921536 +/-   11.0644
Period (y)              295.8669 +/-     22.54
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -42.56146911 +/-    0.0790
Ecliptic Y           12.07533476 +/-    0.0230
Ecliptic Z            1.06816486 +/-    0.0020
Ecliptic XDOT        -0.00095680 +/-    0.0006
Ecliptic YDOT        -0.00240510 +/-    0.0002
Ecliptic ZDOT        -0.00009359 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.25419007 +/-    0.0763
Geocenter to KBO     43.29773175 +/-    0.0823
# Hcoef:  6.27

The following table shows the complete astrometric record for 23FB55. 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 (23FB55) followed by the observatory code and reference code for the source of the astrometry.

2023 03  21.33902  11 02 28.813  +07 40 38.79  22.6r 23FB55    568  C~7xZo      
2023 03  21.54320  11 02 27.967  +07 40 44.30  22.6r 23FB55    568  C~7xZo      
2023 05  15.11417  10 59 52.289  +07 55 04.42  22.7r 23FB55    304  C~7xZo      
2023 05  16.09506  10 59 51.320  +07 55 07.81  22.7r 23FB55    304  C~7xZo      
2024 03  07.28002  11 07 59.142  +07 03 21.18  22.6r 23FB55    304  C~7xZo      
2024 03  08.27537  11 07 54.804  +07 03 47.69  22.7r 23FB55    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    -0.08       0.00    -0.28
     2   0.0006    -13.73     0.08       0.24     0.26
     3   0.1500  -2480.26     0.06     -95.92     0.09
     4   0.1527  -2494.85    -0.06     -98.32    -0.07
     5   0.9636   5398.27    -0.05    -162.31     0.04
     6   0.9663   5328.42     0.05    -162.95    -0.04

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.

23FB55    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