Orbit Fit and Astrometric record for 22UY172

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: 22UY172   
# Created Tue Sep  2 01:12:13 2025
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:  21.77d
# First observation: 2022/10/29
#  Last observation: 2022/11/20
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.014826   0.000000  -0.003583   0.016842   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     2.55 DOF:      7 RMS:  0.12
# Min/Max residuals:    -0.15    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.157423E-05  1.245660E-02 -3.171430E-06 -3.757454E-03  1.644878E-02 -4.082850E-03
# Covariance matrix:
  1.9936E-12  1.1511E-09  3.6907E-14  8.0026E-11  2.1031E-10 -1.1540E-09
  1.1511E-09  1.0494E-06  3.2957E-11  7.2199E-08  1.8912E-07 -1.4729E-06
  3.6907E-14  3.2957E-11  6.9909E-13 -1.1054E-11  5.9811E-12  5.0149E-12
  8.0026E-11  7.2199E-08 -1.1054E-11  5.3659E-09  1.3002E-08 -1.2110E-07
  2.1031E-10  1.8912E-07  5.9811E-12  1.3002E-08  3.4142E-08 -2.0596E-07
 -1.1540E-09 -1.4729E-06  5.0149E-12 -1.2110E-07 -2.0596E-07  7.9623E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
    7.191915   17.670451   -0.307407    0.117157   -0.929995  2459881.757931
# Heliocentric elements and errors
Epoch:              2459880.5000  =  2022/10/28
Mean Anomaly:          302.35137 +/-    60.632
Argument of Peri:      248.73815 +/-    24.918
Long of Asc Node:      220.20253 +/-     2.013
Inclination:            18.16654 +/-     1.458
Eccentricity:         0.30252893 +/-    0.6767
Semi-Major Axis:     67.22495481 +/-   32.7743
Time of Perihelion: 2492119.4372 +/-   24369.8
Perihelion:          46.88746144 +/-   50.9134
Aphelion:            87.56244817 +/-   62.3861
Period (y)              551.1934 +/-    403.09
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           58.27935160 +/-    0.6456
Ecliptic Y           18.88600305 +/-    0.2056
Ecliptic Z            7.61089434 +/-    0.0855
Ecliptic XDOT        -0.00119731 +/-    0.0014
Ecliptic YDOT         0.00180371 +/-    0.0004
Ecliptic ZDOT        -0.00070565 +/-    0.0002
# Distances at JD0 (AU)
Heliocenter to KBO   61.73402342 +/-    0.6128
Geocenter to KBO     60.79479845 +/-    0.6829
# Hcoef:  7.20

The following table shows the complete astrometric record for 22UY172. 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 (22UY172) followed by the observatory code and reference code for the source of the astrometry.

2022 10  29.25713  00 53 53.842  +13 34 16.54  24.8r 22UY172   T09  C~90JZ      
2022 10  29.46481  00 53 53.204  +13 34 11.80  25.0r 22UY172   T09  C~90JZ      
2022 11  15.24420  00 53 07.999  +13 27 52.79        22UY172   G37  C~90JZ      
2022 11  15.25144  00 53 08.003  +13 27 52.55        22UY172   G37  C~90JZ      
2022 11  19.02517  00 52 59.242  +13 26 31.24  25.1r 22UY172   269  C~90JZ      
2022 11  20.02792  00 52 57.027  +13 26 10.18  25.2r 22UY172   269  C~90JZ      

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    -0.09
     2   0.0006    -10.41    -0.09      -0.74     0.04
     3   0.0465   -765.34    -0.09     -92.40     0.23
     4   0.0465   -765.38     0.17     -92.64     0.03
     5   0.0569   -914.80    -0.11    -117.56    -0.15
     6   0.0596   -952.78     0.05    -124.32    -0.07

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.

22UY172    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