Orbit Fit and Astrometric record for 22UD146

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: 22UD146   
# Created Fri May  3 01:19:03 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:   0.94y
# First observation: 2022/10/29
#  Last observation: 2023/10/07
Preliminary a, adot, b, bdot, g, gdot:
   0.000000   0.012953   0.000001  -0.001681   0.017759   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     0.35 DOF:      7 RMS:  0.04
# Min/Max residuals:    -0.05    0.05
# Exact a, adot, b, bdot, g, gdot:
  1.157187E-05  1.287164E-02 -1.416620E-06 -1.675384E-03  1.780978E-02 -2.761737E-03
# Covariance matrix:
  7.6886E-13  2.5950E-11  8.5705E-14 -2.5784E-12  8.4058E-12  1.5834E-09
  2.5950E-11  2.3705E-08  7.5454E-11 -2.2382E-09  6.0898E-09  1.3737E-06
  8.5705E-14  7.5454E-11  6.4363E-13 -7.5892E-12  1.9393E-11  4.3731E-09
 -2.5784E-12 -2.2382E-09 -7.5892E-12  2.1272E-10 -5.7543E-10 -1.2972E-07
  8.4058E-12  6.0898E-09  1.9393E-11 -5.7543E-10  1.5724E-09  3.5318E-07
  1.5834E-09  1.3737E-06  4.3731E-09 -1.2972E-07  3.5318E-07  7.9620E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.398572   22.611523   -0.225959   -0.006871   -0.960214  2459881.783171
# Heliocentric elements and errors
Epoch:              2459880.5000  =  2022/10/28
Mean Anomaly:          237.45641 +/-   102.071
Argument of Peri:      327.47245 +/-    88.765
Long of Asc Node:      199.81069 +/-     0.003
Inclination:             7.38774 +/-     0.005
Eccentricity:         0.27510681 +/-    0.3162
Semi-Major Axis:     47.96776129 +/-    8.5652
Time of Perihelion: 2501186.2674 +/-   32577.7
Perihelion:          34.77150368 +/-   16.3872
Aphelion:            61.16401890 +/-   18.6887
Period (y)              332.2251 +/-     88.98
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           52.64006290 +/-    0.1154
Ecliptic Y           22.16538605 +/-    0.0481
Ecliptic Z           -0.39068488 +/-    0.0009
Ecliptic XDOT        -0.00115449 +/-    0.0013
Ecliptic YDOT         0.00167177 +/-    0.0005
Ecliptic ZDOT        -0.00025466 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   57.11771350 +/-    0.1080
Geocenter to KBO     56.14893152 +/-    0.1250
# Hcoef:  7.11

The following table shows the complete astrometric record for 22UD146. 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 (22UD146) followed by the observatory code and reference code for the source of the astrometry.

2022 10  29.28237  01 24 15.106  +08 25 37.73  24.5r 22UD146   568  C~7Bop      
2022 10  29.48932  01 24 14.395  +08 25 33.47  24.5r 22UD146   568  C~7Bop      
2022 11  28.09295  01 22 46.295  +08 16 26.81  24.7r 22UD146   304  C~7Bop      
2022 11  29.04771  01 22 44.026  +08 16 12.59  24.6r 22UD146   304  C~7Bop      
2023 10  06.26243  01 28 32.074  +08 45 05.67  24.5r 22UD146   304  C~7Bop      
2023 10  07.17295  01 28 28.956  +08 44 46.39  24.7r 22UD146   304  C~7Bop      

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    -0.03       0.00    -0.01
     2   0.0006    -11.38     0.03      -0.04     0.05
     3   0.0816  -1428.41    -0.01     -21.62     0.01
     4   0.0842  -1464.96     0.01     -22.28    -0.05
     5   0.9363   3973.46    -0.01    -324.82    -0.04
     6   0.9388   3923.37     0.01    -325.71     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.

22UD146    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