Orbit Fit and Astrometric record for 23PL5

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: 23PL5     
# Created Sun Apr 27 01:11:33 2025
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:  54.68d
# First observation: 2023/08/13
#  Last observation: 2023/10/07
Preliminary a, adot, b, bdot, g, gdot:
  -0.000001   0.028210  -0.000004  -0.002695   0.025258   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     0.61 DOF:      7 RMS:  0.06
# Min/Max residuals:    -0.10    0.10
# Exact a, adot, b, bdot, g, gdot:
  1.559975E-05  2.474250E-02 -2.162008E-06 -3.094272E-03  2.471889E-02 -2.254552E-03
# Covariance matrix:
  7.7096E-13  4.5568E-11 -3.7892E-14  5.6047E-12  8.6290E-12 -1.2637E-09
  4.5568E-11  6.5841E-08 -6.3396E-11  7.9295E-09  8.8867E-09 -2.4931E-06
 -3.7892E-14 -6.3396E-11  7.1355E-13 -1.2907E-11 -8.3237E-12  2.4930E-09
  5.6047E-12  7.9295E-09 -1.2907E-11  1.0263E-09  1.0601E-09 -3.0476E-07
  8.6290E-12  8.8867E-09 -8.3237E-12  1.0601E-09  1.2395E-09 -3.2237E-07
 -1.2637E-09 -2.4931E-06  2.4930E-09 -3.0476E-07 -3.2237E-07  9.9888E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
    5.313762  -58.502613   -0.313672    0.088442   -0.953814  2460169.838551
# Heliocentric elements and errors
Epoch:              2460160.5000  =  2023/08/04
Mean Anomaly:          317.33643 +/-    81.005
Argument of Peri:      196.46839 +/-   120.019
Long of Asc Node:      157.72449 +/-     0.455
Inclination:             8.83147 +/-     0.096
Eccentricity:         0.11514937 +/-    0.3551
Semi-Major Axis:     44.90659793 +/-    4.6564
Time of Perihelion: 2473186.7187 +/-   24649.8
Perihelion:          39.73563126 +/-   16.4698
Aphelion:            50.07756461 +/-   16.7702
Period (y)              300.9355 +/-     46.81
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           21.82224574 +/-    0.0300
Ecliptic Y          -34.99693289 +/-    0.0489
Ecliptic Z            3.74648624 +/-    0.0053
Ecliptic XDOT         0.00221998 +/-    0.0006
Ecliptic YDOT         0.00162488 +/-    0.0010
Ecliptic ZDOT        -0.00036436 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   41.41294339 +/-    0.0443
Geocenter to KBO     40.45489714 +/-    0.0576
# Hcoef:  6.97

The following table shows the complete astrometric record for 23PL5. 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 (23PL5) followed by the observatory code and reference code for the source of the astrometry.

2023 08  13.33775  20 10 06.056  -14 38 24.00  23.1r 23PL5     T09  C~8nlW      
2023 08  13.47621  20 10 05.416  -14 38 26.69  23.1r 23PL5     T09  C~8nlW      
2023 09  14.00609  20 08 08.966  -14 47 56.59  23.3r 23PL5     269  C~8nlW      
2023 09  15.01136  20 08 06.320  -14 48 12.96  23.2r 23PL5     269  C~8nlW      
2023 10  06.02489  20 07 31.163  -14 53 08.65  23.0r 23PL5     269  C~8nlW      
2023 10  07.01658  20 07 30.518  -14 53 19.97  23.0r 23PL5     269  C~8nlW      

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     0.05       0.00     0.04
     2   0.0004     -9.65    -0.05      -0.63    -0.03
     3   0.0867  -1781.88     0.07    -196.28    -0.03
     4   0.0895  -1822.86    -0.06    -204.11     0.02
     5   0.1470  -2383.83    -0.10    -384.85    -0.01
     6   0.1497  -2395.37     0.10    -393.93     0.01

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.

23PL5    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