Orbit Fit and Astrometric record for 02PE153

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: 02PE153   
# Created Tue Apr 23 01:10:47 2024
# Orbit generated from Bernstein formalism
# Fitting      5 observations of      5
# Arc:   2.33d
# First observation: 2002/08/13
#  Last observation: 2002/08/15
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit:     1.63 DOF:      6 RMS:  0.10
# Min/Max residuals:    -0.15    0.19
# Exact a, adot, b, bdot, g, gdot:
  1.618652E-05  2.414594E-02  8.254281E-08  3.814501E-04  2.468784E-02  0.000000E+00
# Covariance matrix:
  3.4664E-11  5.2582E-08  1.4077E-15  1.2137E-11  8.6855E-09  0.0000E+00
  5.2582E-08  8.1615E-05  2.1890E-12  1.8788E-08  1.3447E-05  0.0000E+00
  1.4077E-15  2.1890E-12  6.2943E-13 -1.1074E-10  3.6054E-13  0.0000E+00
  1.2137E-11  1.8788E-08 -1.1074E-10  3.6550E-08  3.0969E-09  0.0000E+00
  8.6855E-09  1.3447E-05  3.6054E-13  3.0969E-09  2.2165E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  1.9800E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.118858  -50.304091   -0.179504    0.002046   -1.000865  2452499.518433
# Heliocentric elements and errors
Epoch:              2452490.5000  =  2002/08/04
Mean Anomaly:           86.48693 +/-    34.796
Argument of Peri:      280.35010 +/-   107.496
Long of Asc Node:      302.69875 +/-     4.440
Inclination:             0.91910 +/-     0.561
Eccentricity:         0.00332876 +/-    0.5843
Semi-Major Axis:     41.51072945 +/-   21.2485
Time of Perihelion: 2429021.9126 +/- 2646943.1
Perihelion:          41.37255034 +/-   32.1983
Aphelion:            41.64890856 +/-   32.2915
Period (y)              267.4538 +/-    205.36
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           26.64908227 +/-    1.5600
Ecliptic Y          -31.81669098 +/-    1.8796
Ecliptic Z            0.08402743 +/-    0.0051
Ecliptic XDOT         0.00205258 +/-    0.0012
Ecliptic YDOT         0.00170774 +/-    0.0013
Ecliptic ZDOT         0.00004251 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.50280076 +/-    1.7549
Geocenter to KBO     40.50576663 +/-    2.4427
# Hcoef:  6.50

The following table shows the complete astrometric record for 02PE153. 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 (02PE153) followed by the observatory code and reference code for the source of the astrometry.

2002 08  13.01769  20 48 24.97   -17 42 28.3         02PE153   807  Cg3360      
2002 08  13.17629  20 48 24.22   -17 42 31.3         02PE153   807  Cg3360      
2002 08  15.04597  20 48 15.25   -17 43 06.3         02PE153   807  Cg3360      
2002 08  15.20558  20 48 14.49   -17 43 09.3   22.3R 02PE153   807  Cg3360      
2002 08  15.34750  20 48 13.81   -17 43 12.0         02PE153   807  Cg3360      

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    -0.15       0.00     0.03
     2   0.0004    -11.13     0.19      -0.03    -0.05
     3   0.0056   -143.99    -0.14       0.40     0.08
     4   0.0060   -155.26     0.04       0.40     0.02
     5   0.0064   -165.34     0.08       0.39    -0.08

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.

02PE153    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