Orbit Fit and Astrometric record for 00PM30

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: 00PM30    
# Created Fri Apr 26 01:10:13 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:  20.13y
# First observation: 1999/07/20
#  Last observation: 2019/09/04
# Chi-squared of fit:    32.51 DOF:     38 RMS:  0.21
# Min/Max residuals:    -0.44    0.43
# Exact a, adot, b, bdot, g, gdot:
  1.527006E-05  2.072555E-02  1.151113E-06 -8.202128E-04  2.256291E-02  1.190052E-03
# Covariance matrix:
  3.7866E-13 -1.8824E-13 -9.8387E-15  7.6942E-15  2.1862E-13 -4.2966E-13
 -1.8824E-13  1.3190E-13  6.9004E-15 -5.4100E-15 -5.6938E-14  3.0182E-13
 -9.8387E-15  6.9004E-15  8.9200E-14 -7.0582E-15 -3.7825E-15  1.6078E-14
  7.6942E-15 -5.4100E-15 -7.0582E-15  2.2467E-15  2.8911E-15 -1.2601E-14
  2.1862E-13 -5.6938E-14 -3.7825E-15  2.8911E-15  5.5811E-13 -1.6285E-13
 -4.2966E-13  3.0182E-13  1.6078E-14 -1.2601E-14 -1.6285E-13  7.0310E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.265856  -43.248659    0.343302   -0.004660   -0.954016  2451380.033203
# Heliocentric elements and errors
Epoch:              2451380.5000  =  1999/07/21
Mean Anomaly:          115.50746 +/-     0.132
Argument of Peri:       65.75608 +/-     0.117
Long of Asc Node:      129.77509 +/-     0.001
Inclination:             2.27899 +/-     0.000
Eccentricity:         0.05271682 +/-    0.0000
Semi-Major Axis:     44.18103638 +/-    0.0061
Time of Perihelion: 2416964.5461 +/-      39.9
Perihelion:          41.85195282 +/-    0.0061
Aphelion:            46.51011993 +/-    0.0067
Period (y)              293.6717 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           32.75016972 +/-    0.0011
Ecliptic Y          -31.26835108 +/-    0.0010
Ecliptic Z           -0.20558285 +/-    0.0000
Ecliptic XDOT         0.00182452 +/-    0.0000
Ecliptic YDOT         0.00174171 +/-    0.0000
Ecliptic ZDOT        -0.00010015 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.28049191 +/-    0.0010
Geocenter to KBO     44.32051903 +/-    0.0015
# Hcoef:  7.91

The following table shows the complete astrometric record for 00PM30. 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 (00PM30) followed by the observatory code and reference code for the source of the astrometry.

1999 07  20.53246  21 17 09.07   -16 04 09.0   24.2R 00PM30    568  Cd4319      
1999 07  20.56054  21 17 08.94   -16 04 09.6   24.3R 00PM30    568  Cd4319      
1999 07  20.58760  21 17 08.84   -16 04 10.0   24.3R 00PM30    568  Cd4319      
2000 08  05.44974  21 20 43.50   -15 50 49.9         00PM30    568  Cb8005      
2000 08  05.49114  21 20 43.32   -15 50 51.0   24.2R 00PM30    568  Cb8005      
2000 08  05.53261  21 20 43.14   -15 50 51.7         00PM30    568  Cb8005      
2000 08  06.43790  21 20 39.11   -15 51 10.8   23.7R 00PM30    568  Cb8005      
2000 08  06.48026  21 20 38.94   -15 51 11.8   23.6R 00PM30    568  Cb8005      
2000 08  06.52202  21 20 38.75   -15 51 12.6         00PM30    568  Cb8005      
2000 09  23.27096  21 17 29.24   -16 05 59.1   24.0R 00PM30    568  Cb9232      
2000 09  23.31927  21 17 29.09   -16 05 59.8         00PM30    568  Cb9232      
2000 09  23.36754  21 17 28.93   -16 06 00.5         00PM30    568  Cb9232      
2001 07  25.52128  21 26 16.07   -15 27 41.8   23.9R 00PM30    568  Cd4319      
2001 07  25.55535  21 26 15.93   -15 27 42.7   24.1R 00PM30    568  Cd4319      
2001 07  25.59235  21 26 15.78   -15 27 43.2   24.0R 00PM30    568  Cd4319      
2001 08  11.31470  21 25 03.22   -15 33 36.0         00PM30    807  Cd4319      
2001 08  11.35089  21 25 03.06   -15 33 36.3         00PM30    807  Cd4319      
2002 07  06.37425  21 32 11.84   -15 01 56.3   24.3R 00PM30    695  Cf8836      
2002 07  06.41674  21 32 11.69   -15 01 57.3   24.5R 00PM30    695  Cf8836      
2002 07  06.45235  21 32 11.57   -15 01 57.5   24.4R 00PM30    695  Cf8836      
2019 09  04.227990 22 45 05.778  -09 09 56.65  24.2G 00PM30    G37  C~3cUl      
2019 09  04.300330 22 45 05.459  -09 09 58.28        00PM30    G37  C~3cUl      

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    -0.04       0.00    -0.39
     2   0.0001      0.00    -0.22       0.00    -0.44
     3   0.0002      0.00    -0.01       0.00    -0.32
     4   1.0456      0.00     0.25       0.00     0.37
     5   1.0457      0.00     0.34       0.00     0.13
     6   1.0459      0.00     0.43       0.00     0.30
     7   1.0483      0.00    -0.12       0.00     0.19
     8   1.0485      0.00     0.19       0.00     0.07
     9   1.0486      0.00     0.16       0.00     0.14
    10   1.1793      0.00    -0.00       0.00     0.11
    11   1.1794      0.00    -0.05       0.00     0.07
    12   1.1796      0.00    -0.25       0.00     0.03
    13   2.0150      0.00    -0.33       0.00     0.19
    14   2.0151      0.00    -0.25       0.00    -0.02
    15   2.0152      0.00    -0.14       0.00     0.23
    16   2.0610      0.00    -0.14       0.00    -0.36
    17   2.0611      0.00    -0.11       0.00     0.11
    18   2.9619      0.00     0.14       0.00    -0.08
    19   2.9620      0.00     0.07       0.00    -0.35
    20   2.9621      0.00     0.10       0.00     0.06
    21  20.1251      0.00     0.10       0.00    -0.12
    22  20.1253      0.00    -0.10       0.00     0.09

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.

00PM30    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        44.109    44.109    44.109
ecceobj         0.053     0.053     0.053
incobj          2.280     2.280     2.280
qmin           40.817    40.830    40.812
qmax           47.488    47.490    47.505
amean          44.068    44.068    44.068
amin           43.727    43.726    43.727
amax           44.436    44.431    44.428
emean           0.054     0.054     0.054
emin            0.038     0.038     0.038
emax            0.069     0.069     0.069
imean           1.495     1.495     1.495
imin            0.782     0.782     0.782
imax            2.169     2.168     2.168
excite_mean     0.061     0.061     0.061
fracstop        1.000     1.000     1.000
cjmean          3.098     3.098     3.098

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       187.6     187.5     187.5
kozaiamp        180.0     180.0     180.0