Orbit Fit and Astrometric record for 00PL30

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: 00PL30    
# Created Thu Apr 25 01:10:10 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     21 observations of     21
# Arc:  23.09y
# First observation: 2000/08/05
#  Last observation: 2023/09/06
# Chi-squared of fit:   189.66 DOF:     36 RMS:  0.53
# Min/Max residuals:    -1.57    0.82
# Exact a, adot, b, bdot, g, gdot:
  1.040803E-05  1.629064E-02 -1.001031E-08  1.656768E-03  2.054813E-02 -2.548616E-03
# Covariance matrix:
  1.3952E-13 -3.0458E-14  1.9052E-15 -2.8710E-15  1.2441E-13 -6.9963E-14
 -3.0458E-14  3.1827E-14 -2.3062E-15  3.3101E-15 -2.4545E-14  8.0211E-14
  1.9052E-15 -2.3062E-15  1.0412E-13 -5.3838E-15  2.0362E-15 -5.9458E-15
 -2.8710E-15  3.3101E-15 -5.3838E-15  1.0163E-15 -3.8725E-15  8.5777E-15
  1.2441E-13 -2.4545E-14  2.0362E-15 -3.8725E-15  7.4705E-13 -9.6568E-14
 -6.9963E-14  8.0211E-14 -5.9458E-15  8.5777E-15 -9.6568E-14  2.0798E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.778244  -41.290754    0.102450   -0.013897   -1.008249  2451761.943623
# Heliocentric elements and errors
Epoch:              2451762.5000  =  2000/08/06
Mean Anomaly:          229.95846 +/-     0.033
Argument of Peri:      139.90292 +/-     0.016
Long of Asc Node:      326.04711 +/-     0.000
Inclination:             5.86177 +/-     0.000
Eccentricity:         0.23955994 +/-    0.0001
Semi-Major Axis:     42.06594380 +/-    0.0054
Time of Perihelion: 2487760.1359 +/-      15.4
Perihelion:          31.98862897 +/-    0.0055
Aphelion:            52.14325863 +/-    0.0076
Period (y)              272.8376 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           37.25913807 +/-    0.0015
Ecliptic Y          -32.84869861 +/-    0.0014
Ecliptic Z           -0.66098782 +/-    0.0000
Ecliptic XDOT         0.00117229 +/-    0.0000
Ecliptic YDOT         0.00185851 +/-    0.0000
Ecliptic ZDOT         0.00022549 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   49.67622266 +/-    0.0015
Geocenter to KBO     48.66635538 +/-    0.0020
# Hcoef:  7.32

The following table shows the complete astrometric record for 00PL30. 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 (00PL30) followed by the observatory code and reference code for the source of the astrometry.

2000 08  05.44288  21 25 33.61   -15 57 26.7         00PL30    568  Cb8005      
2000 08  05.48448  21 25 33.45   -15 57 27.4         00PL30    568  Cb8005      
2000 08  05.52555  21 25 33.27   -15 57 28.3   23.4R 00PL30    568  Cb8005      
2000 08  06.43095  21 25 29.53   -15 57 45.2         00PL30    568  Cb8005      
2000 08  06.47320  21 25 29.35   -15 57 46.0   23.7R 00PL30    568  Cb8005      
2000 08  06.51483  21 25 29.17   -15 57 46.8         00PL30    568  Cb8005      
2000 09  24.27180  21 22 26.20   -16 10 59.6   24.5R 00PL30    568  Cd2824      
2000 09  24.32190  21 22 26.06   -16 11 00.1   24.4R 00PL30    568  Cd2824      
2000 09  24.38171  21 22 25.88   -16 11 01.0   24.3R 00PL30    568  Cd2824      
2001 08  12.54968  21 28 39.09   -15 36 38.7         00PL30    568  Cd2824      
2001 08  12.58664  21 28 38.91   -15 36 39.5         00PL30    568  Cd2824      
2001 08  13.40598  21 28 35.55   -15 36 54.4         00PL30    568  Cd2824      
2001 08  13.44202  21 28 35.39   -15 36 54.6         00PL30    568  Cd2824      
2003 07  08.45504  21 38 03.21   -14 39 05.6   24.0R 00PL30    568  Ci2628      
2003 07  09.50134  21 37 59.84   -14 39 21.5         00PL30    568  Ci2628      
2019 09  04.220010 22 33 03.593  -07 53 03.35  23.3G 00PL30    G37  C~3cUl      
2019 09  04.292170 22 33 03.293  -07 53 05.06        00PL30    G37  C~3cUl      
2019 09  04.339690 22 33 03.100  -07 53 06.22        00PL30    G37  C~3cUl      
2023 09  06.271050 22 48 22.356  -05 53 12.86  23.4G 00PL30    G37  C~7ALU      
2023 09  06.307600 22 48 22.205  -05 53 13.35        00PL30    G37  C~7ALU      
2023 09  06.344290 22 48 22.049  -05 53 14.34        00PL30    G37  C~7ALU      

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     0.35       0.00     0.39
     2   0.0001      0.00     0.57       0.00     0.46
     3   0.0002      0.00     0.46       0.00     0.32
     4   0.0027      0.00     0.44       0.00     0.27
     5   0.0028      0.00     0.41       0.00     0.25
     6   0.0029      0.00     0.34       0.00     0.22
     7   0.1364      0.00     0.28       0.00     0.08
     8   0.1366      0.00     0.36       0.00     0.16
     9   0.1367      0.00     0.27       0.00    -0.06
    10   1.0188      0.00    -1.20       0.00    -0.67
    11   1.0189      0.00    -1.57       0.00    -0.78
    12   1.0211      0.00    -1.07       0.00    -0.22
    13   1.0212      0.00    -1.18       0.00     0.26
    14   2.9213      0.00     0.69       0.00    -0.56
    15   2.9242      0.00     0.82       0.00    -0.34
    16  19.0795      0.00     0.07       0.00     0.13
    17  19.0797      0.00     0.15       0.00     0.13
    18  19.0798      0.00     0.27       0.00     0.09
    19  23.0851      0.00    -0.19       0.00    -0.29
    20  23.0852      0.00    -0.12       0.00     0.12
    21  23.0853      0.00    -0.10       0.00     0.03

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.

00PL30    quality flag:3

Type:          5:3EE     5:3EE     5:3EE

axisobj        42.133    42.133    42.133
ecceobj         0.238     0.238     0.238
incobj          5.853     5.853     5.853
qmin           31.519    31.568    31.502
qmax           54.023    54.017    54.026
amean          42.328    42.328    42.328
amin           41.740    41.704    41.739
amax           42.995    43.044    43.018
emean           0.240     0.239     0.241
emin            0.221     0.225     0.226
emax            0.257     0.256     0.258
imean           7.093     6.110     7.002
imin            5.628     4.034     5.649
imax            8.195     8.201     8.190
excite_mean     0.270     0.263     0.271
fracstop        1.000     1.000     1.000
cjmean          2.994     3.000     2.994

libcent 0       179.9     180.8     178.9
libamp  0       141.6     151.3     144.9
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       188.4     188.3     187.4
kozaiamp        180.0     179.9     179.9