Orbit Fit and Astrometric record for 19CM32

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: 19CM32    
# Created Wed Dec 25 02:11:00 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:  15.21y
# First observation: 2003/12/23
#  Last observation: 2019/03/08
# Chi-squared of fit:     8.66 DOF:     38 RMS:  0.11
# Min/Max residuals:    -0.20    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.496999E-05  2.355314E-02  3.693864E-07  9.165986E-04  2.407941E-02  5.285019E-04
# Covariance matrix:
  4.8956E-13 -6.4953E-14  8.7024E-17 -1.2583E-15 -3.1949E-14 -8.8231E-14
 -6.4953E-14  1.7296E-12 -3.9945E-15  6.4588E-14  2.6516E-12  4.5784E-12
  8.7024E-17 -3.9945E-15  4.8748E-13 -3.2763E-14 -5.9867E-15 -1.0610E-14
 -1.2583E-15  6.4588E-14 -3.2763E-14  4.9031E-15  9.8580E-14  1.7130E-13
 -3.1949E-14  2.6516E-12 -5.9867E-15  9.8580E-14  4.2826E-12  6.9994E-12
 -8.8231E-14  4.5784E-12 -1.0610E-14  1.7130E-13  6.9994E-12  1.2141E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.433803  156.297365    0.891143    0.003169   -0.409533  2452996.991773
# Heliocentric elements and errors
Epoch:              2452996.5000  =  2003/12/23
Mean Anomaly:            3.66635 +/-     0.346
Argument of Peri:        7.02939 +/-     0.364
Long of Asc Node:      144.20416 +/-     0.002
Inclination:             2.27498 +/-     0.000
Eccentricity:         0.02459603 +/-    0.0001
Semi-Major Axis:     43.00809279 +/-    0.0101
Time of Perihelion: 2451947.3077 +/-      99.1
Perihelion:          41.95026452 +/-    0.0115
Aphelion:            44.06592106 +/-    0.0120
Period (y)              282.0548 +/-      0.10
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.04533985 +/-    0.0033
Ecliptic Y           17.67679372 +/-    0.0014
Ecliptic Z            0.31443377 +/-    0.0000
Ecliptic XDOT        -0.00113508 +/-    0.0000
Ecliptic YDOT        -0.00243459 +/-    0.0000
Ecliptic ZDOT         0.00010482 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.95254106 +/-    0.0030
Geocenter to KBO     41.52926656 +/-    0.0036
# Hcoef:  8.03

The following table shows the complete astrometric record for 19CM32. 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 (19CM32) followed by the observatory code and reference code for the source of the astrometry.

2003 12  23.49103  10 32 53.50   +09 36 15.8         19CM32    T14  C~8Sg4      
2003 12  23.54279  10 32 53.41   +09 36 16.3         19CM32    T14  C~8Sg4      
2003 12  23.59369  10 32 53.33   +09 36 16.8         19CM32    T14  C~8Sg4      
2018 03  18.503027 11 39 50.89   +03 26 47.1         19CM32    T09  C~8Sg4      
2018 04  24.35200  11 37 22.37   +03 42 40.0   23.9z 19CM32    T09  C~8Sg4      
2018 04  24.36908  11 37 22.29   +03 42 40.3   23.2z 19CM32    T09  C~8Sg4      
2018 04  24.39881  11 37 22.20   +03 42 41.0   23.8z 19CM32    T09  C~8Sg4      
2018 04  24.442549 11 37 22.07   +03 42 41.8         19CM32    T09  C~8Sg4      
2019 02  02.639350 11 47 53.62   +02 36 51.7         19CM32    T09  C~8Sg4      
2019 02  02.653403 11 47 53.60   +02 36 52.0         19CM32    T09  C~8Sg4      
2019 02  04.58455  11 47 47.64   +02 37 34.1   25.1g 19CM32    T09  C~8Sg4      
2019 02  04.58665  11 47 47.64   +02 37 34.1   25.2g 19CM32    T09  C~8Sg4      
2019 02  04.61839  11 47 47.55   +02 37 34.9   25.5g 19CM32    T09  C~8Sg4      
2019 02  04.66041  11 47 47.39   +02 37 35.6   25.0g 19CM32    T09  C~8Sg4      
2019 02  05.50891  11 47 44.71   +02 37 54.6   24.4i 19CM32    T09  C~8Sg4      
2019 02  05.51157  11 47 44.70   +02 37 54.9   23.9i 19CM32    T09  C~8Sg4      
2019 03  03.508780 11 46 04.60   +02 49 20.3         19CM32    T09  C~8Sg4      
2019 03  08.34835  11 45 43.37   +02 51 42.4   24.3r 19CM32    T09  C~8Sg4      
2019 03  08.35813  11 45 43.34   +02 51 42.7   24.1r 19CM32    T09  C~8Sg4      
2019 03  08.40222  11 45 43.14   +02 51 43.7   23.9r 19CM32    T09  C~8Sg4      
2019 03  08.43185  11 45 43.00   +02 51 44.7   23.8r 19CM32    T09  C~8Sg4      
2019 03  08.43394  11 45 43.00   +02 51 44.9   23.8r 19CM32    T09  C~8Sg4      

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     0.11       0.00     0.01
     2   0.0001      0.00    -0.06       0.00    -0.00
     3   0.0003      0.00    -0.09       0.00    -0.00
     4  14.2341      0.00    -0.00       0.00     0.08
     5  14.3350      0.00     0.15       0.00     0.02
     6  14.3351      0.00    -0.20       0.00    -0.03
     7  14.3351      0.00    -0.07       0.00     0.07
     8  14.3353      0.00     0.14       0.00    -0.01
     9  15.1133      0.00    -0.14       0.00     0.03
    10  15.1134      0.00     0.21       0.00     0.03
    11  15.1187      0.00    -0.05       0.00     0.02
    12  15.1187      0.00     0.05       0.00    -0.02
    13  15.1188      0.00     0.23       0.00     0.07
    14  15.1189      0.00    -0.14       0.00    -0.16
    15  15.1212      0.00    -0.12       0.00    -0.15
    16  15.1212      0.00    -0.14       0.00     0.09
    17  15.1924      0.00     0.19       0.00    -0.12
    18  15.2056      0.00    -0.17       0.00     0.11
    19  15.2057      0.00     0.04       0.00     0.12
    20  15.2058      0.00     0.01       0.00    -0.18
    21  15.2059      0.00    -0.08       0.00    -0.05
    22  15.2059      0.00     0.06       0.00     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.

19CM32    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        42.617    42.617    42.617
ecceobj         0.016     0.016     0.016
incobj          2.283     2.283     2.283
qmin           40.768    40.767    40.768
qmax           44.909    44.909    44.911
amean          42.751    42.751    42.751
amin           42.424    42.424    42.424
amax           43.085    43.085    43.086
emean           0.022     0.022     0.022
emin            0.001     0.001     0.001
emax            0.042     0.042     0.042
imean           2.471     2.471     2.471
imin            1.323     1.323     1.323
imax            3.354     3.354     3.354
excite_mean     0.049     0.049     0.049
fracstop        1.000     1.000     1.000
cjmean          3.084     3.084     3.084

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       180.0     180.0     180.0
kozaiamp        180.0     180.0     180.0