Orbit Fit and Astrometric record for 19EU7

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: 19EU7     
# Created Sun Nov 24 02:10:55 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:  10.12y
# First observation: 2009/01/23
#  Last observation: 2019/03/08
# Chi-squared of fit:     9.23 DOF:     38 RMS:  0.11
# Min/Max residuals:    -0.17    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.592409E-05  2.274825E-02 -3.351566E-07 -5.317125E-05  2.359225E-02 -1.711432E-03
# Covariance matrix:
  7.3425E-13 -1.5402E-13 -1.3854E-17  1.7256E-16 -7.9139E-14 -3.4229E-13
 -1.5402E-13  1.3163E-12  2.0752E-15 -3.8859E-15  2.2608E-12  5.2981E-12
 -1.3854E-17  2.0752E-15  7.1842E-13 -7.3587E-14  4.2120E-15  8.2334E-15
  1.7256E-16 -3.8859E-15 -7.3587E-14  8.2526E-15 -7.0814E-15 -1.5639E-14
 -7.9139E-14  2.2608E-12  4.2120E-15 -7.0814E-15  4.2367E-12  9.0666E-12
 -3.4229E-13  5.2981E-12  8.2334E-15 -1.5639E-14  9.0666E-12  2.1485E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    3.241866  164.906131    0.655684    0.041933   -0.739632  2454854.936257
# Heliocentric elements and errors
Epoch:              2454854.5000  =  2009/01/23
Mean Anomaly:          286.55389 +/-     0.082
Argument of Peri:      175.59365 +/-     0.086
Long of Asc Node:       72.46988 +/-     0.004
Inclination:             3.18725 +/-     0.000
Eccentricity:         0.09366243 +/-    0.0002
Semi-Major Axis:     43.93384973 +/-    0.0126
Time of Perihelion: 2476554.6948 +/-      43.9
Perihelion:          39.81889851 +/-    0.0155
Aphelion:            48.04880096 +/-    0.0173
Period (y)              291.2105 +/-      0.13
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -41.40143441 +/-    0.0036
Ecliptic Y           11.84078473 +/-    0.0010
Ecliptic Z            2.39699129 +/-    0.0002
Ecliptic XDOT        -0.00049088 +/-    0.0000
Ecliptic YDOT        -0.00259727 +/-    0.0000
Ecliptic ZDOT        -0.00001750 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   43.12810723 +/-    0.0034
Geocenter to KBO     42.38686740 +/-    0.0037
# Hcoef:  7.46

The following table shows the complete astrometric record for 19EU7. 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 (19EU7) followed by the observatory code and reference code for the source of the astrometry.

2009 01  23.435491 11 09 28.30   +08 56 03.2         19EU7     T09  C~870X      
2009 01  23.494395 11 09 28.13   +08 56 04.3         19EU7     T09  C~870X      
2018 03  18.48012  11 50 09.19   +04 31 30.1   23.2i 19EU7     T09  C~870X      
2018 03  18.55199  11 50 08.87   +04 31 31.8   22.9i 19EU7     T09  C~870X      
2018 03  18.59206  11 50 08.70   +04 31 33.1   22.9i 19EU7     T09  C~870X      
2018 04  12.112846 11 48 23.256  +04 42 23.87  24.7V 19EU7     W84  C~8HR7      
2018 04  13.110564 11 48 19.313  +04 42 46.98  23.8V 19EU7     W84  C~8HR7      
2018 04  24.37585  11 47 37.96   +04 46 42.2   23.2z 19EU7     T09  C~870X      
2018 04  24.41489  11 47 37.84   +04 46 42.8   22.7z 19EU7     T09  C~870X      
2018 04  24.49874  11 47 37.53   +04 46 44.5   23.6z 19EU7     T09  C~870X      
2019 02  04.565972 11 57 54.56   +03 38 44.4         19EU7     T09  C~870X      
2019 02  04.643619 11 57 54.32   +03 38 46.1         19EU7     T09  C~870X      
2019 03  02.45121  11 56 19.61   +03 50 02.8   23.3y 19EU7     T09  C~83GA      
2019 03  02.53504  11 56 19.25   +03 50 05.4   22.9y 19EU7     T09  C~83GA      
2019 03  02.57800  11 56 19.07   +03 50 06.5   23.0y 19EU7     T09  C~83GA      
2019 03  02.61624  11 56 18.90   +03 50 07.5   23.1y 19EU7     T09  C~83GA      
2019 03  07.57007  11 55 57.67   +03 52 31.2   23.2y 19EU7     T09  C~83GA      
2019 03  07.58345  11 55 57.59   +03 52 31.5   23.0y 19EU7     T09  C~83GA      
2019 03  07.62089  11 55 57.43   +03 52 32.5   23.2y 19EU7     T09  C~83GA      
2019 03  08.37278  11 55 54.19   +03 52 54.6   25.0r 19EU7     T09  C~83GA      
2019 03  08.40641  11 55 54.02   +03 52 55.6   24.5r 19EU7     T09  C~83GA      
2019 03  08.41689  11 55 53.99   +03 52 55.9   25.0r 19EU7     T09  C~83GA      

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     0.11
     2   0.0002      0.00     0.11       0.00    -0.13
     3   9.1473      0.00    -0.05       0.00     0.24
     4   9.1475      0.00     0.05       0.00    -0.12
     5   9.1476      0.00     0.22       0.00     0.03
     6   9.2147      0.00    -0.13       0.00     0.05
     7   9.2175      0.00    -0.13       0.00     0.03
     8   9.2483      0.00    -0.03       0.00    -0.01
     9   9.2484      0.00     0.20       0.00    -0.13
    10   9.2486      0.00    -0.13       0.00     0.02
    11  10.0318      0.00     0.01       0.00     0.07
    12  10.0321      0.00    -0.05       0.00     0.02
    13  10.1027      0.00    -0.11       0.00    -0.13
    14  10.1029      0.00    -0.10       0.00     0.07
    15  10.1031      0.00    -0.03       0.00    -0.07
    16  10.1032      0.00    -0.12       0.00    -0.17
    17  10.1167      0.00     0.20       0.00     0.05
    18  10.1168      0.00    -0.12       0.00    -0.04
    19  10.1169      0.00    -0.04       0.00    -0.12
    20  10.1189      0.00     0.23       0.00     0.06
    21  10.1190      0.00    -0.08       0.00     0.08
    22  10.1190      0.00     0.16       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.

19EU7    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