Orbit Fit and Astrometric record for 19EE6

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: 19EE6     
# Created Tue May  7 01:17:34 2024
# Orbit generated from Bernstein formalism
# Fitting      7 observations of      7
# Arc:  62.89d
# First observation: 2019/03/05
#  Last observation: 2019/05/07
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.014068  -0.000000   0.004364   0.017821   0.000000
# WARNING Fitting with energy constraint
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     0.37 DOF:      9 RMS:  0.04
# Min/Max residuals:    -0.10    0.06
# Exact a, adot, b, bdot, g, gdot:
  1.058667E-05  1.165929E-02  3.841926E-06  4.262533E-03  1.746493E-02 -7.514885E-03
# Covariance matrix:
  3.0607E-10  3.2556E-07  9.2691E-12  1.6348E-08  5.9025E-08  3.3242E-07
  3.2556E-07  3.4712E-04  9.8830E-09  1.7430E-05  6.2934E-05  3.5425E-04
  9.2691E-12  9.8830E-09  1.0101E-12  4.9202E-10  1.7918E-09  1.0100E-08
  1.6348E-08  1.7430E-05  4.9202E-10  8.7529E-07  3.1602E-06  1.7819E-05
  5.9025E-08  6.2934E-05  1.7918E-09  3.1602E-06  1.1411E-05  6.4354E-05
  3.3242E-07  3.5425E-04  1.0100E-08  1.7819E-05  6.4354E-05  4.0957E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    7.894593  174.660262    0.186467    0.134304   -0.968208  2458547.900321
# Heliocentric elements and errors
Epoch:              2458540.5000  =  2019/02/26
Mean Anomaly:          302.45569 +/-    79.484
Argument of Peri:      141.09429 +/-   102.309
Long of Asc Node:      154.21025 +/-    25.559
Inclination:            21.47677 +/-    23.608
Eccentricity:         0.52381037 +/-    1.5305
Semi-Major Axis:     59.57889682 +/-   31.2105
Time of Perihelion: 2485390.0490 +/-   30500.5
Perihelion:          28.37085302 +/-   92.3912
Aphelion:            90.78694062 +/-  102.8450
Period (y)              459.8825 +/-    361.36
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -57.42347012 +/-   10.9217
Ecliptic Y            5.54643902 +/-    1.0217
Ecliptic Z            7.86460897 +/-    1.5211
Ecliptic XDOT         0.00109129 +/-    0.0036
Ecliptic YDOT        -0.00193831 +/-    0.0023
Ecliptic ZDOT         0.00049985 +/-    0.0005
# Distances at JD0 (AU)
Heliocenter to KBO   58.22430748 +/-   10.7739
Geocenter to KBO     57.25760845 +/-   11.0744
# Hcoef:  7.47

The following table shows the complete astrometric record for 19EE6. 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 (19EE6) followed by the observatory code and reference code for the source of the astrometry.

2019 03  05.39952  11 53 02.706  +09 21 45.77  25.0r 19EE6     568  C~5agn      
2019 03  05.56697  11 53 02.148  +09 21 50.06  25.0r 19EE6     568  C~5agn      
2019 05  07.21615  11 49 52.619  +09 41 52.18        19EE6     G37  C~5agn      
2019 05  07.22346  11 49 52.603  +09 41 52.25        19EE6     G37  C~5agn      
2019 05  07.23075  11 49 52.586  +09 41 52.22        19EE6     G37  C~5agn      
2019 05  07.23803  11 49 52.576  +09 41 52.37        19EE6     G37  C~5agn      
2019 05  07.29033  11 49 52.456  +09 41 52.72        19EE6     G37  C~5agn      

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    -0.01       0.00     0.00
     2   0.0005     -9.29     0.01       0.61    -0.00
     3   0.1720  -3059.97    -0.00     -20.28     0.04
     4   0.1720  -3060.22    -0.01     -20.31     0.04
     5   0.1720  -3060.44     0.01     -20.43    -0.05
     6   0.1720  -3060.63     0.05     -20.36     0.06
     7   0.1722  -3062.40    -0.04     -20.74    -0.10

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.

19EE6    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