Orbit Fit and Astrometric record for 16EZ365

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: 16EZ365   
# Created Tue Apr  1 01:10:44 2025
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:  90.76d
# First observation: 2016/03/07
#  Last observation: 2016/06/06
Preliminary a, adot, b, bdot, g, gdot:
  -0.000026   0.026650  -0.000007  -0.000202   0.024868   0.000000
# Chi-squared of fit:     8.10 DOF:     38 RMS:  0.11
# Min/Max residuals:    -0.28    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.550419E-05  2.409712E-02 -1.731408E-08 -2.412024E-04  2.445367E-02  8.723248E-04
# Covariance matrix:
  2.1753E-13 -8.2307E-12  2.0259E-14 -1.1153E-13 -7.0428E-13  1.2066E-10
 -8.2307E-12  4.8649E-09 -1.8104E-11  7.9560E-11  8.1816E-10 -7.2703E-09
  2.0259E-14 -1.8104E-11  2.0505E-13 -9.6642E-13 -3.1139E-12  1.4556E-11
 -1.1153E-13  7.9560E-11 -9.6642E-13  7.6826E-12  1.3499E-11 -9.9588E-11
 -7.0428E-13  8.1816E-10 -3.1139E-12  1.3499E-11  1.4246E-10 -3.2340E-10
  1.2066E-10 -7.2703E-09  1.4556E-11 -9.9588E-11 -3.2340E-10  1.8396E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
   11.578850 -151.645515    0.652519    0.149394   -0.728451  2457455.112099
# Heliocentric elements and errors
Epoch:              2457450.5000  =  2016/03/03
Mean Anomaly:           34.43433 +/-    21.502
Argument of Peri:       55.02126 +/-    23.565
Long of Asc Node:      115.42073 +/-     0.040
Inclination:            11.37774 +/-     0.000
Eccentricity:         0.03720522 +/-    0.0109
Semi-Major Axis:     42.92876467 +/-    0.1685
Time of Perihelion: 2447623.7433 +/-    6136.0
Perihelion:          41.33159059 +/-    0.4957
Aphelion:            44.52593875 +/-    0.5000
Period (y)              281.2748 +/-      1.66
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -36.22288239 +/-    0.0172
Ecliptic Y          -18.80754222 +/-    0.0093
Ecliptic Z            8.20804316 +/-    0.0040
Ecliptic XDOT         0.00119221 +/-    0.0000
Ecliptic YDOT        -0.00242924 +/-    0.0000
Ecliptic ZDOT        -0.00000684 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.63163251 +/-    0.0156
Geocenter to KBO     40.89365364 +/-    0.0200
# Hcoef:  8.12

The following table shows the complete astrometric record for 16EZ365. 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 (16EZ365) followed by the observatory code and reference code for the source of the astrometry.

2016 03  07.61131  14 01 46.76   -00 03 09.0   25.8g 16EZ365   T09  C~89T9      
2016 03  07.62907  14 01 46.69   -00 03 08.3   25.2g 16EZ365   T09  C~89T9      
2016 03  07.64195  14 01 46.68   -00 03 08.0   25.0g 16EZ365   T09  C~89T9      
2016 03  07.64626  14 01 46.66   -00 03 07.8   25.6g 16EZ365   T09  C~89T9      
2016 03  16.46294  14 01 18.19   +00 01 10.9   23.7z 16EZ365   T09  C~89T9      
2016 03  16.46636  14 01 18.18   +00 01 11.1   23.9z 16EZ365   T09  C~89T9      
2016 03  16.49093  14 01 18.09   +00 01 11.6   24.1z 16EZ365   T09  C~89T9      
2016 03  16.54349  14 01 17.90   +00 01 13.3   23.2z 16EZ365   T09  C~89T9      
2016 03  16.57637  14 01 17.79   +00 01 14.1   24.1z 16EZ365   T09  C~89T9      
2016 03  16.58986  14 01 17.74   +00 01 14.8   23.8z 16EZ365   T09  C~89T9      
2016 03  16.60069  14 01 17.70   +00 01 15.1   23.7z 16EZ365   T09  C~89T9      
2016 04  15.47312  13 59 13.89   +00 15 38.8   22.8y 16EZ365   T09  C~89T9      
2016 04  15.50154  13 59 13.76   +00 15 39.5   23.2y 16EZ365   T09  C~89T9      
2016 04  15.53400  13 59 13.60   +00 15 40.5   23.5y 16EZ365   T09  C~89T9      
2016 04  15.54480  13 59 13.55   +00 15 40.7   23.5y 16EZ365   T09  C~89T9      
2016 06  05.38217  13 55 44.69   +00 29 33.0   24.1r 16EZ365   T09  C~89T9      
2016 06  05.40134  13 55 44.63   +00 29 33.0   24.3r 16EZ365   T09  C~89T9      
2016 06  05.41197  13 55 44.61   +00 29 32.8   24.4r 16EZ365   T09  C~89T9      
2016 06  05.41411  13 55 44.58   +00 29 32.8   24.6r 16EZ365   T09  C~89T9      
2016 06  06.34511  13 55 41.81   +00 29 36.2   25.5g 16EZ365   T09  C~89T9      
2016 06  06.35361  13 55 41.78   +00 29 36.3   25.4g 16EZ365   T09  C~89T9      
2016 06  06.37484  13 55 41.71   +00 29 36.2   26.2g 16EZ365   T09  C~89T9      

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     0.02       0.00    -0.03
     2   0.0000     -1.23    -0.28       0.29     0.06
     3   0.0001     -1.47     0.15       0.52     0.15
     4   0.0001     -1.83     0.02       0.60     0.18
     5   0.0242   -492.42    -0.01      93.44    -0.08
     6   0.0242   -492.63    -0.02      93.57     0.02
     7   0.0243   -494.07     0.04      93.57    -0.21
     8   0.0245   -497.33    -0.03      94.17    -0.09
     9   0.0245   -499.16     0.14      94.34    -0.21
    10   0.0246   -500.10     0.02      94.73     0.06
    11   0.0246   -500.77     0.01      94.80     0.03
    12   0.1064  -2542.88     0.04     253.78     0.04
    13   0.1065  -2544.95     0.08     253.75     0.00
    14   0.1066  -2547.55    -0.11     253.85     0.08
    15   0.1066  -2548.32    -0.08     253.77     0.00
    16   0.2458  -5775.68    -0.05     -63.12     0.12
    17   0.2458  -5776.53    -0.04     -63.44     0.05
    18   0.2459  -5776.74     0.23     -63.73    -0.10
    19   0.2459  -5777.16    -0.10     -63.89    -0.23
    20   0.2484  -5817.30     0.05     -75.25     0.08
    21   0.2484  -5817.76    -0.03     -75.31     0.13
    22   0.2485  -5818.71    -0.05     -75.77    -0.05

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.

16EZ365    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        42.439    42.997    41.905
ecceobj         0.028     0.043     0.021
incobj         11.378    11.378    11.379
qmin           40.477    40.473    39.788
qmax           45.145    46.316    44.865
amean          42.712    43.278    42.175
amin           42.388    42.940    41.857
amax           43.047    43.626    42.509
emean           0.033     0.047     0.029
emin            0.019     0.034     0.007
emax            0.049     0.062     0.056
imean           9.884     9.838     9.836
imin            9.128     9.234     8.987
imax           10.618    10.504    10.816
excite_mean     0.175     0.177     0.174
fracstop        1.000     1.000     1.000
cjmean          3.050     3.056     3.045

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       179.8     180.8     177.5
kozaiamp        180.0     180.0     180.0