Orbit Fit and Astrometric record for 16YY39

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: 16YY39    
# Created Fri Nov 22 02:10:47 2024
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   1.79y
# First observation: 2016/04/04
#  Last observation: 2018/01/17
Preliminary a, adot, b, bdot, g, gdot:
   0.000218   0.037467  -0.000009  -0.001531   0.033970   0.000000
# Chi-squared of fit:    11.16 DOF:     34 RMS:  0.13
# Min/Max residuals:    -0.31    0.36
# Exact a, adot, b, bdot, g, gdot:
  1.744831E-05  3.755769E-02 -2.641555E-07 -1.522166E-03  3.426526E-02  9.752913E-03
# Covariance matrix:
  4.8875E-13 -6.9597E-13 -4.9136E-15  1.2325E-14 -1.8198E-13 -5.0734E-12
 -6.9597E-13  2.5371E-12  1.4802E-14 -9.7201E-14 -5.9125E-14  2.2673E-11
 -4.9136E-15  1.4802E-14  3.5853E-13 -3.7874E-13  5.7294E-15  2.1426E-13
  1.2325E-14 -9.7201E-14 -3.7874E-13  5.0676E-13  9.5852E-15 -1.0287E-12
 -1.8198E-13 -5.9125E-14  5.7294E-15  9.5852E-15  4.5436E-13  2.9686E-12
 -5.0734E-12  2.2673E-11  2.1426E-13 -1.0287E-12  2.9686E-12  2.8167E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
  -13.496809  145.634269   -0.751495   -0.152447   -0.635785  2457482.744867
# Heliocentric elements and errors
Epoch:              2457480.5000  =  2016/04/02
Mean Anomaly:           79.85135 +/-     0.078
Argument of Peri:      149.95850 +/-     0.040
Long of Asc Node:      246.18929 +/-     0.005
Inclination:            13.35938 +/-     0.000
Eccentricity:         0.27493337 +/-    0.0004
Semi-Major Axis:     29.05977983 +/-    0.0078
Time of Perihelion: 2444788.8919 +/-      11.2
Perihelion:          21.07027654 +/-    0.0121
Aphelion:            37.04928312 +/-    0.0146
Period (y)              156.6559 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -24.39267605 +/-    0.0005
Ecliptic Y           15.76493461 +/-    0.0003
Ecliptic Z           -6.81130135 +/-    0.0001
Ecliptic XDOT        -0.00229587 +/-    0.0000
Ecliptic YDOT        -0.00207239 +/-    0.0000
Ecliptic ZDOT        -0.00030013 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   29.83168842 +/-    0.0004
Geocenter to KBO     29.18407623 +/-    0.0006
# Hcoef:  9.97

The following table shows the complete astrometric record for 16YY39. 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 (16YY39) followed by the observatory code and reference code for the source of the astrometry.

2016 04  04.244078 09 33 32.41   +00 14 26.6         16YY39    T09  C~81Bh      
2016 04  04.255396 09 33 32.37   +00 14 27.0         16YY39    T09  C~81Bh      
2016 04  04.265999 09 33 32.34   +00 14 27.5         16YY39    T09  C~81Bh      
2016 12  25.46448  09 50 33.36   -01 16 53.3   24.9r 16YY39    T09  C~7xTe      
2016 12  25.48961  09 50 33.25   -01 16 53.3   25.2r 16YY39    T09  C~7xTe      
2016 12  25.49379  09 50 33.25   -01 16 53.6   25.1r 16YY39    T09  C~7xTe      
2017 01  26.45718  09 47 54.69   -01 12 59.7   24.3z 16YY39    T09  C~7xTe      
2017 01  26.47468  09 47 54.59   -01 12 59.7   24.5z 16YY39    T09  C~7xTe      
2017 01  26.49073  09 47 54.49   -01 12 59.2   24.0z 16YY39    T09  C~7xTe      
2017 01  26.49344  09 47 54.48   -01 12 59.5   24.5z 16YY39    T09  C~7xTe      
2017 01  28.42233  09 47 42.72   -01 12 18.6   25.6g 16YY39    T09  C~7xTe      
2017 01  28.44025  09 47 42.60   -01 12 18.4   25.4g 16YY39    T09  C~7xTe      
2017 01  28.45292  09 47 42.52   -01 12 17.9   25.5g 16YY39    T09  C~7xTe      
2017 01  28.46551  09 47 42.45   -01 12 17.4   25.0g 16YY39    T09  C~7xTe      
2017 03  04.39457  09 44 01.57   -00 53 42.1   24.3i 16YY39    T09  C~7xTe      
2017 03  04.39725  09 44 01.55   -00 53 42.1   24.0i 16YY39    T09  C~7xTe      
2017 03  04.43505  09 44 01.33   -00 53 40.4   24.4i 16YY39    T09  C~7xTe      
2017 03  06.38592  09 43 49.76   -00 52 23.4   24.7i 16YY39    T09  C~7xTe      
2017 03  06.39997  09 43 49.67   -00 52 22.5   24.3i 16YY39    T09  C~7xTe      
2018 01  17.577575 09 56 33.56   -02 01 21.0         16YY39    T09  C~81Bh      

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    -0.09
     2   0.0000     -0.70    -0.02       0.18    -0.13
     3   0.0001     -1.29     0.04       0.51    -0.02
     4   0.7261  16297.24     0.14    -151.15     0.05
     5   0.7262  16295.67    -0.18    -151.69     0.10
     6   0.7262  16295.77     0.12    -151.97    -0.08
     7   0.8137  13960.14    -0.25    -711.73     0.13
     8   0.8138  13958.72    -0.01    -712.22    -0.16
     9   0.8138  13957.13    -0.08    -712.24    -0.00
    10   0.8138  13957.09     0.13    -712.57    -0.31
    11   0.8191  13776.25     0.09    -731.77     0.11
    12   0.8192  13774.48     0.04    -732.18    -0.11
    13   0.8192  13773.18    -0.04    -732.10     0.10
    14   0.8192  13772.02     0.01    -731.97     0.36
    15   0.9149  10264.85    -0.05    -764.55     0.08
    16   0.9149  10264.57    -0.07    -764.65    -0.04
    17   0.9150  10260.88     0.01    -764.13     0.21
    18   0.9203  10071.24     0.17    -748.29    -0.14
    19   0.9203  10069.66    -0.03    -747.88     0.16
    20   1.7887  22326.55    -0.00    -908.21    -0.22

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.

16YY39    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        29.099    29.124    29.073
ecceobj         0.281     0.281     0.280
incobj         13.338    13.338    13.338
qmin           20.391    20.516    20.512
qmax           37.639    37.459    40.298
amean          28.324    28.707    30.315
amin           27.341    28.132    28.587
amax           29.273    29.124    33.616
emean           0.262     0.264     0.243
emin            0.214     0.224     0.147
emax            0.286     0.286     0.310
imean          14.439    14.718    16.503
imin           13.799    14.007    13.702
imax           15.198    16.095    19.520
excite_mean     0.362     0.367     0.377
fracstop        0.013     0.018     0.111
cjmean          2.880     2.875     2.859

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       193.7     203.8     207.9
kozaiamp         44.9      48.1     179.1