Orbit Fit and Astrometric record for 16YZ40

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: 16YZ40    
# Created Sun Dec 22 02:10:54 2024
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   0.82y
# First observation: 2016/04/02
#  Last observation: 2017/01/28
Preliminary a, adot, b, bdot, g, gdot:
  -0.000013   0.033787   0.000007  -0.008579   0.028216   0.000000
# Chi-squared of fit:    10.77 DOF:     34 RMS:  0.13
# Min/Max residuals:    -0.27    0.27
# Exact a, adot, b, bdot, g, gdot:
  1.806616E-05  3.210013E-02 -4.471856E-06 -8.456619E-03  2.898506E-02 -2.021475E-03
# Covariance matrix:
  1.8515E-13  5.1578E-13  3.9935E-16 -1.3488E-13  2.3711E-13  1.8451E-11
  5.1578E-13  5.2662E-10  2.6420E-13 -9.5338E-11  1.7125E-10  1.3070E-08
  3.9935E-16  2.6420E-13  1.8424E-13 -2.8013E-13  7.2427E-14  6.2153E-12
 -1.3488E-13 -9.5338E-11 -2.8013E-13  1.7859E-11 -3.1643E-11 -2.3839E-09
  2.3711E-13  1.7125E-10  7.2427E-14 -3.1643E-11  5.9924E-11  4.3612E-09
  1.8451E-11  1.3070E-08  6.2153E-12 -2.3839E-09  4.3612E-09  3.2741E-07
#      lat0       lon0       xBary       yBary       zBary        JD0
  -14.126045  144.360636   -0.743918   -0.161338   -0.641679  2457480.823679
# Heliocentric elements and errors
Epoch:              2457480.5000  =  2016/04/02
Mean Anomaly:          349.06197 +/-     4.127
Argument of Peri:      240.73132 +/-     6.142
Long of Asc Node:      282.64022 +/-     0.014
Inclination:            19.89580 +/-     0.005
Eccentricity:         0.18158180 +/-    0.0056
Semi-Major Axis:     42.69607172 +/-    0.1056
Time of Perihelion: 2460576.6132 +/-    1168.2
Perihelion:          34.94324232 +/-    0.2562
Aphelion:            50.44890111 +/-    0.2715
Period (y)              278.9909 +/-      1.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -28.16604486 +/-    0.0073
Ecliptic Y           19.27331119 +/-    0.0052
Ecliptic Z           -8.42019090 +/-    0.0022
Ecliptic XDOT        -0.00145771 +/-    0.0000
Ecliptic YDOT        -0.00269265 +/-    0.0000
Ecliptic ZDOT        -0.00072803 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   35.15232882 +/-    0.0065
Geocenter to KBO     34.50053323 +/-    0.0092
# Hcoef:  8.27

The following table shows the complete astrometric record for 16YZ40. 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 (16YZ40) followed by the observatory code and reference code for the source of the astrometry.

2016 04  02.32289  09 28 02.57   +00 02 55.7   23.5i 16YZ40    T09  C~8Dlp      
2016 04  02.33913  09 28 02.51   +00 02 56.2   23.4i 16YZ40    T09  C~8Dlp      
2016 04  02.34721  09 28 02.51   +00 02 56.2   23.2i 16YZ40    T09  C~8Dlp      
2016 04  02.35235  09 28 02.50   +00 02 56.6   23.5i 16YZ40    T09  C~8Dlp      
2016 04  04.24125  09 27 57.10   +00 03 52.2   24.4g 16YZ40    T09  C~8Dlp      
2016 04  04.25331  09 27 57.05   +00 03 52.5   24.6g 16YZ40    T09  C~8Dlp      
2016 04  04.26390  09 27 57.03   +00 03 52.8   24.5g 16YZ40    T09  C~8Dlp      
2016 04  04.27871  09 27 57.01   +00 03 53.3   24.5g 16YZ40    T09  C~8Dlp      
2016 12  25.47498  09 42 09.87   -01 30 52.7   23.8r 16YZ40    T09  C~86ue      
2016 12  25.47707  09 42 09.88   -01 30 52.7   23.9r 16YZ40    T09  C~86ue      
2016 12  25.48752  09 42 09.85   -01 30 53.1   23.8r 16YZ40    T09  C~86ue      
2016 12  25.50008  09 42 09.79   -01 30 53.2   23.7r 16YZ40    T09  C~86ue      
2017 01  21.37468  09 40 14.65   -01 30 45.8   23.6z 16YZ40    T09  C~86ue      
2017 01  21.40688  09 40 14.47   -01 30 45.4   23.0z 16YZ40    T09  C~86ue      
2017 01  21.56385  09 40 13.65   -01 30 43.7   23.3z 16YZ40    T09  C~86ue      
2017 01  21.62985  09 40 13.32   -01 30 43.1   23.5z 16YZ40    T09  C~86ue      
2017 01  21.63790  09 40 13.27   -01 30 43.2   23.6z 16YZ40    T09  C~86ue      
2017 01  28.38299  09 39 37.85   -01 29 20.5   24.3g 16YZ40    T09  C~86ue      
2017 01  28.41043  09 39 37.69   -01 29 20.4   23.9g 16YZ40    T09  C~86ue      
2017 01  28.41954  09 39 37.65   -01 29 19.9   24.1g 16YZ40    T09  C~86ue      

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    -0.03
     2   0.0000     -1.01    -0.27       0.18    -0.06
     3   0.0001     -1.01     0.16       0.18    -0.17
     4   0.0001     -1.28     0.16       0.51     0.09
     5   0.0053    -95.91     0.02      26.94     0.07
     6   0.0053    -96.72    -0.18      26.98    -0.05
     7   0.0053    -97.10    -0.03      27.17    -0.01
     8   0.0054    -97.54     0.27      27.55     0.16
     9   0.7314  13865.91    -0.18   -1223.37     0.09
    10   0.7314  13866.05     0.05   -1223.32     0.19
    11   0.7315  13865.75     0.22   -1223.85    -0.07
    12   0.7315  13864.93    -0.04   -1224.23    -0.14
    13   0.8051  12221.87     0.09   -1774.91    -0.05
    14   0.8052  12219.18    -0.12   -1775.41    -0.04
    15   0.8056  12206.95    -0.20   -1777.76     0.09
    16   0.8058  12202.05     0.01   -1778.79     0.10
    17   0.8058  12201.37    -0.05   -1779.13    -0.11
    18   0.8243  11670.21     0.09   -1872.25     0.07
    19   0.8243  11667.90     0.05   -1872.93    -0.26
    20   0.8244  11667.17     0.07   -1872.65     0.14

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.

16YZ40    quality flag:1

Type:       CENTAURS  SCATEXTD     5:3EE

axisobj        42.455    42.650    42.391
ecceobj         0.175     0.178     0.176
incobj         19.882    19.898    19.879
qmin           30.081    34.079    33.572
qmax           55.463    51.693    51.374
amean          42.326    42.582    42.327
amin           41.831    42.181    41.922
amax           42.927    43.029    42.798
emean           0.206     0.177     0.138
emin            0.079     0.153     0.061
emax            0.292     0.202     0.204
imean          20.578    21.515    22.344
imin           17.831    20.658    21.037
imax           23.708    22.217    23.661
excite_mean     0.412     0.407     0.406
fracstop        1.000     1.000     1.000
cjmean          2.878     2.883     2.882

libcent 0      -180.0    -180.0     181.1
libamp  0      -180.0    -180.0     110.9
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       281.6     181.4     189.1
kozaiamp         53.5     179.9     179.9