Orbit Fit and Astrometric record for 16QR164

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: 16QR164   
# Created Mon Jul  7 01:11:12 2025
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:   0.97y
# First observation: 2016/08/28
#  Last observation: 2017/08/19
Preliminary a, adot, b, bdot, g, gdot:
  -0.000016   0.031840  -0.000000  -0.006142   0.026797   0.000000
# Chi-squared of fit:     7.34 DOF:     34 RMS:  0.11
# Min/Max residuals:    -0.32    0.20
# Exact a, adot, b, bdot, g, gdot:
  1.808093E-05  3.156017E-02 -3.142379E-06 -6.120150E-03  2.767195E-02 -3.447458E-03
# Covariance matrix:
  4.9756E-13  3.8613E-11  1.0899E-14 -7.2602E-12  1.9874E-11  1.2010E-09
  3.8613E-11  5.9651E-09  1.7275E-12 -1.1141E-09  3.0554E-09  1.8433E-07
  1.0899E-14  1.7275E-12  2.4356E-13 -5.8296E-13  8.9587E-13  5.3480E-11
 -7.2602E-12 -1.1141E-09 -5.8296E-13  2.0851E-10 -5.7075E-10 -3.4432E-08
  1.9874E-11  3.0554E-09  8.9587E-13 -5.7075E-10  1.5663E-09  9.4434E-08
  1.2010E-09  1.8433E-07  5.3480E-11 -3.4432E-08  9.4434E-08  5.6968E-06
#      lat0       lon0       xBary       yBary       zBary        JD0
   15.459712  -24.642773   -0.001200    0.269906   -0.975467  2457628.798529
# Heliocentric elements and errors
Epoch:              2457620.5000  =  2016/08/20
Mean Anomaly:          345.96799 +/-     8.076
Argument of Peri:      152.08616 +/-    16.438
Long of Asc Node:      208.37845 +/-     0.079
Inclination:            18.59429 +/-     0.019
Eccentricity:         0.29622745 +/-    0.0417
Semi-Major Axis:     51.45995178 +/-    1.4425
Time of Perihelion: 2462876.0702 +/-    3016.8
Perihelion:          36.21610126 +/-    2.3737
Aphelion:            66.70380231 +/-    2.8460
Period (y)              369.1580 +/-     15.52
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           32.57508534 +/-    0.0453
Ecliptic Y          -14.94617949 +/-    0.0208
Ecliptic Z            9.63281804 +/-    0.0138
Ecliptic XDOT         0.00115144 +/-    0.0002
Ecliptic YDOT         0.00290098 +/-    0.0001
Ecliptic ZDOT        -0.00067457 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   37.11220351 +/-    0.0408
Geocenter to KBO     36.13767607 +/-    0.0517
# Hcoef:  9.56

The following table shows the complete astrometric record for 16QR164. 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 (16QR164) followed by the observatory code and reference code for the source of the astrometry.

2016 08  28.29774  22 06 11.00   +04 51 33.4   25.4i 16QR164   T09  C~8vII      
2016 08  28.30044  22 06 10.98   +04 51 33.4   25.0i 16QR164   T09  C~8vII      
2016 08  28.30855  22 06 10.95   +04 51 33.1   24.9i 16QR164   T09  C~8vII      
2016 08  30.28003  22 06 01.38   +04 50 28.7   24.9i 16QR164   T09  C~8vII      
2016 08  30.31574  22 06 01.21   +04 50 27.5   24.7i 16QR164   T09  C~8vII      
2016 08  30.32391  22 06 01.17   +04 50 27.2   24.9i 16QR164   T09  C~8vII      
2017 06  24.46602  22 17 40.98   +05 25 09.6   25.0i 16QR164   T09  C~8vII      
2017 06  24.47137  22 17 40.99   +05 25 09.6   25.0i 16QR164   T09  C~8vII      
2017 06  24.47938  22 17 40.96   +05 25 09.6   24.9i 16QR164   T09  C~8vII      
2017 06  24.49808  22 17 40.94   +05 25 09.9   25.2i 16QR164   T09  C~8vII      
2017 08  18.32705  22 14 18.57   +05 16 12.9   25.6g 16QR164   T09  C~8vII      
2017 08  18.32984  22 14 18.55   +05 16 12.7   25.7g 16QR164   T09  C~8vII      
2017 08  18.33960  22 14 18.49   +05 16 12.5   25.8g 16QR164   T09  C~8vII      
2017 08  18.35223  22 14 18.44   +05 16 12.2   25.8g 16QR164   T09  C~8vII      
2017 08  18.36060  22 14 18.40   +05 16 11.9   25.3g 16QR164   T09  C~8vII      
2017 08  19.34646  22 14 13.61   +05 15 44.7   24.8r 16QR164   T09  C~8vII      
2017 08  19.34926  22 14 13.60   +05 15 44.9   25.6r 16QR164   T09  C~8vII      
2017 08  19.35919  22 14 13.55   +05 15 44.7   25.5r 16QR164   T09  C~8vII      
2017 08  19.37181  22 14 13.47   +05 15 44.0   25.0r 16QR164   T09  C~8vII      
2017 08  19.38020  22 14 13.42   +05 15 43.7   25.1r 16QR164   T09  C~8vII      

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    -0.07
     2   0.0000     -0.28    -0.07       0.11     0.04
     3   0.0000     -0.81     0.05      -0.01    -0.05
     4   0.0054   -157.46    -0.04      -8.11     0.06
     5   0.0055   -160.26     0.03      -8.31     0.01
     6   0.0055   -160.93     0.02      -8.37    -0.02
     7   0.8218  10350.12    -0.13   -1840.30     0.16
     8   0.8218  10350.26     0.13   -1840.35     0.01
     9   0.8219  10349.84    -0.11   -1840.19     0.02
    10   0.8219  10349.67     0.15   -1839.81     0.05
    11   0.9720   7330.44     0.13   -1253.95    -0.03
    12   0.9720   7330.08    -0.00   -1254.03    -0.12
    13   0.9721   7329.18    -0.15   -1253.89     0.01
    14   0.9721   7328.37     0.04   -1253.90    -0.02
    15   0.9721   7327.70     0.03   -1253.97    -0.09
    16   0.9748   7251.06     0.03   -1253.58    -0.13
    17   0.9748   7251.00     0.18   -1253.34     0.11
    18   0.9748   7250.23     0.20   -1253.26     0.18
    19   0.9749   7248.86    -0.18   -1253.48    -0.05
    20   0.9749   7248.05    -0.32   -1253.49    -0.06

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.

16QR164    quality flag:1

Type:       SCATNEAR  CENTAURS  SCATNEAR

axisobj        51.878    58.103    51.552
ecceobj         0.303     0.446     0.289
incobj         18.561    18.616    18.545
qmin           34.655    29.807    35.804
qmax           69.721    88.835    67.799
amean          51.718    57.972    51.450
amin           51.084    53.762    50.968
amax           52.509    60.282    52.073
emean           0.302     0.450     0.285
emin            0.283     0.408     0.269
emax            0.330     0.480     0.303
imean          18.879    18.427    19.156
imin           17.778    16.053    18.443
imax           19.576    20.368    19.678
excite_mean     0.443     0.550     0.435
fracstop        1.000     1.000     1.000
cjmean          2.945     2.869     2.952

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       178.0     183.7     193.7
kozaiamp        180.0     179.9     180.0