Orbit Fit and Astrometric record for 16LH106

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: 16LH106   
# Created Sun Dec 22 02:10:43 2024
# Orbit generated from Bernstein formalism
# Fitting     20 observations of     20
# Arc:  80.94d
# First observation: 2016/03/16
#  Last observation: 2016/06/05
Preliminary a, adot, b, bdot, g, gdot:
  -0.000109   0.063388  -0.000010  -0.010227   0.044275   0.000000
# Chi-squared of fit:    12.77 DOF:     34 RMS:  0.14
# Min/Max residuals:    -0.36    0.39
# Exact a, adot, b, bdot, g, gdot:
  2.050705E-05  5.995577E-02 -4.020701E-06 -1.037140E-02  4.390233E-02  3.367230E-03
# Covariance matrix:
  2.9522E-13  5.8704E-13 -9.8120E-15 -1.8439E-13  1.0404E-12  9.5477E-11
  5.8704E-13  6.2313E-09 -2.8298E-11  1.8608E-10  1.0558E-09 -4.3432E-09
 -9.8120E-15 -2.8298E-11  2.9429E-13 -1.8658E-12 -4.8181E-12  1.7904E-11
 -1.8439E-13  1.8608E-10 -1.8658E-12  1.7331E-11  3.0206E-11 -3.0369E-10
  1.0404E-12  1.0558E-09 -4.8181E-12  3.0206E-11  1.8376E-10 -1.6424E-10
  9.5477E-11 -4.3432E-09  1.7904E-11 -3.0369E-10 -1.6424E-10  7.5201E-08
#      lat0       lon0       xBary       yBary       zBary        JD0
   11.650647 -150.139485    0.552948    0.166290   -0.805780  2457463.970569
# Heliocentric elements and errors
Epoch:              2457460.5000  =  2016/03/13
Mean Anomaly:           10.31301 +/-     1.315
Argument of Peri:      115.34575 +/-     1.842
Long of Asc Node:       77.82179 +/-     0.044
Inclination:            14.68445 +/-     0.010
Eccentricity:         0.15899848 +/-    0.0020
Semi-Major Axis:     27.93496821 +/-    0.0517
Time of Perihelion: 2455915.5885 +/-     196.9
Perihelion:          23.49335077 +/-    0.0711
Aphelion:            32.37658565 +/-    0.0821
Period (y)              147.6490 +/-      0.41
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -20.33925514 +/-    0.0060
Ecliptic Y          -11.03965266 +/-    0.0034
Ecliptic Z            4.59977141 +/-    0.0014
Ecliptic XDOT         0.00156992 +/-    0.0000
Ecliptic YDOT        -0.00341700 +/-    0.0000
Ecliptic ZDOT        -0.00059104 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   23.59485384 +/-    0.0054
Geocenter to KBO     22.77783247 +/-    0.0070
# Hcoef: 11.09

The following table shows the complete astrometric record for 16LH106. 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 (16LH106) followed by the observatory code and reference code for the source of the astrometry.

2016 03  16.46978  14 07 24.73   -00 29 52.3   24.4z 16LH106   T09  C~89Tk      
2016 03  16.49362  14 07 24.60   -00 29 51.4   24.7z 16LH106   T09  C~89Tk      
2016 03  16.54620  14 07 24.26   -00 29 48.9   24.6z 16LH106   T09  C~89Tk      
2016 03  16.57077  14 07 24.10   -00 29 47.9   24.8z 16LH106   T09  C~89Tk      
2016 03  16.59256  14 07 24.00   -00 29 46.6   24.5z 16LH106   T09  C~89Tk      
2016 04  11.43756  14 04 28.80   -00 11 01.5   24.9i 16LH106   T09  C~89Tk      
2016 04  11.46218  14 04 28.61   -00 11 00.6   24.5i 16LH106   T09  C~89Tk      
2016 04  11.47868  14 04 28.49   -00 11 00.0   25.0i 16LH106   T09  C~89Tk      
2016 04  11.48411  14 04 28.44   -00 10 59.6   25.2i 16LH106   T09  C~89Tk      
2016 04  11.50575  14 04 28.28   -00 10 58.6   24.7i 16LH106   T09  C~89Tk      
2016 04  11.50846  14 04 28.27   -00 10 58.6   24.6i 16LH106   T09  C~89Tk      
2016 04  11.52732  14 04 28.11   -00 10 58.0   24.1i 16LH106   T09  C~89Tk      
2016 04  11.53541  14 04 28.03   -00 10 57.6   24.2i 16LH106   T09  C~89Tk      
2016 04  11.54904  14 04 27.96   -00 10 56.9   24.5i 16LH106   T09  C~89Tk      
2016 04  11.55443  14 04 27.90   -00 10 56.8   24.5i 16LH106   T09  C~89Tk      
2016 06  05.37008  13 58 03.96   +00 09 44.6   24.7r 16LH106   T09  C~89Tk      
2016 06  05.38217  13 58 03.89   +00 09 44.6   24.5r 16LH106   T09  C~89Tk      
2016 06  05.38431  13 58 03.89   +00 09 44.6   24.3r 16LH106   T09  C~89Tk      
2016 06  05.39709  13 58 03.82   +00 09 44.7   24.9r 16LH106   T09  C~89Tk      
2016 06  05.41411  13 58 03.73   +00 09 44.7   25.2r 16LH106   T09  C~89Tk      

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     0.22       0.00     0.06
     2   0.0001     -2.14     0.39       0.17    -0.04
     3   0.0002     -7.79    -0.15       0.76    -0.05
     4   0.0003    -10.39    -0.36       0.87    -0.21
     5   0.0003    -12.24    -0.10       1.57     0.24
     6   0.0711  -2867.19    -0.08     150.89     0.01
     7   0.0712  -2870.18    -0.04     150.75    -0.08
     8   0.0712  -2872.08     0.09     150.70    -0.11
     9   0.0712  -2872.92    -0.08     150.81     0.02
    10   0.0713  -2875.52    -0.02     150.92     0.16
    11   0.0713  -2875.66     0.17     150.87     0.12
    12   0.0713  -2878.12     0.03     150.61    -0.12
    13   0.0714  -2879.38    -0.24     150.57    -0.14
    14   0.0714  -2880.61     0.20     150.86     0.18
    15   0.0714  -2881.49    -0.02     150.65    -0.03
    16   0.2215  -8720.22     0.04    -672.08    -0.05
    17   0.2215  -8721.21    -0.07    -672.44    -0.08
    18   0.2215  -8721.21     0.09    -672.44    -0.02
    19   0.2216  -8722.23    -0.01    -672.71     0.07
    20   0.2216  -8723.50    -0.05    -673.18     0.08

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.

16LH106    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        27.690    28.037    27.363
ecceobj         0.151     0.165     0.137
incobj         14.685    14.665    14.704
qmin           23.507    20.961    23.391
qmax           32.317    33.567    31.714
amean          28.099    27.605    27.514
amin           27.690    26.621    27.217
amax           28.305    28.243    27.789
emean           0.144     0.190     0.139
emin            0.140     0.165     0.134
emax            0.151     0.213     0.145
imean          13.424    12.751    13.332
imin           13.340    12.436    13.294
imax           13.469    13.369    13.363
excite_mean     0.273     0.291     0.269
fracstop        0.000     0.016     0.002
cjmean          2.928     2.921     2.934

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       111.2     164.7     124.5
kozaiamp          3.6      54.5       8.2