Orbit Fit and Astrometric record for 19GK196

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: 19GK196   
# Created Tue Jan 21 02:11:21 2025
# Orbit generated from Bernstein formalism
# Fitting     22 observations of     22
# Arc:   3.18y
# First observation: 2016/04/01
#  Last observation: 2019/06/08
Preliminary a, adot, b, bdot, g, gdot:
   0.000029   0.034159  -0.000042  -0.019144   0.033536   0.000000
# Chi-squared of fit:    61.19 DOF:     38 RMS:  0.29
# Min/Max residuals:    -1.59    0.51
# Exact a, adot, b, bdot, g, gdot:
  1.705671E-05  3.432765E-02 -9.767603E-06 -1.927012E-02  3.205233E-02 -7.597152E-04
# Covariance matrix:
  2.4473E-13 -4.7251E-14  7.9866E-17 -1.8974E-14  5.7743E-15  3.2497E-13
 -4.7251E-14  3.8226E-11  1.3796E-13 -2.1795E-11  2.5861E-11  3.6848E-10
  7.9866E-17  1.3796E-13  2.4466E-13 -1.5844E-13  9.4535E-14  1.3303E-12
 -1.8974E-14 -2.1795E-11 -1.5844E-13  1.2475E-11 -1.4746E-11 -2.1031E-10
  5.7743E-15  2.5861E-11  9.4535E-14 -1.4746E-11  1.7995E-11  2.4918E-10
  3.2497E-13  3.6848E-10  1.3303E-12 -2.1031E-10  2.4918E-10  3.5556E-09
#      lat0       lon0       xBary       yBary       zBary        JD0
   -2.874508  154.526827   -0.600575   -0.039648   -0.792666  2457479.745730
# Heliocentric elements and errors
Epoch:              2457470.5000  =  2016/03/23
Mean Anomaly:          359.15002 +/-     0.287
Argument of Peri:      187.06206 +/-     0.469
Long of Asc Node:      330.60939 +/-     0.000
Inclination:            29.31964 +/-     0.001
Eccentricity:         0.22732402 +/-    0.0002
Semi-Major Axis:     41.41231940 +/-    0.0122
Time of Perihelion: 2457700.3252 +/-      77.7
Perihelion:          31.99830457 +/-    0.0115
Aphelion:            50.82633423 +/-    0.0163
Period (y)              266.5033 +/-      0.12
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -29.10937925 +/-    0.0037
Ecliptic Y           13.19806677 +/-    0.0018
Ecliptic Z           -1.56488012 +/-    0.0002
Ecliptic XDOT        -0.00112798 +/-    0.0000
Ecliptic YDOT        -0.00271751 +/-    0.0000
Ecliptic ZDOT        -0.00164069 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   31.99990276 +/-    0.0035
Geocenter to KBO     31.19898459 +/-    0.0041
# Hcoef:  9.49

The following table shows the complete astrometric record for 19GK196. 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 (19GK196) followed by the observatory code and reference code for the source of the astrometry.

2016 04  01.244941 10 21 20.35   +07 10 20.3         19GK196   T09  C~8Zq9      
2016 04  01.263605 10 21 20.26   +07 10 20.5         19GK196   T09  C~8Zq9      
2016 04  01.328656 10 21 19.95   +07 10 21.8         19GK196   T09  C~8Zq9      
2016 04  01.350040 10 21 19.85   +07 10 22.3         19GK196   T09  C~8Zq9      
2016 04  01.416527 10 21 19.52   +07 10 23.6         19GK196   T09  C~8Zq9      
2016 04  01.441479 10 21 19.40   +07 10 24.0         19GK196   T09  C~8Zq9      
2019 01  09.527373 10 46 05.02   +01 28 39.7         19GK196   T09  C~8Zq9      
2019 04  07.33655  10 38 07.63   +01 57 39.1   25.5g 19GK196   T09  C~8Mho      
2019 04  07.36014  10 38 07.52   +01 57 39.8   25.2g 19GK196   T09  C~8Mho      
2019 04  07.37920  10 38 07.43   +01 57 40.3   25.7g 19GK196   T09  C~8Mho      
2019 04  08.24145  10 38 03.48   +01 57 59.2   23.4y 19GK196   T09  C~8Mho      
2019 04  08.27248  10 38 03.35   +01 58 01.2   23.3y 19GK196   T09  C~8Mho      
2019 04  08.33583  10 38 03.07   +01 58 03.5   23.6y 19GK196   T09  C~8Mho      
2019 04  08.36293  10 38 02.95   +01 58 03.7   24.2y 19GK196   T09  C~8Mho      
2019 05  08.33595  10 36 29.78   +02 06 45.4   25.3i 19GK196   T09  C~8Mho      
2019 05  08.36272  10 36 29.73   +02 06 45.6   24.6i 19GK196   T09  C~8Mho      
2019 05  08.39224  10 36 29.67   +02 06 45.9   24.5i 19GK196   T09  C~8Mho      
2019 05  08.39491  10 36 29.68   +02 06 46.3   24.7i 19GK196   T09  C~8Mho      
2019 05  31.263106 10 36 24.16   +02 07 43.4         19GK196   T09  C~8Zq9      
2019 05  31.333330 10 36 24.21   +02 07 42.9         19GK196   T09  C~8Zq9      
2019 06  08.258078 10 36 36.31   +02 06 40.6         19GK196   T09  C~8Zq9      
2019 06  08.316058 10 36 36.41   +02 06 40.0         19GK196   T09  C~8Zq9      

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    -0.03       0.00     0.05
     2   0.0001     -1.32     0.03      -0.30    -0.10
     3   0.0002     -6.09     0.06      -0.76    -0.03
     4   0.0003     -7.66     0.07      -0.83     0.07
     5   0.0005    -12.71    -0.07      -1.39     0.05
     6   0.0005    -14.52    -0.05      -1.67    -0.03
     7   2.7742  28370.35     0.18  -11015.38     0.12
     8   3.0146  20962.47    -0.07  -12021.90    -0.04
     9   3.0147  20960.66    -0.10  -12021.85     0.09
    10   3.0147  20959.20    -0.12  -12021.87     0.13
    11   3.0171  20896.45     0.02  -12025.90    -1.59
    12   3.0172  20893.87    -0.26  -12024.74    -0.33
    13   3.0174  20889.06    -0.38  -12024.12     0.50
    14   3.0174  20887.30    -0.14  -12024.60     0.11
    15   3.0995  19379.97     0.25  -12048.07     0.22
    16   3.0996  19379.19     0.18  -12048.16     0.13
    17   3.0997  19378.24     0.00  -12048.21     0.08
    18   3.0997  19378.23     0.07  -12047.78     0.51
    19   3.1623  19279.22     0.14  -12024.58     0.19
    20   3.1625  19280.11    -0.08  -12024.77    -0.05
    21   3.1842  19473.68     0.23  -12016.63    -0.02
    22   3.1843  19475.31     0.08  -12016.64    -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.

19GK196    quality flag:3

Type:         8:5EEE    8:5EEE    8:5EEE
Type:         8:5EII    8:5EII    8:5EII

axisobj        41.179    41.209    41.150
ecceobj         0.222     0.223     0.221
incobj         29.396    29.399    29.393
qmin           31.511    31.540    31.133
qmax           51.242    51.237    51.618
amean          41.188    41.188    41.188
amin           40.865    40.848    40.839
amax           41.575    41.580    41.578
emean           0.193     0.195     0.179
emin            0.153     0.156     0.127
emax            0.234     0.233     0.243
imean          31.047    31.022    31.232
imin           30.048    30.070    30.031
imax           31.598    31.543    32.119
excite_mean     0.551     0.551     0.550
fracstop        1.000     1.000     1.000
cjmean          2.696     2.695     2.696

libcent 0       179.2     179.1     180.2
libamp  0        50.4      42.6      75.3
libcent 1       181.7     181.7     179.6
libamp  1        67.7      61.1      93.9
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       180.3     180.2     182.4
kozaiamp         19.1      18.4      23.9