Orbit Fit and Astrometric record for 16GU370

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: 16GU370   
# Created Wed Nov 27 02:10:38 2024
# Orbit generated from Bernstein formalism
# Fitting     26 observations of     26
# Arc:  62.95d
# First observation: 2016/04/02
#  Last observation: 2016/06/04
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.031336  -0.000001  -0.003674   0.026340   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:    10.20 DOF:     47 RMS:  0.11
# Min/Max residuals:    -0.21    0.25
# Exact a, adot, b, bdot, g, gdot:
  1.576406E-05  2.602188E-02 -2.262294E-06 -3.897288E-03  2.549093E-02 -5.416686E-03
# Covariance matrix:
  1.8439E-13  1.2793E-10 -3.1665E-14  5.4956E-12  2.0088E-11 -2.3859E-09
  1.2793E-10  2.5350E-07 -6.5296E-11  1.1189E-08  3.8104E-08 -5.1403E-06
 -3.1665E-14 -6.5296E-11  1.0289E-13 -3.4499E-12 -9.7817E-12  1.3336E-09
  5.4956E-12  1.1189E-08 -3.4499E-12  5.0563E-10  1.6778E-09 -2.2806E-07
  2.0088E-11  3.8104E-08 -9.7817E-12  1.6778E-09  5.7456E-09 -7.6756E-07
 -2.3859E-09 -5.1403E-06  1.3336E-09 -2.2806E-07 -7.6756E-07  1.0569E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.960457 -176.310016   -0.157191    0.033773   -0.982546  2457480.887349
# Heliocentric elements and errors
Epoch:              2457480.5000  =  2016/04/02
Mean Anomaly:          316.17934 +/-    15.849
Argument of Peri:      234.43726 +/-    31.991
Long of Asc Node:       16.49274 +/-     0.296
Inclination:             8.71832 +/-     0.199
Eccentricity:         0.23831853 +/-    0.4078
Semi-Major Axis:     46.58319039 +/-   10.9423
Time of Perihelion: 2471616.2433 +/-    1153.5
Perihelion:          35.48155290 +/-   20.7432
Aphelion:            57.68482787 +/-   23.3328
Period (y)              317.9450 +/-    112.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -40.10010318 +/-    0.1163
Ecliptic Y           -2.74605764 +/-    0.0075
Ecliptic Z            1.34197013 +/-    0.0040
Ecliptic XDOT         0.00074592 +/-    0.0011
Ecliptic YDOT        -0.00275957 +/-    0.0000
Ecliptic ZDOT        -0.00043824 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.21641445 +/-    0.1160
Geocenter to KBO     39.22964044 +/-    0.1167
# Hcoef:  8.33

The following table shows the complete astrometric record for 16GU370. 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 (16GU370) followed by the observatory code and reference code for the source of the astrometry.

2016 04  02.38656  12 16 39.50   +00 19 56.7   23.7i 16GU370   T09  C~8COU      
2016 04  02.40035  12 16 39.42   +00 19 57.2   23.8i 16GU370   T09  C~8COU      
2016 04  02.41462  12 16 39.36   +00 19 57.5   23.7i 16GU370   T09  C~8COU      
2016 04  02.43920  12 16 39.25   +00 19 58.2   23.8i 16GU370   T09  C~8COU      
2016 04  02.46633  12 16 39.12   +00 19 58.9   23.9i 16GU370   T09  C~8COU      
2016 04  02.47448  12 16 39.08   +00 19 59.2   23.9i 16GU370   T09  C~8COU      
2016 04  02.49902  12 16 38.97   +00 19 59.7   23.9i 16GU370   T09  C~8COU      
2016 04  02.52059  12 16 38.86   +00 20 00.4   23.6i 16GU370   T09  C~8COU      
2016 04  04.34312  12 16 30.42   +00 20 50.0   25.6g 16GU370   T09  C~8COU      
2016 04  04.35452  12 16 30.38   +00 20 50.0   25.4g 16GU370   T09  C~8COU      
2016 04  04.36588  12 16 30.33   +00 20 50.3   25.3g 16GU370   T09  C~8COU      
2016 04  04.38727  12 16 30.22   +00 20 51.0   25.2g 16GU370   T09  C~8COU      
2016 04  04.39376  12 16 30.20   +00 20 51.3   25.4g 16GU370   T09  C~8COU      
2016 04  04.41084  12 16 30.11   +00 20 51.6   25.5g 16GU370   T09  C~8COU      
2016 04  04.41295  12 16 30.10   +00 20 52.0   25.2g 16GU370   T09  C~8COU      
2016 04  15.39732  12 15 40.83   +00 25 34.9   24.2y 16GU370   T09  C~8COV      
2016 04  15.41093  12 15 40.75   +00 25 35.6   24.1y 16GU370   T09  C~8COV      
2016 04  15.43760  12 15 40.65   +00 25 36.1   24.8y 16GU370   T09  C~8COV      
2016 04  15.45396  12 15 40.56   +00 25 36.7   23.5y 16GU370   T09  C~8COV      
2016 06  04.25886  12 13 16.72   +00 37 19.6   24.0z 16GU370   T09  C~8COV      
2016 06  04.27580  12 13 16.69   +00 37 19.6   23.7z 16GU370   T09  C~8COV      
2016 06  04.28656  12 13 16.68   +00 37 19.4   23.7z 16GU370   T09  C~8COV      
2016 06  04.30275  12 13 16.66   +00 37 19.6   24.1z 16GU370   T09  C~8COV      
2016 06  04.31085  12 13 16.66   +00 37 19.4   24.2z 16GU370   T09  C~8COV      
2016 06  04.32438  12 13 16.65   +00 37 19.4   23.9z 16GU370   T09  C~8COV      
2016 06  04.34057  12 13 16.63   +00 37 19.4   23.9z 16GU370   T09  C~8COV      

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     0.08       0.00    -0.03
     2   0.0000     -1.30    -0.17      -0.02    -0.01
     3   0.0001     -2.24    -0.03      -0.10    -0.04
     4   0.0001     -4.04     0.04      -0.11     0.02
     5   0.0002     -6.10     0.04      -0.24    -0.02
     6   0.0002     -6.77    -0.01      -0.21     0.04
     7   0.0003     -8.49     0.14      -0.40    -0.08
     8   0.0004    -10.28    -0.02      -0.41    -0.02
     9   0.0054   -146.17    -0.21      -5.14     0.08
    10   0.0054   -146.72     0.10      -5.38    -0.12
    11   0.0054   -147.52     0.15      -5.40    -0.10
    12   0.0055   -149.32    -0.03      -5.42    -0.04
    13   0.0055   -149.71     0.07      -5.26     0.13
    14   0.0055   -151.07    -0.00      -5.52    -0.07
    15   0.0055   -151.36    -0.14      -5.21     0.24
    16   0.0356   -941.98     0.25     -38.91    -0.16
    17   0.0357   -943.36    -0.17     -38.75     0.06
    18   0.0357   -944.94     0.13     -38.88     0.02
    19   0.0358   -946.41    -0.20     -38.87     0.10
    20   0.1721  -3205.94    -0.01    -250.02     0.18
    21   0.1722  -3206.36    -0.15    -250.20     0.09
    22   0.1722  -3206.42    -0.04    -250.44    -0.09
    23   0.1723  -3206.77    -0.14    -250.38     0.06
    24   0.1723  -3206.69     0.07    -250.56    -0.08
    25   0.1723  -3206.83     0.14    -250.62    -0.07
    26   0.1724  -3207.10     0.12    -250.74    -0.10

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.