Orbit Fit and Astrometric record for 16PU298

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: 16PU298   
# Created Wed Nov 27 02:10:40 2024
# Orbit generated from Bernstein formalism
# Fitting     23 observations of     23
# Arc:  28.98d
# First observation: 2016/07/03
#  Last observation: 2016/08/01
Preliminary a, adot, b, bdot, g, gdot:
  -0.000001   0.055108  -0.000001  -0.003185   0.037978   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     8.14 DOF:     41 RMS:  0.11
# Min/Max residuals:    -0.31    0.22
# Exact a, adot, b, bdot, g, gdot:
  2.265699E-05  5.286389E-02 -1.315548E-06 -3.057694E-03  3.698691E-02 -2.401956E-03
# Covariance matrix:
  2.7306E-13 -3.6515E-11  2.4491E-15  2.0424E-12 -9.4076E-12  3.2145E-10
 -3.6515E-11  6.8441E-08 -2.6771E-11 -3.9069E-09  2.8235E-08  4.8997E-06
  2.4491E-15 -2.6771E-11  1.5137E-13 -8.6082E-13 -1.1497E-11 -2.1787E-09
  2.0424E-12 -3.9069E-09 -8.6082E-13  2.9720E-10 -1.6098E-09 -2.7781E-07
 -9.4076E-12  2.8235E-08 -1.1497E-11 -1.6098E-09  1.1850E-08  2.1353E-06
  3.2145E-10  4.8997E-06 -2.1787E-09 -2.7781E-07  2.1353E-06  4.1709E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.267364   -7.066683    0.958865    0.013261   -0.332312  2457573.074099
# Heliocentric elements and errors
Epoch:              2457570.5000  =  2016/07/01
Mean Anomaly:          354.34202 +/-    25.773
Argument of Peri:      160.78310 +/-    72.481
Long of Asc Node:      205.46853 +/-     0.464
Inclination:             3.94345 +/-     0.047
Eccentricity:         0.42581889 +/-    0.1068
Semi-Major Axis:     47.17848393 +/-    4.0643
Time of Perihelion: 2459430.7580 +/-    8470.3
Perihelion:          27.08899422 +/-    5.5524
Aphelion:            67.26797364 +/-    7.6788
Period (y)              324.0591 +/-     41.87
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           27.01864776 +/-    0.0789
Ecliptic Y           -4.31813538 +/-    0.0098
Ecliptic Z            1.06966250 +/-    0.0032
Ecliptic XDOT         0.00031496 +/-    0.0015
Ecliptic YDOT         0.00389712 +/-    0.0002
Ecliptic ZDOT        -0.00023321 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   27.38243594 +/-    0.0779
Geocenter to KBO     27.03659178 +/-    0.0796
# Hcoef:  8.94

The following table shows the complete astrometric record for 16PU298. 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 (16PU298) followed by the observatory code and reference code for the source of the astrometry.

2016 07  03.57331  23 30 27.66   -00 43 19.0   23.5r 16PU298   T09  C~89Tz      
2016 07  03.58369  23 30 27.65   -00 43 19.0   23.6r 16PU298   T09  C~89Tz      
2016 07  03.59409  23 30 27.64   -00 43 19.0   23.6r 16PU298   T09  C~89Tz      
2016 07  03.60455  23 30 27.63   -00 43 19.0   23.4r 16PU298   T09  C~89Tz      
2016 07  07.53078  23 30 23.45   -00 43 33.0   24.7g 16PU298   T09  C~89Tz      
2016 07  07.55077  23 30 23.43   -00 43 33.1   24.3g 16PU298   T09  C~89Tz      
2016 07  07.56088  23 30 23.42   -00 43 33.1   24.4g 16PU298   T09  C~89Tz      
2016 07  09.54573  23 30 20.55   -00 43 45.1   22.9y 16PU298   T09  C~89Tz      
2016 07  09.55995  23 30 20.51   -00 43 45.4   23.2y 16PU298   T09  C~89Tz      
2016 07  09.57417  23 30 20.50   -00 43 45.4   23.1y 16PU298   T09  C~89Tz      
2016 07  09.58875  23 30 20.49   -00 43 45.6   23.1y 16PU298   T09  C~89Tz      
2016 07  12.53976  23 30 15.32   -00 44 09.4   22.8z 16PU298   T09  C~89Tz      
2016 07  12.55404  23 30 15.30   -00 44 09.6   22.9z 16PU298   T09  C~89Tz      
2016 07  12.56833  23 30 15.26   -00 44 09.6   22.8z 16PU298   T09  C~89Tz      
2016 07  12.58266  23 30 15.23   -00 44 09.6   23.1z 16PU298   T09  C~89Tz      
2016 07  12.59705  23 30 15.21   -00 44 09.9   22.9z 16PU298   T09  C~89Tz      
2016 07  29.54752  23 29 26.06   -00 48 41.5   22.8z 16PU298   T09  C~89Tz      
2016 07  29.56202  23 29 25.99   -00 48 41.7   23.1z 16PU298   T09  C~89Tz      
2016 07  29.57647  23 29 25.94   -00 48 42.1   23.0z 16PU298   T09  C~89Tz      
2016 07  29.59087  23 29 25.89   -00 48 42.4   23.1z 16PU298   T09  C~89Tz      
2016 08  01.43913  23 29 14.63   -00 49 49.1   23.5z 16PU298   T09  C~89Tz      
2016 08  01.53573  23 29 14.23   -00 49 51.8   23.0z 16PU298   T09  C~89Tz      
2016 08  01.55739  23 29 14.12   -00 49 52.1   23.7z 16PU298   T09  C~89Tz      

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     0.00
     2   0.0000     -0.14    -0.01       0.06     0.02
     3   0.0001     -0.28    -0.00       0.12     0.04
     4   0.0001     -0.41     0.00       0.18     0.06
     5   0.0108    -63.54    -0.03      12.07    -0.02
     6   0.0109    -63.86     0.09      12.09    -0.06
     7   0.0109    -64.00     0.17      12.15    -0.04
     8   0.0164   -108.28     0.00      18.12     0.03
     9   0.0164   -108.95    -0.30      18.08    -0.06
    10   0.0164   -109.09    -0.06      18.14    -0.05
    11   0.0165   -109.31     0.10      18.02    -0.23
    12   0.0245   -189.95    -0.05      26.76     0.03
    13   0.0246   -190.30     0.05      26.70    -0.09
    14   0.0246   -190.85    -0.04      26.93     0.10
    15   0.0247   -191.27     0.00      27.11     0.22
    16   0.0247   -191.66     0.07      26.95     0.01
    17   0.0711   -976.20     0.06      68.42    -0.01
    18   0.0712   -977.24    -0.06      68.65     0.18
    19   0.0712   -978.09     0.00      68.58     0.07
    20   0.0712   -978.90     0.10      68.60     0.05
    21   0.0790  -1160.40     0.04      73.98     0.05
    22   0.0793  -1166.98     0.02      73.86    -0.31
    23   0.0794  -1168.61    -0.14      74.24     0.01

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.