Orbit Fit and Astrometric record for 16PV298

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: 16PV298   
# Created Wed Nov 27 02:10:40 2024
# Orbit generated from Bernstein formalism
# Fitting     23 observations of     23
# Arc:  36.99d
# First observation: 2016/07/03
#  Last observation: 2016/08/09
Preliminary a, adot, b, bdot, g, gdot:
  -0.000001   0.031885   0.000000  -0.006767   0.028040   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     4.42 DOF:     41 RMS:  0.08
# Min/Max residuals:    -0.16    0.17
# Exact a, adot, b, bdot, g, gdot:
  1.807855E-05  3.000747E-02 -3.393486E-06 -6.589725E-03  2.727077E-02 -3.033085E-03
# Covariance matrix:
  2.3565E-13 -4.1275E-11  6.4114E-15  2.9880E-12 -1.3222E-11 -1.3772E-09
 -4.1275E-11  4.5231E-08 -7.5781E-12 -3.9052E-09  1.7096E-08  2.6369E-06
  6.4114E-15 -7.5781E-12  1.5944E-13 -1.4424E-12 -2.8730E-12 -4.4556E-10
  2.9880E-12 -3.9052E-09 -1.4424E-12  3.8745E-10 -1.4922E-09 -2.3621E-07
 -1.3222E-11  1.7096E-08 -2.8730E-12 -1.4922E-09  6.5271E-09  1.0311E-06
 -1.3772E-09  2.6369E-06 -4.4556E-10 -2.3621E-07  1.0311E-06  1.7288E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.563501   -7.182846    0.958188    0.015065   -0.334180  2457573.074099
# Heliocentric elements and errors
Epoch:              2457570.5000  =  2016/07/01
Mean Anomaly:          335.33493 +/-    55.945
Argument of Peri:      207.64817 +/-   102.195
Long of Asc Node:      182.73527 +/-     0.178
Inclination:            12.64019 +/-     0.193
Eccentricity:         0.23035092 +/-    0.2962
Semi-Major Axis:     46.05092516 +/-    5.5650
Time of Perihelion: 2465391.0233 +/-   17681.7
Perihelion:          35.44305214 +/-   14.2985
Aphelion:            56.65879818 +/-   15.2638
Period (y)              312.5113 +/-     56.65
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           36.55357090 +/-    0.1077
Ecliptic Y           -5.57493034 +/-    0.0136
Ecliptic Z            1.64002801 +/-    0.0049
Ecliptic XDOT         0.00010520 +/-    0.0013
Ecliptic YDOT         0.00301628 +/-    0.0002
Ecliptic ZDOT        -0.00067454 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   37.01260712 +/-    0.1064
Geocenter to KBO     36.66929961 +/-    0.1086
# Hcoef:  8.20

The following table shows the complete astrometric record for 16PV298. 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 (16PV298) followed by the observatory code and reference code for the source of the astrometry.

2016 07  03.57331  23 29 34.01   -00 29 44.4   24.1r 16PV298   T09  C~89Tz      
2016 07  03.58369  23 29 34.01   -00 29 44.2   24.3r 16PV298   T09  C~89Tz      
2016 07  03.59409  23 29 34.00   -00 29 44.4   24.1r 16PV298   T09  C~89Tz      
2016 07  03.60455  23 29 33.99   -00 29 44.4   24.3r 16PV298   T09  C~89Tz      
2016 07  07.53078  23 29 29.84   -00 30 09.9   25.3g 16PV298   T09  C~89Tz      
2016 07  07.54078  23 29 29.83   -00 30 10.1   25.3g 16PV298   T09  C~89Tz      
2016 07  07.55077  23 29 29.82   -00 30 10.2   25.3g 16PV298   T09  C~89Tz      
2016 07  07.56088  23 29 29.81   -00 30 10.2   25.2g 16PV298   T09  C~89Tz      
2016 07  12.53976  23 29 22.51   -00 30 56.6   23.5z 16PV298   T09  C~89Tz      
2016 07  12.55404  23 29 22.50   -00 30 56.6   23.3z 16PV298   T09  C~89Tz      
2016 07  12.56833  23 29 22.46   -00 30 56.9   23.4z 16PV298   T09  C~89Tz      
2016 07  12.58266  23 29 22.45   -00 30 57.1   23.3z 16PV298   T09  C~89Tz      
2016 07  29.54752  23 28 41.75   -00 35 24.4   23.5z 16PV298   T09  C~89Tz      
2016 07  29.56202  23 28 41.71   -00 35 24.7   23.4z 16PV298   T09  C~89Tz      
2016 07  29.57647  23 28 41.67   -00 35 25.0   23.4z 16PV298   T09  C~89Tz      
2016 07  29.59087  23 28 41.62   -00 35 25.4   23.6z 16PV298   T09  C~89Tz      
2016 08  01.43571  23 28 32.62   -00 36 25.7   23.2z 16PV298   T09  C~89Tz      
2016 08  01.53573  23 28 32.28   -00 36 27.8   23.3z 16PV298   T09  C~89Tz      
2016 08  01.55739  23 28 32.21   -00 36 28.4   23.4z 16PV298   T09  C~89Tz      
2016 08  01.58729  23 28 32.11   -00 36 29.0   23.0z 16PV298   T09  C~89Tz      
2016 08  09.42245  23 28 04.39   -00 39 36.6   23.7y 16PV298   T09  C~89Tz      
2016 08  09.50129  23 28 04.08   -00 39 38.6   24.0y 16PV298   T09  C~89Tz      
2016 08  09.56495  23 28 03.82   -00 39 40.3   23.5y 16PV298   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    -0.14       0.00    -0.09
     2   0.0000      0.08     0.10       0.18     0.09
     3   0.0001     -0.14     0.04       0.06    -0.05
     4   0.0001     -0.28     0.06       0.12     0.00
     5   0.0108    -67.53    -0.07       1.26     0.16
     6   0.0109    -67.75    -0.07       1.13     0.03
     7   0.0109    -67.93    -0.04       1.10    -0.01
     8   0.0109    -68.07     0.04       1.16     0.04
     9   0.0245   -186.99    -0.10       1.74    -0.03
    10   0.0246   -187.12     0.17       1.80     0.02
    11   0.0246   -187.79    -0.09       1.76    -0.02
    12   0.0247   -188.01     0.11       1.63    -0.16
    13   0.0711   -854.43    -0.11      -3.05     0.05
    14   0.0712   -855.10    -0.03      -3.09     0.02
    15   0.0712   -855.76     0.05      -3.12    -0.02
    16   0.0712   -856.61    -0.06      -3.20    -0.09
    17   0.0790  -1004.45     0.05      -5.33    -0.03
    18   0.0793  -1009.96     0.03      -5.25     0.08
    19   0.0794  -1011.16     0.03      -5.38    -0.05
    20   0.0794  -1012.78     0.06      -5.34     0.00
    21   0.1009  -1468.86     0.09     -13.65    -0.03
    22   0.1011  -1473.92     0.04     -13.65     0.03
    23   0.1013  -1478.17    -0.16     -13.67     0.05

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.