Orbit Fit and Astrometric record for 17DE168

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: 17DE168   
# Created Wed Nov 27 02:10:49 2024
# Orbit generated from Bernstein formalism
# Fitting      9 observations of      9
# Arc:   2.15d
# First observation: 2017/02/21
#  Last observation: 2017/02/23
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit:     2.36 DOF:     14 RMS:  0.09
# Min/Max residuals:    -0.24    0.17
# Exact a, adot, b, bdot, g, gdot:
  1.168198E-05  1.345768E-02 -5.444752E-06 -7.593329E-03  1.822949E-02  0.000000E+00
# Covariance matrix:
  3.3855E-11  3.8702E-08 -2.0583E-12 -2.3577E-09  7.5332E-09  0.0000E+00
  3.8702E-08  4.4578E-05 -2.3680E-09 -2.7124E-06  8.6667E-06  0.0000E+00
 -2.0583E-12 -2.3680E-09  3.1818E-13  1.1831E-10 -4.6061E-10  0.0000E+00
 -2.3577E-09 -2.7124E-06  1.1831E-10  1.8805E-07 -5.2761E-07  0.0000E+00
  7.5332E-09  8.6667E-06 -4.6061E-10 -5.2761E-07  1.6858E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  7.9716E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
    4.876805 -170.921314    0.588739    0.067632   -0.790827  2457806.006401
# Heliocentric elements and errors
Epoch:              2457800.5000  =  2017/02/16
Mean Anomaly:          333.23471 +/-   123.560
Argument of Peri:      198.08763 +/-   193.264
Long of Asc Node:       16.96835 +/-     3.651
Inclination:            29.65343 +/-    10.659
Eccentricity:         0.02056197 +/-    0.5764
Semi-Major Axis:     56.68987630 +/-   29.2386
Time of Perihelion: 2469391.6394 +/-  677065.6
Perihelion:          55.52422082 +/-   43.4489
Aphelion:            57.85553179 +/-   44.2506
Period (y)              426.8413 +/-    330.22
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -54.85269902 +/-    3.8442
Ecliptic Y           -8.17325620 +/-    0.6140
Ecliptic Z            4.66321877 +/-    0.3322
Ecliptic XDOT         0.00022632 +/-    0.0013
Ecliptic YDOT        -0.00201782 +/-    0.0009
Ecliptic ZDOT        -0.00113637 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   55.65398742 +/-    3.7901
Geocenter to KBO     54.85617902 +/-    3.9071
# Hcoef:  7.22

The following table shows the complete astrometric record for 17DE168. 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 (17DE168) followed by the observatory code and reference code for the source of the astrometry.

2017 02  21.50560  12 41 01.96   +00 53 09.0   24.5z 17DE168   T09  C~86uz      
2017 02  21.50898  12 41 01.96   +00 53 09.3   24.2z 17DE168   T09  C~86uz      
2017 02  21.52849  12 41 01.90   +00 53 09.7   24.3z 17DE168   T09  C~86uz      
2017 02  21.54193  12 41 01.86   +00 53 09.8   24.1z 17DE168   T09  C~86uz      
2017 02  21.57429  12 41 01.77   +00 53 10.5   24.5z 17DE168   T09  C~86uz      
2017 02  21.61448  12 41 01.67   +00 53 11.0   24.4z 17DE168   T09  C~86uz      
2017 02  23.55566  12 40 56.21   +00 53 43.8   24.7r 17DE168   T09  C~86uz      
2017 02  23.62285  12 40 56.02   +00 53 44.8   25.1r 17DE168   T09  C~86uz      
2017 02  23.65247  12 40 55.93   +00 53 45.5   25.0r 17DE168   T09  C~86uz      

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    -0.00       0.00    -0.24
     2   0.0000     -0.12     0.03       0.28     0.04
     3   0.0001     -1.10    -0.06       0.29     0.08
     4   0.0001     -1.69    -0.04       0.15    -0.04
     5   0.0002     -3.21    -0.09       0.26     0.11
     6   0.0003     -4.79     0.17       0.13     0.04
     7   0.0056    -92.98    -0.05      -1.88     0.01
     8   0.0058    -95.99     0.09      -2.08    -0.09
     9   0.0059    -97.51    -0.04      -1.96     0.07

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.