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: 16GA391
# Created Wed Nov 27 02:10:38 2024
# Orbit generated from Bernstein formalism
# Fitting 13 observations of 13
# Arc: 6.13d
# First observation: 2016/04/02
# Last observation: 2016/04/08
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit: 6.02 DOF: 22 RMS: 0.12
# Min/Max residuals: -0.21 0.22
# Exact a, adot, b, bdot, g, gdot:
1.136807E-05 1.028687E-02 1.291601E-06 1.150005E-03 1.392990E-02 0.000000E+00
# Covariance matrix:
1.4840E-11 1.2744E-08 5.6898E-14 5.7803E-11 2.0729E-09 0.0000E+00
1.2744E-08 1.1098E-05 4.9494E-11 5.0279E-08 1.8031E-06 0.0000E+00
5.6898E-14 4.9494E-11 1.7589E-13 -1.1519E-11 8.0429E-12 0.0000E+00
5.7803E-11 5.0279E-08 -1.1519E-11 2.4292E-09 8.1705E-09 0.0000E+00
2.0729E-09 1.8031E-06 8.0429E-12 8.1705E-09 2.9300E-07 0.0000E+00
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 3.5569E-05
# lat0 lon0 xBary yBary zBary JD0
1.265746 -176.285292 -0.156766 0.021859 -0.982951 2457480.887349
# Heliocentric elements and errors
Epoch: 2457480.5000 = 2016/04/02
Mean Anomaly: 5.18435 +/- 204.344
Argument of Peri: 5.68969 +/- 270.943
Long of Asc Node: 172.76825 +/- 3.365
Inclination: 6.47537 +/- 1.933
Eccentricity: 0.02494999 +/- 0.5354
Semi-Major Axis: 74.62902720 +/- 38.0888
Time of Perihelion: 2454089.3117 +/- 840111.2
Perihelion: 72.76703351 +/- 54.5528
Aphelion: 76.49102089 +/- 55.8640
Period (y) 644.7181 +/- 493.57
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -72.59440215 +/- 2.7831
Ecliptic Y -4.87289764 +/- 0.1804
Ecliptic Z 1.58588608 +/- 0.0616
Ecliptic XDOT 0.00013608 +/- 0.0012
Ecliptic YDOT -0.00202424 +/- 0.0006
Ecliptic ZDOT 0.00022598 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 72.77504648 +/- 2.7762
Geocenter to KBO 71.78802055 +/- 2.7896
# Hcoef: 7.26
The following table shows the complete astrometric record for 16GA391. 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 (16GA391) followed by the observatory code and reference code for the source of the astrometry.
2016 04 02.38656 12 15 38.76 -00 18 54.1 26.0i 16GA391 T09 C~8HFs 2016 04 02.40651 12 15 38.70 -00 18 53.7 25.5i 16GA391 T09 C~8HFs 2016 04 02.41462 12 15 38.69 -00 18 53.6 25.5i 16GA391 T09 C~8HFs 2016 04 02.43374 12 15 38.62 -00 18 53.2 25.4i 16GA391 T09 C~8HFs 2016 04 02.48823 12 15 38.49 -00 18 52.4 25.7i 16GA391 T09 C~8HFs 2016 04 02.51252 12 15 38.41 -00 18 51.9 25.1i 16GA391 T09 C~8HFs 2016 04 04.34312 12 15 33.64 -00 18 20.1 26.7g 16GA391 T09 C~8HFs 2016 04 04.35952 12 15 33.59 -00 18 19.3 26.6g 16GA391 T09 C~8HFs 2016 04 04.36588 12 15 33.58 -00 18 19.3 26.4g 16GA391 T09 C~8HFs 2016 04 08.50449 12 15 22.88 -00 17 08.1 26.0r 16GA391 T09 C~8HFs 2016 04 08.50945 12 15 22.84 -00 17 08.1 25.2r 16GA391 T09 C~8HFs 2016 04 08.51156 12 15 22.84 -00 17 08.1 25.5r 16GA391 T09 C~8HFs 2016 04 08.51792 12 15 22.84 -00 17 07.9 25.6r 16GA391 T09 C~8HFs
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 0.06 0.00 0.00
2 0.0001 -0.98 -0.05 0.01 0.01
3 0.0001 -1.16 0.13 0.04 0.04
4 0.0001 -2.28 -0.16 -0.01 -0.01
5 0.0003 -4.39 0.12 -0.05 -0.07
6 0.0003 -5.69 -0.12 -0.06 -0.09
7 0.0054 -83.99 0.15 0.72 -0.21
8 0.0054 -84.99 -0.14 1.16 0.22
9 0.0054 -85.13 -0.01 1.10 0.16
10 0.0167 -260.70 0.16 2.74 0.12
11 0.0168 -261.25 -0.18 2.50 -0.12
12 0.0168 -261.25 -0.09 2.50 -0.12
13 0.0168 -261.33 0.10 2.68 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.