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: 16FU59 # Created Fri Apr 26 01:17:51 2024 # Orbit generated from Bernstein formalism # Fitting 12 observations of 12 # Arc: 3.04d # First observation: 2016/03/29 # Last observation: 2016/04/01 # WARNING Fitting with energy constraint # WARNING and with gdot fixed = 0 # Chi-squared of fit: 32.66 DOF: 20 RMS: 0.29 # Min/Max residuals: -0.75 0.48 # Exact a, adot, b, bdot, g, gdot: 1.713150E-05 1.794200E-02 4.988034E-06 6.433176E-03 2.104149E-02 0.000000E+00 # Covariance matrix: 3.1024E-11 4.0686E-08 -9.0910E-14 -3.6386E-10 6.4913E-09 0.0000E+00 4.0686E-08 5.3960E-05 -1.2037E-10 -4.8194E-07 8.5978E-06 0.0000E+00 -9.0910E-14 -1.2037E-10 2.7296E-13 -4.2898E-11 -1.9185E-11 0.0000E+00 -3.6386E-10 -4.8194E-07 -4.2898E-11 1.7174E-08 -7.6809E-08 0.0000E+00 6.4913E-09 8.5978E-06 -1.9185E-11 -7.6809E-08 1.3703E-06 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 1.2259E-04 # lat0 lon0 xBary yBary zBary JD0 -8.986510 -174.007189 -0.045984 -0.155005 -0.981256 2457476.716889 # Heliocentric elements and errors Epoch: 2457470.5000 = 2016/03/23 Mean Anomaly: 9.31808 +/- 194.652 Argument of Peri: 325.71095 +/- 260.385 Long of Asc Node: 209.21138 +/- 8.656 Inclination: 21.48971 +/- 6.917 Eccentricity: 0.01388596 +/- 0.5642 Semi-Major Axis: 49.18423835 +/- 25.4322 Time of Perihelion: 2454209.4210 +/- 824061.4 Perihelion: 48.50126809 +/- 37.4019 Aphelion: 49.86720861 +/- 37.8791 Period (y) 344.9428 +/- 267.54 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -47.67216638 +/- 2.5972 Ecliptic Y -5.05317512 +/- 0.2724 Ecliptic Z -7.42329445 +/- 0.4130 Ecliptic XDOT 0.00011377 +/- 0.0014 Ecliptic YDOT -0.00234243 +/- 0.0008 Ecliptic ZDOT 0.00082680 +/- 0.0002 # Distances at JD0 (AU) Heliocenter to KBO 48.51056922 +/- 2.5533 Geocenter to KBO 47.52515149 +/- 2.6439 # Hcoef: 7.03
The following table shows the complete astrometric record for 16FU59. 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 (16FU59) followed by the observatory code and reference code for the source of the astrometry.
2016 03 29.21610 12 07 34.49 -10 37 19.9 23.9V 16FU59 W84 C~1qoK 2016 03 29.22304 12 07 34.51 -10 37 20.0 16FU59 W84 C~1qoK 2016 03 29.22998 12 07 34.51 -10 37 19.8 16FU59 W84 C~1qoK 2016 03 30.23733 12 07 30.55 -10 36 49.7 16FU59 W84 C~1qoK 2016 03 30.24427 12 07 30.54 -10 36 49.7 16FU59 W84 C~1qoK 2016 03 30.25121 12 07 30.53 -10 36 49.7 16FU59 W84 C~1qoK 2016 03 31.22984 12 07 26.68 -10 36 20.1 16FU59 W84 C~1qoK 2016 03 31.23678 12 07 26.68 -10 36 20.0 16FU59 W84 C~1qoK 2016 03 31.24372 12 07 26.68 -10 36 19.9 16FU59 W84 C~1qoK 2016 04 01.24388 12 07 22.73 -10 35 49.7 16FU59 W84 C~1qoK 2016 04 01.25082 12 07 22.75 -10 35 49.4 16FU59 W84 C~1qoK 2016 04 01.25776 12 07 22.75 -10 35 49.3 16FU59 W84 C~1qoK
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 -0.75 0.00 -0.03
2 0.0000 0.31 0.01 0.03 -0.03
3 0.0000 0.23 0.39 0.21 0.13
4 0.0028 -65.33 -0.16 4.26 0.06
5 0.0028 -65.47 0.16 4.20 -0.02
6 0.0028 -65.60 0.47 4.14 -0.11
7 0.0055 -129.48 -0.35 8.39 -0.07
8 0.0055 -129.52 0.07 8.48 -0.01
9 0.0056 -129.56 0.48 8.57 0.05
10 0.0083 -195.03 -0.63 12.77 -0.25
11 0.0083 -194.88 -0.03 13.16 0.12
12 0.0083 -194.92 0.38 13.25 0.18
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.
16FU59 quality flag:0 Type: ERR2LARGE ERR2LARGE ERR2LARGE axisobj 0.000 0.000 0.000 ecceobj -1.000 -1.000 -1.000 incobj -1.000 -1.000 -1.000 qmin 0.000 0.000 0.000 qmax 0.000 0.000 0.000 amean 0.000 0.000 0.000 amin 0.000 0.000 0.000 amax 0.000 0.000 0.000 emean 0.000 0.000 0.000 emin 0.000 0.000 0.000 emax 0.000 0.000 0.000 imean 0.000 0.000 0.000 imin 0.000 0.000 0.000 imax 0.000 0.000 0.000 excite_mean 0.000 0.000 0.000 fracstop 0.000 0.000 0.000 cjmean 0.000 0.000 0.000 libcent 0 -180.0 -180.0 -180.0 libamp 0 -180.0 -180.0 -180.0 libcent 1 -180.0 -180.0 -180.0 libamp 1 -180.0 -180.0 -180.0 libcent 2 -180.0 -180.0 -180.0 libamp 2 -180.0 -180.0 -180.0 libcent 3 -180.0 -180.0 -180.0 libamp 3 -180.0 -180.0 -180.0 libcent 4 -180.0 -180.0 -180.0 libamp 4 -180.0 -180.0 -180.0 kozaimean 0.0 0.0 0.0 kozaiamp 0.0 0.0 0.0