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: 14WJ602 # Created Wed May 8 01:16:44 2024 # Orbit generated from Bernstein formalism # Fitting 15 observations of 15 # Arc: 3.98y # First observation: 2014/11/21 # Last observation: 2018/11/15 Preliminary a, adot, b, bdot, g, gdot: 0.000205 0.019513 -0.000039 -0.000106 0.021901 0.000000 # Chi-squared of fit: 3.45 DOF: 24 RMS: 0.08 # Min/Max residuals: -0.16 0.18 # Exact a, adot, b, bdot, g, gdot: 1.468253E-05 1.993359E-02 -1.423823E-07 -1.231931E-04 2.155232E-02 6.133577E-03 # Covariance matrix: 4.5215E-13 -4.4791E-13 5.8404E-15 1.0150E-16 -1.0541E-13 -4.6599E-12 -4.4791E-13 8.3329E-13 -4.2461E-15 -6.6467E-15 -1.8562E-14 1.0730E-11 5.8404E-15 -4.2461E-15 2.9371E-13 -1.1862E-13 -2.7519E-14 -6.1981E-14 1.0150E-16 -6.6467E-15 -1.1862E-13 7.2655E-14 1.9357E-14 -9.2227E-14 -1.0541E-13 -1.8562E-14 -2.7519E-14 1.9357E-14 7.8394E-13 -2.0149E-13 -4.6599E-12 1.0730E-11 -6.1981E-14 -9.2227E-14 -2.0149E-13 1.5128E-10 # lat0 lon0 xBary yBary zBary JD0 -24.792875 10.196170 -0.737299 -0.275925 -0.597820 2456982.712828 # Heliocentric elements and errors Epoch: 2456980.5000 = 2014/11/19 Mean Anomaly: 52.61430 +/- 0.058 Argument of Peri: 180.70277 +/- 0.024 Long of Asc Node: 101.41820 +/- 0.002 Inclination: 24.45453 +/- 0.000 Eccentricity: 0.32532912 +/- 0.0006 Semi-Major Axis: 52.83692024 +/- 0.0302 Time of Perihelion: 2436478.0393 +/- 14.1 Perihelion: 35.64753157 +/- 0.0394 Aphelion: 70.02630891 +/- 0.0523 Period (y) 384.0736 +/- 0.33 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 41.97163522 +/- 0.0017 Ecliptic Y 8.30035921 +/- 0.0003 Ecliptic Z -19.45687298 +/- 0.0008 Ecliptic XDOT 0.00023722 +/- 0.0000 Ecliptic YDOT 0.00261129 +/- 0.0000 Ecliptic ZDOT -0.00034084 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 47.00089395 +/- 0.0016 Geocenter to KBO 46.39872451 +/- 0.0019 # Hcoef: 6.74
The following table shows the complete astrometric record for 14WJ602. 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 (14WJ602) followed by the observatory code and reference code for the source of the astrometry.
2014 11 21.21205 01 17 30.485 -18 42 43.38 23.1i 14WJ602 W84 C~55TE 2014 12 12.15687 01 16 36.528 -18 37 56.01 23.0z 14WJ602 W84 C~55TE 2015 01 09.06894 01 16 17.154 -18 24 01.72 24.3r 14WJ602 W84 C~55TE 2015 10 07.22227 01 24 53.604 -18 06 31.81 23.0r 14WJ602 W84 C~55TE 2015 11 06.11613 01 22 47.918 -18 14 42.97 23.2r 14WJ602 W84 C~55TE 2015 11 07.14158 01 22 43.881 -18 14 49.08 23.1i 14WJ602 W84 C~55TE 2015 11 07.14296 01 22 43.883 -18 14 49.10 24.7g 14WJ602 W84 C~55TE 2016 09 30.28598 01 29 35.719 -17 35 26.80 23.1r 14WJ602 W84 C~55TE 2016 09 30.28871 01 29 35.700 -17 35 27.17 24.4g 14WJ602 W84 C~55TE 2016 12 05.16148 01 25 26.484 -17 44 38.74 23.0i 14WJ602 W84 C~55TE 2016 12 05.16285 01 25 26.485 -17 44 38.67 23.7r 14WJ602 W84 C~55TE 2017 11 17.12045 01 30 33.952 -17 19 14.78 23.2i 14WJ602 W84 C~55TE 2017 11 17.12183 01 30 33.930 -17 19 14.73 24.1g 14WJ602 W84 C~55TE 2017 11 27.06486 01 30 01.075 -17 18 29.69 23.3i 14WJ602 W84 C~55TE 2018 11 15.21902 01 34 49.701 -16 51 16.14 23.4r 14WJ602 W84 C~55TE
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 0.01 2 0.0573 -579.77 -0.08 578.24 -0.07 3 0.1338 -487.14 -0.03 1451.99 0.03 4 0.8761 6639.18 0.01 -663.61 -0.09 5 0.9580 4806.33 0.06 -354.24 0.07 6 0.9608 4751.54 0.06 -335.63 0.03 7 0.9608 4751.55 0.15 -335.66 -0.02 8 1.8592 11086.30 0.07 -689.80 0.18 9 1.8592 11085.90 -0.16 -690.02 -0.04 10 2.0396 7620.85 -0.05 328.42 -0.09 11 2.0396 7620.89 0.02 328.47 -0.08 12 2.9895 12259.60 0.10 -168.20 -0.01 13 2.9895 12259.33 -0.10 -168.02 0.14 14 3.0167 11852.27 -0.12 74.92 0.05 15 3.9836 16311.31 0.09 -237.82 -0.11
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.
14WJ602 quality flag:3 Type: 7:3EEEE 7:3EEEE 7:3EEEE Type: 7:3EEII axisobj 53.420 53.509 53.331 ecceobj 0.329 0.330 0.327 incobj 24.460 24.460 24.460 qmin 35.260 34.535 35.255 qmax 71.598 72.404 71.487 amean 52.968 52.968 52.968 amin 52.350 52.276 52.446 amax 53.694 53.798 53.631 emean 0.300 0.332 0.257 emin 0.250 0.317 0.134 emax 0.334 0.348 0.333 imean 24.015 22.636 25.357 imin 22.760 22.106 22.758 imax 25.777 22.996 28.430 excite_mean 0.506 0.508 0.503 fracstop 1.000 1.000 1.000 cjmean 2.879 2.878 2.880 libcent 0 185.5 177.1 119.2 libamp 0 137.0 158.6 108.8 libcent 1 -180.0 -180.0 210.5 libamp 1 -180.0 -180.0 72.4 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 220.0 209.3 202.1 kozaiamp 180.0 179.9 34.8