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: 15OL194 # Created Wed May 21 01:10:34 2025 # Orbit generated from Bernstein formalism # Fitting 10 observations of 10 # Arc: 8.03d # First observation: 2015/07/15 # Last observation: 2015/07/23 Preliminary a, adot, b, bdot, g, gdot: -0.000000 0.040568 0.000000 -0.013855 0.030502 0.000000 # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # WARNING Fitting with energy constraint # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # Chi-squared of fit: 3.51 DOF: 15 RMS: 0.10 # Min/Max residuals: -0.17 0.32 # Exact a, adot, b, bdot, g, gdot: 1.760737E-05 3.171968E-02 -6.682057E-06 -1.223911E-02 2.848155E-02 -2.776296E-03 # Covariance matrix: 7.5137E-12 1.3004E-08 -1.3481E-12 -2.3540E-09 2.8952E-09 1.0439E-08 1.3004E-08 2.4058E-05 -2.4895E-09 -4.3471E-06 5.3465E-06 1.8966E-05 -1.3481E-12 -2.4895E-09 7.1704E-13 4.2700E-10 -5.5329E-10 -2.0051E-09 -2.3540E-09 -4.3471E-06 4.2700E-10 7.8723E-07 -9.6615E-07 -3.4778E-06 2.8952E-09 5.3465E-06 -5.5329E-10 -9.6615E-07 1.1883E-06 4.3808E-06 1.0439E-08 1.8966E-05 -2.0051E-09 -3.4778E-06 4.3808E-06 3.9833E-04 # lat0 lon0 xBary yBary zBary JD0 11.052524 -20.373138 0.743917 0.133199 -0.681417 2457218.974529 # Heliocentric elements and errors Epoch: 2457210.5000 = 2015/07/07 Mean Anomaly: 347.60804 +/- 64.213 Argument of Peri: 176.24437 +/- 133.547 Long of Asc Node: 184.54867 +/- 1.971 Inclination: 23.49006 +/- 1.517 Eccentricity: 0.31070123 +/- 0.3205 Semi-Major Axis: 50.83345257 +/- 15.3080 Time of Perihelion: 2461767.3025 +/- 23522.8 Perihelion: 35.03943636 +/- 19.4098 Aphelion: 66.62746879 +/- 25.8452 Period (y) 362.4371 +/- 163.72 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 32.69232558 +/- 1.2363 Ecliptic Y -12.93519683 +/- 0.4592 Ecliptic Z 6.73081029 +/- 0.2576 Ecliptic XDOT 0.00102512 +/- 0.0018 Ecliptic YDOT 0.00286476 +/- 0.0007 Ecliptic ZDOT -0.00120579 +/- 0.0004 # Distances at JD0 (AU) Heliocenter to KBO 35.79680538 +/- 1.1423 Geocenter to KBO 35.11045151 +/- 1.3438 # Hcoef: 7.85
The following table shows the complete astrometric record for 15OL194. 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 (15OL194) followed by the observatory code and reference code for the source of the astrometry.
2015 07 15.47374 22 28 10.17 +02 17 28.4 23.4r 15OL194 T09 C~8r6x 2015 07 15.47587 22 28 10.16 +02 17 28.4 23.3r 15OL194 T09 C~8r6x 2015 07 15.49326 22 28 10.10 +02 17 28.2 22.7r 15OL194 T09 C~8r6x 2015 07 22.42468 22 27 45.76 +02 15 48.1 23.6z 15OL194 T09 C~8r6x 2015 07 22.44091 22 27 45.71 +02 15 47.7 23.7z 15OL194 T09 C~8r6x 2015 07 22.46248 22 27 45.64 +02 15 47.6 23.0z 15OL194 T09 C~8r6x 2015 07 22.48140 22 27 45.55 +02 15 47.2 23.3z 15OL194 T09 C~8r6x 2015 07 23.45259 22 27 41.87 +02 15 30.6 23.5y 15OL194 T09 C~8r6x 2015 07 23.47699 22 27 41.78 +02 15 30.1 23.1y 15OL194 T09 C~8r6x 2015 07 23.49892 22 27 41.69 +02 15 29.8 23.1y 15OL194 T09 C~8r6x
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 -0.02
2 0.0000 -0.14 -0.03 0.06 0.02
3 0.0001 -1.05 -0.05 0.21 0.04
4 0.0190 -376.86 -0.07 43.50 0.02
5 0.0191 -377.70 0.05 43.40 -0.17
6 0.0191 -378.71 0.32 43.70 0.00
7 0.0192 -380.11 0.05 43.84 0.02
8 0.0218 -437.48 -0.14 49.02 0.07
9 0.0219 -438.92 -0.09 49.06 -0.03
10 0.0220 -440.28 -0.12 49.29 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.
15OL194 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