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: 136120 # Created Fri Nov 22 02:06:54 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 20 observations of 20 # Arc: 11.00y # First observation: 2003/06/01 # Last observation: 2014/05/30 # Chi-squared of fit: 35.44 DOF: 34 RMS: 0.24 # Min/Max residuals: -0.48 0.51 # Exact a, adot, b, bdot, g, gdot: 1.915846E-05 3.911576E-02 6.277393E-06 1.429775E-02 3.139658E-02 3.440939E-03 # Covariance matrix: 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 # lat0 lon0 xBary yBary zBary JD0 -0.642702 -123.795194 -0.250769 -0.011034 -0.985662 2452791.706733 # Heliocentric elements and errors Epoch: 2452792.5000 = 2003/06/02 Mean Anomaly: 5.07117 +/- 0.000 Argument of Peri: 341.91647 +/- 0.000 Long of Asc Node: 238.33732 +/- 0.000 Inclination: 20.11919 +/- 0.000 Eccentricity: 0.47938182 +/- 0.0000 Semi-Major Axis: 62.25080501 +/- 0.0000 Time of Perihelion: 2450265.4037 +/- 0.0 Perihelion: 32.40890110 +/- 0.0000 Aphelion: 92.09270891 +/- 0.0000 Period (y) 491.1630 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -18.05673971 +/- 0.0000 Ecliptic Y -27.42208548 +/- 0.0000 Ecliptic Z -0.35706804 +/- 0.0000 Ecliptic XDOT 0.00265405 +/- 0.0000 Ecliptic YDOT -0.00216338 +/- 0.0000 Ecliptic ZDOT 0.00124354 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 32.83504384 +/- 0.0000 Geocenter to KBO 31.85058724 +/- 0.0000 # Hcoef: 7.47
The following table shows the complete astrometric record for 136120. 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 (136120) followed by the observatory code and reference code for the source of the astrometry.
2003 06 01.20599 15 34 54.79 -19 55 40.1 22.3R 136120 807 Ci2139 2003 06 02.14031 15 34 49.47 -19 55 14.2 136120 807 Ci2139 2003 06 02.20299 15 34 49.14 -19 55 11.8 136120 807 Ci2139 2003 07 06.30907 15 32 10.07 -19 41 01.7 22.9R 136120 568 Ci2707 2003 07 06.38996 15 32 09.79 -19 40 59.8 136120 568 Ci2707 2004 07 15.09464 15 41 37.04 -19 21 50.8 22.6R 136120 807 Cn5943 2004 07 16.01386 15 41 34.72 -19 21 36.0 136120 807 Cn5943 2004 07 16.05665 15 41 34.61 -19 21 35.2 136120 807 Cn5943 2005 05 10.23355 15 56 58.44 -19 28 41.8 22.5R 136120 807 Cn5342 2005 05 10.30035 15 56 58.04 -19 28 39.7 136120 807 Cn5342 2005 05 11.16077 15 56 53.05 -19 28 17.8 136120 807 Cn5342 2006 05 04.41951 16 07 19.48 -19 09 52.5 22.9R 136120 250 S~06HM 2006 05 04.42391 16 07 19.45 -19 09 52.4 136120 250 S~06HM 2006 05 04.42831 16 07 19.43 -19 09 52.3 136120 250 S~06HM 2006 05 04.43270 16 07 19.41 -19 09 52.2 136120 250 S~06HM 2006 06 22.03890 16 02 43.51 -18 50 51.6 23.1R 136120 304 Cr4835 2006 06 22.07397 16 02 43.32 -18 50 50.9 136120 304 Cr4835 2014 05 30.26483 17 17 21.63 -15 22 33.6 20.3R 136120 695 C~1LoQ 2014 05 30.39545 17 17 20.89 -15 22 31.5 136120 695 C~1LoQ 2014 05 30.43229 17 17 20.66 -15 22 31.0 136120 695 C~1LoQ
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 0.16 0.00 0.16
2 0.0026 0.00 -0.05 0.00 -0.14
3 0.0027 0.00 0.43 0.00 0.51
4 0.0961 0.00 -0.34 0.00 -0.10
5 0.0963 0.00 -0.40 0.00 0.13
6 1.1222 0.00 0.01 0.00 0.06
7 1.1247 0.00 0.24 0.00 0.11
8 1.1248 0.00 0.26 0.00 0.23
9 1.9412 0.00 -0.06 0.00 -0.21
10 1.9414 0.00 -0.17 0.00 0.18
11 1.9438 0.00 -0.48 0.00 0.13
12 2.9246 0.00 0.26 0.00 -0.31
13 2.9246 0.00 0.17 0.00 -0.31
14 2.9246 0.00 0.23 0.00 -0.32
15 2.9246 0.00 0.29 0.00 -0.32
16 3.0577 0.00 0.21 0.00 0.02
17 3.0578 0.00 0.05 0.00 0.01
18 10.9954 0.00 0.11 0.00 0.06
19 10.9957 0.00 0.07 0.00 0.16
20 10.9958 0.00 -0.26 0.00 0.09
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.
136120 quality flag:3 Type: 3:1EE 3:1EE 3:1EE axisobj 61.527 61.527 61.527 ecceobj 0.473 0.473 0.473 incobj 20.151 20.151 20.151 qmin 31.851 31.633 31.871 qmax 95.652 95.787 95.767 amean 62.628 62.632 62.632 amin 61.527 61.527 61.527 amax 64.047 64.082 64.109 emean 0.481 0.481 0.481 emin 0.468 0.469 0.469 emax 0.493 0.495 0.495 imean 21.304 21.194 21.269 imin 21.018 20.551 20.996 imax 21.595 21.617 21.593 excite_mean 0.602 0.602 0.602 fracstop 1.000 1.000 1.000 cjmean 2.837 2.837 2.837 libcent 0 179.4 180.9 179.3 libamp 0 164.0 162.0 165.2 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 177.9 176.6 180.1 kozaiamp 180.0 180.0 180.0