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: 612084 # Created Fri Mar 29 01:09:17 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 59 observations of 59 # Arc: 24.10y # First observation: 1999/02/11 # Last observation: 2023/03/18 # Chi-squared of fit: 177.40 DOF: 112 RMS: 0.31 # Min/Max residuals: -0.75 0.92 # Exact a, adot, b, bdot, g, gdot: 1.804593E-05 2.989379E-02 -3.408521E-06 -1.071896E-02 2.579861E-02 -4.553673E-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 0.489564 121.604216 -0.352642 0.007717 -0.928743 2451220.779063 # Heliocentric elements and errors Epoch: 2451220.5000 = 1999/02/11 Mean Anomaly: 355.02359 +/- 0.000 Argument of Peri: 199.66367 +/- 0.000 Long of Asc Node: 303.43658 +/- 0.000 Inclination: 19.73441 +/- 0.000 Eccentricity: 0.56165283 +/- 0.0000 Semi-Major Axis: 88.36055398 +/- 0.0000 Time of Perihelion: 2455414.2222 +/- 0.0 Perihelion: 38.73259903 +/- 0.0000 Aphelion: 137.98850892 +/- 0.0000 Period (y) 830.6075 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -21.09168269 +/- 0.0000 Ecliptic Y 33.61768416 +/- 0.0000 Ecliptic Z 0.33106124 +/- 0.0000 Ecliptic XDOT -0.00245548 +/- 0.0000 Ecliptic YDOT -0.00205679 +/- 0.0000 Ecliptic ZDOT -0.00114163 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 39.68784804 +/- 0.0000 Geocenter to KBO 38.76191973 +/- 0.0000 # Hcoef: 7.15
The following table shows the complete astrometric record for 612084. 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 (612084) followed by the observatory code and reference code for the source of the astrometry.
1999 02 11.27832 08 15 51.18 +20 16 48.2 23.0R 612084 568 Ca4178 1999 02 11.32043 08 15 50.97 +20 16 48.6 23.0R 612084 568 Ca4178 1999 02 17.24042 08 15 22.32 +20 17 41.7 23.0R 612084 568 Ca4178 1999 02 17.32277 08 15 21.91 +20 17 42.5 23.0R 612084 568 Ca4178 1999 04 08.26531 08 13 02.23 +20 19 32.0 23.1R 612084 568 Ca4843 1999 04 09.25789 08 13 01.82 +20 19 26.8 23.1R 612084 568 Ca4843 1999 05 06.25461 08 13 30.58 +20 14 56.8 23.3R 612084 568 Ca4843 1999 05 06.30545 08 13 30.72 +20 14 56.3 23.3R 612084 568 Ca4843 1999 12 29.61447 08 26 09.36 +19 09 03.1 612084 568 Ca8502 1999 12 29.63415 08 26 09.26 +19 09 03.4 612084 568 Ca8502 1999 12 30.60682 08 26 04.71 +19 09 13.3 612084 568 Ca8502 1999 12 31.43598 08 26 00.70 +19 09 22.1 22.8R 612084 695 Ca8502 1999 12 31.44434 08 26 00.72 +19 09 22.1 22.6R 612084 695 Ca8502 1999 12 31.51453 08 26 00.38 +19 09 22.6 612084 695 Ca8502 1999 12 31.52179 08 26 00.36 +19 09 22.7 612084 695 Ca8502 2000 01 29.12666 08 23 32.24 +19 14 49.5 612084 705 Ca9922 2000 01 29.15234 08 23 32.16 +19 14 49.5 612084 705 Ca9922 2000 01 29.18577 08 23 31.95 +19 14 50.2 22.9R 612084 705 Ca9922 2000 01 30.14579 08 23 26.84 +19 15 01.1 612084 705 Ca9922 2000 01 30.17000 08 23 26.70 +19 15 01.5 612084 705 Ca9922 2000 01 30.20438 08 23 26.51 +19 15 02.2 612084 705 Ca9922 2001 01 26.30391 08 30 13.81 +18 13 19.6 22.5R 612084 695 Cc6423 2001 01 26.37647 08 30 13.41 +18 13 20.4 612084 695 Cc6423 2002 04 10.30291 08 32 13.83 +17 21 11.6 612084 568 Ch3072 2002 04 10.34891 08 32 13.80 +17 21 11.5 612084 568 Ch3072 2002 04 11.25257 08 32 13.22 +17 21 09.7 612084 568 Ch3072 2002 04 11.26285 08 32 13.21 +17 21 09.9 612084 568 Ch3072 2005 03 10.226910 08 52 33.32 +14 07 38.5 612084 645 C~1cF1 2005 03 10.227743 08 52 33.31 +14 07 38.5 612084 645 C~1cF1 2005 03 10.230231 08 52 33.30 +14 07 38.5 612084 645 C~1cF1 2005 12 06.439912 09 05 43.85 +12 44 03.1 22.3V 612084 645 C~1cF2 2005 12 06.440741 09 05 43.85 +12 44 03.0 22.4V 612084 645 C~1cF2 2005 12 06.443229 09 05 43.84 +12 44 03.0 23.4V 612084 645 C~1cF2 2006 01 31.343332 09 01 55.60 +12 51 35.9 612084 645 C~1cF2 2006 01 31.344161 09 01 55.60 +12 51 35.9 612084 645 C~1cF2 2006 01 31.346649 09 01 55.58 +12 51 36.0 612084 645 C~1cF2 2013 03 12.13729 09 42 07.43 +05 03 05.6 22.0R 612084 695 C~0uco 2013 03 12.19997 09 42 07.16 +05 03 07.0 612084 695 C~0uco 2013 03 13.13373 09 42 03.17 +05 03 27.7 612084 695 C~0uco 2015 02 01.24277 09 57 25.15 +02 29 45.6 612084 W84 C~2KVJ 2015 02 01.31738 09 57 24.78 +02 29 46.6 23.2r 612084 W84 C~2KVJ 2015 02 01.32060 09 57 24.76 +02 29 46.6 612084 W84 C~2KVJ 2015 04 17.035139 09 52 19.08 +02 56 20.1 612084 W84 C~3i8v 2015 04 17.036574 09 52 19.08 +02 56 20.3 612084 W84 C~3i8v 2016 01 14.317917 10 04 43.93 +01 16 59.7 612084 W84 C~3i8v 2016 01 14.319063 10 04 43.92 +01 16 59.8 612084 W84 C~3i8v 2016 12 29.300480 10 11 29.09 +00 08 00.0 612084 W84 C~3i8v 2016 12 29.301765 10 11 29.09 +00 07 59.9 612084 W84 C~3i8v 2017 02 02.38415 10 09 17.26 +00 10 42.7 23.1r 612084 T09 C~7uXI 2017 02 02.50029 10 09 16.72 +00 10 44.4 23.0r 612084 T09 C~7uXI 2017 02 02.51130 10 09 16.67 +00 10 44.6 22.8r 612084 T09 C~7uXI 2017 02 02.52029 10 09 16.62 +00 10 44.6 23.0r 612084 T09 C~7uXI 2017 02 02.53379 10 09 16.56 +00 10 44.9 22.9r 612084 T09 C~7uXI 2017 03 29.23660 10 05 06.95 +00 31 08.9 23.8g 612084 T09 C~7wHo 2017 03 29.24497 10 05 06.93 +00 31 08.9 23.7g 612084 T09 C~7wHo 2017 03 29.35491 10 05 06.52 +00 31 11.6 23.6g 612084 T09 C~7wHo 2023 03 18.257010 10 41 03.118 -06 21 08.03 22.6G 612084 G37 C~6bsf 2023 03 18.298790 10 41 02.931 -06 21 06.00 612084 G37 C~6bsf 2023 03 18.343750 10 41 02.716 -06 21 04.97 612084 G37 C~6bsf
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 -0.10 0.00 -0.65 2 0.0001 0.00 -0.05 0.00 -0.66 3 0.0163 0.00 0.30 0.00 -0.75 4 0.0165 0.00 0.05 0.00 -0.67 5 0.1533 0.00 0.17 0.00 -0.15 6 0.1560 0.00 0.01 0.00 0.05 7 0.2299 0.00 -0.45 0.00 -0.02 8 0.2301 0.00 -0.17 0.00 0.22 9 0.8798 0.00 0.92 0.00 -0.61 10 0.8798 0.00 0.81 0.00 -0.50 11 0.8825 0.00 0.74 0.00 -0.17 12 0.8848 0.00 -0.75 0.00 0.39 13 0.8848 0.00 0.15 0.00 0.31 14 0.8850 0.00 0.12 0.00 0.12 15 0.8850 0.00 0.35 0.00 0.15 16 0.9633 0.00 -0.65 0.00 0.37 17 0.9634 0.00 0.22 0.00 0.06 18 0.9635 0.00 -0.23 0.00 0.35 19 0.9661 0.00 -0.30 0.00 -0.05 20 0.9662 0.00 -0.45 0.00 0.06 21 0.9663 0.00 -0.52 0.00 0.34 22 1.9576 0.00 0.25 0.00 0.74 23 1.9578 0.00 0.14 0.00 0.63 24 3.1595 0.00 0.05 0.00 0.53 25 3.1597 0.00 0.13 0.00 0.51 26 3.1621 0.00 0.03 0.00 0.21 27 3.1622 0.00 -0.02 0.00 0.43 28 6.0752 0.00 -0.02 0.00 0.08 29 6.0752 0.00 -0.12 0.00 0.07 30 6.0752 0.00 -0.13 0.00 0.04 31 6.8177 0.00 -0.28 0.00 -0.21 32 6.8177 0.00 -0.26 0.00 -0.31 33 6.8177 0.00 -0.32 0.00 -0.30 34 6.9707 0.00 -0.14 0.00 -0.25 35 6.9707 0.00 -0.08 0.00 -0.26 36 6.9708 0.00 -0.18 0.00 -0.20 37 14.0804 0.00 0.12 0.00 0.19 38 14.0806 0.00 0.17 0.00 0.19 39 14.0831 0.00 -0.01 0.00 0.11 40 15.9725 0.00 0.29 0.00 0.12 41 15.9727 0.00 0.13 0.00 0.02 42 15.9727 0.00 0.06 0.00 -0.03 43 16.1773 0.00 0.08 0.00 -0.07 44 16.1773 0.00 0.12 0.00 0.11 45 16.9228 0.00 0.18 0.00 -0.07 46 16.9228 0.00 0.09 0.00 0.03 47 17.8810 0.00 -0.05 0.00 -0.06 48 17.8810 0.00 -0.00 0.00 -0.16 49 17.9770 0.00 -0.17 0.00 -0.03 50 17.9773 0.00 -0.01 0.00 0.00 51 17.9774 0.00 0.02 0.00 0.04 52 17.9774 0.00 -0.09 0.00 -0.09 53 17.9774 0.00 -0.03 0.00 0.02 54 18.1272 0.00 -0.04 0.00 0.04 55 18.1272 0.00 0.12 0.00 -0.16 56 18.1275 0.00 0.00 0.00 -0.19 57 24.0958 0.00 -0.12 0.00 -0.45 58 24.0959 0.00 -0.06 0.00 0.41 59 24.0960 0.00 -0.21 0.00 0.19
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.
612084 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 89.009 89.009 89.010 ecceobj 0.565 0.565 0.565 incobj 19.710 19.710 19.710 qmin 37.096 37.074 37.067 qmax 144.249 144.069 143.958 amean 88.907 88.917 88.907 amin 87.541 87.534 87.535 amax 91.134 90.992 91.077 emean 0.568 0.568 0.568 emin 0.554 0.554 0.554 emax 0.583 0.583 0.583 imean 20.728 20.731 20.729 imin 19.979 19.991 19.984 imax 21.639 21.631 21.623 excite_mean 0.669 0.669 0.669 fracstop 1.000 1.000 1.000 cjmean 2.983 2.983 2.983 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 199.0 198.9 198.9 kozaiamp 180.0 180.0 180.0