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: 02FV6 # Created Sat Apr 27 01:10:41 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 19 observations of 19 # Arc: 12.92y # First observation: 2002/03/20 # Last observation: 2015/02/18 # Chi-squared of fit: 51.76 DOF: 32 RMS: 0.29 # Min/Max residuals: -0.40 0.84 # Exact a, adot, b, bdot, g, gdot: 1.308368E-05 1.542842E-02 1.030946E-07 -6.791640E-04 1.922210E-02 1.353913E-03 # Covariance matrix: 2.4664E-13 -1.4170E-13 -3.7925E-15 4.6524E-15 3.7372E-13 -5.1680E-13 -1.4170E-13 1.8633E-13 4.8303E-15 -7.2326E-15 -1.9217E-13 8.0752E-13 -3.7925E-15 4.8303E-15 1.2959E-13 -1.2305E-14 -8.4973E-15 2.0567E-14 4.6524E-15 -7.2326E-15 -1.2305E-14 4.2222E-15 3.0392E-15 -3.3117E-14 3.7372E-13 -1.9217E-13 -8.4973E-15 3.0392E-15 2.4407E-12 -3.1442E-13 -5.1680E-13 8.0752E-13 2.0567E-14 -3.3117E-14 -3.1442E-13 3.7034E-12 # lat0 lon0 xBary yBary zBary JD0 -1.828801 168.054261 -0.202676 -0.031210 -0.975411 2452353.790823 # Heliocentric elements and errors Epoch: 2452354.5000 = 2002/03/21 Mean Anomaly: 137.52368 +/- 0.101 Argument of Peri: 67.69548 +/- 0.069 Long of Asc Node: 312.63397 +/- 0.003 Inclination: 3.07919 +/- 0.000 Eccentricity: 0.15541287 +/- 0.0002 Semi-Major Axis: 47.15495642 +/- 0.0136 Time of Perihelion: 2407172.6044 +/- 38.5 Perihelion: 39.82646912 +/- 0.0141 Aphelion: 54.48344372 +/- 0.0178 Period (y) 323.8167 +/- 0.14 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -51.86691610 +/- 0.0041 Ecliptic Y 10.77118671 +/- 0.0009 Ecliptic Z -1.66022784 +/- 0.0001 Ecliptic XDOT -0.00064881 +/- 0.0000 Ecliptic YDOT -0.00211182 +/- 0.0000 Ecliptic ZDOT -0.00010262 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 52.99948270 +/- 0.0040 Geocenter to KBO 52.02343689 +/- 0.0042 # Hcoef: 6.81
The following table shows the complete astrometric record for 02FV6. 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 (02FV6) followed by the observatory code and reference code for the source of the astrometry.
2002 03 20.29008 11 13 11.99 +03 02 19.7 24.0R 02FV6 568 Cf5861 2002 03 20.32480 11 13 11.87 +03 02 20.5 24.2R 02FV6 568 Cf5861 2002 03 20.35929 11 13 11.74 +03 02 21.3 23.9R 02FV6 568 Cf5861 2002 03 22.32156 11 13 04.70 +03 03 05.7 23.1R 02FV6 568 Cf5861 2002 03 22.35862 11 13 04.57 +03 03 06.6 23.2R 02FV6 568 Cf5861 2002 03 22.41437 11 13 04.35 +03 03 08.0 02FV6 568 Cf5861 2002 06 03.17224 11 10 38.89 +03 19 57.9 24. R 02FV6 675 Cf8969 2002 06 04.20833 11 10 39.12 +03 19 57.4 02FV6 675 Cf8969 2002 06 07.20417 11 10 40.22 +03 19 57.0 02FV6 675 Cf8969 2002 06 08.23045 11 10 40.69 +03 19 55.5 24. R 02FV6 675 Cf8969 2003 03 30.19290 11 15 50.16 +02 43 06.9 23.7R 02FV6 695 Ch8263 2003 03 30.28934 11 15 49.82 +02 43 09.1 02FV6 695 Ch8263 2003 03 31.29162 11 15 46.39 +02 43 31.5 02FV6 695 Ch8263 2003 03 31.33598 11 15 46.28 +02 43 32.2 02FV6 695 Ch8263 2005 03 10.31173 11 23 22.39 +01 50 05.5 23.3R 02FV6 695 Cn0182 2005 03 10.44558 11 23 21.90 +01 50 08.7 02FV6 695 Cn0182 2015 02 18.30405 11 55 49.13 -02 01 53.2 23.7R 02FV6 695 C~1M63 2015 02 18.39757 11 55 48.82 -02 01 51.6 02FV6 695 C~1M63 2015 02 18.48611 11 55 48.55 -02 01 50.0 02FV6 695 C~1M63
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 -0.13 0.00 -0.09
2 0.0001 0.00 -0.02 0.00 -0.09
3 0.0002 0.00 -0.08 0.00 -0.08
4 0.0056 0.00 -0.16 0.00 -0.40
5 0.0057 0.00 -0.10 0.00 -0.34
6 0.0058 0.00 -0.36 0.00 -0.21
7 0.2050 0.00 0.11 0.00 0.84
8 0.2079 0.00 0.16 0.00 -0.12
9 0.2161 0.00 0.53 0.00 0.75
10 0.2189 0.00 -0.06 0.00 0.58
11 1.0264 0.00 0.23 0.00 -0.30
12 1.0267 0.00 0.15 0.00 -0.22
13 1.0294 0.00 -0.29 0.00 0.14
14 1.0296 0.00 0.35 0.00 -0.13
15 2.9734 0.00 -0.30 0.00 -0.23
16 2.9737 0.00 -0.16 0.00 -0.12
17 12.9172 0.00 0.15 0.00 0.10
18 12.9175 0.00 -0.11 0.00 0.00
19 12.9177 0.00 -0.00 0.00 -0.00
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.
02FV6 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 46.854 46.855 46.854 ecceobj 0.161 0.161 0.161 incobj 3.091 3.091 3.091 qmin 38.806 38.804 38.809 qmax 55.631 55.602 55.589 amean 47.015 47.015 47.015 amin 46.603 46.606 46.599 amax 47.493 47.502 47.493 emean 0.158 0.158 0.158 emin 0.143 0.143 0.143 emax 0.171 0.171 0.171 imean 4.459 4.459 4.459 imin 3.879 3.878 3.876 imax 5.013 5.013 5.013 excite_mean 0.176 0.176 0.176 fracstop 1.000 1.000 1.000 cjmean 3.100 3.100 3.100 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 177.9 177.9 177.9 kozaiamp 180.0 180.0 179.9