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: 612333
# Created Sun Apr 28 01:09:13 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 34 observations of 34
# Arc: 21.04y
# First observation: 2002/02/07
# Last observation: 2023/02/20
# Chi-squared of fit: 94.03 DOF: 62 RMS: 0.29
# Min/Max residuals: -0.50 0.91
# Exact a, adot, b, bdot, g, gdot:
1.579922E-05 1.891859E-02 -1.487135E-06 2.097415E-04 2.142541E-02 3.666980E-04
# 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
1.596793 134.367977 -0.071068 0.027259 -0.980601 2452312.716373
# Heliocentric elements and errors
Epoch: 2452312.5000 = 2002/02/07
Mean Anomaly: 155.31010 +/- 0.000
Argument of Peri: 270.04571 +/- 0.000
Long of Asc Node: 66.50489 +/- 0.000
Inclination: 1.68715 +/- 0.000
Eccentricity: 0.05782281 +/- 0.0000
Semi-Major Axis: 45.25530854 +/- 0.0000
Time of Perihelion: 2404339.1638 +/- 0.0
Perihelion: 42.63851959 +/- 0.0000
Aphelion: 47.87209749 +/- 0.0000
Period (y) 304.4476 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -33.36053148 +/- 0.0000
Ecliptic Y 34.00889937 +/- 0.0000
Ecliptic Z 1.30052339 +/- 0.0000
Ecliptic XDOT -0.00176892 +/- 0.0000
Ecliptic YDOT -0.00165822 +/- 0.0000
Ecliptic ZDOT 0.00002831 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 47.65732085 +/- 0.0000
Geocenter to KBO 46.67357533 +/- 0.0000
# Hcoef: 6.87
The following table shows the complete astrometric record for 612333. 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 (612333) followed by the observatory code and reference code for the source of the astrometry.
2002 02 07.21563 09 09 17.06 +18 02 52.5 22.9R 612333 695 Cf0409 2002 02 08.18356 09 09 12.75 +18 03 10.4 612333 695 Cf0409 2002 02 08.27432 09 09 12.36 +18 03 12.3 612333 695 Cf0409 2002 03 08.34630 09 07 16.63 +18 11 19.0 22.9R 612333 568 Cf2752 2002 03 08.43474 09 07 16.30 +18 11 20.0 612333 568 Cf2752 2002 03 13.37748 09 06 59.12 +18 12 28.6 612333 696 Cf5586 2005 02 10.31228 09 22 07.40 +17 07 16.1 23.9g 612333 568 C~0VDX 2005 02 10.39529 09 22 07.03 +17 07 17.8 24.3g 612333 568 C~0VDX 2005 02 10.43481 09 22 06.85 +17 07 18.7 24.3g 612333 568 C~0VDX 2005 02 15.33591 09 21 45.44 +17 08 57.0 23.5g 612333 568 C~0VDX 2005 03 09.24738 09 20 16.32 +17 15 32.4 23.2R 612333 695 Cn3092 2005 03 09.33718 09 20 15.98 +17 15 34.3 612333 695 Cn3092 2005 03 10.24763 09 20 12.67 +17 15 48.4 612333 695 Cn3092 2005 04 11.14899 09 18 47.55 +17 21 29.0 23.2R 612333 695 Cn3092 2005 04 12.14827 09 18 46.05 +17 21 34.0 612333 695 Cn3092 2005 04 12.26135 09 18 45.91 +17 21 35.4 24.7i 612333 568 C~0VDX 2005 04 12.36980 09 18 45.74 +17 21 36.1 24.0i 612333 568 C~0VDX 2005 04 13.14863 09 18 44.59 +17 21 38.3 612333 695 Cn3092 2006 01 11.35083 09 28 33.06 +16 37 26.0 23.3R 612333 250 S~06AT 2006 01 11.35522 09 28 33.04 +16 37 26.1 612333 250 S~06AT 2006 01 11.35962 09 28 33.02 +16 37 26.2 612333 250 S~06AT 2006 01 11.36402 09 28 33.01 +16 37 26.2 612333 250 S~06AT 2006 02 03.47735 09 26 57.62 +16 45 15.6 612333 568 C~0VDX 2006 02 06.32831 09 26 45.17 +16 46 15.5 23.1r 612333 568 C~0VDX 2006 02 06.36908 09 26 44.99 +16 46 16.2 23.3r 612333 568 C~0VDX 2006 02 06.40731 09 26 44.85 +16 46 17.1 23.8r 612333 568 C~0VDX 2006 11 23.50414 09 34 33.23 +16 07 33.6 612333 695 C~0VDX 2006 11 24.50685 09 34 32.97 +16 07 37.1 612333 695 C~0VDX 2013 03 13.23507 09 54 00.49 +14 33 40.6 23.5R 612333 695 C~0ucs 2013 03 14.18899 09 53 56.92 +14 33 58.2 612333 695 C~0ucs 2013 03 14.34016 09 53 56.35 +14 34 01.2 612333 695 C~0ucs 2023 02 20.287380 10 36 44.141 +10 36 53.00 22.9G 612333 G37 C~6ImY 2023 02 20.339780 10 36 43.962 +10 36 53.66 612333 G37 C~6ImY 2023 02 20.392330 10 36 43.718 +10 36 55.49 612333 G37 C~6ImY
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 -0.28 0.00 0.43
2 0.0027 0.00 -0.50 0.00 -0.38
3 0.0029 0.00 -0.22 0.00 -0.24
4 0.0798 0.00 0.17 0.00 0.18
5 0.0800 0.00 0.11 0.00 -0.10
6 0.0935 0.00 0.43 0.00 0.02
7 3.0092 0.00 0.11 0.00 0.12
8 3.0094 0.00 0.12 0.00 0.12
9 3.0095 0.00 0.07 0.00 0.22
10 3.0229 0.00 0.10 0.00 0.14
11 3.0829 0.00 -0.05 0.00 -0.38
12 3.0832 0.00 -0.12 0.00 0.11
13 3.0856 0.00 -0.05 0.00 -0.07
14 3.1730 0.00 -0.21 0.00 -0.09
15 3.1757 0.00 -0.04 0.00 -0.10
16 3.1760 0.00 0.35 0.00 0.71
17 3.1763 0.00 0.29 0.00 0.91
18 3.1785 0.00 -0.42 0.00 -0.45
19 3.9264 0.00 0.50 0.00 -0.28
20 3.9265 0.00 0.45 0.00 -0.27
21 3.9265 0.00 0.40 0.00 -0.25
22 3.9265 0.00 0.49 0.00 -0.33
23 3.9898 0.00 -0.36 0.00 -0.37
24 3.9976 0.00 -0.25 0.00 -0.02
25 3.9977 0.00 -0.23 0.00 -0.17
26 3.9978 0.00 0.22 0.00 -0.08
27 4.7920 0.00 -0.24 0.00 0.25
28 4.7948 0.00 -0.43 0.00 0.24
29 11.0938 0.00 -0.06 0.00 -0.00
30 11.0964 0.00 -0.06 0.00 -0.14
31 11.0969 0.00 -0.02 0.00 0.07
32 21.0351 0.00 -0.26 0.00 0.26
33 21.0352 0.00 0.35 0.00 -0.38
34 21.0354 0.00 -0.01 0.00 0.16
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.
612333 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 44.997 44.997 44.997 ecceobj 0.064 0.064 0.064 incobj 1.686 1.686 1.686 qmin 41.460 41.461 41.460 qmax 48.844 48.846 48.843 amean 45.034 45.033 45.034 amin 44.677 44.673 44.677 amax 45.401 45.402 45.398 emean 0.063 0.063 0.063 emin 0.048 0.048 0.048 emax 0.076 0.076 0.076 imean 0.788 0.788 0.788 imin 0.181 0.181 0.181 imax 1.210 1.210 1.210 excite_mean 0.064 0.064 0.064 fracstop 1.000 1.000 1.000 cjmean 3.109 3.109 3.109 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 203.8 203.8 203.7 kozaiamp 180.0 180.0 180.0