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: 612176
# Created Thu Apr 25 01:09:10 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 55 observations of 55
# Arc: 19.17y
# First observation: 2000/08/25
# Last observation: 2019/10/26
# Chi-squared of fit: 180.13 DOF: 104 RMS: 0.32
# Min/Max residuals: -0.73 0.75
# Exact a, adot, b, bdot, g, gdot:
1.653113E-05 2.979129E-02 -1.025812E-06 -1.153313E-03 2.685902E-02 2.735094E-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
3.030882 -9.715706 0.317119 0.050419 -0.955312 2451781.721203
# Heliocentric elements and errors
Epoch: 2451782.5000 = 2000/08/26
Mean Anomaly: 16.55835 +/- 0.000
Argument of Peri: 100.10302 +/- 0.000
Long of Asc Node: 223.48504 +/- 0.000
Inclination: 3.66562 +/- 0.000
Eccentricity: 0.21929531 +/- 0.0000
Semi-Major Axis: 48.01887100 +/- 0.0000
Time of Perihelion: 2446192.2554 +/- 0.0
Perihelion: 37.48855758 +/- 0.0000
Aphelion: 58.54918443 +/- 0.0000
Period (y) 332.7562 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 37.54124255 +/- 0.0000
Ecliptic Y -6.74346036 +/- 0.0000
Ecliptic Z 1.96853070 +/- 0.0000
Ecliptic XDOT 0.00078574 +/- 0.0000
Ecliptic YDOT 0.00295049 +/- 0.0000
Ecliptic ZDOT -0.00010250 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 38.19280344 +/- 0.0000
Geocenter to KBO 37.23141580 +/- 0.0000
# Hcoef: 6.70
The following table shows the complete astrometric record for 612176. 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 (612176) followed by the observatory code and reference code for the source of the astrometry.
2000 08 25.22046 23 19 31.63 -01 03 41.0 22.2R 612176 807 Cd1703 2000 08 25.28442 23 19 31.34 -01 03 42.8 612176 807 Cd1703 2000 09 21.22717 23 17 24.72 -01 17 21.1 21.9R 612176 695 Cd1703 2000 09 21.29762 23 17 24.39 -01 17 23.1 612176 695 Cd1703 2001 08 19.25242 23 26 20.86 -00 24 26.4 21.5R 612176 807 Cd7651 2001 08 19.33589 23 26 20.50 -00 24 28.4 612176 807 Cd7651 2001 08 20.30271 23 26 16.42 -00 24 53.4 21.4R 612176 807 Cd7651 2001 08 20.38861 23 26 16.02 -00 24 55.6 612176 807 Cd7651 2001 08 21.29828 23 26 12.14 -00 25 19.5 21.2R 612176 807 Cd7651 2001 08 21.36656 23 26 11.85 -00 25 21.2 612176 807 Cd7651 2001 09 16.30833 23 24 12.04 -00 38 06.4 612176 695 Cd5768 2001 09 16.33153 23 24 11.93 -00 38 07.2 612176 695 Cd5768 2001 09 18.24345 23 24 02.84 -00 39 07.3 612176 695 Cd5768 2001 09 18.27912 23 24 02.68 -00 39 08.3 612176 695 Cd5768 2002 09 05.294527 23 31 25.60 +00 03 59.8 612176 645 C~1Q3A 2002 09 05.295356 23 31 25.60 +00 03 59.8 612176 645 C~1Q3A 2002 09 05.297842 23 31 25.59 +00 03 59.7 612176 645 C~1Q3A 2003 09 28.273269 23 35 56.67 +00 28 17.1 22.5V 612176 645 C~1Q3A 2003 09 28.274099 23 35 56.67 +00 28 17.1 22.3V 612176 645 C~1Q3A 2003 09 28.276587 23 35 56.65 +00 28 17.1 23.4V 612176 645 C~1Q3A 2005 06 07.41411 23 52 43.43 +02 03 40.6 22.3R 612176 304 Cn6460 2005 06 07.42417 23 52 43.45 +02 03 40.7 612176 304 Cn6460 2006 07 25.44211 23 58 46.90 +02 40 53.7 22.8R 612176 250 S~06AN 2006 07 25.44651 23 58 46.89 +02 40 53.7 612176 250 S~06AN 2006 07 25.45091 23 58 46.88 +02 40 53.6 612176 250 S~06AN 2006 07 25.45531 23 58 46.87 +02 40 53.6 612176 250 S~06AN 2007 07 15.93654 00 05 06.19 +03 16 22.7 23.4R 612176 250 S~06AN 2007 07 15.94418 00 05 06.18 +03 16 22.7 612176 250 S~06AN 2007 07 15.95182 00 05 06.17 +03 16 22.7 612176 250 S~06AN 2007 07 15.95945 00 05 06.16 +03 16 22.7 612176 250 S~06AN 2007 07 19.40459 00 05 01.98 +03 16 06.2 612176 250 S~06AN 2007 07 19.41293 00 05 01.97 +03 16 06.2 612176 250 S~06AN 2007 07 19.42057 00 05 01.96 +03 16 06.1 612176 250 S~06AN 2007 08 05.45807 00 04 26.81 +03 13 04.5 612176 250 S~06AN 2007 08 05.46571 00 04 26.79 +03 13 04.4 612176 250 S~06AN 2007 08 05.51501 00 04 26.65 +03 13 03.7 612176 250 S~06AN 2007 08 05.52265 00 04 26.63 +03 13 03.6 612176 250 S~06AN 2007 08 27.70517 00 03 10.02 +03 05 26.5 612176 250 S~06AN 2007 08 27.71142 00 03 09.99 +03 05 26.4 612176 250 S~06AN 2007 08 27.71906 00 03 09.95 +03 05 26.1 612176 250 S~06AN 2007 08 27.76073 00 03 09.79 +03 05 25.1 612176 250 S~06AN 2007 08 27.76976 00 03 09.75 +03 05 24.9 612176 250 S~06AN 2007 08 27.77948 00 03 09.71 +03 05 24.6 612176 250 S~06AN 2007 08 27.78712 00 03 09.69 +03 05 24.5 612176 250 S~06AN 2007 08 27.82601 00 03 09.48 +03 05 24.3 612176 250 S~06AN 2008 08 25.33585 00 09 23.26 +03 40 36.2 612176 250 S~06AN 2008 08 25.34349 00 09 23.23 +03 40 36.0 612176 250 S~06AN 2008 08 25.35182 00 09 23.20 +03 40 35.8 612176 250 S~06AN 2008 08 25.40321 00 09 23.00 +03 40 34.5 612176 250 S~06AN 2008 10 03.225019 00 06 29.34 +03 21 43.8 22.6V 612176 645 C~1Q3A 2008 10 03.225849 00 06 29.33 +03 21 43.8 22.3V 612176 645 C~1Q3A 2008 10 03.228336 00 06 29.32 +03 21 43.8 23.4V 612176 645 C~1Q3A 2019 10 26.117880 01 10 00.390 +09 02 49.37 22.8G 612176 G37 C~3cUm 2019 10 26.186570 01 10 00.077 +09 02 47.37 612176 G37 C~3cUm 2019 10 26.298750 01 09 59.567 +09 02 44.11 612176 G37 C~3cUm
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 0.15
2 0.0002 0.00 0.23 0.00 0.13
3 0.0739 0.00 -0.01 0.00 0.15
4 0.0741 0.00 0.06 0.00 0.36
5 0.9830 0.00 -0.14 0.00 -0.02
6 0.9832 0.00 -0.15 0.00 0.12
7 0.9859 0.00 0.14 0.00 0.07
8 0.9861 0.00 -0.27 0.00 0.11
9 0.9886 0.00 -0.11 0.00 0.01
10 0.9888 0.00 0.03 0.00 0.11
11 1.0598 0.00 0.31 0.00 -0.02
12 1.0599 0.00 0.34 0.00 -0.09
13 1.0651 0.00 -0.21 0.00 0.02
14 1.0652 0.00 -0.03 0.00 0.15
15 2.0290 0.00 -0.25 0.00 -0.73
16 2.0290 0.00 -0.20 0.00 -0.70
17 2.0290 0.00 -0.17 0.00 -0.73
18 3.0912 0.00 0.12 0.00 -0.32
19 3.0912 0.00 0.18 0.00 -0.30
20 3.0912 0.00 0.06 0.00 -0.22
21 4.7836 0.00 -0.19 0.00 -0.28
22 4.7836 0.00 -0.19 0.00 -0.36
23 5.9144 0.00 0.29 0.00 0.71
24 5.9144 0.00 0.27 0.00 0.75
25 5.9144 0.00 0.26 0.00 0.70
26 5.9144 0.00 0.24 0.00 0.74
27 6.8877 0.00 -0.38 0.00 0.29
28 6.8877 0.00 -0.41 0.00 0.32
29 6.8877 0.00 -0.44 0.00 0.34
30 6.8877 0.00 -0.47 0.00 0.37
31 6.8972 0.00 -0.39 0.00 0.29
32 6.8972 0.00 -0.37 0.00 0.34
33 6.8972 0.00 -0.36 0.00 0.29
34 6.9438 0.00 0.54 0.00 -0.17
35 6.9439 0.00 0.55 0.00 -0.16
36 6.9440 0.00 0.47 0.00 -0.10
37 6.9440 0.00 0.48 0.00 -0.08
38 7.0047 0.00 0.23 0.00 -0.39
39 7.0048 0.00 0.16 0.00 -0.34
40 7.0048 0.00 0.03 0.00 -0.44
41 7.0049 0.00 0.17 0.00 -0.39
42 7.0049 0.00 0.12 0.00 -0.36
43 7.0050 0.00 0.11 0.00 -0.42
44 7.0050 0.00 0.28 0.00 -0.33
45 7.0051 0.00 -0.50 0.00 0.46
46 8.0003 0.00 -0.34 0.00 0.25
47 8.0003 0.00 -0.34 0.00 0.23
48 8.0004 0.00 -0.31 0.00 0.23
49 8.0005 0.00 -0.30 0.00 0.17
50 8.1068 0.00 0.23 0.00 -0.37
51 8.1068 0.00 0.14 0.00 -0.34
52 8.1068 0.00 0.16 0.00 -0.26
53 19.1674 0.00 0.03 0.00 -0.08
54 19.1676 0.00 0.02 0.00 -0.11
55 19.1679 0.00 0.05 0.00 -0.14
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.
612176 quality flag:3 Type: 2:1E 2:1E 2:1E axisobj 48.139 48.139 48.139 ecceobj 0.221 0.221 0.221 incobj 3.666 3.666 3.666 qmin 36.515 36.515 36.515 qmax 59.771 59.771 59.771 amean 47.798 47.798 47.798 amin 47.271 47.271 47.271 amax 48.409 48.409 48.409 emean 0.208 0.208 0.208 emin 0.180 0.180 0.180 emax 0.235 0.235 0.235 imean 5.842 5.842 5.842 imin 4.560 4.560 4.560 imax 7.127 7.127 7.127 excite_mean 0.232 0.232 0.232 fracstop 1.000 1.000 1.000 cjmean 3.081 3.081 3.081 libcent 0 87.6 87.6 87.6 libamp 0 39.0 39.0 39.0 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 175.5 175.5 175.5 kozaiamp 180.0 180.0 180.0