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: 612575
# Created Fri Nov 1 01:07:38 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 56 observations of 56
# Arc: 21.02y
# First observation: 2003/08/25
# Last observation: 2024/08/30
# Chi-squared of fit: 255.97 DOF: 106 RMS: 0.38
# Min/Max residuals: -0.96 1.50
# Exact a, adot, b, bdot, g, gdot:
2.030468E-05 2.908523E-02 2.140366E-06 1.666864E-03 2.530827E-02 -5.334741E-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
2.411353 -48.510067 -0.345364 0.040211 -0.953778 2452876.630013
# Heliocentric elements and errors
Epoch: 2452876.5000 = 2003/08/25
Mean Anomaly: 347.36228 +/- 0.000
Argument of Peri: 69.54743 +/- 0.000
Long of Asc Node: 276.13515 +/- 0.000
Inclination: 4.01677 +/- 0.000
Eccentricity: 0.42719993 +/- 0.0000
Semi-Major Axis: 67.10157971 +/- 0.0000
Time of Perihelion: 2459924.4629 +/- 0.0
Perihelion: 38.43578962 +/- 0.0000
Aphelion: 95.76736981 +/- 0.0000
Period (y) 549.6767 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 27.04248962 +/- 0.0000
Ecliptic Y -30.05383954 +/- 0.0000
Ecliptic Z 1.66252419 +/- 0.0000
Ecliptic XDOT 0.00196464 +/- 0.0000
Ecliptic YDOT 0.00251636 +/- 0.0000
Ecliptic ZDOT 0.00015605 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 40.46360858 +/- 0.0000
Geocenter to KBO 39.51295304 +/- 0.0000
# Hcoef: 7.19
The following table shows the complete astrometric record for 612575. 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 (612575) followed by the observatory code and reference code for the source of the astrometry.
2003 08 25.12927 20 53 02.29 -15 00 59.6 21.8R 612575 807 Ci4137 2003 08 26.02489 20 52 58.36 -15 01 15.9 612575 807 Ci4137 2003 08 26.12384 20 52 57.92 -15 01 17.7 612575 807 Ci4137 2003 10 01.22477 20 50 56.45 -15 10 26.5 23.1R 612575 568 Ci6964 2003 10 01.30181 20 50 56.29 -15 10 27.5 612575 568 Ci6964 2003 10 02.22040 20 50 54.47 -15 10 37.4 612575 568 Ci6964 2004 08 12.11446 21 00 31.29 -14 23 42.2 21.8R 612575 807 Cn7007 2004 08 12.21694 21 00 30.79 -14 23 44.3 612575 807 Cn7007 2005 06 09.24825 21 11 17.32 -13 33 29.0 22.5R 612575 304 Cn7007 2005 06 09.28043 21 11 17.27 -13 33 29.3 612575 304 Cn7007 2006 06 17.26905 21 17 31.78 -12 58 46.6 22.5R 612575 250 S~06Ad 2006 06 17.33169 21 17 31.62 -12 58 47.0 612575 250 S~06Ad 2006 06 17.33608 21 17 31.61 -12 58 47.0 612575 250 S~06Ad 2006 06 17.34048 21 17 31.60 -12 58 47.1 612575 250 S~06Ad 2007 09 11.23039 21 18 10.00 -12 47 47.6 22.5r 612575 695 Cv8575 2007 09 11.29715 21 18 09.73 -12 47 48.9 22.6r 612575 695 Cv8575 2008 06 07.34574 21 30 59.63 -11 44 17.3 612575 807 Cz1375 2008 06 07.40408 21 30 59.54 -11 44 17.5 612575 807 Cz1375 2008 09 24.176796 21 23 59.92 -12 15 07.4 612575 645 C~1PqY 2008 09 24.177626 21 23 59.92 -12 15 07.4 612575 645 C~1PqY 2008 09 24.180113 21 23 59.91 -12 15 07.4 612575 645 C~1PqY 2011 07 22.46222 21 48 48.423 -09 54 49.46 23.9G 612575 F51 C~2r7B 2011 07 28.49116 21 48 22.627 -09 56 46.66 22.8G 612575 F51 C~2r7B 2011 08 31.40402 21 45 44.542 -10 09 51.48 22.9G 612575 F51 C~2r7B 2012 08 13.41357 21 53 50.628 -09 22 10.50 23.0G 612575 F51 C~2r7B 2012 08 13.42805 21 53 50.557 -09 22 11.12 23.2G 612575 F51 C~2r7B 2012 08 13.45735 21 53 50.429 -09 22 11.67 23.3G 612575 F51 C~2r7B 2013 05 20.60265 22 04 00.788 -08 28 29.27 22.8G 612575 F51 C~2r7B 2013 06 20.55713 22 03 48.973 -08 26 30.26 23.0G 612575 F51 C~2r7B 2013 08 12.44815 22 00 41.436 -08 40 15.26 23.0G 612575 F51 C~2r7B 2013 08 12.46368 22 00 41.344 -08 40 15.83 22.4G 612575 F51 C~2r7B 2013 08 12.47870 22 00 41.259 -08 40 16.14 22.7G 612575 F51 C~2r7B 2013 08 12.49366 22 00 41.213 -08 40 16.23 22.6G 612575 F51 C~2r7B 2013 11 25.23963 21 56 15.842 -09 08 39.74 23.3G 612575 F51 C~2r7B 2014 06 26.56392 22 10 17.957 -07 45 14.89 22.9G 612575 F51 C~2r7B 2014 06 28.53114 22 10 13.646 -07 45 28.44 23.1G 612575 F51 C~2r7B 2014 07 06.59602 22 09 52.742 -07 46 44.36 23.7G 612575 F51 C~2r7B 2014 07 25.55617 22 08 46.360 -07 51 35.52 22.7G 612575 F51 C~2r7B 2014 08 20.43718 22 06 50.473 -08 01 21.77 23.0G 612575 F51 C~2r7B 2014 08 27.42195 22 06 17.385 -08 04 20.72 22.9G 612575 F51 C~2r7B 2014 09 02.37237 22 05 49.502 -08 06 55.18 22.7G 612575 F51 C~2r7B 2014 09 16.34607 22 04 47.217 -08 12 52.84 23.3G 612575 F51 C~2r7B 2015 06 25.57429 22 17 01.074 -07 02 47.97 23.1G 612575 F51 C~2r7B 2015 06 27.59775 22 16 57.129 -07 02 58.92 23.2G 612575 F51 C~2r7B 2015 07 28.50287 22 15 19.989 -07 09 49.57 22.7G 612575 F51 C~2r7B 2015 08 21.41983 22 13 32.995 -07 19 02.02 22.8G 612575 F51 C~2r7B 2015 09 09.39621 22 12 04.297 -07 27 20.26 22.2G 612575 F51 C~2r7B 2015 12 01.22952 22 09 35.463 -07 46 27.34 22.8G 612575 F51 C~2r7B 2016 07 06.56505 22 23 16.202 -06 21 22.44 23.3G 612575 F51 C~2r7B 2016 07 11.52256 22 23 02.166 -06 22 18.36 23.5G 612575 F51 C~2r7B 2016 08 03.48106 22 21 37.255 -06 28 58.13 23.4G 612575 F51 C~2r7B 2019 09 04.223770 22 39 37.053 -04 29 35.44 22.9G 612575 G37 C~3cWO 2019 09 04.296120 22 39 36.709 -04 29 37.52 612575 G37 C~3cWO 2019 09 04.343930 22 39 36.489 -04 29 38.93 612575 G37 C~3cWO 2024 08 30.372320 23 13 55.640 -00 40 57.48 22.8G 612575 G37 C~8FmC 2024 08 30.428970 23 13 55.397 -00 40 59.03 612575 G37 C~8FmC
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 -0.37 0.00 -0.34
2 0.0025 0.00 -0.23 0.00 -0.06
3 0.0027 0.00 -0.20 0.00 -0.02
4 0.1016 0.00 -0.20 0.00 0.05
5 0.1018 0.00 -0.14 0.00 -0.14
6 0.1043 0.00 0.03 0.00 -0.45
7 0.9664 0.00 -0.24 0.00 -0.06
8 0.9667 0.00 -0.30 0.00 -0.12
9 1.7909 0.00 -0.96 0.00 -0.20
10 1.7910 0.00 -0.68 0.00 -0.34
11 2.8122 0.00 1.48 0.00 0.51
12 2.8123 0.00 1.47 0.00 0.58
13 2.8123 0.00 1.49 0.00 0.61
14 2.8124 0.00 1.50 0.00 0.54
15 4.0468 0.00 -0.07 0.00 0.13
16 4.0470 0.00 -0.10 0.00 0.14
17 4.7864 0.00 -0.54 0.00 0.23
18 4.7865 0.00 -0.54 0.00 0.15
19 5.0843 0.00 0.17 0.00 0.05
20 5.0843 0.00 0.21 0.00 0.07
21 5.0843 0.00 0.19 0.00 0.11
22 7.9078 0.00 -0.10 0.00 -0.11
23 7.9243 0.00 -0.37 0.00 0.13
24 8.0172 0.00 0.09 0.00 -0.05
25 8.9700 0.00 0.05 0.00 0.05
26 8.9700 0.00 0.03 0.00 -0.23
27 8.9701 0.00 0.23 0.00 -0.08
28 9.7371 0.00 -0.31 0.00 -0.32
29 9.8218 0.00 -0.28 0.00 -0.13
30 9.9667 0.00 0.07 0.00 -0.04
31 9.9667 0.00 -0.20 0.00 -0.23
32 9.9667 0.00 -0.40 0.00 -0.19
33 9.9668 0.00 -0.02 0.00 0.08
34 10.2536 0.00 0.53 0.00 0.17
35 10.8376 0.00 -0.29 0.00 -0.06
36 10.8430 0.00 -0.20 0.00 -0.02
37 10.8651 0.00 -0.39 0.00 -0.31
38 10.9170 0.00 -0.07 0.00 -0.05
39 10.9878 0.00 0.04 0.00 0.03
40 11.0070 0.00 -0.03 0.00 -0.10
41 11.0233 0.00 0.24 0.00 -0.14
42 11.0615 0.00 0.32 0.00 -0.15
43 11.8342 0.00 -0.12 0.00 -0.03
44 11.8397 0.00 -0.31 0.00 0.04
45 11.9244 0.00 -0.38 0.00 0.17
46 11.9898 0.00 0.13 0.00 -0.17
47 12.0418 0.00 0.00 0.00 -0.09
48 12.2686 0.00 0.26 0.00 0.05
49 12.8664 0.00 -0.04 0.00 -0.16
50 12.8799 0.00 -0.22 0.00 0.08
51 12.9428 0.00 0.11 0.00 -0.11
52 16.0276 0.00 0.15 0.00 0.23
53 16.0278 0.00 0.17 0.00 0.17
54 16.0280 0.00 0.28 0.00 0.10
55 21.0164 0.00 -0.12 0.00 0.10
56 21.0166 0.00 0.17 0.00 0.10
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.
612575 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 68.079 68.079 68.080 ecceobj 0.436 0.436 0.436 incobj 4.014 4.014 4.014 qmin 37.720 37.752 37.741 qmax 99.371 99.330 99.496 amean 67.711 67.748 67.801 amin 66.803 66.865 66.940 amax 68.933 68.905 69.003 emean 0.430 0.431 0.431 emin 0.420 0.420 0.422 emax 0.442 0.442 0.443 imean 5.779 5.772 5.769 imin 5.511 5.510 5.495 imax 6.076 6.096 6.077 excite_mean 0.442 0.442 0.443 fracstop 1.000 1.000 1.000 cjmean 3.138 3.138 3.138 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 184.5 185.9 184.7 kozaiamp 179.9 180.0 180.0