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: 05GX186
# Created Wed Dec 25 02:08:43 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 57 observations of 57
# Arc: 22.17y
# First observation: 2001/02/20
# Last observation: 2023/04/24
# Chi-squared of fit: 37.73 DOF: 108 RMS: 0.14
# Min/Max residuals: -0.36 0.41
# Exact a, adot, b, bdot, g, gdot:
1.533009E-05 2.245209E-02 2.117789E-06 1.467516E-03 2.349267E-02 -2.288205E-04
# Covariance matrix:
2.6681E-13 -3.8262E-14 8.1660E-15 -1.9771E-15 3.3710E-15 -5.7399E-14
-3.8262E-14 8.2431E-15 -2.0434E-15 4.9498E-16 7.7287E-15 1.4159E-14
8.1660E-15 -2.0434E-15 1.4773E-13 -9.7760E-15 -9.6132E-16 -3.9770E-15
-1.9771E-15 4.9498E-16 -9.7760E-15 7.8477E-16 2.3571E-16 9.6305E-16
3.3710E-15 7.7287E-15 -9.6132E-16 2.3571E-16 1.1317E-13 4.0423E-15
-5.7399E-14 1.4159E-14 -3.9770E-15 9.6305E-16 4.0423E-15 2.7819E-14
# lat0 lon0 xBary yBary zBary JD0
0.545207 167.348853 0.258680 0.008925 -0.955844 2451960.923034
# Heliocentric elements and errors
Epoch: 2451960.5000 = 2001/02/20
Mean Anomaly: 309.15024 +/- 0.112
Argument of Peri: 60.43452 +/- 0.117
Long of Asc Node: 158.91144 +/- 0.000
Inclination: 3.78499 +/- 0.000
Eccentricity: 0.01642776 +/- 0.0000
Semi-Major Axis: 43.96890885 +/- 0.0025
Time of Perihelion: 2467002.4241 +/- 34.1
Perihelion: 43.24659838 +/- 0.0027
Aphelion: 44.69121932 +/- 0.0028
Period (y) 291.5592 +/- 0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -42.40308407 +/- 0.0006
Ecliptic Y 9.78846527 +/- 0.0001
Ecliptic Z 0.40515710 +/- 0.0000
Ecliptic XDOT -0.00055377 +/- 0.0000
Ecliptic YDOT -0.00255596 +/- 0.0000
Ecliptic ZDOT 0.00017095 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 43.52011562 +/- 0.0006
Geocenter to KBO 42.56649693 +/- 0.0006
# Hcoef: 7.21
The following table shows the complete astrometric record for 05GX186. 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 (05GX186) followed by the observatory code and reference code for the source of the astrometry.
2001 02 20.422291 11 14 18.36 +05 29 59.9 23.0V 05GX186 645 C~1DLx 2001 02 20.423120 11 14 18.36 +05 29 59.9 22.3V 05GX186 645 C~1DLx 2001 02 20.425608 11 14 18.35 +05 30 00.0 24.3V 05GX186 645 C~1DLx 2005 04 10.21298 11 30 28.62 +04 09 21.2 23.3R 05GX186 695 Cn3379 2005 04 11.21598 11 30 24.89 +04 09 45.3 05GX186 695 Cn3379 2005 04 11.30781 11 30 24.55 +04 09 47.5 05GX186 695 Cn3379 2006 03 02.39898 11 38 06.18 +03 25 11.4 22.7R 05GX186 695 Cr3594 2006 03 02.45107 11 38 05.95 +03 25 13.0 05GX186 695 Cr3594 2006 03 02.50340 11 38 05.73 +03 25 14.5 05GX186 695 Cr3594 2006 04 26.05300 11 34 28.71 +03 49 02.4 22.1R 05GX186 807 Cr3594 2006 04 26.13648 11 34 28.45 +03 49 04.0 05GX186 807 Cr3594 2006 04 28.04040 11 34 22.89 +03 49 39.7 05GX186 807 Cr3594 2007 02 15.28762 11 44 00.45 +02 51 59.8 05GX186 304 Cu1516 2007 02 15.32606 11 44 00.28 +02 52 00.8 05GX186 304 Cu1516 2007 02 15.36483 11 44 00.15 +02 52 01.7 05GX186 304 Cu1516 2013 03 07.276203 12 11 53.80 +00 22 50.7 23.9r 05GX186 309 C~2HNs 2013 03 07.280879 12 11 53.78 +00 22 50.8 23.9r 05GX186 309 C~2HNs 2013 03 07.285567 12 11 53.76 +00 22 50.9 24.3r 05GX186 309 C~2HNs 2013 03 07.290254 12 11 53.74 +00 22 51.0 24.3r 05GX186 309 C~2HNs 2013 03 07.294953 12 11 53.72 +00 22 51.2 24.3r 05GX186 309 C~2HNs 2013 03 14.28531 12 11 24.36 +00 26 11.8 23.2R 05GX186 695 C~0udF 2013 03 14.39492 12 11 23.88 +00 26 14.9 05GX186 695 C~0udF 2013 03 14.45549 12 11 23.64 +00 26 16.9 05GX186 695 C~0udF 2016 04 02.38313 12 24 42.93 -00 44 34.0 23.0i 05GX186 T09 C~89LB 2016 04 02.39342 12 24 42.89 -00 44 33.5 23.1i 05GX186 T09 C~89LB 2016 04 02.41191 12 24 42.80 -00 44 33.3 23.1i 05GX186 T09 C~89LB 2016 04 02.43645 12 24 42.70 -00 44 32.5 23.0i 05GX186 T09 C~89LB 2016 04 02.46904 12 24 42.54 -00 44 31.5 23.2i 05GX186 T09 C~89LB 2016 04 02.49363 12 24 42.44 -00 44 31.0 23.6i 05GX186 T09 C~89LB 2016 04 02.51521 12 24 42.37 -00 44 30.3 23.1i 05GX186 T09 C~89LB 2016 04 02.51791 12 24 42.34 -00 44 30.1 23.5i 05GX186 T09 C~89LB 2016 04 04.34027 12 24 34.53 -00 43 38.9 24.6g 05GX186 T09 C~89LB 2016 04 04.34883 12 24 34.49 -00 43 38.6 24.4g 05GX186 T09 C~89LB 2016 04 04.36377 12 24 34.43 -00 43 38.1 24.5g 05GX186 T09 C~89LB 2016 04 04.38940 12 24 34.31 -00 43 37.2 24.4g 05GX186 T09 C~89LB 2016 04 04.40858 12 24 34.22 -00 43 36.9 24.2g 05GX186 T09 C~89LB 2016 04 04.41735 12 24 34.19 -00 43 36.5 24.1g 05GX186 T09 C~89LB 2016 04 04.50037 12 24 33.83 -00 43 34.2 24.8g 05GX186 T09 C~89LB 2016 06 04.25539 12 21 29.31 -00 24 30.4 23.0z 05GX186 T09 C~8Pvk 2016 06 04.26765 12 21 29.28 -00 24 30.4 22.8z 05GX186 T09 C~8Pvk 2016 06 04.27307 12 21 29.30 -00 24 30.4 22.8z 05GX186 T09 C~8Pvk 2016 06 04.32166 12 21 29.22 -00 24 30.1 22.8z 05GX186 T09 C~8Pvk 2016 06 04.33787 12 21 29.21 -00 24 30.2 22.8z 05GX186 T09 C~8Pvk 2016 06 05.31150 12 21 28.16 -00 24 25.0 23.6r 05GX186 T09 C~8Pvk 2016 06 05.32218 12 21 28.15 -00 24 25.0 23.4r 05GX186 T09 C~8Pvk 2016 06 05.32429 12 21 28.14 -00 24 24.9 23.4r 05GX186 T09 C~8Pvk 2016 06 05.34129 12 21 28.13 -00 24 24.7 23.3r 05GX186 T09 C~8Pvk 2016 06 05.35188 12 21 28.12 -00 24 24.9 23.3r 05GX186 T09 C~8Pvk 2017 02 23.52446 12 32 13.08 -01 28 55.9 23.5r 05GX186 T09 C~7xJG 2017 02 23.62726 12 32 12.72 -01 28 53.6 24.0r 05GX186 T09 C~7xJG 2017 02 23.62935 12 32 12.70 -01 28 53.3 24.1r 05GX186 T09 C~7xJG 2021 05 12.178190 12 46 40.685 -02 41 18.31 23.1G 05GX186 G37 C~4pRW 2021 05 12.229740 12 46 40.530 -02 41 17.40 05GX186 G37 C~4pRW 2021 05 12.276900 12 46 40.378 -02 41 16.49 05GX186 G37 C~4pRW 2023 04 24.151440 12 57 37.548 -03 40 45.75 23.3G 05GX186 G37 C~6hGE 2023 04 24.213380 12 57 37.272 -03 40 44.14 05GX186 G37 C~6hGE 2023 04 24.273610 12 57 37.021 -03 40 42.71 05GX186 G37 C~6hGE
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 -0.20
2 0.0000 0.00 -0.08 0.00 -0.22
3 0.0000 0.00 -0.07 0.00 -0.19
4 4.1336 0.00 -0.03 0.00 -0.09
5 4.1363 0.00 -0.17 0.00 -0.11
6 4.1366 0.00 -0.09 0.00 -0.10
7 5.0266 0.00 0.30 0.00 0.02
8 5.0268 0.00 0.20 0.00 0.14
9 5.0269 0.00 0.26 0.00 0.15
10 5.1763 0.00 -0.03 0.00 0.27
11 5.1765 0.00 -0.09 0.00 0.28
12 5.1817 0.00 -0.06 0.00 0.40
13 5.9846 0.00 0.19 0.00 0.01
14 5.9847 0.00 -0.20 0.00 0.03
15 5.9848 0.00 0.02 0.00 -0.06
16 12.0407 0.00 0.07 0.00 -0.06
17 12.0407 0.00 0.07 0.00 -0.10
18 12.0407 0.00 0.06 0.00 -0.13
19 12.0407 0.00 0.06 0.00 -0.16
20 12.0407 0.00 0.05 0.00 -0.09
21 12.0599 0.00 0.13 0.00 0.10
22 12.0602 0.00 0.07 0.00 0.02
23 12.0603 0.00 0.41 0.00 0.27
24 15.1128 0.00 -0.16 0.00 0.03
25 15.1129 0.00 -0.09 0.00 0.23
26 15.1129 0.00 -0.22 0.00 -0.09
27 15.1130 0.00 -0.10 0.00 0.01
28 15.1131 0.00 -0.36 0.00 0.09
29 15.1131 0.00 -0.24 0.00 -0.11
30 15.1132 0.00 0.13 0.00 -0.02
31 15.1132 0.00 -0.15 0.00 0.10
32 15.1182 0.00 -0.02 0.00 -0.17
33 15.1182 0.00 -0.06 0.00 -0.11
34 15.1183 0.00 0.02 0.00 -0.03
35 15.1183 0.00 -0.10 0.00 0.15
36 15.1184 0.00 -0.19 0.00 -0.09
37 15.1184 0.00 -0.07 0.00 0.06
38 15.1186 0.00 -0.03 0.00 0.03
39 15.2850 0.00 0.17 0.00 0.06
40 15.2850 0.00 -0.06 0.00 -0.01
41 15.2850 0.00 0.34 0.00 -0.03
42 15.2851 0.00 0.00 0.00 -0.00
43 15.2852 0.00 0.14 0.00 -0.19
44 15.2879 0.00 -0.04 0.00 -0.04
45 15.2879 0.00 -0.01 0.00 -0.10
46 15.2879 0.00 -0.13 0.00 -0.01
47 15.2879 0.00 0.00 0.00 0.11
48 15.2880 0.00 0.03 0.00 -0.14
49 16.0085 0.00 -0.10 0.00 0.21
50 16.0088 0.00 -0.06 0.00 -0.03
51 16.0088 0.00 -0.25 0.00 0.22
52 20.2211 0.00 -0.07 0.00 -0.06
53 20.2212 0.00 0.14 0.00 -0.13
54 20.2214 0.00 0.17 0.00 -0.11
55 22.1704 0.00 0.23 0.00 0.02
56 22.1705 0.00 -0.03 0.00 0.06
57 22.1707 0.00 -0.01 0.00 -0.03
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.
05GX186 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 43.810 43.810 43.810 ecceobj 0.015 0.015 0.015 incobj 3.790 3.790 3.790 qmin 42.665 42.672 42.662 qmax 45.558 45.552 45.568 amean 44.028 44.028 44.028 amin 43.690 43.688 43.690 amax 44.365 44.367 44.368 emean 0.014 0.014 0.014 emin 0.000 0.000 0.000 emax 0.027 0.027 0.027 imean 3.560 3.560 3.560 imin 3.004 3.004 3.005 imax 4.187 4.187 4.187 excite_mean 0.064 0.064 0.064 fracstop 1.000 1.000 1.000 cjmean 3.097 3.097 3.097 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 176.9 177.2 176.9 kozaiamp 180.0 180.0 180.0