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: 612086
# Created Sat Apr 20 01:09:10 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 36 observations of 36
# Arc: 23.15y
# First observation: 1999/02/11
# Last observation: 2022/04/08
# Chi-squared of fit: 113.72 DOF: 66 RMS: 0.31
# Min/Max residuals: -1.26 1.00
# Exact a, adot, b, bdot, g, gdot:
1.488028E-05 2.147847E-02 3.495857E-06 3.697316E-03 2.370516E-02 -5.349234E-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
0.291069 129.349677 -0.224729 0.004697 -0.967718 2451220.806763
# Heliocentric elements and errors
Epoch: 2451220.5000 = 1999/02/11
Mean Anomaly: 277.02947 +/- 0.000
Argument of Peri: 111.06365 +/- 0.000
Long of Asc Node: 127.98680 +/- 0.000
Inclination: 9.77266 +/- 0.000
Eccentricity: 0.23226402 +/- 0.0000
Semi-Major Axis: 42.09223452 +/- 0.0000
Time of Perihelion: 2474209.6409 +/- 0.0
Perihelion: 32.31572306 +/- 0.0000
Aphelion: 51.86874598 +/- 0.0000
Period (y) 273.0934 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -27.52662733 +/- 0.0000
Ecliptic Y 33.22630014 +/- 0.0000
Ecliptic Z 0.21444755 +/- 0.0000
Ecliptic XDOT -0.00152688 +/- 0.0000
Ecliptic YDOT -0.00204329 +/- 0.0000
Ecliptic ZDOT 0.00042388 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 43.14812557 +/- 0.0000
Geocenter to KBO 42.18508971 +/- 0.0000
# Hcoef: 7.08
The following table shows the complete astrometric record for 612086. 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 (612086) followed by the observatory code and reference code for the source of the astrometry.
1999 02 11.30602 08 47 28.29 +18 11 42.5 22.7R 612086 568 Ca4191 1999 02 11.38707 08 47 27.89 +18 11 44.1 22.7R 612086 568 Ca4191 1999 02 17.43889 08 46 59.44 +18 13 48.1 22.7R 612086 568 Ca4191 1999 02 18.39633 08 46 55.05 +18 14 07.2 22.7R 612086 568 Ca4191 1999 03 19.25198 08 45 03.95 +18 22 13.9 612086 696 Ca4191 1999 03 19.30211 08 45 03.85 +18 22 14.5 612086 696 Ca4191 1999 03 19.34969 08 45 03.81 +18 22 14.5 612086 696 Ca4191 1999 04 11.33934 08 44 18.72 +18 25 49.6 23.4R 612086 568 Ca4843 1999 04 12.37049 08 44 17.78 +18 25 54.7 23.4R 612086 568 Ca4843 1999 05 06.27330 08 44 24.37 +18 26 08.6 23.1R 612086 568 Cc9919 1999 05 06.32238 08 44 24.43 +18 26 08.5 23.1R 612086 568 Cc9919 1999 12 30.63648 08 56 03.84 +17 48 48.6 612086 568 Ca8502 1999 12 31.61208 08 55 59.92 +17 49 07.3 612086 568 Ca8502 1999 12 31.63278 08 55 59.83 +17 49 07.6 612086 568 Ca8502 2002 02 03.49523 09 04 00.95 +17 43 55.5 23.2R 612086 568 Cf1463 2002 02 04.46888 09 03 56.12 +17 44 18.1 612086 568 Cf1463 2002 02 04.53420 09 03 55.81 +17 44 19.6 612086 568 Cf1463 2005 02 10.30899 09 19 50.50 +17 15 45.1 23.9g 612086 568 C~0Wz5 2005 02 10.39196 09 19 50.09 +17 15 47.0 24.0g 612086 568 C~0Wz5 2005 02 10.43152 09 19 49.90 +17 15 47.7 23.6g 612086 568 C~0Wz5 2005 02 15.33214 09 19 25.83 +17 17 48.0 23.3g 612086 568 C~0Wz5 2005 04 11.30482 09 16 08.68 +17 33 28.6 23.4i 612086 568 C~0Wz5 2005 04 11.33442 09 16 08.63 +17 33 28.8 23.5i 612086 568 C~0Wz5 2005 04 11.35929 09 16 08.59 +17 33 28.9 23.3i 612086 568 C~0Wz5 2013 03 13.24431 10 03 12.76 +15 36 50.1 22.5R 612086 695 C~0uco 2013 03 14.20106 10 03 08.49 +15 37 12.8 612086 695 C~0uco 2013 03 14.35133 10 03 07.81 +15 37 16.3 612086 695 C~0uco 2016 01 17.267344 10 25 39.59 +14 14 31.8 612086 W84 C~3i8v 2016 01 17.268414 10 25 39.60 +14 14 31.9 612086 W84 C~3i8v 2017 01 09.253831 10 32 11.41 +13 51 00.2 612086 W84 C~3i8v 2017 01 09.322431 10 32 11.20 +13 51 02.0 612086 W84 C~3i8v 2018 03 17.170417 10 33 22.70 +14 03 44.0 612086 W84 C~3i8w 2018 03 17.171985 10 33 22.69 +14 03 43.9 612086 W84 C~3i8w 2022 04 08.134160 10 57 03.342 +12 42 44.69 22.8G 612086 G37 C~5aUX 2022 04 08.168930 10 57 03.181 +12 42 45.57 612086 G37 C~5aUX 2022 04 08.204070 10 57 03.054 +12 42 46.76 612086 G37 C~5aUX
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 -0.18 0.00 -0.17
2 0.0002 0.00 -0.27 0.00 -0.27
3 0.0168 0.00 -0.26 0.00 -0.10
4 0.0194 0.00 -0.19 0.00 -0.13
5 0.0984 0.00 -1.26 0.00 -0.27
6 0.0986 0.00 -0.52 0.00 -0.31
7 0.0987 0.00 1.00 0.00 -0.92
8 0.1616 0.00 0.41 0.00 0.25
9 0.1644 0.00 0.24 0.00 0.06
10 0.2299 0.00 0.08 0.00 0.02
11 0.2300 0.00 -0.00 0.00 0.12
12 0.8825 0.00 0.22 0.00 -0.05
13 0.8852 0.00 -0.14 0.00 0.12
14 0.8852 0.00 -0.22 0.00 0.03
15 2.9793 0.00 0.58 0.00 -0.08
16 2.9820 0.00 0.08 0.00 -0.11
17 2.9821 0.00 0.34 0.00 -0.11
18 5.9986 0.00 -0.11 0.00 0.51
19 5.9989 0.00 -0.02 0.00 0.34
20 5.9990 0.00 0.11 0.00 0.06
21 6.0124 0.00 -0.11 0.00 0.33
22 6.1629 0.00 0.28 0.00 0.41
23 6.1630 0.00 0.28 0.00 0.40
24 6.1630 0.00 0.31 0.00 0.32
25 14.0833 0.00 -0.18 0.00 0.27
26 14.0860 0.00 -0.19 0.00 0.08
27 14.0864 0.00 -0.20 0.00 0.02
28 16.9308 0.00 -0.23 0.00 -0.05
29 16.9308 0.00 -0.02 0.00 0.02
30 17.9109 0.00 -0.03 0.00 -0.13
31 17.9111 0.00 0.05 0.00 -0.09
32 19.0934 0.00 0.01 0.00 -0.07
33 19.0934 0.00 -0.03 0.00 -0.22
34 23.1535 0.00 0.19 0.00 -0.38
35 23.1536 0.00 -0.12 0.00 -0.22
36 23.1537 0.00 0.09 0.00 0.25
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.
612086 quality flag:3 Type: 5:3EE 5:3EE 5:3EE axisobj 42.199 42.199 42.200 ecceobj 0.231 0.231 0.231 incobj 9.760 9.760 9.760 qmin 31.609 31.609 31.609 qmax 53.603 53.603 53.602 amean 42.327 42.327 42.327 amin 41.877 41.877 41.877 amax 42.857 42.856 42.862 emean 0.227 0.227 0.227 emin 0.204 0.204 0.204 emax 0.251 0.251 0.251 imean 9.139 9.140 9.138 imin 7.974 7.974 7.974 imax 9.824 9.825 9.824 excite_mean 0.278 0.278 0.278 fracstop 1.000 1.000 1.000 cjmean 2.991 2.991 2.991 libcent 0 178.7 178.6 179.1 libamp 0 71.8 71.9 72.2 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 158.6 158.3 158.8 kozaiamp 179.9 179.9 179.9