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: 548504
# Created Sun Nov 24 02:07:30 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 138 observations of 138
# Arc: 11.80y
# First observation: 2010/05/13
# Last observation: 2022/03/02
# Chi-squared of fit: 173.12 DOF: 270 RMS: 0.20
# Min/Max residuals: -0.68 1.01
# Exact a, adot, b, bdot, g, gdot:
1.511628E-05 2.241235E-02 -3.982036E-07 -3.263046E-04 2.341393E-02 -5.059416E-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
2.712794 172.491568 -0.871761 0.024210 -0.511908 2455329.810666
# Heliocentric elements and errors
Epoch: 2455330.5000 = 2010/05/14
Mean Anomaly: 256.44198 +/- 0.000
Argument of Peri: 212.24550 +/- 0.000
Long of Asc Node: 65.25999 +/- 0.000
Inclination: 2.82443 +/- 0.000
Eccentricity: 0.00282556 +/- 0.0000
Semi-Major Axis: 43.19713238 +/- 0.0000
Time of Perihelion: 2485161.1042 +/- 0.0
Perihelion: 43.07507644 +/- 0.0000
Aphelion: 43.31918833 +/- 0.0000
Period (y) 283.9165 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -42.91399321 +/- 0.0000
Ecliptic Y 4.77458347 +/- 0.0000
Ecliptic Z 2.02144226 +/- 0.0000
Ecliptic XDOT -0.00028395 +/- 0.0000
Ecliptic YDOT -0.00259977 +/- 0.0000
Ecliptic ZDOT -0.00004095 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 43.22607826 +/- 0.0000
Geocenter to KBO 42.70969223 +/- 0.0000
# Hcoef: 6.33
The following table shows the complete astrometric record for 548504. 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 (548504) followed by the observatory code and reference code for the source of the astrometry.
2010 05 13.30990 11 36 43.384 +05 28 16.05 21.8G 548504 F51 C~3458 2010 07 01.28353 11 36 46.460 +05 24 30.86 22.1G 548504 F51 C~3458 2010 07 01.29142 11 36 46.470 +05 24 30.85 23.2G 548504 F51 C~3458 2010 12 15.56883 11 48 28.786 +04 09 14.30 22.6G 548504 F51 C~3458 2010 12 15.57444 11 48 28.794 +04 09 14.28 22.3G 548504 F51 C~3458 2010 12 15.58403 11 48 28.800 +04 09 14.18 22.3G 548504 F51 C~3458 2010 12 15.58964 11 48 28.793 +04 09 13.96 23.0G 548504 F51 C~3458 2011 03 11.36183 11 45 15.230 +04 34 01.88 21.9G 548504 F51 C~3458 2011 04 02.30488 11 43 39.787 +04 44 05.08 22.5G 548504 F51 C~3458 2011 04 02.32003 11 43 39.735 +04 44 05.40 22.6G 548504 F51 C~3458 2011 04 02.33617 11 43 39.648 +04 44 05.88 22.7G 548504 F51 C~3458 2011 04 02.35128 11 43 39.582 +04 44 06.01 22.3G 548504 F51 C~3458 2011 06 24.30379 11 41 10.794 +04 55 20.19 22.7G 548504 F51 C~3458 2012 02 14.61569 11 51 40.637 +03 50 26.07 22.2G 548504 F51 C~3458 2012 02 26.40569 11 50 55.404 +03 55 39.40 22.6G 548504 F51 C~3458 2012 02 26.42010 11 50 55.345 +03 55 40.12 23.0G 548504 F51 C~3458 2012 02 26.43450 11 50 55.294 +03 55 40.04 22.3G 548504 F51 C~3458 2012 02 26.44891 11 50 55.214 +03 55 40.69 22.8G 548504 F51 C~3458 2012 02 26.54614 11 50 54.819 +03 55 42.99 22.0G 548504 F51 C~3458 2012 03 27.33065 11 48 46.245 +04 09 41.16 22.9G 548504 F51 C~3458 2012 03 27.34509 11 48 46.193 +04 09 41.62 22.4G 548504 F51 C~3458 2012 03 27.35953 11 48 46.089 +04 09 41.92 22.3G 548504 F51 C~3458 2012 03 27.37400 11 48 46.051 +04 09 42.52 22.4G 548504 F51 C~3458 2012 05 16.26166 11 45 59.790 +04 25 29.89 22.1G 548504 F51 C~3458 2013 03 08.44710 11 54 54.042 +03 28 26.27 22.5G 548504 F51 C~3458 2013 03 08.46122 11 54 54.020 +03 28 27.07 22.2G 548504 F51 C~3458 2013 06 28.28482 11 50 31.302 +03 51 45.89 22.5G 548504 F51 C~3458 2014 02 09.56161 12 01 21.722 +02 44 06.95 22.1G 548504 F51 C~3458 2014 02 26.55964 12 00 20.223 +02 51 18.64 22.1G 548504 F51 C~3458 2014 02 26.57187 12 00 20.141 +02 51 18.58 22.5G 548504 F51 C~3458 2014 02 26.58408 12 00 20.136 +02 51 19.09 22.4G 548504 F51 C~3458 2014 02 26.59634 12 00 20.061 +02 51 19.45 22.2G 548504 F51 C~3458 2014 02 27.48333 12 00 16.516 +02 51 43.64 22.7G 548504 F51 C~3458 2014 02 27.49557 12 00 16.471 +02 51 44.22 22.7G 548504 F51 C~3458 2014 02 27.50788 12 00 16.427 +02 51 43.97 22.5G 548504 F51 C~3458 2014 02 27.52022 12 00 16.366 +02 51 44.64 23.6G 548504 F51 C~3458 2014 03 24.35708 11 58 29.957 +03 03 25.17 22.4G 548504 F51 C~3458 2014 03 24.36919 11 58 29.906 +03 03 25.65 21.6G 548504 F51 C~3458 2014 03 24.38131 11 58 29.842 +03 03 25.99 22.9G 548504 F51 C~3458 2014 03 24.39347 11 58 29.774 +03 03 26.72 22.5G 548504 F51 C~3458 2014 06 28.27024 11 55 07.888 +03 20 19.80 22.8G 548504 F51 C~3458 2014 06 28.27419 11 55 07.895 +03 20 20.16 22.5G 548504 F51 C~3458 2014 11 30.64464 12 06 24.665 +02 05 25.44 22.7G 548504 F51 C~3458 2015 01 19.57733 12 06 54.600 +02 05 14.23 22.9G 548504 F51 C~3458 2015 01 19.59086 12 06 54.582 +02 05 14.31 22.2G 548504 F51 C~3458 2015 01 19.60439 12 06 54.561 +02 05 14.53 22.5G 548504 F51 C~3458 2015 01 19.61791 12 06 54.527 +02 05 14.85 23.2G 548504 F51 C~3458 2015 01 21.60273 12 06 51.273 +02 05 42.42 22.4G 548504 F51 C~3458 2015 01 21.61494 12 06 51.252 +02 05 42.72 23.0G 548504 F51 C~3458 2015 01 21.62723 12 06 51.236 +02 05 42.92 22.6G 548504 F51 C~3458 2015 01 21.63952 12 06 51.210 +02 05 42.99 22.8G 548504 F51 C~3458 2015 02 18.53386 12 05 35.215 +02 15 12.28 23.2G 548504 F51 C~3458 2015 02 18.54632 12 05 35.160 +02 15 12.77 22.9G 548504 F51 C~3458 2015 02 18.55879 12 05 35.154 +02 15 13.41 23.1G 548504 F51 C~3458 2015 02 18.57125 12 05 35.066 +02 15 13.28 22.0G 548504 F51 C~3458 2015 02 19.50359 12 05 31.710 +02 15 37.31 22.0G 548504 F51 C~3458 2015 02 19.51600 12 05 31.655 +02 15 37.42 21.8G 548504 F51 C~3458 2015 02 19.52845 12 05 31.605 +02 15 37.16 22.0G 548504 F51 C~3458 2015 02 19.54091 12 05 31.596 +02 15 38.21 22.4G 548504 F51 C~3458 2015 03 23.47771 12 03 19.300 +02 30 22.62 23.2G 548504 F51 C~3458 2015 03 23.49027 12 03 19.258 +02 30 22.62 22.1G 548504 F51 C~3458 2015 03 23.50283 12 03 19.210 +02 30 23.37 22.9G 548504 F51 C~3458 2015 03 23.51541 12 03 19.133 +02 30 23.63 22.5G 548504 F51 C~3458 2015 03 24.41514 12 03 15.215 +02 30 48.64 21.9G 548504 F51 C~3458 2015 03 24.42961 12 03 15.142 +02 30 49.06 22.4G 548504 F51 C~3458 2015 03 24.44408 12 03 15.054 +02 30 49.68 22.7G 548504 F51 C~3458 2015 03 24.45859 12 03 15.006 +02 30 50.16 22.1G 548504 F51 C~3458 2016 01 16.55624 12 11 39.551 +01 32 21.01 22.6G 548504 F51 C~3458 2016 01 16.56836 12 11 39.543 +01 32 21.42 22.4G 548504 F51 C~3458 2016 01 16.58047 12 11 39.536 +01 32 21.58 22.5G 548504 F51 C~3458 2016 01 16.59270 12 11 39.497 +01 32 21.33 22.9G 548504 F51 C~3458 2016 01 21.64226 12 11 32.448 +01 33 24.41 22.6G 548504 F51 C~3458 2016 02 02.57574 12 11 07.740 +01 36 42.02 22.8G 548504 F51 C~3458 2016 02 09.49295 12 10 48.745 +01 39 04.17 22.5G 548504 F51 C~3458 2016 02 09.50512 12 10 48.689 +01 39 04.62 22.7G 548504 F51 C~3458 2016 02 09.51730 12 10 48.663 +01 39 04.45 22.9G 548504 F51 C~3458 2016 02 29.51417 12 09 38.122 +01 47 21.21 22.7G 548504 F51 C~3458 2016 03 07.47183 12 09 09.623 +01 50 33.96 22.3G 548504 F51 C~3458 2016 04 03.38734 12 07 13.088 +02 03 06.65 22.1G 548504 F51 C~3458 2016 04 03.39912 12 07 13.035 +02 03 06.95 22.8G 548504 F51 C~3458 2016 04 03.41095 12 07 12.983 +02 03 07.44 22.6G 548504 F51 C~3458 2016 04 03.42279 12 07 12.931 +02 03 07.55 22.4G 548504 F51 C~3458 2016 04 29.43273 12 05 32.632 +02 13 06.97 23.4G 548504 F51 C~3458 2017 02 21.47654 12 14 49.444 +01 11 34.62 23.2G 548504 F51 C~3458 2017 02 21.48875 12 14 49.389 +01 11 34.18 22.1G 548504 F51 C~3458 2017 02 21.50099 12 14 49.375 +01 11 34.53 22.5G 548504 F51 C~3458 2017 02 21.51323 12 14 49.299 +01 11 34.90 22.3G 548504 F51 C~3458 2017 03 04.44397 12 14 07.124 +01 16 24.65 22.8G 548504 F51 C~3458 2017 03 04.45615 12 14 07.084 +01 16 24.70 22.2G 548504 F51 C~3458 2017 03 04.46836 12 14 07.040 +01 16 25.25 22.5G 548504 F51 C~3458 2017 03 04.48061 12 14 06.975 +01 16 25.44 22.8G 548504 F51 C~3458 2017 03 20.34143 12 12 59.574 +01 23 51.55 21.5G 548504 F51 C~3458 2017 03 20.35323 12 12 59.546 +01 23 51.86 22.0G 548504 F51 C~3458 2017 03 20.36510 12 12 59.512 +01 23 52.26 21.9G 548504 F51 C~3458 2017 03 20.37694 12 12 59.450 +01 23 52.66 21.8G 548504 F51 C~3458 2017 03 29.40242 12 12 20.002 +01 28 05.80 22.2G 548504 F51 C~3458 2017 03 29.41474 12 12 19.899 +01 28 05.86 22.8G 548504 F51 C~3458 2017 03 29.42831 12 12 19.837 +01 28 06.44 22.6G 548504 F51 C~3458 2017 04 03.46024 12 11 58.050 +01 30 23.67 22.2G 548504 F51 C~3458 2017 04 03.47413 12 11 57.980 +01 30 23.83 22.6G 548504 F51 C~3458 2017 04 03.48808 12 11 57.926 +01 30 24.25 22.1G 548504 F51 C~3458 2017 04 03.50201 12 11 57.852 +01 30 24.56 22.0G 548504 F51 C~3458 2017 04 16.30279 12 11 04.839 +01 35 50.01 22.5G 548504 F51 C~3458 2017 04 16.31489 12 11 04.785 +01 35 50.31 22.6G 548504 F51 C~3458 2017 04 16.32694 12 11 04.749 +01 35 51.08 22.3G 548504 F51 C~3458 2017 04 16.33901 12 11 04.695 +01 35 50.85 22.4G 548504 F51 C~3458 2017 04 20.36550 12 10 49.078 +01 37 24.11 22.3G 548504 F51 C~3458 2017 04 20.37618 12 10 49.008 +01 37 24.52 22.3G 548504 F51 C~3458 2017 04 20.38684 12 10 48.985 +01 37 24.44 22.9G 548504 F51 C~3458 2017 04 20.39750 12 10 48.899 +01 37 24.60 24.4G 548504 F51 C~3458 2017 04 27.30745 12 10 23.760 +01 39 51.91 22.5G 548504 F51 C~3458 2017 04 27.32115 12 10 23.708 +01 39 52.18 22.3G 548504 F51 C~3458 2017 04 27.33488 12 10 23.644 +01 39 52.45 22.3G 548504 F51 C~3458 2017 04 27.34867 12 10 23.613 +01 39 52.71 21.8G 548504 F51 C~3458 2017 12 28.62919 12 21 02.543 +00 26 28.98 22.7G 548504 F51 C~3458 2017 12 28.63763 12 21 02.572 +00 26 28.78 22.7G 548504 F51 C~3458 2017 12 28.64610 12 21 02.600 +00 26 28.90 23.2G 548504 F51 C~3458 2017 12 28.65460 12 21 02.607 +00 26 28.68 22.8G 548504 F51 C~3458 2018 03 10.46339 12 18 27.123 +00 46 24.71 22.2G 548504 F51 C~3458 2018 03 10.47418 12 18 27.094 +00 46 24.94 22.2G 548504 F51 C~3458 2018 03 17.43524 12 17 57.378 +00 49 40.90 22.9G 548504 F51 C~3458 2018 03 17.44925 12 17 57.323 +00 49 41.17 22.3G 548504 F51 C~3458 2018 03 17.46323 12 17 57.281 +00 49 42.08 22.4G 548504 F51 C~3458 2018 03 17.47725 12 17 57.272 +00 49 42.64 22.6G 548504 F51 C~3458 2018 03 19.39179 12 17 48.899 +00 50 36.24 22.3G 548504 F51 C~3458 2018 03 19.40472 12 17 48.846 +00 50 36.62 22.5G 548504 F51 C~3458 2018 03 19.41769 12 17 48.787 +00 50 37.11 22.7G 548504 F51 C~3458 2018 03 19.43074 12 17 48.737 +00 50 37.41 22.5G 548504 F51 C~3458 2018 04 13.34940 12 16 01.407 +01 01 54.24 22.2G 548504 F51 C~3458 2018 04 13.36191 12 16 01.357 +01 01 54.77 22.9G 548504 F51 C~3458 2018 04 13.37449 12 16 01.283 +01 01 55.17 20.9G 548504 F51 C~3458 2021 03 15.419600 12 32 14.954 -00 49 03.15 22.4w 548504 F51 C~4fRq 2021 03 15.433144 12 32 14.888 -00 49 02.81 22.2w 548504 F51 C~4fRq 2021 03 15.446705 12 32 14.828 -00 49 02.25 22.3w 548504 F51 C~4fRq 2021 03 15.460394 12 32 14.757 -00 49 01.98 22.4w 548504 F51 C~4fRq 2022 03 02.416490 12 37 50.526 -01 27 28.01 22.5G 548504 G37 C~5V4S 2022 03 02.457620 12 37 50.373 -01 27 26.97 548504 G37 C~5V4S 2022 03 02.497540 12 37 50.235 -01 27 25.74 548504 G37 C~5V4S
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 0.02 0.00 0.03
2 0.1341 0.00 0.15 0.00 -0.05
3 0.1341 0.00 0.06 0.00 0.07
4 0.5921 0.00 -0.07 0.00 -0.02
5 0.5921 0.00 -0.03 0.00 -0.03
6 0.5921 0.00 -0.08 0.00 -0.10
7 0.5921 0.00 -0.27 0.00 -0.30
8 0.8270 0.00 0.07 0.00 0.24
9 0.8870 0.00 0.04 0.00 0.08
10 0.8871 0.00 0.23 0.00 0.01
11 0.8871 0.00 -0.04 0.00 0.07
12 0.8872 0.00 -0.06 0.00 -0.18
13 1.1143 0.00 0.09 0.00 -0.22
14 1.7585 0.00 0.00 0.00 -0.03
15 1.7908 0.00 0.04 0.00 -0.01
16 1.7909 0.00 0.05 0.00 0.31
17 1.7909 0.00 0.18 0.00 -0.16
18 1.7909 0.00 -0.13 0.00 0.09
19 1.7912 0.00 0.00 0.00 -0.30
20 1.8727 0.00 0.02 0.00 0.06
21 1.8728 0.00 0.19 0.00 0.13
22 1.8728 0.00 -0.42 0.00 0.04
23 1.8729 0.00 -0.03 0.00 0.24
24 2.0095 0.00 -0.18 0.00 -0.21
25 2.8204 0.00 -0.16 0.00 -0.03
26 2.8204 0.00 0.44 0.00 0.37
27 3.1266 0.00 0.10 0.00 0.09
28 3.7461 0.00 0.42 0.00 0.46
29 3.7926 0.00 0.02 0.00 0.24
30 3.7926 0.00 -0.47 0.00 -0.15
31 3.7927 0.00 0.20 0.00 0.03
32 3.7927 0.00 -0.18 0.00 0.05
33 3.7951 0.00 -0.13 0.00 -0.04
34 3.7952 0.00 -0.05 0.00 0.21
35 3.7952 0.00 0.05 0.00 -0.38
36 3.7952 0.00 -0.11 0.00 -0.05
37 3.8632 0.00 -0.06 0.00 -0.23
38 3.8633 0.00 -0.02 0.00 -0.09
39 3.8633 0.00 -0.17 0.00 -0.09
40 3.8633 0.00 -0.38 0.00 0.30
41 4.1258 0.00 -0.15 0.00 -0.29
42 4.1258 0.00 -0.12 0.00 0.12
43 4.5512 0.00 -0.06 0.00 -0.04
44 4.6879 0.00 -0.05 0.00 0.10
45 4.6880 0.00 0.02 0.00 -0.01
46 4.6880 0.00 0.04 0.00 0.03
47 4.6880 0.00 -0.14 0.00 0.17
48 4.6935 0.00 0.01 0.00 -0.17
49 4.6935 0.00 0.03 0.00 -0.04
50 4.6935 0.00 0.12 0.00 -0.02
51 4.6936 0.00 0.07 0.00 -0.13
52 4.7699 0.00 0.06 0.00 -0.22
53 4.7700 0.00 -0.08 0.00 -0.05
54 4.7700 0.00 0.51 0.00 0.28
55 4.7701 0.00 -0.12 0.00 -0.17
56 4.7726 0.00 -0.10 0.00 0.22
57 4.7726 0.00 -0.23 0.00 0.02
58 4.7727 0.00 -0.29 0.00 -0.56
59 4.7727 0.00 0.27 0.00 0.17
60 4.8601 0.00 -0.04 0.00 0.08
61 4.8602 0.00 0.18 0.00 -0.27
62 4.8602 0.00 0.30 0.00 0.13
63 4.8602 0.00 -0.02 0.00 0.03
64 4.8627 0.00 0.25 0.00 -0.21
65 4.8628 0.00 0.13 0.00 -0.19
66 4.8628 0.00 -0.23 0.00 0.02
67 4.8628 0.00 0.03 0.00 0.09
68 5.6790 0.00 -0.02 0.00 -0.03
69 5.6790 0.00 0.09 0.00 0.24
70 5.6790 0.00 0.21 0.00 0.27
71 5.6791 0.00 -0.14 0.00 -0.12
72 5.6929 0.00 0.09 0.00 -0.07
73 5.7256 0.00 -0.34 0.00 0.10
74 5.7445 0.00 0.23 0.00 -0.05
75 5.7445 0.00 -0.05 0.00 0.13
76 5.7446 0.00 0.12 0.00 -0.31
77 5.7993 0.00 0.26 0.00 -0.40
78 5.8184 0.00 0.06 0.00 -0.05
79 5.8921 0.00 0.09 0.00 -0.00
80 5.8921 0.00 0.06 0.00 -0.02
81 5.8921 0.00 0.05 0.00 0.16
82 5.8922 0.00 0.05 0.00 -0.05
83 5.9634 0.00 0.14 0.00 -0.24
84 6.7794 0.00 -0.11 0.00 0.70
85 6.7794 0.00 -0.26 0.00 -0.05
86 6.7794 0.00 0.21 0.00 -0.01
87 6.7795 0.00 -0.25 0.00 0.05
88 6.8094 0.00 -0.17 0.00 0.09
89 6.8094 0.00 -0.01 0.00 -0.19
90 6.8095 0.00 0.09 0.00 0.02
91 6.8095 0.00 -0.13 0.00 -0.12
92 6.8529 0.00 -0.48 0.00 0.05
93 6.8530 0.00 -0.11 0.00 0.02
94 6.8530 0.00 0.17 0.00 0.08
95 6.8530 0.00 0.03 0.00 0.15
96 6.8777 0.00 0.71 0.00 0.17
97 6.8778 0.00 -0.01 0.00 -0.11
98 6.8778 0.00 -0.04 0.00 0.10
99 6.8916 0.00 0.05 0.00 0.21
100 6.8916 0.00 -0.09 0.00 -0.00
101 6.8917 0.00 0.02 0.00 0.04
102 6.8917 0.00 -0.18 0.00 -0.02
103 6.9267 0.00 0.05 0.00 -0.02
104 6.9268 0.00 -0.03 0.00 -0.01
105 6.9268 0.00 0.16 0.00 0.48
106 6.9268 0.00 0.08 0.00 -0.04
107 6.9379 0.00 0.15 0.00 0.01
108 6.9379 0.00 -0.28 0.00 0.18
109 6.9379 0.00 -0.01 0.00 -0.14
110 6.9380 0.00 -0.68 0.00 -0.22
111 6.9569 0.00 -0.01 0.00 -0.08
112 6.9569 0.00 -0.05 0.00 -0.09
113 6.9569 0.00 -0.28 0.00 -0.09
114 6.9570 0.00 -0.01 0.00 -0.11
115 7.6285 0.00 -0.51 0.00 0.19
116 7.6285 0.00 -0.15 0.00 -0.01
117 7.6286 0.00 0.20 0.00 0.12
118 7.6286 0.00 0.23 0.00 -0.10
119 7.8252 0.00 0.03 0.00 0.07
120 7.8252 0.00 0.29 0.00 -0.00
121 7.8443 0.00 -0.17 0.00 -0.02
122 7.8443 0.00 -0.07 0.00 -0.15
123 7.8444 0.00 0.22 0.00 0.36
124 7.8444 0.00 1.01 0.00 0.53
125 7.8496 0.00 -0.09 0.00 -0.09
126 7.8497 0.00 -0.03 0.00 -0.07
127 7.8497 0.00 -0.05 0.00 0.05
128 7.8497 0.00 0.07 0.00 -0.02
129 7.9180 0.00 -0.10 0.00 -0.27
130 7.9180 0.00 -0.07 0.00 -0.05
131 7.9180 0.00 -0.39 0.00 0.04
132 10.8395 0.00 0.16 0.00 -0.13
133 10.8395 0.00 0.05 0.00 -0.16
134 10.8395 0.00 0.02 0.00 0.02
135 10.8396 0.00 -0.15 0.00 -0.09
136 11.8032 0.00 -0.16 0.00 -0.10
137 11.8033 0.00 -0.11 0.00 -0.11
138 11.8034 0.00 0.10 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.
548504 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 43.225 43.225 43.225 ecceobj 0.001 0.001 0.001 incobj 2.824 2.824 2.824 qmin 42.135 42.135 42.137 qmax 44.850 44.850 44.848 amean 43.413 43.413 43.413 amin 43.084 43.084 43.084 amax 43.747 43.747 43.746 emean 0.012 0.012 0.012 emin 0.000 0.000 0.000 emax 0.025 0.025 0.025 imean 1.348 1.348 1.347 imin 0.472 0.472 0.472 imax 2.016 2.016 2.016 excite_mean 0.027 0.027 0.027 fracstop 1.000 1.000 1.000 cjmean 3.094 3.094 3.094 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 175.9 175.9 176.1 kozaiamp 180.0 180.0 179.9