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: 577627 # Created Fri Apr 19 01:09:00 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 53 observations of 53 # Arc: 10.19y # First observation: 2011/04/30 # Last observation: 2021/07/09 # Chi-squared of fit: 55.37 DOF: 100 RMS: 0.18 # Min/Max residuals: -0.51 0.94 # Exact a, adot, b, bdot, g, gdot: 1.536671E-05 2.935489E-02 3.083423E-06 5.314804E-03 2.767961E-02 1.776040E-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 18.126133 -141.800922 -0.021376 0.314223 -0.960050 2455681.902786 # Heliocentric elements and errors Epoch: 2455682.5000 = 2011/05/01 Mean Anomaly: 29.13672 +/- 0.000 Argument of Peri: 24.70687 +/- 0.000 Long of Asc Node: 159.21741 +/- 0.000 Inclination: 20.35205 +/- 0.000 Eccentricity: 0.10764675 +/- 0.0000 Semi-Major Axis: 40.79180516 +/- 0.0000 Time of Perihelion: 2447980.6340 +/- 0.0 Perihelion: 36.40069992 +/- 0.0000 Aphelion: 45.18291041 +/- 0.0000 Period (y) 260.5359 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -27.75883455 +/- 0.0000 Ecliptic Y -21.87437859 +/- 0.0000 Ecliptic Z 11.23982221 +/- 0.0000 Ecliptic XDOT 0.00179095 +/- 0.0000 Ecliptic YDOT -0.00227798 +/- 0.0000 Ecliptic ZDOT 0.00055430 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 37.08601218 +/- 0.0000 Geocenter to KBO 36.12767879 +/- 0.0000 # Hcoef: 7.10
The following table shows the complete astrometric record for 577627. 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 (577627) followed by the observatory code and reference code for the source of the astrometry.
2011 04 30.40202 14 46 22.593 +02 57 40.65 23.1w 577627 F51 C~1w3u 2011 04 30.40268 14 46 22.578 +02 57 40.74 23.0w 577627 F51 C~1w3u 2011 04 30.41556 14 46 22.516 +02 57 41.27 23.2w 577627 F51 C~1w3u 2011 04 30.41622 14 46 22.504 +02 57 41.21 23.3w 577627 F51 C~1w3u 2011 04 30.43063 14 46 22.427 +02 57 41.66 23.1w 577627 F51 C~1w3u 2011 04 30.43131 14 46 22.430 +02 57 41.71 23.2w 577627 F51 C~1w3u 2011 04 30.44428 14 46 22.366 +02 57 41.90 23.3w 577627 F51 C~1w3u 2012 04 27.51748 14 53 18.563 +02 42 27.37 23.6G 577627 F51 C~2r7O 2012 05 18.36776 14 51 33.100 +02 50 36.45 22.8w 577627 F51 C~1w3u 2012 05 18.38135 14 51 33.046 +02 50 36.56 22.9w 577627 F51 C~1w3u 2012 05 18.39497 14 51 32.969 +02 50 37.16 22.9w 577627 F51 C~1w3u 2012 05 18.40931 14 51 32.894 +02 50 37.27 22.8w 577627 F51 C~1w3u 2013 04 17.50886 15 00 52.241 +02 22 47.25 22.2w 577627 F51 C~1w3u 2013 04 17.53916 15 00 52.066 +02 22 48.15 22.3w 577627 F51 C~1w3u 2013 04 17.55432 15 00 52.016 +02 22 49.03 22.3w 577627 F51 C~1w3u 2013 05 10.39243 14 58 58.117 +02 33 34.74 22.8w 577627 F51 C~1w3u 2013 05 10.40727 14 58 58.049 +02 33 34.98 22.6w 577627 F51 C~1w3u 2013 05 10.42214 14 58 57.976 +02 33 35.53 22.3w 577627 F51 C~1w3u 2013 05 10.43701 14 58 57.886 +02 33 35.91 22.3w 577627 F51 C~1w3u 2013 07 14.28011 14 54 55.653 +02 34 53.66 23.3G 577627 F51 C~2r7O 2014 04 08.50520 15 08 14.984 +02 03 01.43 22.3w 577627 F51 C~1w3u 2014 04 08.53065 15 08 14.858 +02 03 01.81 21.8G 577627 F51 C~2r7O 2014 05 04.39550 15 06 12.257 +02 16 38.32 23.2G 577627 F51 C~2r7O 2014 05 04.40750 15 06 12.192 +02 16 39.00 22.7G 577627 F51 C~2r7O 2014 05 04.41950 15 06 12.141 +02 16 39.19 23.7G 577627 F51 C~2r7O 2014 05 04.43156 15 06 12.071 +02 16 39.44 22.7G 577627 F51 C~2r7O 2014 05 08.39051 15 05 51.887 +02 18 18.07 22.8G 577627 F51 C~2r7O 2014 05 28.36314 15 04 12.002 +02 24 15.11 22.6G 577627 F51 C~2r7O 2014 07 01.39809 15 01 59.818 +02 24 15.13 22.4G 577627 F51 C~2r7O 2015 02 18.59626 15 16 37.645 +01 18 29.06 23.2G 577627 F51 C~2r7O 2015 04 04.47932 15 15 11.514 +01 45 58.53 22.3G 577627 F51 C~2r7O 2015 04 12.41248 15 14 39.165 +01 50 42.99 22.8G 577627 F51 C~2r7O 2015 04 13.58175 15 14 34.070 +01 51 23.51 23.3G 577627 F51 C~2r7O 2015 05 13.41969 15 12 08.594 +02 05 36.36 21.6G 577627 F51 C~2r7O 2015 06 05.39890 15 10 15.955 +02 10 59.92 23.1G 577627 F51 C~2r7O 2015 07 09.29524 15 08 17.404 +02 08 14.55 22.8G 577627 F51 C~2r7O 2015 07 09.30786 15 08 17.389 +02 08 14.32 23.1G 577627 F51 C~2r7O 2015 07 09.32045 15 08 17.356 +02 08 13.94 23.0G 577627 F51 C~2r7O 2015 07 09.33304 15 08 17.324 +02 08 13.84 23.0G 577627 F51 C~2r7O 2015 07 12.29664 15 08 11.154 +02 07 23.51 22.6G 577627 F51 C~2r7O 2015 07 12.32183 15 08 11.101 +02 07 23.04 21.9G 577627 F51 C~2r7O 2015 07 12.33443 15 08 11.075 +02 07 22.77 23.0G 577627 F51 C~2r7O 2016 02 24.59391 15 23 09.581 +01 07 27.95 23.1G 577627 F51 C~2r7O 2016 04 10.55839 15 21 22.188 +01 35 34.52 21.8G 577627 F51 C~2r7O 2016 04 17.53690 15 20 51.823 +01 39 32.42 23.1G 577627 F51 C~2r7O 2016 06 04.40760 15 16 55.901 +01 56 30.25 22.8G 577627 F51 C~2r7O 2016 07 01.33854 15 15 11.501 +01 55 34.44 23.3G 577627 F51 C~2r7O 2018 05 20.173280 15 31 27.72 +01 24 15.6 22.6G 577627 705 C~2rA8 2018 05 20.218900 15 31 27.48 +01 24 16.6 22.4G 577627 705 C~2rA8 2018 05 20.255070 15 31 27.30 +01 24 17.2 22.6G 577627 705 C~2rA8 2021 07 09.211340 15 47 24.777 +00 42 43.60 22.9G 577627 G37 C~4uuH 2021 07 09.245890 15 47 24.677 +00 42 43.52 577627 G37 C~4uuH 2021 07 09.278790 15 47 24.573 +00 42 42.98 577627 G37 C~4uuH
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 0.27 0.00 -0.10
2 0.0000 0.00 0.10 0.00 -0.03
3 0.0000 0.00 0.17 0.00 0.14
4 0.0000 0.00 0.04 0.00 0.06
5 0.0001 0.00 0.00 0.00 0.11
6 0.0001 0.00 0.10 0.00 0.14
7 0.0001 0.00 0.15 0.00 -0.03
8 0.9942 0.00 -0.19 0.00 -0.06
9 1.0512 0.00 -0.18 0.00 0.01
10 1.0513 0.00 0.04 0.00 -0.11
11 1.0513 0.00 -0.08 0.00 0.25
12 1.0514 0.00 -0.12 0.00 0.11
13 1.9661 0.00 -0.07 0.00 0.02
14 1.9662 0.00 -0.51 0.00 -0.09
15 1.9662 0.00 -0.16 0.00 0.28
16 2.0287 0.00 0.01 0.00 -0.16
17 2.0288 0.00 0.15 0.00 -0.25
18 2.0288 0.00 0.21 0.00 -0.03
19 2.0288 0.00 0.02 0.00 0.01
20 2.2064 0.00 -0.21 0.00 0.07
21 2.9407 0.00 0.07 0.00 0.14
22 2.9408 0.00 -0.18 0.00 -0.39
23 3.0116 0.00 0.02 0.00 -0.42
24 3.0117 0.00 -0.02 0.00 -0.06
25 3.0117 0.00 0.14 0.00 -0.18
26 3.0117 0.00 0.03 0.00 -0.24
27 3.0226 0.00 -0.24 0.00 -0.04
28 3.0772 0.00 -0.20 0.00 -0.07
29 3.1704 0.00 -0.01 0.00 0.13
30 3.8061 0.00 -0.21 0.00 -0.12
31 3.9290 0.00 0.26 0.00 0.08
32 3.9507 0.00 0.19 0.00 -0.10
33 3.9539 0.00 0.13 0.00 -0.19
34 4.0356 0.00 0.37 0.00 0.14
35 4.0986 0.00 -0.27 0.00 -0.07
36 4.1914 0.00 -0.06 0.00 0.09
37 4.1914 0.00 0.15 0.00 0.07
38 4.1914 0.00 0.09 0.00 -0.11
39 4.1915 0.00 0.05 0.00 -0.01
40 4.1996 0.00 -0.04 0.00 0.05
41 4.1996 0.00 -0.06 0.00 0.03
42 4.1997 0.00 -0.07 0.00 -0.01
43 4.8219 0.00 -0.18 0.00 -0.12
44 4.9477 0.00 0.08 0.00 0.20
45 4.9668 0.00 -0.09 0.00 0.94
46 5.0979 0.00 0.17 0.00 0.04
47 5.1716 0.00 0.16 0.00 0.22
48 7.0548 0.00 0.08 0.00 -0.22
49 7.0549 0.00 0.02 0.00 -0.02
50 7.0550 0.00 0.13 0.00 -0.04
51 10.1925 0.00 -0.12 0.00 -0.25
52 10.1926 0.00 -0.02 0.00 0.16
53 10.1927 0.00 -0.05 0.00 0.08
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.
577627 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 40.689 40.689 40.689 ecceobj 0.106 0.106 0.106 incobj 20.363 20.363 20.363 qmin 35.550 35.678 35.483 qmax 46.687 46.590 46.734 amean 40.979 40.983 40.993 amin 40.643 40.660 40.660 amax 41.335 41.341 41.354 emean 0.113 0.111 0.114 emin 0.098 0.096 0.098 emax 0.130 0.128 0.131 imean 19.712 19.760 19.714 imin 18.990 18.990 18.966 imax 20.512 20.533 20.513 excite_mean 0.356 0.356 0.356 fracstop 1.000 1.000 1.000 cjmean 2.917 2.917 2.917 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 175.0 175.7 174.7 kozaiamp 179.9 179.9 180.0