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: 16EF391 # Created Mon Jul 7 01:11:04 2025 # Orbit generated from Bernstein formalism # Fitting 128 observations of 128 # Arc: 3.00y # First observation: 2015/01/16 # Last observation: 2018/01/17 Preliminary a, adot, b, bdot, g, gdot: -0.000006 0.017009 -0.000004 -0.004189 0.021510 0.000000 # Chi-squared of fit: 56.44 DOF: 250 RMS: 0.12 # Min/Max residuals: -0.45 0.33 # Exact a, adot, b, bdot, g, gdot: 1.260009E-05 1.704516E-02 -2.247334E-06 -4.196649E-03 2.154418E-02 1.732139E-03 # Covariance matrix: 2.5150E-14 2.4912E-15 6.6318E-16 -2.1999E-15 3.0851E-14 2.1396E-13 2.4912E-15 1.1167E-13 4.8866E-15 -2.4287E-14 1.1248E-13 2.2995E-12 6.6318E-16 4.8866E-15 1.7786E-14 -1.0532E-14 5.8407E-15 1.1466E-13 -2.1999E-15 -2.4287E-14 -1.0532E-14 2.0442E-14 -2.5976E-14 -5.8138E-13 3.0851E-14 1.1248E-13 5.8407E-15 -2.5976E-14 1.7785E-13 2.4752E-12 2.1396E-13 2.2995E-12 1.1466E-13 -5.8138E-13 2.4752E-12 5.4986E-11 # lat0 lon0 xBary yBary zBary JD0 -9.038675 151.950368 0.580260 -0.124261 -0.782175 2457039.036108 # Heliocentric elements and errors Epoch: 2457030.5000 = 2015/01/08 Mean Anomaly: 151.66591 +/- 0.086 Argument of Peri: 52.10350 +/- 0.086 Long of Asc Node: 299.25528 +/- 0.001 Inclination: 16.44605 +/- 0.000 Eccentricity: 0.21135500 +/- 0.0001 Semi-Major Axis: 39.53981423 +/- 0.0019 Time of Perihelion: 2418771.3040 +/- 21.5 Perihelion: 31.18287686 +/- 0.0047 Aphelion: 47.89675160 +/- 0.0050 Period (y) 248.6338 +/- 0.02 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X -40.88482047 +/- 0.0008 Ecliptic Y 22.44034669 +/- 0.0004 Ecliptic Z -7.29217352 +/- 0.0001 Ecliptic XDOT -0.00114037 +/- 0.0000 Ecliptic YDOT -0.00185420 +/- 0.0000 Ecliptic ZDOT -0.00056118 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 47.20501561 +/- 0.0007 Geocenter to KBO 46.41625838 +/- 0.0009 # Hcoef: 7.92
The following table shows the complete astrometric record for 16EF391. 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 (16EF391) followed by the observatory code and reference code for the source of the astrometry.
2015 01 16.53533 10 02 54.50 +02 19 34.4 23.9z 16EF391 T09 C~8uZJ 2015 01 16.53924 10 02 54.50 +02 19 34.4 24.2z 16EF391 T09 C~8uZJ 2015 01 16.54315 10 02 54.48 +02 19 34.4 24.2z 16EF391 T09 C~8uZJ 2015 01 16.54710 10 02 54.46 +02 19 34.6 24.2z 16EF391 T09 C~8uZJ 2015 01 16.56037 10 02 54.41 +02 19 34.8 24.4z 16EF391 T09 C~8uZJ 2015 01 16.56849 10 02 54.39 +02 19 34.8 24.1z 16EF391 T09 C~8uZJ 2015 01 16.57237 10 02 54.37 +02 19 34.8 24.3z 16EF391 T09 C~8uZJ 2015 01 16.57632 10 02 54.35 +02 19 34.8 24.2z 16EF391 T09 C~8uZJ 2015 01 16.58024 10 02 54.35 +02 19 34.8 24.2z 16EF391 T09 C~8uZJ 2015 01 16.58807 10 02 54.32 +02 19 34.9 24.6z 16EF391 T09 C~8uZJ 2015 01 16.59524 10 02 54.28 +02 19 35.1 24.4z 16EF391 T09 C~8uZJ 2015 01 16.60268 10 02 54.26 +02 19 35.1 24.1z 16EF391 T09 C~8uZJ 2015 01 16.62232 10 02 54.19 +02 19 35.4 24.5z 16EF391 T09 C~8uZJ 2015 01 16.65500 10 02 54.08 +02 19 35.8 24.6z 16EF391 T09 C~8uZJ 2015 01 16.66214 10 02 54.05 +02 19 35.8 24.5z 16EF391 T09 C~8uZJ 2015 01 17.40063 10 02 51.43 +02 19 43.2 24.6i 16EF391 T09 C~8uZJ 2015 01 17.40524 10 02 51.40 +02 19 43.2 24.6i 16EF391 T09 C~8uZJ 2015 01 17.40983 10 02 51.41 +02 19 43.2 24.5i 16EF391 T09 C~8uZJ 2015 01 17.41902 10 02 51.36 +02 19 43.2 24.4i 16EF391 T09 C~8uZJ 2015 01 17.42357 10 02 51.36 +02 19 43.2 24.4i 16EF391 T09 C~8uZJ 2015 01 17.42812 10 02 51.34 +02 19 43.3 24.9i 16EF391 T09 C~8uZJ 2015 01 17.43268 10 02 51.32 +02 19 43.5 24.6i 16EF391 T09 C~8uZJ 2015 01 17.44180 10 02 51.30 +02 19 43.5 24.5i 16EF391 T09 C~8uZJ 2015 01 18.42960 10 02 47.73 +02 19 53.6 23.9y 16EF391 T09 C~8uZJ 2015 01 18.43466 10 02 47.72 +02 19 53.8 24.1y 16EF391 T09 C~8uZJ 2015 01 18.43924 10 02 47.71 +02 19 53.6 24.2y 16EF391 T09 C~8uZJ 2015 01 18.45296 10 02 47.64 +02 19 53.8 24.2y 16EF391 T09 C~8uZJ 2015 01 18.45938 10 02 47.62 +02 19 53.9 23.9y 16EF391 T09 C~8uZJ 2015 01 18.53842 10 02 47.33 +02 19 54.6 24.0y 16EF391 T09 C~8uZJ 2015 01 19.42888 10 02 44.08 +02 20 04.4 24.4z 16EF391 T09 C~8uZJ 2015 01 19.43347 10 02 44.08 +02 20 04.4 24.2z 16EF391 T09 C~8uZJ 2015 01 19.43808 10 02 44.06 +02 20 04.5 24.4z 16EF391 T09 C~8uZJ 2015 01 19.44263 10 02 44.03 +02 20 04.4 24.2z 16EF391 T09 C~8uZJ 2015 01 19.44721 10 02 44.03 +02 20 04.5 23.9z 16EF391 T09 C~8uZJ 2015 01 19.45179 10 02 44.01 +02 20 04.4 24.3z 16EF391 T09 C~8uZJ 2015 01 19.45634 10 02 43.99 +02 20 04.7 24.3z 16EF391 T09 C~8uZJ 2015 01 20.45227 10 02 40.31 +02 20 15.5 26.0g 16EF391 T09 C~8uZJ 2015 01 20.45704 10 02 40.29 +02 20 15.8 26.1g 16EF391 T09 C~8uZJ 2015 01 20.46183 10 02 40.29 +02 20 15.8 26.4g 16EF391 T09 C~8uZJ 2015 01 21.55881 10 02 36.18 +02 20 28.6 24.3i 16EF391 T09 C~8uZJ 2015 01 21.56266 10 02 36.16 +02 20 28.6 24.2i 16EF391 T09 C~8uZJ 2015 01 21.56653 10 02 36.13 +02 20 28.6 24.2i 16EF391 T09 C~8uZJ 2015 01 21.57101 10 02 36.12 +02 20 28.6 24.8i 16EF391 T09 C~8uZJ 2015 01 21.57962 10 02 36.10 +02 20 28.6 24.1i 16EF391 T09 C~8uZJ 2015 01 21.58764 10 02 36.07 +02 20 28.9 24.3i 16EF391 T09 C~8uZJ 2015 01 21.59154 10 02 36.05 +02 20 28.9 24.3i 16EF391 T09 C~8uZJ 2015 01 21.59540 10 02 36.03 +02 20 28.9 24.3i 16EF391 T09 C~8uZJ 2015 01 21.59912 10 02 36.03 +02 20 28.9 24.2i 16EF391 T09 C~8uZJ 2015 01 21.60626 10 02 35.99 +02 20 28.9 24.3i 16EF391 T09 C~8uZJ 2015 01 21.61742 10 02 35.94 +02 20 29.3 24.3i 16EF391 T09 C~8uZJ 2015 01 21.62126 10 02 35.94 +02 20 29.3 24.3i 16EF391 T09 C~8uZJ 2015 01 21.63940 10 02 35.85 +02 20 29.4 24.9i 16EF391 T09 C~8uZJ 2015 01 21.65094 10 02 35.82 +02 20 29.6 24.4i 16EF391 T09 C~8uZJ 2015 01 27.54714 10 02 12.99 +02 21 46.6 24.0y 16EF391 T09 C~8uaE 2015 01 27.55100 10 02 12.97 +02 21 46.6 24.3y 16EF391 T09 C~8uaE 2015 01 27.55498 10 02 12.97 +02 21 46.6 24.0y 16EF391 T09 C~8uaE 2015 01 27.55889 10 02 12.97 +02 21 46.6 24.1y 16EF391 T09 C~8uaE 2015 01 27.56344 10 02 12.94 +02 21 46.6 24.0y 16EF391 T09 C~8uaE 2015 01 27.58016 10 02 12.88 +02 21 47.0 23.9y 16EF391 T09 C~8uaE 2015 01 27.58412 10 02 12.85 +02 21 47.0 24.0y 16EF391 T09 C~8uaE 2015 01 27.58809 10 02 12.84 +02 21 47.0 23.8y 16EF391 T09 C~8uaE 2015 01 27.59204 10 02 12.82 +02 21 47.0 24.0y 16EF391 T09 C~8uaE 2015 01 27.61047 10 02 12.74 +02 21 47.3 24.6y 16EF391 T09 C~8uaE 2015 01 27.61446 10 02 12.72 +02 21 47.3 24.0y 16EF391 T09 C~8uaE 2015 01 27.61834 10 02 12.72 +02 21 47.3 24.3y 16EF391 T09 C~8uaE 2015 03 18.39076 09 58 46.66 +02 38 54.0 25.4r 16EF391 T09 C~8uZJ 2015 03 18.40838 09 58 46.59 +02 38 54.6 25.2r 16EF391 T09 C~8uZJ 2015 03 18.41164 09 58 46.57 +02 38 54.6 25.1r 16EF391 T09 C~8uZJ 2015 03 18.42254 09 58 46.52 +02 38 54.8 25.3r 16EF391 T09 C~8uZJ 2015 03 18.42649 09 58 46.52 +02 38 55.0 25.1r 16EF391 T09 C~8uZJ 2015 03 18.42974 09 58 46.51 +02 38 55.0 25.3r 16EF391 T09 C~8uZJ 2015 03 18.44066 09 58 46.47 +02 38 55.3 24.7r 16EF391 T09 C~8uZJ 2015 03 18.44463 09 58 46.45 +02 38 55.3 24.9r 16EF391 T09 C~8uZJ 2015 03 18.44789 09 58 46.43 +02 38 55.3 24.8r 16EF391 T09 C~8uZJ 2015 03 20.33757 09 58 39.57 +02 39 39.6 24.7i 16EF391 T09 C~8uZJ 2015 03 20.35412 09 58 39.51 +02 39 40.1 24.9i 16EF391 T09 C~8uZJ 2015 03 20.36873 09 58 39.46 +02 39 40.3 24.6i 16EF391 T09 C~8uZJ 2015 03 20.38334 09 58 39.41 +02 39 40.8 25.0i 16EF391 T09 C~8uZJ 2016 03 04.43361 10 02 59.13 +01 59 30.2 24.2i 16EF391 T09 C~8HEi 2016 03 04.46258 10 02 59.00 +01 59 30.9 24.0i 16EF391 T09 C~8HEi 2016 03 04.46608 10 02 58.98 +01 59 31.1 24.0i 16EF391 T09 C~8HEi 2016 03 07.28619 10 02 47.45 +02 00 37.1 25.8g 16EF391 T09 C~8HEi 2016 03 07.30636 10 02 47.37 +02 00 37.5 25.4g 16EF391 T09 C~8HEi 2016 03 07.30953 10 02 47.36 +02 00 37.5 25.9g 16EF391 T09 C~8HEi 2016 03 07.31343 10 02 47.34 +02 00 37.6 26.0g 16EF391 T09 C~8HEi 2016 03 07.31730 10 02 47.33 +02 00 37.8 26.1g 16EF391 T09 C~8HEi 2016 03 07.32114 10 02 47.32 +02 00 38.0 25.9g 16EF391 T09 C~8HEi 2016 03 07.32886 10 02 47.30 +02 00 38.0 25.7g 16EF391 T09 C~8HEi 2016 03 09.29704 10 02 39.36 +02 01 24.7 24.8r 16EF391 T09 C~8HEi 2016 03 09.30726 10 02 39.32 +02 01 24.9 25.0r 16EF391 T09 C~8HEi 2016 03 09.31742 10 02 39.27 +02 01 24.9 24.5r 16EF391 T09 C~8HEi 2016 03 09.32069 10 02 39.26 +02 01 25.2 25.2r 16EF391 T09 C~8HEi 2016 03 09.32455 10 02 39.25 +02 01 25.4 25.5r 16EF391 T09 C~8HEi 2016 03 09.32844 10 02 39.22 +02 01 25.4 25.8r 16EF391 T09 C~8HEi 2016 03 09.33236 10 02 39.22 +02 01 25.4 25.2r 16EF391 T09 C~8HEi 2016 03 09.33622 10 02 39.19 +02 01 25.6 25.5r 16EF391 T09 C~8HEi 2016 03 09.34016 10 02 39.17 +02 01 25.7 25.2r 16EF391 T09 C~8HEi 2016 03 12.40209 10 02 27.09 +02 02 37.8 23.7z 16EF391 T09 C~8HEi 2016 03 12.43157 10 02 26.96 +02 02 39.0 23.8z 16EF391 T09 C~8HEi 2016 03 12.43532 10 02 26.96 +02 02 39.0 24.3z 16EF391 T09 C~8HEi 2016 03 12.43918 10 02 26.92 +02 02 39.2 24.0z 16EF391 T09 C~8HEi 2016 03 12.44304 10 02 26.92 +02 02 39.2 24.2z 16EF391 T09 C~8HEi 2016 03 12.44690 10 02 26.91 +02 02 39.3 24.3z 16EF391 T09 C~8HEi 2016 03 12.45077 10 02 26.89 +02 02 39.3 23.9z 16EF391 T09 C~8HEi 2016 03 12.45461 10 02 26.87 +02 02 39.5 24.2z 16EF391 T09 C~8HEi 2016 03 12.45847 10 02 26.86 +02 02 39.5 24.0z 16EF391 T09 C~8HEi 2016 03 12.47004 10 02 26.80 +02 02 40.0 23.9z 16EF391 T09 C~8HEi 2016 03 12.47390 10 02 26.80 +02 02 40.0 24.6z 16EF391 T09 C~8HEi 2016 03 15.49118 10 02 15.17 +02 03 51.5 23.3y 16EF391 T09 C~8HEi 2016 03 15.49503 10 02 15.19 +02 03 52.0 24.0y 16EF391 T09 C~8HEi 2016 03 15.49888 10 02 15.17 +02 03 52.1 24.4y 16EF391 T09 C~8HEi 2016 03 15.50274 10 02 15.15 +02 03 52.0 24.0y 16EF391 T09 C~8HEi 2017 02 02.50623 10 08 26.61 +01 15 03.8 24.5r 16EF391 T09 C~8uaE 2017 02 02.51587 10 08 26.59 +01 15 03.9 24.6r 16EF391 T09 C~8uaE 2017 02 02.52702 10 08 26.53 +01 15 04.3 24.7r 16EF391 T09 C~8uaE 2017 03 22.39453 10 05 10.51 +01 32 23.2 24.6z 16EF391 T09 C~8uaE 2017 03 22.42021 10 05 10.42 +01 32 24.0 24.1z 16EF391 T09 C~8uaE 2017 03 22.47157 10 05 10.24 +01 32 25.0 24.2z 16EF391 T09 C~8uaE 2017 03 22.49332 10 05 10.14 +01 32 25.7 24.5z 16EF391 T09 C~8uaE 2018 01 17.46460 10 12 46.82 +00 37 37.0 24.6i 16EF391 T09 C~8uaE 2018 01 17.48599 10 12 46.75 +00 37 37.3 23.9i 16EF391 T09 C~8uaE 2018 01 17.51296 10 12 46.66 +00 37 37.7 24.2i 16EF391 T09 C~8uaE 2018 01 17.51563 10 12 46.64 +00 37 37.7 24.0i 16EF391 T09 C~8uaE 2018 01 17.54265 10 12 46.54 +00 37 37.8 23.9i 16EF391 T09 C~8uaE 2018 01 17.54803 10 12 46.52 +00 37 38.0 24.1i 16EF391 T09 C~8uaE 2018 01 17.57490 10 12 46.43 +00 37 38.2 24.3i 16EF391 T09 C~8uaF 2018 01 17.59901 10 12 46.34 +00 37 38.4 24.0i 16EF391 T09 C~8uaF 2018 01 17.61241 10 12 46.31 +00 37 38.4 24.5i 16EF391 T09 C~8uaF
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 -0.17
2 0.0000 0.00 0.19 0.00 -0.13
3 0.0000 -0.28 0.12 -0.11 -0.20
4 0.0000 -0.63 -0.01 -0.02 -0.08
5 0.0001 -1.40 -0.07 -0.10 -0.02
6 0.0001 -1.68 0.09 -0.20 -0.05
7 0.0001 -1.96 0.02 -0.31 -0.11
8 0.0001 -2.25 -0.05 -0.42 -0.18
9 0.0001 -2.25 0.16 -0.42 -0.14
10 0.0001 -2.70 0.13 -0.48 -0.12
11 0.0002 -3.33 -0.12 -0.50 -0.08
12 0.0002 -3.61 0.00 -0.61 -0.11
13 0.0002 -4.70 -0.02 -0.70 0.00
14 0.0003 -6.39 0.05 -0.90 0.12
15 0.0003 -6.81 0.02 -1.06 0.03
16 0.0024 -46.17 -0.18 -7.93 0.10
17 0.0024 -46.59 -0.35 -8.08 -0.01
18 0.0024 -46.45 0.04 -8.03 0.08
19 0.0024 -47.15 -0.16 -8.30 -0.09
20 0.0024 -47.15 0.09 -8.30 -0.04
21 0.0024 -47.47 0.02 -8.31 -0.01
22 0.0025 -47.82 -0.08 -8.23 0.11
23 0.0025 -48.10 0.14 -8.33 0.10
24 0.0052 -101.74 -0.07 -17.67 0.00
25 0.0052 -101.95 0.00 -17.54 0.18
26 0.0052 -102.02 0.19 -17.78 -0.01
27 0.0053 -103.08 -0.11 -17.96 -0.06
28 0.0053 -103.39 -0.06 -17.97 -0.01
29 0.0055 -107.71 0.01 -18.84 -0.12
30 0.0079 -156.76 -0.22 -26.78 0.08
31 0.0079 -156.76 0.03 -26.78 0.12
32 0.0079 -157.07 -0.02 -26.79 0.15
33 0.0080 -157.46 -0.15 -27.04 -0.05
34 0.0080 -157.49 0.07 -26.95 0.08
35 0.0080 -157.74 0.08 -27.15 -0.07
36 0.0080 -158.12 -0.05 -26.97 0.15
37 0.0107 -213.56 -0.03 -36.24 -0.14
38 0.0107 -213.94 -0.14 -36.06 0.08
39 0.0108 -213.94 0.13 -36.06 0.12
40 0.0138 -276.11 0.02 -45.72 0.18
41 0.0138 -276.39 -0.04 -45.82 0.11
42 0.0138 -276.81 -0.24 -45.98 -0.01
43 0.0138 -276.95 -0.12 -46.03 -0.02
44 0.0138 -277.23 0.10 -46.14 -0.05
45 0.0138 -277.76 0.04 -46.02 0.15
46 0.0138 -278.04 -0.02 -46.12 0.08
47 0.0139 -278.32 -0.08 -46.23 0.01
48 0.0139 -278.32 0.14 -46.23 0.04
49 0.0139 -278.88 -0.01 -46.44 -0.10
50 0.0139 -279.73 -0.21 -46.33 0.11
51 0.0139 -279.73 0.01 -46.33 0.14
52 0.0140 -281.02 -0.24 -46.71 -0.07
53 0.0140 -281.51 -0.06 -46.68 0.06
54 0.0301 -628.92 -0.13 -94.77 0.06
55 0.0302 -629.20 -0.17 -94.88 -0.01
56 0.0302 -629.20 0.08 -94.88 0.02
57 0.0302 -629.20 0.32 -94.88 0.05
58 0.0302 -629.62 0.18 -95.03 -0.07
59 0.0302 -630.61 0.23 -94.98 0.12
60 0.0302 -631.03 0.05 -95.13 -0.00
61 0.0303 -631.17 0.15 -95.19 -0.03
62 0.0303 -631.45 0.12 -95.29 -0.10
63 0.0303 -632.68 0.03 -95.43 -0.09
64 0.0303 -632.96 -0.01 -95.54 -0.17
65 0.0303 -632.96 0.23 -95.54 -0.14
66 0.1666 -3885.27 0.15 -217.79 0.02
67 0.1667 -3886.46 0.03 -217.60 0.18
68 0.1667 -3886.74 -0.05 -217.70 0.06
69 0.1667 -3887.51 -0.16 -217.78 -0.04
70 0.1667 -3887.58 0.01 -217.59 0.14
71 0.1667 -3887.73 0.06 -217.64 0.08
72 0.1667 -3888.39 0.06 -217.57 0.13
73 0.1668 -3888.67 0.02 -217.68 0.01
74 0.1668 -3888.95 -0.06 -217.78 -0.10
75 0.1719 -4000.79 -0.09 -212.33 -0.05
76 0.1720 -4001.81 -0.12 -212.18 0.06
77 0.1720 -4002.58 -0.02 -212.26 -0.05
78 0.1721 -4003.46 -0.03 -212.05 0.12
79 1.1305 488.08 0.08 -1103.05 -0.04
80 1.1305 486.01 -0.05 -1103.08 -0.06
81 1.1305 485.66 -0.17 -1103.00 0.02
82 1.1383 300.64 -0.11 -1101.94 -0.04
83 1.1383 299.38 -0.04 -1101.98 -0.09
84 1.1383 299.23 0.03 -1102.03 -0.15
85 1.1383 298.92 -0.02 -1102.05 -0.16
86 1.1383 298.71 0.02 -1101.91 -0.03
87 1.1384 298.50 0.06 -1101.78 0.11
88 1.1384 298.22 0.29 -1101.88 -0.00
89 1.1438 170.37 0.04 -1099.97 0.14
90 1.1438 169.74 0.08 -1100.00 0.11
91 1.1438 169.04 0.04 -1100.26 -0.16
92 1.1438 168.79 0.01 -1100.03 0.07
93 1.1438 168.58 0.05 -1099.90 0.20
94 1.1439 168.16 -0.12 -1100.06 0.04
95 1.1439 168.16 0.14 -1100.06 0.03
96 1.1439 167.67 -0.10 -1100.03 0.06
97 1.1439 167.35 -0.16 -1100.04 0.05
98 1.1523 -27.52 0.33 -1096.15 -0.39
99 1.1524 -29.77 -0.03 -1095.71 0.01
100 1.1524 -29.77 0.21 -1095.71 0.00
101 1.1524 -30.40 -0.17 -1095.73 -0.03
102 1.1524 -30.40 0.08 -1095.73 -0.03
103 1.1524 -30.58 0.15 -1095.69 0.00
104 1.1524 -30.86 0.11 -1095.80 -0.11
105 1.1524 -31.21 0.01 -1095.71 -0.03
106 1.1524 -31.35 0.12 -1095.77 -0.09
107 1.1525 -32.37 -0.16 -1095.61 0.05
108 1.1525 -32.37 0.09 -1095.61 0.04
109 1.1607 -220.71 -0.31 -1089.91 -0.45
110 1.1607 -220.61 0.03 -1089.33 0.12
111 1.1607 -220.92 -0.05 -1089.35 0.10
112 1.1608 -221.17 -0.05 -1089.55 -0.11
113 2.0478 6024.28 -0.18 -1872.53 -0.00
114 2.0479 6023.96 0.13 -1872.54 0.05
115 2.0479 6022.98 -0.14 -1872.48 0.19
116 2.1789 2904.33 -0.01 -1933.99 0.03
117 2.1790 2902.78 -0.04 -1933.71 0.22
118 2.1792 2899.90 0.11 -1933.73 0.03
119 2.1792 2898.25 -0.27 -1933.60 0.08
120 3.0032 10475.88 0.07 -2602.37 -0.18
121 3.0033 10474.79 0.10 -2602.46 -0.05
122 3.0034 10473.38 0.11 -2602.56 0.13
123 3.0034 10473.10 -0.03 -2602.67 0.05
124 3.0034 10471.65 -0.05 -2603.10 -0.10
125 3.0035 10471.30 -0.12 -2603.02 0.03
126 3.0035 10469.96 -0.04 -2603.31 0.02
127 3.0036 10468.63 -0.11 -2603.60 -0.02
128 3.0036 10468.20 0.18 -2603.76 -0.04
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.
16EF391 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.373 39.378 39.367 ecceobj 0.218 0.219 0.218 incobj 16.476 16.477 16.476 qmin 27.488 27.480 27.530 qmax 51.979 51.901 51.877 amean 39.455 39.455 39.454 amin 39.016 39.030 39.018 amax 39.940 39.969 39.950 emean 0.252 0.252 0.252 emin 0.183 0.183 0.184 emax 0.302 0.301 0.301 imean 16.419 16.418 16.416 imin 13.800 13.801 13.786 imax 19.224 19.219 19.222 excite_mean 0.381 0.381 0.381 fracstop 1.000 1.000 1.000 cjmean 2.886 2.886 2.886 libcent 0 180.6 180.5 180.7 libamp 0 72.4 72.3 72.5 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 85.3 85.2 85.2 kozaiamp 53.1 52.1 53.4