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: 15RE280
# Created Sun Nov 24 02:10:25 2024
# Orbit generated from Bernstein formalism
# Fitting 30 observations of 30
# Arc: 2.50y
# First observation: 2015/06/23
# Last observation: 2017/12/23
Preliminary a, adot, b, bdot, g, gdot:
-0.000063 0.020155 0.000000 0.000342 0.022050 0.000000
# Chi-squared of fit: 6.65 DOF: 54 RMS: 0.08
# Min/Max residuals: -0.18 0.33
# Exact a, adot, b, bdot, g, gdot:
1.481625E-05 1.972777E-02 5.804515E-08 3.373602E-04 2.169460E-02 8.832841E-04
# Covariance matrix:
1.8533E-13 3.9635E-14 -9.6132E-16 2.2797E-15 1.6269E-13 2.7762E-12
3.9635E-14 3.5506E-13 -2.7671E-15 8.5344E-15 2.9235E-13 1.0348E-11
-9.6132E-16 -2.7671E-15 9.6318E-14 -6.2342E-14 -2.8673E-15 -1.0500E-13
2.2797E-15 8.5344E-15 -6.2342E-14 7.9398E-14 8.1141E-15 3.3777E-13
1.6269E-13 2.9235E-13 -2.8673E-15 8.1141E-15 3.6802E-13 9.8515E-12
2.7762E-12 1.0348E-11 -1.0500E-13 3.3777E-13 9.8515E-12 4.0933E-10
# lat0 lon0 xBary yBary zBary JD0
0.167457 11.166769 1.002823 -0.000385 0.165123 2457197.114678
# Heliocentric elements and errors
Epoch: 2457190.5000 = 2015/06/17
Mean Anomaly: 150.45043 +/- 1.121
Argument of Peri: 216.75009 +/- 1.120
Long of Asc Node: 0.24909 +/- 0.009
Inclination: 1.00084 +/- 0.001
Eccentricity: 0.04549007 +/- 0.0004
Semi-Major Axis: 44.16767309 +/- 0.0033
Time of Perihelion: 2412383.4712 +/- 333.7
Perihelion: 42.15848240 +/- 0.0190
Aphelion: 46.17686378 +/- 0.0191
Period (y) 293.5384 +/- 0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 45.25023216 +/- 0.0013
Ecliptic Y 7.91155852 +/- 0.0002
Ecliptic Z 0.13477499 +/- 0.0000
Ecliptic XDOT -0.00037538 +/- 0.0000
Ecliptic YDOT 0.00245783 +/- 0.0000
Ecliptic ZDOT 0.00004297 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 45.93685267 +/- 0.0012
Geocenter to KBO 46.09442928 +/- 0.0013
# Hcoef: 7.83
The following table shows the complete astrometric record for 15RE280. 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 (15RE280) followed by the observatory code and reference code for the source of the astrometry.
2015 06 23.61390 00 40 48.000 +04 34 20.24 25.0r 15RE280 568 C~2nvp 2015 07 14.57141 00 41 01.516 +04 35 55.60 24.4r 15RE280 568 C~2nvp 2015 07 19.54942 00 40 59.655 +04 35 45.89 24.8r 15RE280 568 C~2nvp 2015 08 11.50339 00 40 27.078 +04 32 28.68 24.3r 15RE280 568 C~2nvp 2015 08 11.54506 00 40 26.976 +04 32 28.13 24.3r 15RE280 568 C~2nvp 2015 09 08.40906 00 39 02.740 +04 23 42.16 24.4r 15RE280 568 C~2nvp 2015 09 08.51318 00 39 02.354 +04 23 39.73 24.6r 15RE280 568 C~2nvp 2015 09 08.55681 00 39 02.189 +04 23 38.75 24.2r 15RE280 568 C~2nvp 2015 09 09.53240 00 38 58.582 +04 23 15.93 24.7w 15RE280 568 C~2nvp 2015 09 10.47324 00 38 55.064 +04 22 53.81 24.5w 15RE280 568 C~2nvp 2015 09 16.46364 00 38 32.021 +04 20 28.76 24.7w 15RE280 568 C~2nvp 2015 10 03.39174 00 37 22.996 +04 13 12.61 24.5w 15RE280 568 C~2nvp 2015 10 07.35863 00 37 06.526 +04 11 28.44 24.2r 15RE280 568 C~2nvp 2015 10 07.41176 00 37 06.312 +04 11 26.78 25.0r 15RE280 568 C~2nvp 2015 11 07.25497 00 35 08.372 +03 58 56.92 24.7w 15RE280 568 C~2nvp 2015 11 07.30780 00 35 08.191 +03 58 55.73 24.7w 15RE280 568 C~2nvp 2015 11 10.39374 00 34 58.316 +03 57 52.65 24.8w 15RE280 568 C~2nvp 2015 12 07.33142 00 33 57.410 +03 51 23.03 24.6w 15RE280 568 C~2nvp 2016 01 01.26036 00 33 50.306 +03 50 36.34 24.6w 15RE280 568 C~2nvp 2016 09 05.53675 00 43 24.195 +04 52 41.08 24.7w 15RE280 568 C~2nvp 2016 09 07.52244 00 43 17.042 +04 51 56.44 24.9w 15RE280 568 C~2nvp 2016 11 04.28299 00 39 28.995 +04 27 58.16 24.7w 15RE280 568 C~2nvp 2016 11 04.34222 00 39 28.785 +04 27 56.88 24.7w 15RE280 568 C~2nvp 2016 12 29.26158 00 37 57.492 +04 18 12.80 24.8w 15RE280 568 C~2nvp 2017 01 03.23211 00 38 00.896 +04 18 34.14 23.4w 15RE280 568 C~2nvp 2017 01 28.23958 00 38 48.364 +04 23 35.02 25.0w 15RE280 568 C~2nvp 2017 09 16.50467 00 46 58.117 +05 16 35.44 24.2w 15RE280 568 C~2nvp 2017 09 17.40380 00 46 54.607 +05 16 13.54 15RE280 568 C~2nvp 2017 09 22.45810 00 46 34.489 +05 14 07.97 24.6w 15RE280 568 C~2nvp 2017 12 23.29716 00 42 05.687 +04 45 49.28 24.8w 15RE280 568 C~2nvp
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 -0.09 0.00 0.04
2 0.0574 223.29 0.09 8.64 -0.01
3 0.0710 193.89 0.03 10.60 -0.12
4 0.1339 -331.54 0.02 19.84 -0.06
5 0.1340 -333.16 -0.05 19.93 -0.00
6 0.2103 -1698.26 -0.04 29.60 0.12
7 0.2105 -1704.52 0.02 29.63 0.07
8 0.2107 -1707.18 0.02 29.69 0.11
9 0.2133 -1765.76 0.05 29.85 -0.02
10 0.2159 -1822.84 -0.02 30.13 0.01
11 0.2323 -2196.79 0.09 31.85 0.02
12 0.2787 -3317.82 -0.09 35.79 0.01
13 0.2895 -3585.39 -0.02 36.71 0.17
14 0.2897 -3588.99 0.02 36.44 -0.13
15 0.3741 -5507.25 0.15 40.22 -0.02
16 0.3742 -5510.21 0.05 40.19 -0.08
17 0.3827 -5671.00 -0.16 40.30 -0.18
18 0.4564 -6663.13 -0.04 40.64 -0.00
19 0.5247 -6779.37 -0.01 39.55 0.05
20 1.2044 2579.64 0.00 100.05 -0.02
21 1.2099 2463.78 -0.04 100.72 0.02
22 1.3680 -1236.66 -0.05 111.20 0.01
23 1.3682 -1240.06 -0.07 111.26 0.03
24 1.5185 -2725.27 -0.12 109.39 -0.07
25 1.5322 -2670.05 0.33 109.04 0.01
26 1.6006 -1898.87 -0.11 107.33 0.04
27 2.2338 6083.81 -0.00 174.32 0.02
28 2.2362 6026.95 -0.07 174.56 0.05
29 2.2501 5701.00 0.10 175.93 0.03
30 2.5015 1338.47 -0.01 179.66 -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.
15RE280 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 44.595 44.607 44.584 ecceobj 0.037 0.039 0.037 incobj 0.996 0.996 0.996 qmin 41.813 41.779 41.823 qmax 47.151 47.152 47.098 amean 44.368 44.380 44.357 amin 44.020 44.039 44.007 amax 44.730 44.741 44.713 emean 0.039 0.040 0.039 emin 0.024 0.025 0.023 emax 0.054 0.055 0.054 imean 2.120 2.122 2.119 imin 1.448 1.450 1.445 imax 2.629 2.628 2.629 excite_mean 0.054 0.055 0.054 fracstop 1.000 1.000 1.000 cjmean 3.102 3.102 3.102 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 166.0 166.5 166.0 kozaiamp 180.0 179.9 179.9