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: 15RN280
# Created Fri Apr 19 01:17:40 2024
# Orbit generated from Bernstein formalism
# Fitting 37 observations of 37
# Arc: 2.25y
# First observation: 2015/06/23
# Last observation: 2017/09/22
Preliminary a, adot, b, bdot, g, gdot:
-0.000087 0.017750 0.000005 -0.006268 0.021707 0.000000
# Chi-squared of fit: 10.59 DOF: 68 RMS: 0.09
# Min/Max residuals: -0.41 0.24
# Exact a, adot, b, bdot, g, gdot:
1.309576E-05 1.738430E-02 -4.219655E-06 -6.167318E-03 2.142517E-02 5.386144E-04
# Covariance matrix:
1.3684E-13 9.1039E-15 1.2472E-15 -2.6689E-14 1.2361E-13 2.4393E-12
9.1039E-15 2.4729E-13 1.2696E-14 -8.9659E-14 2.0741E-13 8.1164E-12
1.2472E-15 1.2696E-14 8.0390E-14 -7.0936E-14 1.2036E-14 8.8399E-13
-2.6689E-14 -8.9659E-14 -7.0936E-14 1.5266E-13 -1.0485E-13 -5.3897E-12
1.2361E-13 2.0741E-13 1.2036E-14 -1.0485E-13 3.1123E-13 9.5172E-12
2.4393E-12 8.1164E-12 8.8399E-13 -5.3897E-12 9.5172E-12 4.8679E-10
# lat0 lon0 xBary yBary zBary JD0
2.995073 7.970124 1.010408 -0.005629 0.109402 2457197.079268
# Heliocentric elements and errors
Epoch: 2457190.5000 = 2015/06/17
Mean Anomaly: 176.30293 +/- 0.459
Argument of Peri: 353.93060 +/- 0.462
Long of Asc Node: 195.13623 +/- 0.000
Inclination: 19.72335 +/- 0.001
Eccentricity: 0.12922109 +/- 0.0000
Semi-Major Axis: 41.25038560 +/- 0.0023
Time of Perihelion: 2506569.2597 +/- 123.3
Perihelion: 35.91996569 +/- 0.0028
Aphelion: 46.58080552 +/- 0.0032
Period (y) 264.9416 +/- 0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 46.18820411 +/- 0.0012
Ecliptic Y 5.44744932 +/- 0.0002
Ecliptic Z 2.43858378 +/- 0.0001
Ecliptic XDOT -0.00020164 +/- 0.0000
Ecliptic YDOT 0.00220903 +/- 0.0000
Ecliptic ZDOT -0.00078336 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 46.57221912 +/- 0.0012
Geocenter to KBO 46.67406520 +/- 0.0012
# Hcoef: 7.60
The following table shows the complete astrometric record for 15RN280. 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 (15RN280) followed by the observatory code and reference code for the source of the astrometry.
2015 06 23.57849 00 24 31.768 +05 54 46.68 24.7r 15RN280 568 C~2nvq 2015 06 23.58498 00 24 31.771 +05 54 46.71 24.4r 15RN280 568 C~2nvq 2015 07 14.57552 00 24 38.219 +05 55 37.41 24.5r 15RN280 568 C~2nvq 2015 07 19.55444 00 24 34.772 +05 55 16.72 24.2r 15RN280 568 C~2nvq 2015 08 13.46762 00 23 50.960 +05 50 31.08 21.5r 15RN280 568 C~2nvq 2015 08 13.52103 00 23 50.817 +05 50 30.03 24.1r 15RN280 568 C~2nvq 2015 08 19.57132 00 23 34.162 +05 48 37.57 24.2r 15RN280 568 C~2nvq 2015 08 19.60028 00 23 34.054 +05 48 36.97 24.5r 15RN280 568 C~2nvq 2015 08 20.40327 00 23 31.729 +05 48 21.19 24.3r 15RN280 568 C~2nvq 2015 08 20.45053 00 23 31.597 +05 48 20.09 24.3r 15RN280 568 C~2nvq 2015 09 07.55043 00 22 30.509 +05 41 17.50 24.4w 15RN280 568 C~2nvq 2015 09 09.37654 00 22 23.666 +05 40 29.12 24.4r 15RN280 568 C~2nvq 2015 09 09.42093 00 22 23.504 +05 40 27.99 24.6r 15RN280 568 C~2nvq 2015 09 09.46188 00 22 23.350 +05 40 26.86 24.8r 15RN280 568 C~2nvq 2015 09 10.48550 00 22 19.455 +05 39 59.41 24.5w 15RN280 568 C~2nvq 2015 09 18.44074 00 21 48.421 +05 36 17.70 24.5w 15RN280 568 C~2nvq 2015 09 18.48843 00 21 48.221 +05 36 16.34 24.8w 15RN280 568 C~2nvq 2015 10 08.32880 00 20 28.030 +05 26 24.28 24.6w 15RN280 568 C~2nvq 2015 10 08.38143 00 20 27.817 +05 26 22.61 24.4w 15RN280 568 C~2nvq 2015 10 09.29850 00 20 24.148 +05 25 54.74 24.5w 15RN280 568 C~2nvq 2015 11 10.41160 00 18 31.395 +05 10 42.77 24.8w 15RN280 568 C~2nvq 2015 11 15.27884 00 18 18.505 +05 08 45.94 24.8w 15RN280 568 C~2nvq 2015 12 08.22307 00 17 39.397 +05 01 42.33 24.7w 15RN280 568 C~2nvq 2016 01 01.28580 00 17 42.755 +04 58 53.77 24.9w 15RN280 568 C~2nvq 2016 09 05.49854 00 26 54.732 +05 46 05.10 24.4w 15RN280 568 C~2nvq 2016 09 05.51877 00 26 54.654 +05 46 04.65 24.6w 15RN280 568 C~2nvq 2016 09 06.49401 00 26 51.082 +05 45 39.33 25.1w 15RN280 568 C~2nvq 2016 09 07.45899 00 26 47.519 +05 45 14.12 24.4w 15RN280 568 C~2nvq 2016 09 07.50445 00 26 47.348 +05 45 13.04 24.6w 15RN280 568 C~2nvq 2016 09 26.53383 00 25 32.577 +05 36 14.83 24.7w 15RN280 568 C~2nvq 2016 10 30.34461 00 23 21.993 +05 19 33.35 24.6w 15RN280 568 C~2nvq 2016 11 03.29848 00 23 08.950 +05 17 45.99 24.1w 15RN280 568 C~2nvq 2016 12 24.26796 00 21 51.029 +05 03 28.69 23.6w 15RN280 568 C~2nvq 2017 01 02.25760 00 21 58.284 +05 03 08.96 23.9w 15RN280 568 C~2nvq 2017 01 26.23696 00 22 49.184 +05 05 45.40 24.7w 15RN280 568 C~2nvq 2017 09 15.44018 00 30 37.663 +05 45 51.52 24.5w 15RN280 568 C~2nvq 2017 09 22.50534 00 30 09.648 +05 42 29.78 24.4w 15RN280 568 C~2nvq
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 -0.05 0.00 -0.07
2 0.0000 0.05 -0.12 0.01 -0.06
3 0.0575 108.47 0.10 8.47 -0.01
4 0.0711 53.05 0.15 9.83 -0.03
5 0.1393 -660.34 0.22 6.55 0.20
6 0.1395 -662.72 0.14 6.43 0.09
7 0.1560 -935.48 -0.11 1.70 -0.10
8 0.1561 -937.19 -0.41 1.79 0.01
9 0.1583 -975.30 -0.01 1.05 0.10
10 0.1584 -977.55 0.08 0.83 -0.10
11 0.2080 -1982.15 -0.01 -25.46 0.02
12 0.2130 -2095.11 -0.11 -29.33 -0.01
13 0.2131 -2097.78 0.03 -29.41 -0.01
14 0.2132 -2100.34 0.07 -29.53 -0.07
15 0.2160 -2164.60 -0.03 -31.65 0.01
16 0.2378 -2677.88 0.18 -51.21 -0.04
17 0.2379 -2681.16 0.10 -51.27 0.01
18 0.2923 -4015.49 0.00 -118.79 0.10
19 0.2924 -4019.07 -0.00 -119.06 0.02
20 0.2949 -4080.45 -0.06 -122.85 0.05
21 0.3828 -5989.49 -0.04 -289.25 0.02
22 0.3962 -6212.85 0.07 -319.70 -0.04
23 0.4590 -6918.30 -0.07 -475.44 -0.05
24 0.5249 -6939.51 -0.01 -650.13 0.03
25 1.2044 1753.09 -0.02 -1322.94 -0.03
26 1.2045 1751.84 -0.03 -1322.89 0.05
27 1.2072 1692.86 -0.08 -1325.09 -0.04
28 1.2098 1634.05 -0.07 -1327.24 -0.05
29 1.2099 1631.28 -0.01 -1327.22 0.05
30 1.2620 393.30 -0.04 -1380.29 -0.05
31 1.3546 -1793.85 0.09 -1527.63 -0.04
32 1.3654 -2015.29 -0.14 -1548.95 0.03
33 1.5050 -3424.27 -0.08 -1874.06 -0.12
34 1.5296 -3332.59 -0.03 -1935.22 0.05
35 1.5952 -2572.27 0.24 -2093.42 -0.03
36 2.2310 4806.29 0.10 -2647.87 -0.05
37 2.2503 4342.25 -0.03 -2668.66 0.13
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.
15RN280 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 41.576 41.583 41.568 ecceobj 0.120 0.120 0.120 incobj 19.616 19.617 19.616 qmin 34.945 35.031 34.952 qmax 48.137 48.045 48.063 amean 41.385 41.402 41.391 amin 41.027 41.071 41.038 amax 41.757 41.764 41.784 emean 0.134 0.131 0.134 emin 0.117 0.113 0.117 emax 0.153 0.151 0.152 imean 19.927 19.988 19.953 imin 19.203 19.252 19.243 imax 20.713 20.729 20.747 excite_mean 0.366 0.366 0.367 fracstop 1.000 1.000 1.000 cjmean 2.913 2.913 2.912 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 176.9 179.9 178.0 kozaiamp 180.0 180.0 179.9