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: 14SM363 # Created Thu Apr 18 01:16:22 2024 # Orbit generated from Bernstein formalism # Fitting 28 observations of 31 # Arc: 4.24y # First observation: 2014/08/19 # Last observation: 2018/11/15 Preliminary a, adot, b, bdot, g, gdot: 0.000129 0.021449 -0.000025 -0.004205 0.023611 0.000000 # Chi-squared of fit: 7.72 DOF: 50 RMS: 0.09 # Min/Max residuals: -0.27 0.27 # Exact a, adot, b, bdot, g, gdot: 1.446399E-05 2.158363E-02 -2.871663E-06 -4.243422E-03 2.356016E-02 2.977271E-03 # Covariance matrix: 2.3957E-13 -9.7787E-14 -5.8423E-15 1.3980E-14 6.9780E-14 -9.5148E-13 -9.7787E-14 2.1773E-13 2.8794E-14 -4.9422E-14 1.3484E-13 2.9554E-12 -5.8423E-15 2.8794E-14 1.8018E-13 -6.7856E-14 2.0461E-14 4.5298E-13 1.3980E-14 -4.9422E-14 -6.7856E-14 4.2882E-14 -2.8338E-14 -8.0293E-13 6.9780E-14 1.3484E-13 2.0461E-14 -2.8338E-14 2.6253E-13 1.4963E-12 -9.5148E-13 2.9554E-12 4.5298E-13 -8.0293E-13 1.4963E-12 4.8757E-11 # lat0 lon0 xBary yBary zBary JD0 -20.710794 5.192089 0.640345 -0.278295 -0.736425 2456888.823468 # Heliocentric elements and errors Epoch: 2456880.5000 = 2014/08/11 Mean Anomaly: 98.61985 +/- 0.079 Argument of Peri: 129.75134 +/- 0.067 Long of Asc Node: 124.67291 +/- 0.001 Inclination: 23.25459 +/- 0.000 Eccentricity: 0.12104618 +/- 0.0003 Semi-Major Axis: 41.84470793 +/- 0.0044 Time of Perihelion: 2429795.9831 +/- 21.3 Perihelion: 36.77956605 +/- 0.0120 Aphelion: 46.90984982 +/- 0.0124 Period (y) 270.6880 +/- 0.04 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 40.37838148 +/- 0.0009 Ecliptic Y 3.02843720 +/- 0.0001 Ecliptic Z -15.01066945 +/- 0.0003 Ecliptic XDOT -0.00008324 +/- 0.0000 Ecliptic YDOT 0.00250709 +/- 0.0000 Ecliptic ZDOT -0.00058348 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 43.18454955 +/- 0.0008 Geocenter to KBO 42.44452486 +/- 0.0009 # Hcoef: 6.68
The following table shows the complete astrometric record for 14SM363. 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 (14SM363) followed by the observatory code and reference code for the source of the astrometry.
2014 08 19.32269 00 52 45.843 -16 54 20.62 22.6i 14SM363 W84 C~55S5 2014 09 17.18464 00 51 02.70 -17 13 08.8 14SM363 W84 C~2gaD 2014 09 17.26012 00 51 02.347 -17 13 10.77 14SM363 807 C~3wpO 2014 09 17.33254 00 51 02.06 -17 13 14.1 23.3V 14SM363 W84 C~2gaD 2014 09 18.37122 00 50 57.65 -17 13 51.1 14SM363 W84 C~2gaD 2014 10 24.02997 00 48 18.402 -17 29 41.76 14SM363 304 C~3wpO 2014 10 25.01114 00 48 14.174 -17 29 56.82 14SM363 304 C~3wpO 2014 11 21.17724 00 46 34.568 -17 32 13.80 24.2g 14SM363 W84 C~55S5 2014 11 21.17861 00 46 34.556 -17 32 13.97 23.7r 14SM363 W84 C~55S5 2015 08 18.32660 00 57 54.892 -16 35 58.32 23.2r 14SM363 W84 C~55S5 2015 08 22.30759 00 57 44.181 -16 38 39.19 23.1r 14SM363 W84 C~55S5 2015 10 08.20305 00 54 38.925 -17 06 38.76 23.3g 14SM363 W84 C~55S5 2015 11 03.10662 00 52 45.879 -17 14 34.32 22.9i 14SM363 W84 C~55S5 2016 08 24.39579 01 02 39.417 -16 22 39.16 22.3z 14SM363 W84 C~55S5 2016 08 29.35556 01 02 24.163 -16 25 58.68 22.9r 14SM363 W84 C~55S5 2016 08 29.35692 01 02 24.161 -16 25 58.67 22.9i 14SM363 W84 C~55S5 2016 08 29.35830 01 02 24.169 -16 25 58.45 23.4g 14SM363 W84 C~55S5 2016 10 27.13397 00 58 17.194 -16 55 45.88 22.8i 14SM363 W84 C~55S5 2016 10 27.13534 00 58 17.191 -16 55 45.73 23.5r 14SM363 W84 C~55S5 2016 10 27.13673 00 58 17.170 -16 55 45.89 24.1g 14SM363 W84 C~55S5 2016 11 07.12473 00 57 32.509 -16 57 40.13 22.3z 14SM363 W84 C~55S5 2017 10 03.20767 01 05 08.514 -16 28 34.01 22.5z 14SM363 W84 C~55S5 2017 11 18.15074 01 01 56.240 -16 40 16.28 22.6i 14SM363 W84 C~55S5 2017 11 23.05697 01 01 40.734 -16 40 00.36 23.1z 14SM363 W84 C~55S5 2017 11 26.07878 01 01 31.966 -16 39 41.27 22.8z 14SM363 W84 C~55S5 2017 11 27.04262 01 01 29.312 -16 39 33.70 22.9i 14SM363 W84 C~55S5 2017 12 08.05399 01 01 03.851 -16 37 17.98 22.9r 14SM363 W84 C~55S5 2017 12 08.05537 01 01 03.841 -16 37 17.85 23.6g 14SM363 W84 C~55S5 2018 10 18.29039 01 09 02.585 -16 16 26.84 23.4r 14SM363 W84 C~55S5 2018 10 20.07305 01 08 54.628 -16 17 04.52 22.2z 14SM363 W84 C~55S5 2018 11 15.20378 01 07 07.175 -16 22 03.04 22.6i 14SM363 W84 C~55S5
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 0.00 0.00 0.00
2 0.0790 -1813.02 -0.06 -416.56 0.01
3 0.0792 -1818.44 ( -0.11) -416.27 ( 0.85)
4 0.0794 -1823.56 -0.08 -417.61 0.02
5 0.0823 -1896.38 0.08 -425.29 -0.02
6 0.1799 -4366.16 ( 0.04) -356.65 ( 0.45)
7 0.1826 -4427.55 ( -0.14) -345.67 ( 0.67)
8 0.2570 -5785.22 0.13 110.32 0.10
9 0.2570 -5785.44 -0.05 110.23 -0.01
10 0.9966 4495.01 0.05 -849.27 0.07
11 1.0075 4287.65 -0.04 -930.66 -0.02
12 1.1359 1169.28 0.06 -1344.92 0.03
13 1.2068 -502.05 -0.07 -1105.01 -0.27
14 2.0153 8546.08 -0.10 -1855.42 -0.03
15 2.0288 8262.12 -0.07 -1942.72 -0.01
16 2.0288 8262.09 -0.01 -1942.70 0.03
17 2.0288 8262.29 0.27 -1942.55 0.20
18 2.1898 4286.69 -0.07 -2061.83 -0.09
19 2.1898 4286.72 0.04 -2061.67 0.04
20 2.1898 4286.38 -0.22 -2061.69 0.01
21 2.2199 3656.55 0.05 -1896.13 -0.10
22 3.1236 10338.99 0.04 -3093.63 -0.05
23 3.2494 7533.39 0.06 -2548.94 0.00
24 3.2628 7338.09 0.09 -2439.84 -0.05
25 3.2711 7231.94 0.02 -2369.03 0.00
26 3.2737 7200.56 0.06 -2345.98 -0.00
27 3.3039 6926.25 -0.05 -2067.74 -0.02
28 3.3039 6926.17 -0.10 -2067.56 0.12
29 4.1642 13705.08 -0.22 -3889.89 0.01
30 4.1691 13584.93 0.03 -3874.22 -0.04
31 4.2406 12054.27 0.17 -3474.69 0.06
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.
14SM363 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 42.156 42.170 42.142 ecceobj 0.120 0.121 0.120 incobj 23.227 23.227 23.226 qmin 36.138 36.148 36.130 qmax 48.165 48.198 48.156 amean 41.975 41.981 41.964 amin 41.631 41.637 41.628 amax 42.357 42.360 42.340 emean 0.119 0.120 0.118 emin 0.104 0.105 0.102 emax 0.137 0.138 0.137 imean 21.773 21.759 21.789 imin 21.207 21.206 21.207 imax 22.358 22.353 22.354 excite_mean 0.390 0.390 0.390 fracstop 1.000 1.000 1.000 cjmean 2.895 2.895 2.895 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 183.0 183.3 181.0 kozaiamp 180.0 180.0 180.0