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: 14UM271 # Created Wed Nov 27 02:10:05 2024 # Orbit generated from Bernstein formalism # Fitting 90 observations of 90 # Arc: 6.18d # First observation: 2014/10/24 # Last observation: 2014/10/30 Preliminary a, adot, b, bdot, g, gdot: 0.000001 0.035672 -0.000000 -0.007276 0.028049 0.000000 # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # WARNING Fitting with energy constraint # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution # Chi-squared of fit: 28.81 DOF: 175 RMS: 0.10 # Min/Max residuals: -0.28 0.23 # Exact a, adot, b, bdot, g, gdot: 1.984835E-05 3.371303E-02 -4.597790E-06 -7.405551E-03 2.774538E-02 6.013267E-03 # Covariance matrix: 2.3941E-12 4.0560E-09 2.0863E-14 2.6091E-10 6.4600E-10 -2.0028E-09 4.0560E-09 7.0192E-06 3.5934E-11 4.5125E-07 1.1168E-06 -4.1689E-06 2.0863E-14 3.5934E-11 4.5763E-14 -8.5600E-13 5.7293E-12 1.1912E-11 2.6091E-10 4.5125E-07 -8.5600E-13 2.9357E-08 7.1789E-08 -2.9328E-07 6.4600E-10 1.1168E-06 5.7293E-12 7.1789E-08 1.7771E-07 -6.0373E-07 -2.0028E-09 -4.1689E-06 1.1912E-11 -2.9328E-07 -6.0373E-07 1.7028E-04 # lat0 lon0 xBary yBary zBary JD0 33.564915 27.877764 -0.045387 0.550412 -0.829293 2456954.828088 # Heliocentric elements and errors Epoch: 2456950.5000 = 2014/10/20 Mean Anomaly: 8.67374 +/- 14.956 Argument of Peri: 78.16625 +/- 54.774 Long of Asc Node: 276.08673 +/- 2.016 Inclination: 34.68774 +/- 0.391 Eccentricity: 0.50972704 +/- 0.2847 Semi-Major Axis: 71.78532773 +/- 30.7013 Time of Perihelion: 2451598.0107 +/- 8566.4 Perihelion: 35.19440485 +/- 25.3794 Aphelion: 108.37625060 +/- 50.6550 Period (y) 608.2215 +/- 390.19 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 27.40283190 +/- 0.4034 Ecliptic Y 14.55014446 +/- 0.2133 Ecliptic Z 19.92682763 +/- 0.3028 Ecliptic XDOT -0.00076579 +/- 0.0010 Ecliptic YDOT 0.00335595 +/- 0.0005 Ecliptic ZDOT -0.00028074 +/- 0.0007 # Distances at JD0 (AU) Heliocenter to KBO 36.87411503 +/- 0.3517 Geocenter to KBO 36.04203461 +/- 0.5476 # Hcoef: 7.58
The following table shows the complete astrometric record for 14UM271. 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 (14UM271) followed by the observatory code and reference code for the source of the astrometry.
2014 10 24.32731 00 42 18.66 +41 28 15.7 23.9g 14UM271 568 C~4qPy 2014 10 24.33134 00 42 18.65 +41 28 15.4 23.9g 14UM271 568 C~4qPy 2014 10 24.33538 00 42 18.63 +41 28 15.3 23.7g 14UM271 568 C~4qPy 2014 10 24.35331 00 42 18.52 +41 28 14.5 23.7g 14UM271 568 C~4qPy 2014 10 24.35734 00 42 18.49 +41 28 14.3 23.8g 14UM271 568 C~4qPy 2014 10 24.36137 00 42 18.47 +41 28 14.2 23.9g 14UM271 568 C~4qPy 2014 10 24.37931 00 42 18.36 +41 28 13.4 24.5g 14UM271 568 C~4qPy 2014 10 24.38335 00 42 18.33 +41 28 13.2 23.8g 14UM271 568 C~4qPy 2014 10 24.38738 00 42 18.31 +41 28 13.1 23.8g 14UM271 568 C~4qPy 2014 10 24.40546 00 42 18.20 +41 28 12.2 23.7g 14UM271 568 C~4qPy 2014 10 24.40950 00 42 18.17 +41 28 12.1 23.9g 14UM271 568 C~4qPy 2014 10 24.41353 00 42 18.14 +41 28 11.9 23.6g 14UM271 568 C~4qPy 2014 10 24.43147 00 42 18.04 +41 28 11.0 23.4g 14UM271 568 C~4qPy 2014 10 24.43550 00 42 18.01 +41 28 10.9 23.7g 14UM271 568 C~4qPy 2014 10 24.43954 00 42 17.98 +41 28 10.9 23.6g 14UM271 568 C~4qPy 2014 10 24.45783 00 42 17.88 +41 28 10.0 23.8g 14UM271 568 C~4qPy 2014 10 24.46186 00 42 17.86 +41 28 09.7 24.0g 14UM271 568 C~4qPy 2014 10 24.46589 00 42 17.83 +41 28 09.4 24.3g 14UM271 568 C~4qPy 2014 10 24.48382 00 42 17.73 +41 28 08.7 23.7g 14UM271 568 C~4qPy 2014 10 24.48785 00 42 17.70 +41 28 08.5 24.0g 14UM271 568 C~4qPy 2014 10 24.49195 00 42 17.68 +41 28 08.3 23.9g 14UM271 568 C~4qPy 2014 10 24.51461 00 42 17.55 +41 28 07.3 24.0g 14UM271 568 C~4qPy 2014 10 24.51864 00 42 17.52 +41 28 07.2 23.7g 14UM271 568 C~4qPy 2014 10 24.52267 00 42 17.49 +41 28 07.1 23.8g 14UM271 568 C~4qPy 2014 10 24.54121 00 42 17.40 +41 28 06.1 24.2g 14UM271 568 C~4qPy 2014 10 24.54525 00 42 17.37 +41 28 06.1 24.5g 14UM271 568 C~4qPy 2014 10 24.54934 00 42 17.32 +41 28 05.8 24.4g 14UM271 568 C~4qPy 2014 10 24.56724 00 42 17.24 +41 28 05.1 23.2g 14UM271 568 C~4qPy 2014 10 24.57127 00 42 17.19 +41 28 04.8 23.3g 14UM271 568 C~4qPy 2014 10 28.20160 00 41 56.04 +41 25 18.4 23.6g 14UM271 568 C~4qPy 2014 10 28.21949 00 41 55.92 +41 25 17.5 23.4g 14UM271 568 C~4qPy 2014 10 28.22353 00 41 55.90 +41 25 17.6 23.6g 14UM271 568 C~4qPy 2014 10 28.22756 00 41 55.88 +41 25 17.1 23.6g 14UM271 568 C~4qPy 2014 10 28.27158 00 41 55.62 +41 25 15.0 23.7g 14UM271 568 C~4qPy 2014 10 28.27965 00 41 55.57 +41 25 14.9 23.6g 14UM271 568 C~4qPy 2014 10 28.29759 00 41 55.46 +41 25 13.9 23.7g 14UM271 568 C~4qPy 2014 10 28.30163 00 41 55.45 +41 25 13.7 23.6g 14UM271 568 C~4qPy 2014 10 28.30566 00 41 55.42 +41 25 13.8 23.6g 14UM271 568 C~4qPy 2014 10 28.32362 00 41 55.32 +41 25 12.8 23.6g 14UM271 568 C~4qPy 2014 10 28.32765 00 41 55.29 +41 25 12.6 23.8g 14UM271 568 C~4qPy 2014 10 28.33446 00 41 55.25 +41 25 12.1 23.5g 14UM271 568 C~4qPy 2014 10 28.35250 00 41 55.14 +41 25 11.5 23.5g 14UM271 568 C~4qPy 2014 10 28.35653 00 41 55.13 +41 25 11.3 23.9g 14UM271 568 C~4qPy 2014 10 28.36057 00 41 55.09 +41 25 11.2 23.4g 14UM271 568 C~4qPy 2014 10 28.39008 00 41 54.93 +41 25 09.5 23.5g 14UM271 568 C~4qPy 2014 10 28.41205 00 41 54.80 +41 25 08.7 24.0g 14UM271 568 C~4qPy 2014 10 28.41608 00 41 54.77 +41 25 08.3 23.5g 14UM271 568 C~4qPy 2014 10 28.43402 00 41 54.67 +41 25 07.7 23.4g 14UM271 568 C~4qPy 2014 10 28.46808 00 41 54.46 +41 25 06.0 24.1g 14UM271 568 C~4qPy 2014 10 28.48633 00 41 54.35 +41 25 04.9 23.4g 14UM271 568 C~4qPy 2014 10 28.49036 00 41 54.35 +41 25 04.7 23.5g 14UM271 568 C~4qPy 2014 10 28.49439 00 41 54.29 +41 25 04.7 23.4g 14UM271 568 C~4qPy 2014 10 28.51233 00 41 54.19 +41 25 03.7 23.6g 14UM271 568 C~4qPy 2014 10 30.19307 00 41 44.73 +41 23 42.9 23.9g 14UM271 568 C~4qPy 2014 10 30.19710 00 41 44.71 +41 23 42.7 23.7g 14UM271 568 C~4qPy 2014 10 30.20113 00 41 44.67 +41 23 42.6 23.5g 14UM271 568 C~4qPy 2014 10 30.21903 00 41 44.57 +41 23 41.7 23.6g 14UM271 568 C~4qPy 2014 10 30.22306 00 41 44.56 +41 23 41.5 23.5g 14UM271 568 C~4qPy 2014 10 30.22709 00 41 44.51 +41 23 41.5 23.7g 14UM271 568 C~4qPy 2014 10 30.24502 00 41 44.41 +41 23 40.4 23.5g 14UM271 568 C~4qPy 2014 10 30.24905 00 41 44.40 +41 23 40.2 23.7g 14UM271 568 C~4qPy 2014 10 30.25308 00 41 44.37 +41 23 40.1 23.5g 14UM271 568 C~4qPy 2014 10 30.27101 00 41 44.29 +41 23 39.3 23.6g 14UM271 568 C~4qPy 2014 10 30.27505 00 41 44.26 +41 23 39.0 23.9g 14UM271 568 C~4qPy 2014 10 30.27908 00 41 44.22 +41 23 38.9 23.7g 14UM271 568 C~4qPy 2014 10 30.29701 00 41 44.14 +41 23 38.1 23.9g 14UM271 568 C~4qPy 2014 10 30.30104 00 41 44.09 +41 23 37.7 23.7g 14UM271 568 C~4qPy 2014 10 30.30508 00 41 44.08 +41 23 37.6 23.6g 14UM271 568 C~4qPy 2014 10 30.32303 00 41 43.98 +41 23 36.8 23.8g 14UM271 568 C~4qPy 2014 10 30.32706 00 41 43.95 +41 23 36.7 23.9g 14UM271 568 C~4qPy 2014 10 30.34904 00 41 43.82 +41 23 35.4 23.3g 14UM271 568 C~4qPy 2014 10 30.35307 00 41 43.81 +41 23 35.3 23.5g 14UM271 568 C~4qPy 2014 10 30.35710 00 41 43.79 +41 23 35.1 23.6g 14UM271 568 C~4qPy 2014 10 30.37507 00 41 43.70 +41 23 34.1 23.6g 14UM271 568 C~4qPy 2014 10 30.37911 00 41 43.67 +41 23 33.9 23.5g 14UM271 568 C~4qPy 2014 10 30.38314 00 41 43.64 +41 23 33.7 23.5g 14UM271 568 C~4qPy 2014 10 30.40110 00 41 43.53 +41 23 32.9 23.4g 14UM271 568 C~4qPy 2014 10 30.40514 00 41 43.51 +41 23 32.7 23.6g 14UM271 568 C~4qPy 2014 10 30.40917 00 41 43.48 +41 23 32.5 23.5g 14UM271 568 C~4qPy 2014 10 30.42748 00 41 43.37 +41 23 31.5 23.6g 14UM271 568 C~4qPy 2014 10 30.43151 00 41 43.36 +41 23 31.4 23.0g 14UM271 568 C~4qPy 2014 10 30.43555 00 41 43.33 +41 23 31.2 23.7g 14UM271 568 C~4qPy 2014 10 30.45348 00 41 43.24 +41 23 30.4 23.8g 14UM271 568 C~4qPy 2014 10 30.45752 00 41 43.21 +41 23 30.0 23.9g 14UM271 568 C~4qPy 2014 10 30.46155 00 41 43.20 +41 23 29.9 23.8g 14UM271 568 C~4qPy 2014 10 30.47951 00 41 43.07 +41 23 29.0 23.8g 14UM271 568 C~4qPy 2014 10 30.48354 00 41 43.05 +41 23 28.9 23.5g 14UM271 568 C~4qPy 2014 10 30.48952 00 41 43.03 +41 23 28.5 23.5g 14UM271 568 C~4qPy 2014 10 30.50786 00 41 42.91 +41 23 27.7 23.6g 14UM271 568 C~4qPy 2014 10 30.51189 00 41 42.90 +41 23 27.3 23.7g 14UM271 568 C~4qPy
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 -0.13 0.00 0.08
2 0.0000 -0.24 -0.04 -0.21 -0.11
3 0.0000 -0.49 0.04 -0.19 -0.06
4 0.0001 -1.95 0.02 -0.32 -0.07
5 0.0001 -2.34 -0.04 -0.34 -0.06
6 0.0001 -2.59 0.04 -0.32 -0.01
7 0.0001 -4.06 0.02 -0.45 -0.01
8 0.0002 -4.45 -0.04 -0.47 -0.00
9 0.0002 -4.69 0.04 -0.45 0.04
10 0.0002 -6.21 -0.01 -0.66 -0.04
11 0.0002 -6.55 -0.02 -0.59 0.06
12 0.0002 -6.94 -0.09 -0.61 0.07
13 0.0003 -8.36 -0.05 -0.88 -0.07
14 0.0003 -8.70 -0.07 -0.81 0.03
15 0.0003 -9.00 -0.04 -0.65 0.22
16 0.0004 -10.42 0.03 -0.92 0.09
17 0.0004 -10.76 0.02 -1.08 -0.03
18 0.0004 -11.19 -0.09 -1.19 -0.11
19 0.0004 -12.52 0.04 -1.28 -0.06
20 0.0004 -12.91 -0.02 -1.29 -0.05
21 0.0005 -13.20 0.02 -1.37 -0.09
22 0.0005 -14.96 0.09 -1.56 -0.10
23 0.0005 -15.30 0.07 -1.49 -0.00
24 0.0005 -15.65 0.05 -1.42 0.10
25 0.0006 -17.01 0.19 -1.83 -0.15
26 0.0006 -17.31 0.22 -1.67 0.04
27 0.0006 -17.95 -0.09 -1.67 0.07
28 0.0007 -19.07 0.23 -1.87 0.02
29 0.0007 -19.71 -0.08 -1.87 0.06
30 0.0106 -307.81 0.07 -37.05 -0.11
31 0.0107 -309.42 -0.12 -37.21 -0.09
32 0.0107 -309.58 0.05 -37.02 0.15
33 0.0107 -310.01 -0.06 -37.35 -0.15
34 0.0108 -313.58 -0.12 -37.83 -0.17
35 0.0108 -314.12 -0.01 -37.65 0.09
36 0.0109 -315.68 -0.14 -37.95 -0.03
37 0.0109 -315.88 -0.01 -38.08 -0.11
38 0.0109 -316.13 0.06 -37.83 0.18
39 0.0109 -317.59 0.04 -38.18 0.02
40 0.0110 -317.98 -0.03 -38.20 0.04
41 0.0110 -318.61 -0.11 -38.43 -0.12
42 0.0110 -319.99 -0.04 -38.38 0.13
43 0.0110 -320.18 0.09 -38.50 0.05
44 0.0110 -320.63 -0.02 -38.38 0.22
45 0.0111 -323.01 -0.04 -39.03 -0.12
46 0.0112 -324.68 0.06 -39.05 0.11
47 0.0112 -325.17 -0.10 -39.25 -0.04
48 0.0112 -326.44 0.07 -39.25 0.16
49 0.0113 -329.33 -0.07 -39.64 0.16
50 0.0114 -330.93 -0.22 -40.03 -0.02
51 0.0114 -331.03 0.01 -40.20 -0.15
52 0.0114 -331.62 -0.26 -39.88 0.22
53 0.0115 -333.09 -0.28 -40.24 0.08
54 0.0161 -465.02 0.07 -61.46 -0.12
55 0.0161 -465.31 0.10 -61.53 -0.14
56 0.0161 -465.76 -0.03 -61.41 0.03
57 0.0161 -467.17 -0.03 -61.67 -0.01
58 0.0161 -467.37 0.10 -61.80 -0.09
59 0.0162 -467.86 -0.08 -61.53 0.23
60 0.0162 -469.37 -0.17 -61.97 0.00
61 0.0162 -469.57 -0.04 -62.09 -0.07
62 0.0162 -469.91 -0.07 -62.02 0.05
63 0.0163 -471.08 0.19 -62.31 -0.01
64 0.0163 -471.52 0.07 -62.41 -0.07
65 0.0163 -471.96 -0.05 -62.29 0.10
66 0.0163 -473.14 0.20 -62.57 0.04
67 0.0164 -473.82 -0.16 -62.66 0.00
68 0.0164 -473.97 0.01 -62.69 0.02
69 0.0164 -475.34 0.08 -62.87 0.07
70 0.0164 -475.68 0.05 -62.80 0.19
71 0.0165 -477.58 -0.09 -63.26 0.00
72 0.0165 -477.73 0.08 -63.29 0.02
73 0.0165 -478.02 0.11 -63.36 0.00
74 0.0166 -479.39 0.18 -63.77 -0.18
75 0.0166 -479.78 0.11 -63.79 -0.14
76 0.0166 -480.17 0.05 -63.80 -0.11
77 0.0166 -481.64 0.01 -63.93 0.00
78 0.0166 -481.93 0.04 -64.00 -0.02
79 0.0167 -482.32 -0.03 -64.01 0.02
80 0.0167 -483.89 -0.13 -64.31 -0.04
81 0.0167 -484.03 0.05 -64.35 -0.02
82 0.0167 -484.43 -0.02 -64.37 0.01
83 0.0168 -485.70 0.14 -64.60 0.02
84 0.0168 -486.18 -0.02 -64.79 -0.12
85 0.0168 -486.33 0.16 -64.83 -0.10
86 0.0168 -488.04 -0.12 -64.93 0.04
87 0.0169 -488.29 -0.05 -64.91 0.11
88 0.0169 -488.67 0.04 -65.16 -0.05
89 0.0169 -490.24 -0.06 -65.23 0.13
90 0.0169 -490.53 -0.03 -65.53 -0.12
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.
14UM271 quality flag:0 Type: ERR2LARGE ERR2LARGE ERR2LARGE axisobj 0.000 0.000 0.000 ecceobj -1.000 -1.000 -1.000 incobj -1.000 -1.000 -1.000 qmin 0.000 0.000 0.000 qmax 0.000 0.000 0.000 amean 0.000 0.000 0.000 amin 0.000 0.000 0.000 amax 0.000 0.000 0.000 emean 0.000 0.000 0.000 emin 0.000 0.000 0.000 emax 0.000 0.000 0.000 imean 0.000 0.000 0.000 imin 0.000 0.000 0.000 imax 0.000 0.000 0.000 excite_mean 0.000 0.000 0.000 fracstop 0.000 0.000 0.000 cjmean 0.000 0.000 0.000 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 0.0 0.0 0.0 kozaiamp 0.0 0.0 0.0