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: 14UU240 # Created Fri Apr 26 01:16:38 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 54 observations of 54 # Arc: 6.20y # First observation: 2014/10/29 # Last observation: 2021/01/11 # Chi-squared of fit: 10.30 DOF: 102 RMS: 0.08 # Min/Max residuals: -0.17 0.16 # Exact a, adot, b, bdot, g, gdot: 1.554130E-05 3.419941E-02 6.930119E-06 1.442743E-02 3.331331E-02 -1.740066E-03 # Covariance matrix: 8.1092E-14 -2.8178E-14 -2.5441E-15 -1.4019E-14 7.9734E-14 -1.4252E-13 -2.8178E-14 6.3455E-14 -1.2753E-14 2.8207E-14 1.5115E-14 3.3239E-13 -2.5441E-15 -1.2753E-14 4.5202E-14 -1.7913E-14 -1.9074E-14 -7.2927E-14 -1.4019E-14 2.8207E-14 -1.7913E-14 2.6666E-14 -4.8457E-15 1.8415E-13 7.9734E-14 1.5115E-14 -1.9074E-14 -4.8457E-15 2.0627E-13 -2.7916E-15 -1.4252E-13 3.3239E-13 -7.2927E-14 1.8415E-13 -2.7916E-15 2.1437E-12 # lat0 lon0 xBary yBary zBary JD0 -29.095002 33.783526 -0.029360 -0.483355 -0.868984 2456959.831218 # Heliocentric elements and errors Epoch: 2456960.5000 = 2014/10/30 Mean Anomaly: 238.53451 +/- 0.044 Argument of Peri: 72.18288 +/- 0.039 Long of Asc Node: 82.05493 +/- 0.000 Inclination: 35.72367 +/- 0.000 Eccentricity: 0.05016508 +/- 0.0000 Semi-Major Axis: 30.04962979 +/- 0.0015 Time of Perihelion: 2477261.0361 +/- 7.9 Perihelion: 28.54218778 +/- 0.0020 Aphelion: 31.55707180 +/- 0.0021 Period (y) 164.7278 +/- 0.01 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 22.60846626 +/- 0.0003 Ecliptic Y 15.16442098 +/- 0.0002 Ecliptic Z -14.59641777 +/- 0.0002 Ecliptic XDOT -0.00119196 +/- 0.0000 Ecliptic YDOT 0.00258235 +/- 0.0000 Ecliptic ZDOT 0.00110574 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 30.88946710 +/- 0.0003 Geocenter to KBO 30.01808653 +/- 0.0004 # Hcoef: 8.09
The following table shows the complete astrometric record for 14UU240. 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 (14UU240) followed by the observatory code and reference code for the source of the astrometry.
2014 10 29.33044 02 45 24.576 -14 38 48.11 22.6r 14UU240 W84 C~4yUy 2014 10 29.33044 02 45 24.58 -14 38 48.1 22.7r 14UU240 W84 C~3coO 2014 10 29.330446 02 45 24.576 -14 38 48.12 22.7r 14UU240 W84 C~2fCE 2014 10 29.33181 02 45 24.551 -14 38 48.09 23.2g 14UU240 W84 C~4yUy 2014 10 29.33181 02 45 24.55 -14 38 48.1 23.5g 14UU240 W84 C~3coO 2014 10 29.331812 02 45 24.554 -14 38 48.10 23.5g 14UU240 W84 C~2fCE 2014 10 31.286840 02 45 11.43 -14 39 32.8 23.5g 14UU240 W84 C~352R 2014 10 31.287367 02 45 11.429 -14 39 32.80 23.7g 14UU240 W84 C~2fCE 2014 10 31.28737 02 45 11.429 -14 39 32.80 23.6g 14UU240 W84 C~4yUy 2014 10 31.288194 02 45 11.41 -14 39 32.9 22.7r 14UU240 W84 C~352R 2014 10 31.288721 02 45 11.413 -14 39 32.85 22.9r 14UU240 W84 C~2fCE 2014 10 31.28873 02 45 11.414 -14 39 32.85 22.9r 14UU240 W84 C~4yUy 2014 11 21.266030 02 42 50.89 -14 43 15.8 23.1g 14UU240 W84 C~352R 2014 11 21.26656 02 42 50.884 -14 43 15.62 23.3g 14UU240 W84 C~4yUy 2014 11 28.23346 02 42 06.868 -14 42 38.60 23.3r 14UU240 W84 C~4yUy 2014 11 28.23346 02 42 06.87 -14 42 38.6 23.3r 14UU240 W84 C~3coO 2014 11 28.233467 02 42 06.868 -14 42 38.60 23.3r 14UU240 W84 C~2gaE 2014 11 28.234317 02 42 06.85 -14 42 38.4 22.7i 14UU240 W84 C~352R 2014 11 28.23484 02 42 06.858 -14 42 38.48 22.9i 14UU240 W84 C~4yUy 2014 12 14.13695 02 40 37.864 -14 37 39.16 23.5g 14UU240 W84 C~4yUy 2014 12 15.19793 02 40 32.642 -14 37 08.53 23.6g 14UU240 W84 C~4yUy 2014 12 15.19793 02 40 32.64 -14 37 08.5 23.7g 14UU240 W84 C~3coO 2014 12 15.197934 02 40 32.643 -14 37 08.53 23.7g 14UU240 W84 C~2gaE 2014 12 16.196279 02 40 27.833 -14 36 38.77 23.0i 14UU240 W84 C~2gaE 2014 12 16.19628 02 40 27.833 -14 36 38.77 22.9i 14UU240 W84 C~4yUy 2014 12 16.19628 02 40 27.83 -14 36 38.8 23.0i 14UU240 W84 C~3coO 2014 12 23.10996 02 39 57.152 -14 32 41.82 23.8g 14UU240 W84 C~4yUy 2015 01 13.11891 02 38 56.767 -14 15 43.57 23.0r 14UU240 W84 C~4yUy 2015 01 13.11891 02 38 56.77 -14 15 43.6 22.9r 14UU240 W84 C~3coO 2015 01 13.118918 02 38 56.768 -14 15 43.55 22.9r 14UU240 W84 C~2gaE 2015 12 17.166650 02 46 46.186 -13 10 35.56 23.1i 14UU240 W84 C~2gaE 2015 12 17.16665 02 46 46.19 -13 10 35.6 23.1i 14UU240 W84 C~3coO 2015 12 17.16665 02 46 46.186 -13 10 35.57 23.0i 14UU240 W84 C~4yUy 2015 12 17.168015 02 46 46.177 -13 10 35.60 23.1r 14UU240 W84 C~2gaE 2015 12 17.16802 02 46 46.177 -13 10 35.60 23.1r 14UU240 W84 C~4yUy 2015 12 17.16802 02 46 46.18 -13 10 35.6 23.1r 14UU240 W84 C~3coO 2015 12 17.16939 02 46 46.164 -13 10 35.45 23.8g 14UU240 W84 C~4yUy 2015 12 17.16939 02 46 46.16 -13 10 35.5 23.8g 14UU240 W84 C~3coO 2015 12 17.169393 02 46 46.164 -13 10 35.46 23.8g 14UU240 W84 C~2gaE 2016 01 17.089757 02 45 07.81 -12 47 38.9 22.3z 14UU240 W84 C~352R 2016 10 26.32515 02 58 26.943 -11 42 42.20 23.1r 14UU240 W84 C~4yUy 2016 10 26.32515 02 58 26.94 -11 42 42.2 23.5r 14UU240 W84 C~3coO 2016 10 26.32652 02 58 26.920 -11 42 42.45 23.2g 14UU240 W84 C~4yUy 2016 10 26.32652 02 58 26.92 -11 42 42.4 23.3g 14UU240 W84 C~3coO 2016 11 22.21421 02 55 26.851 -11 49 12.88 22.5i 14UU240 W84 C~4yUy 2016 11 22.21421 02 55 26.85 -11 49 12.9 22.7i 14UU240 W84 C~3coO 2017 10 29.32415 03 04 26.949 -10 15 11.31 22.6i 14UU240 W84 C~4yUy 2017 10 29.32553 03 04 26.954 -10 15 11.29 23.4g 14UU240 W84 C~4yUy 2017 11 29.17766 03 01 01.446 -10 20 43.59 22.0z 14UU240 W84 C~4yUy 2017 12 22.16896 02 58 53.331 -10 13 57.49 22.5i 14UU240 W84 C~4yUy 2017 12 22.17034 02 58 53.330 -10 13 57.55 22.7r 14UU240 W84 C~4yUy 2021 01 11.127600 03 16 06.960 -05 36 00.16 22.3G 14UU240 G37 C~4UEd 2021 01 11.192580 03 16 06.759 -05 35 57.79 14UU240 G37 C~4UEd 2021 01 11.244140 03 16 06.616 -05 35 55.55 14UU240 G37 C~4UEd
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 0.14 0.00 0.03
2 0.0000 0.00 0.08 0.00 0.02
3 0.0000 0.00 0.09 0.00 0.01
4 0.0000 0.00 -0.15 0.00 0.08
5 0.0000 0.00 -0.17 0.00 0.07
6 0.0000 0.00 -0.11 0.00 0.07
7 0.0054 0.00 0.08 0.00 0.00
8 0.0054 0.00 0.12 0.00 0.01
9 0.0054 0.00 0.12 0.00 0.01
10 0.0054 0.00 -0.08 0.00 -0.07
11 0.0054 0.00 0.02 0.00 -0.01
12 0.0054 0.00 0.03 0.00 -0.01
13 0.0628 0.00 -0.02 0.00 -0.08
14 0.0628 0.00 -0.06 0.00 0.10
15 0.0819 0.00 0.04 0.00 -0.08
16 0.0819 0.00 0.07 0.00 -0.08
17 0.0819 0.00 0.04 0.00 -0.08
18 0.0819 0.00 -0.15 0.00 0.11
19 0.0819 0.00 0.02 0.00 0.02
20 0.1254 0.00 -0.08 0.00 -0.17
21 0.1283 0.00 -0.08 0.00 0.05
22 0.1283 0.00 -0.05 0.00 0.02
23 0.1283 0.00 -0.03 0.00 0.02
24 0.1310 0.00 0.06 0.00 -0.03
25 0.1310 0.00 0.02 0.00 -0.06
26 0.1310 0.00 0.06 0.00 -0.03
27 0.1500 0.00 0.00 0.00 -0.01
28 0.2075 0.00 0.06 0.00 0.01
29 0.2075 0.00 0.02 0.00 0.04
30 0.2075 0.00 0.03 0.00 0.06
31 1.1330 0.00 0.06 0.00 0.04
32 1.1330 0.00 0.06 0.00 0.03
33 1.1330 0.00 0.12 0.00 0.00
34 1.1330 0.00 0.03 0.00 -0.04
35 1.1330 0.00 0.08 0.00 -0.04
36 1.1330 0.00 0.03 0.00 -0.04
37 1.1330 0.00 -0.12 0.00 0.02
38 1.1330 0.00 -0.06 0.00 0.07
39 1.1330 0.00 -0.06 0.00 0.06
40 1.2177 0.00 -0.05 0.00 0.14
41 1.9931 0.00 0.04 0.00 0.07
42 1.9931 0.00 0.09 0.00 0.07
43 1.9931 0.00 -0.12 0.00 -0.09
44 1.9931 0.00 -0.12 0.00 -0.14
45 2.0668 0.00 -0.02 0.00 -0.12
46 2.0668 0.00 -0.00 0.00 -0.10
47 3.0007 0.00 -0.08 0.00 0.06
48 3.0007 0.00 0.13 0.00 0.11
49 3.0851 0.00 0.01 0.00 0.05
50 3.1481 0.00 -0.05 0.00 0.09
51 3.1481 0.00 0.03 0.00 -0.02
52 6.2034 0.00 -0.01 0.00 0.16
53 6.2036 0.00 -0.06 0.00 -0.17
54 6.2037 0.00 0.13 0.00 -0.07
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.
14UU240 quality flag:3 Type: 1:1 1:1 1:1 axisobj 30.239 30.239 30.239 ecceobj 0.044 0.044 0.044 incobj 35.730 35.730 35.730 qmin 28.102 28.102 28.102 qmax 32.183 32.183 32.183 amean 30.108 30.108 30.108 amin 29.908 29.908 29.908 amax 30.320 30.320 30.320 emean 0.033 0.033 0.033 emin 0.002 0.002 0.002 emax 0.062 0.062 0.062 imean 34.359 34.359 34.359 imin 34.134 34.134 34.134 imax 34.578 34.578 34.578 excite_mean 0.566 0.566 0.566 fracstop 1.000 1.000 1.000 cjmean 2.651 2.651 2.651 libcent 0 57.6 57.6 57.6 libamp 0 4.4 4.4 4.4 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 173.9 174.0 174.0 kozaiamp 180.0 180.0 180.0