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: 15KT175
# Created Wed Jul 17 01:10:57 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 40 observations of 40
# Arc: 9.93y
# First observation: 2014/05/29
# Last observation: 2024/05/04
# Chi-squared of fit: 6.99 DOF: 74 RMS: 0.07
# Min/Max residuals: -0.23 0.19
# Exact a, adot, b, bdot, g, gdot:
1.545084E-05 2.303763E-02 -1.264477E-06 -1.829739E-03 2.366058E-02 1.039570E-03
# Covariance matrix:
1.9871E-13 -1.5974E-13 -1.0688E-14 1.1297E-14 -1.8043E-14 -5.8628E-13
-1.5974E-13 1.6461E-13 1.1007E-14 -1.1984E-14 3.2823E-15 6.2358E-13
-1.0688E-14 1.1007E-14 5.8734E-14 -1.2282E-14 3.2001E-15 4.3787E-14
1.1297E-14 -1.1984E-14 -1.2282E-14 7.1832E-15 -8.1088E-16 -4.7282E-14
-1.8043E-14 3.2823E-15 3.2001E-15 -8.1088E-16 1.1774E-13 3.0246E-14
-5.8628E-13 6.2358E-13 4.3787E-14 -4.7282E-14 3.0246E-14 2.4585E-12
# lat0 lon0 xBary yBary zBary JD0
5.597263 -127.961334 -0.276231 0.095275 -0.971589 2456806.847808
# Heliocentric elements and errors
Epoch: 2456806.5000 = 2014/05/29
Mean Anomaly: 46.47944 +/- 0.027
Argument of Peri: 77.14092 +/- 0.032
Long of Asc Node: 102.33744 +/- 0.001
Inclination: 7.13357 +/- 0.000
Eccentricity: 0.07052673 +/- 0.0001
Semi-Major Axis: 45.30962753 +/- 0.0034
Time of Perihelion: 2442423.7305 +/- 8.5
Perihelion: 42.11408750 +/- 0.0049
Aphelion: 48.50516757 +/- 0.0052
Period (y) 304.9959 +/- 0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -26.25816944 +/- 0.0004
Ecliptic Y -34.10167237 +/- 0.0005
Ecliptic Z 4.12227588 +/- 0.0001
Ecliptic XDOT 0.00201016 +/- 0.0000
Ecliptic YDOT -0.00175410 +/- 0.0000
Ecliptic ZDOT -0.00019886 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 43.23662400 +/- 0.0004
Geocenter to KBO 42.26440517 +/- 0.0006
# Hcoef: 7.54
The following table shows the complete astrometric record for 15KT175. 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 (15KT175) followed by the observatory code and reference code for the source of the astrometry.
2014 05 29.34703 15 24 24.102 -12 51 49.98 23.8r 15KT175 568 C~2nvi 2014 05 29.38590 15 24 23.920 -12 51 49.56 23.8r 15KT175 568 C~2nvi 2014 05 29.42474 15 24 23.747 -12 51 48.90 24.0r 15KT175 568 C~2nvi 2014 05 31.37090 15 24 15.070 -12 51 22.63 23.9r 15KT175 568 C~2nvi 2014 07 19.26644 15 21 37.462 -12 46 28.27 23.9r 15KT175 568 C~2nvi 2015 02 20.65258 15 34 35.864 -13 40 48.95 23.7r 15KT175 568 C~2nvi 2015 03 19.56666 15 34 12.038 -13 36 29.74 23.6r 15KT175 568 C~2nvi 2015 04 12.48402 15 33 01.177 -13 30 24.95 23.8r 15KT175 568 C~2nvi 2015 04 12.52502 15 33 01.017 -13 30 24.53 24.0r 15KT175 568 C~2nvi 2015 04 18.50669 15 32 37.745 -13 28 42.70 23.9r 15KT175 568 C~2nvi 2015 05 17.37425 15 30 28.805 -13 20 35.48 23.6r 15KT175 568 C~2nvi 2015 05 17.37924 15 30 28.767 -13 20 35.42 23.5r 15KT175 568 C~2nvi 2015 05 17.42094 15 30 28.571 -13 20 34.72 23.4r 15KT175 568 C~2nvi 2015 05 17.46306 15 30 28.366 -13 20 34.09 23.6r 15KT175 568 C~2nvi 2015 05 24.36500 15 29 56.263 -13 18 49.31 23.7r 15KT175 568 C~2nvi 2015 05 24.41125 15 29 56.046 -13 18 48.66 23.7r 15KT175 568 C~2nvi 2015 05 24.45211 15 29 55.853 -13 18 48.03 23.8r 15KT175 568 C~2nvi 2015 05 26.43973 15 29 46.709 -13 18 19.50 23.6r 15KT175 568 C~2nvi 2015 06 18.33918 15 28 09.254 -13 13 54.51 23.9r 15KT175 568 C~2nvi 2015 06 18.38024 15 28 09.094 -13 13 54.23 24.0r 15KT175 568 C~2nvi 2015 06 21.35487 15 27 58.037 -13 13 30.26 23.8r 15KT175 568 C~2nvi 2015 07 10.38689 15 27 00.149 -13 12 03.98 23.6r 15KT175 568 C~2nvi 2015 07 15.31053 15 26 49.342 -13 12 02.02 23.9r 15KT175 568 C~2nvi 2015 07 17.34121 15 26 45.408 -13 12 03.57 23.8r 15KT175 568 C~2nvi 2015 07 18.31267 15 26 43.675 -13 12 05.08 23.9r 15KT175 568 C~2nvi 2015 08 11.33945 15 26 26.062 -13 14 25.53 24.3r 15KT175 568 C~2nvi 2016 02 05.64298 15 39 20.647 -14 05 52.29 24.2w 15KT175 568 C~2nvi 2016 03 15.58610 15 39 24.317 -14 01 50.71 24.4w 15KT175 568 C~2nvi 2016 03 17.60533 15 39 20.695 -14 01 26.74 24.4w 15KT175 568 C~2nvi 2016 04 03.53855 15 38 37.600 -13 57 32.33 24.3w 15KT175 568 C~2nvi 2016 04 08.58811 15 38 20.762 -13 56 13.61 24.2w 15KT175 568 C~2nvi 2016 04 29.46970 15 36 56.935 -13 50 29.35 24.2w 15KT175 568 C~2nvi 2016 05 04.40478 15 36 34.756 -13 49 07.49 24.0w 15KT175 568 C~2nvi 2016 05 30.47820 15 34 33.924 -13 42 34.23 23.9w 15KT175 568 C~2nvi 2016 07 04.28603 15 32 20.465 -13 37 35.77 23.9w 15KT175 568 C~2nvi 2016 07 05.35431 15 32 17.436 -13 37 32.24 24.9w 15KT175 568 C~2nvi 2016 07 05.37863 15 32 17.359 -13 37 32.21 24.1w 15KT175 568 C~2nvi 2024 05 04.365800 16 17 59.767 -16 52 31.95 24.0G 15KT175 G37 C~82mo 2024 05 04.400950 16 17 59.603 -16 52 31.74 15KT175 G37 C~82mo 2024 05 04.435400 16 17 59.464 -16 52 31.12 15KT175 G37 C~82mo
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 -0.01 0.00 0.01
2 0.0001 0.00 -0.07 0.00 -0.10
3 0.0002 0.00 -0.01 0.00 0.02
4 0.0055 0.00 0.04 0.00 -0.04
5 0.1394 0.00 0.01 0.00 -0.07
6 0.7318 0.00 0.03 0.00 -0.05
7 0.8055 0.00 0.06 0.00 0.03
8 0.8710 0.00 -0.03 0.00 0.16
9 0.8711 0.00 -0.08 0.00 -0.11
10 0.8875 0.00 -0.04 0.00 0.03
11 0.9665 0.00 0.19 0.00 -0.01
12 0.9665 0.00 -0.02 0.00 -0.03
13 0.9667 0.00 0.02 0.00 0.02
14 0.9668 0.00 -0.05 0.00 -0.02
15 0.9857 0.00 -0.01 0.00 0.04
16 0.9858 0.00 0.00 0.00 0.02
17 0.9859 0.00 -0.01 0.00 0.05
18 0.9914 0.00 0.01 0.00 -0.02
19 1.0541 0.00 0.03 0.00 0.06
20 1.0542 0.00 0.02 0.00 -0.01
21 1.0623 0.00 -0.04 0.00 -0.05
22 1.1144 0.00 0.05 0.00 0.14
23 1.1279 0.00 0.16 0.00 0.04
24 1.1335 0.00 -0.23 0.00 0.16
25 1.1361 0.00 0.00 0.00 -0.02
26 1.2019 0.00 0.01 0.00 0.01
27 1.6901 0.00 0.06 0.00 -0.07
28 1.7967 0.00 -0.11 0.00 0.12
29 1.8022 0.00 -0.14 0.00 -0.08
30 1.8486 0.00 0.04 0.00 -0.14
31 1.8624 0.00 -0.03 0.00 -0.01
32 1.9196 0.00 0.01 0.00 -0.06
33 1.9331 0.00 0.08 0.00 -0.10
34 2.0045 0.00 0.02 0.00 0.05
35 2.0998 0.00 -0.02 0.00 -0.01
36 2.1027 0.00 0.05 0.00 0.08
37 2.1028 0.00 -0.06 0.00 0.03
38 9.9330 0.00 0.03 0.00 0.07
39 9.9331 0.00 -0.10 0.00 -0.14
40 9.9332 0.00 0.09 0.00 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.
15KT175 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 45.014 45.014 45.014 ecceobj 0.064 0.064 0.064 incobj 7.129 7.129 7.129 qmin 41.589 41.599 41.581 qmax 49.366 49.367 49.376 amean 45.363 45.363 45.363 amin 45.004 45.005 45.003 amax 45.743 45.746 45.743 emean 0.067 0.067 0.067 emin 0.054 0.054 0.054 emax 0.080 0.079 0.080 imean 5.455 5.455 5.455 imin 5.061 5.061 5.061 imax 5.907 5.908 5.907 excite_mean 0.116 0.116 0.116 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 178.9 178.8 178.9 kozaiamp 180.0 179.9 180.0