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: 501105 # Created Fri Apr 26 01:08:09 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 53 observations of 53 # Arc: 3.83y # First observation: 2013/09/23 # Last observation: 2017/07/25 # Chi-squared of fit: 247.27 DOF: 100 RMS: 0.38 # Min/Max residuals: -1.53 1.02 # Exact a, adot, b, bdot, g, gdot: 1.715750E-05 2.166566E-02 -3.957571E-06 -1.705289E-02 2.642088E-02 3.913732E-04 # Covariance matrix: 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 # lat0 lon0 xBary yBary zBary JD0 16.129183 8.757550 0.140062 0.276120 -0.954627 2456559.452558 # Heliocentric elements and errors Epoch: 2456558.5000 = 2013/09/23 Mean Anomaly: 10.34445 +/- 0.000 Argument of Peri: 143.54004 +/- 0.000 Long of Asc Node: 207.60009 +/- 0.000 Inclination: 40.77145 +/- 0.000 Eccentricity: 0.07090282 +/- 0.0000 Semi-Major Axis: 41.70617473 +/- 0.0000 Time of Perihelion: 2453731.6433 +/- 0.0 Perihelion: 38.74908938 +/- 0.0000 Aphelion: 44.66326008 +/- 0.0000 Period (y) 269.3449 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 36.93820941 +/- 0.0000 Ecliptic Y 5.55177198 +/- 0.0000 Ecliptic Z 10.51444585 +/- 0.0000 Ecliptic XDOT 0.00017569 +/- 0.0000 Ecliptic YDOT 0.00229832 +/- 0.0000 Ecliptic ZDOT -0.00168614 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 38.80472131 +/- 0.0000 Geocenter to KBO 37.84888555 +/- 0.0000 # Hcoef: 7.10
The following table shows the complete astrometric record for 501105. 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 (501105) followed by the observatory code and reference code for the source of the astrometry.
2013 09 23.95178 00 05 43.00 +18 14 37.3 22.5R 501105 G36 C~0x7u 2013 09 24.09661 00 05 42.26 +18 14 32.8 21.8R 501105 G36 C~0x7u 2013 09 24.11598 00 05 42.21 +18 14 31.9 21.8R 501105 G36 C~0x7u 2013 09 24.12570 00 05 42.17 +18 14 32.0 22.3R 501105 G36 C~0x7u 2013 09 24.17192 00 05 41.89 +18 14 30.2 22.0R 501105 G36 C~0x7u 2013 09 24.83418 00 05 38.72 +18 14 03.8 22.0R 501105 G36 C~0x7u 2013 09 24.85478 00 05 38.59 +18 14 02.5 22.9R 501105 G36 C~0x7u 2013 09 24.86674 00 05 38.52 +18 14 03.3 22.3R 501105 G36 C~0x7u 2013 09 24.93214 00 05 38.14 +18 14 00.5 22.5R 501105 G36 C~0x7u 2013 09 24.95088 00 05 38.06 +18 13 59.8 22.7R 501105 G36 C~0x7u 2013 09 25.00686 00 05 37.77 +18 13 57.3 22.7R 501105 G36 C~0x7u 2013 09 25.02554 00 05 37.66 +18 13 56.6 22.6R 501105 G36 C~0x7u 2013 09 25.86715 00 05 33.56 +18 13 23.2 22.7R 501105 G36 C~0x7u 2013 09 25.88277 00 05 33.44 +18 13 22.4 22.9R 501105 G36 C~0x7u 2013 09 25.89837 00 05 33.35 +18 13 21.6 22.5R 501105 G36 C~0x7u 2013 09 25.91745 00 05 33.28 +18 13 20.9 22.7R 501105 G36 C~0x7u 2013 09 25.93651 00 05 33.15 +18 13 19.8 23.1R 501105 G36 C~0x7u 2013 09 25.99362 00 05 32.86 +18 13 17.8 22.8R 501105 G36 C~0x7u 2013 09 26.01261 00 05 32.79 +18 13 17.3 23.2R 501105 G36 C~0x7u 2013 09 26.05065 00 05 32.65 +18 13 15.0 22.4R 501105 G36 C~0x7u 2013 09 26.06964 00 05 32.51 +18 13 13.9 23.0R 501105 G36 C~0x7u 2013 09 30.83801 00 05 08.95 +18 09 57.5 23.4R 501105 G36 C~0x7u 2013 09 30.86938 00 05 08.81 +18 09 55.9 23.7R 501105 G36 C~0x7u 2013 10 01.11980 00 05 07.55 +18 09 45.3 22.8R 501105 G36 C~0x7u 2013 11 06.77214 00 02 30.68 +17 40 51.9 501105 G36 C~0x7u 2013 11 06.78653 00 02 30.66 +17 40 51.2 501105 G36 C~0x7u 2013 11 06.80517 00 02 30.54 +17 40 50.1 501105 G36 C~0x7u 2013 11 06.83485 00 02 30.47 +17 40 48.9 501105 G36 C~0x7u 2014 08 25.01918 00 14 28.50 +18 06 47.1 501105 G36 C~1EHp 2014 08 25.03165 00 14 28.42 +18 06 46.6 501105 G36 C~1EHp 2014 08 25.06040 00 14 28.32 +18 06 46.1 501105 G36 C~1EHp 2014 08 25.09370 00 14 28.16 +18 06 45.3 501105 G36 C~1EHp 2014 08 25.12320 00 14 28.05 +18 06 44.7 501105 G36 C~1EHp 2014 10 22.16928 00 09 56.20 +17 31 13.7 22.3R 501105 G37 C~1EHp 2014 10 22.27617 00 09 55.72 +17 31 08.7 501105 G37 C~1EHp 2014 11 17.78664 00 08 22.50 +17 10 00.0 501105 G36 C~1EHp 2014 11 17.81216 00 08 22.42 +17 09 58.6 501105 G36 C~1EHp 2014 11 17.87366 00 08 22.26 +17 09 55.6 501105 G36 C~1EHp 2015 11 07.85156 00 15 14.16 +16 54 49.1 501105 G36 C~1ddc 2015 11 07.86290 00 15 14.16 +16 54 48.8 501105 G36 C~1ddc 2015 11 07.88528 00 15 14.06 +16 54 47.8 501105 G36 C~1ddc 2015 11 07.89647 00 15 13.99 +16 54 47.4 501105 G36 C~1ddc 2015 11 07.94231 00 15 13.84 +16 54 45.2 501105 G36 C~1ddc 2015 11 09.82574 00 15 07.50 +16 53 16.4 501105 G36 C~1ddc 2015 11 09.83761 00 15 07.40 +16 53 15.5 501105 G36 C~1ddc 2016 10 29.91618 00 22 05.24 +16 37 12.8 501105 G36 C~20qm 2016 10 29.94569 00 22 05.15 +16 37 12.1 501105 G36 C~20qm 2017 07 24.10485 00 34 47.36 +16 57 40.1 501105 G36 C~2IXz 2017 07 24.14587 00 34 47.32 +16 57 40.5 501105 G36 C~2IXz 2017 07 25.02289 00 34 46.18 +16 57 42.5 501105 G36 C~2IXz 2017 07 25.11438 00 34 46.09 +16 57 42.6 501105 G36 C~2IXz 2017 07 25.13250 00 34 46.08 +16 57 42.3 501105 G36 C~2IXz 2017 07 25.15065 00 34 46.10 +16 57 42.6 501105 G36 C~2IXz
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 -0.27 0.00 -1.53
2 0.0004 0.00 -0.43 0.00 -0.34
3 0.0004 0.00 0.28 0.00 -0.47
4 0.0005 0.00 0.41 0.00 0.01
5 0.0006 0.00 -0.32 0.00 0.04
6 0.0024 0.00 1.02 0.00 -0.20
7 0.0025 0.00 0.62 0.00 -0.69
8 0.0025 0.00 0.47 0.00 0.58
9 0.0027 0.00 -0.30 0.00 0.36
10 0.0027 0.00 -0.09 0.00 0.40
11 0.0029 0.00 -0.21 0.00 0.12
12 0.0029 0.00 -0.45 0.00 0.16
13 0.0052 0.00 0.44 0.00 0.41
14 0.0053 0.00 -0.18 0.00 0.24
15 0.0053 0.00 -0.36 0.00 0.06
16 0.0054 0.00 0.03 0.00 0.12
17 0.0054 0.00 -0.48 0.00 -0.21
18 0.0056 0.00 -0.52 0.00 0.08
19 0.0056 0.00 -0.14 0.00 0.34
20 0.0057 0.00 0.64 0.00 -0.42
21 0.0058 0.00 -0.03 0.00 -0.76
22 0.0189 0.00 -0.19 0.00 0.15
23 0.0189 0.00 0.06 0.00 -0.13
24 0.0196 0.00 -0.09 0.00 -0.08
25 0.1200 0.00 -0.02 0.00 -0.02
26 0.1200 0.00 0.40 0.00 -0.02
27 0.1201 0.00 -0.47 0.00 -0.21
28 0.1201 0.00 -0.04 0.00 0.04
29 0.9174 0.00 0.44 0.00 0.36
30 0.9174 0.00 0.00 0.00 0.11
31 0.9175 0.00 0.26 0.00 0.18
32 0.9176 0.00 -0.09 0.00 0.04
33 0.9176 0.00 0.07 0.00 0.03
34 1.0766 0.00 -0.10 0.00 0.45
35 1.0769 0.00 -0.21 0.00 0.56
36 1.1494 0.00 0.06 0.00 0.38
37 1.1495 0.00 -0.14 0.00 0.15
38 1.1497 0.00 -0.14 0.00 -0.00
39 2.1216 0.00 -0.09 0.00 -0.10
40 2.1216 0.00 0.51 0.00 0.14
41 2.1217 0.00 0.20 0.00 0.20
42 2.1217 0.00 -0.25 0.00 0.33
43 2.1218 0.00 -0.07 0.00 0.30
44 2.1270 0.00 0.53 0.00 0.34
45 2.1270 0.00 -0.37 0.00 0.00
46 3.0991 0.00 -0.27 0.00 -1.00
47 3.0992 0.00 0.22 0.00 -0.32
48 3.8307 0.00 0.39 0.00 -0.57
49 3.8308 0.00 0.55 0.00 -0.26
50 3.8332 0.00 -0.87 0.00 0.29
51 3.8334 0.00 -0.43 0.00 0.25
52 3.8335 0.00 -0.22 0.00 -0.08
53 3.8335 0.00 0.44 0.00 0.19
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.
501105 quality flag:3 Type: SCATEXTD SCATEXTD SCATEXTD axisobj 41.900 41.900 41.900 ecceobj 0.076 0.076 0.076 incobj 40.707 40.707 40.707 qmin 38.110 38.111 38.109 qmax 45.578 45.577 45.577 amean 41.736 41.736 41.736 amin 41.427 41.427 41.428 amax 42.082 42.082 42.081 emean 0.071 0.071 0.071 emin 0.060 0.060 0.060 emax 0.083 0.083 0.083 imean 41.188 41.188 41.188 imin 40.949 40.949 40.948 imax 41.420 41.421 41.420 excite_mean 0.662 0.662 0.662 fracstop 1.000 1.000 1.000 cjmean 2.488 2.488 2.488 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 193.6 193.5 193.6 kozaiamp 179.9 179.9 179.9