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: 385695 # Created Sat Apr 20 01:07:51 2024 # Orbit generated by ELGB # -->Covariance matrix from a Bernstein fit # Fitting 40 observations of 40 # Arc: 16.16y # First observation: 2003/09/28 # Last observation: 2019/11/27 # Chi-squared of fit: 219.97 DOF: 74 RMS: 0.41 # Min/Max residuals: -1.15 1.05 # Exact a, adot, b, bdot, g, gdot: 1.814598E-05 3.783567E-02 1.164836E-06 -3.380600E-03 3.375633E-02 -1.938188E-03 # 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 -1.289310 3.041973 -0.025639 -0.022575 -1.004315 2452910.799720 # Heliocentric elements and errors Epoch: 2452910.5000 = 2003/09/28 Mean Anomaly: 253.37447 +/- 0.000 Argument of Peri: 306.27163 +/- 0.000 Long of Asc Node: 169.42080 +/- 0.000 Inclination: 5.26013 +/- 0.000 Eccentricity: 0.05503175 +/- 0.0000 Semi-Major Axis: 30.07064637 +/- 0.0000 Time of Perihelion: 2470749.5316 +/- 0.0 Perihelion: 28.41580596 +/- 0.0000 Aphelion: 31.72548678 +/- 0.0000 Period (y) 164.9006 +/- 0.00 # Ecliptic coordinates at JD0 (AU and AU/d) Ecliptic X 30.57361791 +/- 0.0000 Ecliptic Y 1.65454877 +/- 0.0000 Ecliptic Z -0.66651382 +/- 0.0000 Ecliptic XDOT -0.00033090 +/- 0.0000 Ecliptic YDOT 0.00304980 +/- 0.0000 Ecliptic ZDOT -0.00027042 +/- 0.0000 # Distances at JD0 (AU) Heliocenter to KBO 30.62563551 +/- 0.0000 Geocenter to KBO 29.62414146 +/- 0.0000 # Hcoef: 8.50
The following table shows the complete astrometric record for 385695. 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 (385695) followed by the observatory code and reference code for the source of the astrometry.
2003 09 28.298977 00 13 12.86 +00 01 34.8 23.1V 385695 645 C~1SfQ 2003 09 28.299806 00 13 12.85 +00 01 34.8 22.7V 385695 645 C~1SfQ 2003 09 28.302294 00 13 12.84 +00 01 34.7 24.4V 385695 645 C~1SfQ 2005 10 08.09245 00 28 45.27 +01 16 41.8 385695 304 Co7672 2005 10 08.13089 00 28 45.05 +01 16 40.4 22.9R 385695 304 Co7672 2005 10 08.16274 00 28 44.84 +01 16 39.2 22.9R 385695 304 Co7672 2005 10 25.11067 00 27 08.59 +01 06 03.3 385695 304 Co7672 2005 10 25.14367 00 27 08.41 +01 06 01.9 23.0R 385695 304 C56101 2005 11 03.03811 00 26 23.50 +01 01 11.9 385695 304 Cq3855 2005 11 04.03612 00 26 18.80 +01 00 41.4 385695 304 Cq3855 2005 11 04.06612 00 26 18.67 +01 00 40.4 385695 304 Cq3855 2005 11 28.04168 00 24 52.55 +00 51 43.3 385695 304 Cq3855 2005 11 28.09478 00 24 52.40 +00 51 42.7 23.2R 385695 304 Cq3855 2005 11 30.02868 00 24 48.05 +00 51 17.1 385695 304 Cq3855 2005 12 01.14645 00 24 45.72 +00 51 03.4 22.6R 385695 695 Cp9909 2005 12 02.14382 00 24 43.76 +00 50 52.1 385695 695 Cp9909 2005 12 02.18322 00 24 43.68 +00 50 51.6 385695 695 Cp9909 2005 12 24.29398 00 24 31.31 +00 50 07.8 385695 568 Cq3855 2005 12 25.32600 00 24 32.16 +00 50 15.3 385695 568 Cq3855 2005 12 26.34108 00 24 33.16 +00 50 23.7 385695 568 Cq3855 2006 06 01.59826 00 40 52.82 +02 32 01.0 23.3R 385695 568 Cr3926 2006 06 01.61088 00 40 52.87 +02 32 01.6 385695 568 Cr3926 2006 06 02.61517 00 40 57.68 +02 32 27.0 385695 568 Cr3926 2006 11 12.12222 00 34 00.034 +01 37 50.66 23.3R 385695 304 Cs8726 2006 11 13.02638 00 33 56.224 +01 37 27.12 385695 304 Cs8726 2006 11 13.03958 00 33 56.220 +01 37 26.42 385695 304 Cs8726 2007 09 18.41666 00 47 27.83 +02 52 26.0 385695 675 Cy6770 2007 09 18.44556 00 47 27.65 +02 52 24.8 385695 675 Cy6770 2008 06 09.08573 00 57 31.49 +03 53 26.9 25.2R 385695 250 S~06Av 2008 06 09.09198 00 57 31.51 +03 53 27.0 385695 250 S~06Av 2008 06 09.09823 00 57 31.54 +03 53 27.2 385695 250 S~06Av 2008 06 09.10448 00 57 31.57 +03 53 27.3 385695 250 S~06Av 2008 10 03.258190 00 54 21.82 +03 23 09.8 22.7V 385695 645 C~1SfQ 2008 10 03.259019 00 54 21.81 +03 23 09.8 21.8V 385695 645 C~1SfQ 2008 10 03.261507 00 54 21.80 +03 23 09.7 23.1V 385695 645 C~1SfQ 2013 10 05.40535 01 37 08.42 +06 45 02.9 22.9R 385695 695 C~0zdm 2013 10 05.46873 01 37 08.04 +06 45 00.4 385695 695 C~0zdm 2013 10 06.41406 01 37 02.33 +06 44 24.4 385695 695 C~0zdm 2019 11 27.137130 02 25 03.555 +10 04 50.77 23.1G 385695 G37 C~3Tpg 2019 11 27.211930 02 25 03.129 +10 04 48.74 385695 G37 C~3Tpg
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 0.15 0.00 -0.55
2 0.0000 0.00 0.07 0.00 -0.52
3 0.0000 0.00 0.15 0.00 -0.52
4 2.0282 0.00 0.23 0.00 -0.12
5 2.0283 0.00 0.41 0.00 0.01
6 2.0284 0.00 0.15 0.00 0.07
7 2.0748 0.00 0.34 0.00 0.23
8 2.0749 0.00 0.33 0.00 -0.03
9 2.0992 0.00 -0.23 0.00 0.48
10 2.1019 0.00 -0.27 0.00 0.11
11 2.1020 0.00 -0.07 0.00 0.01
12 2.1677 0.00 0.05 0.00 -0.14
13 2.1678 0.00 -0.23 0.00 0.00
14 2.1731 0.00 -0.01 0.00 0.09
15 2.1762 0.00 0.03 0.00 0.22
16 2.1789 0.00 -0.00 0.00 0.18
17 2.1790 0.00 -0.02 0.00 0.11
18 2.2395 0.00 0.20 0.00 0.23
19 2.2424 0.00 -0.57 0.00 0.09
20 2.2452 0.00 -0.85 0.00 0.12
21 2.6757 0.00 0.64 0.00 -0.12
22 2.6757 0.00 0.49 0.00 0.15
23 2.6785 0.00 0.26 0.00 -0.08
24 3.1234 0.00 -0.26 0.00 0.22
25 3.1259 0.00 -0.75 0.00 0.22
26 3.1259 0.00 0.03 0.00 -0.14
27 3.9729 0.00 1.05 0.00 -0.38
28 3.9730 0.00 0.86 0.00 -0.44
29 4.6976 0.00 -1.02 0.00 0.28
30 4.6976 0.00 -1.15 0.00 0.24
31 4.6976 0.00 -1.12 0.00 0.30
32 4.6976 0.00 -1.10 0.00 0.26
33 5.0156 0.00 0.65 0.00 -0.18
34 5.0156 0.00 0.58 0.00 -0.14
35 5.0156 0.00 0.66 0.00 -0.14
36 10.0208 0.00 0.04 0.00 0.21
37 10.0210 0.00 0.14 0.00 0.13
38 10.0236 0.00 -0.10 0.00 0.22
39 16.1638 0.00 0.01 0.00 -0.24
40 16.1640 0.00 0.13 0.00 -0.35
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.
385695 quality flag:3 Type: 1:1 1:1 1:1 axisobj 30.327 30.327 30.327 ecceobj 0.052 0.052 0.052 incobj 5.240 5.240 5.240 qmin 27.781 27.781 27.780 qmax 32.642 32.651 32.634 amean 30.110 30.110 30.110 amin 29.817 29.817 29.817 amax 30.415 30.417 30.418 emean 0.052 0.052 0.052 emin 0.029 0.029 0.029 emax 0.074 0.075 0.074 imean 4.676 4.676 4.676 imin 4.490 4.491 4.490 imax 4.865 4.865 4.865 excite_mean 0.097 0.097 0.097 fracstop 1.000 1.000 1.000 cjmean 2.992 2.992 2.992 libcent 0 62.4 62.4 62.4 libamp 0 18.4 18.4 18.4 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 179.3 179.4 179.3 kozaiamp 180.0 180.0 180.0