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: 03SO317
# Created Fri Nov 22 02:08:30 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 39 observations of 39
# Arc: 20.06y
# First observation: 2001/10/15
# Last observation: 2021/11/05
# Chi-squared of fit: 176.16 DOF: 72 RMS: 0.38
# Min/Max residuals: -0.98 0.83
# Exact a, adot, b, bdot, g, gdot:
1.921515E-05 3.837712E-02 -1.033641E-06 -4.343810E-03 3.234083E-02 7.458900E-03
# Covariance matrix:
2.3301E-13 -8.4311E-14 -1.9728E-14 9.0077E-15 4.9194E-15 -9.9572E-14
-8.4311E-14 4.4953E-14 1.1247E-14 -5.1430E-15 -4.1406E-14 5.7125E-14
-1.9728E-14 1.1247E-14 7.0586E-14 -7.4064E-15 -1.1851E-14 1.4766E-14
9.0077E-15 -5.1430E-15 -7.4064E-15 1.9097E-15 5.4571E-15 -6.7540E-15
4.9194E-15 -4.1406E-14 -1.1851E-14 5.4571E-15 2.3041E-13 -6.1937E-14
-9.9572E-14 5.7125E-14 1.4766E-14 -6.7540E-15 -6.1937E-14 7.5072E-14
# lat0 lon0 xBary yBary zBary JD0
1.066503 -2.472419 -0.407253 0.016749 -0.905544 2452197.804970
# Heliocentric elements and errors
Epoch: 2452198.5000 = 2001/10/16
Mean Anomaly: 34.40135 +/- 0.006
Argument of Peri: 112.60955 +/- 0.008
Long of Asc Node: 187.32364 +/- 0.000
Inclination: 6.55686 +/- 0.000
Eccentricity: 0.27431345 +/- 0.0000
Semi-Major Axis: 39.38531049 +/- 0.0035
Time of Perihelion: 2443571.2411 +/- 2.0
Perihelion: 28.58139014 +/- 0.0031
Aphelion: 50.18923083 +/- 0.0048
Period (y) 247.1779 +/- 0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X 31.81118917 +/- 0.0005
Ecliptic Y -0.95966349 +/- 0.0000
Ecliptic Z 0.57550155 +/- 0.0000
Ecliptic XDOT 0.00076906 +/- 0.0000
Ecliptic YDOT 0.00321894 +/- 0.0000
Ecliptic ZDOT -0.00035570 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 31.83074587 +/- 0.0005
Geocenter to KBO 30.92059091 +/- 0.0005
# Hcoef: 8.07
The following table shows the complete astrometric record for 03SO317. 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 (03SO317) followed by the observatory code and reference code for the source of the astrometry.
2001 10 15.304227 23 49 13.80 -00 00 16.4 22.7V 03SO317 645 C~1SKv 2001 10 15.305056 23 49 13.79 -00 00 16.5 22.7V 03SO317 645 C~1SKv 2001 10 15.306744 23 49 13.78 -00 00 16.6 23.7V 03SO317 645 C~1SKv 2003 09 25.39506 00 07 44.12 +01 28 48.7 03SO317 568 Cq9897 2003 09 25.44253 00 07 43.86 +01 28 46.7 03SO317 568 Cq9897 2003 09 25.51444 00 07 43.44 +01 28 44.0 03SO317 568 Cq9897 2003 09 27.35364 00 07 33.24 +01 27 32.1 22.6g 03SO317 568 Cq9897 2003 09 27.40595 00 07 32.92 +01 27 30.1 23.2g 03SO317 568 Cq9897 2003 09 27.45116 00 07 32.68 +01 27 28.2 23.9g 03SO317 568 Cq9897 2003 11 16.162647 00 03 44.63 +01 00 09.2 22.8V 03SO317 645 C~2Jx9 2003 11 16.163476 00 03 44.63 +01 00 09.2 24.0V 03SO317 645 C~2Jx9 2003 11 16.165964 00 03 44.63 +01 00 08.8 23.7V 03SO317 645 C~2Jx9 2004 09 11.31269 00 17 04.97 +02 14 07.7 03SO317 695 Cq9897 2004 09 11.35860 00 17 04.74 +02 14 05.9 03SO317 695 Cq9897 2004 09 11.40376 00 17 04.51 +02 14 04.3 03SO317 695 Cq9897 2004 09 12.35963 00 16 59.45 +02 13 29.1 03SO317 695 Cq9897 2004 09 12.38585 00 16 59.30 +02 13 28.2 03SO317 695 Cq9897 2004 09 12.41210 00 16 59.14 +02 13 27.3 03SO317 695 Cq9897 2004 09 16.33136 00 16 38.11 +02 11 00.6 03SO317 675 Cq9897 2004 09 16.37340 00 16 37.86 +02 10 59.1 03SO317 675 Cq9897 2004 09 16.42405 00 16 37.59 +02 10 57.3 03SO317 675 Cq9897 2004 09 17.31251 00 16 32.78 +02 10 23.4 03SO317 675 Cq9897 2004 09 17.37539 00 16 32.44 +02 10 21.1 03SO317 675 Cq9897 2004 09 21.40952 00 16 10.38 +02 07 49.6 23.5r 03SO317 568 Cq9897 2004 09 21.44066 00 16 10.19 +02 07 48.3 23.5r 03SO317 568 Cq9897 2004 09 21.46948 00 16 10.04 +02 07 47.2 23.3r 03SO317 568 Cq9897 2004 09 22.41446 00 16 04.82 +02 07 10.3 23.6r 03SO317 568 Cq9897 2004 12 03.24625 00 11 10.51 +01 31 54.0 23.4i 03SO317 568 Cq9897 2004 12 03.29858 00 11 10.44 +01 31 53.3 23.6i 03SO317 568 Cq9897 2005 07 08.55589 00 28 10.23 +03 12 36.4 22.8r 03SO317 568 Cq9897 2005 07 08.61960 00 28 10.24 +03 12 36.4 22.5r 03SO317 568 Cq9897 2005 07 09.44999 00 28 10.43 +03 12 35.5 03SO317 675 Cq9897 2005 07 09.58999 00 28 10.39 +03 12 36.2 22.7r 03SO317 568 Cq9897 2005 07 10.46001 00 28 10.55 +03 12 34.0 03SO317 675 Cq9897 2014 09 27.43424 01 30 37.15 +07 29 22.8 23.8R 03SO317 695 C~1LJE 2014 09 27.48817 01 30 36.88 +07 29 21.1 03SO317 695 C~1LJE 2021 11 05.248730 02 13 32.060 +10 06 19.33 22.8G 03SO317 G37 C~5B75 2021 11 05.303720 02 13 31.763 +10 06 17.53 03SO317 G37 C~5B75 2021 11 05.363380 02 13 31.431 +10 06 15.94 03SO317 G37 C~5B75
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 0.00 0.00 -0.24
2 0.0000 0.00 -0.08 0.00 -0.31
3 0.0000 0.00 -0.11 0.00 -0.35
4 1.9441 0.00 0.09 0.00 0.55
5 1.9443 0.00 0.24 0.00 0.39
6 1.9444 0.00 0.06 0.00 0.48
7 1.9495 0.00 0.40 0.00 0.00
8 1.9496 0.00 0.05 0.00 0.03
9 1.9498 0.00 0.30 0.00 -0.11
10 2.0859 0.00 -0.20 0.00 -0.27
11 2.0859 0.00 -0.16 0.00 -0.26
12 2.0859 0.00 -0.05 0.00 -0.60
13 2.9076 0.00 -0.34 0.00 0.07
14 2.9077 0.00 -0.09 0.00 -0.05
15 2.9079 0.00 0.11 0.00 0.00
16 2.9105 0.00 0.13 0.00 -0.10
17 2.9106 0.00 0.00 0.00 -0.03
18 2.9106 0.00 -0.27 0.00 0.04
19 2.9214 0.00 -0.05 0.00 -0.73
20 2.9215 0.00 -0.32 0.00 -0.65
21 2.9216 0.00 -0.18 0.00 -0.55
22 2.9240 0.00 -0.07 0.00 -0.98
23 2.9242 0.00 0.05 0.00 -0.91
24 2.9353 0.00 0.56 0.00 0.82
25 2.9353 0.00 0.33 0.00 0.71
26 2.9354 0.00 0.51 0.00 0.71
27 2.9380 0.00 0.26 0.00 -0.04
28 3.1347 0.00 -0.04 0.00 0.83
29 3.1348 0.00 -0.09 0.00 0.69
30 3.7296 0.00 -0.08 0.00 0.09
31 3.7298 0.00 -0.09 0.00 0.12
32 3.7321 0.00 0.06 0.00 -0.03
33 3.7325 0.00 -0.85 0.00 0.77
34 3.7349 0.00 0.19 0.00 -0.04
35 12.9504 0.00 -0.15 0.00 0.31
36 12.9505 0.00 -0.15 0.00 0.35
37 20.0573 0.00 0.24 0.00 -0.07
38 20.0575 0.00 0.13 0.00 -0.34
39 20.0577 0.00 -0.14 0.00 -0.26
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.
03SO317 quality flag:3 Type: 3:2E 3:2E 3:2E axisobj 39.648 39.649 39.648 ecceobj 0.278 0.278 0.278 incobj 6.547 6.547 6.547 qmin 27.952 27.954 27.946 qmax 51.672 51.620 51.643 amean 39.455 39.455 39.455 amin 38.950 38.954 38.943 amax 40.033 40.067 40.041 emean 0.275 0.275 0.275 emin 0.259 0.259 0.259 emax 0.292 0.291 0.291 imean 7.157 7.159 7.157 imin 6.453 6.453 6.453 imax 7.876 7.874 7.870 excite_mean 0.302 0.302 0.302 fracstop 1.000 1.000 1.000 cjmean 2.947 2.947 2.947 libcent 0 179.5 180.1 180.3 libamp 0 99.2 99.2 99.8 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 182.7 182.6 182.4 kozaiamp 180.0 180.0 180.0