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: 05EE296
# Created Sun Dec 22 02:08:48 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 39 observations of 39
# Arc: 14.90y
# First observation: 2005/02/10
# Last observation: 2020/01/04
# Chi-squared of fit: 230.35 DOF: 72 RMS: 0.43
# Min/Max residuals: -1.17 1.58
# Exact a, adot, b, bdot, g, gdot:
1.312104E-05 1.992862E-02 -1.080608E-06 -1.046443E-03 2.211952E-02 -1.047863E-03
# Covariance matrix:
8.8731E-14 -3.5290E-14 -7.6602E-16 1.3432E-15 5.0816E-14 -8.9015E-14
-3.5290E-14 3.5864E-14 1.2536E-15 -1.6549E-15 -9.3993E-15 1.0842E-13
-7.6602E-16 1.2536E-15 5.0871E-14 -5.9532E-15 9.1021E-16 4.3414E-15
1.3432E-15 -1.6549E-15 -5.9532E-15 2.9293E-15 -5.6614E-19 -5.5177E-15
5.0816E-14 -9.3993E-15 9.1021E-16 -5.6614E-19 1.5620E-13 -3.6103E-15
-8.9015E-14 1.0842E-13 4.3414E-15 -5.5177E-15 -3.6103E-15 3.6086E-13
# lat0 lon0 xBary yBary zBary JD0
1.376277 137.830327 -0.061938 0.023690 -0.981304 2453411.813023
# Heliocentric elements and errors
Epoch: 2453412.5000 = 2005/02/11
Mean Anomaly: 235.45763 +/- 0.044
Argument of Peri: 286.32538 +/- 0.037
Long of Asc Node: 342.07989 +/- 0.001
Inclination: 3.28669 +/- 0.000
Eccentricity: 0.06651695 +/- 0.0000
Semi-Major Axis: 44.39320585 +/- 0.0031
Time of Perihelion: 2490788.0699 +/- 15.1
Perihelion: 41.44030505 +/- 0.0036
Aphelion: 47.34610665 +/- 0.0039
Period (y) 295.7896 +/- 0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -34.27120010 +/- 0.0006
Ecliptic Y 30.95392081 +/- 0.0005
Ecliptic Z 1.08578344 +/- 0.0000
Ecliptic XDOT -0.00156233 +/- 0.0000
Ecliptic YDOT -0.00192034 +/- 0.0000
Ecliptic ZDOT -0.00013253 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 46.19353247 +/- 0.0006
Geocenter to KBO 45.20900603 +/- 0.0008
# Hcoef: 6.64
The following table shows the complete astrometric record for 05EE296. 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 (05EE296) followed by the observatory code and reference code for the source of the astrometry.
2005 02 10.31228 09 22 50.86 +16 47 52.8 24.1g 05EE296 568 C~0VE0 2005 02 10.39529 09 22 50.47 +16 47 54.6 23.8g 05EE296 568 C~0VE0 2005 02 10.43481 09 22 50.29 +16 47 55.3 23.8g 05EE296 568 C~0VE0 2005 03 09.24209 09 20 56.19 +16 56 11.2 22.8R 05EE296 695 Cn0309 2005 03 09.33149 09 20 55.85 +16 56 12.6 05EE296 695 Cn0309 2005 03 10.24246 09 20 52.42 +16 56 26.9 05EE296 695 Cn0309 2005 03 12.195455 09 20 45.18 +16 56 56.8 22.7V 05EE296 645 C~2JxC 2005 03 12.196285 09 20 45.18 +16 56 56.8 22.7V 05EE296 645 C~2JxC 2005 03 12.198772 09 20 45.18 +16 56 56.8 23.7V 05EE296 645 C~2JxC 2005 04 10.15339 09 19 25.92 +17 02 02.2 22.8R 05EE296 695 Cn3133 2005 04 11.15418 09 19 24.26 +17 02 07.2 05EE296 695 Cn3133 2005 04 12.15323 09 19 22.73 +17 02 12.1 05EE296 695 Cn3133 2005 04 12.26136 09 19 22.54 +17 02 13.0 23.4i 05EE296 568 C~0VE0 2005 04 12.34223 09 19 22.42 +17 02 13.5 23.7i 05EE296 568 C~0VE0 2005 04 12.36980 09 19 22.38 +17 02 13.8 23.6i 05EE296 568 C~0VE0 2005 04 13.16365 09 19 21.20 +17 02 16.9 05EE296 695 Cn3133 2006 02 03.47735 09 27 50.77 +16 20 39.6 05EE296 568 C74769 2006 02 06.32831 09 27 37.89 +16 21 39.0 22.9r 05EE296 568 C74769 2006 02 06.36908 09 27 37.73 +16 21 39.9 22.5r 05EE296 568 C74769 2006 02 06.40731 09 27 37.55 +16 21 40.7 23.0r 05EE296 568 C74769 2006 03 02.22794 09 25 52.64 +16 29 34.0 22.8R 05EE296 695 Cr3594 2006 03 02.28430 09 25 52.39 +16 29 34.9 05EE296 695 Cr3594 2006 03 02.34040 09 25 52.16 +16 29 36.1 05EE296 695 Cr3594 2006 04 26.01108 09 23 33.45 +16 38 38.5 21.7R 05EE296 807 Cr3594 2006 04 28.01271 09 23 32.64 +16 38 37.1 05EE296 807 Cr3594 2006 11 23.51542 09 35 40.62 +15 38 21.5 05EE296 695 C~0VE0 2006 11 25.47075 09 35 40.11 +15 38 26.1 05EE296 695 C~0VE0 2006 12 21.37965 09 35 02.50 +15 41 55.9 22.5R 05EE296 695 Ct5520 2006 12 21.52007 09 35 02.13 +15 41 57.7 05EE296 695 Ct5520 2007 02 18.30702 09 31 12.15 +16 00 34.9 05EE296 568 Cu1516 2007 02 18.33757 09 31 12.00 +16 00 35.4 05EE296 568 Cu1516 2007 02 18.34973 09 31 11.94 +16 00 35.7 05EE296 568 Cu1516 2007 02 20.38766 09 31 02.78 +16 01 19.3 23.3R 05EE296 568 Cu1516 2007 02 20.40850 09 31 02.69 +16 01 19.5 23.4R 05EE296 568 Cu1516 2007 02 20.42607 09 31 02.62 +16 01 20.3 23.3R 05EE296 568 Cu1516 2013 03 13.14623 09 56 01.77 +13 30 36.9 22.9R 05EE296 G37 C~0qSZ 2013 03 13.19699 09 56 01.57 +13 30 37.9 05EE296 G37 C~0qSZ 2020 01 04.448160 10 31 04.65 +09 45 50.9 23.4G 05EE296 705 C~3sm7 2020 01 04.513850 10 31 04.48 +09 45 51.8 23.6G 05EE296 705 C~3sm7
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 0.25 0.00 -0.01
2 0.0002 0.00 0.13 0.00 0.09
3 0.0003 0.00 0.16 0.00 -0.01
4 0.0737 0.00 -0.02 0.00 -0.19
5 0.0740 0.00 0.06 0.00 -0.20
6 0.0765 0.00 0.04 0.00 -0.25
7 0.0818 0.00 -0.25 0.00 -0.36
8 0.0818 0.00 -0.20 0.00 -0.37
9 0.0818 0.00 -0.06 0.00 -0.41
10 0.1611 0.00 -0.15 0.00 0.09
11 0.1638 0.00 -0.24 0.00 -0.17
12 0.1666 0.00 0.36 0.00 -0.14
13 0.1669 0.00 -0.03 0.00 0.22
14 0.1671 0.00 0.11 0.00 0.35
15 0.1672 0.00 0.16 0.00 0.53
16 0.1693 0.00 0.01 0.00 0.14
17 0.9806 0.00 0.30 0.00 0.08
18 0.9884 0.00 -0.13 0.00 -0.14
19 0.9885 0.00 0.27 0.00 -0.10
20 0.9886 0.00 0.21 0.00 -0.10
21 1.0538 0.00 0.26 0.00 -0.04
22 1.0540 0.00 0.06 0.00 -0.17
23 1.0541 0.00 0.15 0.00 0.02
24 1.2038 0.00 -0.20 0.00 0.19
25 1.2093 0.00 -0.17 0.00 -0.24
26 1.7829 0.00 -0.21 0.00 -0.00
27 1.7883 0.00 0.00 0.00 -0.20
28 1.8592 0.00 0.01 0.00 -0.36
29 1.8596 0.00 -0.14 0.00 -0.39
30 2.0205 0.00 0.76 0.00 -0.50
31 2.0206 0.00 0.58 0.00 -0.64
32 2.0206 0.00 0.51 0.00 -0.59
33 2.0262 0.00 -1.17 0.00 1.36
34 2.0263 0.00 -1.11 0.00 1.14
35 2.0263 0.00 -0.98 0.00 1.58
36 8.0844 0.00 0.35 0.00 -0.02
37 8.0846 0.00 0.39 0.00 -0.02
38 14.8970 0.00 -0.03 0.00 -0.08
39 14.8972 0.00 -0.19 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.
05EE296 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 44.150 44.150 44.151 ecceobj 0.066 0.066 0.066 incobj 3.300 3.300 3.300 qmin 40.595 40.599 40.593 qmax 48.076 48.078 48.076 amean 44.211 44.211 44.211 amin 43.867 43.865 43.867 amax 44.580 44.580 44.579 emean 0.064 0.064 0.064 emin 0.048 0.048 0.048 emax 0.079 0.079 0.079 imean 4.263 4.263 4.263 imin 3.563 3.563 3.563 imax 4.816 4.816 4.816 excite_mean 0.098 0.098 0.098 fracstop 1.000 1.000 1.000 cjmean 3.092 3.092 3.092 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 182.7 182.7 182.6 kozaiamp 180.0 180.0 180.0