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: 06AM98
# Created Sat Apr 20 01:12:32 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 34 observations of 34
# Arc: 15.28y
# First observation: 2003/11/21
# Last observation: 2019/03/02
# Chi-squared of fit: 58.19 DOF: 62 RMS: 0.23
# Min/Max residuals: -0.64 0.66
# Exact a, adot, b, bdot, g, gdot:
1.836116E-05 3.624907E-02 -5.094932E-06 -8.440794E-03 2.761729E-02 5.580729E-03
# Covariance matrix:
5.5117E-13 -1.1282E-13 -4.3255E-14 2.4346E-14 2.0894E-13 -1.9061E-13
-1.1282E-13 5.4647E-14 2.2746E-14 -1.2854E-14 -2.7031E-15 1.0392E-13
-4.3255E-14 2.2746E-14 1.0511E-13 -1.6062E-14 -2.0612E-16 4.5218E-14
2.4346E-14 -1.2854E-14 -1.6062E-14 5.4616E-15 3.8451E-17 -2.5558E-14
2.0894E-13 -2.7031E-15 -2.0612E-16 3.8451E-17 1.6225E-13 4.6416E-15
-1.9061E-13 1.0392E-13 4.5218E-14 -2.5558E-14 4.6416E-15 2.0694E-13
# lat0 lon0 xBary yBary zBary JD0
1.205479 124.851865 0.903467 0.008420 -0.397197 2452965.135868
# Heliocentric elements and errors
Epoch: 2452964.5000 = 2003/11/21
Mean Anomaly: 1.77539 +/- 0.001
Argument of Peri: 157.91433 +/- 0.002
Long of Asc Node: 308.58556 +/- 0.000
Inclination: 13.05818 +/- 0.000
Eccentricity: 0.73366480 +/- 0.0001
Semi-Major Axis: 135.01812380 +/- 0.0420
Time of Perihelion: 2450138.4624 +/- 1.9
Perihelion: 35.96007919 +/- 0.0155
Aphelion: 234.07616841 +/- 0.0736
Period (y) 1568.9038 +/- 0.73
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -20.17682296 +/- 0.0003
Ecliptic Y 30.55289702 +/- 0.0004
Ecliptic Z 0.76157813 +/- 0.0000
Ecliptic XDOT -0.00327963 +/- 0.0000
Ecliptic YDOT -0.00159137 +/- 0.0000
Ecliptic ZDOT -0.00082480 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 36.62180566 +/- 0.0004
Geocenter to KBO 36.20911652 +/- 0.0005
# Hcoef: 7.34
The following table shows the complete astrometric record for 06AM98. 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 (06AM98) followed by the observatory code and reference code for the source of the astrometry.
2003 11 21.635125 08 30 01.71 +20 13 19.2 23.1r 06AM98 T14 C~63RQ 2004 04 13.176003 08 20 55.30 +20 32 18.0 23.0r 06AM98 645 C~63RQ 2005 04 05.318769 08 29 03.72 +19 35 57.1 22.8i 06AM98 T14 C~63RQ 2005 04 06.264504 08 29 02.82 +19 35 54.9 22.9i 06AM98 T14 C~63RQ 2005 04 06.330142 08 29 02.75 +19 35 54.8 22.9i 06AM98 T14 C~63RQ 2006 01 04.584192 08 43 30.17 +18 20 59.6 06AM98 T09 C~63RQ 2006 01 04.616615 08 43 30.02 +18 21 00.0 06AM98 T09 C~63RQ 2006 01 04.642039 08 43 29.90 +18 21 00.7 06AM98 T09 C~63RQ 2006 01 05.53253 08 43 25.55 +18 21 13.8 06AM98 568 Cq2894 2006 01 05.57222 08 43 25.34 +18 21 14.3 06AM98 568 Cq2894 2006 01 06.62466 08 43 20.09 +18 21 28.9 23.4R 06AM98 568 Cq2894 2006 01 06.64615 08 43 20.05 +18 21 29.4 23.3R 06AM98 568 Cq2894 2006 01 31.280905 08 41 08.64 +18 27 49.8 06AM98 T09 C~63RQ 2006 01 31.293049 08 41 08.56 +18 27 50.1 06AM98 T09 C~63RQ 2006 01 31.305153 08 41 08.50 +18 27 50.3 06AM98 T09 C~63RQ 2006 02 01.279768 08 41 03.15 +18 28 06.0 06AM98 T09 C~63RQ 2006 02 01.291967 08 41 03.09 +18 28 06.2 06AM98 T09 C~63RQ 2006 02 01.305159 08 41 03.02 +18 28 06.4 06AM98 T09 C~63RQ 2006 03 02.20430 08 38 37.55 +18 34 49.2 22.6R 06AM98 695 Cq7133 2006 03 02.26109 08 38 37.30 +18 34 50.2 06AM98 695 Cq7133 2006 03 02.31743 08 38 37.05 +18 34 50.6 06AM98 695 Cq7133 2006 04 25.98536 08 36 56.83 +18 36 33.0 22.0R 06AM98 807 Cr3950 2006 04 26.98379 08 36 57.93 +18 36 24.5 06AM98 807 Cr3950 2006 04 27.98663 08 36 59.08 +18 36 15.1 06AM98 807 Cr3950 2006 05 01.159617 08 37 03.61 +18 35 43.1 23.3r 06AM98 695 C~4q6b 2006 05 01.247044 08 37 03.77 +18 35 41.9 06AM98 695 C~4q6b 2013 02 14.294141 09 30 52.54 +11 30 32.7 06AM98 T14 C~63RQ 2013 02 14.295389 09 30 52.52 +11 30 32.8 06AM98 T14 C~63RQ 2013 02 14.296650 09 30 52.52 +11 30 32.7 06AM98 T14 C~63RQ 2016 01 12.306860 09 52 45.42 +08 24 33.1 22.7z 06AM98 W84 C~63RQ 2016 01 13.308172 09 52 41.62 +08 24 45.4 23.8g 06AM98 W84 C~63RQ 2016 01 13.309947 09 52 41.59 +08 24 45.3 23.1r 06AM98 W84 C~63RQ 2019 03 02.218854 10 07 02.03 +05 50 33.2 23.9g 06AM98 W84 C~63RQ 2019 03 02.264463 10 07 01.81 +05 50 34.2 06AM98 W84 C~63RQ
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 0.52 0.00 -0.07
2 0.3930 0.00 0.14 0.00 0.01
3 1.3708 0.00 0.05 0.00 -0.17
4 1.3734 0.00 -0.03 0.00 -0.11
5 1.3736 0.00 -0.10 0.00 -0.03
6 2.1217 0.00 -0.21 0.00 -0.22
7 2.1218 0.00 -0.05 0.00 -0.26
8 2.1219 0.00 0.04 0.00 0.09
9 2.1243 0.00 0.09 0.00 0.66
10 2.1244 0.00 -0.07 0.00 0.61
11 2.1273 0.00 -0.64 0.00 0.26
12 2.1273 0.00 0.39 0.00 0.46
13 2.1948 0.00 0.11 0.00 -0.39
14 2.1948 0.00 -0.08 0.00 -0.29
15 2.1949 0.00 0.03 0.00 -0.28
16 2.1975 0.00 -0.23 0.00 0.02
17 2.1976 0.00 -0.12 0.00 0.03
18 2.1976 0.00 -0.07 0.00 0.01
19 2.2767 0.00 -0.03 0.00 -0.26
20 2.2769 0.00 -0.03 0.00 0.11
21 2.2770 0.00 -0.06 0.00 -0.11
22 2.4267 0.00 -0.20 0.00 -0.21
23 2.4294 0.00 0.14 0.00 0.10
24 2.4322 0.00 -0.49 0.00 -0.05
25 2.4409 0.00 0.05 0.00 0.12
26 2.4411 0.00 0.43 0.00 -0.11
27 9.2338 0.00 0.29 0.00 0.09
28 9.2338 0.00 0.08 0.00 0.16
29 9.2338 0.00 0.18 0.00 0.04
30 12.1415 0.00 0.01 0.00 -0.15
31 12.1442 0.00 0.22 0.00 0.01
32 12.1442 0.00 -0.12 0.00 -0.11
33 15.2761 0.00 -0.08 0.00 0.04
34 15.2762 0.00 -0.23 0.00 -0.01
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.
06AM98 quality flag:3 Type: SCATNEAR SCATNEAR SCATNEAR axisobj 133.002 133.003 133.002 ecceobj 0.730 0.730 0.730 incobj 13.085 13.085 13.085 qmin 34.254 34.231 34.202 qmax 238.415 244.937 240.750 amean 128.679 130.842 131.264 amin 123.756 126.000 126.618 amax 137.274 140.485 138.095 emean 0.722 0.726 0.728 emin 0.706 0.713 0.713 emax 0.737 0.744 0.743 imean 13.980 14.083 13.714 imin 12.914 12.958 12.758 imax 15.221 15.350 14.975 excite_mean 0.761 0.766 0.766 fracstop 1.000 1.000 1.000 cjmean 3.010 3.008 3.010 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 257.5 258.8 246.3 kozaiamp 100.9 100.1 83.9