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: 612019
# Created Wed Dec 25 02:07:36 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 43 observations of 44
# Arc: 21.11y
# First observation: 1994/03/13
# Last observation: 2015/04/24
# Chi-squared of fit: 509.91 DOF: 80 RMS: 0.61
# Min/Max residuals: -1.87 1.20
# Exact a, adot, b, bdot, g, gdot:
1.807162E-05 2.104652E-02 -5.253524E-06 -6.092089E-04 2.285425E-02 4.364376E-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
0.032617 -161.008363 0.445457 0.000529 -0.888770 2449424.988597
# Heliocentric elements and errors
Epoch: 2449424.5000 = 1994/03/13
Mean Anomaly: 164.55195 +/- 0.000
Argument of Peri: 13.27507 +/- 0.000
Long of Asc Node: 19.52408 +/- 0.000
Inclination: 1.65702 +/- 0.000
Eccentricity: 0.03680169 +/- 0.0000
Semi-Major Axis: 43.11597208 +/- 0.0000
Time of Perihelion: 2402157.6970 +/- 0.0
Perihelion: 41.52923124 +/- 0.0000
Aphelion: 44.70271291 +/- 0.0000
Period (y) 283.1167 +/- 0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -42.35962902 +/- 0.0000
Ecliptic Y -14.11467503 +/- 0.0000
Ecliptic Z 0.02469387 +/- 0.0000
Ecliptic XDOT 0.00077609 +/- 0.0000
Ecliptic YDOT -0.00240502 +/- 0.0000
Ecliptic ZDOT -0.00007308 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 44.64932579 +/- 0.0000
Geocenter to KBO 43.75555313 +/- 0.0000
# Hcoef: 7.15
The following table shows the complete astrometric record for 612019. 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 (612019) followed by the observatory code and reference code for the source of the astrometry.
1994 03 13.4879 13 10 08.82 -07 24 27.2 23.3R 612019 568 A23286 1994 03 13.5000 13 10 08.79 -07 24 27.2 612019 568 A23286 1994 03 13.5120 13 10 08.74 -07 24 26.9 612019 568 A23286 1994 03 14.5250 13 10 04.86 -07 24 04.8 612019 568 A23286 1994 03 14.5408 13 10 04.80 -07 24 04.1 612019 568 A23286 1994 03 15.5385 13 10 01.00 -07 23 41.6 612019 568 A23286 1994 03 15.5508 13 10 00.99 -07 23 41.3 612019 568 A23286 1994 03 15.5976 13 10 00.75 -07 23 40.3 612019 568 A23286 1994 04 13.4916 13 07 59.79 -07 11 30.8 23. R 612019 568 A23389 1994 04 13.5038 13 07 59.71 -07 11 30.3 612019 568 A23389 1994 04 15.4842 13 07 51.26 -07 10 39.7 612019 568 A23389 1994 05 05.40132 13 06 30.25 -07 02 31.2 23.2V 612019 568 C23582 1994 05 05.48792 13 06 29.98 -07 02 28.9 612019 568 C23582 1994 05 07.34912 13 06 23.06 -07 01 46.9 23.5V 612019 568 C23582 1994 05 10.89722 13 06 10.30 -07 00 30.8 23.4R 612019 950 C23646 1994 06 07.2909 13 04 54.99 -06 52 57.3 612019 568 A23582 1994 06 07.3065 13 04 54.99 -06 52 57.3 612019 568 A23582 1994 06 07.3432 13 04 54.89 -06 52 56.8 612019 568 A23582 1994 06 07.3481 13 04 54.86 -06 52 56.6 612019 568 A23582 1995 02 25.5504 13 15 30.47 -07 59 10.6 23.5R 612019 568 A24813 1995 02 25.5595 13 15 30.44 -07 59 10.4 612019 568 A24813 1995 02 26.5354 13 15 27.59 -07 58 54.0 612019 568 A24813 1995 02 27.5361 13 15 24.62 -07 58 36.9 612019 568 A24813 1995 02 27.5469 13 15 24.59 -07 58 36.5 612019 568 A24813 1995 04 01.0377 13 13 22.37 -07 46 29.7 612019 950 C25182 1995 04 01.1500 13 13 21.97 -07 46 25.1 23.8R 612019 950 C25029 1997 06 03.23343 13 18 18.54 -08 21 07.7 612019 711 C30029 1997 06 03.24113 13 18 18.69 -08 21 09.7 612019 711 C30029 1997 06 04.21633 13 18 16.24 -08 20 53.3 612019 711 C30029 1997 06 04.23987 13 18 16.23 -08 20 52.8 612019 711 C30029 1997 06 04.28622 13 18 16.18 -08 20 53.4 612019 711 C30029 1997 06 04.29476 13 18 16.04 -08 20 52.4 612019 711 C30029 1998 05 24.94307 13 23 11.07 -08 52 25.2 612019 950 Ca1681 1998 05 25.00008 13 23 10.89 -08 52 24.5 612019 950 Ca1681 1998 05 25.04237 13 23 10.77 -08 52 23.0 612019 950 Ca1681 1998 06 23.18818 13 22 09.52 -08 46 25.6 23.3R 612019 705 Ca1681 1998 06 24.22135 13 22 08.48 -08 46 19.8 612019 705 Ca1681 2000 06 28.94307 13 30 53.21 -09 42 18.8 612019 950 Cb7358 2000 06 29.91659 13 30 52.56 -09 42 14.9 612019 950 Cb7358 2014 04 30.14005 14 38 18.15 -16 07 38.2 612019 W84 C~2fbj 2014 04 30.20903 14 38 17.84 -16 07 36.7 23.8V 612019 W84 C~2fbj 2014 05 01.12675 14 38 13.66 -16 07 17.6 612019 W84 C~2fbj 2015 04 24.25229 14 43 31.30 -16 33 33.2 23.4R 612019 G37 C~1Re7 2015 04 24.42161 14 43 30.54 -16 33 29.6 612019 G37 C~1Re7
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 -0.29 0.00 1.20
2 0.0000 0.00 -0.04 0.00 0.92
3 0.0001 0.00 -0.10 0.00 0.95
4 0.0028 0.00 -0.44 0.00 -0.11
5 0.0029 0.00 -0.42 0.00 0.23
6 0.0056 0.00 0.14 0.00 -0.32
7 0.0056 0.00 0.72 0.00 -0.30
8 0.0058 0.00 -0.12 0.00 -0.39
9 0.0849 0.00 0.12 0.00 0.42
10 0.0849 0.00 -0.28 0.00 0.60
11 0.0903 0.00 0.22 0.00 0.01
12 0.1449 0.00 -0.77 0.00 -0.06
13 0.1451 0.00 0.15 0.00 0.27
14 0.1502 0.00 0.11 0.00 0.49
15 0.1599 0.00 0.55 0.00 -0.54
16 0.2349 0.00 0.52 0.00 0.90
17 0.2350 0.00 0.98 0.00 0.73
18 0.2351 0.00 0.54 0.00 0.82
19 0.2351 0.00 0.23 0.00 0.97
20 0.9557 0.00 -0.40 0.00 -0.95
21 0.9557 0.00 -0.44 0.00 -0.91
22 0.9584 0.00 -0.49 0.00 -1.34
23 0.9611 0.00 -0.30 0.00 -1.87
24 0.9611 0.00 -0.24 0.00 -1.66
25 1.0501 0.00 -0.63 0.00 -1.75
26 1.0504 0.00 0.67 0.00 -0.01
27 3.2245 0.00 -0.88 0.00 -0.24
28 3.2245 0.00 ( 1.65) 0.00 ( -2.35)
29 3.2272 0.00 -0.60 0.00 0.51
30 3.2272 0.00 0.10 0.00 0.69
31 3.2274 0.00 1.00 0.00 -0.55
32 3.2274 0.00 -0.80 0.00 0.33
33 4.1984 0.00 0.30 0.00 0.03
34 4.1985 0.00 0.29 0.00 -0.30
35 4.1986 0.00 0.48 0.00 0.44
36 4.2784 0.00 0.04 0.00 0.64
37 4.2813 0.00 -0.16 0.00 0.55
38 6.2956 0.00 0.00 0.00 -0.18
39 6.2982 0.00 0.34 0.00 -0.12
40 20.1305 0.00 -0.13 0.00 -0.13
41 20.1307 0.00 -0.00 0.00 -0.05
42 20.1332 0.00 -0.24 0.00 0.04
43 21.1137 0.00 0.04 0.00 -0.08
44 21.1141 0.00 0.20 0.00 0.16
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.
612019 quality flag:3 Type: CLASSICAL CLASSICAL CLASSICAL axisobj 42.649 42.649 42.649 ecceobj 0.048 0.048 0.048 incobj 1.661 1.661 1.661 qmin 39.681 39.680 39.683 qmax 46.414 46.412 46.417 amean 42.950 42.950 42.950 amin 42.611 42.609 42.614 amax 43.298 43.298 43.300 emean 0.053 0.053 0.053 emin 0.030 0.030 0.030 emax 0.072 0.072 0.072 imean 1.825 1.825 1.825 imin 0.436 0.436 0.436 imax 2.744 2.744 2.743 excite_mean 0.063 0.063 0.063 fracstop 1.000 1.000 1.000 cjmean 3.084 3.084 3.084 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 180.2 180.3 180.2 kozaiamp 180.0 180.0 180.0