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: 19GM140
# Created Fri Apr 26 01:18:23 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting 33 observations of 33
# Arc: 19.15y
# First observation: 2000/04/10
# Last observation: 2019/06/05
# Chi-squared of fit: 82.03 DOF: 60 RMS: 0.28
# Min/Max residuals: -0.66 0.86
# Exact a, adot, b, bdot, g, gdot:
1.606331E-05 2.810288E-02 -1.963325E-06 2.299355E-03 2.763269E-02 -2.550324E-03
# Covariance matrix:
3.8614E-13 -3.8013E-14 2.2958E-15 -1.5865E-15 -2.0672E-13 -2.9419E-14
-3.8013E-14 2.5327E-14 -4.7319E-15 2.1290E-15 -2.7858E-14 3.7915E-14
2.2958E-15 -4.7319E-15 1.6993E-13 -1.0096E-14 9.4404E-15 -7.5356E-15
-1.5865E-15 2.1290E-15 -1.0096E-14 9.1093E-16 -3.5312E-15 3.3477E-15
-2.0672E-13 -2.7858E-14 9.4404E-15 -3.5312E-15 3.4058E-13 -6.1376E-14
-2.9419E-14 3.7915E-14 -7.5356E-15 3.3477E-15 -6.1376E-14 5.9527E-14
# lat0 lon0 xBary yBary zBary JD0
0.542607 167.853408 -0.546543 0.007826 -0.848522 2451644.653693
# Heliocentric elements and errors
Epoch: 2451644.5000 = 2000/04/10
Mean Anomaly: 259.43724 +/- 0.000
Argument of Peri: 115.37647 +/- 0.001
Long of Asc Node: 162.23451 +/- 0.000
Inclination: 4.70274 +/- 0.000
Eccentricity: 0.07553560 +/- 0.0001
Semi-Major Axis: 36.33714104 +/- 0.2893
Time of Perihelion: 2473993.5594 +/- 688.6
Perihelion: 33.59239346 +/- 0.2675
Aphelion: 39.08188861 +/- 0.3112
Period (y) 219.0455 +/- 2.62
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -36.31537673 +/- 0.0010
Ecliptic Y 7.26149042 +/- 0.0002
Ecliptic Z 0.34265862 +/- 0.0000
Ecliptic XDOT -0.00034299 +/- 0.0000
Ecliptic YDOT -0.00276907 +/- 0.0000
Ecliptic ZDOT 0.00022554 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 37.03587990 +/- 0.0010
Geocenter to KBO 36.18911371 +/- 0.0010
# Hcoef: 7.46
The following table shows the complete astrometric record for 19GM140. 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 (19GM140) followed by the observatory code and reference code for the source of the astrometry.
2000 04 10.15295 11 16 10.10 +05 18 02.5 24.1R 19GM140 695 C~5bpr 2000 04 10.23822 11 16 09.74 +05 18 04.8 19GM140 695 C~5bpr 2001 02 20.430213 11 26 18.01 +04 21 01.4 22.6r 19GM140 645 C~5bpr 2001 02 20.431043 11 26 18.01 +04 21 01.3 22.5i 19GM140 645 C~5bpr 2001 02 20.432701 11 26 18.01 +04 21 01.7 21.5z 19GM140 645 C~5bpr 2001 02 20.433530 11 26 18.00 +04 21 01.2 23.4g 19GM140 645 C~5bpr 2004 03 20.395492 11 42 39.88 +03 02 14.5 19GM140 568 C~5bpr 2004 11 19.600902 11 52 07.45 +02 03 39.3 19GM140 568 C~5bpr 2004 11 19.606918 11 52 07.46 +02 03 39.1 19GM140 568 C~5bpr 2004 11 19.612929 11 52 07.54 +02 03 38.9 19GM140 568 C~5bpr 2004 11 19.637390 11 52 07.63 +02 03 38.3 19GM140 568 C~5bpr 2013 04 01.244807 12 39 04.68 -01 46 48.0 19GM140 W84 C~5bpr 2014 02 25.656253 12 48 21.51 -02 39 21.1 19GM140 568 C~5bpr 2014 02 25.664032 12 48 21.48 -02 39 20.7 19GM140 568 C~5bpr 2015 03 30.574217 12 52 21.87 -02 55 08.4 19GM140 568 C~5bpr 2015 03 30.612482 12 52 21.67 -02 55 07.5 19GM140 568 C~5bpr 2019 03 06.265361 13 20 55.56 -05 22 06.1 19GM140 W84 C~5bpr 2019 04 05.11880 13 18 34.40 -05 06 16.9 21.9R 19GM140 W93 C~5agp 2019 04 05.14681 13 18 34.27 -05 06 16.4 22.4R 19GM140 W93 C~5agp 2019 04 05.17434 13 18 34.11 -05 06 15.2 22.5R 19GM140 W93 C~5agp 2019 04 07.07876 13 18 24.12 -05 05 10.9 23.1R 19GM140 W93 C~5agp 2019 04 07.13606 13 18 23.86 -05 05 09.8 22.7R 19GM140 W93 C~5agp 2019 04 07.16372 13 18 23.72 -05 05 08.8 22.0R 19GM140 W93 C~5agp 2019 04 09.10709 13 18 13.50 -05 04 04.2 22.8R 19GM140 W93 C~5agp 2019 04 09.13510 13 18 13.38 -05 04 03.3 23.3R 19GM140 W93 C~5agp 2019 04 09.16310 13 18 13.20 -05 04 02.2 22.9R 19GM140 W93 C~5agp 2019 04 11.11212 13 18 03.02 -05 02 58.2 22.5R 19GM140 W93 C~5agp 2019 04 11.14373 13 18 02.82 -05 02 56.9 22.9R 19GM140 W93 C~5agp 2019 04 11.17176 13 18 02.67 -05 02 56.1 22.8R 19GM140 W93 C~5agp 2019 04 13.12178 13 17 52.41 -05 01 51.4 22.4R 19GM140 W93 C~5agp 2019 04 13.15280 13 17 52.24 -05 01 50.5 22.4R 19GM140 W93 C~5agp 2019 04 13.18017 13 17 52.10 -05 01 49.9 22.6R 19GM140 W93 C~5agp 2019 06 05.087676 13 14 04.43 -04 39 58.0 19GM140 W84 C~5bpr
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 0.27 0.00 0.62
2 0.0002 0.00 0.25 0.00 0.61
3 0.8659 0.00 -0.09 0.00 -0.02
4 0.8659 0.00 -0.03 0.00 -0.14
5 0.8659 0.00 0.09 0.00 0.20
6 0.8659 0.00 -0.00 0.00 -0.32
7 3.9432 0.00 0.12 0.00 -0.04
8 4.6118 0.00 -0.47 0.00 -0.12
9 4.6118 0.00 -0.66 0.00 -0.19
10 4.6118 0.00 0.19 0.00 -0.26
11 4.6119 0.00 0.12 0.00 -0.31
12 12.9749 0.00 0.10 0.00 -0.43
13 13.8795 0.00 0.05 0.00 -0.27
14 13.8796 0.00 0.07 0.00 -0.10
15 14.9690 0.00 -0.11 0.00 0.20
16 14.9691 0.00 -0.12 0.00 -0.21
17 18.9024 0.00 -0.06 0.00 -0.40
18 18.9842 0.00 0.10 0.00 0.20
19 18.9842 0.00 0.37 0.00 -0.23
20 18.9843 0.00 0.16 0.00 0.05
21 18.9895 0.00 -0.49 0.00 0.86
22 18.9897 0.00 0.17 0.00 0.05
23 18.9898 0.00 0.28 0.00 0.13
24 18.9951 0.00 -0.22 0.00 0.10
25 18.9952 0.00 0.22 0.00 0.08
26 18.9952 0.00 -0.24 0.00 0.25
27 19.0006 0.00 0.56 0.00 -0.30
28 19.0007 0.00 0.09 0.00 -0.04
29 19.0007 0.00 0.09 0.00 -0.17
30 19.0061 0.00 -0.22 0.00 0.31
31 19.0062 0.00 -0.29 0.00 0.20
32 19.0062 0.00 -0.20 0.00 -0.10
33 19.1511 0.00 -0.24 0.00 -0.14
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.
19GM140 quality flag:3 Type: 4:3E 4:3E 4:3E axisobj 36.315 36.315 36.316 ecceobj 0.076 0.076 0.076 incobj 4.704 4.704 4.704 qmin 32.697 32.698 32.696 qmax 40.649 40.644 40.653 amean 36.482 36.482 36.482 amin 36.122 36.123 36.121 amax 36.871 36.872 36.868 emean 0.083 0.083 0.083 emin 0.062 0.062 0.062 emax 0.103 0.103 0.103 imean 2.764 2.764 2.764 imin 0.063 0.066 0.063 imax 4.381 4.381 4.380 excite_mean 0.098 0.098 0.098 fracstop 1.000 1.000 1.000 cjmean 3.017 3.017 3.017 libcent 0 179.7 179.9 179.6 libamp 0 78.7 78.4 78.8 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 179.5 179.5 179.4 kozaiamp 179.9 180.0 180.0