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: 19GR140
# Created Fri Nov 1 01:10:38 2024
# Orbit generated from Bernstein formalism
# Fitting 12 observations of 12
# Arc: 9.04d
# First observation: 2019/04/04
# Last observation: 2019/04/13
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution
# Chi-squared of fit: 19.93 DOF: 20 RMS: 0.23
# Min/Max residuals: -0.30 0.74
# Exact a, adot, b, bdot, g, gdot:
1.649935E-05 2.617853E-02 3.577437E-07 -4.671282E-04 2.551731E-02 0.000000E+00
# Covariance matrix:
2.9301E-11 4.7428E-08 -2.7693E-13 -2.2856E-11 7.5717E-09 0.0000E+00
4.7428E-08 7.8017E-05 -4.5530E-10 -3.7578E-08 1.2449E-05 0.0000E+00
-2.7693E-13 -4.5530E-10 4.4212E-13 -2.3602E-11 -7.2651E-11 0.0000E+00
-2.2856E-11 -3.7578E-08 -2.3602E-11 1.8078E-09 -5.9961E-09 0.0000E+00
7.5717E-09 1.2449E-05 -7.2651E-11 -5.9961E-09 1.9864E-06 0.0000E+00
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 2.1864E-04
# lat0 lon0 xBary yBary zBary JD0
0.878235 -160.253241 0.111008 0.015272 -0.993415 2458577.637273
# Heliocentric elements and errors
Epoch: 2458570.5000 = 2019/03/28
Mean Anomaly: 356.29340 +/- 38.583
Argument of Peri: 144.28770 +/- 105.416
Long of Asc Node: 59.59332 +/- 9.579
Inclination: 1.33254 +/- 0.267
Eccentricity: 0.07474849 +/- 0.5478
Semi-Major Axis: 43.42165131 +/- 23.3507
Time of Perihelion: 2459646.5465 +/- 115707.6
Perihelion: 40.17594845 +/- 32.1323
Aphelion: 46.66735416 +/- 34.5762
Period (y) 286.1328 +/- 230.81
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -37.85112896 +/- 2.0371
Ecliptic Y -13.47838364 +/- 0.7311
Ecliptic Z 0.60067897 +/- 0.0332
Ecliptic XDOT 0.00095656 +/- 0.0015
Ecliptic YDOT -0.00264491 +/- 0.0009
Ecliptic ZDOT -0.00005033 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 40.18377289 +/- 1.9344
Geocenter to KBO 39.18908675 +/- 2.1645
# Hcoef: 7.47
The following table shows the complete astrometric record for 19GR140. 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 (19GR140) followed by the observatory code and reference code for the source of the astrometry.
2019 04 04.136472 13 14 15.26 -06 54 37.2 19GR140 W84 C~6CIK 2019 04 05.132972 13 14 10.60 -06 54 08.7 23.7V 19GR140 W84 C~6CIK 2019 04 07.10799 13 14 01.38 -06 53 13.4 19GR140 W93 C~5bps 2019 04 07.13606 13 14 01.19 -06 53 12.3 22.8R 19GR140 W93 C~5bps 2019 04 07.16372 13 14 01.05 -06 53 11.5 19GR140 W93 C~5bps 2019 04 09.10709 13 13 51.94 -06 52 16.1 23.2R 19GR140 W93 C~5bps 2019 04 09.13510 13 13 51.78 -06 52 15.5 23.3R 19GR140 W93 C~5bps 2019 04 11.14373 13 13 42.37 -06 51 18.9 22.9R 19GR140 W93 C~5bps 2019 04 11.17176 13 13 42.21 -06 51 17.9 19GR140 W93 C~5bps 2019 04 13.12178 13 13 33.03 -06 50 22.8 19GR140 W93 C~5bps 2019 04 13.15280 13 13 32.88 -06 50 22.1 19GR140 W93 C~5bps 2019 04 13.18017 13 13 32.76 -06 50 21.4 23.0R 19GR140 W93 C~5bps
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 -0.06 0.00 -0.13
2 0.0027 -75.02 -0.14 0.22 0.20
3 0.0081 -223.03 0.74 -0.35 -0.09
4 0.0082 -226.07 -0.15 -0.40 -0.12
5 0.0083 -228.30 -0.27 -0.44 -0.14
6 0.0136 -374.84 -0.01 -0.32 0.33
7 0.0137 -377.28 -0.30 -0.67 0.01
8 0.0192 -528.41 0.43 -1.13 0.04
9 0.0193 -531.00 -0.00 -1.11 0.08
10 0.0246 -678.40 -0.17 -1.68 0.05
11 0.0247 -680.73 -0.13 -1.88 -0.12
12 0.0248 -682.65 0.04 -1.90 -0.12
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.
19GR140 quality flag:0 Type: ERR2LARGE ERR2LARGE ERR2LARGE axisobj 0.000 0.000 0.000 ecceobj -1.000 -1.000 -1.000 incobj -1.000 -1.000 -1.000 qmin 0.000 0.000 0.000 qmax 0.000 0.000 0.000 amean 0.000 0.000 0.000 amin 0.000 0.000 0.000 amax 0.000 0.000 0.000 emean 0.000 0.000 0.000 emin 0.000 0.000 0.000 emax 0.000 0.000 0.000 imean 0.000 0.000 0.000 imin 0.000 0.000 0.000 imax 0.000 0.000 0.000 excite_mean 0.000 0.000 0.000 fracstop 0.000 0.000 0.000 cjmean 0.000 0.000 0.000 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 0.0 0.0 0.0 kozaiamp 0.0 0.0 0.0