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: 19GO140
# Created Tue May 7 01:17:34 2024
# Orbit generated from Bernstein formalism
# Fitting 11 observations of 11
# Arc: 6.26d
# First observation: 2019/04/05
# Last observation: 2019/04/11
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after 13 iterations -- oscilliatory solution
# Chi-squared of fit: 25.40 DOF: 18 RMS: 0.27
# Min/Max residuals: -0.81 0.44
# Exact a, adot, b, bdot, g, gdot:
1.734464E-05 3.078466E-02 2.628580E-06 2.472462E-03 2.836983E-02 0.000000E+00
# Covariance matrix:
3.4666E-11 6.1928E-08 -1.3256E-13 -4.9998E-11 9.8884E-09 0.0000E+00
6.1928E-08 1.1174E-04 -2.3909E-10 -9.0178E-08 1.7835E-05 0.0000E+00
-1.3256E-13 -2.3909E-10 3.1796E-13 -2.4248E-11 -3.8161E-11 0.0000E+00
-4.9998E-11 -9.0178E-08 -2.4248E-11 3.3207E-09 -1.4394E-08 0.0000E+00
9.8884E-09 1.7835E-05 -3.8161E-11 -1.4394E-08 2.8467E-06 0.0000E+00
0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 0.0000E+00 3.0046E-04
# lat0 lon0 xBary yBary zBary JD0
1.004196 -160.010295 0.098437 0.017482 -0.994862 2458578.619601
# Heliocentric elements and errors
Epoch: 2458570.5000 = 2019/03/28
Mean Anomaly: 357.10610 +/- 319.517
Argument of Peri: 15.48364 +/- 24.931
Long of Asc Node: 187.85136 +/- 4.032
Inclination: 4.68941 +/- 1.551
Eccentricity: 0.09095318 +/- 0.5508
Semi-Major Axis: 39.86525589 +/- 21.8404
Time of Perihelion: 2459309.5451 +/- 81596.2
Perihelion: 36.23938417 +/- 29.6037
Aphelion: 43.49112761 +/- 32.4024
Period (y) 251.7097 +/- 206.85
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -34.08702836 +/- 1.9698
Ecliptic Y -12.30375552 +/- 0.7164
Ecliptic Z 0.61784234 +/- 0.0367
Ecliptic XDOT 0.00102783 +/- 0.0016
Ecliptic YDOT -0.00279150 +/- 0.0010
Ecliptic ZDOT 0.00023835 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 36.24485662 +/- 1.8684
Geocenter to KBO 35.24871562 +/- 2.0963
# Hcoef: 7.99
The following table shows the complete astrometric record for 19GO140. 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 (19GO140) followed by the observatory code and reference code for the source of the astrometry.
2019 04 05.11880 13 15 21.13 -06 53 06.7 23.0R 19GO140 W93 C~5bps 2019 04 05.14681 13 15 20.98 -06 53 05.8 23.5R 19GO140 W93 C~5bps 2019 04 05.17434 13 15 20.85 -06 53 04.6 23.1R 19GO140 W93 C~5bps 2019 04 07.10799 13 15 10.97 -06 52 01.4 22.9R 19GO140 W93 C~5bps 2019 04 07.13606 13 15 10.82 -06 52 00.4 23.4R 19GO140 W93 C~5bps 2019 04 07.16372 13 15 10.69 -06 51 59.6 19GO140 W93 C~5bps 2019 04 09.10709 13 15 00.73 -06 50 56.2 23.4R 19GO140 W93 C~5bps 2019 04 09.16310 13 15 00.45 -06 50 54.6 23.2R 19GO140 W93 C~5bps 2019 04 11.11212 13 14 50.43 -06 49 50.4 19GO140 W93 C~5bps 2019 04 11.17176 13 14 50.13 -06 49 48.9 23.1R 19GO140 W93 C~5bps 2019 04 11.375187 13 14 49.03 -06 49 43.1 23.5g 19GO140 T09 C~6oI0
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 -0.04 0.00 -0.26
2 0.0001 -2.41 -0.10 -0.01 -0.29
3 0.0002 -4.65 -0.04 0.38 0.06
4 0.0054 -164.76 -0.03 3.52 0.17
5 0.0055 -167.20 -0.12 3.60 0.23
6 0.0056 -169.30 0.11 3.61 0.21
7 0.0109 -330.58 0.13 6.48 0.15
8 0.0111 -335.05 0.39 6.39 0.01
9 0.0164 -497.47 -0.13 9.64 0.44
10 0.0166 -502.18 0.19 9.34 0.10
11 0.0171 -519.54 -0.39 8.54 -0.81
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.
19GO140 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