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: 19CN30
# Created Wed Nov 27 02:10:54 2024
# Orbit generated from Bernstein formalism
# Fitting 10 observations of 10
# Arc: 31.85d
# First observation: 2019/02/04
# Last observation: 2019/03/08
Preliminary a, adot, b, bdot, g, gdot:
-0.000000 0.076952 -0.000001 0.019466 0.046327 0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit: 3.39 DOF: 15 RMS: 0.10
# Min/Max residuals: -0.19 0.15
# Exact a, adot, b, bdot, g, gdot:
2.418752E-05 6.860538E-02 6.242710E-06 1.938190E-02 4.450222E-02 8.126737E-03
# Covariance matrix:
1.0219E-12 1.8978E-09 -5.0496E-14 -5.4602E-12 3.7769E-10 1.4447E-08
1.8978E-09 5.5101E-06 -1.4465E-10 -1.7381E-08 1.0915E-06 4.0906E-05
-5.0496E-14 -1.4465E-10 3.6295E-13 -4.0990E-12 -2.8733E-11 -1.1038E-09
-5.4602E-12 -1.7381E-08 -4.0990E-12 1.9813E-10 -3.3666E-09 -9.9950E-08
3.7769E-10 1.0915E-06 -2.8733E-11 -3.3666E-09 2.1635E-07 8.1493E-06
1.4447E-08 4.0906E-05 -1.1038E-09 -9.9950E-08 8.1493E-06 3.2116E-04
# lat0 lon0 xBary yBary zBary JD0
1.595757 177.373328 0.669262 0.020448 -0.731737 2458519.087451
# Heliocentric elements and errors
Epoch: 2458510.5000 = 2019/01/27
Mean Anomaly: 3.56643 +/- 9.498
Argument of Peri: 351.80630 +/- 37.601
Long of Asc Node: 170.28841 +/- 0.236
Inclination: 15.85085 +/- 0.609
Eccentricity: 0.53345625 +/- 0.1576
Semi-Major Axis: 49.24619363 +/- 13.3218
Time of Perihelion: 2457259.9844 +/- 3291.5
Perihelion: 22.97550363 +/- 9.9436
Aphelion: 75.51688363 +/- 21.8533
Period (y) 345.5948 +/- 140.23
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -23.13804545 +/- 0.2345
Ecliptic Y 1.72346388 +/- 0.0108
Ecliptic Z 0.62588536 +/- 0.0065
Ecliptic XDOT -0.00065147 +/- 0.0011
Ecliptic YDOT -0.00419657 +/- 0.0001
Ecliptic ZDOT 0.00120566 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 23.21058396 +/- 0.2338
Geocenter to KBO 22.47078765 +/- 0.2349
# Hcoef: 10.81
The following table shows the complete astrometric record for 19CN30. 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 (19CN30) followed by the observatory code and reference code for the source of the astrometry.
2019 02 04.58665 11 52 53.89 +02 30 31.5 25.1g 19CN30 T09 C~83G8 2019 02 04.58875 11 52 53.87 +02 30 31.5 25.5g 19CN30 T09 C~83G8 2019 02 04.62048 11 52 53.73 +02 30 32.8 25.3g 19CN30 T09 C~83G8 2019 02 04.66250 11 52 53.53 +02 30 34.7 25.0g 19CN30 T09 C~83G8 2019 03 02.43427 11 50 25.22 +02 52 49.9 23.9y 19CN30 T09 C~83G8 2019 03 02.55921 11 50 24.36 +02 52 56.8 23.8y 19CN30 T09 C~83G8 2019 03 02.61357 11 50 23.99 +02 53 00.2 23.9y 19CN30 T09 C~83G8 2019 03 08.35114 11 49 44.61 +02 58 31.7 24.3r 19CN30 T09 C~83G8 2019 03 08.36022 11 49 44.54 +02 58 32.4 24.3r 19CN30 T09 C~83G8 2019 03 08.43394 11 49 44.01 +02 58 36.4 24.2r 19CN30 T09 C~83G8
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 0.13
2 0.0000 -0.27 -0.07 -0.12 -0.01
3 0.0001 -2.72 0.07 0.24 -0.07
4 0.0002 -6.22 -0.04 0.79 -0.07
5 0.0708 -2576.19 -0.05 342.64 0.09
6 0.0711 -2590.75 0.06 343.85 -0.13
7 0.0713 -2597.19 -0.01 344.77 0.15
8 0.0870 -3270.40 0.08 414.69 -0.01
9 0.0870 -3271.64 -0.06 414.92 0.11
10 0.0872 -3280.52 -0.02 415.44 -0.19
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.
19CN30 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