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: 19CS30
# Created Tue Apr 1 01:11:11 2025
# Orbit generated from Bernstein formalism
# Fitting 11 observations of 11
# Arc: 57.94d
# First observation: 2019/02/05
# Last observation: 2019/04/04
Preliminary a, adot, b, bdot, g, gdot:
0.000000 0.024271 -0.000001 0.000455 0.023963 0.000000
# Chi-squared of fit: 5.84 DOF: 16 RMS: 0.13
# Min/Max residuals: -0.27 0.34
# Exact a, adot, b, bdot, g, gdot:
1.552907E-05 2.310285E-02 2.834508E-07 4.757290E-04 2.362834E-02 1.499231E-03
# Covariance matrix:
4.4057E-13 1.1755E-10 -7.3531E-14 -2.5733E-12 2.5275E-11 1.4987E-09
1.1755E-10 1.9028E-07 -1.1132E-10 -4.1725E-09 3.8593E-08 1.8862E-06
-7.3531E-14 -1.1132E-10 3.6860E-13 2.1476E-13 -2.2636E-11 -1.1210E-09
-2.5733E-12 -4.1725E-09 2.1476E-13 1.2051E-10 -8.4558E-10 -4.1100E-08
2.5275E-11 3.8593E-08 -2.2636E-11 -8.4558E-10 7.8444E-09 3.8756E-07
1.4987E-09 1.8862E-06 -1.1210E-09 -4.1100E-08 3.8756E-07 2.0266E-05
# lat0 lon0 xBary yBary zBary JD0
4.323451 -177.732903 0.717770 0.051678 -0.682694 2458520.055801
# Heliocentric elements and errors
Epoch: 2458520.5000 = 2019/02/06
Mean Anomaly: 40.95580 +/- 82.960
Argument of Peri: 27.32397 +/- 101.768
Long of Asc Node: 107.84331 +/- 0.487
Inclination: 4.43673 +/- 0.011
Eccentricity: 0.06560210 +/- 0.1699
Semi-Major Axis: 45.15720297 +/- 2.3083
Time of Perihelion: 2445910.8829 +/- 25523.6
Perihelion: 42.19479570 +/- 7.9686
Aphelion: 48.11961023 +/- 8.0559
Period (y) 303.4581 +/- 23.27
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X -42.88003781 +/- 0.1581
Ecliptic Y -0.98743572 +/- 0.0062
Ecliptic Z 3.19052509 +/- 0.0120
Ecliptic XDOT -0.00005500 +/- 0.0005
Ecliptic YDOT -0.00268321 +/- 0.0001
Ecliptic ZDOT 0.00006786 +/- 0.0000
# Distances at JD0 (AU)
Heliocenter to KBO 43.00990726 +/- 0.1576
Geocenter to KBO 42.32206521 +/- 0.1586
# Hcoef: 8.50
The following table shows the complete astrometric record for 19CS30. 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 (19CS30) followed by the observatory code and reference code for the source of the astrometry.
2019 02 05.55500 12 15 11.98 +03 03 55.4 24.5i 19CS30 T09 C~83G8 2019 02 05.55837 12 15 11.99 +03 03 55.4 24.5i 19CS30 T09 C~83G8 2019 02 05.60072 12 15 11.85 +03 03 56.4 24.7i 19CS30 T09 C~83G8 2019 02 05.62764 12 15 11.77 +03 03 57.1 24.1i 19CS30 T09 C~83G8 2019 03 03.52028 12 13 43.53 +03 15 17.5 24.8z 19CS30 T09 C~83G8 2019 03 03.52832 12 13 43.46 +03 15 18.0 24.2z 19CS30 T09 C~83G8 2019 03 03.58484 12 13 43.24 +03 15 19.5 24.4z 19CS30 T09 C~83G8 2019 04 04.44950 12 11 26.64 +03 30 33.4 25.3g 19CS30 T09 C~83G8 2019 04 04.46994 12 11 26.56 +03 30 34.0 25.5g 19CS30 T09 C~83G8 2019 04 04.47203 12 11 26.54 +03 30 34.2 25.8g 19CS30 T09 C~83G8 2019 04 04.49303 12 11 26.45 +03 30 34.7 25.4g 19CS30 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 -0.01 0.00 0.01
2 0.0000 0.14 0.28 0.06 0.05
3 0.0001 -2.18 -0.07 0.14 -0.05
4 0.0002 -3.56 -0.20 0.31 -0.01
5 0.0711 -1486.78 0.34 98.71 0.00
6 0.0711 -1487.94 -0.27 98.75 0.03
7 0.0713 -1491.56 -0.07 98.82 -0.02
8 0.1585 -3732.10 0.01 124.50 -0.10
9 0.1586 -3733.44 0.12 124.58 0.00
10 0.1586 -3733.80 -0.09 124.64 0.07
11 0.1586 -3735.23 -0.04 124.57 0.02
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.
19CS30 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