Orbit Fit and Astrometric record for 17BF241

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: 17BF241   
# Created Wed Nov 27 02:10:46 2024
# Orbit generated from Bernstein formalism
# Fitting      7 observations of      7
# Arc:  31.00d
# First observation: 2017/01/23
#  Last observation: 2017/02/23
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# Chi-squared of fit:     4.00 DOF:     10 RMS:  0.13
# Min/Max residuals:    -0.26    0.24
# Exact a, adot, b, bdot, g, gdot:
  1.358156E-05  2.268414E-02 -8.891043E-06 -1.344163E-02  2.629809E-02  0.000000E+00
# Covariance matrix:
  7.0717E-11  1.2098E-07 -3.3695E-12 -5.5693E-09  2.8822E-08  0.0000E+00
  1.2098E-07  2.0805E-04 -5.7942E-09 -9.5772E-06  4.9564E-05  0.0000E+00
 -3.3695E-12 -5.7942E-09  5.2399E-13  2.6246E-10 -1.3804E-09  0.0000E+00
 -5.5693E-09 -9.5772E-06  2.6246E-10  4.4099E-07 -2.2816E-06  0.0000E+00
  2.8822E-08  4.9564E-05 -1.3804E-09 -2.2816E-06  1.1808E-05  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  2.3933E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.392617 -172.764067    0.885973    0.018232   -0.432255  2457777.111061
# Heliocentric elements and errors
Epoch:              2457770.5000  =  2017/01/17
Mean Anomaly:          232.73370 +/-   209.367
Argument of Peri:      304.89695 +/-   182.485
Long of Asc Node:        9.92325 +/-     2.162
Inclination:            30.60965 +/-    14.643
Eccentricity:         0.02577403 +/-    0.5750
Semi-Major Axis:     37.86560635 +/-   16.2191
Time of Perihelion: 2487857.3495 +/-  304203.9
Perihelion:          36.88965702 +/-   26.9012
Aphelion:            38.84155567 +/-   27.4006
Period (y)              233.0105 +/-    149.71
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.23390975 +/-    4.9248
Ecliptic Y           -3.96552991 +/-    0.6250
Ecliptic Z            1.58709666 +/-    0.2074
Ecliptic XDOT         0.00024233 +/-    0.0016
Ecliptic YDOT        -0.00235686 +/-    0.0012
Ecliptic ZDOT        -0.00139823 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   38.47175793 +/-    4.8947
Geocenter to KBO     38.02557619 +/-    4.9686
# Hcoef:  9.68

The following table shows the complete astrometric record for 17BF241. 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 (17BF241) followed by the observatory code and reference code for the source of the astrometry.

2017 01  23.61026  12 30 21.50   -00 40 25.0   25.2i 17BF241   T09  C~86um      
2017 01  23.62432  12 30 21.48   -00 40 25.2   25.9i 17BF241   T09  C~86um      
2017 01  23.64653  12 30 21.41   -00 40 24.7   25.4i 17BF241   T09  C~86um      
2017 01  23.65191  12 30 21.41   -00 40 25.0   25.6i 17BF241   T09  C~86um      
2017 02  23.53583  12 28 43.88   -00 32 35.0   25.0r 17BF241   T09  C~86um      
2017 02  23.56346  12 28 43.77   -00 32 34.7   25.6r 17BF241   T09  C~86um      
2017 02  23.60592  12 28 43.58   -00 32 33.6   25.2r 17BF241   T09  C~86um      

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     0.17
     2   0.0000     -0.20     0.24      -0.30    -0.07
     3   0.0001     -1.36    -0.26      -0.26     0.08
     4   0.0001     -1.24     0.02      -0.53    -0.18
     5   0.0847  -1530.88    -0.12    -146.04     0.09
     6   0.0847  -1532.51     0.14    -146.42    -0.12
     7   0.0849  -1535.57    -0.01    -146.53     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.