Orbit Fit and Astrometric record for 14SB350

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: 14SB350   
# Created Wed Nov 27 02:09:58 2024
# Orbit generated from Bernstein formalism
# Fitting      7 observations of      7
# Arc:  62.03d
# First observation: 2014/09/19
#  Last observation: 2014/11/20
Preliminary a, adot, b, bdot, g, gdot:
  -0.000001   0.020328   0.000004  -0.006361   0.021640   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     1.04 DOF:      9 RMS:  0.07
# Min/Max residuals:    -0.17    0.14
# Exact a, adot, b, bdot, g, gdot:
  1.300569E-05  1.765302E-02 -4.533937E-06 -5.891994E-03  2.125307E-02  5.780490E-03
# Covariance matrix:
  5.0477E-13  1.5322E-11  1.7794E-14 -3.3155E-12  3.3930E-12 -4.1606E-10
  1.5322E-11  2.0172E-08  2.5422E-11 -3.4572E-09  2.5173E-09 -8.9677E-07
  1.7794E-14  2.5422E-11  4.7445E-13 -7.4793E-12  3.0496E-12 -1.1810E-09
 -3.3155E-12 -3.4572E-09 -7.4793E-12  6.3705E-10 -4.3578E-10  1.5273E-07
  3.3930E-12  2.5173E-09  3.0496E-12 -4.3578E-10  3.4032E-10 -1.0260E-07
 -4.1606E-10 -8.9677E-07 -1.1810E-09  1.5273E-07 -1.0260E-07  4.3522E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
  -10.240567  -20.712844   -0.286025   -0.171559   -0.950371  2456919.570608
# Heliocentric elements and errors
Epoch:              2456910.5000  =  2014/09/10
Mean Anomaly:           69.44927 +/-    36.783
Argument of Peri:      104.75564 +/-    12.535
Long of Asc Node:      132.18264 +/-     0.238
Inclination:            21.00148 +/-     0.154
Eccentricity:         0.30102822 +/-    0.3207
Semi-Major Axis:     48.84876014 +/-    9.6377
Time of Perihelion: 2432853.3628 +/-   10567.0
Perihelion:          34.14390468 +/-   17.0512
Aphelion:            63.55361560 +/-   20.0645
Period (y)              341.4197 +/-    101.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           44.31197425 +/-    0.0376
Ecliptic Y          -16.44854623 +/-    0.0142
Ecliptic Z           -8.36519623 +/-    0.0073
Ecliptic XDOT         0.00135883 +/-    0.0008
Ecliptic YDOT         0.00191111 +/-    0.0003
Ecliptic ZDOT        -0.00087920 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   48.00085669 +/-    0.0351
Geocenter to KBO     47.05202089 +/-    0.0408
# Hcoef:  7.38

The following table shows the complete astrometric record for 14SB350. 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 (14SB350) followed by the observatory code and reference code for the source of the astrometry.

2014 09  19.06983  22 59 32.489  -17 33 04.30  24.1r 14SB350   807  C~1x8l      
2014 09  19.14530  22 59 32.183  -17 33 06.29        14SB350   807  C~1x8l      
2014 09  19.22379  22 59 31.862  -17 33 07.81        14SB350   807  C~1x8l      
2014 10  23.07516  22 57 36.626  -17 42 13.14        14SB350   304  C~1x8l      
2014 10  23.14879  22 57 36.425  -17 42 13.78        14SB350   304  C~1x8l      
2014 11  19.09321  22 56 52.631  -17 42 26.14        14SB350   304  C~1x8l      
2014 11  20.09935  22 56 52.076  -17 42 19.04        14SB350   304  C~1x8l      

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     0.03       0.00     0.03
     2   0.0002     -4.81    -0.06      -0.12    -0.17
     3   0.0004     -9.63     0.03       0.27     0.14
     4   0.0931  -1739.41     0.06     138.82     0.01
     5   0.0933  -1742.31    -0.06     139.34    -0.02
     6   0.1671  -2324.08    -0.00     370.42     0.06
     7   0.1698  -2328.64     0.00     380.04    -0.05

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.

14SB350    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