Orbit Fit and Astrometric record for 14SL350

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: 14SL350   
# Created Fri Nov  1 01:09:47 2024
# Orbit generated from Bernstein formalism
# Fitting      7 observations of      7
# Arc:  60.01d
# First observation: 2014/09/21
#  Last observation: 2014/11/20
Preliminary a, adot, b, bdot, g, gdot:
  -0.000001   0.017851   0.000003  -0.000402   0.019596   0.000000
# WARNING Fitting with energy constraint
# Chi-squared of fit:     5.04 DOF:      9 RMS:  0.15
# Min/Max residuals:    -0.24    0.22
# Exact a, adot, b, bdot, g, gdot:
  1.243298E-05  1.567797E-02 -2.519881E-07 -1.976074E-05  1.927539E-02 -9.619741E-04
# Covariance matrix:
  5.1182E-13  2.2677E-11  2.2942E-14 -4.4511E-12  4.3308E-12 -7.7138E-10
  2.2677E-11  2.8455E-08  3.2369E-11 -5.0855E-09  3.5677E-09 -1.3440E-06
  2.2942E-14  3.2369E-11  4.8609E-13 -9.0834E-12  3.8875E-12 -1.6064E-09
 -4.4511E-12 -5.0855E-09 -9.0834E-12  9.5623E-10 -6.3350E-10  2.4276E-07
  4.3308E-12  3.5677E-09  3.8875E-12 -6.3350E-10  4.7684E-10 -1.5655E-07
 -7.7138E-10 -1.3440E-06 -1.6064E-09  2.4276E-07 -1.5655E-07  6.8764E-05
#      lat0       lon0       xBary       yBary       zBary        JD0
   -9.124094  -18.569125   -0.282775   -0.153062   -0.953885  2456921.581428
# Heliocentric elements and errors
Epoch:              2456920.5000  =  2014/09/20
Mean Anomaly:          209.46955 +/-   196.043
Argument of Peri:       66.74546 +/-   194.745
Long of Asc Node:       71.88859 +/-     0.262
Inclination:             8.95834 +/-     0.000
Eccentricity:         0.12902538 +/-    0.1646
Semi-Major Axis:     47.35046082 +/-    3.1143
Time of Perihelion: 2506683.5064 +/-   64622.5
Perihelion:          41.24104942 +/-    8.2505
Aphelion:            53.45987223 +/-    8.5485
Period (y)              325.8326 +/-     32.15
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           49.56017943 +/-    0.0550
Ecliptic Y          -16.34958182 +/-    0.0185
Ecliptic Z           -8.22674428 +/-    0.0093
Ecliptic XDOT         0.00057616 +/-    0.0011
Ecliptic YDOT         0.00214949 +/-    0.0004
Ecliptic ZDOT         0.00001901 +/-    0.0002
# Distances at JD0 (AU)
Heliocenter to KBO   52.83180418 +/-    0.0519
Geocenter to KBO     51.87962768 +/-    0.0588
# Hcoef:  7.77

The following table shows the complete astrometric record for 14SL350. 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 (14SL350) followed by the observatory code and reference code for the source of the astrometry.

2014 09  21.08065  23 05 50.327  -15 41 50.68  24.9r 14SL350   807  C~1x8m      
2014 09  21.17068  23 05 49.967  -15 41 52.41        14SL350   807  C~1x8m      
2014 09  21.23335  23 05 49.769  -15 41 53.83        14SL350   807  C~1x8m      
2014 10  26.02642  23 04 01.211  -15 49 11.02        14SL350   304  C~1x8m      
2014 10  26.06306  23 04 01.117  -15 49 10.99        14SL350   304  C~1x8m      
2014 11  19.08709  23 03 23.173  -15 48 53.64        14SL350   304  C~1x8m      
2014 11  20.08888  23 03 22.482  -15 48 46.68        14SL350   304  C~1x8m      

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     0.09       0.00     0.05
     2   0.0002     -5.46    -0.24       0.44     0.18
     3   0.0004     -8.65     0.15       0.26    -0.24
     4   0.0957  -1622.10     0.00     210.08    -0.10
     5   0.0958  -1623.34     0.01     210.64     0.13
     6   0.1616  -2121.02    -0.23     439.84     0.04
     7   0.1643  -2127.50     0.22     450.13    -0.06

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.

14SL350    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