Orbit Fit and Astrometric record for 14SB349

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: 14SB349   
# Created Fri Nov 22 02:10:00 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     35 observations of     35
# Arc:   9.29y
# First observation: 2014/09/24
#  Last observation: 2024/01/09
# Chi-squared of fit:    30.03 DOF:     64 RMS:  0.16
# Min/Max residuals:    -0.47    0.39
# Exact a, adot, b, bdot, g, gdot:
  1.980511E-05  5.448055E-02  1.367098E-06  1.970249E-03  4.224217E-02 -8.110466E-03
# Covariance matrix:
  1.9543E-13 -1.3937E-13  6.7751E-15 -6.2391E-15 -2.2200E-14 -2.2191E-13
 -1.3937E-13  1.8847E-13 -8.0505E-15  6.3644E-15  1.3619E-13  2.8782E-13
  6.7751E-15 -8.0505E-15  6.7947E-14 -1.2747E-14 -3.8310E-15 -1.3327E-14
 -6.2391E-15  6.3644E-15 -1.2747E-14  5.7996E-15  1.4241E-15  1.1029E-14
 -2.2200E-14  1.3619E-13 -3.8310E-15  1.4241E-15  2.3275E-13  1.7389E-13
 -2.2191E-13  2.8782E-13 -1.3327E-14  1.1029E-14  1.7389E-13  4.6513E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
  -15.958077   35.266550    0.567942   -0.228032   -0.798015  2456924.791368
# Heliocentric elements and errors
Epoch:              2456924.5000  =  2014/09/24
Mean Anomaly:          297.76377 +/-     0.006
Argument of Peri:      358.55861 +/-     0.008
Long of Asc Node:      117.27261 +/-     0.000
Inclination:            15.51895 +/-     0.000
Eccentricity:         0.17984213 +/-    0.0000
Semi-Major Axis:     25.91486019 +/-    0.0011
Time of Perihelion: 2465254.8359 +/-       2.6
Perihelion:          21.25427647 +/-    0.0010
Aphelion:            30.57544391 +/-    0.0013
Period (y)              131.9263 +/-      0.01
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           19.58645260 +/-    0.0002
Ecliptic Y           13.15884192 +/-    0.0002
Ecliptic Z           -6.50851825 +/-    0.0001
Ecliptic XDOT        -0.00242741 +/-    0.0000
Ecliptic YDOT         0.00260690 +/-    0.0000
Ecliptic ZDOT         0.00026741 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   24.47752294 +/-    0.0002
Geocenter to KBO     23.67313101 +/-    0.0003
# Hcoef:  9.41

The following table shows the complete astrometric record for 14SB349. 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 (14SB349) followed by the observatory code and reference code for the source of the astrometry.

2014 09  24.290590 02 32 58.19   -01 48 03.7         14SB349   W84  C~1bR3      
2014 09  24.291991 02 32 58.18   -01 48 03.9         14SB349   W84  C~1bR3      
2014 10  01.374641 02 32 16.87   -01 54 01.9         14SB349   W84  C~1bR3      
2014 10  23.308565 02 29 43.85   -02 11 01.2         14SB349   W84  C~1bR3      
2014 10  29.294468 02 28 58.20   -02 14 57.6         14SB349   W84  C~1bR3      
2015 08  31.295440 02 46 11.70   -00 20 56.6   23.1z 14SB349   W84  C~1bR3      
2015 09  19.327002 02 45 09.18   -00 35 56.9   24.3r 14SB349   W84  C~1bR3      
2015 09  19.329363 02 45 09.18   -00 35 57.2   23.1i 14SB349   W84  C~1bR3      
2015 09  26.227500 02 44 34.75   -00 41 39.1   23.8i 14SB349   W84  C~1bR3      
2015 09  26.231285 02 44 34.75   -00 41 39.6   22.7z 14SB349   W84  C~1bR3      
2015 10  09.208461 02 43 16.09   -00 52 13.7   22.9r 14SB349   W84  C~1bR3      
2015 10  09.210810 02 43 16.09   -00 52 13.8   22.9i 14SB349   W84  C~1bR3      
2015 10  16.294670 02 42 26.93   -00 57 42.8   23.8g 14SB349   W84  C~1bR3      
2015 10  16.296875 02 42 26.93   -00 57 42.9   22.7r 14SB349   W84  C~1bR3      
2015 10  16.299225 02 42 26.91   -00 57 43.0   23.0i 14SB349   W84  C~1bR3      
2015 10  16.303032 02 42 26.89   -00 57 43.2   22.9z 14SB349   W84  C~1bR3      
2015 10  20.211296 02 41 58.39   -01 00 36.0   22.8i 14SB349   W84  C~1bR3      
2015 10  20.215104 02 41 58.37   -01 00 36.2   23.6z 14SB349   W84  C~1bR3      
2016 01  15.23241  02 33 38.31   -01 08 50.5   24.0z 14SB349   T09  C~8Afo      
2016 01  15.25231  02 33 38.27   -01 08 49.8   23.5z 14SB349   T09  C~8Afo      
2016 01  15.29336  02 33 38.24   -01 08 48.3   24.3z 14SB349   T09  C~8Afo      
2016 10  20.272743 02 53 54.17   +00 08 11.4   23.0i 14SB349   W84  C~2Azv      
2016 10  20.279363 02 53 54.17   +00 08 11.4   22.7z 14SB349   W84  C~2Azv      
2016 10  27.115301 02 53 02.55   +00 03 31.5   23.0r 14SB349   W84  C~2Azv      
2016 11  10.109769 02 51 12.58   -00 04 30.4   22.8i 14SB349   W84  C~2Azv      
2016 11  10.116400 02 51 12.55   -00 04 30.5   22.6z 14SB349   W84  C~2Azv      
2016 12  17.173704 02 46 53.32   -00 11 52.0   22.8i 14SB349   W84  C~2Azv      
2016 12  17.180336 02 46 53.31   -00 11 51.9   22.5z 14SB349   W84  C~2Azv      
2016 12  24.046597 02 46 19.09   -00 10 37.9   22.8r 14SB349   W84  C~2Azv      
2017 01  03.081250 02 45 40.52   -00 07 20.4   23.2r 14SB349   W84  C~2Azv      
2017 01  03.083611 02 45 40.50   -00 07 20.1   22.9i 14SB349   W84  C~2Azv      
2017 01  03.087593 02 45 40.48   -00 07 20.1   22.6z 14SB349   W84  C~2Azv      
2024 01  09.150700 04 14 42.405  +08 16 30.34  23.0G 14SB349   G37  C~7gqt      
2024 01  09.264930 04 14 41.727  +08 16 32.21        14SB349   G37  C~7gqt      
2024 01  09.379110 04 14 41.060  +08 16 33.77        14SB349   G37  C~7gqt      

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     0.16       0.00    -0.08
     2   0.0000      0.00     0.12       0.00    -0.21
     3   0.0194      0.00     0.39       0.00    -0.04
     4   0.0794      0.00    -0.14       0.00     0.22
     5   0.0958      0.00    -0.05       0.00    -0.29
     6   0.9336      0.00    -0.10       0.00     0.14
     7   0.9857      0.00    -0.26       0.00     0.14
     8   0.9857      0.00    -0.09       0.00    -0.04
     9   1.0046      0.00    -0.19       0.00     0.03
    10   1.0046      0.00     0.13       0.00    -0.28
    11   1.0402      0.00    -0.06       0.00     0.04
    12   1.0402      0.00     0.18       0.00     0.05
    13   1.0596      0.00    -0.19       0.00     0.03
    14   1.0596      0.00     0.05       0.00     0.03
    15   1.0596      0.00     0.01       0.00     0.04
    16   1.0596      0.00     0.12       0.00     0.01
    17   1.0703      0.00    -0.06       0.00    -0.00
    18   1.0703      0.00     0.07       0.00    -0.04
    19   1.3085      0.00     0.16       0.00    -0.14
    20   1.3086      0.00    -0.15       0.00    -0.20
    21   1.3087      0.00     0.01       0.00    -0.28
    22   2.0725      0.00    -0.47       0.00    -0.16
    23   2.0725      0.00     0.27       0.00     0.12
    24   2.0912      0.00     0.20       0.00    -0.00
    25   2.1296      0.00    -0.08       0.00     0.02
    26   2.1296      0.00     0.27       0.00     0.12
    27   2.2310      0.00    -0.16       0.00     0.13
    28   2.2310      0.00     0.24       0.00     0.19
    29   2.2498      0.00     0.01       0.00     0.24
    30   2.2773      0.00     0.06       0.00     0.05
    31   2.2773      0.00    -0.12       0.00     0.29
    32   2.2773      0.00    -0.23       0.00     0.19
    33   9.2919      0.00     0.00       0.00    -0.02
    34   9.2922      0.00    -0.01       0.00     0.03
    35   9.2925      0.00     0.04       0.00    -0.21

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.

14SB349    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        26.041    26.040    26.041
ecceobj         0.177     0.177     0.177
incobj         15.521    15.521    15.521
qmin           21.322    18.116    21.322
qmax           30.741    30.987    30.742
amean          25.960    24.024    25.961
amin           25.664    22.961    25.664
amax           26.327    26.324    26.333
emean           0.167     0.205     0.167
emin            0.153     0.153     0.152
emax            0.177     0.250     0.177
imean          13.949    12.748    13.949
imin           13.839    11.510    13.835
imax           13.995    14.032    13.995
excite_mean     0.293     0.302     0.293
fracstop        0.002     0.028     0.002
cjmean          2.938     2.958     2.938

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        21.2     157.7      21.3
kozaiamp        178.2     178.2     178.2