Orbit Fit and Astrometric record for 99SA28

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: 99SA28    
# Created Wed Apr 24 01:09:58 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:  23.86h
# First observation: 1999/09/16
#  Last observation: 1999/09/17
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit:     2.85 DOF:      8 RMS:  0.12
# Min/Max residuals:    -0.20    0.20
# Exact a, adot, b, bdot, g, gdot:
  1.746372E-05  3.526469E-02  6.554054E-07  1.942066E-03  3.161975E-02  0.000000E+00
# Covariance matrix:
  4.9308E-11  9.7423E-08  3.1357E-12  6.2831E-09  1.6500E-08  0.0000E+00
  9.7423E-08  1.9445E-04  6.2469E-09  1.2517E-05  3.2870E-05  0.0000E+00
  3.1357E-12  6.2469E-09  5.4686E-13  2.8485E-10  1.0567E-09  0.0000E+00
  6.2831E-09  1.2517E-05  2.8485E-10  9.4287E-07  2.1174E-06  0.0000E+00
  1.6500E-08  3.2870E-05  1.0567E-09  2.1174E-06  5.5603E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  4.1600E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   10.999482  -24.228538   -0.292738    0.181840   -0.936772  2451437.791233
# Heliocentric elements and errors
Epoch:              2451430.5000  =  1999/09/09
Mean Anomaly:           10.65748 +/-   219.413
Argument of Peri:       62.67736 +/-   287.162
Long of Asc Node:      262.46779 +/-     3.326
Inclination:            11.10536 +/-     0.176
Eccentricity:         0.03394690 +/-    0.5868
Semi-Major Axis:     33.69297938 +/-   18.0399
Time of Perihelion: 2449315.7471 +/-  186399.0
Perihelion:          32.54920701 +/-   26.3562
Aphelion:            34.83675175 +/-   27.1816
Period (y)              195.5768 +/-    157.07
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           29.30846007 +/-    2.1112
Ecliptic Y          -12.86227633 +/-    0.9503
Ecliptic Z            6.03424884 +/-    0.4500
Ecliptic XDOT         0.00121961 +/-    0.0016
Ecliptic YDOT         0.00280593 +/-    0.0011
Ecliptic ZDOT         0.00016513 +/-    0.0003
# Distances at JD0 (AU)
Heliocenter to KBO   32.57047962 +/-    1.9382
Geocenter to KBO     31.62580101 +/-    2.3585
# Hcoef:  7.17

The following table shows the complete astrometric record for 99SA28. 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 (99SA28) followed by the observatory code and reference code for the source of the astrometry.

1999 09  16.29049  22 14 10.08   +00 50 56.1   23.1  99SA28    568  Cd1603      
1999 09  16.29854  22 14 10.04   +00 50 55.9   23.2  99SA28    568  Cd1603      
1999 09  16.30659  22 14 09.99   +00 50 55.2         99SA28    568  Cd1603      
1999 09  17.26864  22 14 04.99   +00 50 20.3         99SA28    568  Cd1604      
1999 09  17.27659  22 14 04.96   +00 50 20.1         99SA28    568  Cd1604      
1999 09  17.28460  22 14 04.93   +00 50 19.9         99SA28    568  Cd1604      

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     0.04       0.00     0.07
     2   0.0000     -0.63     0.11       0.03     0.14
     3   0.0000     -1.58    -0.14      -0.35    -0.20
     4   0.0027    -84.13    -0.20      -5.67    -0.02
     5   0.0027    -84.62    -0.00      -5.69     0.00
     6   0.0027    -85.11     0.20      -5.71     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.

99SA28    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