Orbit Fit and Astrometric record for 99CX118

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: 99CX118   
# Created Wed Nov 27 02:07:55 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:  61.99d
# First observation: 1999/02/10
#  Last observation: 1999/04/13
Preliminary a, adot, b, bdot, g, gdot:
  -0.000000   0.018271   0.000001   0.000653   0.022264   0.000000
# WARNING MRQMIN stopped after  13 iterations -- oscilliatory solution
# WARNING Fitting with energy constraint
# Chi-squared of fit:     1.57 DOF:      7 RMS:  0.09
# Min/Max residuals:    -0.14    0.22
# Exact a, adot, b, bdot, g, gdot:
  1.235724E-05  1.740139E-02  1.155244E-06  6.518841E-04  2.207838E-02 -1.115411E-02
# Covariance matrix:
  6.2455E-12  8.3523E-09  8.9845E-14  3.2863E-12  1.4863E-09  3.0783E-08
  8.3523E-09  1.2591E-05  1.3718E-10  4.6710E-09  2.2316E-06  4.3942E-05
  8.9845E-14  1.3718E-10  4.1856E-13 -2.6789E-12  2.4289E-11  4.7199E-10
  3.2863E-12  4.6710E-09 -2.6789E-12  4.4945E-11  8.3147E-10  1.7368E-08
  1.4863E-09  2.2316E-06  2.4289E-11  8.3147E-10  3.9561E-07  7.8195E-06
  3.0783E-08  4.3942E-05  4.7199E-10  1.7368E-08  7.8195E-06  1.6263E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.135046  172.102235    0.503956   -0.002248   -0.855931  2451219.999173
# Heliocentric elements and errors
Epoch:              2451210.5000  =  1999/02/01
Mean Anomaly:          303.35288 +/-    55.169
Argument of Peri:      118.22180 +/-     7.113
Long of Asc Node:      174.96793 +/-     0.723
Inclination:             2.17387 +/-     0.461
Eccentricity:         0.54949264 +/-    0.5214
Semi-Major Axis:     47.00723125 +/-   24.3088
Time of Perihelion: 2469733.9042 +/-   10908.0
Perihelion:          21.17710368 +/-   26.8465
Aphelion:            72.83735883 +/-   44.9395
Period (y)              322.2962 +/-    250.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -45.63378577 +/-    1.2781
Ecliptic Y            6.83983284 +/-    0.1774
Ecliptic Z           -0.10669547 +/-    0.0030
Ecliptic XDOT         0.00107168 +/-    0.0017
Ecliptic YDOT        -0.00231842 +/-    0.0002
Ecliptic ZDOT         0.00008410 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.14365721 +/-    1.2642
Geocenter to KBO     45.29316815 +/-    1.2903
# Hcoef:  6.96

The following table shows the complete astrometric record for 99CX118. 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 (99CX118) followed by the observatory code and reference code for the source of the astrometry.

1999 02  10.49843  11 30 46.40   +03 00 32.7   23.0R 99CX118   568  Ca4013      
1999 02  10.54462  11 30 46.23   +03 00 33.8   23.0R 99CX118   568  Ca4013      
1999 02  18.58637  11 30 16.32   +03 03 48.8   23.0R 99CX118   568  Ca4013      
1999 02  18.59797  11 30 16.28   +03 03 49.2   23.0R 99CX118   568  Ca4013      
1999 04  13.41191  11 26 38.40   +03 27 30.1   23.8R 99CX118   568  Ca4506      
1999 04  13.48486  11 26 38.14   +03 27 31.7   23.8R 99CX118   568  Ca4506      

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     0.02       0.00    -0.14
     2   0.0001     -2.77    -0.02       0.01    -0.13
     3   0.0221   -491.39    -0.02       2.45     0.09
     4   0.0222   -492.09     0.02       2.58     0.22
     5   0.1695  -4051.42    -0.02      22.83     0.01
     6   0.1697  -4055.63     0.02      22.76    -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.

99CX118    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