Orbit Fit and Astrometric record for 99CB119

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: 99CB119   
# Created Sun Nov 24 02:07:55 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     37 observations of     37
# Arc:  23.16y
# First observation: 1999/02/10
#  Last observation: 2022/04/08
# Chi-squared of fit:    42.48 DOF:     68 RMS:  0.19
# Min/Max residuals:    -0.79    0.44
# Exact a, adot, b, bdot, g, gdot:
  1.678664E-05  2.577841E-02  3.004784E-06  3.966229E-03  2.499315E-02  6.790833E-04
# Covariance matrix:
  1.4502E-13 -1.7453E-14  5.0338E-15 -2.0751E-15  5.1558E-14 -2.3100E-14
 -1.7453E-14  6.4798E-15 -2.1727E-15  9.2460E-16  5.5741E-15  1.0229E-14
  5.0338E-15 -2.1727E-15  9.5162E-14 -6.1038E-15 -3.9185E-16 -3.8397E-15
 -2.0751E-15  9.2460E-16 -6.1038E-15  7.2347E-16  3.1940E-16  1.6271E-15
  5.1558E-14  5.5741E-15 -3.9185E-16  3.1940E-16  1.4776E-13  3.2062E-15
 -2.3100E-14  1.0229E-14 -3.8397E-15  1.6271E-15  3.2062E-15  1.8015E-14
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.280473  166.928455    0.425644   -0.004618   -0.897426  2451219.940773
# Heliocentric elements and errors
Epoch:              2451220.5000  =  1999/02/11
Mean Anomaly:            6.90690 +/-     0.003
Argument of Peri:      349.28462 +/-     0.004
Long of Asc Node:      168.10758 +/-     0.000
Inclination:             8.77211 +/-     0.000
Eccentricity:         0.12380088 +/-    0.0001
Semi-Major Axis:     46.61964266 +/-    0.0034
Time of Perihelion: 2448989.8456 +/-       1.0
Perihelion:          40.84808988 +/-    0.0038
Aphelion:            52.39119544 +/-    0.0045
Period (y)              318.3183 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -39.74352055 +/-    0.0006
Ecliptic Y            9.66607312 +/-    0.0001
Ecliptic Z           -0.19573684 +/-    0.0000
Ecliptic XDOT        -0.00071488 +/-    0.0000
Ecliptic YDOT        -0.00272438 +/-    0.0000
Ecliptic ZDOT         0.00043411 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.90254014 +/-    0.0006
Geocenter to KBO     40.01096909 +/-    0.0006
# Hcoef:  7.11

The following table shows the complete astrometric record for 99CB119. 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 (99CB119) followed by the observatory code and reference code for the source of the astrometry.

1999 02  10.44003  11 11 27.56   +04 54 11.4   22.7R 99CB119   568  Ca4178      
1999 02  10.48103  11 11 27.37   +04 54 11.8   22.7R 99CB119   568  Ca4178      
1999 02  18.52084  11 10 53.80   +04 58 02.7   22.7R 99CB119   568  Ca4178      
1999 02  18.53244  11 10 53.74   +04 58 03.0   22.7R 99CB119   568  Ca4178      
1999 03  10.50725  11 09 23.92   +05 08 16.5   22.7R 99CB119   568  Ca4506      
1999 04  12.51044  11 07 06.46   +05 24 04.1   22.5R 99CB119   568  Ca4506      
1999 04  13.45486  11 07 03.21   +05 24 27.0   22.5R 99CB119   568  Ca4506      
2000 04  07.40590  11 13 10.26   +05 00 28.5   23.0R 99CB119   568  Cd0744      
2000 04  07.45841  11 13 10.04   +05 00 30.1   23.0R 99CB119   568  Cd0744      
2001 02  20.427681 11 22 20.00   +04 15 12.9   22.9V 99CB119   645  C~1cF1      
2001 02  20.428510 11 22 20.00   +04 15 12.9   22.4V 99CB119   645  C~1cF1      
2001 02  20.430998 11 22 19.99   +04 15 13.0   24.2V 99CB119   645  C~1cF1      
2001 02  25.55225  11 21 57.74   +04 17 48.6   22.9R 99CB119   568  Cd0744      
2001 02  25.59795  11 21 57.55   +04 17 49.8         99CB119   568  Cd0744      
2006 01  07.510011 11 53 05.71   +02 07 23.6   23.0V 99CB119   645  C~1cF1      
2006 01  07.510840 11 53 05.71   +02 07 23.6   22.7V 99CB119   645  C~1cF1      
2006 01  07.513328 11 53 05.71   +02 07 23.6   24.4V 99CB119   645  C~1cF1      
2007 04  15.203137 11 53 08.10   +02 26 40.3         99CB119   645  C~1cF1      
2007 04  15.203958 11 53 08.09   +02 26 40.3         99CB119   645  C~1cF1      
2007 04  15.206447 11 53 08.09   +02 26 40.4         99CB119   645  C~1cF1      
2007 06  15.97937  11 51 11.64   +02 39 36.4         99CB119   304  Cv1518      
2007 06  16.05278  11 51 11.69   +02 39 36.1         99CB119   304  Cv1518      
2013 03  14.29017  12 29 28.64   -00 05 16.3   22.5R 99CB119   695  C~0uco      
2013 03  14.39987  12 29 28.16   -00 05 12.9         99CB119   695  C~0uco      
2013 03  14.46026  12 29 27.90   -00 05 11.1         99CB119   695  C~0uco      
2016 02  04.44520  12 48 22.56   -01 29 29.6   23.4R 99CB119   G37  C~1lut      
2016 02  04.49965  12 48 22.44   -01 29 28.1         99CB119   G37  C~1lut      
2016 04  04.43375  12 44 46.74   -01 01 59.4   24.5g 99CB119   T09  C~8CLR      
2016 04  04.47417  12 44 46.56   -01 01 58.2   24.3g 99CB119   T09  C~8CLR      
2016 04  04.50883  12 44 46.40   -01 01 57.2   24.6g 99CB119   T09  C~8CLR      
2016 04  04.54725  12 44 46.22   -01 01 56.0   24.2g 99CB119   T09  C~8CLR      
2017 04  27.37712  12 48 45.73   -01 13 52.7   22.7i 99CB119   T09  C~7xIi      
2017 04  27.40547  12 48 45.62   -01 13 52.1   22.6i 99CB119   T09  C~7xIi      
2017 04  27.42903  12 48 45.53   -01 13 51.4   22.7i 99CB119   T09  C~7xIi      
2022 04  08.247920 13 17 49.798  -03 12 21.07  23.1G 99CB119   G37  C~5ZUp      
2022 04  08.288530 13 17 49.626  -03 12 20.10        99CB119   G37  C~5ZUp      
2022 04  08.329260 13 17 49.445  -03 12 18.82        99CB119   G37  C~5ZUp      

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    -0.13       0.00    -0.06
     2   0.0001      0.00    -0.46       0.00    -0.79
     3   0.0221      0.00     0.09       0.00     0.11
     4   0.0222      0.00    -0.05       0.00     0.07
     5   0.0768      0.00     0.08       0.00     0.44
     6   0.1672      0.00    -0.00       0.00    -0.05
     7   0.1698      0.00     0.16       0.00    -0.13
     8   1.1553      0.00    -0.03       0.00    -0.14
     9   1.1554      0.00    -0.29       0.00     0.08
    10   2.0287      0.00    -0.03       0.00    -0.23
    11   2.0287      0.00     0.03       0.00    -0.26
    12   2.0287      0.00     0.04       0.00    -0.23
    13   2.0427      0.00     0.18       0.00     0.40
    14   2.0429      0.00     0.41       0.00     0.20
    15   6.9078      0.00    -0.07       0.00     0.07
    16   6.9078      0.00    -0.06       0.00     0.06
    17   6.9078      0.00    -0.03       0.00     0.04
    18   8.1746      0.00     0.03       0.00    -0.08
    19   8.1746      0.00    -0.08       0.00    -0.10
    20   8.1746      0.00     0.07       0.00    -0.07
    21   8.3437      0.00     0.11       0.00     0.25
    22   8.3439      0.00     0.27       0.00     0.26
    23  14.0886      0.00     0.01       0.00     0.17
    24  14.0889      0.00    -0.00       0.00     0.16
    25  14.0890      0.00     0.05       0.00     0.09
    26  16.9829      0.00     0.18       0.00    -0.16
    27  16.9831      0.00    -0.03       0.00     0.31
    28  17.1471      0.00    -0.11       0.00     0.07
    29  17.1473      0.00    -0.06       0.00     0.05
    30  17.1473      0.00    -0.12       0.00     0.01
    31  17.1475      0.00    -0.22       0.00     0.05
    32  18.2093      0.00    -0.06       0.00     0.06
    33  18.2094      0.00     0.01       0.00    -0.05
    34  18.2094      0.00     0.10       0.00     0.07
    35  23.1562      0.00    -0.11       0.00    -0.12
    36  23.1563      0.00     0.05       0.00    -0.34
    37  23.1564      0.00     0.09       0.00    -0.25

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.

99CB119    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        46.722    46.722    46.722
ecceobj         0.126     0.126     0.126
incobj          8.767     8.767     8.767
qmin           40.206    40.206    40.207
qmax           54.148    54.143    54.154
amean          46.980    46.980    46.980
amin           46.576    46.579    46.576
amax           47.439    47.439    47.437
emean           0.129     0.129     0.129
emin            0.116     0.117     0.116
emax            0.142     0.142     0.142
imean           8.257     8.257     8.257
imin            7.884     7.887     7.882
imax            8.620     8.620     8.621
excite_mean     0.193     0.193     0.193
fracstop        1.000     1.000     1.000
cjmean          3.092     3.092     3.092

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       170.9     170.8     170.9
kozaiamp        180.0     180.0     180.0