Orbit Fit and Astrometric record for 11UG411

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: 11UG411   
# Created Fri Nov 22 02:09:14 2024
# Orbit generated from Bernstein formalism
# Fitting     21 observations of     21
# Arc:   3.96y
# First observation: 2011/10/25
#  Last observation: 2015/10/09
Preliminary a, adot, b, bdot, g, gdot:
  -0.000020   0.024509   0.000018  -0.004061   0.024106   0.000000
# Chi-squared of fit:     9.59 DOF:     36 RMS:  0.12
# Min/Max residuals:    -0.36    0.19
# Exact a, adot, b, bdot, g, gdot:
  1.669736E-05  2.463166E-02 -2.897062E-06 -4.084815E-03  2.439010E-02  1.913008E-03
# Covariance matrix:
  1.5138E-13 -1.6962E-13 -4.3096E-15  1.9856E-14  3.1797E-14 -1.2366E-12
 -1.6962E-13  5.3328E-13  2.1984E-14 -7.8524E-14  8.2297E-14  4.8584E-12
 -4.3096E-15  2.1984E-14  1.0834E-13 -4.2185E-14  1.2552E-14  2.2649E-13
  1.9856E-14 -7.8524E-14 -4.2185E-14  5.3702E-14 -1.9217E-14 -7.8155E-13
  3.1797E-14  8.2297E-14  1.2552E-14 -1.9217E-14  3.2214E-13  1.1424E-12
 -1.2366E-12  4.8584E-12  2.2649E-13 -7.8155E-13  1.1424E-12  4.8306E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
    5.223876   30.598394   -0.014933    0.090218   -0.986796  2455859.847326
# Heliocentric elements and errors
Epoch:              2455850.5000  =  2011/10/16
Mean Anomaly:           26.73299 +/-     0.062
Argument of Peri:      115.50644 +/-     0.091
Long of Asc Node:      238.89106 +/-     0.001
Inclination:            10.67085 +/-     0.000
Eccentricity:         0.14728220 +/-    0.0002
Semi-Major Axis:     48.04880379 +/-    0.0071
Time of Perihelion: 2446816.7647 +/-      20.9
Perihelion:          40.97207012 +/-    0.0125
Aphelion:            55.12553746 +/-    0.0136
Period (y)              333.0674 +/-      0.07
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           35.99313849 +/-    0.0008
Ecliptic Y           21.30198990 +/-    0.0005
Ecliptic Z            3.73285189 +/-    0.0001
Ecliptic XDOT        -0.00119105 +/-    0.0000
Ecliptic YDOT         0.00251516 +/-    0.0000
Ecliptic ZDOT        -0.00043701 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   41.99065343 +/-    0.0007
Geocenter to KBO     41.00024146 +/-    0.0010
# Hcoef:  8.62

The following table shows the complete astrometric record for 11UG411. 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 (11UG411) followed by the observatory code and reference code for the source of the astrometry.

2011 10  25.34656  01 46 19.042  +16 34 08.22  24.6r 11UG411   568  C~1C6N      
2011 10  25.39635  01 46 18.810  +16 34 06.75        11UG411   568  C~1C6N      
2011 10  25.40523  01 46 18.750  +16 34 06.61  24.4r 11UG411   568  C~1C6N      
2011 10  26.30517  01 46 14.568  +16 33 40.62  24.7r 11UG411   568  C~1C6N      
2011 10  26.34841  01 46 14.368  +16 33 39.68  24.8r 11UG411   568  C~1C6N      
2011 10  26.39151  01 46 14.160  +16 33 38.40  24.4r 11UG411   568  C~1C6N      
2011 10  31.39702  01 45 50.884  +16 31 13.97  25.5r 11UG411   568  C~1C6N      
2011 11  24.25792  01 44 09.322  +16 19 46.40        11UG411   568  C~1C6N      
2011 11  26.47841  01 44 01.137  +16 18 45.54  24.7r 11UG411   568  C~1C6N      
2012 01  25.30732  01 42 49.387  +16 02 37.26  25.0r 11UG411   568  C~1C6N      
2012 01  27.22612  01 42 52.560  +16 02 35.01  24.7r 11UG411   568  C~1C6N      
2012 08  24.45714  01 55 59.347  +17 10 07.67  24.8r 11UG411   568  C~1C6N      
2012 08  27.55400  01 55 53.049  +17 09 47.20        11UG411   568  C~1C6N      
2012 10  21.33604  01 52 25.906  +16 52 30.43  24.6r 11UG411   568  C~1C6N      
2012 10  21.36172  01 52 25.788  +16 52 29.86        11UG411   568  C~1C6N      
2012 10  21.38781  01 52 25.656  +16 52 28.99  25.1r 11UG411   568  C~1C6N      
2013 01  14.32680  01 48 21.481  +16 20 19.14        11UG411   568  C~1C6N      
2013 02  03.29696  01 48 49.256  +16 19 31.00        11UG411   568  C~1C6N      
2015 10  09.41854  02 10 54.178  +17 43 52.50  25.0w 11UG411   568  C~2jM3      
2015 10  09.46193  02 10 53.969  +17 43 51.63  25.0w 11UG411   568  C~2jM3      
2015 10  09.49526  02 10 53.821  +17 43 50.68  25.0w 11UG411   568  C~2jM3      

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    -0.15       0.00     0.05
     2   0.0001     -3.64    -0.10      -0.18    -0.03
     3   0.0002     -4.50    -0.29      -0.00     0.17
     4   0.0026    -69.94    -0.09      -2.80    -0.23
     5   0.0027    -72.96     0.09      -2.65     0.01
     6   0.0029    -76.21     0.04      -2.77    -0.02
     7   0.0166   -440.42     0.17     -17.99    -0.11
     8   0.0819  -2051.14     0.09    -135.58     0.05
     9   0.0880  -2182.99     0.00    -149.97     0.11
    10   0.2518  -3496.47     0.19    -680.53     0.10
    11   0.2570  -3454.62     0.03    -699.15     0.16
    12   0.8326   8562.36     0.07    -907.15    -0.07
    13   0.8411   8470.43    -0.04    -895.12    -0.09
    14   0.9911   5320.66     0.07    -833.00    -0.06
    15   0.9911   5318.88     0.17    -832.94     0.04
    16   0.9912   5316.80     0.02    -833.09    -0.07
    17   1.2238   1350.80     0.09   -1401.91    -0.06
    18   1.2784   1707.60    -0.36   -1588.72     0.01
    19   3.9564  21373.80     0.11   -3323.73    -0.03
    20   3.9565  21370.66    -0.04   -3323.57     0.14
    21   3.9566  21368.33    -0.07   -3323.77    -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.

11UG411    quality flag:3

Type:           2:1E      2:1E      2:1E

axisobj        48.161    48.183    48.139
ecceobj         0.150     0.150     0.149
incobj         10.667    10.667    10.667
qmin           39.462    39.269    39.158
qmax           56.645    56.750    56.993
amean          47.798    47.798    47.798
amin           47.342    47.366    47.340
amax           48.304    48.272    48.322
emean           0.143     0.145     0.143
emin            0.105     0.109     0.101
emax            0.174     0.176     0.180
imean          12.049    12.017    12.080
imin           11.275    11.308    11.266
imax           12.876    12.868    13.025
excite_mean     0.253     0.254     0.254
fracstop        1.000     1.000     1.000
cjmean          3.068     3.067     3.068

libcent 0        92.2      89.7      94.4
libamp  0        32.5      24.5      40.6
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       176.9     183.0     184.8
kozaiamp        180.0     180.0     180.0