Orbit Fit and Astrometric record for 149349

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: 149349    
# Created Sat Apr 27 01:07:32 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     50 observations of     50
# Arc:  21.03y
# First observation: 2002/11/09
#  Last observation: 2023/11/19
# Chi-squared of fit:    78.58 DOF:     94 RMS:  0.22
# Min/Max residuals:    -0.87    0.52
# Exact a, adot, b, bdot, g, gdot:
  1.455172E-05  2.514150E-02 -4.175966E-06 -2.984892E-03  2.558398E-02 -6.315812E-03
# Covariance matrix:
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.039617   27.762341   -0.314699    0.033290   -0.935619  2452587.704403
# Heliocentric elements and errors
Epoch:              2452588.5000  =  2002/11/10
Mean Anomaly:          296.98235 +/-     0.000
Argument of Peri:      254.24574 +/-     0.000
Long of Asc Node:      224.52944 +/-     0.000
Inclination:             7.05914 +/-     0.000
Eccentricity:         0.24322898 +/-    0.0000
Semi-Major Axis:     42.42075347 +/-    0.0000
Time of Perihelion: 2470253.9911 +/-       0.0
Perihelion:          32.10279680 +/-    0.0000
Aphelion:            52.73871014 +/-    0.0000
Period (y)              276.2967 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           35.24626513 +/-    0.0000
Ecliptic Y           18.91542908 +/-    0.0000
Ecliptic Z            1.39097674 +/-    0.0000
Ecliptic XDOT        -0.00184832 +/-    0.0000
Ecliptic YDOT         0.00206800 +/-    0.0000
Ecliptic ZDOT        -0.00034307 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   40.02548448 +/-    0.0000
Geocenter to KBO     39.08716383 +/-    0.0000
# Hcoef:  6.51

The following table shows the complete astrometric record for 149349. 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 (149349) followed by the observatory code and reference code for the source of the astrometry.

2002 11  09.20366  01 40 07.30   +12 34 52.3   22.2R 149349    695  Cg8319      
2002 11  09.28734  01 40 06.92   +12 34 49.6         149349    695  Cg8319      
2002 11  30.27880  01 38 42.46   +12 25 35.4   22.6R 149349    568  Cg8319      
2002 11  30.34751  01 38 42.22   +12 25 33.8         149349    568  Cg8319      
2002 12  01.27244  01 38 39.10   +12 25 12.2         149349    568  Cg8319      
2003 10  23.18473  01 47 18.51   +13 04 45.0   21.9R 149349    695  Cj4694      
2003 10  23.27963  01 47 18.04   +13 04 42.2         149349    695  Cj4694      
2003 11  24.15715  01 44 51.95   +12 49 40.9   21.8R 149349    695  Cj4694      
2003 11  24.22581  01 44 51.67   +12 49 38.4         149349    695  Cj4694      
2004 11  09.18308  01 51 46.24   +13 17 22.8   22.0R 149349    695  Cl9844      
2004 11  10.25916  01 51 41.17   +13 16 52.2         149349    695  Cl9844      
2005 09  30.33653  02 00 59.35   +13 56 52.3   22.6R 149349    688  Co3857      
2005 09  30.42808  02 00 58.90   +13 56 50.2         149349    688  Co3857      
2006 12  24.11328  02 01 03.73   +13 42 02.1   22.7R 149349    688  Ct2062      
2006 12  24.22147  02 01 03.44   +13 42 00.8         149349    688  Ct2062      
2010 11  03.44841  02 29 38.054  +15 21 16.71  22.5w 149349    F51  C~1vqk      
2010 11  03.47391  02 29 37.924  +15 21 16.05  22.1w 149349    F51  C~1vqk      
2010 11  03.48655  02 29 37.857  +15 21 15.48  22.6w 149349    F51  C~1vqk      
2012 12  07.23645  02 40 03.893  +15 44 01.86  22.3w 149349    F51  C~1vqk      
2012 12  07.25146  02 40 03.821  +15 44 01.80  22.6w 149349    F51  C~1vqk      
2012 12  07.26642  02 40 03.781  +15 44 01.43  22.4w 149349    F51  C~1vqk      
2012 12  07.28150  02 40 03.697  +15 44 01.18  22.4w 149349    F51  C~1vqk      
2013 10  05.51606  02 52 06.78   +16 27 38.5   21.9R 149349    695  C~0zw1      
2013 10  06.35505  02 52 03.13   +16 27 20.7         149349    695  C~0zw1      
2013 10  06.47497  02 52 02.62   +16 27 18.3         149349    695  C~0zw1      
2013 11  24.29410  02 47 51.858  +16 07 07.03  22.3w 149349    F51  C~1vqk      
2013 11  24.30739  02 47 51.784  +16 07 06.69  22.4w 149349    F51  C~1vqk      
2013 11  24.32069  02 47 51.710  +16 07 06.24  22.5w 149349    F51  C~1vqk      
2013 11  24.33403  02 47 51.655  +16 07 05.89  22.4w 149349    F51  C~1vqk      
2014 07  28.60597  03 00 18.335  +16 52 39.66  22.4w 149349    F51  C~1vqk      
2014 07  28.60861  03 00 18.351  +16 52 39.62  22.5w 149349    F51  C~1vqk      
2014 07  28.61125  03 00 18.357  +16 52 40.04  22.5w 149349    F51  C~1vqk      
2014 07  28.61387  03 00 18.368  +16 52 40.08  22.3w 149349    F51  C~1vqk      
2014 11  17.46323  02 55 21.892  +16 27 18.09  22.4w 149349    F51  C~1vqk      
2014 11  17.47689  02 55 21.790  +16 27 17.81  22.5w 149349    F51  C~1vqk      
2014 11  17.49059  02 55 21.709  +16 27 17.70  22.4w 149349    F51  C~1vqk      
2014 11  17.50426  02 55 21.651  +16 27 16.98  22.5w 149349    F51  C~1vqk      
2014 12  13.34976  02 53 14.755  +16 17 17.34  22.5w 149349    F51  C~1vqk      
2014 12  13.36267  02 53 14.702  +16 17 16.87  22.4w 149349    F51  C~1vqk      
2014 12  13.37561  02 53 14.651  +16 17 16.61  22.4w 149349    F51  C~1vqk      
2017 08  19.60939  03 21 40.556  +17 38 22.96        149349    568  C~2N74      
2023 11  18.80420  04 02 04.90   +18 26 20.7   22.0w 149349    O18  C~7aHP      
2023 11  18.80528  04 02 04.89   +18 26 20.4   22.4w 149349    O18  C~7aHP      
2023 11  18.81068  04 02 04.85   +18 26 20.5   22.0w 149349    O18  C~7aHP      
2023 11  18.81175  04 02 04.85   +18 26 20.5   22.5w 149349    O18  C~7aHP      
2023 11  18.81707  04 02 04.82   +18 26 20.2   21.9w 149349    O18  C~7aHP      
2023 11  18.81812  04 02 04.81   +18 26 20.1   22.3w 149349    O18  C~7aHP      
2023 11  19.85147  04 01 58.73   +18 26 00.3   21.9w 149349    O18  C~7aHP      
2023 11  19.85803  04 01 58.70   +18 26 00.2   21.6w 149349    O18  C~7aHP      
2023 11  19.86458  04 01 58.65   +18 26 00.1   22.0w 149349    O18  C~7aHP      

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     0.52
     2   0.0002      0.00     0.10       0.00     0.22
     3   0.0577      0.00     0.33       0.00    -0.41
     4   0.0579      0.00     0.33       0.00    -0.40
     5   0.0604      0.00     0.26       0.00    -0.47
     6   0.9527      0.00    -0.02       0.00    -0.11
     7   0.9530      0.00     0.04       0.00    -0.15
     8   1.0403      0.00    -0.32       0.00     0.22
     9   1.0404      0.00    -0.37       0.00    -0.52
    10   2.0013      0.00     0.51       0.00     0.11
    11   2.0043      0.00     0.09       0.00     0.09
    12   2.8915      0.00     0.06       0.00     0.05
    13   2.8918      0.00    -0.49       0.00     0.19
    14   4.1230      0.00     0.04       0.00     0.03
    15   4.1233      0.00    -0.87       0.00     0.33
    16   7.9842      0.00     0.04       0.00    -0.01
    17   7.9843      0.00     0.13       0.00     0.03
    18   7.9843      0.00     0.14       0.00    -0.19
    19  10.0781      0.00    -0.07       0.00    -0.07
    20  10.0782      0.00    -0.17       0.00     0.20
    21  10.0782      0.00     0.22       0.00     0.16
    22  10.0782      0.00    -0.05       0.00     0.24
    23  10.9057      0.00    -0.29       0.00     0.25
    24  10.9080      0.00    -0.44       0.00     0.18
    25  10.9083      0.00    -0.05       0.00     0.34
    26  11.0420      0.00     0.10       0.00     0.09
    27  11.0420      0.00     0.02       0.00     0.08
    28  11.0421      0.00    -0.06       0.00    -0.05
    29  11.0421      0.00     0.16       0.00    -0.07
    30  11.7164      0.00    -0.03       0.00    -0.12
    31  11.7164      0.00     0.12       0.00    -0.18
    32  11.7164      0.00     0.11       0.00     0.22
    33  11.7164      0.00     0.19       0.00     0.24
    34  12.0226      0.00     0.39       0.00    -0.26
    35  12.0227      0.00    -0.02       0.00    -0.20
    36  12.0227      0.00    -0.11       0.00     0.04
    37  12.0227      0.00     0.14       0.00    -0.33
    38  12.0935      0.00    -0.10       0.00     0.19
    39  12.0935      0.00    -0.06       0.00    -0.02
    40  12.0936      0.00     0.02       0.00    -0.02
    41  14.7773      0.00     0.08       0.00    -0.06
    42  21.0256      0.00     0.04       0.00     0.11
    43  21.0256      0.00    -0.01       0.00    -0.17
    44  21.0256      0.00    -0.13       0.00     0.04
    45  21.0256      0.00    -0.03       0.00     0.06
    46  21.0256      0.00    -0.01       0.00    -0.14
    47  21.0256      0.00    -0.06       0.00    -0.22
    48  21.0285      0.00    -0.03       0.00    -0.06
    49  21.0285      0.00     0.11       0.00    -0.03
    50  21.0285      0.00    -0.06       0.00    -0.00

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.

149349    quality flag:3

Type:          5:3EE     5:3EE     5:3EE

axisobj        42.658    42.658    42.658
ecceobj         0.241     0.241     0.241
incobj          7.046     7.046     7.046
qmin           31.662    31.662    31.662
qmax           53.362    53.361    53.362
amean          42.327    42.327    42.327
amin           41.956    41.956    41.956
amax           42.772    42.772    42.772
emean           0.235     0.235     0.235
emin            0.221     0.221     0.221
emax            0.248     0.248     0.248
imean           8.298     8.298     8.298
imin            7.887     7.887     7.887
imax            8.610     8.610     8.610
excite_mean     0.276     0.276     0.276
fracstop        1.000     1.000     1.000
cjmean          2.992     2.992     2.992

libcent 0       180.7     180.7     180.7
libamp  0        14.5      14.4      14.7
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       189.3     189.2     189.3
kozaiamp        180.0     180.0     180.0