Orbit Fit and Astrometric record for 12UY174

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: 12UY174   
# Created Sun Dec 22 02:09:22 2024
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     66 observations of     66
# Arc:   5.37y
# First observation: 2009/09/08
#  Last observation: 2015/01/23
# Chi-squared of fit:   106.46 DOF:    126 RMS:  0.22
# Min/Max residuals:    -0.73    0.63
# Exact a, adot, b, bdot, g, gdot:
  4.443829E-05  4.941648E-01  6.884983E-06  9.237369E-02  1.780474E-01  2.508968E-02
# Covariance matrix:
  1.5534E-08  1.2633E-02  3.0977E-09  2.5195E-03  6.2183E-13  2.2455E-03
  1.2633E-02  1.0475E+04  2.5194E-03  2.0891E+03  5.0533E-07  1.8619E+03
  3.0977E-09  2.5194E-03  6.1934E-10  5.0246E-04  1.2401E-13  4.4782E-04
  2.5195E-03  2.0891E+03  5.0246E-04  4.1664E+02  1.0078E-07  3.7132E+02
  6.2183E-13  5.0533E-07  1.2401E-13  1.0078E-07  2.4895E-17  8.9822E-08
  2.2455E-03  1.8619E+03  4.4782E-04  3.7132E+02  8.9822E-08  3.3093E+02
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.590979  -22.974414   -0.153319   -0.010249   -0.991489  2455082.826000
# Heliocentric elements and errors
Epoch:              2455082.5000  =  2009/09/08
Mean Anomaly:            7.41213 +/-     0.002
Argument of Peri:      341.02372 +/-     0.000
Long of Asc Node:      341.01548 +/-     0.000
Inclination:            10.61294 +/-     0.000
Eccentricity:         0.34795922 +/-  129.7829
Semi-Major Axis:     10.03915255 +/-    0.0000
Time of Perihelion: 2454843.2870 +/-       0.0
Perihelion:           6.54593688 +/- 1302.9107
Aphelion:            13.53236823 +/- 1302.9107
Period (y)               31.8093 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X            6.14688528 +/-    0.0000
Ecliptic Y           -2.44126576 +/-    0.0000
Ecliptic Z           -0.05786572 +/-    0.0000
Ecliptic XDOT         0.00333861 +/-    0.0004
Ecliptic YDOT         0.00684472 +/-    0.0006
Ecliptic ZDOT         0.00141630 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO    6.61415824 +/-    0.0000
Geocenter to KBO      5.61650319 +/-    0.0000
# Hcoef: 13.14

The following table shows the complete astrometric record for 12UY174. 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 (12UY174) followed by the observatory code and reference code for the source of the astrometry.

2009 09  08.325234 22 35 52.283  -09 28 50.52  21.4G 12UY174   F51  C~8MSZ      
2009 09  08.335388 22 35 52.072  -09 28 51.48  21.2G 12UY174   F51  C~8MSZ      
2009 09  21.23748  22 31 15.20   -09 43 40.5   21.9V 12UY174   G96  C~8MSZ      
2009 09  21.24462  22 31 15.09   -09 43 41.5   21.5V 12UY174   G96  C~8MSZ      
2009 09  21.25174  22 31 14.91   -09 43 41.9   21.2V 12UY174   G96  C~8MSZ      
2009 09  21.25892  22 31 14.80   -09 43 42.1   21.1V 12UY174   G96  C~8MSZ      
2009 09  21.373469 22 31 12.532  -09 43 48.53  21.0G 12UY174   F51  C~8MSZ      
2009 09  28.306238 22 29 02.896  -09 49 51.20  21.2G 12UY174   F51  C~8MSZ      
2009 09  28.313748 22 29 02.781  -09 49 51.66  20.7G 12UY174   F51  C~8MSZ      
2010 06  15.556750 00 12 27.672  +04 21 46.87  22.0G 12UY174   F51  C~8MSZ      
2010 06  15.563983 00 12 27.773  +04 21 48.35  21.9G 12UY174   F51  C~8MSZ      
2010 06  16.552608 00 12 44.347  +04 24 42.06  22.1G 12UY174   F51  C~8MSZ      
2010 06  19.538508 00 13 31.691  +04 33 11.95  21.7G 12UY174   F51  C~8MSZ      
2010 06  19.544620 00 13 31.795  +04 33 12.56  21.8G 12UY174   F51  C~8MSZ      
2010 06  22.543693 00 14 15.296  +04 41 21.22  21.4G 12UY174   F51  C~8MSZ      
2010 06  22.550928 00 14 15.324  +04 41 22.06  22.2G 12UY174   F51  C~8MSZ      
2010 09  13.471198 00 05 54.285  +05 25 56.37  21.6G 12UY174   F51  C~8MSZ      
2010 09  13.484487 00 05 53.989  +05 25 55.29  21.0G 12UY174   F51  C~8MSZ      
2010 09  13.496272 00 05 53.730  +05 25 54.31  21.0G 12UY174   F51  C~8MSZ      
2010 09  15.487746 00 05 10.490  +05 23 04.82  21.3G 12UY174   F51  C~8MSZ      
2010 09  15.496973 00 05 10.292  +05 23 04.02  21.5G 12UY174   F51  C~8MSZ      
2010 09  15.506316 00 05 10.066  +05 23 03.04  21.3G 12UY174   F51  C~8MSZ      
2010 09  15.515684 00 05 09.858  +05 23 02.26  21.1G 12UY174   F51  C~8MSZ      
2010 09  16.435312 00 04 49.792  +05 21 41.95  21.4G 12UY174   F51  C~8MSZ      
2010 09  16.439125 00 04 49.704  +05 21 41.47  21.4G 12UY174   F51  C~8MSZ      
2010 09  16.446472 00 04 49.541  +05 21 40.89  21.5G 12UY174   F51  C~8MSZ      
2010 09  16.450429 00 04 49.459  +05 21 40.41  21.1G 12UY174   F51  C~8MSZ      
2010 10  03.383367 23 58 36.292  +04 54 21.59  21.1G 12UY174   F51  C~8MSZ      
2010 10  03.396639 23 58 36.003  +04 54 20.30  21.5G 12UY174   F51  C~8MSZ      
2010 10  03.411248 23 58 35.686  +04 54 18.74  21.5G 12UY174   F51  C~8MSZ      
2010 10  03.425249 23 58 35.369  +04 54 17.17  21.6G 12UY174   F51  C~8MSZ      
2010 10  09.280518 23 56 32.314  +04 44 23.76  21.1G 12UY174   F51  C~8MSZ      
2010 10  09.292061 23 56 32.084  +04 44 22.53  21.4G 12UY174   F51  C~8MSZ      
2010 10  09.305107 23 56 31.801  +04 44 21.26  21.9G 12UY174   F51  C~8MSZ      
2010 10  14.349824 23 54 51.670  +04 36 01.65  21.6G 12UY174   F51  C~8MSZ      
2010 10  14.361607 23 54 51.431  +04 36 00.44  21.8G 12UY174   F51  C~8MSZ      
2010 12  31.217517 23 52 46.142  +04 26 45.33  21.6G 12UY174   F51  C~8MSZ      
2010 12  31.223662 23 52 46.259  +04 26 45.95  22.2G 12UY174   F51  C~8MSZ      
2010 12  31.230370 23 52 46.365  +04 26 46.83  22.0G 12UY174   F51  C~8MSZ      
2010 12  31.236469 23 52 46.472  +04 26 47.40  22.4G 12UY174   F51  C~8MSZ      
2011 01  01.224861 23 53 04.190  +04 28 36.99  21.8G 12UY174   F51  C~8MSZ      
2011 01  01.231014 23 53 04.309  +04 28 37.64  22.1G 12UY174   F51  C~8MSZ      
2011 10  21.26764  01 13 42.85   +16 49 35.4   21.2V 12UY174   G96  C~8MSZ      
2011 10  21.27581  01 13 42.63   +16 49 35.3   21.5V 12UY174   G96  C~8MSZ      
2011 10  21.28402  01 13 42.49   +16 49 34.2   21.6V 12UY174   G96  C~8MSZ      
2011 10  21.29218  01 13 42.27   +16 49 32.6   22.2V 12UY174   G96  C~8MSZ      
2011 11  12.444059 01 06 28.773  +16 08 31.36  21.8G 12UY174   F51  C~8MSZ      
2011 11  12.457333 01 06 28.577  +16 08 30.09  21.6G 12UY174   F51  C~8MSZ      
2012 01  21.213251 01 06 24.246  +15 27 18.97  21.5G 12UY174   F51  C~8MSZ      
2012 10  23.494518 02 27 13.061  +25 34 49.90  22.3w 12UY174   F51  c~0knY      
2012 10  23.509643 02 27 12.730  +25 34 48.59  21.9w 12UY174   F51  c~0knY      
2012 10  23.539961 02 27 12.045  +25 34 46.47  21.9w 12UY174   F51  c~0knY      
2012 10  24.542395 02 26 49.759  +25 33 35.62  22.4G 12UY174   F51  C~8MSZ      
2012 10  25.44441  02 26 29.64   +25 32 30.1   21.3R 12UY174   291  C~0knY      
2012 10  25.45507  02 26 29.40   +25 32 29.1   21.4R 12UY174   291  C~0knY      
2012 10  25.46573  02 26 29.10   +25 32 27.9         12UY174   291  C~0knY      
2012 11  05.44896  02 22 22.89   +25 17 02.4         12UY174   F51  C~7ufB      
2012 11  05.46115  02 22 22.64   +25 17 01.3   21.9i 12UY174   F51  C~7ufB      
2013 12  03.285485 03 20 44.318  +30 18 12.24  22.6G 12UY174   F51  C~8MSZ      
2013 12  03.299616 03 20 44.008  +30 18 10.97  22.7G 12UY174   F51  C~8MSZ      
2013 12  03.313737 03 20 43.670  +30 18 09.58  22.0G 12UY174   F51  C~8MSZ      
2013 12  03.327880 03 20 43.426  +30 18 08.43  22.3G 12UY174   F51  C~8MSZ      
2014 11  27.350198 04 25 15.355  +33 33 17.24  22.6G 12UY174   F51  C~8MSZ      
2015 01  23.336961 04 08 59.668  +32 25 04.62  22.8G 12UY174   F51  C~8MSZ      
2015 01  23.349522 04 08 59.609  +32 25 03.78  22.8G 12UY174   F51  C~8MSZ      
2015 01  23.362073 04 08 59.481  +32 25 02.92  22.7G 12UY174   F51  C~8MSZ      

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    -0.21       0.00     0.21
     2   0.0000      0.00     0.15       0.00     0.03
     3   0.0354      0.00    -0.49       0.00     0.22
     4   0.0354      0.00     0.05       0.00    -0.36
     5   0.0354      0.00    -0.46       0.00    -0.34
     6   0.0354      0.00     0.09       0.00    -0.11
     7   0.0357      0.00     0.12       0.00    -0.02
     8   0.0547      0.00     0.04       0.00     0.22
     9   0.0547      0.00     0.35       0.00     0.10
    10   0.7672      0.00     0.10       0.00    -0.23
    11   0.7673      0.00    -0.19       0.00    -0.03
    12   0.7700      0.00    -0.05       0.00    -0.09
    13   0.7781      0.00    -0.31       0.00     0.30
    14   0.7782      0.00    -0.12       0.00    -0.11
    15   0.7864      0.00     0.32       0.00     0.51
    16   0.7864      0.00    -0.73       0.00     0.19
    17   1.0134      0.00     0.08       0.00    -0.01
    18   1.0134      0.00     0.05       0.00     0.02
    19   1.0135      0.00     0.09       0.00     0.02
    20   1.0189      0.00     0.07       0.00     0.05
    21   1.0190      0.00     0.20       0.00     0.05
    22   1.0190      0.00    -0.06       0.00    -0.12
    23   1.0190      0.00    -0.03       0.00    -0.09
    24   1.0215      0.00     0.03       0.00    -0.00
    25   1.0215      0.00    -0.00       0.00    -0.15
    26   1.0216      0.00     0.03       0.00    -0.08
    27   1.0216      0.00     0.14       0.00    -0.21
    28   1.0679      0.00     0.02       0.00     0.03
    29   1.0680      0.00     0.09       0.00     0.09
    30   1.0680      0.00     0.17       0.00     0.02
    31   1.0680      0.00     0.06       0.00    -0.13
    32   1.0841      0.00     0.01       0.00    -0.01
    33   1.0841      0.00     0.18       0.00    -0.08
    34   1.0841      0.00     0.04       0.00    -0.05
    35   1.0979      0.00     0.13       0.00    -0.04
    36   1.0980      0.00     0.03       0.00    -0.11
    37   1.3111      0.00     0.04       0.00     0.05
    38   1.3112      0.00     0.21       0.00    -0.00
    39   1.3112      0.00     0.06       0.00     0.15
    40   1.3112      0.00     0.08       0.00     0.05
    41   1.3139      0.00     0.04       0.00    -0.02
    42   1.3139      0.00     0.19       0.00    -0.06
    43   2.1162      0.00    -0.09       0.00    -0.13
    44   2.1162      0.00    -0.66       0.00     0.63
    45   2.1162      0.00    -0.02       0.00     0.41
    46   2.1163      0.00    -0.60       0.00    -0.32
    47   2.1769      0.00    -0.38       0.00    -0.44
    48   2.1770      0.00     0.03       0.00    -0.25
    49   2.3679      0.00     0.21       0.00    -0.02
    50   3.1244      0.00     0.08       0.00     0.27
    51   3.1244      0.00     0.26       0.00     0.02
    52   3.1245      0.00     0.28       0.00     0.05
    53   3.1272      0.00     0.24       0.00    -0.05
    54   3.1297      0.00     0.25       0.00     0.23
    55   3.1297      0.00     0.27       0.00     0.04
    56   3.1297      0.00    -0.61       0.00    -0.35
    57   3.1598      0.00    -0.21       0.00     0.06
    58   3.1599      0.00     0.20       0.00     0.11
    59   4.2353      0.00     0.11       0.00     0.03
    60   4.2354      0.00    -0.06       0.00     0.03
    61   4.2354      0.00    -0.66       0.00    -0.10
    62   4.2355      0.00     0.17       0.00     0.03
    63   5.2184      0.00     0.29       0.00    -0.07
    64   5.3744      0.00    -0.15       0.00    -0.21
    65   5.3745      0.00     0.30       0.00    -0.04
    66   5.3745      0.00    -0.28       0.00     0.11

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.

12UY174    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj        10.070    10.070    10.070
ecceobj         0.353     0.353     0.353
incobj         10.591    10.591    10.591
qmin            6.348     6.516     5.745
qmax           14.285    13.624    14.316
amean          10.144     9.971     9.557
amin           10.036     9.871     8.603
amax           10.321    10.070    10.414
emean           0.356     0.331     0.342
emin            0.333     0.310     0.308
emax            0.384     0.353     0.375
imean          11.565    11.370    13.236
imin           10.808    10.808    10.808
imax           13.154    11.830    17.288
excite_mean     0.409     0.385     0.413
fracstop        0.001     0.001     0.001
cjmean          4.030     4.082     4.195

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       163.7     178.1     174.5
kozaiamp        166.8     166.9     167.0