Orbit Fit and Astrometric record for 15GH58

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: 15GH58    
# Created Sun Nov 24 02:10:18 2024
# Orbit generated from Bernstein formalism
# Fitting     36 observations of     36
# Arc:   2.25y
# First observation: 2015/02/17
#  Last observation: 2017/05/18
Preliminary a, adot, b, bdot, g, gdot:
  -0.000094   0.023618   0.000003  -0.000468   0.023926   0.000000
# Chi-squared of fit:     5.15 DOF:     66 RMS:  0.07
# Min/Max residuals:    -0.28    0.13
# Exact a, adot, b, bdot, g, gdot:
  1.562153E-05  2.353321E-02 -3.904523E-07 -4.666047E-04  2.399078E-02  3.735059E-04
# Covariance matrix:
  1.6091E-13 -2.4287E-14 -1.9808E-16 -1.0859E-15  1.0256E-13  1.6595E-12
 -2.4287E-14  2.6192E-13  2.9797E-16 -4.6302E-15  1.6244E-13  6.4429E-12
 -1.9808E-16  2.9797E-16  1.0145E-13 -7.7315E-14 -5.2104E-17  1.4710E-14
 -1.0859E-15 -4.6302E-15 -7.7315E-14  9.8398E-14 -4.1069E-15 -1.8648E-13
  1.0256E-13  1.6244E-13 -5.2104E-17 -4.1069E-15  2.2019E-13  5.8900E-12
  1.6595E-12  6.4429E-12  1.4710E-14 -1.8648E-13  5.8900E-12  2.5798E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.918374 -155.761237    0.816158    0.018617   -0.551673  2457071.085238
# Heliocentric elements and errors
Epoch:              2457070.5000  =  2015/02/17
Mean Anomaly:          357.65916 +/-     1.135
Argument of Peri:      122.63326 +/-     1.215
Long of Asc Node:       82.97898 +/-     0.017
Inclination:             2.18870 +/-     0.000
Eccentricity:         0.03319702 +/-    0.0000
Semi-Major Axis:     43.69398760 +/-    0.0024
Time of Perihelion: 2457756.4631 +/-     332.7
Perihelion:          42.24347752 +/-    0.0030
Aphelion:            45.14449768 +/-    0.0032
Period (y)              288.8290 +/-      0.02
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -38.82787971 +/-    0.0007
Ecliptic Y          -16.58521600 +/-    0.0003
Ecliptic Z            1.39534180 +/-    0.0000
Ecliptic XDOT         0.00105844 +/-    0.0000
Ecliptic YDOT        -0.00247266 +/-    0.0000
Ecliptic ZDOT        -0.00005170 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   42.24477022 +/-    0.0007
Geocenter to KBO     41.68267362 +/-    0.0008
# Hcoef:  7.52

The following table shows the complete astrometric record for 15GH58. 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 (15GH58) followed by the observatory code and reference code for the source of the astrometry.

2015 02  17.58446  13 32 37.425  -07 36 50.40  23.9r 15GH58    568  C~2nvZ      
2015 02  17.62541  13 32 37.335  -07 36 49.86  23.7r 15GH58    568  C~2nvZ      
2015 02  20.61856  13 32 30.720  -07 36 04.43  23.3r 15GH58    568  C~2nvZ      
2015 03  18.56291  13 31 07.789  -07 27 14.09  23.7r 15GH58    568  C~2nvZ      
2015 03  18.60407  13 31 07.622  -07 27 13.11  23.9r 15GH58    568  C~2nvZ      
2015 03  20.56704  13 30 59.834  -07 26 25.25  23.7r 15GH58    568  C~2nvZ      
2015 04  11.50134  13 29 24.871  -07 16 56.30  23.4r 15GH58    568  C~2nvZ      
2015 04  13.36562  13 29 16.454  -07 16 06.98  23.8r 15GH58    568  C~2nvZ      
2015 04  13.40656  13 29 16.263  -07 16 05.90  23.7r 15GH58    568  C~2nvZ      
2015 04  13.50913  13 29 15.791  -07 16 03.14  23.7r 15GH58    568  C~2nvZ      
2015 04  19.40635  13 28 49.142  -07 13 28.17  23.8r 15GH58    568  C~2nvZ      
2015 05  18.32905  13 26 48.627  -07 02 12.82  23.9r 15GH58    568  C~2nvZ      
2015 06  20.27906  13 25 23.725  -06 55 12.81  24.1r 15GH58    568  C~2nvZ      
2015 06  20.31989  13 25 23.664  -06 55 12.52  24.0r 15GH58    568  C~2nvZ      
2015 06  22.32371  13 25 21.085  -06 55 03.26  23.8r 15GH58    568  C~2nvZ      
2015 07  14.27603  13 25 15.070  -06 55 36.64  23.8r 15GH58    568  C~2nvZ      
2015 07  20.26893  13 25 20.661  -06 56 28.72  23.8r 15GH58    568  C~2nvZ      
2016 02  04.56733  13 37 58.676  -08 10 14.10  24.3w 15GH58    568  C~2nvZ      
2016 02  10.55526  13 37 52.029  -08 09 20.58  23.3w 15GH58    568  C~2nvZ      
2016 02  10.60492  13 37 51.958  -08 09 20.07  23.6w 15GH58    568  C~2nvZ      
2016 02  11.57713  13 37 50.571  -08 09 09.80  24.1w 15GH58    568  C~2nvZ      
2016 03  11.55250  13 36 35.702  -08 00 59.22  23.1w 15GH58    568  C~2nvZ      
2016 03  12.47618  13 36 32.417  -08 00 38.59  24.0w 15GH58    568  C~2nvZ      
2016 04  03.43722  13 35 02.896  -07 51 39.45  24.1w 15GH58    568  C~2nvZ      
2016 04  09.41701  13 34 36.162  -07 49 02.90  23.8w 15GH58    568  C~2nvZ      
2016 05  28.29624  13 31 15.919  -07 30 32.67  24.4w 15GH58    568  C~2nvZ      
2016 05  28.30839  13 31 15.878  -07 30 32.37  24.3w 15GH58    568  C~2nvZ      
2016 05  29.31531  13 31 12.795  -07 30 16.71  24.2w 15GH58    568  C~2nvZ      
2016 06  04.37369  13 30 55.622  -07 28 50.87  24.0w 15GH58    568  C~2nvZ      
2016 06  27.33366  13 30 15.189  -07 25 58.70  24.4w 15GH58    568  C~2nvZ      
2016 06  27.34232  13 30 15.180  -07 25 58.45  24.3w 15GH58    568  C~2nvZ      
2016 07  07.32400  13 30 11.041  -07 26 05.28  24.1w 15GH58    568  C~2nvZ      
2016 07  07.33209  13 30 11.033  -07 26 05.32  24.0w 15GH58    568  C~2nvZ      
2017 02  24.64707  13 42 26.498  -08 36 50.92        15GH58    568  C~2nvZ      
2017 03  29.46871  13 40 31.727  -08 25 08.69  23.9w 15GH58    568  C~2nvZ      
2017 05  18.26658  13 36 55.609  -08 04 55.03  23.9w 15GH58    568  C~2nvZ      

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     0.02
     2   0.0001     -1.44    -0.02       0.01    -0.04
     3   0.0083   -109.60    -0.02       6.30    -0.03
     4   0.0793  -1451.42    -0.03      47.95     0.05
     5   0.0795  -1454.09    -0.05      47.95     0.02
     6   0.0848  -1579.41     0.01      49.99     0.02
     7   0.1449  -3102.55    -0.05      60.43     0.04
     8   0.1500  -3237.18    -0.00      60.25     0.01
     9   0.1501  -3240.22    -0.04      60.21    -0.01
    10   0.1504  -3247.77    -0.04      60.19     0.04
    11   0.1665  -3673.63     0.09      58.44     0.08
    12   0.2457  -5590.99     0.04      25.39    -0.11
    13   0.3359  -6922.07     0.12     -51.15    -0.03
    14   0.3360  -6923.02     0.07     -51.22     0.03
    15   0.3415  -6962.17    -0.02     -56.81    -0.00
    16   0.4016  -7033.14    -0.06    -120.98    -0.15
    17   0.4180  -6936.42    -0.01    -138.60     0.04
    18   0.9637   5176.16    -0.01    -126.30     0.01
    19   0.9801   5064.70     0.05    -112.25     0.10
    20   0.9802   5063.53     0.07    -112.16     0.10
    21   0.9829   5040.60     0.01    -110.06    -0.02
    22   1.0622   3825.90    -0.08     -57.04    -0.28
    23   1.0647   3772.93     0.13     -55.57    -0.05
    24   1.1249   2337.64     0.00     -37.82     0.02
    25   1.1412   1910.60     0.07     -36.95     0.03
    26   1.2750  -1266.10     0.06     -92.47    -0.01
    27   1.2751  -1266.78    -0.02     -92.41     0.08
    28   1.2778  -1315.18     0.03     -94.65     0.02
    29   1.2944  -1584.27     0.00    -108.47     0.02
    30   1.3573  -2206.91     0.03    -169.03    -0.08
    31   1.3573  -2207.13    -0.08    -168.84     0.13
    32   1.3846  -2261.89    -0.05    -197.81     0.01
    33   1.3847  -2261.99    -0.15    -197.89    -0.04
    34   2.0207   9464.49    -0.10    -177.88    -0.00
    35   2.1106   7620.05    -0.02    -137.33    -0.05
    36   2.2469   4187.21     0.09    -169.21     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.

15GH58    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.283    43.290    43.275
ecceobj         0.024     0.024     0.024
incobj          2.189     2.189     2.189
qmin           41.623    41.603    41.611
qmax           45.654    45.712    45.644
amean          43.562    43.570    43.555
amin           43.225    43.236    43.223
amax           43.905    43.917    43.896
emean           0.024     0.024     0.024
emin            0.007     0.006     0.006
emax            0.040     0.041     0.040
imean           0.763     0.762     0.763
imin            0.333     0.328     0.339
imax            1.100     1.101     1.099
excite_mean     0.028     0.028     0.027
fracstop        1.000     1.000     1.000
cjmean          3.095     3.095     3.095

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       201.4     200.5     201.9
kozaiamp        179.9     180.0     180.0