Orbit Fit and Astrometric record for 15GG57

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: 15GG57    
# Created Sun Nov 24 02:10:17 2024
# Orbit generated from Bernstein formalism
# Fitting     33 observations of     34
# Arc:   2.11y
# First observation: 2015/02/17
#  Last observation: 2017/03/29
Preliminary a, adot, b, bdot, g, gdot:
  -0.000088   0.019475  -0.000000   0.000332   0.021666   0.000000
# Chi-squared of fit:     6.32 DOF:     60 RMS:  0.08
# Min/Max residuals:    -0.20    0.25
# Exact a, adot, b, bdot, g, gdot:
  1.382519E-05  1.936918E-02  9.142207E-08  3.298357E-04  2.169185E-02 -5.052811E-05
# Covariance matrix:
  1.8410E-13 -3.0603E-14 -5.6508E-16  1.5406E-15  1.2573E-13  2.3967E-12
 -3.0603E-14  2.5292E-13 -1.3263E-15  4.7881E-15  1.5165E-13  7.4088E-12
 -5.6508E-16 -1.3263E-15  1.0568E-13 -8.5282E-14 -1.5240E-15 -7.2640E-14
  1.5406E-15  4.7881E-15 -8.5282E-14  1.1836E-13  4.9318E-15  2.6764E-13
  1.2573E-13  1.5165E-13 -1.5240E-15  4.9318E-15  2.4402E-13  7.6459E-12
  2.3967E-12  7.4088E-12 -7.2640E-14  2.6764E-13  7.6459E-12  4.1399E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.664963 -154.425058    0.829468    0.006318   -0.531734  2457071.015468
# Heliocentric elements and errors
Epoch:              2457070.5000  =  2015/02/17
Mean Anomaly:          199.19671 +/-     0.929
Argument of Peri:      196.51403 +/-     0.930
Long of Asc Node:      170.89007 +/-     0.028
Inclination:             1.18554 +/-     0.001
Eccentricity:         0.05793040 +/-    0.0003
Semi-Major Axis:     44.20847456 +/-    0.0029
Time of Perihelion: 2505027.1831 +/-     277.1
Perihelion:          41.64745973 +/-    0.0143
Aphelion:            46.76948940 +/-    0.0143
Period (y)              293.9453 +/-      0.03
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -42.42112183 +/-    0.0010
Ecliptic Y          -19.38108537 +/-    0.0004
Ecliptic Z            0.53501742 +/-    0.0000
Ecliptic XDOT         0.00105789 +/-    0.0000
Ecliptic YDOT        -0.00220777 +/-    0.0000
Ecliptic ZDOT         0.00004165 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   46.64187272 +/-    0.0009
Geocenter to KBO     46.10027205 +/-    0.0010
# Hcoef:  7.57

The following table shows the complete astrometric record for 15GG57. 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 (15GG57) followed by the observatory code and reference code for the source of the astrometry.

2015 02  17.51469  13 35 48.290  -09 16 05.82  24.0r 15GG57    568  C~2nvV      
2015 02  17.55579  13 35 48.206  -09 16 05.36  24.1r 15GG57    568  C~2nvV      
2015 02  20.48657  13 35 42.350  -09 15 28.51  24.2r 15GG57    568  C~2nvV      
2015 03  18.49249  13 34 26.731  -09 07 48.86  23.9r 15GG57    568  C~2nvV      
2015 03  18.53407  13 34 26.579  -09 07 48.06  23.9r 15GG57    568  C~2nvV      
2015 03  20.53726  13 34 19.303  -09 07 04.50  24.0r 15GG57    568  C~2nvV      
2015 04  11.47256  13 32 52.229  -08 58 28.59  24.7r 15GG57    568  C~2nvV      
2015 04  12.37938  13 32 48.459  -08 58 06.34  24.2r 15GG57    568  C~2nvV      
2015 04  12.42509  13 32 48.276  -08 58 05.24  23.7r 15GG57    568  C~2nvV      
2015 04  12.46730  13 32 48.092  -08 58 04.22  23.9r 15GG57    568  C~2nvV      
2015 05  16.28656  13 30 34.345  -08 45 03.62  24.1r 15GG57    568  C~2nvV      
2015 05  17.24686  13 30 31.010  -08 44 44.74  24.1r 15GG57    568  C~2nvV      
2015 05  25.38864  13 30 04.550  -08 42 12.77  24.3r 15GG57    568  C~2nvV      
2015 05  25.44647  13 30 04.372  -08 42 11.76  24.3r 15GG57    568  C~2nvV      
2015 06  21.33827  13 29 04.771  -08 36 36.91  24.6r 15GG57    568  C~2nvV      
2015 06  22.29486  13 29 03.568  -08 36 30.44  24.2r 15GG57    568  C~2nvV      
2015 07  12.28879  13 28 54.302  -08 35 50.14  24.7r 15GG57    568  C~2nvV      
2015 07  19.27863  13 28 58.458  -08 36 19.65  24.2r 15GG57    568  C~2nvV      
2016 02  04.60217  13 40 19.339  -09 41 04.79  24.6w 15GG57    568  C~2nvV      
2016 02  10.62117  13 40 13.175  -09 40 23.12  24.6w 15GG57    568  C~2nvV      
2016 02  11.58525  13 40 11.934  -09 40 14.75  24.3w 15GG57    568  C~2nvV      
2016 03  11.58783  13 39 03.329  -09 33 14.57  24.4w 15GG57    568  C~2nvV      
2016 03  11.63454  13 39 03.170  -09 33 13.68  24.3w 15GG57    568  C~2nvV      
2016 04  09.44264  13 37 13.669  -09 22 28.27  24.4w 15GG57    568  C~2nvV      
2016 05  02.31935  13 35 39.344  -09 13 21.33  24.4w 15GG57    568  C~2nvV      
2016 05  06.32911  13 35 23.594  -09 11 50.57  24.3w 15GG57    568  C~2nvV      
2016 05  07.36327  13 35 19.610  -09 11 27.79  24.3w 15GG57    568  C~2nvV      
2016 05  28.31243  13 34 08.055  -09 04 39.72  24.3w 15GG57    568  C~2nvV      
2016 05  29.31935  13 34 05.149  -09 04 23.32  24.6w 15GG57    568  C~2nvV      
2016 06  27.30147  13 33 09.590  -08 59 18.26  24.4w 15GG57    568  C~2nvV      
2016 06  27.30677  13 33 09.589  -08 59 18.34  24.3w 15GG57    568  C~2nvV      
2016 07  07.30364  13 33 04.611  -08 58 56.64  25.1w 15GG57    568  C~2nvV      
2017 03  29.48748  13 42 16.157  -09 50 10.61  24.9w 15GG57    568  C~2nvV      
2017 03  29.50900  13 42 16.061  -09 50 09.85  25.1w 15GG57    568  C~2nvV      

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     0.06       0.00     0.03
     2   0.0001     -1.33     0.02      -0.02    -0.01
     3   0.0081    -95.49    -0.02       2.78     0.02
     4   0.0793  -1305.71     0.04      23.29     0.06
     5   0.0795  -1308.10     0.08      23.22    -0.03
     6   0.0849  -1424.33    -0.07      24.51     0.04
     7   0.1450  -2813.66     0.04      34.06    -0.08
     8   0.1475  -2873.80    -0.07      34.36    -0.07
     9   0.1476  -2876.73     0.08      34.39    -0.02
    10   0.1477  -2879.64     0.02      34.34    -0.07
    11   0.2403  -5010.86 (   0.12)     34.85 (   0.45)
    12   0.2429  -5063.82     0.05      34.27     0.10
    13   0.2652  -5484.80     0.00      31.64     0.06
    14   0.2654  -5487.63     0.02      31.61     0.07
    15   0.3390  -6433.46    -0.08      18.23     0.02
    16   0.3416  -6452.45    -0.05      17.68     0.04
    17   0.3964  -6595.20    -0.07       4.60     0.07
    18   0.4155  -6526.96    -0.02      -0.17     0.08
    19   0.9640   4281.50     0.02      54.63     0.03
    20   0.9804   4181.42    -0.09      60.64    -0.20
    21   0.9831   4161.27     0.02      61.83    -0.01
    22   1.0625   3063.04    -0.11      87.39    -0.15
    23   1.0626   3060.53    -0.15      87.37    -0.19
    24   1.1415   1316.41    -0.02     102.50    -0.00
    25   1.2041   -183.19     0.25     105.07    -0.06
    26   1.2151   -433.43    -0.05     104.79     0.07
    27   1.2179   -496.67     0.03     104.55    -0.02
    28   1.2753  -1632.26    -0.01      98.59     0.01
    29   1.2780  -1678.32    -0.02      98.16     0.01
    30   1.3574  -2556.03    -0.05      81.80     0.02
    31   1.3574  -2556.02     0.04      81.72    -0.05
    32   1.3848  -2632.61     0.03      74.98     0.06
    33   2.1108   6090.28     0.15     166.86    -0.01
    34   2.1109   6088.69    -0.09     167.06     0.19

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.

15GG57    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.823    43.831    43.815
ecceobj         0.067     0.068     0.068
incobj          1.191     1.191     1.191
qmin           40.320    40.317    40.286
qmax           48.126    48.139    48.118
amean          44.104    44.112    44.099
amin           43.760    43.757    43.753
amax           44.466    44.482    44.464
emean           0.067     0.067     0.067
emin            0.051     0.051     0.051
emax            0.082     0.082     0.082
imean           2.113     2.112     2.116
imin            1.446     1.447     1.447
imax            2.748     2.747     2.752
excite_mean     0.076     0.076     0.076
fracstop        1.000     1.000     1.000
cjmean          3.096     3.096     3.096

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       186.3     186.0     186.3
kozaiamp        179.9     180.0     180.0