Orbit Fit and Astrometric record for 15GR57

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: 15GR57    
# Created Sun Nov 24 02:10:18 2024
# Orbit generated from Bernstein formalism
# Fitting     38 observations of     38
# Arc:   2.35y
# First observation: 2015/02/17
#  Last observation: 2017/06/25
Preliminary a, adot, b, bdot, g, gdot:
  -0.000113   0.021193   0.000001  -0.000564   0.022628   0.000000
# Chi-squared of fit:     8.00 DOF:     70 RMS:  0.08
# Min/Max residuals:    -0.18    0.32
# Exact a, adot, b, bdot, g, gdot:
  1.445964E-05  2.111389E-02 -3.929026E-07 -5.628852E-04  2.267176E-02  1.548056E-03
# Covariance matrix:
  1.4209E-13 -1.9294E-14  1.3871E-16 -1.5217E-15  9.2897E-14  1.4166E-12
 -1.9294E-14  2.4713E-13  1.5798E-15 -7.7711E-15  1.4794E-13  7.0705E-12
  1.3871E-16  1.5798E-15  8.6665E-14 -6.0896E-14  1.0624E-15  6.7201E-14
 -1.5217E-15 -7.7711E-15 -6.0896E-14  7.7049E-14 -6.2789E-15 -3.2489E-13
  9.2897E-14  1.4794E-13  1.0624E-15 -6.2789E-15  1.9972E-13  5.7531E-12
  1.4166E-12  7.0705E-12  6.7201E-14 -3.2489E-13  5.7531E-12  2.9538E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    0.758627 -152.377758    0.847863    0.006791   -0.501878  2457071.023648
# Heliocentric elements and errors
Epoch:              2457070.5000  =  2015/02/17
Mean Anomaly:           97.75271 +/-     0.237
Argument of Peri:       49.36786 +/-     0.225
Long of Asc Node:       52.96584 +/-     0.011
Inclination:             1.68411 +/-     0.001
Eccentricity:         0.05733083 +/-    0.0008
Semi-Major Axis:     44.13817114 +/-    0.0050
Time of Perihelion: 2427987.0305 +/-      70.4
Perihelion:          41.60769307 +/-    0.0342
Aphelion:            46.66864921 +/-    0.0343
Period (y)              293.2444 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -39.91762610 +/-    0.0008
Ecliptic Y          -19.92977458 +/-    0.0004
Ecliptic Z            0.58397204 +/-    0.0000
Ecliptic XDOT         0.00101208 +/-    0.0000
Ecliptic YDOT        -0.00235177 +/-    0.0000
Ecliptic ZDOT        -0.00006540 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.62010546 +/-    0.0007
Geocenter to KBO     44.10774468 +/-    0.0009
# Hcoef:  7.53

The following table shows the complete astrometric record for 15GR57. 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 (15GR57) followed by the observatory code and reference code for the source of the astrometry.

2015 02  17.52287  13 43 41.255  -09 55 09.63  24.1r 15GR57    568  C~2nvX      
2015 02  17.56399  13 43 41.174  -09 55 09.11  24.0r 15GR57    568  C~2nvX      
2015 02  20.59770  13 43 35.330  -09 54 34.16  24.0r 15GR57    568  C~2nvX      
2015 03  18.50144  13 42 19.904  -09 47 14.66  24.0r 15GR57    568  C~2nvX      
2015 03  18.54235  13 42 19.742  -09 47 13.81  23.1r 15GR57    568  C~2nvX      
2015 03  20.54594  13 42 12.337  -09 46 31.16  24.2r 15GR57    568  C~2nvX      
2015 04  11.48071  13 40 42.477  -09 37 59.21  23.4r 15GR57    568  C~2nvX      
2015 04  12.38760  13 40 38.582  -09 37 37.17  23.8r 15GR57    568  C~2nvX      
2015 04  12.43323  13 40 38.376  -09 37 35.94  23.7r 15GR57    568  C~2nvX      
2015 04  12.47547  13 40 38.173  -09 37 34.68  24.2r 15GR57    568  C~2nvX      
2015 04  18.44608  13 40 12.193  -09 35 08.10  24.2r 15GR57    568  C~2nvX      
2015 04  18.49382  13 40 11.992  -09 35 06.92  23.8r 15GR57    568  C~2nvX      
2015 05  17.25497  13 38 13.519  -09 24 06.32  24.0r 15GR57    568  C~2nvX      
2015 05  25.39688  13 37 45.085  -09 21 30.82  24.2r 15GR57    568  C~2nvX      
2015 05  25.45500  13 37 44.886  -09 21 29.73  24.1r 15GR57    568  C~2nvX      
2015 06  21.34643  13 36 39.205  -09 15 43.50  24.2r 15GR57    568  C~2nvX      
2015 06  22.30309  13 36 37.809  -09 15 36.65  24.2r 15GR57    568  C~2nvX      
2015 07  12.29701  13 36 25.177  -09 14 51.42  24.2r 15GR57    568  C~2nvX      
2015 07  19.28682  13 36 28.489  -09 15 20.36  24.4r 15GR57    568  C~2nvX      
2016 02  04.62644  13 48 29.603  -10 24 24.72  23.9w 15GR57    568  C~2nvX      
2016 02  04.63139  13 48 29.595  -10 24 24.68  23.8w 15GR57    568  C~2nvX      
2016 02  04.63544  13 48 29.591  -10 24 24.64  23.8w 15GR57    568  C~2nvX      
2016 02  11.60966  13 48 23.212  -10 23 44.25  24.4w 15GR57    568  C~2nvX      
2016 02  11.61375  13 48 23.207  -10 23 44.17  24.4w 15GR57    568  C~2nvX      
2016 03  11.60894  13 47 16.129  -10 17 13.84  24.1w 15GR57    568  C~2nvX      
2016 04  03.48576  13 45 49.180  -10 09 01.92  24.2w 15GR57    568  C~2nvX      
2016 04  09.46692  13 45 23.725  -10 06 39.24  24.4w 15GR57    568  C~2nvX      
2016 05  02.35585  13 43 44.878  -09 57 29.92  24.3w 15GR57    568  C~2nvX      
2016 05  07.35921  13 43 24.170  -09 55 35.94  24.1w 15GR57    568  C~2nvX      
2016 05  29.33148  13 42 04.336  -09 48 22.13  24.5w 15GR57    568  C~2nvX      
2016 06  04.39391  13 41 46.624  -09 46 47.94  24.3w 15GR57    568  C~2nvX      
2016 06  27.31561  13 41 02.307  -09 43 03.68  24.4w 15GR57    568  C~2nvX      
2016 07  07.31185  13 40 55.545  -09 42 38.52  24.3w 15GR57    568  C~2nvX      
2017 02  27.64549  13 52 25.842  -10 48 07.75        15GR57    568  C~2nvX      
2017 03  30.51590  13 50 42.587  -10 38 27.75  24.3w 15GR57    568  C~2nvX      
2017 03  31.45116  13 50 38.789  -10 38 06.82  24.3w 15GR57    568  C~2nvX      
2017 05  24.25622  13 46 56.433  -10 17 51.46  24.4w 15GR57    568  C~2nvX      
2017 06  25.28243  13 45 37.035  -10 11 00.56  24.2w 15GR57    568  C~2nvX      

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     0.05       0.00     0.00
     2   0.0001     -1.30    -0.02       0.06     0.05
     3   0.0084    -94.44     0.05       1.79    -0.00
     4   0.0793  -1292.64    -0.06      12.72    -0.07
     5   0.0795  -1295.18    -0.18      12.65    -0.13
     6   0.0849  -1412.66    -0.05      13.19    -0.02
     7   0.1450  -2836.65    -0.10      13.53    -0.02
     8   0.1475  -2898.34     0.32      13.36    -0.05
     9   0.1476  -2901.62     0.21      13.41     0.03
    10   0.1477  -2904.88    -0.10      13.51     0.15
    11   0.1641  -3316.21    -0.10      11.91     0.09
    12   0.1642  -3319.41     0.05      11.94     0.16
    13   0.2429  -5193.26    -0.03      -4.47     0.03
    14   0.2652  -5642.13     0.01     -11.70    -0.01
    15   0.2654  -5645.28    -0.07     -11.74     0.00
    16   0.3390  -6677.82     0.03     -41.18    -0.04
    17   0.3416  -6699.59     0.02     -42.29     0.01
    18   0.3964  -6890.48    -0.01     -67.98     0.00
    19   0.4155  -6834.23     0.03     -77.16     0.03
    20   0.9640   4604.01     0.08    -124.15     0.00
    21   0.9640   4603.89     0.01    -124.15    -0.00
    22   0.9640   4603.82    -0.01    -124.14     0.01
    23   0.9831   4501.45     0.05    -119.72    -0.04
    24   0.9831   4501.35     0.04    -119.67     0.00
    25   1.0625   3437.03    -0.08    -105.93    -0.18
    26   1.1252   2062.21    -0.03    -102.82    -0.01
    27   1.1415   1660.13    -0.02    -103.48     0.03
    28   1.2042    100.18     0.02    -111.85     0.01
    29   1.2179   -226.30    -0.01    -114.91     0.00
    30   1.2781  -1483.23     0.02    -132.83    -0.06
    31   1.2947  -1761.42    -0.04    -138.92    -0.03
    32   1.3574  -2453.47    -0.02    -165.09    -0.06
    33   1.3848  -2555.82    -0.11    -177.57    -0.07
    34   2.0291   8368.98    -0.07    -226.71    -0.08
    35   2.1136   6738.23    -0.09    -219.51     0.16
    36   2.1162   6678.39     0.04    -219.67    -0.02
    37   2.2635   3178.62     0.18    -244.41    -0.03
    38   2.3512   1936.93     0.00    -277.57     0.15

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.

15GR57    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.733    43.749    43.718
ecceobj         0.058     0.060     0.056
incobj          1.689     1.689     1.689
qmin           40.318    40.273    40.414
qmax           47.858    48.013    47.812
amean          44.008    44.027    43.996
amin           43.657    43.680    43.654
amax           44.381    44.398    44.373
emean           0.064     0.066     0.062
emin            0.048     0.049     0.046
emax            0.079     0.082     0.078
imean           1.115     1.120     1.118
imin            0.277     0.276     0.276
imax            1.651     1.677     1.671
excite_mean     0.067     0.069     0.066
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       167.0     165.0     165.7
kozaiamp        180.0     180.0     180.0