Orbit Fit and Astrometric record for 15GY57

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: 15GY57    
# Created Sun Nov 24 02:10:18 2024
# Orbit generated from Bernstein formalism
# Fitting     38 observations of     38
# Arc:   2.34y
# First observation: 2015/02/17
#  Last observation: 2017/06/22
Preliminary a, adot, b, bdot, g, gdot:
  -0.000091   0.020874   0.000003  -0.000158   0.022473   0.000000
# Chi-squared of fit:    10.94 DOF:     70 RMS:  0.09
# Min/Max residuals:    -0.36    0.23
# Exact a, adot, b, bdot, g, gdot:
  1.419307E-05  2.086625E-02 -4.124191E-07 -1.580231E-04  2.257384E-02  1.806830E-03
# Covariance matrix:
  1.8250E-13 -5.2539E-15 -7.2880E-16 -2.9991E-16  1.3869E-13  2.4695E-12
 -5.2539E-15  2.2827E-13 -5.8858E-16 -1.0578E-15  1.6531E-13  6.5122E-12
 -7.2880E-16 -5.8858E-16  9.6551E-14 -7.3469E-14 -1.1828E-15 -2.1510E-14
 -2.9991E-16 -1.0578E-15 -7.3469E-14  9.3028E-14 -1.0422E-15 -5.4629E-14
  1.3869E-13  1.6531E-13 -1.1828E-15 -1.0422E-15  2.6140E-13  7.0848E-12
  2.4695E-12  6.5122E-12 -2.1510E-14 -5.4629E-14  7.0848E-12  3.2645E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.308185 -157.340126    0.800806    0.023260   -0.573560  2457071.068908
# Heliocentric elements and errors
Epoch:              2457070.5000  =  2015/02/17
Mean Anomaly:          100.28316 +/-     0.235
Argument of Peri:      351.43505 +/-     0.221
Long of Asc Node:      101.86419 +/-     0.020
Inclination:             2.31165 +/-     0.000
Eccentricity:         0.07273362 +/-    0.0008
Semi-Major Axis:     44.08905352 +/-    0.0056
Time of Perihelion: 2427283.9568 +/-      69.5
Perihelion:          40.88229724 +/-    0.0354
Aphelion:            47.29580979 +/-    0.0356
Period (y)              292.7550 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -41.68739169 +/-    0.0009
Ecliptic Y          -16.53494904 +/-    0.0004
Ecliptic Z            1.78410656 +/-    0.0000
Ecliptic XDOT         0.00076857 +/-    0.0000
Ecliptic YDOT        -0.00242562 +/-    0.0000
Ecliptic ZDOT        -0.00001023 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.88235958 +/-    0.0009
Geocenter to KBO     44.29906715 +/-    0.0010
# Hcoef:  8.26

The following table shows the complete astrometric record for 15GY57. 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 (15GY57) followed by the observatory code and reference code for the source of the astrometry.

2015 02  17.56813  13 27 17.207  -06 40 16.44  24.6r 15GY57    568  C~2nvY      
2015 02  17.60905  13 27 17.109  -06 40 15.75  24.7r 15GY57    568  C~2nvY      
2015 02  20.60184  13 27 10.469  -06 39 28.36  24.5r 15GY57    568  C~2nvY      
2015 03  18.54653  13 25 49.615  -06 30 34.00  25.0r 15GY57    568  C~2nvY      
2015 03  18.58746  13 25 49.481  -06 30 33.22  25.0r 15GY57    568  C~2nvY      
2015 03  20.55033  13 25 42.003  -06 29 45.88  24.8r 15GY57    568  C~2nvY      
2015 04  11.49312  13 24 11.462  -06 20 31.67  24.7r 15GY57    568  C~2nvY      
2015 04  13.35741  13 24 03.491  -06 19 44.28  24.3r 15GY57    568  C~2nvY      
2015 04  13.39836  13 24 03.316  -06 19 43.13  24.5r 15GY57    568  C~2nvY      
2015 04  13.47268  13 24 02.989  -06 19 41.37  24.7r 15GY57    568  C~2nvY      
2015 04  13.47763  13 24 02.962  -06 19 41.13  24.2r 15GY57    568  C~2nvY      
2015 04  19.51516  13 23 37.168  -06 17 09.15  24.6r 15GY57    568  C~2nvY      
2015 05  18.27253  13 21 44.940  -06 06 34.75  24.7r 15GY57    568  C~2nvY      
2015 06  20.27087  13 20 26.758  -06 00 15.06  24.7r 15GY57    568  C~2nvY      
2015 06  20.31175  13 20 26.703  -06 00 14.80  25.0r 15GY57    568  C~2nvY      
2015 06  22.31546  13 20 24.420  -06 00 07.43  25.2r 15GY57    568  C~2nvY      
2015 07  14.26780  13 20 20.302  -06 00 56.67  24.6r 15GY57    568  C~2nvY      
2015 07  20.29800  13 20 26.007  -06 01 51.42  24.8r 15GY57    568  C~2nvY      
2016 02  04.55115  13 32 05.062  -07 09 49.46  25.2w 15GY57    568  C~2nvY      
2016 02  10.53908  13 31 57.827  -07 08 48.72  25.2w 15GY57    568  C~2nvY      
2016 03  11.54027  13 30 42.048  -07 00 09.87  25.0w 15GY57    568  C~2nvY      
2016 04  03.42105  13 29 13.088  -06 50 58.39  24.8w 15GY57    568  C~2nvY      
2016 04  09.40078  13 28 47.717  -06 48 26.71  24.6w 15GY57    568  C~2nvY      
2016 05  01.35239  13 27 15.197  -06 39 30.44  24.8w 15GY57    568  C~2nvY      
2016 05  01.36453  13 27 15.161  -06 39 30.01  25.5w 15GY57    568  C~2nvY      
2016 05  02.29500  13 27 11.412  -06 39 09.19  25.2w 15GY57    568  C~2nvY      
2016 05  02.30717  13 27 11.357  -06 39 08.80  25.1w 15GY57    568  C~2nvY      
2016 05  06.30476  13 26 55.546  -06 37 40.28  25.3w 15GY57    568  C~2nvY      
2016 05  06.31695  13 26 55.502  -06 37 40.15  25.0w 15GY57    568  C~2nvY      
2016 05  28.26791  13 25 40.542  -06 30 58.48  24.9w 15GY57    568  C~2nvY      
2016 05  28.27195  13 25 40.530  -06 30 58.51  24.9w 15GY57    568  C~2nvY      
2016 06  04.34936  13 25 21.899  -06 29 26.34  25.1w 15GY57    568  C~2nvY      
2016 06  04.35340  13 25 21.905  -06 29 26.28  25.5w 15GY57    568  C~2nvY      
2016 06  27.27271  13 24 45.655  -06 27 00.83  25.0w 15GY57    568  C~2nvY      
2016 07  06.30847  13 24 42.491  -06 27 12.19  24.6w 15GY57    568  C~2nvY      
2017 02  24.63168  13 35 56.332  -07 31 59.84        15GY57    568  C~2nvY      
2017 03  29.44523  13 34 05.046  -07 20 14.29  24.8w 15GY57    568  C~2nvY      
2017 06  22.26639  13 29 16.996  -06 54 06.87  25.1w 15GY57    568  C~2nvY      

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     0.09       0.00     0.06
     2   0.0001     -1.61    -0.06       0.10     0.08
     3   0.0083   -111.05    -0.23       7.57    -0.02
     4   0.0793  -1428.09    -0.36      58.31    -0.02
     5   0.0795  -1430.23     0.04      58.30    -0.07
     6   0.0848  -1551.30     0.12      61.01     0.07
     7   0.1449  -3010.37     0.04      75.51     0.06
     8   0.1500  -3138.33     0.08      75.42    -0.08
     9   0.1501  -3141.18     0.08      75.52     0.04
    10   0.1503  -3146.37     0.09      75.35    -0.10
    11   0.1503  -3146.83    -0.03      75.42    -0.02
    12   0.1669  -3560.45     0.01      73.81    -0.22
    13   0.2456  -5350.77     0.05      40.76     0.02
    14   0.3359  -6575.50     0.00     -41.12    -0.03
    15   0.3361  -6576.36    -0.06     -41.19     0.04
    16   0.3415  -6610.75    -0.10     -47.04     0.14
    17   0.4016  -6649.44     0.02    -115.66    -0.04
    18   0.4182  -6549.96     0.10    -134.76    -0.04
    19   0.9637   4638.87     0.04     -69.14     0.08
    20   0.9801   4516.35     0.08     -52.19     0.03
    21   1.0622   3276.12     0.12      15.67    -0.20
    22   1.1249   1841.24    -0.05      40.52     0.06
    23   1.1412   1434.04    -0.07      42.17    -0.03
    24   1.2013    -44.83    -0.05      31.68     0.01
    25   1.2014    -45.48     0.09      31.88     0.23
    26   1.2039   -105.08     0.11      30.58    -0.08
    27   1.2039   -105.99    -0.00      30.64    -0.00
    28   1.2149   -357.60    -0.02      25.80     0.07
    29   1.2149   -358.25     0.09      25.68    -0.03
    30   1.2750  -1544.64     0.07     -14.50     0.08
    31   1.2750  -1544.79     0.10     -14.59     0.00
    32   1.2944  -1836.87    -0.13     -31.82    -0.03
    33   1.2944  -1836.81     0.09     -31.74     0.07
    34   1.3572  -2392.58    -0.24     -96.88    -0.03
    35   1.3819  -2432.18    -0.03    -124.92     0.05
    36   2.0207   8331.36    -0.06     -47.03    -0.04
    37   2.1105   6530.39     0.01       4.32    -0.10
    38   2.3428   1964.83    -0.05    -113.23    -0.01

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.

15GY57    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj        43.686    43.703    43.669
ecceobj         0.074     0.076     0.073
incobj          2.311     2.311     2.311
qmin           39.469    39.406    39.492
qmax           48.707    48.804    48.626
amean          43.946    43.963    43.929
amin           43.594    43.613    43.574
amax           44.327    44.347    44.306
emean           0.082     0.084     0.080
emin            0.063     0.066     0.062
emax            0.099     0.101     0.097
imean           1.084     1.087     1.081
imin            0.093     0.093     0.093
imax            1.718     1.725     1.712
excite_mean     0.085     0.086     0.083
fracstop        1.000     1.000     1.000
cjmean          3.092     3.092     3.092

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       173.8     173.6     174.0
kozaiamp        180.0     180.0     180.0