Orbit Fit and Astrometric record for 15FP398

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: 15FP398   
# Created Tue Jun 17 01:10:28 2025
# Orbit generated from Bernstein formalism
# Fitting      7 observations of      7
# Arc:   2.06d
# First observation: 2015/03/18
#  Last observation: 2015/03/20
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit:     0.05 DOF:     10 RMS:  0.02
# Min/Max residuals:    -0.02    0.03
# Exact a, adot, b, bdot, g, gdot:
  1.466363E-05  2.096088E-02 -1.243000E-06 -1.733159E-03  2.237536E-02  0.000000E+00
# Covariance matrix:
  2.7908E-11  3.8879E-08 -1.1467E-14 -2.8691E-11  6.1758E-09  0.0000E+00
  3.8879E-08  5.4906E-05 -1.6179E-11 -4.0438E-08  8.7061E-06  0.0000E+00
 -1.1467E-14 -1.6179E-11  2.9397E-13 -4.9096E-11 -2.5661E-12  0.0000E+00
 -2.8691E-11 -4.0438E-08 -4.9096E-11  2.8704E-08 -6.4157E-09  0.0000E+00
  6.1758E-09  8.7061E-06 -2.5661E-12 -6.4157E-09  1.3812E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  1.4741E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
    1.447236  179.424204    0.035628    0.025169   -0.991198  2457099.992657
# Heliocentric elements and errors
Epoch:              2457090.5000  =  2015/03/09
Mean Anomaly:            1.15386 +/-   101.849
Argument of Peri:      162.01683 +/-   168.255
Long of Asc Node:       16.05528 +/-     5.701
Inclination:             4.92241 +/-     1.633
Eccentricity:         0.02715306 +/-    0.5594
Semi-Major Axis:     46.96122767 +/-   24.5886
Time of Perihelion: 2456713.7444 +/-  385892.9
Perihelion:          45.68608652 +/-   35.5283
Aphelion:            48.23636883 +/-   36.4408
Period (y)              321.8232 +/-    252.76
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -45.66975308 +/-    2.3465
Ecliptic Y            0.49435198 +/-    0.0238
Ecliptic Z            1.12871964 +/-    0.0593
Ecliptic XDOT        -0.00003455 +/-    0.0015
Ecliptic YDOT        -0.00257036 +/-    0.0008
Ecliptic ZDOT        -0.00021191 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   45.68637366 +/-    2.3457
Geocenter to KBO     44.69202429 +/-    2.3474
# Hcoef:  6.55

The following table shows the complete astrometric record for 15FP398. 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 (15FP398) followed by the observatory code and reference code for the source of the astrometry.

2015 03  18.491879 12 00 11.407  +01 33 24.57  22.9r 15FP398   568  C~2TuH      
2015 03  18.518557 12 00 11.292  +01 33 25.26  23.1r 15FP398   568  C~2TuH      
2015 03  18.520734 12 00 11.281  +01 33 25.33  23.1r 15FP398   568  C~2TuH      
2015 03  18.549212 12 00 11.161  +01 33 26.11  23.3r 15FP398   568  C~2TuH      
2015 03  20.474493 12 00 03.126  +01 34 16.45  22.7i 15FP398   568  C~2TuH      
2015 03  20.518991 12 00 02.935  +01 34 17.62  22.6i 15FP398   568  C~2TuH      
2015 03  20.554741 12 00 02.784  +01 34 18.56  22.6i 15FP398   568  C~2TuH      

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     0.03       0.00     0.00
     2   0.0001     -1.86     0.01      -0.05    -0.01
     3   0.0001     -2.04    -0.02      -0.05    -0.01
     4   0.0002     -4.00    -0.02      -0.05     0.02
     5   0.0054   -134.56     0.02      -1.81    -0.00
     6   0.0055   -137.65    -0.01      -1.88    -0.00
     7   0.0056   -140.10    -0.00      -1.91     0.00

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.

15FP398    quality flag:0

Type:      ERR2LARGE ERR2LARGE ERR2LARGE

axisobj         0.000     0.000     0.000
ecceobj        -1.000    -1.000    -1.000
incobj         -1.000    -1.000    -1.000
qmin            0.000     0.000     0.000
qmax            0.000     0.000     0.000
amean           0.000     0.000     0.000
amin            0.000     0.000     0.000
amax            0.000     0.000     0.000
emean           0.000     0.000     0.000
emin            0.000     0.000     0.000
emax            0.000     0.000     0.000
imean           0.000     0.000     0.000
imin            0.000     0.000     0.000
imax            0.000     0.000     0.000
excite_mean     0.000     0.000     0.000
fracstop        0.000     0.000     0.000
cjmean          0.000     0.000     0.000

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         0.0       0.0       0.0
kozaiamp          0.0       0.0       0.0