Orbit Fit and Astrometric record for 95GJ

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: 95GJ      
# Created Fri Nov  1 01:07:48 2024
# Orbit generated from Bernstein formalism
# Fitting      6 observations of      6
# Arc:   1.04d
# First observation: 1995/04/03
#  Last observation: 1995/04/04
# WARNING Fitting with energy constraint
# WARNING and with gdot fixed = 0
# Chi-squared of fit:     0.27 DOF:      8 RMS:  0.04
# Min/Max residuals:    -0.08    0.05
# Exact a, adot, b, bdot, g, gdot:
  1.461127E-05  2.391781E-02 -6.466653E-06 -1.071903E-02  2.591375E-02  0.000000E+00
# Covariance matrix:
  5.8023E-11  9.3820E-08 -9.4043E-14 -6.2506E-11  1.8118E-08  0.0000E+00
  9.3820E-08  1.5308E-04 -1.5343E-10 -1.0143E-07  2.9501E-05  0.0000E+00
 -9.4043E-14 -1.5343E-10  3.3762E-13 -1.0972E-10 -2.9570E-11  0.0000E+00
 -6.2506E-11 -1.0143E-07 -1.0972E-10  1.3036E-07 -1.9593E-08  0.0000E+00
  1.8118E-08  2.9501E-05 -2.9570E-11 -1.9593E-08  5.6904E-06  0.0000E+00
  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  0.0000E+00  2.2899E-04
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.115783  158.360286   -0.563088   -0.001688   -0.826035  2449810.742408
# Heliocentric elements and errors
Epoch:              2449810.5000  =  1995/04/03
Mean Anomaly:           27.08835 +/-   336.820
Argument of Peri:      151.96146 +/-    45.285
Long of Asc Node:      338.93542 +/-     0.056
Inclination:            24.15844 +/-    11.082
Eccentricity:         0.02291879 +/-    0.5953
Semi-Major Axis:     40.23183476 +/-   21.0196
Time of Perihelion: 2442797.0249 +/-  366789.3
Perihelion:          39.30976988 +/-   31.5506
Aphelion:            41.15389965 +/-   32.1861
Period (y)              255.1896 +/-    199.99
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X          -36.84379676 +/-    3.3019
Ecliptic Y           14.00377067 +/-    1.3102
Ecliptic Z           -0.07823424 +/-    0.0072
Ecliptic XDOT        -0.00092260 +/-    0.0015
Ecliptic YDOT        -0.00235069 +/-    0.0012
Ecliptic ZDOT        -0.00113267 +/-    0.0001
# Distances at JD0 (AU)
Heliocenter to KBO   39.41544207 +/-    3.1213
Geocenter to KBO     38.58954663 +/-    3.5523
# Hcoef:  6.85

The following table shows the complete astrometric record for 95GJ. 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 (95GJ) followed by the observatory code and reference code for the source of the astrometry.

1995 04  03.2417   10 39 49.23   +08 19 39.5   22.5R 95GJ      568  C25120      
1995 04  03.2708   10 39 49.11   +08 19 40.0         95GJ      568  C25120      
1995 04  03.3043   10 39 48.97   +08 19 40.7         95GJ      568  C25120      
1995 04  04.2678   10 39 45.07   +08 19 57.8         95GJ      568  C25120      
1995 04  04.2731   10 39 45.04   +08 19 57.9         95GJ      568  C25120      
1995 04  04.2778   10 39 45.03   +08 19 58.0         95GJ      568  C25120      

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    -0.00       0.00    -0.02
     2   0.0001     -1.84     0.02      -0.20    -0.03
     3   0.0002     -4.03    -0.02      -0.33     0.05
     4   0.0028    -64.11     0.04      -6.10     0.00
     5   0.0028    -64.56    -0.08      -6.17    -0.04
     6   0.0028    -64.73     0.04      -6.13     0.03

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.

95GJ    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