Orbit Fit and Astrometric record for 04VX130

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: 04VX130   
# Created Fri Dec  3 02:10:10 2021
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting     22 observations of     22
# Arc:  16.08y
# First observation: 2004/11/09
#  Last observation: 2020/12/09
# Chi-squared of fit:    72.81 DOF:     38 RMS:  0.32
# Min/Max residuals:    -0.50    0.73
# Exact a, adot, b, bdot, g, gdot:
  1.725467E-05  3.277187E-02  3.305954E-06  3.290422E-03  2.961564E-02  5.634018E-03
# Covariance matrix:
  1.9305E-13 -1.2147E-13  1.1721E-14 -1.2089E-14  1.6880E-13 -2.2992E-13
 -1.2147E-13  1.3545E-13 -1.3806E-14  1.4241E-14 -2.1984E-13  2.7112E-13
  1.1721E-14 -1.3806E-14  9.6992E-14 -9.5953E-15  2.3541E-14 -2.8163E-14
 -1.2089E-14  1.4241E-14 -9.5953E-15  3.8813E-15 -2.4315E-14  2.9052E-14
  1.6880E-13 -2.1984E-13  2.3541E-14 -2.4315E-14  7.2244E-13 -4.6717E-13
 -2.2992E-13  2.7112E-13 -2.8163E-14  2.9052E-14 -4.6717E-13  5.5331E-13
#      lat0       lon0       xBary       yBary       zBary        JD0
   -0.331938   41.051423   -0.103737   -0.005616   -0.987383  2453318.888263
# Heliocentric elements and errors
Epoch:              2453318.5000  =  2004/11/09
Mean Anomaly:           45.69964 +/-     0.019
Argument of Peri:      291.02927 +/-     0.024
Long of Asc Node:       44.42922 +/-     0.000
Inclination:             5.75477 +/-     0.000
Eccentricity:         0.20533385 +/-    0.0001
Semi-Major Axis:     39.33957712 +/-    0.0065
Time of Perihelion: 2441877.7825 +/-       5.5
Perihelion:          31.26183025 +/-    0.0060
Aphelion:            47.41732399 +/-    0.0084
Period (y)              246.7475 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           26.13501991 +/-    0.0007
Ecliptic Y           22.90275254 +/-    0.0006
Ecliptic Z           -0.19551258 +/-    0.0000
Ecliptic XDOT        -0.00159674 +/-    0.0000
Ecliptic YDOT         0.00262073 +/-    0.0000
Ecliptic ZDOT         0.00030125 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   34.75063282 +/-    0.0007
Geocenter to KBO     33.76588760 +/-    0.0010
# Hcoef:  7.64

The following table shows the complete astrometric record for 04VX130. 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 (04VX130) followed by the observatory code and reference code for the source of the astrometry.

2004 11  09.38752  02 34 55.59   +14 49 40.1   23.1g 04VX130   568  C~0Ur5      
2004 11  09.41396  02 34 55.44   +14 49 39.5   23.1g 04VX130   568  C~0Ur5      
2004 11  09.43995  02 34 55.30   +14 49 38.9   23.1g 04VX130   568  C~0Ur5      
2004 11  10.30006  02 34 50.34   +14 49 17.5   23.0g 04VX130   568  C~0Ur5      
2004 11  10.30379  02 34 50.36   +14 49 17.6   23.0g 04VX130   568  C~0Ur5      
2005 01  05.22568  02 30 55.55   +14 32 44.7   23.1i 04VX130   568  C~0Ur5      
2005 01  05.28317  02 30 55.44   +14 32 44.3   23.4i 04VX130   568  C~0Ur5      
2005 01  05.35171  02 30 55.30   +14 32 44.2   23.0i 04VX130   568  C~0Ur5      
2005 10  25.51435  02 43 29.59   +15 40 47.6   22.8r 04VX130   568  C~0Ur5      
2005 10  25.58096  02 43 29.21   +15 40 46.1   23.1r 04VX130   568  C~0Ur5      
2005 10  25.59068  02 43 29.15   +15 40 45.8   23.1r 04VX130   568  C~0Ur5      
2005 10  26.55437  02 43 23.68   +15 40 22.6   23.2r 04VX130   568  C~0Ur5      
2006 10  23.24732  02 50 48.55   +16 25 08.7         04VX130   675  C~0Ur5      
2006 10  23.28645  02 50 48.33   +16 25 07.8   22.5R 04VX130   675  C~0Ur5      
2006 10  23.33627  02 50 48.04   +16 25 06.7         04VX130   675  C~0Ur5      
2007 11  08.21242  02 56 21.96   +17 01 13.5   23.4r 04VX130   695  C~0Ur5      
2007 11  08.27227  02 56 21.61   +17 01 12.1   23.7r 04VX130   695  C~0Ur5      
2009 08  18.45633  03 14 55.88   +18 35 55.7         04VX130   675  C~0Ur5      
2009 08  19.45039  03 14 56.36   +18 36 00.3         04VX130   675  C~0Ur5      
2020 12  09.284290 04 22 16.886  +23 56 25.81  22.7G 04VX130   G37  C~4Ty3      
2020 12  09.327050 04 22 16.586  +23 56 25.42        04VX130   G37  C~4Ty3      
2020 12  09.363010 04 22 16.387  +23 56 25.06        04VX130   G37  C~4Ty3      

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     0.15       0.00    -0.29
     2   0.0001      0.00     0.22       0.00    -0.22
     3   0.0001      0.00     0.40       0.00    -0.17
     4   0.0025      0.00    -0.29       0.00     0.02
     5   0.0025      0.00     0.33       0.00     0.21
     6   0.1556      0.00    -0.17       0.00     0.18
     7   0.1558      0.00    -0.20       0.00     0.14
     8   0.1560      0.00    -0.38       0.00     0.46
     9   0.9586      0.00     0.07       0.00    -0.43
    10   0.9588      0.00     0.11       0.00    -0.32
    11   0.9588      0.00     0.05       0.00    -0.39
    12   0.9614      0.00    -0.02       0.00    -0.50
    13   1.9517      0.00    -0.23       0.00     0.73
    14   1.9518      0.00    -0.23       0.00     0.70
    15   1.9519      0.00    -0.36       0.00     0.72
    16   2.9947      0.00     0.37       0.00    -0.11
    17   2.9949      0.00     0.42       0.00    -0.15
    18   4.7723      0.00    -0.07       0.00    -0.33
    19   4.7750      0.00    -0.08       0.00    -0.27
    20  16.0819      0.00     0.44       0.00    -0.11
    21  16.0820      0.00    -0.30       0.00     0.04
    22  16.0821      0.00    -0.12       0.00     0.14

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.

04VX130    quality flag:3

Type:           3:2E      3:2E      3:2E

axisobj        39.847    39.847    39.847
ecceobj         0.213     0.213     0.213
incobj          5.730     5.730     5.730
qmin           30.493    30.494    30.493
qmax           48.912    48.907    48.916
amean          39.455    39.455    39.455
amin           39.091    39.091    39.090
amax           39.873    39.870    39.876
emean           0.206     0.207     0.206
emin            0.188     0.188     0.188
emax            0.227     0.227     0.227
imean           4.844     4.844     4.844
imin            4.278     4.278     4.278
imax            5.625     5.625     5.625
excite_mean     0.223     0.223     0.223
fracstop        1.000     1.000     1.000
cjmean          2.995     2.995     2.995

libcent 0       179.9     180.0     179.8
libamp  0        36.8      36.8      36.8
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       205.0     205.1     205.1
kozaiamp        179.9     180.0     179.9