Orbit Fit and Astrometric record for 05VD

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: 05VD      
# Created Sun May 19 01:37:30 2013
# Orbit generated by ELGB
# -->Covariance matrix from a Bernstein fit
# Fitting   36 observations of   37
# Arc:   0.82y
# First observation: 2005/11/01
#  Last observation: 2006/08/28
# Chi-squared of fit:   222.54 DOF:   66 RMS:  0.44
# Min/Max residuals:    -1.43    1.60
# Exact a, adot, b, bdot, g, gdot:
 -4.934117E-05 -7.432717E-01 -4.341360E-06 -9.312462E-02  2.393350E-01  5.171161E-02
# Covariance matrix:
  1.0641E-13 -7.7319E-13  3.5628E-15 -6.8689E-14  2.5237E-13  8.3356E-13
 -7.7319E-13  3.6853E-11 -2.4368E-13  8.3396E-12  1.5925E-12 -1.0216E-10
  3.5628E-15 -2.4368E-13  5.8871E-14 -1.3966E-13 -1.8988E-14  7.1578E-13
 -6.8689E-14  8.3396E-12 -1.3966E-13  2.5421E-12  1.0671E-12 -2.6129E-11
  2.5237E-13  1.5925E-12 -1.8988E-14  1.0671E-12  2.2844E-12 -1.3134E-11
  8.3356E-13 -1.0216E-10  7.1578E-13 -2.6129E-11 -1.3134E-11  3.2033E-10
#      lat0       lon0       xBary       yBary       zBary        JD0
    2.583738    1.942573   -0.597059    0.036089   -0.797403  2453675.714113
# Heliocentric elements and errors
Epoch:              2453675.5000  =  2005/11/01
Mean Anomaly:          352.10023 +/-     0.005
Argument of Peri:      176.13903 +/-     0.008
Long of Asc Node:      171.36457 +/-     0.000
Inclination:           172.82934 +/-     0.000
Eccentricity:         0.25466136 +/-    0.0000
Semi-Major Axis:      6.67934789 +/-    0.0004
Time of Perihelion: 2453813.8603 +/-       0.5
Perihelion:           4.97837609 +/-    0.0003
Aphelion:             8.38031969 +/-    0.0005
Period (y)               17.2627 +/-      0.00
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X            4.94509865 +/-    0.0000
Ecliptic Y            0.76324050 +/-    0.0000
Ecliptic Z            0.18834626 +/-    0.0000
Ecliptic XDOT         0.00092906 +/-    0.0000
Ecliptic YDOT        -0.00848249 +/-    0.0000
Ecliptic ZDOT        -0.00103753 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO    5.00720562 +/-    0.0000
Geocenter to KBO      4.17827407 +/-    0.0000
# Hcoef: 14.17

The following table shows the complete astrometric record for 05VD. 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 (05VD) followed by the observatory code and reference code for the source of the astrometry.

2005 11  01.21337  00 03 00.93   +03 08 35.1   21.3V 05VD      G96  Co7993      
2005 11  01.22213  00 03 00.32   +03 08 30.9   21.6V 05VD      G96  Co7993      
2005 11  01.23086  00 02 59.82   +03 08 26.2   21.3V 05VD      G96  Co7993      
2005 11  01.23961  00 02 59.17   +03 08 21.6   21.4V 05VD      G96  Co7993      
2005 11  01.26787  00 02 57.34   +03 08 07.8   21.2V 05VD      G96  Co7993      
2005 11  01.28425  00 02 56.24   +03 07 59.3   21.1V 05VD      G96  Co7993      
2005 11  01.29242  00 02 55.73   +03 07 55.2   21.4V 05VD      G96  Co7993      
2005 11  03.07575  00 01 01.23   +02 53 02.5         05VD      291  Co7993      
2005 11  03.08063  00 01 00.92   +02 52 59.2         05VD      291  Co7993      
2005 11  03.08632  00 01 00.59   +02 52 56.4         05VD      291  Co7993      
2005 11  03.14427  00 00 56.84   +02 52 27.5   20.5V 05VD      G96  Co7993      
2005 11  03.15141  00 00 56.41   +02 52 23.9   21.5V 05VD      G96  Co7993      
2005 11  03.15854  00 00 55.94   +02 52 20.2   21.2V 05VD      G96  Co7993      
2005 11  03.16569  00 00 55.51   +02 52 16.3   20.2V 05VD      G96  Co7993      
2005 11  11.266237 23 52 55.200  +01 48 47.06  21.5R 05VD      568  Cp1149      
2005 11  11.268035 23 52 55.104  +01 48 46.25  21.2R 05VD      568  Cp1149      
2005 11  11.275620 23 52 54.675  +01 48 42.87  21.5R 05VD      568  Cp1149      
2005 11  25.08925  23 41 56.11   +00 17 56.1         05VD      696  Cp2326      
2005 11  25.09640  23 41 55.76   +00 17 53.4         05VD      696  Cp2327      
2005 11  25.09998  23 41 55.47   +00 17 51.2         05VD      696  Cp2327      
2005 11  25.11072  23 41 55.18   +00 17 48.7         05VD      696  Cp2327      
2005 11  25.23385  23 41 50.13   +00 17 06.2   21.8V 05VD      705  cu5560      
2005 11  25.23468  23 41 50.12   +00 17 05.8   22.2  05VD      705  cu5560      
2005 11  26.21029  23 41 11.57   +00 11 35.0   21.8V 05VD      705  cu5560      
2005 11  26.21112  23 41 11.55   +00 11 34.9   22.5  05VD      705  cu5560      
2005 11  30.19419  23 38 44.86   -00 09 41.7   22.2V 05VD      705  cu5560      
2005 11  30.19502  23 38 44.83   -00 09 42.0   23.3  05VD      705  cu5560      
2005 12  01.19488  23 38 10.67   -00 14 43.9   21.9V 05VD      705  cu5560      
2005 12  01.19571  23 38 10.64   -00 14 44.2   22.6  05VD      705  cu5560      
2005 12  28.220799 23 28 59.414  -01 47 13.52  21.5R 05VD      568  Cq0485      
2005 12  28.243490 23 28 59.210  -01 47 16.23  21.4R 05VD      568  Cq0485      
2006 08  21.28405  23 00 00.34   -08 19 03.4   20.9V 05VD      691  Cr7076      
2006 08  21.30135  22 59 58.97   -08 19 13.2   20.9V 05VD      691  Cr7076      
2006 08  21.31865  22 59 57.62   -08 19 22.4   20.6V 05VD      691  Cr7076      
2006 08  28.30545  22 50 43.12   -09 23 25.6   20.9V 05VD      691  Cr7076      
2006 08  28.32564  22 50 41.46   -09 23 36.8   20.6V 05VD      691  Cr7076      
2006 08  28.34295  22 50 40.03   -09 23 46.5   20.2V 05VD      691  Cr7076      

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 (  -3.38)      0.00 ( -22.90)
  2   0.0000      0.00     0.44       0.00     0.29
  3   0.0000      0.00     1.57       0.00     0.02
  4   0.0001      0.00     0.46       0.00    -0.15
  5   0.0001      0.00     0.92       0.00     0.37
  6   0.0002      0.00     0.58       0.00     0.17
  7   0.0002      0.00     0.99       0.00     0.21
  8   0.0051      0.00     0.38       0.00     1.51
  9   0.0051      0.00     0.42       0.00     0.63
 10   0.0051      0.00     0.93       0.00     0.65
 11   0.0053      0.00     0.37       0.00     0.49
 12   0.0053      0.00     0.78       0.00     0.43
 13   0.0053      0.00     0.59       0.00     0.26
 14   0.0053      0.00     1.01       0.00    -0.10
 15   0.0275      0.00     0.55       0.00     0.49
 16   0.0275      0.00     0.62       0.00     0.47
 17   0.0275      0.00     0.54       0.00     0.46
 18   0.0654      0.00     1.60       0.00     0.61
 19   0.0654      0.00     0.73       0.00     0.36
 20   0.0654      0.00    -1.43       0.00    -0.61
 21   0.0654      0.00     0.81       0.00     0.58
 22   0.0658      0.00     0.38       0.00     0.35
 23   0.0658      0.00     0.74       0.00     0.24
 24   0.0684      0.00     0.41       0.00     0.11
 25   0.0684      0.00     0.60       0.00     0.29
 26   0.0793      0.00     0.47       0.00     0.27
 27   0.0793      0.00     0.46       0.00     0.22
 28   0.0821      0.00     0.37       0.00     0.30
 29   0.0821      0.00     0.34       0.00     0.25
 30   0.1561      0.00    -0.03       0.00     0.11
 31   0.1561      0.00    -0.03       0.00     0.13
 32   0.8024      0.00     0.93       0.00     0.48
 33   0.8024      0.00     0.81       0.00     0.17
 34   0.8025      0.00     1.00       0.00     0.46
 35   0.8216      0.00     1.24       0.00     0.57
 36   0.8217      0.00     0.93       0.00     0.48
 37   0.8217      0.00     0.57       0.00     0.29

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.

05VD    quality flag:3

Type:       CENTAURR  CENTAURR  CENTAURR

axisobj         6.668     6.668     6.668
ecceobj         0.250     0.250     0.250
incobj        172.810   172.810   172.810
qmin            4.995     4.995     4.995
qmax            8.348     8.348     8.348
amean           6.672     6.672     6.672
amin            6.672     6.672     6.672
amax            6.672     6.672     6.672
emean           0.251     0.251     0.251
emin            0.251     0.251     0.251
emax            0.251     0.251     0.251
imean         171.966   171.966   171.966
imin          171.966   171.966   171.966
imax          171.966   171.966   171.966
excite_mean     0.287     0.287     0.288
fracstop        0.000     0.000     0.000
cjmean          3.611     3.611     3.611

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       175.7     175.7     175.7
kozaiamp          0.0       0.0       0.0