Orbit Fit and Astrometric record for 07RT15

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: 07RT15    
# Created Thu May 24 01:37:35 2012
# Orbit generated from Bernstein formalism
# Fitting   20 observations of   22
# Arc:   4.78y
# First observation: 2003/10/22
#  Last observation: 2008/08/03
Preliminary a, adot, b, bdot, g, gdot:
   0.000490   0.041867   0.000042   0.003453   0.033591   0.000000
# Chi-squared of fit:    55.30 DOF:   34 RMS:  0.29
# Min/Max residuals:    -1.23    0.61
# Exact a, adot, b, bdot, g, gdot:
  1.994268E-05  4.224744E-02  1.793607E-06  3.505193E-03  3.374118E-02  1.831137E-03
# Covariance matrix:
  4.8929E-13 -2.1114E-13  1.3266E-15 -7.9754E-15 -7.6504E-14 -5.2708E-13
 -2.1114E-13  6.1373E-13 -7.1175E-15  4.7965E-14  5.3946E-13  3.2274E-12
  1.3266E-15 -7.1175E-15  4.7308E-13 -1.1546E-13 -1.7128E-15 -3.6524E-14
 -7.9754E-15  4.7965E-14 -1.1546E-13  3.7002E-14  4.3790E-14  2.6611E-13
 -7.6504E-14  5.3946E-13 -1.7128E-15  4.3790E-14  9.3365E-13  3.2661E-12
 -5.2708E-13  3.2274E-12 -3.6524E-14  2.6611E-13  3.2661E-12  1.8103E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
  -12.393089   13.868213   -0.245004   -0.207281   -0.943469  2452934.727953
# Heliocentric elements and errors
Epoch:              2452930.5000  =  2003/10/18
Mean Anomaly:            9.63493 +/-     0.019
Argument of Peri:      275.88920 +/-     0.032
Long of Asc Node:       82.29708 +/-     0.001
Inclination:            12.92162 +/-     0.000
Eccentricity:         0.22684242 +/-    0.0001
Semi-Major Axis:     39.28134286 +/-    0.0047
Time of Perihelion: 2450523.7885 +/-       4.8
Perihelion:          30.37066801 +/-    0.0045
Aphelion:            48.19201771 +/-    0.0063
Period (y)              246.1998 +/-      0.04
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           28.97881056 +/-    0.0008
Ecliptic Y            7.41148712 +/-    0.0002
Ecliptic Z           -6.36063304 +/-    0.0002
Ecliptic XDOT        -0.00062626 +/-    0.0000
Ecliptic YDOT         0.00337153 +/-    0.0000
Ecliptic ZDOT         0.00024606 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   30.58037370 +/-    0.0008
Geocenter to KBO     29.63737826 +/-    0.0008
# Hcoef:  6.92

The following table shows the complete astrometric record for 07RT15. 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 (07RT15) followed by the observatory code and reference code for the source of the astrometry.

2003 10  22.22721  01 10 15.58   -05 57 26.1   21.3R 07RT15    675  Cz3609      
2003 10  22.28900  01 10 15.21   -05 57 27.9   21.8R 07RT15    675  Cz3609      
2003 10  22.35265  01 10 14.82   -05 57 29.2   21.5R 07RT15    675  Cz3609      
2007 09  05.39053  01 48 23.21   -01 00 13.9   21.8V 07RT15    705  Cz2999      
2007 09  05.39385  01 48 23.21   -01 00 14.0   22.4  07RT15    705  Cz2999      
2007 09  11.31700  01 47 59.74   -01 03 42.7   21.4R 07RT15    675  Cv5236      
2007 09  11.36045  01 47 59.54   -01 03 45.4   21.9R 07RT15    675  Cv5236      
2007 09  12.35634  01 47 55.28   -01 04 20.7   21.4R 07RT15    675  Cv5236      
2007 09  14.34845  01 47 46.58   -01 05 33.8   21.6V 07RT15    705  Cz2999      
2007 09  14.35177  01 47 46.56   -01 05 33.9   22.5  07RT15    705  Cz2999      
2007 09  16.38006  01 47 37.31   -01 06 48.1   22.0V 07RT15    705  Cz2999      
2007 09  16.38338  01 47 37.33   -01 06 48.3   22.8  07RT15    705  Cz2999      
2007 09  19.39799  01 47 23.02   -01 08 38.8   22.1V 07RT15    705  Cz2999      
2007 09  19.40131  01 47 23.00   -01 08 39.0   22.9  07RT15    705  Cz2999      
2007 10  18.31528  01 44 41.44   -01 25 38.7         07RT15    675  Cx3444      
2007 10  18.36904  01 44 41.11   -01 25 40.2         07RT15    675  Cx3444      
2007 10  18.42292  01 44 40.72   -01 25 42.4         07RT15    675  Cx3444      
2007 12  04.14350  01 40 30.79   -01 39 47.0         07RT15    675  Cx3444      
2007 12  14.10656  01 39 57.07   -01 39 16.9         07RT15    675  Cx3444      
2008 07  31.41417  01 57 35.86   +00 21 31.2         07RT15    675  Cz3609      
2008 08  02.40157  01 57 36.49   +00 20 56.1         07RT15    675  Cz3609      
2008 08  03.39818  01 57 36.64   +00 20 37.2         07RT15    675  Cz3609      

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    -0.03
  2   0.0002     -5.79    -0.03       0.48    -0.13
  3   0.0003    -11.65     0.05       1.55     0.33
  4   3.8718  38952.49     0.02    2931.37     0.01
  5   3.8718  38952.45     0.21    2931.27    -0.05
  6   3.8880  38532.07 (   0.45)   2878.27 (   1.29)
  7   3.8881  38528.10    -0.20    2876.96     0.30
  8   3.8908  38452.90 (  -0.09)   2869.75 (   0.97)
  9   3.8963  38298.93     0.26    2854.10    -0.06
 10   3.8963  38298.61     0.20    2854.12    -0.01
 11   3.9019  38136.40    -0.11    2840.76    -0.02
 12   3.9019  38136.61     0.37    2840.46    -0.31
 13   3.9101  37887.53     0.17    2823.80    -0.04
 14   3.9101  37887.17     0.08    2823.73    -0.10
 15   3.9893  35175.98    -0.24    2847.94    -0.28
 16   3.9894  35170.69    -0.17    2848.53    -0.09
 17   3.9896  35164.27    -1.23    2848.83    -0.19
 18   4.1175  31291.57     0.20    3565.17    -0.31
 19   4.1448  30829.29     0.54    3795.19     0.12
 20   4.7753  48947.97    -0.15    4180.80     0.61
 21   4.7808  48942.30     0.00    4143.81     0.41
 22   4.7835  48936.50     0.08    4125.04    -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.

07RT15    quality flag:3

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

axisobj        39.777    39.792    39.763
ecceobj         0.236     0.237     0.236
incobj         12.918    12.918    12.918
qmin           28.891    28.878    28.912
qmax           50.220    50.233    50.258
amean          39.454    39.454    39.454
amin           39.317    39.317    39.314
amax           39.615    39.607    39.613
emean           0.244     0.244     0.244
emin            0.214     0.214     0.215
emax            0.268     0.268     0.269
imean           9.789     9.773     9.806
imin            8.322     8.294     8.351
imax           11.592    11.593    11.591
excite_mean     0.298     0.298     0.298
fracstop        1.000     1.000     1.000
cjmean          2.951     2.951     2.951

libcent 0       180.2     180.1     179.7
libamp  0        63.0      62.0      64.6
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       269.3     269.3     269.3
kozaiamp         36.5      36.4      36.4