Orbit Fit and Astrometric record for 99RN215

The following information shows the result of the orbit fit based on Gary Bernstein's method. Most of the information should be self-explanatory.

# Object: 99RN215   
# Created Fri May  2 02:36:29 2008
# Orbit generated from Bernstein formalism
# Fitting   20 observations of   22
# Arc:   6.08y
# First observation: 1999/09/07
#  Last observation: 2005/10/06
Preliminary a, adot, b, bdot, g, gdot:
  -0.000007   0.020641   0.000005  -0.003000   0.022777   0.000000
# Chi-squared of fit:    27.91 DOF:   34 RMS:  0.21
# Min/Max residuals:    -0.41    0.40
# Exact a, adot, b, bdot, g, gdot:
  1.491360E-05  2.067072E-02 -1.674387E-06 -3.001857E-03  2.275468E-02  1.499473E-03
# Covariance matrix:
  1.5742E-13 -5.6343E-14 -2.9047E-15  6.2926E-15  9.8051E-14 -3.4594E-13
 -5.6343E-14  1.8663E-13  9.4950E-15 -2.6754E-14  1.2550E-13  1.5255E-12
 -2.9047E-15  9.4950E-15  1.1537E-13 -2.7058E-14  3.0955E-15  8.7077E-14
  6.2926E-15 -2.6754E-14 -2.7058E-14  2.0071E-14 -1.4885E-14 -2.4175E-13
  9.8051E-14  1.2550E-13  3.0955E-15 -1.4885E-14  4.8539E-13  8.9069E-13
 -3.4594E-13  1.5255E-12  8.7077E-14 -2.4175E-13  8.9069E-13  1.3760E-11
#      lat0       lon0       xBary       yBary       zBary        JD0
   -9.399731    8.643998    0.413697   -0.149078   -0.899169  2451429.011913
# Heliocentric elements and errors
Epoch:              2451420.5000  =  1999/08/30
Mean Anomaly:          113.59487 +/-     0.109
Argument of Peri:      107.66199 +/-     0.100
Long of Asc Node:      140.59341 +/-     0.001
Inclination:            12.39676 +/-     0.000
Eccentricity:         0.06816653 +/-    0.0001
Semi-Major Axis:     43.50513904 +/-    0.0047
Time of Perihelion: 2418348.1184 +/-      31.4
Perihelion:          40.53954481 +/-    0.0077
Aphelion:            46.47073326 +/-    0.0080
Period (y)              286.9585 +/-      0.05
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           43.83530053 +/-    0.0013
Ecliptic Y            6.24682451 +/-    0.0002
Ecliptic Z           -7.17754999 +/-    0.0002
Ecliptic XDOT        -0.00026023 +/-    0.0000
Ecliptic YDOT         0.00248506 +/-    0.0000
Ecliptic ZDOT        -0.00038574 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   44.85614353 +/-    0.0013
Geocenter to KBO     43.94701257 +/-    0.0013
# Hcoef:  6.61

The following table shows the complete astrometric record for 99RN215. 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 (99RN215) followed by the observatory code and reference code for the source of the astrometry.

1999 09  07.51117  00 46 34.72   -05 12 47.8   22.7R 99RN215   568  Ca9937      
1999 09  07.55015  00 46 34.56   -05 12 48.6   22.6R 99RN215   568  Ca9937      
1999 09  07.59142  00 46 34.41   -05 12 50.2   22.8R 99RN215   568  Ca9937      
1999 09  09.58802  00 46 27.11   -05 13 51.4   22.9R 99RN215   568  Ca9937      
1999 09  09.59815  00 46 27.07   -05 13 51.8   23.1R 99RN215   568  Ca9937      
1999 10  09.52946  00 44 25.36   -05 28 36.5   23.0R 99RN215   568  Ca9937      
1999 10  10.36662  00 44 21.85   -05 28 59.0   22.9R 99RN215   568  Ca9937      
1999 10  10.40770  00 44 21.67   -05 29 00.2   22.5R 99RN215   568  Ca9937      
1999 11  10.42344  00 42 22.52   -05 39 36.8   22.8R 99RN215   568  Ca9937      
1999 11  10.45826  00 42 22.40   -05 39 37.3   23.0R 99RN215   568  Ca9937      
2000 08  28.49536  00 51 44.75   -04 49 25.6   22.9R 99RN215   568  Cb9109      
2000 08  28.55058  00 51 44.59   -04 49 27.4   22.9R 99RN215   568  Cb9109      
2000 08  29.54245  00 51 41.44   -04 49 57.2   22.9R 99RN215   568  Cb9109      
2000 08  29.57883  00 51 41.34   -04 49 57.9   22.9R 99RN215   568  Cb9109      
2000 12  27.24300  00 45 40.145  -05 21 09.27        99RN215   568  Cl2529      
2000 12  28.25263  00 45 40.385  -05 20 55.16  22.9R 99RN215   568  Cl2529      
2002 11  06.44491  00 56 27.58   -04 42 58.2   22.6R 99RN215   568  Cl8251      
2002 11  07.34025  00 56 24.33   -04 43 12.8         99RN215   568  Cl8251      
2002 11  07.38084  00 56 24.20   -04 43 13.1         99RN215   568  Cl8251      
2005 10  06.26674  01 12 16.461  -03 34 52.36  22.3R 99RN215   500              
2005 10  06.27345  01 12 16.430  -03 34 52.58        99RN215   500              
2005 10  06.28016  01 12 16.402  -03 34 52.77        99RN215   500              

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    -0.11       0.00    -0.08
  2   0.0001     -2.51    -0.17       0.21     0.37
  3   0.0002     -5.20    -0.27      -0.38     0.05
  4   0.0057   -129.55     0.12     -13.54     0.19
  5   0.0057   -130.26     0.06     -13.68     0.12
  6   0.0877  -2149.61     0.23    -109.62    -0.16
  7   0.0900  -2206.65     0.14    -109.64    -0.33
  8   0.0901  -2209.60     0.04    -109.69    -0.41
  9   0.1750  -4095.83    -0.05       5.41    -0.34
 10   0.1751  -4097.67    -0.13       5.66    -0.35
 11   0.9746   4810.17     0.02    -546.05     0.40
 12   0.9748   4807.25     0.19    -546.75     0.15
 13   0.9775   4752.18    -0.22    -555.43     0.09
 14   0.9776   4750.53     0.18    -555.48     0.33
 15   1.3052   -946.91 (   0.40)   -138.99 (   0.92)
 16   1.3080   -938.05 (   0.51)   -127.44 (   0.85)
 17   3.1648   8848.30     0.36   -1872.37    -0.07
 18   3.1672   8797.82    -0.36   -1866.40     0.05
 19   3.1673   8795.92     0.02   -1865.90     0.25
 20   6.0801  23590.97     0.02   -3831.58    -0.07
 21   6.0801  23590.45    -0.03   -3831.59    -0.08
 22   6.0801  23589.99    -0.03   -3831.60    -0.09

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.

99RN215    quality flag:3

Type:      CLASSICAL CLASSICAL CLASSICAL

axisobj       43.479    43.492    43.466
ecceobj        0.068     0.068     0.068
incobj        12.402    12.402    12.402
qmin          39.616    39.610    39.598
qmax          47.045    47.070    47.019
amean         43.218    43.231    43.205
amin          42.882    42.895    42.864
amax          43.577    43.587    43.558
emean          0.065     0.065     0.065
emin           0.051     0.051     0.052
emax           0.080     0.081     0.080
imean         11.348    11.347    11.350
imin          10.802    10.804    10.802
imax          12.031    12.030    12.044
fracstop       1.000     1.000     1.000
cjmean         3.041     3.041     3.041

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      183.5     183.5     183.5
kozaiamp       180.0     180.0     180.0