Orbit Fit and Astrometric record for 99RY214

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: 99RY214   
# Created Fri May  2 02:36:29 2008
# Orbit generated from Bernstein formalism
# Fitting   19 observations of   22
# Arc:   7.85y
# First observation: 1999/09/06
#  Last observation: 2007/07/12
Preliminary a, adot, b, bdot, g, gdot:
  -0.000073   0.029752  -0.000024   0.005320   0.027495   0.000000
# Chi-squared of fit:    28.55 DOF:   32 RMS:  0.22
# Min/Max residuals:    -0.66    0.53
# Exact a, adot, b, bdot, g, gdot:
  1.722099E-05  2.940034E-02  3.839889E-06  5.254383E-03  2.711670E-02 -1.831768E-03
# Covariance matrix:
  1.3747E-13 -5.0129E-14  1.4316E-15 -3.4906E-15  5.7672E-14 -1.2247E-13
 -5.0129E-14  1.7846E-13 -1.3261E-14  3.0698E-14  2.0718E-13  7.4490E-13
  1.4316E-15 -1.3261E-14  1.0991E-13 -2.2822E-14 -2.0500E-14 -6.0130E-14
 -3.4906E-15  3.0698E-14 -2.2822E-14  1.8706E-14  4.6734E-14  1.3910E-13
  5.7672E-14  2.0718E-13 -2.0500E-14  4.6734E-14  6.4691E-13  9.7989E-13
 -1.2247E-13  7.4490E-13 -6.0130E-14  1.3910E-13  9.7989E-13  3.3563E-12
#      lat0       lon0       xBary       yBary       zBary        JD0
    9.362985    9.349903    0.441548    0.145973   -0.886720  2451427.939683
# Heliocentric elements and errors
Epoch:              2451420.5000  =  1999/08/30
Mean Anomaly:          341.18548 +/-     0.013
Argument of Peri:       69.79685 +/-     0.018
Long of Asc Node:      327.27812 +/-     0.001
Inclination:            13.67338 +/-     0.000
Eccentricity:         0.18688257 +/-    0.0001
Semi-Major Axis:     45.62555328 +/-    0.0063
Time of Perihelion: 2457303.5340 +/-       3.7
Perihelion:          37.09893273 +/-    0.0068
Aphelion:            54.15217382 +/-    0.0087
Period (y)              308.1913 +/-      0.06
# Ecliptic coordinates at JD0 (AU and AU/d)
Ecliptic X           36.86894832 +/-    0.0011
Ecliptic Y            5.62425394 +/-    0.0002
Ecliptic Z            5.99972535 +/-    0.0002
Ecliptic XDOT        -0.00075155 +/-    0.0000
Ecliptic YDOT         0.00289364 +/-    0.0000
Ecliptic ZDOT         0.00049342 +/-    0.0000
# Distances at JD0 (AU)
Heliocenter to KBO   37.77496906 +/-    0.0010
Geocenter to KBO     36.87763768 +/-    0.0011
# Hcoef:  7.32

The following table shows the complete astrometric record for 99RY214. 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 (99RY214) followed by the observatory code and reference code for the source of the astrometry.

1999 09  06.43894  00 19 20.48   +12 17 59.3   22.8R 99RY214   568  Ca8546      
1999 09  06.48649  00 19 20.26   +12 17 58.6   22.8R 99RY214   568  Ca8546      
1999 09  06.52690  00 19 20.06   +12 17 57.8   22.8R 99RY214   568  Ca8546      
1999 09  09.47537  00 19 06.24   +12 16 58.6   22.8R 99RY214   568  Ca8546      
1999 09  09.48697  00 19 06.21   +12 16 58.6   22.8R 99RY214   568  Ca8546      
1999 09  10.47595  00 19 01.51   +12 16 37.7   22.9R 99RY214   568  Ca8546      
1999 09  10.48639  00 19 01.46   +12 16 37.3   22.6R 99RY214   568  Ca8546      
1999 10  08.40856  00 16 42.11   +12 04 09.5   23.2R 99RY214   568  Ca8546      
1999 10  08.43404  00 16 42.00   +12 04 08.8   23.0R 99RY214   568  Ca8546      
1999 11  10.31627  00 14 19.64   +11 46 56.2   23.1R 99RY214   568  Ca8546      
1999 11  10.36475  00 14 19.45   +11 46 54.2   23.1R 99RY214   568  Ca8546      
2000 08  27.55819  00 25 52.53   +13 17 31.9   22.9R 99RY214   568  Cb9109      
2000 08  27.59454  00 25 52.37   +13 17 31.1   23.0R 99RY214   568  Cb9109      
2000 08  29.60300  00 25 43.98   +13 17 03.9   22.7R 99RY214   568  Cb9109      
2000 08  29.63530  00 25 43.83   +13 17 03.5   22.9R 99RY214   568  Cb9109      
2000 12  27.22020  00 19 02.621  +12 27 43.75  22.0R 99RY214   568  Cl2529      
2000 12  28.22887  00 19 03.690  +12 27 36.46  22.1R 99RY214   568  Cl2529      
2002 11  05.32464  00 32 15.67   +14 40 40.9   22.5R 99RY214   568  Cl8251      
2002 11  05.36123  00 32 15.51   +14 40 40.1         99RY214   568  Cl8251      
2002 11  06.39525  00 32 11.33   +14 40 06.5         99RY214   568  Cl8251      
2007 07  12.35358  01 09 50.29   +19 33 25.0         99RY214   304  Cv1964      
2007 07  12.43263  01 09 50.35   +19 33 27.3         99RY214   304  Cv1964      

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    -0.02       0.00    -0.16
  2   0.0001     -3.23     0.13       0.65     0.01
  3   0.0002     -6.24     0.00       1.10     0.05
  4   0.0083   -215.50    -0.21      28.28     0.14
  5   0.0083   -215.91     0.24      28.45     0.21
  6   0.0111   -287.39     0.23      37.00     0.14
  7   0.0111   -288.22     0.17      36.93    -0.03
  8   0.0875  -2459.68     0.05     175.90    -0.17
  9   0.0876  -2461.44     0.34     175.91    -0.20
 10   0.1776  -4790.67 (  -0.14)     77.74 (   0.91)
 11   0.1778  -4794.03    -0.66      77.05     0.53
 12   0.9750   6686.06    -0.13     989.17     0.11
 13   0.9751   6683.60    -0.35     989.36    -0.15
 14   0.9806   6560.23     0.03    1012.89    -0.10
 15   0.9807   6558.06    -0.08    1013.39     0.03
 16   1.3081     -4.74 (  -0.54)    640.33 (   0.89)
 17   1.3109      6.66 (  -0.56)    627.36 (   1.00)
 18   3.1646  13793.46    -0.04    3391.79    -0.42
 19   3.1647  13790.99     0.02    3391.95    -0.02
 20   3.1676  13721.72     0.33    3384.59    -0.23
 21   7.8464  51323.98     0.01    7953.89     0.07
 22   7.8467  51325.67    -0.06    7955.83     0.20

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.

99RY214    quality flag:3

Type:       SCATNEAR  SCATNEAR  SCATNEAR

axisobj       45.602    45.620    45.583
ecceobj        0.187     0.187     0.186
incobj        13.679    13.679    13.679
qmin          36.405    36.383    36.445
qmax          54.429    54.371    54.508
amean         45.200    45.216    45.178
amin          44.809    44.817    44.806
amax          45.651    45.655    45.640
emean          0.176     0.176     0.175
emin           0.160     0.162     0.160
emax           0.193     0.192     0.194
imean         14.855    14.862    14.840
imin          14.252    14.273    14.206
imax          15.559    15.539    15.540
fracstop       1.000     1.000     1.000
cjmean         2.997     2.997     2.997

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      180.8     179.2     184.5
kozaiamp       180.0     180.0     180.0