[IGSREPORT-19701] Wk 1631 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Apr 28 06:09:26 PDT 2011


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1631   (Apr 10, 2011 - Apr 16, 2011) 
                                                                               
Contact: J. Ray       (jim.ray at noaa.gov),                  
         J. Griffiths (jake.griffiths at noaa.gov)                            
                                                                               
                                                                               
COMBINATION STRATEGY:                                                            
---------------------                                                            
                                                                               
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1631.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed
to the values of the final IGS (GPS) combination.                                                    
                                                                               
                                                                               
SOFTWARE:                                                                       
---------                                                                       
                                                                               
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:

  Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS 
  Analysis Centers, Bulletin Geodesique, 69, pp 200-222.

  Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
  and Evaluation, Appendix I of the Analysis Coordinator Report, International
  GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.

  Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report, 
  International GPS Service for Geodynamics (IGS) 1995 Annual Report, 
  pp. 45-76.

  Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report, 
  International GPS Service for Geodynamics (IGS) 1996 Annual Report, 
  pp. 55-100.
                                                                               
  Weber R., 2000, IGS Technical Report 1999                                    
                                                                               
                                                                               
PRODUCTS GENERATED:                                                             
-------------------                                                             
                                                                               
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
                                                                               
The following naming convention is used for the result files:
                                                                               
 igl1631[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1631 in the SP3 format.
 igl16317.sum      Combination Report for GPS Week 1631.


    
    
REMARKS concerning the IGL Orbit Combination:                                  
---------------------------------------------

 1. Broadcast (brd) orbits and clocks are included in the combination for
    statistics only.

 2. Having only a few satellites the mcc orbits are included in the combination 
    for statistics only.  The grg orbits are introduced for the first time
    starting 02-Jan-2011 (GPS Week 1617) but only for statistics initially.

 3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
    BKG, ESA, and CODE referred their GLONASS orbit products to the following
    satellite antenna offset (SAO) values (expressed in the spacecraft body
    frame):
    
      X/Y/Z =  0.000/0.000/0.000 meter for GLONASS and
      X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
    
    Starting 5-Nov-2006 (GPS Week 1400, day 0; MJD 54044) the absolute antenna
    model was introduced (IGSMAIL #5438). The antenna phase center offsets and
    phase center variations are given in the file:
        ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.atx
    

 4. The satellite clock values in the combined orbit files are taken from the
    broadcast files. The following gps/glonass time offsets derived from the
    bkg summary files were added to the broadcast clocks.
    
               Day | applied clock offset
               ----+---------------------
                0  |    372.7 ns
                1  |    357.5 ns
                2  |    375.3 ns
                3  |    357.4 ns
                4  |    429.6 ns
                5  |    349.1 ns
                6  |    409.6 ns

 5. The following orbit solutions were excluded from the combination
    because they were biasing the weighted average (generally indicated
    by long arc RMS).
    
               Day | Centre | PRN list
               ----+--------+---------------
                4  |  IAC   | ALL (high Transformation - See Table 2)
                5  |  IAC   | ALL (high Transformation - See Table 2)

    
         
ORBIT COMBINATION AND EVALUATION STATISTICS:                                    
--------------------------------------------                                    
      
Table 1 summarizes all statistics for the week. It contains means and standard 
        deviations over the week of satellite ephemeris  and  clock correction
        transformation parameters for each centre (Tables 1.1631, 1a.1631).
        
Table 2 contains the complete  ephemeris  and  clock correction transformation
        parameters (includes both the apriori and a posteriori values) for each
        centre and each day (Tables 2.1631.0-6)                                                                                
    
Table 3 contains two types of daily  RMS  for each satellite and centre, along
        with the computed  satellite position sigmas  for the  combined orbits 
        (tables 3.1631.0-6). 
        The first type of satellite RMS is based on orbit combination and  the
        second RMS type is a result of the 7-day arc evaluation of each centre
        ephemerides.
                                                                               
   
      
      
Table 1: Week 1631 summary.                      (Apr 10, 2011 - Apr 16, 2011)

Table 1.1631.a     GPS week : 1631   MJD: 55661.0-55667.0

         Mean and standard deviations of transformation parameters to the 
         combined IGL orbit.
         WRMS - orbit RMS weighted by the SP3 header accuracy codes.
         STA  - Mean number of stations in the daily solutions.
   
CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg  150|    1     1     0    -3    34   -28  -.22   50   44 |       0     594   3056   3293
        |    3     3     3    38    58    29   .14           |       0     509
cod  246|    0     0     4    92   -20     4  -.14   28   28 |     ---     ---    ---    ---
        |    1     1     6    34    29    54   .06           |     ---     ---
esx  139|    0     2     3   -24   -26   -17   .41   20   20 |   24337     915   5297   9128
        |    1     1     1    32    23    42   .05           |   30376    3660
gfz  194|    0    -1     1   -32     6    31  -.20   23   21 |  203608    1093   5289   8935
        |    1     0     4    47    36    35   .02           |   29434    2854
grg  135|    0    -3    -3    90    28    73   .11   48   47 |     ---     ---    ---    ---
        |    2     3     4    25    64    54   .08           |     ---     ---
iac  n/a|    1    -1   -28     4    36    82  -.14   52   52 |  379239     266   5302   9359
        |    2     1    14    29    22   127   .12           |   30571    1334
mcc  n/a|    6    -3    62   -23    -2   629   .16  195  195 |     ---     ---    ---    ---
        |    8    11     7    57    64   303   .32           |     ---     ---


Table 1.1631.b     GPS week : 1631   MJD: 55661.0-55667.0   

         Satellite position sigmas for the combined orbits
         (coded in the IGS SP3 orbit files).
         "E" flags eclipsing satellites.
         Units: mm.

              Day of GPS week
 PRN  |    0    1    2    3    4    5    6 |  Remarks
------+------------------------------------+------------------------------------------
 R01  |   14   12   12   12   12   10   11 |
 R02  |   11   10   10   19   17   20   14 |
 R03  |   16   16   19   16   15   24   10 |
 R04  |  249  279  337  324    0    0  280 |
 R05  |   20   11   15   12   15    9   14 |
 R06  |   21   12   12   14   16   12   12 |
 R07  |   14   14   18   14   13   11   13 |
 R08  |    9   12   14   18   14    8   15 |
 R09  |   15   15   16   14   19   17   12 |
 R10  |   16   12   15   15   17   16   11 |
 R11  |   24   28   24   21   19   25   20 |
 R12  |   16   16   23   14   11   11   13 |
 R13  |   18   17   20   21   15   12   12 |
 R15  |   17   18   16   18   11   24   17 |
 R16  |   20   16   16   19   15   13   15 |
 R17  |   21   21   21   23   16   10   25 |
 R18  |   14   14   16   10    9   22   15 |
 R19  |   12   11   14   16   11    9   16 |
 R20  |   17   16   24   20   17   19   18 |
 R21  |   15   18   14   10   10   12   13 |
 R22  |   12   18   16   12   12   14   16 |
 R23  |    9   12   20   11   12   15   10 |
 R24  |   13   27   10   14    9    7   11 |


Table 1.1631.c     GPS week : 1631   MJD: 55661.0-55667.0   

         Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
         Mean and standard deviations of the transformation parameters for the
         whole gpsweek.

CEN WEEK DAY |   DX    DY    DZ     RX      RY      RZ   SCL   RMS   WRMS |    TOFT   TDRFT
             |  [mm]  [mm]  [mm]  [uas]   [uas]   [uas] [ppb]  [mm]  [mm] |    [ps]  [ps/d]
-------------+------------------------------------------------------------+----------------
brd 1631 0   |  114    48   295   -1497    -157  -13920  89.5  1646  1646 |  372677       0
brd 1631 1   |  -33   -51   230      29   -2599  -11550  88.6  2053  2053 |  357525       0
brd 1631 2   |   36  -144    90    1892   -1409  -12880  87.4  1750  1750 |  375297       0
brd 1631 3   |  -81   -69   171     -67   -2590   -7372  85.7  1514  1514 |  357409       0
brd 1631 4   |  -27    23   120   -1696   -1571   -4855  87.2  1785  1785 |  429595       0
brd 1631 5   |  -89    13   134    -666   -2386   -3938  88.8  1641  1641 |  349131       0
brd 1631 6   |  -15    -6   182    -782   -1032   -4652  87.7  1679  1679 |  409638       0
-------------+------------------------------------------------------------+----------------
brd 1631 mean|  -13   -26   174    -398   -1677   -8452  87.8  1724  1724 |  378753       0
brd 1631 sdev|   70    66    70    1200     912    4243   1.2   169   169 |   29920       0



Table 2: Daily transformation of each centre to the combined IGL orbit and
         clocks for each day of the week. The transformation displayed is the
         sum of a priori and estimated transformations.
         WRMS - RMS weighted by the centres SP3 header accuracy codes.
         STA  - Number of stations in the daily solutions.
   
Table 2.1631.0  GPS week: 1631   Day: 0   MJD: 55661                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg  150|   -2    -2    -6    48    -5   -58  -.19   48   41 |       0     649   3401   3656
cod  246|    0     0     9   101     4   -35  -.12   30   33 |     ---     ---    ---    ---
esx  139|   -1     1     4    16     6    20   .46   24   24 |   12429    4796   4977   9512
gfz  194|    1    -1     1  -112   -31    79  -.22   25   25 |  199790    3463   4982   8959
grg  135|    4    -2    -6    65   126    -7   .06   46   46 |     ---     ---    ---    ---
iac  n/a|    1     0   -16   -23    51   -45  -.25   39   39 |  372860    1379   4989   9526
mcc  n/a|   -1     1    67   -20   -97   453  -.15  171  171 |     ---     ---    ---    ---

Table 2.1631.1  GPS week: 1631   Day: 1   MJD: 55662                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg  150|   -3    -2     1     0    29     0  -.09   40   33 |       0    1024   3040   3258
cod  246|    0     2     6    50   -75    45  -.07   31   31 |     ---     ---    ---    ---
esx  139|   -1     6     1    11   -26    32   .46   26   26 |    9656    1820   7004   9815
gfz  194|    2    -2    -3   -32    18    32  -.18   24   18 |  183761    1500   7006   9712
grg  135|    0     0     1   115   -42    97   .07   42   37 |     ---     ---    ---    ---
iac  n/a|   -3    -4    -6    23    33  -101  -.15   46   46 |  357988    -523   7002  10188
mcc  n/a|    1   -18    69  -102    49   464  -.16  154  154 |     ---     ---    ---    ---

Table 2.1631.2  GPS week: 1631   Day: 2   MJD: 55663                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg  150|    0     0     2    26    46   -79  -.11   56   50 |       0    -203   3350   3565
cod  246|   -2     0    13    60   -25    -9  -.13   30   33 |     ---     ---    ---    ---
esx  139|    1     0     3   -46   -30   -50   .42   22   22 |   25097   -5600   4586  10208
gfz  194|    0     0     6     5    12    22  -.24   27   27 |  203714   -2710   4583  10514
grg  135|    1    -4     4    86    -4   138   .10   54   53 |     ---     ---    ---    ---
iac  n/a|    0    -3   -38    28     6   227  -.17   48   48 |  378115   -2103   4591  10318
mcc  n/a|    2   -11    63    66    56   511   .60  135  135 |     ---     ---    ---    ---

Table 2.1631.3  GPS week: 1631   Day: 3   MJD: 55664                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg  150|    6     6     5   -70   152   -14  -.32   58   49 |       0     669   2802   2972
cod  246|   -1    -2     4    82   -42   -14  -.09   28   29 |     ---     ---    ---    ---
esx  139|   -1     0     4   -26   -46   -85   .40   19   19 |   -2092    2364   5035   7406
gfz  194|    1     0     7     5    42    79  -.19   25   24 |  182119    2254   5010   7022
grg  135|   -3    -9    -3   114    30    29   .25   53   53 |     ---     ---    ---    ---
iac  n/a|    2    -2   -43   -35    27   118  -.21   50   50 |  355953    1409   5048   7778
mcc  n/a|   -4    -5    45   -62    72   554   .00  169  169 |     ---     ---    ---    ---

Table 2.1631.4  GPS week: 1631   Day: 4   MJD: 55665                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg  150|    4     2     2   -19   -24   -29  -.48   43   42 |       0    1313   3168   3424
cod  246|    1    -2     0    89    -8   105  -.15   25   26 |     ---     ---    ---    ---
esx  139|   -1     1     1   -74   -43   -43   .36   15   15 |   75652   -1891   5188  10326
gfz  194|    0    -1    -2    10    54     0  -.17   20   20 |  255223   -1320   5165   9503
grg  135|    0    -3    -7   110   -45   120   .04   46   44 |     ---     ---    ---    ---
iac  n/a|    4    -1   -32    39    64   218  -.17   54   54 |  430733    -444   5179  10190
mcc  n/a|   13   -11    62   -29   -55   623  -.01  252  252 |     ---     ---    ---    ---

Table 2.1631.5  GPS week: 1631   Day: 5   MJD: 55666                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg  150|    3     6     1   -23    43    -9  -.20   56   44 |       0     134   2590   2849
cod  246|    0     1    -2   111    -5   -55  -.27   26   24 |     ---     ---    ---    ---
esx  139|    1     0     2   -12     5     3   .35   16   16 |   -5573     549   4347   8506
gfz  194|   -2    -1     0   -18   -42     0  -.18   21   16 |  171669    -840   4349   8596
grg  135|    0    -1    -8    49    50    34   .10   53   51 |     ---     ---    ---    ---
iac  n/a|    2     0   -43   -16    57   132  -.16   58   58 |  348529     842   4340   9043
mcc  n/a|   12     5    63    32   -35   494   .30  303  303 |     ---     ---    ---    ---

Table 2.1631.6  GPS week: 1631   Day: 6   MJD: 55667                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
bkg  150|    3     1    -1    13     1   -11  -.15   46   46 |       0     572   3044   3331
cod  246|   -2     0     0   154     8     0  -.16   23   23 |     ---     ---    ---    ---
esx  139|    0     3     4   -37   -49    -1   .42   19   19 |   55192    4372   5947   8124
gfz  194|    0    -2     0   -83    -8     5  -.19   18   16 |  228982    5304   5934   8244
grg  135|    0     0    -4    90    85    98   .18   46   46 |     ---     ---    ---    ---
iac  n/a|    1    -1   -18    13    13    27   .12   68   68 |  410496    1302   5968   8473
mcc  n/a|   19    13    63   -48    -5  1305   .56  184  184 |     ---     ---    ---    ---

       
       
Table 3: Daily fit for each satellite and each centre resulting from weighted
         average combination and from long arc orbit dynamics (7-day). The
         first IGL column gives resulting satellite accuracy measures found in
         SP3 header. The last IGL column gives the RMS fit of the IGL orbit
         when processed through the 7-day arc evaluation.

         "E"    stands for eclipsing satellites (earth).
         "M"    stands for eclipsing satellites (moon).
         "X"    stands for excluded from the statistics but included in IGL orbit.
         "T"    stands for Total long arc orbit RMS for all satellites.
         "NE"   stands for long arc orbit RMS for Non-Eclipsing satellites only.
         "MEDI" stands for median of the centre's satellite RMS.
         "MD"
         Units: mm.

Table 3.1631.0  GPS week: 1631   Day: 0   MJD: 55661                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  mcc  IGL |   bkg  cod  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 2399   60   21   14   14   29   26  ---   13 |    94   45   53   54   52   58  ---    54
 R02  |  854   24   26   23   15   30   16  ---   10 |    34   47   34   39   58   47  ---    37
 R03E | 1291   30   17   22   24  ---   61  ---   16 |    44   21   37   35  ---   46  ---    26
XR04  | 7412  ---  218  ---  ---  ---  282  ---  248 |   ---  233  ---  ---  ---  367  ---   245
 R05  | 1101   34   50   36   42   44   21   93   19 |    53   71   44   50   45   45   79    45
 R06  | 1038   68   48   42   21   49   23  ---   20 |    84   67   50   43   71   50  ---    46
 R07  | 2070   38   31   28   15   44   28  ---   13 |    46   58   45   48   58   55  ---    46
 R08  | 2282   23   11   16   16   57   25  318    9 |    46   62   67   56   67   57   39    57
 R09E |  918   40   17   24   26   30   42  ---   14 |    54   25   30   38   38   30  ---    25
 R10E | 1083   62   23   16   21   38   41  ---   15 |    85   37   48   39   37   47  ---    42
 R11E |  843   70   47   26   36   65   66  111   23 |    60   30   50   63   71   48   34    40
 R12E |  955   39   28   22   28   48   45  ---   15 |    52   31   36   35   33   45  ---    28
 R13E | 1626   40   19   19   31   50   67  ---   18 |    31   25   38   41   57   50  ---    29
 R15E | 1273   54   12   19   34   36   46  104   16 |    49   32   38   36   57   30   23    27
 R16E | 1141   74   19   35   32   38   42  ---   20 |    45   34   61   68   57   37  ---    46
 R17  | 1109   76   41   31   27   41   47  ---   21 |    53   28   42   45   35   47  ---    24
 R18  | 3989   35   19   24   22   42   43  150   14 |    42   40   28   41   46   29   99    27
 R19  |  706   34   25   14   18   41   28  ---   11 |    53   52   39   42   40   55  ---    43
 R20  | 2056   64   37   14   24   51   33  ---   17 |    60   26   24   38   38   44  ---    25
 R21  | 1144   33   50   19   19   37   15  ---   15 |    51   45   43   42   41   46  ---    34
 R22  | 1857   20   25   21   20   61   30  ---   11 |    46   54   35   34   35   30  ---    33
 R23  | 1299   24   18   14   20   57   17  145    9 |    36   31   26   19   31   23   52    19
 R24  | 1462   32   33   20   19   53   22  ---   12 |   135  131  124  127  132  120  ---   124
------+----------------------------------------------+------------------------------------------
 RMS  | 1646   48   30   24   25   46   39  171      |T   56   53   45   46   52   61   54    48
 WRMS | 1646   41   33   24   25   46   39  171      |NE  59   66   46   48   53   71   67    57
 MEDI | 1273   38   25   21   21   44   33  111      |MD  51   40   39   41   46   47   39    37

Table 3.1631.1  GPS week: 1631   Day: 1   MJD: 55662                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  mcc  IGL |   bkg  cod  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1727   27   22   14   18   29   37  ---   11 |    55   39   47   38   33   54  ---    41
 R02  | 1121   28   14   18   12   46   22  ---    9 |    41   36   33   41   42   49  ---    36
 R03E | 1344   44   17   20   32  ---   48  ---   16 |    39   29   44   31  ---   45  ---    29
XR04  | 8733  ---  226  ---  ---  ---  344  ---  279 |   ---  382  ---  ---  ---  205  ---   244
 R05  | 1375   27   23   21   13   49   28   95   11 |    48   54   57   55   46   41   53    48
 R06  | 1952   19   31   28   15   51   26  ---   12 |    38   50   45   35   34   43  ---    36
 R07  | 4351   18   40   34   18   51   26  ---   14 |    32   58   32   51   46   51  ---    40
 R08  | 1578   24   25   11   20   35   42  256   12 |    30   52   38   42   44   55   56    37
 R09E | 1164   18   21   26   20   36   61  ---   15 |    22   18   28   37   34   41  ---    22
 R10E | 1493   19   21   19   16   32   43  ---   11 |    26   23   25   21   31   40  ---    17
 R11E | 2264   87   49   44   39   33   60  137   28 |    75   49   82   90   54   58   34    64
 R12E |  738   30   17   23   25   30   64  ---   16 |    28   25   43   39   25   50  ---    27
 R13E | 2006   48   25   21   21   36   49  ---   16 |    31   50   52   46   26   47  ---    38
 R15E | 3015   34   17   27   32   31   65  114   17 |    31   45   50   40   48   38   26    35
 R16E | 1361   20   22   18   22   41   69  ---   16 |    36   25   29   24   45   43  ---    16
 R17  | 1237   53   38   22   39   44   62  ---   21 |    38   18   36   53   40   38  ---    21
 R18  | 4951   40   25   27   23   54   22  108   14 |    47   30   31   23   42   38   70    20
 R19  |  467   30   15   13   15   43   40  ---   11 |    36   43   47   46   52   51  ---    39
 R20  | 2034   42   35   23   24   53   33  ---   15 |    20   29   33   19   45   49  ---    21
 R21  |  866   27   46   34   26   22   43  ---   17 |    26   27   50   43   29   23  ---    24
 R22  |  917   26   52   39   25   45   21  ---   17 |    17   32   59   50   36   31  ---    30
 R23  | 1223   26   23   25   20   36   29  154   12 |    17   21   28   31   28   21   20    16
 R24  | 1333   92   52   33   29   55   57  ---   27 |   127  193  180  189  186  156  ---   168
------+----------------------------------------------+------------------------------------------
 RMS  | 2052   40   31   26   24   42   46  154      |T   39   57   48   47   46   55   43    46
 WRMS | 2052   33   31   26   18   37   46  154      |NE  40   70   51   51   50   60   49    54
 MEDI | 1375   27   25   23   21   41   43  114      |MD  32   36   43   40   42   45   34    35

Table 3.1631.2  GPS week: 1631   Day: 2   MJD: 55663                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  mcc  IGL |   bkg  cod  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1544   20   13   18   30   41   34  ---   11 |    49   35   44   54   46   54  ---    43
 R02  | 1058   25   21   10   10   52   38  ---   10 |    55   40   54   52   68   61  ---    49
 R03E | 2140   64   32   19   29  ---   60  ---   18 |    90   39   44   42  ---   51  ---    38
XR04  |12210  ---  252  ---  ---  ---  448  ---  336 |   ---  474  ---  ---  ---  192  ---   358
 R05  | 1549   36   38   21   28   57   27  129   14 |    72   65   42   41   63   40  114    46
 R06  | 1735   26   29   11   19   46   36  ---   11 |    58   65   56   44   39   45  ---    52
 R07  | 2230   28   44   15   49   53   29  ---   18 |    44   54   32   60   48   64  ---    38
 R08  | 1249   41   34   12   28   65   20  166   13 |    37   46   36   46   74   50   55    36
 R09E | 1769   27   24   17   26   51   62  ---   15 |    44   24   42   44   52   37  ---    30
 R10E | 1239   43   17   14   20   51   58  ---   14 |    59   28   34   36   46   38  ---    27
 R11E | 1764   84   41   24   37   48   71  129   23 |    88   47   64   62   60   44   60    51
 R12E |  683   96   32   17   38   43   61  ---   22 |   116   26   51   34   31   40  ---    35
 R13E | 1273   73   22   21   20  ---   74  ---   20 |    65   24   36   41  ---   51  ---    30
 R15E | 2917   56   18   25   28   47   46  109   16 |    59   27   38   37   49   45   34    28
 R16E | 1542   42   25   25   26   45   54  ---   16 |    46   27   47   45   59   48  ---    32
 R17  | 1114   54   24   26   24   69   88  ---   21 |    57   26   53   47   46   32  ---    34
 R18  | 3737   68   27   30   19   51   19  107   16 |    66   31   28   30   46   21  144    17
 R19  |  701   42   32   22   22   64   23  ---   13 |    79   69   43   52   62   44  ---    50
 R20  | 1445  105   34   29   36   64   50  ---   24 |    67   33   43   33   53   24  ---    18
 R21  | 1157   46   29   25   18   73   31  ---   14 |    67   38   37   40   57   43  ---    37
 R22  | 1497   58   33   16   32   59   21  ---   15 |    75   47   30   25   49   18  ---    27
 R23  | 2050   54   47   44   13   29   37  160   20 |    52   38   65   27   34   25   58    29
 R24  | 1018   19   22   17   13   61   25  ---    9 |    94   88   77   82  103   87  ---    82
------+----------------------------------------------+------------------------------------------
 RMS  | 1750   56   30   22   27   54   48  135      |T   65   60   45   44   54   50   77    51
 WRMS | 1750   50   33   22   27   53   48  135      |NE  62   76   45   45   56   53   92    61
 MEDI | 1542   43   29   19   26   51   38  129      |MD  59   38   43   42   49   44   58    36

Table 3.1631.3  GPS week: 1631   Day: 3   MJD: 55664                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  mcc  IGL |   bkg  cod  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1645   38   27   18   15   38   30  ---   12 |    66   33   51   50   51   67  ---    46
 R02  |  941  104   33   14   14   34   24  ---   18 |   105   48   44   39   57   48  ---    39
 R03E | 2402   62   28   15   15  ---   60  ---   16 |    65   27   36   38  ---   54  ---    31
XR04  |17116  ---  128  ---  ---  ---  537  ---  323 |   ---  524  ---  ---  ---  373  ---   488
 R05  | 1028   22   33   20   18   63   24  ---   12 |    39   56   27   44   63   38  ---    36
 R06  | 1249   44   26   12   24   54   43  ---   13 |    81   69   55   67   41   39  ---    58
 R07  | 2150   48   23   20   27   57   32  ---   13 |    68   63   66   61   63   58  ---    59
 R08  | 1893   52   30   27   44   50   38   67   18 |    67   55   46   37   46   59  126    41
 R09E | 2016   33   17   19   20   49   62  ---   14 |    50   27   42   36   53   37  ---    29
 R10E |  912   52   17   18   17   42   64  ---   15 |    52   35   42   35   48   38  ---    30
 R11E |  919   59   38   25   30   69   81  164   21 |    92   52   79   80   66   52   35    66
 R12E |  795   42   23   14   18   34   53  ---   13 |    55   26   32   32   32   39  ---    25
 R13E |  911   92   34   23   31   67   61  ---   21 |    88   38   64   62   55   38  ---    47
 R15E | 1816   46   26   19   41   42   64  133   18 |    47   24   41   37   53   43   42    26
 R16E | 1433   80   25   16   31   45   66  ---   19 |    89   24   42   41   54   44  ---    32
 R17  |  998   51   41   18   35   87   96  ---   22 |    43   27   24   35   57   62  ---    15
 R18  | 1635   36   22   15   14   37   23  290   10 |    45   35   30   27   38   20  106    25
 R19  |  835   85   23   15   15   52   25  ---   15 |   107   53   41   55   45   34  ---    48
 R20  | 2736   96   18   20   32   54   50  ---   19 |    55   32   44   47   46   23  ---    28
 R21  |  784   36   18   13   16   53   21  ---    9 |    43   49   61   72   42   42  ---    53
 R22  | 1051   21   33   25   13   35   22  ---   12 |    57   59   39   52   51   28  ---    44
 R23  | 1718   22   29   19   18   60   21   99   11 |    35   40   22   24   47   24   59    20
 R24  | 1059   54   24   22   15   49   34  ---   13 |   112   98   89   91  101   88  ---    89
------+----------------------------------------------+------------------------------------------
 RMS  | 1513   58   28   19   25   53   50  169      |T   66   64   46   48   52   58   73    59
 WRMS | 1513   49   29   19   24   53   50  169      |NE  65   82   45   50   53   66   97    72
 MEDI | 1249   48   26   18   18   50   43  133      |MD  57   40   42   41   51   42   59    39

Table 3.1631.4  GPS week: 1631   Day: 4   MJD: 55665                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  mcc  IGL |   bkg  cod  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1281   38   16    6   22   31   45  ---   11 |    63   41   47   39   47   54  ---    41
 R02  | 1014   53   30   21   20   31   42  ---   16 |    65   39   34   52   47   37  ---    36
 R03E | 2069   62   20   13   14  ---   49  ---   15 |    61   18   37   35  ---   40  ---    29
XR04  |21363  ---    8  ---  ---  ---  ---  ---    0 |   ---  829  ---  ---  ---  ---  ---   796
 R05  |  988   38   36   11   19   41   28  423   14 |    57   53   52   41   56   44  184    44
 R06  | 2067   35   36   22   15   53   25  ---   15 |    44   50   27   30   49   35  ---    27
 R07  | 1739   34   26   13   22   41   45  ---   13 |    68   51   62   72   44   36  ---    60
 R08  | 2857   19   16   22   30   53   30   41   13 |    42   50   51   43   53   36   55    44
 R09E | 1065   77   22   16   20   40   64  ---   18 |    82   23   42   42   41   45  ---    36
 R10E |  902   54   23   25   19   42   63  ---   16 |    61   24   50   41   44   48  ---    36
 R11E | 2338   47   42   18   30   68   73  147   18 |    69   27   55   61   61   44   20    43
 R12E |  899   26   23   15    9   30   65  ---   10 |    31   33   48   37   31   45  ---    35
 R13E | 1278   54   18   19   14   42   53  ---   14 |    64   40   41   40   50   42  ---    40
 R15E | 3738   31   18    8   19   49   58  146   10 |    55   25   31   46   47   42   29    30
 R16E | 1361   44   28   10   27   44   76  ---   14 |    72   24   45   52   52   51  ---    39
 R17  | 1198   46   31   14   24   26  132  ---   15 |    51   34   45   43   51   78  ---    36
 R18  | 2025   18   20   13    9   40   18  380    8 |    36   27   30   28   25   22   51    25
 R19  | 1291   22   24   16   14   44   28  ---   10 |    48   53   31   43   48   45  ---    40
 R20  | 2658   68   19    5   28   46   44  ---   17 |    29   19   26   31   21   37  ---    20
 R21  | 1645   30   22   12   10   47   38  ---   10 |    57   43   48   44   52   42  ---    44
 R22  |  853   22   24   10   26   68   24  ---   12 |    60   47   55   40   44   39  ---    47
 R23  | 1419   37   23   18   12   50   26  119   12 |    58   39   24   32   34   28   34    28
 R24  | 1147   30   13    9   14   53   35  ---    9 |    79   82   86   92   85   82  ---    84
------+----------------------------------------------+------------------------------------------
 RMS  | 1785   43   25   15   20   46   54  252      |T   56   72   43   44   46   44   62    72
 WRMS | 1785   42   26   15   20   44   54  252      |NE  54   97   44   45   46   43   81    91
 MEDI | 1361   37   23   13   19   44   44  146      |MD  58   39   45   41   47   42   34    39

Table 3.1631.5  GPS week: 1631   Day: 5   MJD: 55666                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  mcc  IGL |   bkg  cod  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  967   25   20   13   11   58   45  ---    9 |    31   36   51   44   39   44  ---    41
 R02  | 1350   35   35   25   44   39   34  ---   20 |    37   35   25   39   38   24  ---    22
 R03E | 2560  114   21   22   15  ---   59  ---   23 |   113   26   37   41  ---   36  ---    36
XR04  | ----  ---  ---  ---  ---  ---  ---  ---    0 |   ---  ---  ---  ---  ---  129  ---     0
 R05  | 1122   23   21    9   12   42   31  474    8 |    37   44   38   38   39   33  146    37
 R06  | 3440   35   22    9   25   30   18  ---   12 |    29   39   37   35   54   40  ---    32
 R07  | 1899   29   13   14   20   57   28  ---   10 |    28   35   34   46   50   32  ---    34
 R08  | 2620   25   10    9   17   38   30   47    8 |    51   37   34   32   34   46   56    33
 R09E |  568   52   35   12   27   47   66  ---   16 |    47   23   41   57   48   49  ---    35
 R10E | 1128   59   24   15   25   37   69  ---   16 |    67   21   37   43   33   47  ---    33
 R11E | 1541   84   44   30   32   58   73  150   24 |    89   38   78   58   52   52   25    58
 R12E |  993   41   19   14   13   39   78  ---   11 |    34   26   35   31   41   43  ---    26
 R13E |  942   37   20   15   17   43   66  ---   11 |    49   25   39   36   41   38  ---    31
 R15E | 1571  112   29   20   18   43   67  151   24 |   112   25   44   42   46   39   23    35
 R16E | 1190   46   24   11   16   37   68  ---   12 |    50   19   35   38   42   53  ---    27
 R17  | 1959   24   24    9   17   57  145  ---   10 |    46   28   36   44   65   74  ---    33
 R18  | 1692   91   43   17   15   49   35  498   22 |    95   30   41   34   48   32   84    31
 R19  | 1350   25   14   11   13   69   21  ---    8 |    66   44   44   44   36   40  ---    44
 R20  | 1811   65   41   23   17   89   66  ---   19 |    45   16   50   27   37   40  ---    29
 R21  | 1419   23   22   17   21   48   28  ---   11 |    44   27   21   33   29   26  ---    22
 R22  |  630   23   32   23   18   78   35  ---   14 |    51   46   56   50   34   43  ---    48
 R23  | 1272   66   11   12   18   45   27  174   14 |    36   31   40   51   30   29   23    33
 R24  |  866   28   10    5   12   67   23  ---    7 |    77   81   74   79   82   77  ---    76
------+----------------------------------------------+------------------------------------------
 RMS  | 1640   56   26   16   21   53   58  303      |T   56   33   42   42   43   46   59    36
 WRMS | 1640   44   24   16   16   51   58  303      |NE  48   37   41   42   43   47   77    36
 MEDI | 1350   35   22   14   17   47   35  151      |MD  47   30   38   41   41   40   25    33

Table 3.1631.6  GPS week: 1631   Day: 6   MJD: 55667                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  mcc  IGL |   bkg  cod  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1629   19   19   12   15   41   65  ---   11 |    65   54   57   58   50   69  ---    55
 R02  | 1476   26   15   20   24   61   78  ---   13 |    62   60   49   67   49   57  ---    56
 R03E | 2462   30   14   16   12  ---   43  ---    9 |    64   25   26   37  ---   47  ---    30
XR04  |18399  ---  129  ---  ---  ---  600  ---  279 |   ---  303  ---  ---  ---  154  ---   281
 R05  | 1161   45   29   23   11   28   48  ---   13 |    40   63   43   44   47   48  ---    43
 R06  | 3159   42   17   10   14   39   62  ---   12 |    53   64   44   53   46   60  ---    49
 R07  | 1878   27   19   26   14   70   66  ---   13 |    53   55   39   47   38   67  ---    45
 R08  |  694   31   18   16   23   33   84   81   14 |    46   50   53   51   44   49   64    46
 R09E |  658   49   17   23   12   32   40  ---   12 |    38   31   48   39   47   47  ---    34
 R10E |  999   40   13   13   13   31   48  ---   10 |    62   35   32   46   46   43  ---    39
 R11E | 1407   81   44   20   22   40   51  127   20 |    63   41   77   76   55   63   20    61
 R12E |  959   48   11   24   21   53   44  ---   13 |    60   30   32   44   50   47  ---    36
 R13E | 1267   29   22   26   14   53   41  ---   12 |    57   37   61   48   45   45  ---    45
 R15E | 1717   59   21   16   33   37   55  222   16 |    60   28   37   44   39   46   27    30
 R16E |  581   61   22   21   19   46   55  ---   15 |    57   23   42   29   43   56  ---    27
 R17  | 1839   64   37   17   31   54  149  ---   24 |    37   38   19   37   41   86  ---    19
 R18  | 1690   47   26   19   15   27   78  ---   15 |    52   39   31   37   35   24  ---    28
 R19  | 1236   47   26   27   12   52   75  ---   15 |    47   55   35   40   48   76  ---    39
 R20  | 3885   74   35   23   14   51   55  ---   18 |    76   34   35   45   29   56  ---    37
 R21  |  779   19   19   19   17   44   72  ---   12 |    44   45   35   45   37   59  ---    39
 R22  |  497   47   27   17   14   62   84  ---   15 |    68   57   37   40   30   40  ---    43
 R23  |  902   34   13   12    8   41   52  252   10 |    30   39   40   37   21   44   39    33
 R24  | 1421   29   16   12   14   40   55  ---   10 |    79   90   92   84   86  100  ---    86
------+----------------------------------------------+------------------------------------------
 RMS  | 1679   46   23   19   18   46   68  184      |T   55   56   43   47   44   60   37    52
 WRMS | 1679   46   23   19   16   46   68  184      |NE  53   69   43   48   42   65   51    59
 MEDI | 1407   42   19   19   14   41   55  127      |MD  57   41   39   44   45   56   27    39




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