[IGSREPORT-19728] Wk 1632 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Fri May 6 09:04:56 PDT 2011


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1632   (Apr 17, 2011 - Apr 23, 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 2.1632.
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:
                                                                               
 igl1632[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1632 in the SP3 format.
 igl16327.sum      Combination Report for GPS Week 1632.


    
    
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) until 16-Apr-2011
    (GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
    (IGSMAIL #5438). The antenna phase center offsets and phase center variations
    are given in the file:
        ftp://igs.org/igscb/station/general/igs05.atx
    These antenna calibrations are also used in the homogeneously reprocessed IGS
    products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
    Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
    model is updated (IGSMAIL #6255 & #6374) as given in the file:
        ftp://igs.org/igscb/station/general/igs08.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  |    381.5 ns
                1  |    335.9 ns
                2  |    365.0 ns
                3  |    360.6 ns
                4  |    374.2 ns
                5  |    324.3 ns
                6  |    343.7 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
               ----+--------+---------------
                0  |  BKG   | R03 R10 R11
                1  |  BKG   | R09 R11 R13
                2  |  BKG   | R09 R12 R16
                6  |  BKG   | R22

    
         
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 1.1632, 1a.1632).
        
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 2.1632.0-6)                                                                                
    
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 3.1632.0-6). 
        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 1632 summary.                      (Apr 17, 2011 - Apr 23, 2011)

Table 1.1632.a     GPS week : 1632   MJD: 55668.0-55674.0

         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  151|    2     6    10   -99    54   219  -.31   72   57 |       0     882   2793   3009
        |    4     3    12    54    68   102   .10           |       0     843
cod  243|    0     0     0    33   -14   -35  -.21   24   24 |     ---     ---    ---    ---
        |    1     2     3    37    25    33   .04           |     ---     ---
esx  138|    0     0     1    30    38   -22   .38   19   17 |    3659    -563   4746   8364
        |    0     1     2    19    22    31   .05           |   21781    3846
gfz  189|    0     0     0   -50   -32   -11  -.21   22   20 |  181500    -571   4734   8416
        |    1     2     3    49    28    26   .08           |   20230    3339
grg  131|   -1    -3   -15    16    -8    55   .10   53   50 |     ---     ---    ---    ---
        |    2     2    10    37    79    68   .16           |     ---     ---
iac  n/a|   -2     0   -12   -20   -49    11   .03   54   54 |  355654    -667   4741   8685
        |    2     2     6    27    29   195   .08           |   21419     886
mcc  n/a|    0    -2    36    62    55   710  -.06  152  152 |     ---     ---    ---    ---
        |    7    10    17    75    69   281   .32           |     ---     ---


Table 1.1632.b     GPS week : 1632   MJD: 55668.0-55674.0   

         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  |   16   12   13   12   15   14   12 |
 R02  |   14   13   10   13   13   13   14 |
 R03  |   13   14   14   17   11   12   12 |
 R04  |  602  272 1011  327  111  152  113 |
 R05  |   16   18   16   13   16   18   15 |
 R06  |   14   16   17   16   12   14   13 |
 R07  |   13   15   13   12   12   10   12 |
 R08  |   20   16   12   15   14   14   12 |
 R09  |   14   13   13   14   14   15   15 |
 R10  |   20   14   12   12   14   10   13 |
 R11  |   20   23   21   17   16   20   16 |
 R12  |   15   17   14   10   11   12   13 |
 R13  |   14   18   17   12   12   16   14 |
 R15  |   14   17   16   18   14   21   15 |
 R16  |   13   16   16   12   15   16   15 |
 R17  |   20   28   19   20   16   12   13 |
 R18  |   16   17   21   16   17   11   16 |
 R19  |   16   17   17   12   13   13   13 |
 R20  |   15   18   15   24   18   20   25 |
 R21  |   12   20   14   15   18   13   14 |
 R22  |   12   13   15   12   13   12   14 |
 R23  |   14   17   11   13   20   13   11 |
 R24  |   16   22   15   13   13   11   12 |


Table 1.1632.c     GPS week : 1632   MJD: 55668.0-55674.0   

         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 1632 0   |    0    31   243   -3137     -53   -6035  84.8  1829  1829 |  381501       0
brd 1632 1   |    0    94   270   -1480    -832   -8036  86.7  2141  2141 |  335883       0
brd 1632 2   |  -24   -80   195     853    -430  -16100  84.5  2065  2065 |  365016       0
brd 1632 3   |  -56    -8   223    -198   -1396  -19260  83.4  1879  1879 |  360560       0
brd 1632 4   |   13   -64   232    2979    -696  -23310  83.5  2448  2448 |  374193       0
brd 1632 5   |   23   -18   288    -389   -1758  -15960  85.5  2339  2339 |  324312       0
brd 1632 6   |   19    -8   407    -925      75  -12360  86.0  2415  2415 |  343732       0
-------------+------------------------------------------------------------+----------------
brd 1632 mean|   -3    -7   265    -328    -727  -14437  84.9  2159  2159 |  355028       0
brd 1632 sdev|   28    58    69    1911     671    6095   1.3   250   250 |   20960       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 2.1632.0  GPS week: 1632   Day: 0   MJD: 55668                            

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  151|   -2    10    -5   -66    88   156  -.36   74   70 |       0    2469   2956   3060
cod  243|    0     1     2    61   -25     9  -.20   25   22 |     ---     ---    ---    ---
esx  138|    1    -2     3    54    47   -35   .39   19   18 |   28154   -4598   4982   8602
gfz  189|    0     1     0  -148   -16     9  -.35   23   19 |  205317   -2690   4960   8667
grg  131|   -3    -3   -13   -38    34   149   .04   49   49 |     ---     ---    ---    ---
iac  n/a|   -4    -1   -11    -1   -28   -52   .09   61   61 |  383529   -2050   4970   8866
mcc  n/a|   -1     3    14    23    53   858  -.57  201  201 |     ---     ---    ---    ---

Table 2.1632.1  GPS week: 1632   Day: 1   MJD: 55669                            

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  151|    4     1    21   -37   -12   370  -.23   87   61 |       0     827   2668   2802
cod  243|    0    -1     1    52     8   -31  -.23   26   30 |     ---     ---    ---    ---
esx  138|    1     0     2    26    18    10   .35   24   22 |  -19504    2644   4625   8976
gfz  189|   -1    -1    -1   -59    -4     5  -.09   23   18 |  156562    3996   4634   8893
grg  131|    2    -3   -21    20   138     0  -.06   56   53 |     ---     ---    ---    ---
iac  n/a|   -4     0    -8   -41   -21  -319   .07   64   64 |  336717    -281   4659   8872
mcc  n/a|    3   -11    40   182   -50   871   .06  182  182 |     ---     ---    ---    ---

Table 2.1632.2  GPS week: 1632   Day: 2   MJD: 55670                            

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  151|    5    11    16  -134    29   245  -.25  110   57 |       0     420   2173   2300
cod  243|    0     0     1    10    -4   -47  -.16   22   23 |     ---     ---    ---    ---
esx  138|    0    -2     2    50    19   -52   .37   18   16 |   16506    4377   4487   7852
gfz  189|   -1     1    -4   -10   -20   -16  -.24   22   26 |  185885    1239   4469   7995
grg  131|   -2    -2   -29    38   -46    78   .41   52   46 |     ---     ---    ---    ---
iac  n/a|   -1     3   -21    -3   -94   189   .03   69   69 |  366005    -638   4481   8318
mcc  n/a|   -3   -20    52   120   107   960   .23  164  164 |     ---     ---    ---    ---

Table 2.1632.3  GPS week: 1632   Day: 3   MJD: 55671                            

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  151|    6     7    -6   -78   174   340  -.42   63   57 |       0    -239   2989   3297
cod  243|    0    -2     5    40   -56    -7  -.26   22   23 |     ---     ---    ---    ---
esx  138|    0     0    -2     8    61     5   .38   17   16 |   11724   -2944   4395   8232
gfz  189|    1    -2     4   -55   -50   -19  -.13   19   18 |  186726   -1732   4411   8371
grg  131|   -4    -4   -25    77     8    -3   .15   55   48 |     ---     ---    ---    ---
iac  n/a|   -1     1   -19    19   -29   -65  -.04   59   59 |  361846   -1042   4387   8522
mcc  n/a|  -10    -3    56    13    62   815  -.47  150  150 |     ---     ---    ---    ---

Table 2.1632.4  GPS week: 1632   Day: 4   MJD: 55672                            

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  151|   -4     4    23   -74   -29   189  -.22   51   44 |       0     686   2969   3178
cod  243|    0    -2     2    76   -11   -28  -.21   22   23 |     ---     ---    ---    ---
esx  138|    0     2     0     3     8   -36   .47   20   18 |   24245   -5210   5436   8924
gfz  189|    0     0     0   -56    -7     9  -.23   24   22 |  204570   -5098   5426   8765
grg  131|   -2    -7   -16     0   -72   -15   .13   55   55 |     ---     ---    ---    ---
iac  n/a|   -4    -1   -14   -57   -29    12   .14   45   45 |  373975   -1349   5423   9114
mcc  n/a|   12     0    47    77   -18   266   .14  103  103 |     ---     ---    ---    ---

Table 2.1632.5  GPS week: 1632   Day: 5   MJD: 55673                            

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  151|    0     2    10  -103    59   134  -.26   52   48 |       0    1325   3308   3773
cod  243|   -2     3    -6    26    19   -92  -.17   25   25 |     ---     ---    ---    ---
esx  138|    0     1     1    37    45    13   .39   21   18 |  -26092    -881   4770   8421
gfz  189|    3    -3     2    -8   -40    -2  -.21   22   20 |  155978   -2634   4728   8474
grg  131|    2    -2    -5    26   -20    42   .06   53   46 |     ---     ---    ---    ---
iac  n/a|    0    -4    -4   -14   -73    26   .03   36   36 |  324353     310   4753   9022
mcc  n/a|    0     1    28    64   147   341   .13  115  115 |     ---     ---    ---    ---

Table 2.1632.6  GPS week: 1632   Day: 6   MJD: 55674                            

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  151|    4     4    16  -202    74   104  -.46   68   62 |       0     688   2491   2655
cod  243|   -3     0    -1   -35   -30   -53  -.23   27   27 |     ---     ---    ---    ---
esx  138|    0     0     3    29    67   -64   .33   16   14 |   -9419    2667   4529   7545
gfz  189|    0     2    -6   -12   -85   -66  -.20   23   18 |  175463    2918   4516   7750
grg  131|   -2     1     0    -9   -99   139  -.05   52   51 |     ---     ---    ---    ---
iac  n/a|    0     0    -7   -41   -70   290  -.09   40   40 |  343159     377   4518   8086
mcc  n/a|    5    11    15   -47    86   858   .02  149  149 |     ---     ---    ---    ---

       
       
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 3.1632.0  GPS week: 1632   Day: 0   MJD: 55668                            

        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  | 1429   71   18   15   17   58   72  ---   15 |    51   37   40   44   45   69  ---    37
 R02  | 1194   38   24   19   28   57   43  ---   13 |    44   45   36   28   37   31  ---    31
 R03E | 3085  146   18   16   18   65   54  ---   13 |    72   28   42   48   53   45  ---    38
XR04  |15450  ---  308  ---  ---  --- 1176  ---  602 |   ---  560  ---  ---  ---  403  ---   493
 R05  | 1759   36   39   18   31   52   42  265   15 |    40   46   30   29   57   42   45    27
 R06  | 3046   42   28   25   20   36   37  ---   13 |    62   45   25   24   39   30  ---    25
 R07  | 1758   40   17   12   26   59   59  ---   12 |    70   42   34   42   50   61  ---    36
 R08  |  941   83   21   19   50   52   50  105   19 |    54   37   37   42   35   53   38    34
 R09E |  875   44   22   20   17   56   58  ---   13 |    69   21   26   28   32   33  ---    19
 R10E | 1469  127   30   21   32   43   82  ---   20 |    84   39   41   25   44   38  ---    28
 R11E | 2294  140   39   21   25   53   75   99   20 |   138   42   72   68   51   45   35    56
 R12E |  747   81   16   12   19   37   44  ---   14 |    71   20   30   34   34   34  ---    24
 R13E | 1037   43   19   17   19   56   66  ---   13 |    63   51   64   64   72   75  ---    57
 R15E | 2451   71   21   11   17   45   46  149   13 |    88   31   30   26   58   31   35    28
 R16E | 1159   34   19   18   18   39   64  ---   12 |    38   35   49   51   41   60  ---    42
 R17  | 2359   88   31   20   21   51   88  ---   20 |    37   37   27   26   43   57  ---    21
 R18  | 2585   53   22   22   13   45   82  279   16 |    75   58   50   45   26   57   76    47
 R19  | 1298   53   18   28   18   36   68  ---   15 |    87   62   50   59   49   46  ---    54
 R20  | 2940   62   30   16   15   41   54  ---   15 |    67   60   41   41   23   43  ---    43
 R21  | 1098   38   19   13   25   43   53  ---   12 |    83   61   62   58   43   50  ---    58
 R22  |  824   42   19   17    9   49   60  ---   12 |    65   67   59   63   37   67  ---    59
 R23  |  661   58   24   14   16   55   62  226   14 |    73   46   45   51   38   59   29    45
 R24  | 1479   62   31   22   24   43   39  ---   15 |    63   53   46   39   48   48  ---    41
------+----------------------------------------------+------------------------------------------
 RMS  | 1829   74   25   19   23   49   61  201      |T   67   66   42   42   43   64   43    58
 WRMS | 1829   70   22   18   19   49   61  201      |NE  62   83   41   42   40   74   47    70
 MEDI | 1469   53   22   18   19   49   59  149      |MD  67   45   41   42   43   48   35    38

Table 3.1632.1  GPS week: 1632   Day: 1   MJD: 55669                            

        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  | 1074   38   15   12   13   49   58  ---   11 |    54   29   46   41   37   57  ---    37
 R02  |  765   61   17   14   20   38   36  ---   12 |    32   28   38   38   43   41  ---    31
 R03E | 4644   42   14   13   32   60   61  ---   14 |    47   23   24   31   40   38  ---    21
XR04  |13149  ---  139  ---  ---  ---  535  ---  271 |   ---  382  ---  ---  ---  504  ---   295
 R05  | 1938   60   30   25   36   92   57  240   18 |    56   38   49   51   49   38   25    38
 R06  | 2710   46   38   18   28   39   27  ---   15 |    45   33   33   33   39   30  ---    23
 R07  | 1856   36   23   26   32   52   40  ---   14 |    50   29   26   22   38   46  ---    21
 R08  | 1759   74   22   12   20   29   56   79   15 |    80   30   26   28   27   51   34    22
 R09E |  848  155   12   12   17   45   61  ---   12 |    74   25   32   28   40   46  ---    26
 R10E | 4530   63   14   13   18   41   55  ---   13 |    69   29   41   46   35   62  ---    38
 R11E | 2738  208   32   34   32   53   78  111   22 |   200   40   68   63   53   50   22    49
 R12E | 1094   70   20   23   26   52   60  ---   16 |    57   17   40   35   35   43  ---    24
 R13E | 1520  132   17   19   19   48   85  ---   17 |   102  105  114  128  101  118  ---   110
 R15E | 2074   96   18   13   16   34   52  128   16 |    76   29   24   25   38   28   19    21
 R16E |  823   67   11   17   21   55   73  ---   15 |    78   30   36   36   52   41  ---    31
 R17  | 2066  116   52   44   27   77   90  ---   28 |    71   31   56   52   44   55  ---    32
 R18  | 3133   40   12   20   17   69   97  185   16 |    84   43   53   41   40   56   37    42
 R19  |  947   81    8   21   13   51   73  ---   16 |    92   36   32   36   50   54  ---    36
 R20  | 1809   83   31   27   19   53   43  ---   17 |    48   28   40   32   37   19  ---    27
 R21  | 1213   41   46   42   22   64   52  ---   20 |    31   38   59   54   59   41  ---    35
 R22  | 1334   29   13   24   15   58   63  ---   12 |    64   46   44   48   35   47  ---    44
 R23  |  828   29   26   34   19   59   80  268   17 |    35   36   51   46   54   35   24    34
 R24  |  655   85   43   29   30   64   66  ---   22 |    79   49   32   34   39   30  ---    24
------+----------------------------------------------+------------------------------------------
 RMS  | 2140   87   26   24   23   56   64  182      |T   69   51   43   43   44   66   26    46
 WRMS | 2140   61   30   22   18   53   64  182      |NE  58   58   41   39   42   73   30    49
 MEDI | 1759   63   20   20   20   52   61  128      |MD  64   31   40   36   40   46   24    32

Table 3.1632.2  GPS week: 1632   Day: 2   MJD: 55670                            

        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  |  743   25   25   14   21   37   67  ---   13 |    60   38   43   45   36   55  ---    38
 R02  |  969   44   13   10   16   33   39  ---   10 |    44   39   51   55   40   51  ---    45
 R03E | 4508   46   14   17   27   43   59  ---   13 |    66   38   46   61   64   54  ---    46
XR04  |11496  ---  457  ---  ---  --- 2234  --- 1011 |   ---  299  ---  ---  --- 9999  ---   274
 R05  | 2813   53   32   18   19   65   65  196   15 |    47   47   31   39   52   40   29    31
 R06  | 1520   50   26   17   38   48   67  ---   17 |    52   37   28   44   33   59  ---    31
 R07  | 1033   37   23    8   28   56   41  ---   12 |    34   24   29   35   45   34  ---    21
 R08  | 2146   33   20   15   18   30   54   40   11 |    45   34   24   22   37   42   31    22
 R09E |  589  392   19   11   17   45   60  ---   12 |   229   22   29   41   20   33  ---    27
 R10E | 5698   44   11   11   18   25   59  ---   11 |    53   29   25   32   34   67  ---    27
 R11E | 1900   76   41   34   25   55   57  130   20 |   127   39   63   61   39   51   35    49
 R12E |  857  173   15   14   20   64   70  ---   14 |   141   22   29   31   53   42  ---    22
 R13E | 2341   78   17   14   33   90   55  ---   16 |    91   88  102  109   71   74  ---    93
 R15E | 1144   53   29   15   23   39   69  157   15 |    46   18   47   54   55   32   19    34
 R16E |  685  170   13   12   15   42   96  ---   16 |   121   36   42   41   51   61  ---    36
 R17  | 1473   71   27   24   17   45   88  ---   18 |    84   26   44   30   54   81  ---    25
 R18  | 2003   74   15   31   29   53  110  117   21 |    96   55   82   44   34   50   53    56
 R19  |  692   72   15   21   16   56   77  ---   16 |   117   69   62   73   61   49  ---    67
 R20  | 1673   53   24   10   21   57   75  ---   15 |    93   47   48   59   39   33  ---    48
 R21  |  550   44   17   15   14   48   84  ---   14 |    40   50   61   53   34   38  ---    47
 R22  |  858   59   21   16   19   48   66  ---   14 |    41   55   36   50   33   52  ---    41
 R23  |  723   31   16   11   14   47   57  258   10 |    65   44   40   35   38   37   33    38
 R24  |  811   42   30   24   21   71   62  ---   15 |    73   55   37   37   47   43  ---    38
------+----------------------------------------------+------------------------------------------
 RMS  | 2065  110   22   18   22   52   69  164      |T   80   52   45   47   44   49   33    50
 WRMS | 2065   57   23   16   26   46   69  164      |NE  63   61   44   44   41   47   36    54
 MEDI | 1144   53   20   15   19   48   66  130      |MD  65   39   42   44   39   49   31    38

Table 3.1632.3  GPS week: 1632   Day: 3   MJD: 55671                            

        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  | 1021   60   17   14   15   32   40  ---   11 |    88   25   31   26   28   57  ---    30
 R02  |  951   52   28   12   13   32   49  ---   13 |    50   37   28   28   33   50  ---    26
 R03E | 5126   95   21   19   24   42   39  ---   16 |    80   32   54   57   74   45  ---    42
XR04  |10570  ---  171  ---  ---  ---  623  ---  327 |   ---  342  ---  ---  ---  837  ---   315
 R05  | 2619   58   18   12   21   70   51  132   13 |    49   46   38   49   70   25   26    37
 R06  |  826   52   21   24   18   64   80  ---   16 |    33   52   35   52   73   39  ---    38
 R07  | 1798   36   18   24   20  113   35  ---   12 |    50   21   25   43  108   47  ---    24
 R08  | 1209   42   30   18   31   51   43   53   14 |    48   36   22   32   45   38   63    20
 R09E |  743   37   24   15   14   50   70  ---   13 |   137   45   31   32   51   49  ---    31
 R10E | 3617   45   14   20   16   31   54  ---   12 |    49   38   41   41   46   41  ---    36
 R11E | 1350   51   40   22   30   47   36  152   16 |    63   47   76   54   56   61   43    55
 R12E | 1841   45   10   13    8   38   50  ---   10 |    67   26   33   25   41   41  ---    27
 R13E | 1504   44   17   13   21   35   43  ---   11 |   115  113  124  116  121  137  ---   119
 R15E | 1405   97   14   13   21   45   72  159   17 |   122   30   35   35   59   42   28    33
 R16E | 1010   45   13   11   15   29   59  ---   11 |    69   23   30   28   34   31  ---    23
 R17  | 1878  111   27   18   21   64   65  ---   19 |    70   38   59   43   54   97  ---    46
 R18  | 1381   51   22   25   16   48   76   88   15 |    59   52   41   53   58   52   86    41
 R19  | 1077   42   23   14    8   69   52  ---   11 |    64   54   49   49   41   44  ---    48
 R20  | 1074  120   35   18   17   46  101  ---   23 |   119   62   45   42   50   78  ---    45
 R21  |  833   49   16   18   16   42   81  ---   15 |    87   53   73   72   36   46  ---    62
 R22  |  632   41   20   18   13   66   48  ---   11 |    78   64   47   50   44   59  ---    52
 R23  | 1713   56   19    8   22   58   53  242   13 |    59   44   30   48   48   55   32    36
 R24  | 1158   62   19    9   12   68   51  ---   12 |    64   60   51   57   42   36  ---    47
------+----------------------------------------------+------------------------------------------
 RMS  | 1879   63   22   17   19   55   59  150      |T   73   58   45   46   55   87   46    53
 WRMS | 1879   57   23   16   18   48   59  150      |NE  65   65   41   46   52  104   51    57
 MEDI | 1350   51   20   15   16   47   52  132      |MD  64   45   38   43   48   47   32    38

Table 3.1632.4  GPS week: 1632   Day: 4   MJD: 55672                            

        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  | 2212   55   20   13   31   53   40  ---   14 |    46   28   36   40   36   43  ---    24
 R02  | 1268   30   21   13   28   32   44  ---   12 |    52   32   30   20   35   37  ---    21
 R03E | 6508   46   18   17   16   46   25  ---   11 |    36   26   39   45   52   52  ---    31
XR04  |12741  ---   66  ---  ---  ---  183  ---  110 |   ---  290  ---  ---  ---  358  ---   228
 R05  | 2405   43   37   22   28   36   31   75   15 |    35   46   23   31   46   40   25    27
 R06  | 1308   34   24   18   17   45   41  ---   12 |    45   37   45   25   60   23  ---    31
 R07  | 2752   26   21   14   24   83   41  ---   11 |    44   24   34   40   73   25  ---    27
 R08  |  917   47   15   13   34   63   41   85   13 |    44   26   22   29   47   45   43    22
 R09E |  561   63   17   11   17   47   42  ---   13 |    82   19   32   29   53   37  ---    21
 R10E | 3548   51   21   16   23   65   50  ---   14 |    52   39   24   37   70   32  ---    25
 R11E | 1691   40   30   28   28   50   46   92   16 |    42   48   65   72   40   55   63    53
 R12E | 2351   42   18   19   19   41   22  ---   11 |    62   29   40   38   44   44  ---    31
 R13E | 1470   41   17   12   24   55   37  ---   11 |    76   58   79   82   90   80  ---    71
 R15E | 3971   47   30   17   21   51   31   94   13 |    46   39   36   31   46   40   51    30
 R16E | 2605   50   22   19   22   31   51  ---   14 |    50   25   39   49   26   32  ---    32
 R17  | 1809   62   19   22   21   60   53  ---   15 |    42   25   50   46   56   74  ---    37
 R18  | 1347   23   29   36   20   40   63   89   17 |    39   43   28   41   47   61   96    27
 R19  | 1441   41   21   18   14   42   47  ---   12 |    44   58   28   49   40   63  ---    41
 R20  | 1906   59   24   29   26   79   65  ---   18 |    74   69   90   52   54   33  ---    61
 R21  |  981   64   20   21   35   63   64  ---   18 |   117   62   83   77   48   36  ---    68
 R22  |  825   55   14   14   12   69   45  ---   12 |   114   58   62   68   55   54  ---    63
 R23  | 2781  103   19   26   27   47   40  161   20 |   112   43   31   44   48   40   72    35
 R24  |  909   33   21   14   31   72   40  ---   13 |    47   43   24   23   52   46  ---    28
------+----------------------------------------------+------------------------------------------
 RMS  | 2447   51   22   20   24   55   45  103      |T   59   50   42   44   50   58   58    44
 WRMS | 2447   44   23   18   22   55   45  103      |NE  61   58   41   41   49   65   59    49
 MEDI | 1809   46   21   17   23   50   42   89      |MD  46   39   36   40   48   43   51    31

Table 3.1632.5  GPS week: 1632   Day: 5   MJD: 55673                            

        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  | 1940   51   24   17   28   36   31  ---   14 |    52   21   24   31   29   26  ---    21
 R02  |  874   56   14   14   23   43   31  ---   12 |    47   31   33   34   46   38  ---    29
 R03E | 6825   52   14   15   27   43   23  ---   12 |    61   22   31   40   47   32  ---    24
XR04  |12501  ---  113  ---  ---  ---  202  ---  152 |   ---  290  ---  ---  ---  138  ---   245
 R05  | 2437   68   38   20   21   33   43   52   17 |    43   32   31   30   27   27   16    20
 R06  | 2659   36   35   12   22   55   33  ---   13 |    35   40   43   36   55   16  ---    33
 R07  | 1334   31   18   14   13   66   26  ---    9 |    30   24   24   26   73   21  ---    19
 R08  | 1271   43   30   19   18   38   38   76   14 |    37   26   28   29   26   31   36    23
 R09E |  484   41   19   19   29   36   51  ---   15 |    65   23   44   50   28   22  ---    33
 R10E | 1755   41   18   14   17   27   19  ---   10 |    60   44   43   40   43   33  ---    38
 R11E |  683   50   50   36   26   75   37   88   19 |    49   35   87   66   61   46   38    56
 R12E | 1796   57   12   16   11   72   32  ---   12 |    39   21   29   29   56   33  ---    22
 R13E | 1582   77   20   22   19   42   37  ---   16 |    54   73   88   77   70   76  ---    73
 R15E | 2043   88   28   20   39   48   53  116   21 |   102   39   61   73   63   30   26    50
 R16E | 3004   61   23   28   31   83   28  ---   16 |    54   22   47   55   46   32  ---    31
 R17  | 3079   41   23   13   17   35   34  ---   12 |    42   27   24   25   45   43  ---    21
 R18  | 1441   28   10   19   14   24   42  164   11 |    36   35   57   47   40   40   61    42
 R19  | 1387   36   16   23   21   45   38  ---   12 |    60   51   46   50   38   37  ---    44
 R20  | 2462   21   34   45   22   35   66  ---   20 |    84   57   46   64   48   62  ---    52
 R21  | 1739   38   31   12   17   99   33  ---   12 |    73   54   66   53   44   88  ---    62
 R22  | 1029   56   24   17   13   63   21  ---   12 |   112   57   52   53   59   64  ---    59
 R23  | 2104   61   21   17   10   42   30  152   13 |    88   29   52   58   68   48   39    48
 R24  | 1421   53   13   15   15   48   18  ---   10 |    60   29   35   54   41   32  ---    36
------+----------------------------------------------+------------------------------------------
 RMS  | 2338   52   25   21   22   53   36  115      |T   58   47   45   46   47   44   36    47
 WRMS | 2338   48   25   18   20   46   36  115      |NE  57   53   40   42   45   47   38    50
 MEDI | 1755   50   23   17   19   43   33   88      |MD  54   32   43   47   46   33   36    36

Table 3.1632.6  GPS week: 1632   Day: 6   MJD: 55674                            

        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  |  674   51   11   15   24   60   35  ---   11 |    41   39   33   46   41   42  ---    34
 R02  |  782   55   23   15   35   57   28  ---   13 |    46   36   33   35   40   36  ---    30
 R03E | 5688   45   20   10   21   32   46  ---   12 |    39   23   34   33   24   30  ---    26
XR04  |14727  ---   49  ---  ---  ---  176  ---  113 |   ---  522  ---  ---  ---  128  ---   508
 R05  | 1249   49   36    8   32   38   37   67   14 |    63   49   28   41   40   31   25    29
 R06  | 1633   42   31   17   22   31   34  ---   13 |    52   42   41   35   42   27  ---    34
 R07  | 1851   49   26   15   22   48   30  ---   12 |    29   24   31   40   40   32  ---    27
 R08  | 1806   50   24   10   19   35   39   63   12 |    58   27   25   29   33   31   39    23
 R09E | 1917   74   28   19   20   56   29  ---   14 |    83   28   44   42   40   23  ---    32
 R10E | 2193   75   26   10   22   44   20  ---   13 |    68   61   59   51   53   54  ---    53
 R11E |  917   43   40   24   31   45   32   97   16 |    69   30   67   67   49   41   33    49
 R12E | 3108   57   21   11   22  ---   36  ---   12 |    47   26   42   39  ---   33  ---    32
 R13E | 1120   91   19   14   12   38   33  ---   14 |    54   43   51   51   47   56  ---    46
 R15E | 2543   76   27   23   18   35   26  152   14 |   107   46   44   34   39   37   30    39
 R16E | 3306   61   27   14   35   32   35  ---   14 |    63   27   39   29   47   36  ---    27
 R17  | 5376   73   30   11   10   59   21  ---   12 |   103   29   61   53   41   58  ---    51
 R18  | 1003   65   39   23   15   32   38  268   16 |    65   54   29   33   40   50   99    31
 R19  | 1120   55   25   12   13   67   42  ---   12 |    74   57   41   44   35   35  ---    44
 R20  | 2529  110   43   19   35   56   90  ---   25 |    77   55   55   47   59   46  ---    49
 R21  | 1628   46   26   13   11   69   57  ---   13 |   103   74   70   64   69   64  ---    69
 R22  | 1074  139   19   25   19  114   38  ---   14 |   140   80   86   72   32   68  ---    78
 R23  | 1310   36   14    9   20   40   41  147   10 |    77   48   46   44   41   83   54    50
 R24  | 1803   60   21   10   16   29   38  ---   12 |    92   51   50   51   50   73  ---    52
------+----------------------------------------------+------------------------------------------
 RMS  | 2415   68   27   16   23   52   40  149      |T   70   63   45   44   42   48   46    61
 WRMS | 2415   62   27   14   18   51   40  149      |NE  72   79   44   45   43   53   54    73
 MEDI | 1803   55   26   14   20   44   36   97      |MD  65   43   42   42   41   41   33    39




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