[IGSREPORT-19774] Wk 1634 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Fri May 20 00:08:15 PDT 2011


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1634   (May 01, 2011 - May 07, 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 2.1634.
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:
                                                                               
 igl1634[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1634 in the SP3 format.
 igl16347.sum      Combination Report for GPS Week 1634.


    
    
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  |    409.5 ns
                1  |    364.8 ns
                2  |    378.6 ns
                3  |    415.3 ns
                4  |    389.6 ns
                5  |    404.1 ns
                6  |    365.4 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
               ----+--------+---------------
                3  |  IAC   | ALL (high Transformation - See Table 2)
                4  |  IAC   | R04
                5  |  IAC   | R04
                6  |  BKG   | R04

    
         
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 1.1634, 1a.1634).
        
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 2.1634.0-6)                                                                                
    
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 3.1634.0-6). 
        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 1634 summary.                      (May 01, 2011 - May 07, 2011)

Table 1.1634.a     GPS week : 1634   MJD: 55682.0-55688.0

         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  153|    2    -1     0    57    24   -40  -.08   48   44 |       0     574   2703   2909
        |    1     2     6    37    71    92   .08           |       0     757
cod  247|   -1     1    -4    12   -19     5  -.16   26   23 |     ---     ---    ---    ---
        |    1     2     1    19    26    34   .07           |     ---     ---
esx  143|    0     0     0    15    48   -12   .40   16   16 |   19064   -2489   4793   9969
        |    1     1     2    30    38    18   .03           |   23298    3128
gfz  193|    0    -2     2   -57   -49    48  -.32   20   18 |  224889   -2503   4801  10378
        |    1     1     1    27    33    26   .06           |   55680    2992
grg  134|    0     2   -16   -10   -30    57  -.04   47   45 |     ---     ---    ---    ---
        |    1     3     5    63    63    61   .12           |     ---     ---
iac  n/a|    0     1     6     0   -36   -72  -.13   53   53 |  390548    -549   4796  10457
        |    1     1    15    51    39    84   .11           |   21554    1999


Table 1.1634.b     GPS week : 1634   MJD: 55682.0-55688.0   

         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  |   12   13   12   13   11   11   13 |
 R02  |   12   11   14   10   11   11   11 |
 R03  |   13   10   13   10   12   11   11 |
 R04  |  101  253  163    0  127  133   86 |
 R05  |   10   11   13   15   11   12   11 |
 R06  |   10   12   13   12   13   13   11 |
 R07  |    0    0    0    0    0   23   16 |
 R08  |   12   12   11   11   11   11    9 |
 R09  |   17   14   13   10    9    9   11 |
 R10  |   13   13   12   13   13   10   13 |
 R11  |   22   20   22   26   18   17   12 |
 R12  |   13   13   14   16    8   13   16 |
 R13  |   14   12   16   11   11   10   14 |
 R15  |   17   15   14   12   15   16   14 |
 R16  |   19   17   13   12   11   14   10 |
 R17  |   16   17   22   17   21   21   23 |
 R18  |   13   17   11   11    9   19   13 |
 R19  |   15   19   14   10   12   10   14 |
 R20  |   23   21   24   14   19   23   18 |
 R21  |   18   15    8   10   10   11   12 |
 R22  |   10   15   13   13   12   10   10 |
 R23  |   12   13   14   14    9   10   12 |
 R24  |   15   13   12   20   12   11   11 |


Table 1.1634.c     GPS week : 1634   MJD: 55682.0-55688.0   

         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 1634 0   |  -64    64   309   -1866    -756   -9168  84.7  1925  1925 |  409484       0
brd 1634 1   |   50    47   417   -1421     448   -9170  84.8  1611  1611 |  364754       0
brd 1634 2   |   14    12   263    -308    -939  -12840  85.9  1828  1828 |  378620       0
brd 1634 3   |   53     7   247    -886      41  -17840  82.7  2078  2078 |  415279       0
brd 1634 4   |  -13   100   299     519    -201  -20070  85.8  2139  2139 |  389572       0
brd 1634 5   | -130    20   282    1961     794  -17200  86.3  1979  1979 |  404052       0
brd 1634 6   |  -18    15   375    1495      17  -20380  83.8  2655  2655 |  365433       0
-------------+------------------------------------------------------------+----------------
brd 1634 mean|  -15    38   313     -72     -85  -15238  84.8  2030  2030 |  389599       0
brd 1634 sdev|   65    34    61    1454     616    4827   1.3   325   325 |   20758       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 2.1634.0  GPS week: 1634   Day: 0   MJD: 55682                            

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  153|    3    -6    -5    81   -66     6  -.17   64   61 |       0     800   2843   3091
cod  247|   -1     2    -3    18   -15   -21  -.25   25   24 |     ---     ---    ---    ---
esx  143|    0     0     0   -24    39   -12   .43   17   16 |   54215   -5385   4739   7976
gfz  193|    0    -3    -1   -41     1    35  -.26   22   17 |  264808   -2956   4734   8022
grg  134|   -2     0    -8    46    85    61  -.03   44   44 |     ---     ---    ---    ---
iac  n/a|    1     1    11    -6   -11   -16  -.05   48   48 |  409646    -686   4731   8767

Table 2.1634.1  GPS week: 1634   Day: 1   MJD: 55683                            

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  153|    3    -4    -4    74    99  -119  -.05   58   52 |       0    1431   2846   3075
cod  247|    0     0    -7     1   -26    -7  -.05   25   25 |     ---     ---    ---    ---
esx  143|    0     0     4    53   121    11   .36   18   17 |   -2765     316   4702   9440
gfz  193|   -1     0     2   -92  -105    89  -.43   22   22 |  218292    2331   4697   9760
grg  134|   -1     0   -12    39   -70   133   .13   55   53 |     ---     ---    ---    ---
iac  n/a|    1     0     0    15   -76  -125   .02   45   45 |  364271    2246   4704  10196

Table 2.1634.2  GPS week: 1634   Day: 2   MJD: 55684                            

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  153|    3    -1     0    65   -64   -22  -.01   56   46 |       0    1407   2750   2914
cod  247|   -1     0    -3    31   -18    28  -.21   24   20 |     ---     ---    ---    ---
esx  143|   -2     0     1    11    55   -18   .40   17   17 |    4109   -6228   5571   8605
gfz  193|    2     0     3  -102   -39    51  -.32   21   19 |  107951   -5275   5609   8817
grg  134|   -1     3   -14   -74   -58     3   .09   48   48 |     ---     ---    ---    ---
iac  n/a|   -2     4     4    49    26  -213  -.11   55   55 |  380417   -3828   5555   9000

Table 2.1634.3  GPS week: 1634   Day: 3   MJD: 55685                            

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  153|    4    -2    -5    82    41  -169  -.03   37   34 |       0     -77   2242   2417
cod  247|    0     0    -2    42   -63    -7  -.12   35   30 |     ---     ---    ---    ---
esx  143|    0     1     1    -9    54     1   .38   14   13 |   34889    -998   4854   8555
gfz  193|    0    -1     1   -38   -38    77  -.33   18   22 |  269894   -4078   4863   8896
grg  134|   -1     8   -15     0   -68   132  -.01   53   53 |     ---     ---    ---    ---
iac  n/a|    1     1    38    37   -72    50  -.09   63   63 |  415062    -147   4822   8863

Table 2.1634.4  GPS week: 1634   Day: 4   MJD: 55686                            

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  153|    2     1     5   -24    93   120  -.19   39   37 |       0     619   2821   3055
cod  247|   -3     6    -3    -7   -16    -8  -.15   25   20 |     ---     ---    ---    ---
esx  143|    0     0    -2    50    15   -47   .39   15   14 |   21860     607   4855   8389
gfz  193|    3    -4     1   -42   -51    18  -.23   19   17 |  241422    -583   4852   8359
grg  134|    2     1   -23   -69    15    74  -.11   47   44 |     ---     ---    ---    ---
iac  n/a|    1    -1     8   -32   -13   -30  -.28   53   53 |  389659    1252   4775   8899

Table 2.1634.5  GPS week: 1634   Day: 5   MJD: 55687                            

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  153|    0     0     2    67    74   -47   .01   38   37 |       0    -666   2847   3113
cod  247|   -4     1    -4    -3   -27    75  -.10   26   23 |     ---     ---    ---    ---
esx  143|    0     0    -1    33    50    -9   .40   17   15 |   32002      -7   4452  17874
gfz  193|    0    -3     5   -43   -74    22  -.31   18   14 |  255269    -799   4478  20868
grg  134|    0     0   -22   -80   -17    22  -.13   40   40 |     ---     ---    ---    ---
iac  n/a|    2     2    -3   -99   -38   -85  -.11   57   57 |  409842   -1951   4669  19137

Table 2.1634.6  GPS week: 1634   Day: 6   MJD: 55688                            

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  153|    1     0    12    55    -3   -54  -.12   43   43 |       0     507   2573   2700
cod  247|   -2    -1    -6     3    27   -18  -.21   23   21 |     ---     ---    ---    ---
esx  143|    0     2     1    -5     0   -11   .46   16   17 |  -10861   -5731   4384   8946
gfz  193|    1    -1     1   -43   -39    46  -.37   19   16 |  216592   -6166   4376   7930
grg  134|    1     3   -17    65  -101   -27  -.21   39   36 |     ---     ---    ---    ---
iac  n/a|    0     0   -11    29   -72   -85  -.26   52   52 |  364942    -735   4320   8342

       
       
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 3.1634.0  GPS week: 1634   Day: 0   MJD: 55682                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  IGL |   bkg  cod  esx  gfz  grg  iac   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1699   65   10    9   21   42   38   12 |    66   60   53   61   65   68    56
 R02  | 1022   50   16   13   19   38   41   11 |    57   62   52   51   68   55    52
 R03E | 2637   37   34   19   15   38   35   13 |    82   64   76   78   71   60    70
XR04  |10578  ---   64  ---  ---  ---  159  101 |   ---  173  ---  ---  ---  268   141
 R05  | 1508   42   22   12   11   31   31   10 |    88   96   83   86   92   94    87
 R06  | 2274   31   10   12   17   49   46   10 |   117  111  111  111  134  129   112
XR07  | ----  ---    4  ---  ---  ---  ---    0 |   ---  599  ---  ---  ---  ---   601
 R08  |  887   45   13   14   14   32   49   11 |    84   82   88   78   94   88    82
 R09E | 1752   88   23   19   30   42   41   17 |    54   27   40   49   49   34    34
 R10E | 1661   59   17   16   19   33   41   13 |   121  124  144  132  108  111   131
 R11E | 1964   81   43   31   32   50   71   22 |   139   89  129  117  110  120   113
 R12E |  919   48   20   20   15   36   42   12 |    77   45   63   61   53   37    54
 R13E | 2055   78   16   17   16   40   38   14 |    61   34   47   44   27   27    40
 R15E | 3134   62   23   12   31   39   68   16 |    46   21   37   32   49   59    29
 R16E |  732  105   21   24   25   45   46   18 |   121   58   57   72   73   71    62
 R17  | 4011   56   15   16   25   52   74   16 |    59   51   56   65   60   89    56
 R18  |  775   49   21   17   18   38   44   12 |    58   59   56   46   69   49    49
 R19  |  669   33   39   18   27   35   43   15 |    61   51   46   65   32   45    45
 R20  | 3577   97   57   15   34   82   45   22 |    96   79   84   97   73   94    83
 R21  |  532  109   23    9   18   39   40   17 |    75   77   66   80   71   79    69
 R22  |  458   36   21   11   14   67   30    9 |    89   75   76   76   56   77    74
 R23  |  816   37   12   12   13   20   59   11 |    51   40   41   43   40   43    37
 R24  | 1565   34   23   26   18   42   56   14 |    50   42   63   56   62   30    46
------+-----------------------------------------+-------------------------------------
 RMS  | 1924   64   25   17   22   44   48      |T   78   92   69   71   69   78    92
 WRMS | 1924   61   24   16   17   44   48      |NE  82   82   74   77   89   86    76
 MEDI | 1565   50   21   16   18   39   43      |MD  75   62   63   65   68   68    62

Table 3.1634.1  GPS week: 1634   Day: 1   MJD: 55683                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  IGL |   bkg  cod  esx  gfz  grg  iac   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  877   31   27   25   11   51   44   13 |    60   40   57   54   63   54    48
 R02  | 1195   26   20   13   12   56   46   11 |    53   69   61   68   68   72    63
 R03E | 1127   38   17   13    9   38   30    9 |   104   78   85   91   90   66    83
XR04  |12431  ---  169  ---  ---  ---  378  253 |   ---  245  ---  ---  ---  261   131
 R05  | 1154   31   24   12   23   46   29   11 |   107  101  106  100  113   90   101
 R06  | 1797   36   19   10   24   35   45   12 |   135  113  121  126  146  121   121
XR07  | ----  ---    4  ---  ---  349  ---    0 |   ---  448  ---  ---  536  ---   450
 R08  | 1381   42   18   22   14   46   31   11 |   106  102   90   92   69   86    93
 R09E | 1331   69   22   16   18   54   38   14 |    89   43   45   38   36   42    39
 R10E | 2519   62   11    8   19   53   43   12 |   115   88  103  102  111   87    97
 R11E | 1530   60   25   25   37   44   72   19 |   105   78  103   93   90   89    89
 R12E | 1227   32   27   17   15   45   48   12 |    50   45   42   39   45   40    38
 R13E |  954   60   19   12   16   38   35   12 |    76   39   51   48   37   25    42
 R15E | 1802   61   30   13   24   44   43   15 |    79   26   39   41   30   46    32
 R16E |  968   85   22   18   36   51   32   17 |   132   72   89   63   55   88    78
 R17  | 2924   68   35   19   21   69   52   17 |    61   44   64   53   39   65    53
 R18  |  731   80   31   18   20   45   39   16 |    85   32   50   41   51   41    38
 R19  |  704   88   34   23   14   51   56   18 |    49   39   32   44   45   58    30
 R20  | 3441   82   47   26   32   69   44   20 |    90   66   57   82   66   93    68
 R21  | 1135   54   23   13   21   45   57   14 |   109   70   76   88   64   73    76
 R22  |  482   45   22   14   26   61   55   14 |    76   56   62   53   46   85    58
 R23  | 1519   49   19   20   17   83   37   12 |    65   33   48   46   76   61    41
 R24  | 1492   55   15   18   22   96   42   13 |    91   53   50   67   87   48    53
------+-----------------------------------------+-------------------------------------
 RMS  | 1610   58   25   18   22   55   45      |T   87   86   68   68   89   76    83
 WRMS | 1610   52   25   17   22   53   45      |NE  88   80   86   87   97   84    83
 MEDI | 1227   55   22   17   20   51   43      |MD  89   66   61   63   64   66    63

Table 3.1634.2  GPS week: 1634   Day: 2   MJD: 55684                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  IGL |   bkg  cod  esx  gfz  grg  iac   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1313   28   19   24   23   31   38   12 |    41   47   44   47   46   62    44
 R02  | 1388   36   15   18   25   31   63   13 |    66   56   59   60   56   63    55
 R03E | 1720   42   15   12   24   49   64   13 |    69   54   58   60   46   50    53
XR04M |12440  ---   85  ---  ---  ---  311  163 |   ---  195  ---  ---  ---  177   132
 R05  |  812   26   34   17   24   34   29   12 |    74   72   71   64   93   82    66
 R06  | 1433   40   21   12   23   36   61   13 |   113   94   94   93  115   84    92
XR07M | ----  ---    4  ---  ---  ---  ---    0 |   ---  535  ---  ---  ---  ---   535
 R08M | 1159   41    9   10   20   37   49   11 |    83   70   73   85   86   69    73
 R09E | 1120   59   22   21   17   30   31   13 |    52   23   44   40   47   33    32
 R10E | 2926   46   18   14   22   32   32   11 |    93   91   90   92   91   69    86
 R11E | 1217   80   48   28   21   47   64   21 |    99   77   99   91   94   72    81
 R12E | 1072   42   23   13   24   29   58   13 |    43   43   47   51   54   31    40
 R13E |  812   39   18   18   25   53   86   16 |    48   32   44   43   54   47    33
 R15E | 3728   56   17   18   27   60   51   14 |    70   26   47   30   56   35    32
 R16E |  729   44   24   14   14   48   49   12 |    88   34   42   41   46   48    38
 R17M | 2642  100   29   18   27   57   86   21 |    64   41   53   67   43   80    46
 R18M | 1014   30   20   12   20   44   50   11 |    51   48   40   36   47   32    37
 R19M |  781   38   11    8   26   54   78   14 |    60   45   52   66   40   65    48
 R20M | 3669  141   34   18   14   59   43   23 |   151   63   55   63   68   64    62
 R21M |  965   26   15   12   11   66   28    8 |    77   74   70   78   71   84    73
 R22M |  497   48   16   14   14   46   58   12 |    56   53   43   53   50   69    45
 R23M | 2725   44   27   27   18   66   37   14 |    39   35   47   35   70   38    31
 R24M | 1131   20   29   19   15   63   36   11 |    49   38   52   43   60   55    42
------+-----------------------------------------+-------------------------------------
 RMS  | 1828   56   24   17   21   48   55      |T   70   80   58   58   63   64    77
 WRMS | 1828   46   20   17   19   48   55      |NE  73   67   67   66   77   72    64
 MEDI | 1159   42   20   17   22   47   50      |MD  66   53   52   60   56   63    48

Table 3.1634.3  GPS week: 1634   Day: 3   MJD: 55685                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  IGL |   bkg  cod  esx  gfz  grg  iac   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1026   29   28   17   20   43   42   12 |    59   43   59   55   47   55    53
 R02  | 1762   31   14   10   17   49   41   10 |    73  100   91   93   92   88    89
 R03E | 2747   23   26   11   16   32   60   10 |    76   80   87   84   85   82    83
XR04  | 9302  ---    5  ---  ---  ---  324    0 |   ---  164  ---  ---  ---  203   171
 R05  | 1446   28   38   16   29   48   96   15 |   108   96   78   91   77   63    89
 R06  |  935   26   34   11   18   38   65   12 |    98   86   89   94   93   96    92
XR07  | ----  ---    5  ---  ---  187  ---    0 |   ---  743  ---  ---  725  ---   743
 R08  |  767   34   21   11   14   57   72   10 |    86   92   93   83   78   75    88
 R09E |  900   27   29    6   11   56   71    9 |    61   48   66   56   45   75    58
 R10E | 4822   43   27   12   12   30   52   12 |   123   84  109  100   93   95   102
 R11E | 1952   63   73   25   33   72   81   25 |   132  100  147  155  125  139   137
 R12E |  614   52   28   14   24   69   53   15 |    74   30   52   46   61   49    43
 R13E | 1240   33   21   11   17   55   71   11 |    54   43   50   60   81   47    51
 R15E | 3900   29   29   13   15   47   58   11 |    56   37   37   45   52   45    35
 R16E |  668   41   23    8   16   42   60   12 |    94   60   72   63   76   82    68
 R17  | 3549   48   46   15   15   58   57   16 |    74   37   46   47   45   61    43
 R18  | 2673   41   14   16    6   62   45   11 |   102   68   66   76   70   69    72
 R19  |  790   27   15    9   19   58   54    9 |    40   47   53   64   42   68    51
 R20  | 1249   50   25   13   16   72   67   14 |    84   94   86   76  114  107    85
 R21  | 1179   27   17   12   17   55   65   10 |    59   65   58   77   63  102    62
 R22  |  611   31   28   10   23   39   46   12 |    65   54   59   54   64   82    53
 R23  | 1829   34   42   15   13   55   72   14 |   147  115  129  118   99  127   124
 R24  | 1699   28   71   27   11   52   78   20 |    45   72   62   45   72   73    44
------+-----------------------------------------+-------------------------------------
 RMS  | 2077   37   35   14   18   53   63      |T   81  102   75   75  104   85   105
 WRMS | 2077   34   30   13   22   53   63      |NE  84   81   79   83   77   75    80
 MEDI | 1249   31   27   12   16   55   60      |MD  74   72   66   76   76   75    72

Table 3.1634.4  GPS week: 1634   Day: 4   MJD: 55686                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  IGL |   bkg  cod  esx  gfz  grg  iac   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  687   18   24   15   20   26   42   10 |    43   40   48   33   39   49    37
 R02  | 1685   20   17    8   20   33   61   10 |    63   55   65   73   57   64    62
 R03E | 3039   27   19   11   26   27   49   11 |    79   70   71   77   67   67    71
XR04  | 1472  204   78  ---  ---  ---  316  127 |   221  145  ---  ---  ---  220   152
 R05  | 1449   28   27   18   17   25   34   11 |    54   46   36   49   55   45    42
 R06  | 1131   22   26   16   22   56   59   12 |    45   43   40   41   60   53    38
XR07  |10644  ---    5  ---  ---  ---  ---    0 |   ---  395  ---  ---  ---  ---   393
 R08  | 1318   41   16   11   15   35   54   11 |    58   41   53   41   41   44    42
 R09E | 1114   28   16    7   15   38   44    9 |    46   34   39   35   46   39    34
 R10E | 6218   54   17    8   16   24   63   13 |   115   66   73   68   71   78    72
 R11E | 1239   34   57   29   18   70   34   18 |   135   87  144  124  118  107   120
 R12E | 1343   30   12    8   18   50   19    8 |    44   33   37   38   49   44    34
 R13E |  981   33   19   17   19   42   40   11 |    59   45   52   49   49   53    46
 R15E | 1590   47   29   18   22   45   57   14 |    56   31   45   48   45   34    36
 R16E |  858   38   18   11   25   38   38   11 |    61   44   53   48   40   52    47
 R17  | 2284   84   45   18   19   40   85   21 |    70   48   65   58   63   90    51
 R18  | 4448   31   16    8   13   43   36    8 |    79   55   64   58   48   60    59
 R19  |  634   37   15   16   19   79   53   11 |    92   47   66   62   49   36    59
 R20  | 1065   67   43   17   24   56   74   19 |   219  215  231  236  237  197   223
 R21  | 1727   21   21    8   10   42   56    9 |    64   72   70   69   61   74    68
 R22  |  610   46   16   18    9   53   46   11 |    80   46   37   45   56   48    43
 R23  |  510   21    9    9   20   31   49    9 |   205  212  209  217  209  193   210
 R24  |  855   22   11   13   15   74   76   11 |    52   49   55   54   46   30    50
------+-----------------------------------------+-------------------------------------
 RMS  | 2138   39   25   15   19   47   53      |T   88   83   73   72   71   76    86
 WRMS | 2138   37   20   14   17   44   53      |NE  51   46   47   49   52   52    44
 MEDI | 1318   31   18   13   19   42   49      |MD  63   48   55   54   55   53    51

Table 3.1634.5  GPS week: 1634   Day: 5   MJD: 55687                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  IGL |   bkg  cod  esx  gfz  grg  iac   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  887   22   25   14   16   32   54   11 |    41   34   45   41   42   51    38
 R02  | 1488   33   15   11   15   40   51   11 |    68   79   92   83   68   64    80
 R03E | 3140   26   21   11   24   35   41   11 |    77   73   83   86   97   77    79
XR04  | 1212  171  102  ---  ---  ---  254  132 |   193  130  ---  ---  ---  187   168
 R05  | 1361   20   31   18   21   58   41   12 |    53   57   57   48   60   45    50
 R06  | 1579   19   20   29   12   16   52   12 |    68   59   76   59   70   65    63
XR07  | 2790  ---   31   19   46   53   77   22 |   ---  454   13   30  333   16   459
 R08  | 2590   19   24   10   22   43   45   11 |    54   54   54   43   67   45    48
 R09E | 1214   19   20   13   16   35   30    9 |    48   31   47   55   34   47    43
 R10E | 4379   30   14   13   10   19   52   10 |    51   53   60   54   50   68    53
 R11E | 1326   36   37   19   16   48   84   16 |    94   73   87   83   65   91    80
 R12E | 1712   52   18   13   14   35   37   12 |    64   26   48   39   42   34    38
 R13E | 1226   37   16   12   14   35   24    9 |    76   55   65   63   64   47    60
 R15E | 1910   33   37   10   28   51   76   16 |    53   42   53   52   27   38    46
 R16E | 1159   27   25   14   23   31   67   13 |    85   58   71   58   47   78    62
 R17  | 1715   70   33   15   28   59   97   21 |    41   27   28   51   54   82    27
 R18  | 4169   25   46   39   16   34   71   18 |    33   39   54   32   40   30    28
 R19  | 1034   31   15   13   12   60   39    9 |    63   42   52   52   36   44    48
 R20  | 1321   98   39   19   24   48   61   23 |   372  334  334  341  343  339   342
 R21  |  835   20   19   16   20   40   43   10 |    78   76   75   91   82   95    80
 R22  |  646   24   15   14   11   36   56   10 |    48   43   49   44   44   40    43
 R23  | 1031   22    9   15   17   26   48    9 |   276  283  291  281  290  278   283
 R24  | 1071   15   19    8   13   31   67   10 |    48   57   46   42   54   56    45
------+-----------------------------------------+-------------------------------------
 RMS  | 1978   38   25   17   18   40   57      |T   90   94   80   78   91   83    98
 WRMS | 1978   37   23   15   14   40   57      |NE  57   57   67   57   60   56    57
 MEDI | 1326   26   21   14   16   35   52      |MD  63   57   54   52   54   56    53

Table 3.1634.6  GPS week: 1634   Day: 6   MJD: 55688                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  bkg  cod  esx  gfz  grg  iac  IGL |   bkg  cod  esx  gfz  grg  iac   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1192   32   26   10   26   38   55   13 |    43   42   48   46   51   65    45
 R02  |  870   18   17   13   20   26   51   10 |    62   76   70   75   77   63    69
 R03E | 2618   38   21   11   19   29   33   10 |    81   91   89   89   85   79    86
XR04  | 1399  357   47  ---  ---  ---  159   86 |   258  107  ---  ---  ---  207   126
 R05  | 1192   27   20    7   18   30   59   11 |    69   75   71   76   76   67    72
 R06  | 1740   30   21    9   19   56   48   11 |    94   95  103  116   79   94   102
XR07  | 3191  ---   19   21   31   58   53   16 |   ---  440   19   37  315   22   437
 R08  | 2112   15   12    9   18   30   47    9 |    91   96   91   98   90   87    93
 R09E |  877   34   27   13   23   29   20   11 |    54   43   49   45   40   45    43
 R10E | 3867   32   26   14   23   49   58   13 |    69   73   74   71   73   87    71
 R11E |  745   37   25   17   18   58   45   12 |    94   87  113   98   95  108   100
 R12E | 1624   55   28   22   14   35   72   16 |    85   38   59   52   36   41    48
 R13E | 2332   74   15   12    9   48   36   14 |    80   48   59   54   45   40    52
 R15E | 6524   42   26   13   28   57   51   14 |    73   61   53   56   50   46    55
 R16E | 1325   24   19   10   17   36   43    9 |    98   80   81   75   67   81    79
 R17  | 5136  101   31   18   28   42   86   22 |    69   48   53   56   61   97    46
 R18  | 4662   26   12   16   16   29   72   12 |    71   66   53   65   61   49    58
 R19  | 1139   36   26   25   15   32   49   13 |    73   60   37   49   50   38    46
 R20  | 2792   45   35   35   13   40   60   17 |   395  419  425  421  415  415   418
 R21  |  592   48   14   14   16   30   51   12 |   118   89   87   98   98  130    94
 R22  | 1198   30   22   10   14   38   41   10 |    88   62   62   67   65   70    64
 R23  | 1256   35   21   15   24   41   36   11 |   368  362  360  363  358  359   362
 R24  |  908   41   21   14   12   28   41   11 |    76   48   48   52   45   29    46
------+-----------------------------------------+-------------------------------------
 RMS  | 2655   43   23   16   19   39   52      |T  114  113   95   98  106  100   113
 WRMS | 2655   43   21   17   16   36   52      |NE  67   72   73   78   70   72    72
 MEDI | 1399   35   21   13   18   36   51      |MD  80   75   62   67   67   70    71




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