[IGSREPORT-20735] Wk 1681 IGLOS Final Orbits

IGS ACC igs.acc at noaa.gov
Thu Apr 12 11:41:08 PDT 2012


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1681   (Mar 25, 2012 - Mar 31, 2012) 
                                                                               
Contact: J. Griffiths (jake.griffiths at noaa.gov)            
         K. Choi (kevin.choi 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 2.1681.
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:
                                                                               
 igl1681[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1681 in the SP3 format.
 igl16817.sum      Combination Report for GPS Week 1681.


    
    
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 until
    22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
    21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
    for the first time starting 11-Sep-2011 (GPS Week 1653).

 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 were added to the
    broadcast clocks. Before GPS Week 1637, the time offsets were derived
    from the bkg summary files; starting Week 1637 the offsets are derived
    from the gfz summary files.
    
               Day | applied clock offset
               ----+---------------------
                0  |    164.6 ns
                1  |    166.1 ns
                2  |    162.2 ns
                3  |    165.9 ns
                4  |    163.9 ns
                5  |    165.3 ns
                6  |    165.0 ns

    
         
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 1.1681, 1a.1681).
        
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 2.1681.0-6)                                                                                
    
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 3.1681.0-6). 
        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 1681 summary.                      (Mar 25, 2012 - Mar 31, 2012)

Table 1.1681.a     GPS week : 1681   MJD: 56011.0-56017.0

         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]
--------+----------------------------------------------------+------------------------------
cod  261|   -1     2     2    42   -26   -65  -.22   36   36 |     ---     ---    ---    ---
        |    1     2     2    47    35    14   .03           |     ---     ---
emx  145|    0    -2     0   -23   -75   -22  -.23   31   32 |  164132     309   4557   7591
        |    1     1     3    52    51    25   .04           |    1047    1461
esx  135|    0     0     3     2    34   -82   .41   19   18 |  164738     482   4548   4662
        |    1     0     4    43    24    39   .04           |    1017    3241
gfz  191|    0    -1     0     3     2    60  -.33   20   19 |       0    -601   4549   7653
        |    1     1     4    57    35    35   .06           |       0    2804
grg  123|   -1     4    -3    31   -55   163   .02   44   42 |  223261    -444   4534  38690
        |    2     3     3    23    28    40   .07           |   73171    3051
iac  n/a|    0     0    -5   -18    24    16   .10   22   22 |  166391    -988   4558   8388
        |    1     1     7    21    27    74   .05           |    1220    1614
mcc  n/a|    1    -3    46   -11    68   300   .16  105  105 |     ---     ---    ---    ---
        |    3     4    17    51    46   218   .25           |     ---     ---


Table 1.1681.b     GPS week : 1681   MJD: 56011.0-56017.0   

         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  |    8   11   12   10    9    9   13 |
 R02  |   12   13   10    9   10    9   13 |
 R03  |   11   10   11   10   10    9   13 |
 R04  |   14   12   11   10    9   10   11 |
 R05  |   10   13   17   12   11   10   10 |
 R06  |    9    9   14   12   10    8   10 |
 R07  |   10   10   12   12   12   14   11 |
 R08  |    9   11   11   11   11   11   11 |
 R09  |   11   11   13   11    9   10   11 |
 R10  |   11   10   11    8    9    9   11 |
 R11  |   18   19   19   19   18   16   17 |
 R12  |   11   11   11    9   12    9   10 |
 R13  |   10   10    9   12   19   10   11 |
 R14  |   14   14   14   12   15   14   14 |
 R15  |   12   11   10    8   11   11   11 |
 R16  |    9   12   11    9   12   10    9 |
 R17  |   11   12   13   11   10    9   11 |
 R18  |    9    9   11   11   10   10   14 |
 R19  |    9   10   10   14   12   10    9 |
 R20  |   19   14   18   18   22   15   19 |
 R21  |   15   17   18   14   16   18   16 |
 R22  |    9   10   13   13   10    9   14 |
 R23  |   10   10    9    9    9    7    9 |
 R24  |    9   11   10   11   11    8   11 |
 R26  |  ---    0    0    0    0    0    0 |


Table 1.1681.c     GPS week : 1681   MJD: 56011.0-56017.0   

         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 1681 0   |  -77    41    96     831   -1585    -971  86.9  1707  1707 |  164635       0
brd 1681 1   |  -68   -96    37     281    -236   -9755  86.5  1774  1774 |  166099       0
brd 1681 2   |   48    70    47    -159    1133   -7294  84.0  2050  2050 |  162218       0
brd 1681 3   |  -16   -35    74    2141     559   -1990  85.0  2159  2159 |  165920       0
brd 1681 4   |  -99    12   144     971   -1012     183  86.5  1812  1812 |  163920       0
brd 1681 5   |    7    12    87    -793    -346   -2216  85.5  1773  1773 |  165261       0
brd 1681 6   |   62   -62    87   -1154    -565    -325  88.3  1730  1730 |  164999       0
-------------+------------------------------------------------------------+----------------
brd 1681 mean|  -20    -8    82     302    -293   -3195  86.1  1857  1857 |  164721       0
brd 1681 sdev|   63    59    35    1128     915    3804   1.4   174   174 |    1330       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 2.1681.0  GPS week: 1681   Day: 0   MJD: 56011                            

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]
--------+----------------------------------------------------+------------------------------
cod  261|   -2     0     0    81    34   -71  -.22   35   35 |     ---     ---    ---    ---
emx  145|    2     0     1    36   -33   -39  -.20   32   34 |  164047     914   4539   7968
esx  135|    0    -1     0    16     0  -104   .44   18   15 |  163511    2563   4554   4662
gfz  191|   -2    -1    -6   -40   -30    48  -.45   22   21 |       0     364   4552   7825
grg  123|    1     0    -7    32   -18   164   .05   40   40 |  294216     414   4619  27755
iac  n/a|    1     1     4    -9    71    70   .08   20   20 |  166111    -750   4576   8488
mcc  n/a|   -3    -4    38    71    48   623   .64  103  103 |     ---     ---    ---    ---

Table 2.1681.1  GPS week: 1681   Day: 1   MJD: 56012                            

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]
--------+----------------------------------------------------+------------------------------
cod  261|   -1     3     4   119    -7   -56  -.27   40   44 |     ---     ---    ---    ---
emx  145|    0    -2     0    50   -31   -21  -.25   30   31 |  164786    1474   3912   7368
esx  135|    0    -1     8    24    40   -12   .44   19   18 |  163666    4388   3908   4006
gfz  191|   -1     0     0   -73     8    37  -.29   21   20 |       0    3390   3914   7687
grg  123|   -1     5    -5    19   -51   142  -.13   47   46 |  177499    3998   3735  20248
iac  n/a|    1     2    -9   -34    -3    -7   .04   19   19 |  167781    1014   3901   8768
mcc  n/a|    0    -1    53   -21   108    -9   .22   93   93 |     ---     ---    ---    ---

Table 2.1681.2  GPS week: 1681   Day: 2   MJD: 56013                            

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]
--------+----------------------------------------------------+------------------------------
cod  261|   -1     4    -1    55   -21   -58  -.23   38   38 |     ---     ---    ---    ---
emx  145|    0    -3    -4   -16  -128   -40  -.16   34   35 |  161936   -1126   4595   7094
esx  135|   -1     0     5    19    23  -119   .39   22   22 |  166117   -4315   4576   4709
gfz  191|    0     1     6     2    38    41  -.29   21   19 |       0   -3583   4570   7272
grg  123|    0     8     0    16  -103   123   .05   47   43 |  173879   -3352   4588  26295
iac  n/a|    0     0   -10   -29    35    26   .10   21   21 |  164871   -3592   4589   8209
mcc  n/a|    0   -11    57   -40    73   152   .15   90   90 |     ---     ---    ---    ---

Table 2.1681.3  GPS week: 1681   Day: 3   MJD: 56014                            

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]
--------+----------------------------------------------------+------------------------------
cod  261|   -2     5     5    -2   -81   -44  -.22   36   38 |     ---     ---    ---    ---
emx  145|    3     0     2   -61  -128     9  -.24   34   36 |  164081    1431   4182   6429
esx  135|   -2    -1     7   -83    27  -115   .33   17   17 |  165073    1732   4148   4257
gfz  191|    0    -2     3   105    51    35  -.32   18   17 |       0     498   4163   6576
grg  123|   -3     5    -5    11   -75   146   .06   50   44 |  352607     575   4174 134349
iac  n/a|    0    -1   -14    21    10   126   .15   22   22 |  167852    -567   4148   7390
mcc  n/a|    7    -5    70    -5   -13   358  -.09   94   94 |     ---     ---    ---    ---

Table 2.1681.4  GPS week: 1681   Day: 4   MJD: 56015                            

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]
--------+----------------------------------------------------+------------------------------
cod  261|    0     2     0    -3   -36   -76  -.25   36   34 |     ---     ---    ---    ---
emx  145|    0    -2     2   -37   -62   -26  -.23   32   34 |  164964   -2146   5589   8345
esx  135|    0     0     0    36    65   -85   .41   19   18 |  165530   -3134   5586   5717
gfz  191|    0    -4     1    20   -36    64  -.37   19   21 |       0   -4970   5586   8321
grg  123|   -1     5     0    43   -39   127   .03   48   41 |  164943   -5261   5589  17775
iac  n/a|    0     0    -6   -31     0    44   .10   23   23 |  165514   -2331   5581   9089
mcc  n/a|    3    -2    56   -78    47   521   .08  127  127 |     ---     ---    ---    ---

Table 2.1681.5  GPS week: 1681   Day: 5   MJD: 56016                            

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]
--------+----------------------------------------------------+------------------------------
cod  261|   -1     1     5    -1   -37   -67  -.17   35   32 |     ---     ---    ---    ---
emx  145|    0    -2    -5   -37  -128   -54  -.24   29   28 |  164192    1599   4457   8125
esx  135|   -1     0    -2   -29    21   -45   .43   16   15 |  163966    2670   4432   4559
gfz  191|    0    -1    -1    29    18    58  -.28   16   14 |       0     429   4440   8098
grg  123|   -4     2     1    78   -37   221   .08   36   37 |  174064    1188   4433  18228
iac  n/a|    1     1     4   -38    44   -61   .09   24   24 |  165385     652   4424   8508
mcc  n/a|    0     0    26   -46    93   199  -.12  120  120 |     ---     ---    ---    ---

Table 2.1681.6  GPS week: 1681   Day: 6   MJD: 56017                            

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]
--------+----------------------------------------------------+------------------------------
cod  261|   -1     0     1    46   -35   -86  -.21   31   31 |     ---     ---    ---    ---
emx  145|   -1    -3     0   -98   -17    11  -.30   29   26 |  164924      17   4626   7813
esx  135|    0     0     3    34    65   -92   .42   21   19 |  165305    -526   4637   4730
gfz  191|    0    -2     1   -16   -29   137  -.33   23   18 |       0    -335   4621   7795
grg  123|   -1     5    -4    18   -64   217   .03   40   41 |  225619    -675   4605  26180
iac  n/a|   -1     1    -4    -9    11   -87   .19   25   25 |  167227   -1342   4687   8268
mcc  n/a|    0     1    24    35   124   259   .24  106  106 |     ---     ---    ---    ---

       
       
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 3.1681.0  GPS week: 1681   Day: 0   MJD: 56011                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1583   15   19   16   20   20   17  ---    8 |    53   59   43   46   61   54  ---    49
 R02  | 1036   21   17   10   20   70   17  ---   11 |    63   54   47   52   46   48  ---    45
XR03  |  962   36   14   12   26  ---   17  ---   10 |    79   47   45   57  ---   48  ---    49
 R04  |  605   32   21   18   37   69   18  ---   14 |    66   36   45   63   82   36  ---    44
 R05  | 1600   33   30   12   19   36   15   77   10 |    68   48   33   43   49   49   56    43
 R06  | 2062   23   23   15   21   30   17  ---    9 |    63   52   46   55   56   40  ---    46
 R07  |  733   41   15    9   30   20   12  ---    9 |    74   49   43   50   56   45  ---    46
 R08  | 1882   24   19   10   26   27   20  166    9 |    63   55   45   58   55   41  125    46
 R09E | 1857   24   31   15   17   42   18  ---   10 |    23   24   26   33   36   21  ---    21
 R10E | 1185   30   39   20   15   37   14  ---   11 |    26   25   32   31   23   28  ---    24
 R11E | 1788   64   51   25   38   50   27  111   18 |    32   30   66   73   62   36   37    46
 R12E | 1359   18   35   21   19   36   17  ---   10 |    17   27   32   34   42   25  ---    23
 R13E | 2954   20   13   19   20   48   18  ---   10 |    22   26   30   38   47   29  ---    27
 R14E | 1032   30   44   31   20   42   27  ---   14 |    31   43   43   47   49   33  ---    34
 R15E | 2194   36   27   19   22   54   16  102   12 |    25   23   32   26   41   26   45    20
 R16E |  619   24   27   13   19   30   17  ---    9 |    28   42   38   36   43   34  ---    31
 R17  | 2018   51   22   15   19   32   17   52   11 |    52   40   25   31   29   31   54    28
 R18  | 3402   38   19   10   19   29   15   67    9 |    46   19   23   30   27   21   46    21
 R19  | 1537   34   18   10   22   16   16  ---    8 |    54   38   33   40   40   27  ---    33
 R20  | 2605   33   84   18   22   29   42  ---   18 |    42   32   25   27   31   29  ---    22
 R21  |  763   57   27   35   15   51   26  ---   15 |    72   39   52   50   35   22  ---    36
 R22  |  805   22   25   15   16   34   15  ---    9 |    55   42   24   31   24   32  ---    28
 R23  |  549   25   17   14   23   38   16  ---    9 |    35   35   20   28   35   20  ---    20
 R24  |  975   49   12   15   17   20    9  ---    9 |    34   23   27   27   29   16  ---    19
------+----------------------------------------------+------------------------------------------
 RMS  | 1707   35   32   18   22   40   20  103      |T   46   37   36   41   43   32   60    33
 WRMS | 1707   35   34   15   21   40   20  103      |NE  57   41   36   43   43   34   70    35
 MEDI | 1359   30   22   15   20   36   17   77      |MD  46   38   33   38   42   31   46    31

Table 3.1681.1  GPS week: 1681   Day: 1   MJD: 56012                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1369   13   36   26   18   40   18  ---   11 |    41   62   32   38   79   45  ---    42
 R02  | 1300   35   29   11   24   67   19  ---   12 |    42   40   28   17   41   35  ---    25
 R03  |  757   28   16    9   13   58   18  ---    9 |    54   48   47   53   73   35  ---    45
 R04  |  771   35   19   19   12   71   11  ---   11 |    51   42   26   31   73   35  ---    32
 R05  | 1567   53   22   19   20   65   14   81   12 |    48   33   27   27   55   29   33    24
 R06  | 2443   34   19   13   16   38   11  ---    8 |    42   32   30   34   49   26  ---    28
 R07  | 1347   46   16   21   16   31   18  ---   10 |    54   46   44   37   55   36  ---    39
 R08  | 2093   30   27   13   26   36   18  138   10 |    48   45   32   39   34   32   96    32
 R09E | 1561   29   29   15   20   41   20  ---   10 |    21   28   27   30   49   26  ---    20
 R10E | 2174   25   31   11   14   39   18  ---    9 |    21   28   28   21   41   21  ---    20
 R11E | 1037   46   58   33   39   69   32   92   19 |    20   34   71   66   63   38   34    45
XR12E | 1148   21   37   17   15  ---   20  ---   11 |    16   25   29   33  ---   17  ---    21
 R13E | 1647   13   23   17   19   41   21  ---    9 |    33   32   39   45   44   20  ---    30
 R14E | 1469   36   39   20   27   49   24  ---   13 |    37   33   34   47   58   35  ---    32
 R15E | 2022   23   28   25   24   44   16   57   11 |    33   24   39   23   42   32   32    25
 R16E | 1377   21   34   25   23   46   23  ---   12 |    37   34   32   37   52   35  ---    28
 R17  | 1649   53   16   18   20   50   17   69   11 |    39   41   29   48   44   30   50    32
 R18  | 3481   37   22   17   20   22   15  101    9 |    35   30   31   33   38   18   55    23
 R19  | 1442   29   23    8   18   52   19  ---   10 |    26   28   24   28   60   16  ---    18
 R20  | 3342   45   56   14   16   39   24  ---   14 |    23   49   31   32   45   37  ---    24
 R21  |  781   93   24   30   25   39   19  ---   16 |    51   27   43   50   31   16  ---    26
 R22  | 1899   41   17   15   13   48   14  ---   10 |    42   41   35   45   33   38  ---    35
 R23  |  691   29   27   15   16   36   20  ---    9 |    31   33   33   32   26   20  ---    23
 R24  | 1076   44   28   26   22   18   14  ---   11 |    38   54   31   36   35   28  ---    30
XR26  | ----  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---  159  ---   158
------+----------------------------------------------+------------------------------------------
 RMS  | 1774   40   30   19   21   47   19   93      |T   36   37   34   36   48   34   50    34
 WRMS | 1774   44   30   18   20   46   19   93      |NE  41   40   32   36   48   37   58    37
 MEDI | 1442   34   27   17   19   41   18   81      |MD  37   33   31   34   45   32   34    28

Table 3.1681.2  GPS week: 1681   Day: 2   MJD: 56013                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  750   20   42   15   24   53   18  ---   12 |    44   62   38   35   34   42  ---    35
 R02  | 1155   21   32   24   15   29   17  ---   10 |    51   53   27   45   53   40  ---    39
 R03  |  726   39   27   17   19   33   22  ---   11 |    58   50   31   37   30   33  ---    35
 R04  | 1122   24   29   13   19   46   20  ---   10 |    49   39   43   44   60   29  ---    37
 R05  |  837   43   36   20   22   96   24   85   16 |    57   45   40   43   93   34   30    36
 R06  | 2635   40   35   19   11   77   12  ---   13 |    48   53   32   34   56   31  ---    29
 R07  | 1715   47   22   32   19   29   16  ---   12 |    56   39   52   48   50   37  ---    39
 R08  | 1838   45   22   17   25   37   14  135   11 |    49   34   24   25   30   28   38    20
 R09E | 1373   19   31   28   19   61   18  ---   12 |    20   32   33   30   85   24  ---    26
 R10E | 1137   15   33   21   17   47   16  ---   10 |    27   35   20   29   55   19  ---    20
 R11E | 1745   46   55   46   30   54   28   96   18 |    27   39   72   59   68   42   31    43
 R12E | 1030   23   37   14   20   35   21  ---   10 |    18   28   25   24   32   21  ---    18
 R13E | 1515   18   26   14   15   29   18  ---    8 |    24   30   29   33   40   24  ---    24
 R14E | 1685   29   36   32   17   37   37  ---   14 |    54   64   77   71   50   45  ---    57
 R15E | 5325   20   26   17   26   16   18   65    9 |    26   25   28   31   26   31   36    20
 R16E | 1920   19   23   28   23   39   15  ---   10 |    25   30   34   39   42   32  ---    27
 R17  | 1269   43   33   25   24   36   20   67   12 |    38   54   21   43   31   39   40    33
 R18  | 3274   39   20   16   19   56   15   70   11 |    45   23   22   37   32   21   37    21
 R19  | 1171   39   19   20   18   31    9  ---    9 |    48   33   28   43   46   32  ---    31
 R20  | 4374   46   84   11   19   37   30  ---   17 |    45   38   29   35   22   21  ---    21
 R21  | 1044   88   26   21   31   39   33  ---   17 |    60   32   34   38   30   21  ---    23
 R22  | 1736   53   19   13   24   49   23  ---   12 |    49   36   27   27   56   22  ---    23
 R23  |  867   13   23   15   15   47   14  ---    9 |    31   29   39   37   29   21  ---    27
 R24  | 1012   36   20   21   17   32   19  ---   10 |    35   33   38   37   39   16  ---    27
XR26  | ----  ---  ---  ---  ---  ---    6  ---    0 |   ---  ---  ---  ---  ---   99  ---    99
------+----------------------------------------------+------------------------------------------
 RMS  | 2050   38   34   22   21   47   21   90      |T   41   39   35   38   45   32   35    32
 WRMS | 2050   38   35   21   19   43   21   90      |NE  47   40   32   38   43   33   36    33
 MEDI | 1269   36   27   19   19   37   18   70      |MD  45   35   31   37   40   31   36    27

Table 3.1681.3  GPS week: 1681   Day: 3   MJD: 56014                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1978   25   33   17   14   40   14  ---    9 |    35   50   31   35   34   30  ---    29
 R02  |  621   31   20   11   21   24   21  ---    9 |    47   43   27   31   34   35  ---    30
 R03  |  782   39   11   14   16   46   21  ---   10 |    64   47   27   46   18   48  ---    39
 R04  | 1002   40   16    9   13   33   26  ---    9 |    59   38   33   39   60   33  ---    36
 R05  |  984   29   25   11   12   79   24   91   12 |    59   39   44   40  114   33   24    42
 R06  | 3192   31   29   16   14   81   18  ---   12 |    49   46   26   35   58   49  ---    33
 R07  | 2134   37   26   17   25   59   18  ---   12 |    47   35   27   38   48   34  ---    29
 R08  | 1584   32   36   18   19   35   17  120   10 |    50   55   34   44   61   40   49    38
 R09E | 2560   21   20   17   21   54   24  ---   10 |    21   28   37   36   68   25  ---    27
 R10E | 1056   15   17   15   12   34   24  ---    8 |    32   40   34   30   44   18  ---    27
 R11E | 1593   50   67   20   32   78   34  122   18 |    31   59   50   60   81   49   30    43
 R12E |  894   23   23   10   25   29   18  ---    9 |    16   22   25   37   39   25  ---    21
 R13E | 1210   28   26   18   14   72   16  ---   11 |    40   40   41   40   71   39  ---    35
 R14E | 1362   21   41   17   17   55   18  ---   11 |    36   41   46   50   52   47  ---    42
 R15E | 5907   15   29   14   13   32   15   44    8 |    33   31   34   42   45   40   49    32
 R16E | 2272   23   15   19   18   43   17  ---    9 |    54   66   51   64   63   65  ---    56
 R17  | 1247   39   31   20   11   39   17  108   10 |    45   29   23   30   35   19   63    21
 R18  | 3127   35   16   24   14   36   26   45   10 |    42   33   33   32   30   33   62    26
 R19  |  959   41   17   29   19   75   20  ---   13 |    45   33   24   29   54   25  ---    18
 R20  | 3864   37   94   17   17   38   16  ---   17 |    44   49   22   22   28   24  ---    22
 R21  | 1702   72   21   12   17   33   39  ---   14 |    76   37   36   36   42   18  ---    29
 R22  | 1470   66   21   16   21   43   17  ---   12 |    71   54   52   62   57   39  ---    48
 R23  |  586   33   19   14   16   28   24  ---    9 |    41   35   32   34   50   20  ---    26
 R24  |  822   24   39   16   10   47   17  ---   10 |    36   51   36   36   31   32  ---    31
XR26  | ----  ---  ---  ---  ---  ---   11  ---    0 |   ---  ---  ---  ---  ---  176  ---   175
------+----------------------------------------------+------------------------------------------
 RMS  | 2158   36   34   17   18   50   22   94      |T   44   41   34   39   50   39   46    38
 WRMS | 2158   38   36   17   17   44   22   94      |NE  50   42   31   36   47   40   49    39
 MEDI | 1362   31   23   16   16   40   18   91      |MD  44   40   33   36   48   33   49    31

Table 3.1681.4  GPS week: 1681   Day: 4   MJD: 56015                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  943   16   18   13   16   41   17  ---    8 |    27   38   37   40   34   35  ---    31
 R02  |  816   39   23   18   20   24   11  ---    9 |    35   26   36   33   28   24  ---    24
 R03  |  911   35   23    8   21   28   18  ---    9 |    45   35   27   39   31   24  ---    28
 R04  | 1171   23   23   19   13   27   17  ---    8 |    43   32   21   38   47   40  ---    30
 R05  | 1238   37   21   30   10   31   17  115   10 |    48   28   22   29   50   31   43    23
 R06  | 1020   26   15   13   13   53   20  ---   10 |    41   29   32   27   39   34  ---    26
 R07  | 2095   35   19   16   20   66   15  ---   12 |    45   24   28   35   78   29  ---    28
 R08  | 2153   34   19   20   24   37   20   66   11 |    39   30   31   35   39   21   35    23
 R09E | 3051   24   20   12   15   27   23  ---    8 |    21   18   27   33   43   31  ---    21
 R10E |  984   11   20   20   16   29   20  ---    8 |    29   29   28   26   34   22  ---    23
 R11E | 1464   34   51   20   19   91   29  119   17 |    25   41   55   51  110   40   44    40
 R12E |  771   20   33   13   14   59   21  ---   11 |    19   33   29   31   52   24  ---    24
 R13E | 1781   25   25   17   21  120   37  ---   18 |    53   64   63   75  132   38  ---    60
 R14E | 1370   33   47   15   35   38   32  ---   14 |    46   50   46   69   50   44  ---    48
 R15E | 3566   21   43    8   20   28   17   68   10 |    31   40   34   41   42   29   58    31
 R16E | 2530   27   31   16   18   56   25  ---   12 |    27   56   47   47   56   43  ---    41
 R17  |  867   30   27   19   21   16   21  240   10 |    45   26   44   59   50   26  147    38
 R18  | 3853   28   20   23   14   30   18   52    9 |    37   26   29   36   23   20   91    25
 R19  |  759   27   47   26   14   28   17  ---   12 |    41   54   20   41   38   31  ---    30
 R20  | 2096   75   77   25   29   43   52  ---   22 |    46   19   41   42   38   25  ---    20
 R21  | 1846   80   21   21   24   52   25  ---   16 |    59   24   23   26   46   26  ---    19
 R22  | 1226   44   19   14   17   26   14  ---    9 |    57   38   44   40   40   28  ---    36
 R23  |  640   33   18   18   18   19   14  ---    8 |    40   32   36   31   27   20  ---    26
 R24  |  573   38   25   28   12   21   16  ---   10 |    37   41   27   20   16   18  ---    15
XR26  | ----  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---  139  ---   138
------+----------------------------------------------+------------------------------------------
 RMS  | 1811   36   32   19   19   48   23  127      |T   39   34   34   39   47   33   69    33
 WRMS | 1811   34   34   18   21   41   23  127      |NE  42   31   31   35   39   33   79    32
 MEDI | 1226   30   23   18   18   30   18   68      |MD  40   32   31   36   40   29   44    28

Table 3.1681.5  GPS week: 1681   Day: 5   MJD: 56016                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  738   17   18   10   11   42   25  ---    9 |    23   26   45   41   46   41  ---    35
 R02  |  862   25   19   11   18   25   23  ---    8 |    31   17   30   28   26   27  ---    21
 R03  |  834   45   17   14   15   21   12  ---    8 |    39   25   22   24   25   23  ---    20
 R04  | 1631   31   23   12   11   43   18  ---    9 |    37   45   26   38   48   32  ---    31
 R05  | 1015   33   23   19   11   30   20  142    9 |    37   22   26   30   38   37   33    26
 R06  | 1393   25   24    9   12   35   13  ---    8 |    34   26   31   28   26   29  ---    24
 R07  | 1456   21   24   14   21   67   38  ---   13 |    31   38   39   44   61   22  ---    29
 R08  | 2250   34   29   18   17   39   21   65   10 |    36   32   30   42   55   28   40    29
 R09E | 2426   26   33   17   19   21   25  ---   10 |    14   32   39   35   42   27  ---    26
 R10E | 2900   27   19   12   14   41   21  ---    9 |    31   35   30   38   38   22  ---    28
 R11E | 2081   63   43   34   20   34   36  105   16 |    32   44   72   63   49   37   56    49
 R12E | 1089   17   27   14   19   26   17  ---    8 |    20   29   23   33   35   24  ---    22
 R13E | 2337   23   31   11   18   35   20  ---    9 |    37   57   40   50   71   27  ---    41
 R14E | 3268   24   43   11   10   57   39  ---   13 |    32   33   33   42   52   36  ---    32
 R15E | 2027   33   40   15   11   35   24  113   11 |    27   29   27   25   33   27   83    20
 R16E | 2092   32   36   15   15   31   20  ---   10 |    47   48   55   53   56   45  ---    47
 R17  | 1298   32   21   16   11   30   14   54    8 |    39   41   14   33   26   35  103    25
 R18  | 2082   31   16   23   12   36   23  188   10 |    34   31   29   27   24   34   91    25
 R19  | 1511   21   34   13   10   30   24  ---    9 |    36   39   35   32   40   23  ---    30
 R20  | 2167   35   49   18   18   40   43  ---   14 |    37   53   36   41   27   47  ---    31
 R21  | 1426   86   32   25   33   47   25  ---   17 |    64   23   40   53   30   27  ---    31
 R22  |  577   36   22   17   12   20   16  ---    8 |    58   51   45   56   58   46  ---    48
 R23  |  550   30   16    9   12   24   15  ---    7 |    39   24   26   27   24   17  ---    22
 R24  |  688   31   17   10   15   22   16  ---    7 |    29   32   24   32   31   23  ---    25
XR26  | ----  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---   96  ---    98
------+----------------------------------------------+------------------------------------------
 RMS  | 1772   35   29   16   16   36   24  120      |T   35   34   34   38   40   33   67    32
 WRMS | 1772   32   28   15   14   37   24  120      |NE  37   32   31   36   36   34   66    32
 MEDI | 1456   31   24   14   14   34   21  105      |MD  34   32   30   35   38   28   56    29

Table 3.1681.6  GPS week: 1681   Day: 6   MJD: 56017                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  emx  esx  gfz  grg  iac  mcc  IGL |   cod  emx  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  | 1248   13   20   14   35   62   23  ---   12 |    33   44   36   58   46   36  ---    35
 R02  | 1118   25   28   23   20   48   27  ---   12 |    43   29   26   26   44   31  ---    24
 R03  |  487   49   16   27   21   35   18  ---   12 |    53   31   40   31   38   26  ---    27
 R04  | 1215   30   17   26   22   32   23  ---   11 |    50   38   29   44   34   33  ---    31
 R05  | 1701   32   20   12   15   43   16  156   10 |    60   40   30   36   33   36   26    34
 R06  | 2771   22   16   21   16   39   19  ---    9 |    48   36   34   35   26   37  ---    32
 R07  | 1810   28   28   14   19   37   23  ---   10 |    47   44   32   37   29   36  ---    31
 R08  | 1899   22   19   16   23   49   26   62   11 |    48   38   34   47   60   41   39    36
 R09E | 1004   19   28   19   21   40   26  ---   11 |    18   32   38   42   49   26  ---    30
 R10E | 2040   29   24   15   21   49   16  ---   11 |    42   48   40   29   66   52  ---    41
 R11E | 3285   34   48   31   42   53   27   96   17 |    31   46   57   60   45   37   37    42
 R12E |  875   15   22   14   21   45   16  ---    9 |    17   25   26   32   45   22  ---    21
 R13E | 2319   16   26   17   20   26   36  ---   11 |    32   38   31   25   33   44  ---    27
 R14E | 2670   18   38   23   22   50   37  ---   14 |    37   45   35   48   64   38  ---    35
 R15E | 2759   26   32   10   29   30   22   88   11 |    26   25   28   41   39   34   47    25
 R16E |  990   24   21   16   20   21   13  ---    8 |    26   27   31   36   40   36  ---    29
 R17  | 1968   42   22   17   20   29   14   58   10 |    71   40   34   34   36   48   71    40
 R18  | 1803   51   27   30   25   21   22  140   13 |    55   44   26   33   14   32   45    24
 R19  |  903   24   10   12   15   37   18  ---    8 |    52   48   30   42   25   44  ---    37
 R20  | 1138   42   74   19   23   36   44  ---   19 |    48   38   44   46   31   44  ---    36
 R21  | 1125   52   20   39   24   48   24  ---   15 |    84   39   60   74   41   35  ---    50
 R22  |  802   37   21   30   14   47   33  ---   13 |    77   52   53   53   28   37  ---    47
 R23  |  569   23   16   14   18   41   16  ---    9 |    55   32   46   52   38   30  ---    39
 R24  |  743   31   25   23   23   12   21  ---   10 |    51   39   45   40   39   26  ---    36
XR26  | ----  ---  ---  ---  ---  ---    6  ---    0 |   ---  ---  ---  ---  ---   81  ---    81
------+----------------------------------------------+------------------------------------------
 RMS  | 1730   31   29   21   23   40   25  106      |T   46   38   36   41   39   37   44    35
 WRMS | 1730   31   26   19   18   41   25  106      |NE  54   39   37   43   35   38   45    37
 MEDI | 1215   26   22   17   21   39   22   88      |MD  48   38   34   40   38   36   39    35




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