[IGSREPORT-20074] Wk 1648 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Aug 25 10:40:14 PDT 2011


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1648   (Aug 07, 2011 - Aug 13, 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 2.1648.
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:
                                                                               
 igl1648[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1648 in the SP3 format.
 igl16487.sum      Combination Report for GPS Week 1648.


    
    
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).

 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  |    161.7 ns
                1  |    162.0 ns
                2  |    162.3 ns
                3  |    163.4 ns
                4  |    159.0 ns
                5  |    158.3 ns
                6  |    159.9 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 1.1648, 1a.1648).
        
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 2.1648.0-6)                                                                                
    
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 3.1648.0-6). 
        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 1648 summary.                      (Aug 07, 2011 - Aug 13, 2011)

Table 1.1648.a     GPS week : 1648   MJD: 55780.0-55786.0

         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  250|   -1     0     0    37   -11    13  -.16   25   26 |     ---     ---    ---    ---
        |    1     1     3    22    24    32   .04           |     ---     ---
esx  130|    0    -1    11   -14    -2   -31   .40   21   20 |  161542   -2651   4930   5440
        |    1     1     2    36    23    30   .05           |    2960    3649
gfz  192|   -1     0     3   -38   -24    47  -.21   22   19 |       0   -1463   4964   9942
        |    2     1     4    33    36    27   .04           |       0    3019
grg  129|    1     2    -7     1    31    99   .18   53   51 |     ---     ---    ---    ---
        |    5     3     4    50    36    47   .14           |     ---     ---
iac  n/a|    1     0   -14    17    30   -66  -.17   24   24 |  162432    -633   4878   9864
        |    2     1     6    44    18    57   .01           |    2550    1571
mcc  n/a|    0     3    -2   109    58  -113  -.14  131  131 |     ---     ---    ---    ---
        |   13    10    20   156   210   410   .40           |     ---     ---


Table 1.1648.b     GPS week : 1648   MJD: 55780.0-55786.0   

         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  |   13   15   16   10   12   11   15 |
 R02  |   14   12   10   12   13   13   13 |
 R03  |   11   10   13   15   11   10   14 |
 R04  |   21   46   29   37   37   56    0 |
 R05  |   14   13   16   13   14   11   13 |
 R06  |   11   12   12    9   10   13   13 |
 R07  |   14   10   14   13   10   13   13 |
 R08  |   12   14   15   12   11   12   13 |
 R09  |   14   14   12   12   10   11   13 |
 R10  |    9   12   12   12   10   10    9 |
 R11  |   19   16   15   17   16   16   20 |
 R12  |   16    9    9   10   13   12   13 |
 R13  |   14    9   15   14   13   13   14 |
 R15  |   10   13   12   24   15   12   12 |
 R16  |   11   11   12   13   15   16   15 |
 R17  |   16   17   19   16   15   19   20 |
 R18  |   12   12   13   20   11   14   11 |
 R19  |    9   16   11   12   11   11   11 |
 R20  |   14   19   19   20   13   13   15 |
 R21  |   13   11   12   14   14   11    9 |
 R22  |   18   11   11   11   14   13   10 |
 R23  |   19   14    9   11   10   13   11 |
 R24  |   13   20   15   14   12   14   16 |


Table 1.1648.c     GPS week : 1648   MJD: 55780.0-55786.0   

         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 1648 0   |   76    30   390    -254   -1202   -8784  88.5  1608  1608 |  161728       0
brd 1648 1   |   16    68   386    -680    1633   -6122  87.3  1648  1648 |  162001       0
brd 1648 2   |  -14    53   289     433      10   -1908  86.3  1752  1752 |  162314       0
brd 1648 3   |  -52    55   297     126   -2090    -544  83.8  1548  1548 |  163370       0
brd 1648 4   |  -22   -34   282     375   -2472   -7074  87.0  2138  2138 |  158971       0
brd 1648 5   |  -37   -42   154     853      22   -6213  87.3  1970  1970 |  158332       0
brd 1648 6   |   21    52   222     443     329   -4616  85.7 >>>>> >>>>> |  159939       0
-------------+------------------------------------------------------------+----------------
brd 1648 mean|   -1    26   289     185    -538   -5037  86.6 43723 43723 |  160950       0
brd 1648 sdev|   43    45    84     509    1453    2912   1.5 >>>>> >>>>> |    1880       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 2.1648.0  GPS week: 1648   Day: 0   MJD: 55780                            

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  250|    0    -2     4    71   -17    20  -.12   29   28 |     ---     ---    ---    ---
esx  130|    0     0    11   -39   -21   -38   .44   21   20 |  163541   -4634   4596   4768
gfz  192|   -1     1     0   -69     0    87  -.19   23   20 |       0   -1801   4655   8745
grg  129|   -3     5    -8    96   -14    96  -.02   56   54 |     ---     ---    ---    ---
iac  n/a|    1    -2   -12    17    34   -97  -.17   22   22 |  162757   -1071   4594   8869
mcc  n/a|   -2     1   -31    64  -187   198  -.14  156  156 |     ---     ---    ---    ---

Table 2.1648.1  GPS week: 1648   Day: 1   MJD: 55781                            

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  250|    0     0     0    57   -48    48  -.14   29   28 |     ---     ---    ---    ---
esx  130|   -1     0     6   -52   -25     0   .38   24   22 |  161801   -2544   5265   5428
gfz  192|   -2     0     2   -29    36    29  -.16   20   18 |       0   -1830   5484   9134
grg  129|   -2     7   -13    15   -14   177   .15   50   48 |     ---     ---    ---    ---
iac  n/a|    3     0    -4    61     6   -85  -.15   23   23 |  163353     677   5313   9220
mcc  n/a|   -3     5    -1   195  -183   303   .48  118  118 |     ---     ---    ---    ---

Table 2.1648.2  GPS week: 1648   Day: 2   MJD: 55782                            

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  250|   -1    -1    -1     9   -14   -38  -.15   24   24 |     ---     ---    ---    ---
esx  130|    0     0     9   -21   -15   -27   .50   20   18 |  161182     228   5310   5546
gfz  192|    0     1    -1   -49   -15    72  -.25   21   16 |       0    1400   5403  15016
grg  129|    2    -3    -5     0    31    99   .08   56   54 |     ---     ---    ---    ---
iac  n/a|    5     0    -9    75    24   -31  -.16   28   28 |  165349    1571   5303  14515
mcc  n/a|    5     1     2   -35   242   268  -.27  108  108 |     ---     ---    ---    ---

Table 2.1648.3  GPS week: 1648   Day: 3   MJD: 55783                            

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  250|   -2     0    -5    20    19   -23  -.17   26   25 |     ---     ---    ---    ---
esx  130|    1     0    12   -27     2   -86   .33   21   18 |  166630   -6453   5482   5897
gfz  192|   -6     0     4    -8   -76    65  -.16   24   23 |       0   -3087   5221   7372
grg  129|   11     0    -9   -73    30    32   .14   54   52 |     ---     ---    ---    ---
iac  n/a|    4     2   -12    43    28    11  -.18   24   24 |  165329   -2521   5094   7672
mcc  n/a|   24   -11   -23    27   113  -614  -.68  117  117 |     ---     ---    ---    ---

Table 2.1648.4  GPS week: 1648   Day: 4   MJD: 55784                            

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  250|   -2     0     1    31    20    16  -.25   24   26 |     ---     ---    ---    ---
esx  130|    0    -1    12    21   -18   -42   .42   18   18 |  161255   -5466   4449   4565
gfz  192|    0    -1    -2   -36   -29    15  -.24   19   18 |       0   -4449   4535   8520
grg  129|    5     1     1     2    54   136   .19   54   51 |     ---     ---    ---    ---
iac  n/a|    1    -2   -17   -25    60   -44  -.19   23   23 |  161355   -1878   4442   7994
mcc  n/a|  -10    10    -7   421   239  -313   .22  122  122 |     ---     ---    ---    ---

Table 2.1648.5  GPS week: 1648   Day: 5   MJD: 55785                            

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  250|    0     2     4    21    -9    43  -.15   23   24 |     ---     ---    ---    ---
esx  130|    1    -3    13   -27    22     6   .39   22   19 |  158186   -3692   5289   5502
gfz  192|   -2     1     8     9   -48    23  -.22   21   17 |       0   -4221   5290  10139
grg  129|   -2     2    -9    -6    52    95   .43   51   51 |     ---     ---    ---    ---
iac  n/a|    0     0   -22   -24    42  -168  -.16   23   23 |  158411   -1815   5256   9837
mcc  n/a|    0    -2    12    92   286    11  -.03  128  128 |     ---     ---    ---    ---

Table 2.1648.6  GPS week: 1648   Day: 6   MJD: 55786                            

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  250|    0     0     0    49   -28    27  -.14   23   24 |     ---     ---    ---    ---
esx  130|   -1     0    11    48    35   -33   .37   24   21 |  158202    3999   4120   6377
gfz  192|    1     0     9   -86   -35    39  -.23   24   24 |       0    3744   4160  10668
grg  129|    0     3    -8   -21    84    58   .26   49   49 |     ---     ---    ---    ---
iac  n/a|   -2     1   -22   -28    12   -49  -.18   26   26 |  160474     605   4148  10945
mcc  n/a|  -17    21    29     1  -101  -649  -.52  166  166 |     ---     ---    ---    ---

       
       
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 3.1648.0  GPS week: 1648   Day: 0   MJD: 55780                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1739   27   25   17   57   19  ---   13 |    54   87   67   42   68  ---    66
 R02  |  702   23   11   24   68   21  ---   13 |    57   44   52   36   56  ---    47
 R03  | 1695   16   15   22   37   24  ---   10 |    26   29   35   23   27  ---    24
XR04E | 3881   33   25  ---   85   23  ---   21 |    32   68  ---    4   47  ---    47
 R05  | 1403   44   17   19   55   17  ---   14 |    75   48   48   43   52  ---    49
 R06  | 1041   25    7   21   50   11  ---   10 |    57   49   48   46   53  ---    47
 R07  | 1183   23   26   15   60   23  ---   13 |    58   56   58   29   59  ---    54
 R08  | 3618   17   24   16   63   13  160   12 |    55   69   48   31   51   27    51
 R09  | 1448   40   15   29   37   23  ---   14 |    27   35   36   41   30  ---    25
 R10  |  965   14   15   20   28   16  ---    9 |    16   28   31   45   21  ---    21
 R11  | 1035   57   38   34   40   23  131   19 |    36   69   56   42   45   41    42
 R12  | 1478   39   21   26   65   24  ---   16 |    27   46   43   48   28  ---    30
 R13  | 1750   29   27   23   37   26  ---   13 |    26   48   39   29   32  ---    30
 R15  | 1763   19   10   19   47   18  173   10 |    23   22   36   40   23   32    21
 R16  | 1065   22   14   16   34   25  ---   10 |    28   32   30   29   33  ---    23
 R17E | 2566   32   34   19   38   38  ---   16 |    25   46   39   54   35  ---    31
 R18E | 1019   23   26   20   40   22  ---   12 |    31   50   47   38   35  ---    36
 R19E | 1944   15   15   19   30   15  ---    9 |    67   78   72   70   65  ---    69
 R20E | 1597   27   25   25   39   27  ---   13 |    58   57   64   61   50  ---    53
 R21E | 1007   20   14   31   43   24  ---   12 |    25   36   39   35   27  ---    27
 R22E | 1197   26   22   26  100   19  ---   17 |    26   44   43   62   27  ---    28
 R23E | 1076   29   14   19  118   17  ---   18 |    17   32   31  104   19  ---    23
 R24E | 1340   23   23   25   44   25  ---   13 |    26   55   57   45   26  ---    37
------+-----------------------------------------+-------------------------------------
 RMS  | 1608   29   21   23   56   22  156      |T   37   49   46   43   39   33    38
 WRMS | 1608   28   20   20   54   22  156      |NE  40   47   44   37   41   33    37
 MEDI | 1403   25   21   20   44   23  160      |MD  28   48   43   42   35   32    36

Table 3.1648.1  GPS week: 1648   Day: 1   MJD: 55781                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1119   24   34   13   71   12  ---   14 |    32   61   42   35   28  ---    37
 R02  |  857   21   16   19   39   27  ---   11 |    34   20   20   32   45  ---    24
 R03  | 2817   22   21   17   28   19  ---   10 |    16   38   31   40   20  ---    21
XR04E | 3470   65   90  ---  ---   34  ---   46 |    33  106  ---  ---   36  ---    54
 R05  | 1389   34   27   16   49   17  ---   13 |    54   32   46   51   29  ---    34
 R06  | 1036   29   13   16   54   12  ---   11 |    42   27   27   26   28  ---    23
 R07  | 1641   15   14   17   46   14  ---   10 |    34   43   48   31   31  ---    35
 R08  | 1901   17   17   25   49   31  133   13 |    33   30   44   30   15   24    23
 R09  | 1145   37   21   24   31   28  ---   14 |    25   26   38   26   20  ---    19
 R10  |  944   20   19   23   39   25  ---   12 |    19   22   36   35   23  ---    19
 R11  |  889   53   38   14   42   17  134   16 |    19   56   40   42   36   33    32
 R12  | 1374   24   19   14   21   16  ---    9 |    17   26   16   34   25  ---    16
 R13  | 1982   25   20   13   27   12  ---    9 |    15   26   20   28   20  ---    12
 R15  | 1002   26   12   16   67   15   78   13 |    14   19   21   64   23   16    14
 R16  | 1067   32   21   16   27   15  ---   11 |    20   31   25   22   18  ---    17
 R17E | 4144   42   32   18   60   30  ---   17 |    26   41   29   50   30  ---    24
 R18E | 1033   27   18   21   42   22  ---   12 |    29   48   57   46   33  ---    39
 R19E | 1104   29   22   26   59   32  ---   16 |    59   83   83   96   56  ---    71
 R20E | 1615   31   35   34   52   39  ---   18 |    47   82   75   50   42  ---    57
 R21E | 1222   15   22   20   28   21  ---   10 |    17   40   35   35   18  ---    23
 R22E | 1793   19   16   22   29   21  ---   10 |    22   42   47   42   26  ---    30
 R23E | 1181   30   22   21   55   22  ---   14 |    13   35   29   45   22  ---    19
 R24E | 1173   23   33   16  107   22  ---   19 |    15   44   39   98   20  ---    26
------+-----------------------------------------+-------------------------------------
 RMS  | 1648   29   24   20   50   23  118      |T   27   42   38   43   28   24    29
 WRMS | 1648   28   22   18   48   23  118      |NE  26   32   32   35   25   24    23
 MEDI | 1181   26   21   17   42   21  133      |MD  25   38   36   35   26   24    24

Table 3.1648.2  GPS week: 1648   Day: 2   MJD: 55782                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  865   26   26   26   70   30  ---   16 |    43   75   77   52   39  ---    57
 R02  | 1063   23   15   10   43   22  ---   10 |    46   51   39   42   34  ---    40
 R03  | 2975   17   17   26   53   28  ---   13 |    23   27   26   36   18  ---    16
XR04E | 5487   32   48  ---  ---   37  ---   28 |    25   75  ---  ---   49  ---    55
 R05  |  603   29   28   29   74   19  ---   16 |    55   63   45   57   53  ---    48
 R06  | 1290   22   14   15   59   26  ---   12 |    58   45   48   54   58  ---    48
 R07  | 2058   17   22   14   83   23  ---   14 |    47   58   45   51   45  ---    45
 R08  | 1707   21   29    9   70   33  121   14 |    44   53   29   46   30   23    33
 R09  | 1037   35   16   14   41   17  ---   11 |    27   36   34   35   26  ---    26
 R10  | 1065   12   17   16   55   29  ---   11 |    14   34   34   61   15  ---    24
 R11  |  976   34   20   22   45   35  133   14 |    17   42   41   34   39   21    28
 R12  | 1478   15   14   11   40   16  ---    8 |    21   23   32   38   29  ---    23
 R13  | 1590   25   18   29   50   37  ---   15 |    20   31   28   26   37  ---    19
 R15  | 1744   22   16   20   48   22   56   11 |    18   32   34   38   17   18    20
 R16  | 1124   28   11   24   46   18  ---   12 |    16   31   28   58   25  ---    21
 R17E | 3976   44   23   32   76   31  ---   18 |    24   45   41   88   40  ---    31
 R18E |  729   18   16   24   55   29  ---   12 |    27   41   37   48   35  ---    29
 R19E | 1350   19   17   17   48   24  ---   11 |    37   53   57   77   40  ---    45
 R20E |  893   22   36   25   37   57  ---   18 |    57   89   71   69   39  ---    61
 R21E | 1192   20   19   22   50   18  ---   11 |    18   32   50   43   22  ---    28
 R22E | 2314   22   16   16   41   26  ---   11 |    26   47   42   52   28  ---    33
 R23E |  670   13   15   19   38   16  ---    9 |    22   29   20   44   26  ---    21
 R24E | 3039   22   17   25   77   24  ---   14 |    33   37   54   89   31  ---    37
------+-----------------------------------------+-------------------------------------
 RMS  | 1752   24   20   21   56   28  108      |T   31   45   41   51   33   20    34
 WRMS | 1752   24   18   16   54   28  108      |NE  32   42   38   44   33   20    32
 MEDI | 1290   22   17   20   50   26  121      |MD  26   42   39   48   34   21    31

Table 3.1648.3  GPS week: 1648   Day: 3   MJD: 55783                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1133    9    7   23   46   21  ---   10 |    41   51   64   34   40  ---    45
 R02  |  775   18   17   13   57   25  ---   12 |    52   57   57   61   37  ---    48
 R03  | 1676   22   18   24   80   18  ---   14 |    17   31   29   64   27  ---    20
XR04E | 3122   31   62  ---  ---   51  ---   36 |    29   76  ---  ---   48  ---    44
 R05  |  879   31   22   14   53   17  ---   12 |    59   57   38   61   38  ---    43
 R06  | 1516   17   12   18   40   14  ---    9 |    49   47   59   34   44  ---    46
 R07  | 1819   20   10   16   70   20  ---   12 |    56   50   45   55   61  ---    49
 R08  | 1333   12   24   24   56   10  146   11 |    46   67   36   30   46   44    45
 R09  |  837   31   14   16   54   19  ---   12 |    27   38   33   72   27  ---    28
 R10  | 1141   23   11   30   36   25  ---   12 |    13   28   49   34   25  ---    21
 R11  |  896   41   23   28   55   31   76   16 |    22   44   49   53   48   42    34
 R12  | 1145   26   14   18   37   14  ---   10 |    28   19   26   30   19  ---    16
 R13  | 1340   37   20   25   49   20  ---   14 |    26   46   35   28   34  ---    29
XR15  |>>>>>   37  ---   26  101   17  110   23 |    25  ---   31   65   33   23    17
 R16  | 1307   31   22   20   49   20  ---   13 |    23   44   48   53   27  ---    29
 R17E | 3709   32   18   20   78   30  ---   16 |    21   47   49   78   37  ---    35
 R18E |  961   29   48   35   71   29  ---   20 |    36   61   47   58   48  ---    37
 R19E | 1208   22   22   18   47   21  ---   12 |    38   52   44   53   38  ---    40
 R20E | 1957   36   29   41   44   47  ---   19 |    71   74   82   68   52  ---    61
 R21E |  939   30   25   24   44   24  ---   13 |    27   35   36   42   24  ---    23
 R22E | 2299   16   14   21   50   21  ---   11 |    24   34   38   64   40  ---    30
 R23E | 1138   15   19   23   33   23  ---   10 |    13   25   35   31   20  ---    19
XR24E | 6040   24   22   29  ---   21  ---   14 |    29   36   50  ---   23  ---    30
------+-----------------------------------------+-------------------------------------
 RMS  | 1547   26   21   24   54   24  117      |T   33   46   44   50   36   36    34
 WRMS | 1547   25   18   23   52   24  117      |NE  34   44   42   48   36   36    33
 MEDI | 1307   26   19   23   50   21  110      |MD  28   46   44   53   37   42    34

Table 3.1648.4  GPS week: 1648   Day: 4   MJD: 55784                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1178   19   27   12   43   27  ---   12 |    34   65   33   42   40  ---    41
 R02  |  922   29   17   26   62   12  ---   13 |    39   23   24   55   22  ---    21
 R03  | 1243   17   20   15   54   15  ---   10 |    19   26   28   39   25  ---    18
XR04E | 2737   56   56  ---  ---   40  ---   36 |    40   60  ---  ---   53  ---    50
 R05  |  881   34   13   17   68   21  ---   13 |    37   31   29   47   28  ---    24
 R06  | 1431   19   16   13   51   17  ---   10 |    39   54   42   50   33  ---    39
 R07  | 3503   15   12   16   46   20  ---    9 |    56   51   41   52   55  ---    48
 R08  | 1155   13   12   14   49   27  143   10 |    48   36   37   64   60   27    43
 R09  |  901   26   14   11   30   18  ---    9 |    27   37   40   41   36  ---    32
 R10  |  807   16   13   19   35   20  ---    9 |    13   28   23   37   27  ---    19
 R11  | 1052   38   18   33   50   25   96   15 |    13   38   33   39   38   61    24
 R12  | 1352   22   16   27   62   20  ---   13 |    29   36   43   59   23  ---    28
 R13  | 1011   36   13   19   41   26  ---   12 |    27   31   33   39   36  ---    26
XR15  | 5284   16   25   18  ---   36  107   14 |    18   37   34  ---   36   46    23
 R16  | 1583   36   28   16   58   22  ---   14 |    24   45   36   41   24  ---    26
 R17E | 3159   27   22   27   39   36  ---   14 |    17   36   45   39   33  ---    26
 R18E | 1371   21   16   18   48   18  ---   10 |    23   41   41   60   28  ---    30
 R19E |  807   17   15   16   52   18  ---   10 |    32   44   48   45   38  ---    39
 R20E | 1143   22   23   19   61   23  ---   13 |    45   43   56   87   49  ---    46
 R21E |  819   22   20   11   79   21  ---   13 |    19   35   30   55   19  ---    22
 R22E | 1511   17   22   17   70   33  ---   14 |    21   41   44   56   37  ---    31
 R23E |  908   14   14   18   32   23  ---    9 |    17   31   37   35   22  ---    23
 R24E | 7089   19   23   16   63   19  ---   12 |    21   45   35   37   25  ---    25
------+-----------------------------------------+-------------------------------------
 RMS  | 2138   24   18   19   54   23  122      |T   28   39   36   48   34   44    30
 WRMS | 2138   26   18   18   51   23  122      |NE  30   38   34   46   34   44    29
 MEDI | 1178   21   17   17   51   21  107      |MD  27   37   36   45   33   46    26

Table 3.1648.5  GPS week: 1648   Day: 5   MJD: 55785                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1448   17   22   15   34   24  ---   10 |    36   60   42   46   46  ---    44
 R02  |  865   28   14   19   63   21  ---   13 |    38   23   30   34   24  ---    23
 R03  | 1706   15   15   15   50   17  ---   10 |    20   20   21   34   21  ---    17
XR04E | 5761   52  ---  ---  ---   58  ---   55 |    56  ---  ---  ---   57  ---    57
 R05  | 1266   20   21    9   53   18  ---   11 |    32   44   30   38   28  ---    30
 R06  | 1451   20   14   18   64   21  ---   12 |    31   31   43   41   42  ---    33
 R07  | 3821   12   23   24   60   21  ---   12 |    37   47   51   30   33  ---    36
 R08  | 2115   10   12   15   66   20  157   11 |    36   44   42   52   45   37    39
 R09  | 1485   31   10   14   31   20  ---   10 |    23   38   44   45   39  ---    34
 R10  | 1133   14   16   19   41   17  ---    9 |    18   27   43   39   23  ---    24
 R11  |  765   44   23   27   38   29   91   16 |    11   36   29   51   39   44    24
 R12  |  984   24   13   10   52   29  ---   12 |    24   24   23   55   28  ---    21
 R13  | 1188   28   25   24   44   15  ---   13 |    22   31   27   30   15  ---    17
XR15  | 3330   21   11   14  ---   32   98   12 |    15   18   16  ---   28   22    13
 R16  | 1164   32   26   36   44   27  ---   16 |    33   36   48   32   27  ---    24
 R17E | 3704   30   36   37   52   39  ---   18 |    22   45   56   39   26  ---    27
 R18E | 1775   15   19   20   71   24  ---   13 |    24   44   41   70   32  ---    33
 R19E |  942   18   15   22   48   19  ---   11 |    54   58   62   61   56  ---    56
 R20E |  948   21   25   22   46   25  ---   13 |    27   49   49   44   43  ---    37
 R21E | 1780   19   20   16   40   19  ---   10 |    17   30   29   54   18  ---    17
 R22E |  706   24   17   21   58   19  ---   12 |    21   37   44   88   39  ---    34
 R23E |  831   15   29   18   40   29  ---   12 |    11   39   35   39   24  ---    21
 R24E | 4704   23   35   18   44   21  ---   13 |    28   52   34   40   25  ---    24
------+-----------------------------------------+-------------------------------------
 RMS  | 1970   23   22   21   51   23  128      |T   27   37   38   45   32   34    29
 WRMS | 1970   24   19   17   51   23  128      |NE  26   34   34   40   31   34    27
 MEDI | 1448   21   19   18   48   21   98      |MD  24   37   41   41   28   37    27

Table 3.1648.6  GPS week: 1648   Day: 6   MJD: 55786                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1304   21   17   13   74   35  ---   15 |    49   83   71   55   82  ---    66
 R02  |  765   14   24   13   61   22  ---   12 |    57   44   47   43   54  ---    47
 R03  | 1363    9   14   25   61   35  ---   13 |    26   31   39   34   28  ---    25
XR04E | ----  ---  ---  ---  ---   11  ---    0 |   ---  ---  ---  ---   65  ---    94
 R05  |  838   26   14   21   60   19  ---   13 |    65   60   68   41   46  ---    53
 R06  |  914   13   29   23   45   25  ---   13 |    49   67   48   32   42  ---    45
 R07  | 1228   27   20   29   34   26  ---   13 |    58   52   43   37   46  ---    46
 R08  | 1869   11   20   13   66   22  244   12 |    45   60   49   39   39   29    44
 R09  |  784   30   22   24   18   24  ---   12 |    35   52   44   41   41  ---    38
 R10  |  891   13   11   24   27   19  ---    9 |    19   30   30   34   32  ---    25
 R11  |  970   49   46   29   44   25  127   20 |    25   76   54   43   42   58    41
 R12  | 1039   21   16   25   39   30  ---   12 |    30   42   54   33   34  ---    33
 R13  | 1481   23   19   34   36   29  ---   13 |    31   39   63   33   29  ---    33
 R15  | 4003   18   12   21   39   32   87   11 |    27   30   39   39   25   24    25
 R16  | 1239   33   27   35   33   21  ---   15 |    42   46   34   38   31  ---    32
 R17E | 4518   32   48   31   66   34  ---   20 |    26   54   41   58   29  ---    29
 R18E | 1488   16   19   20   35   25  ---   11 |    30   38   40   47   34  ---    32
 R19E | 1062   15   17   22   43   20  ---   11 |    49   57   59   60   45  ---    50
 R20E | 1540   24   23   26   62   28  ---   15 |    36   51   53   78   47  ---    43
 R21E | 1774   13   13   13   39   17  ---    9 |    23   32   32   46   32  ---    28
 R22E |  905   20   18   13   26   26  ---   10 |    36   49   41   46   38  ---    39
 R23E | 1422   10   20   21   46   22  ---   11 |    24   32   39   37   33  ---    27
 R24E |>>>>>   20   35   23   64   30  ---   16 |    27   43   37   54   31  ---    30
------+-----------------------------------------+-------------------------------------
 RMS  |>>>>>   23   24   24   49   26  166      |T   36   48   46   44   40   37    40
 WRMS |>>>>>   24   21   24   49   26  166      |NE  39   50   48   38   40   37    39
 MEDI | 1239   20   19   23   43   25  127      |MD  31   46   43   41   38   29    38




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