[IGSREPORT-20092] Wk 1649 IGLOS Final Orbits

Jim Ray igs.acc at noaa.gov
Thu Sep 1 06:36:36 PDT 2011


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1649   (Aug 14, 2011 - Aug 20, 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 2.1649.
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:
                                                                               
 igl1649[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1649 in the SP3 format.
 igl16497.sum      Combination Report for GPS Week 1649.


    
    
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  |    162.3 ns
                1  |    164.7 ns
                2  |    168.7 ns
                3  |    168.0 ns
                4  |    168.5 ns
                5  |    169.4 ns
                6  |     -0.4 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
               ----+--------+---------------
                0  |  GRG   | R24
                1  |  ESX   | R24
                6  |  GRG   | R07

    
         
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 1.1649, 1a.1649).
        
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 2.1649.0-6)                                                                                
    
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 3.1649.0-6). 
        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 1649 summary.                      (Aug 14, 2011 - Aug 20, 2011)

Table 1.1649.a     GPS week : 1649   MJD: 55787.0-55793.0

         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  248|   -1     0    -2    44   -12    11  -.16   27   26 |     ---     ---    ---    ---
        |    2     2     3    19    34    46   .03           |     ---     ---
esx  136|    0    -1    11     3    56    -5   .38   23   20 |  145752   -4859  10651  10850
        |    2     1     2    27    30    34   .05           |   65227   11320
gfz  190|    0     0     5   -20   -26    65  -.19   23   21 |       0    -423   5712   8800
        |    1     1     2    36    35    35   .04           |       0    2920
grg  128|    0     0    -9    -8    -5    69   .16   75   50 |     ---     ---    ---    ---
        |    3     3     4    53    44   141   .16           |     ---     ---
iac  n/a|    0     0   -12    -3    -8   -99  -.19   23   23 | 1014214    -991   6543 162301
        |    1     0     6    32    12    87   .04           | 2303774    1958
mcc  n/a|   -1     4     6    86    27  -402  -.27  110  110 |     ---     ---    ---    ---
        |   14     9    15   122   120   295   .33           |     ---     ---


Table 1.1649.b     GPS week : 1649   MJD: 55787.0-55793.0   

         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   11   13   13    8   13   13 |
 R02  |   19   14   17   12   14   15   12 |
 R03  |   12   12   10   11   12    9   10 |
 R04  |  ---  ---  ---    0   15   19   16 |
 R05  |   12   16   16   14   12   12    9 |
 R06  |   11   10   12   12   12   11   13 |
 R07  |   14   13   16   14   17   13   13 |
 R08  |   11    9   13   11   13   12   10 |
 R09  |   13   13   12   11   10   12   15 |
 R10  |   12   13   14   14   13   10   11 |
 R11  |   19   18   16   19   15   17   17 |
 R12  |   11   12   10   14   14   13   17 |
 R13  |   11   14   11   12   15   13   12 |
 R15  |   11   11   11   12   11   11   13 |
 R16  |   12   11   15   11   14   12   11 |
 R17  |   24   18   18   14   12   17   18 |
 R18  |   11   14   17   10   11   15   10 |
 R19  |    9   16   19   11   14   12   11 |
 R20  |   15   19   15   18   21   20   14 |
 R21  |   11   11   11    9   13   13   10 |
 R22  |   12   11   12   10   11   20   10 |
 R23  |   11    9   10    9   12   11   14 |
 R24  |   43   17   46   13   10   11   14 |


Table 1.1649.c     GPS week : 1649   MJD: 55787.0-55793.0   

         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 1649 0   | -168   189   100   -1445    -102   -1531  85.3  1635  1635 |  162323       0
brd 1649 1   |  -61   -63   198    1546   -1996  -15820  84.6  2272  2272 |  164674       0
brd 1649 2   |   55    87   231    -343    -441  -18570  83.9  2823  2823 |  168714       0
brd 1649 3   | -149    90   146   -1351      50  -17440  84.3  2546  2546 |  168004       0
brd 1649 4   | -127    65   148   -2721    1848  -16400  82.8  2438  2438 |  168472       0
brd 1649 5   |  106   -67   227    -212    -788  -17680  86.6  2076  2076 |  169366       0
brd 1649 6   | -196   -30   230     146   -1772  -16440  85.8  1884  1884 |    -365       0
-------------+------------------------------------------------------------+----------------
brd 1649 mean|  -77    38   183    -625    -457  -14840  84.8  2239  2239 |  143026       0
brd 1649 sdev|  116    95    52    1363    1284    5941   1.3   406   406 |   63281       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 2.1649.0  GPS week: 1649   Day: 0   MJD: 55787                            

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  248|    3    -1     0    64   -28   -27  -.19   23   23 |     ---     ---    ---    ---
esx  136|   -2    -2    13   -11    14   -20   .35   23   20 |  165505   -5019   4635   4852
gfz  190|    0     4     7   -18     1    49  -.14   24   19 |       0   -1842   4591   7791
grg  128|    0    -2    -8    -7   -29    66   .02   56   50 |     ---     ---    ---    ---
iac  n/a|    0     1   -18   -22    16   -21  -.20   22   22 |  164162   -2027   4636   8305
mcc  n/a|   17   -13    25   125    86     3  -.21  119  119 |     ---     ---    ---    ---

Table 2.1649.1  GPS week: 1649   Day: 1   MJD: 55788                            

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  248|   -1    -1     1    12   -64    66  -.22   26   26 |     ---     ---    ---    ---
esx  136|   -3     0     8   -22    81     0   .41   21   18 |  163380    4048   8032   8203
gfz  190|   -4     0     7    27   -17   113  -.24   23   20 |       0    1804   6972  10159
grg  128|    3    -2    -4    11    -5   -40   .20   52   46 |     ---     ---    ---    ---
iac  n/a|    1    -1   -14     1   -14  -171  -.16   22   22 | 6236611       3   8054 999999
mcc  n/a|    2    14    -3    18   -59  -686  -.49  115  115 |     ---     ---    ---    ---

Table 2.1649.2  GPS week: 1649   Day: 2   MJD: 55789                            

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  248|   -4     1     0    32   -41    51  -.13   30   29 |     ---     ---    ---    ---
esx  136|    2    -1    12    35    15   -26   .30   35   24 |  165800    3798   7037   7251
gfz  190|    0     0     9    20    32    83  -.24   31   36 |       0    4565   6984  10349
grg  128|   -1     4   -16  -103    29   141   .21   57   46 |     ---     ---    ---    ---
iac  n/a|    0    -1   -13   -21    -3  -123  -.17   24   24 |  169703    1850   7062  10317
mcc  n/a|   -9     5    -4   -14   -43  -709  -.55  107  107 |     ---     ---    ---    ---

Table 2.1649.3  GPS week: 1649   Day: 3   MJD: 55790                            

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  248|    0    -1    -3    66     3   -54  -.16   26   26 |     ---     ---    ---    ---
esx  136|    1    -1    13   -15    58    -7   .35   22   22 |  170683   -6141   5683   5859
gfz  190|   -1     1     3   -25   -31    17  -.15   19   16 |       0   -3675   5661   8414
grg  128|   -5     4    -6     5   -25   192   .45   52   47 |     ---     ---    ---    ---
iac  n/a|    0     0   -11   -10   -10   -10  -.15   21   21 |  168976   -3035   5694   8988
mcc  n/a|  -28    11    20    41    53  -384   .39  112  112 |     ---     ---    ---    ---

Table 2.1649.4  GPS week: 1649   Day: 4   MJD: 55791                            

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  248|   -2     5    -7    32    18   -20  -.17   27   27 |     ---     ---    ---    ---
esx  136|    1    -3     6    29    60   -58   .36   20   18 |  171310   -3401   7379   7568
gfz  190|    0     1     3   -20   -51   103  -.16   22   19 |       0   -1835   5659   8611
grg  128|   -1    -1   -16     6   -12   -51   .17   61   61 |     ---     ---    ---    ---
iac  n/a|    2     0     1   -13    -8   -22  -.26   21   21 |  190332   -3621  10350  91570
mcc  n/a|    2     0    23    80   -74  -233  -.55  114  114 |     ---     ---    ---    ---

Table 2.1649.5  GPS week: 1649   Day: 5   MJD: 55792                            

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  248|   -2     1    -2    51    32    45  -.13   28   26 |     ---     ---    ---    ---
esx  136|    0     0    13   -21    96    33   .42   19   17 |  184871  -28755  36961  37210
gfz  190|    0    -1     2   -63   -68    50  -.21   21   17 |       0   -2739   5255   7869
grg  128|    5     1    -7    70   -68  -100  -.02   58   56 |     ---     ---    ---    ---
iac  n/a|    0     0    -9    67   -10  -102  -.19   25   25 |  169819    -216   5173   8185
mcc  n/a|    5    13    -3   344   263  -682  -.35  105  105 |     ---     ---    ---    ---

Table 2.1649.6  GPS week: 1649   Day: 6   MJD: 55793                            

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  248|    0     1    -6    48   -10    19  -.13   25   25 |     ---     ---    ---    ---
esx  136|    0    -1    12    33    66    41   .43   20   18 |   -1284    1457   4832   5012
gfz  190|    0     0     8   -66   -50    38  -.18   21   18 |       0     760   4864   8413
grg  128|    1     0    -7   -41    69   280   .09  185   47 |     ---     ---    ---    ---
iac  n/a|    1     0   -18   -28   -25  -243  -.21   23   23 |     -99     103   4833   8747
mcc  n/a|   -2     1   -10     8   -34  -123  -.15  102  102 |     ---     ---    ---    ---

       
       
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 3.1649.0  GPS week: 1649   Day: 0   MJD: 55787                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  998   21   18   24   55   20  ---   12 |    56   74   65   27   65  ---    60
 R02  |  819   15   15   17  131   19  ---   19 |    54   52   50   50   41  ---    42
 R03  | 3642   25   22   16   47   17  ---   11 |    23   32   34   50   20  ---    21
 R05  | 1068   33   10   14   51   16   75   12 |    71   51   45   50   54   77    49
 R06  |  805   15   23   12   54   13  ---   10 |    49   55   52   55   49  ---    49
 R07  | 1133   17   22   35   59   20  ---   14 |    59   56   60  118   53  ---    53
 R08  | 1209   15   13   23   33   24  ---   10 |    52   51   49   40   58  ---    47
 R09  | 1170   24   28   28   45   14  ---   13 |    31   30   25   47   22  ---    21
 R10  | 1368   17   17   25   37   30  ---   12 |    26   25   27   29   44  ---    22
 R11  | 1101   42   40   34   45   26  176   18 |    36   72   52   36   36   80    40
 R12  |  785   28   19   16   34   13  ---   10 |    35   42   40   24   30  ---    32
 R13  | 1986   25   13   20   37   18  ---   10 |    28   25   33   36   25  ---    23
 R15  | 2737   17   19   14   55   16   76   11 |    29   32   34   52   24   37    27
 R16  | 1120   33   22   15   36   17  ---   12 |    41   33   37   39   30  ---    29
 R17E | 1511   34   53   51   63   48  ---   24 |    31   87   75   38   33  ---    45
XR18E | 2373   11   18   16  ---   24  ---   10 |    32   40   44  ---   29  ---    32
 R19E | 1782   12   13    9   39   19  ---    8 |    63   63   59   45   60  ---    58
 R20E | 1344   19   24   36   56   26  ---   15 |    35   39   48   35   33  ---    32
 R21E |  853   14   26   14   40   17  ---   10 |    18   35   28   34   22  ---    22
 R22E | 1398   15   14   16   62   26  ---   12 |    52   43   39   67   46  ---    43
 R23E | 2507   14   12   18   59   19  ---   11 |    68   67   66   62   57  ---    62
XR24E |16173   41  ---  ---  186   43  ---   42 |    39  ---  ---   59   28  ---    25
------+-----------------------------------------+-------------------------------------
 RMS  | 1635   23   23   24   56   22  119      |T   42   47   45   47   39   64    37
 WRMS | 1635   23   20   19   50   22  119      |NE  42   45   43   46   39   64    36
 MEDI | 1209   17   19   17   51   19   76      |MD  36   43   45   45   33   77    32

Table 3.1649.1  GPS week: 1649   Day: 1   MJD: 55788                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1437   16   22   18   43   16  ---   10 |    46   57   45   39   35  ---    42
XR02  | 1053   32   15   22  ---   25  ---   13 |    40   23   37  ---   23  ---    27
 R03  | 4121   22   12   30   56   10  ---   12 |    27   36   43   53   24  ---    29
 R05  | 1085   36   21   20   67   26  160   15 |    51   29   31   41   37   67    28
 R06  |  775   18   10   20   45   13  ---    9 |    39   36   44   26   30  ---    33
 R07  | 2255   15   10   30   48   29  ---   12 |    43   49   79  111   30  ---    49
 R08  | 1311   17   13   11   39   19  ---    9 |    38   36   35   40   31  ---    33
 R09  |  879   33   24   23   40   15  ---   12 |    39   36   29   42   32  ---    29
 R10  | 2879   24   17   25   50   21  ---   12 |    33   31   45   53   27  ---    30
 R11  | 1566   53   39   23   46   18   99   18 |    38   74   61   35   45   44    50
 R12  |  999   27   16   25   42   15  ---   11 |    29   27   32   37   27  ---    23
 R13  | 2031   29   26   18   62   18  ---   14 |    33   31   25   63   24  ---    24
 R15  | 4583   24   16   18   40   15   67   10 |    40   39   31   49   29   33    30
 R16  |  940   27   16   16   48   16  ---   11 |    32   36   35   47   26  ---    28
 R17E | 1989   37   35   28   61   32  ---   18 |    32   61   58   69   37  ---    40
 R18E | 4932   18   11   21   78   27  ---   14 |    35   39   51   50   24  ---    33
 R19E | 1638   19   21   22   42   46  ---   15 |    97  103  103   91   65  ---    89
 R20E | 1584   28   30   44   69   26  ---   18 |    28   52   63   63   32  ---    39
 R21E | 1171   15   15   14   60   20  ---   11 |    27   30   30   48   26  ---    25
 R22E | 1059   20   15   16   41   22  ---   10 |    44   47   42   52   39  ---    40
 R23E | 1054   11   14   15   44   16  ---    9 |    65   60   64   70   58  ---    60
XR24E | 2855   16  293  ---  ---   17  ---   17 |    32   54  ---  ---   28  ---    36
------+-----------------------------------------+-------------------------------------
 RMS  | 2272   26   21   23   52   22  115      |T   40   44   46   53   33   48    37
 WRMS | 2272   26   18   20   46   22  115      |NE  37   38   40   48   30   48    32
 MEDI | 1437   22   16   21   46   18   99      |MD  38   36   43   49   30   44    33

Table 3.1649.2  GPS week: 1649   Day: 2   MJD: 55789                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1370   28   30   21   42   16  ---   13 |    55   63   37   37   41  ---    44
 R02  |  961   47   30   17   62   19  ---   17 |    40   43   36   71   25  ---    26
 R03  | 4776   22   20   17   30   10  ---    9 |    24   38   31   32   28  ---    27
 R05  | 1052   26   17   29   77   18  143   15 |    69   67   93   75   67   43    69
 R06  | 1368   22   16   27   44   16  ---   11 |    48   50   43   31   32  ---    36
 R07  | 3401   12   23   50   53   18  ---   16 |    57   45   97   75   49  ---    54
 R08  |  750   19   21   22   47   23  ---   12 |    54   61   54   34   45  ---    47
 R09  |  898   33   21   19   42   14  ---   12 |    33   32   29   34   18  ---    21
 R10  | 2433   10   20   25   34   36  ---   13 |    38   33   38   38   41  ---    32
 R11  | 1748   45   34   20   37   25   74   16 |    31   56   41   38   35   29    33
 R12  | 1064   23   22   19   27   15  ---   10 |    40   57   49   55   43  ---    44
 R13  | 2125   32   16   20   27   13  ---   10 |    26   33   40   40   25  ---    26
 R15  | 5090   16   25   23   32   16   92   10 |    31   37   42   39   22   26    30
 R16  |  993   41   31   30   15   24  ---   15 |    40   51   63   41   36  ---    40
 R17E | 2569   37   22   36   54   34  ---   17 |    44   52   66   54   38  ---    43
 R18E | 4858   19   23   26   90   14  ---   16 |    26   38   44   78   27  ---    24
 R19E |  890   20   25   20  109   14  ---   19 |    85  100   98  103   85  ---    87
 R20E | 3454   30   24   33   43   27  ---   15 |    32   45   58   46   33  ---    29
 R21E | 1041   16   15   17   33   24  ---   10 |    31   37   40   36   38  ---    31
 R22E |  850   20   20   26   43   19  ---   12 |    44   48   36   48   42  ---    39
 R23E | 1331   13   22   16   40   15  ---   10 |    52   60   55   65   48  ---    51
 R24E | 6761   62  127   85  128   59  ---   45 |    60  113   60   59   33  ---    49
------+-----------------------------------------+-------------------------------------
 RMS  | 2822   30   35   31   57   24  107      |T   43   52   52   51   38   32    40
 WRMS | 2822   29   24   36   46   24  107      |NE  41   47   49   45   36   32    37
 MEDI | 1368   22   22   22   42   18   92      |MD  40   48   43   41   36   29    36

Table 3.1649.3  GPS week: 1649   Day: 3   MJD: 55790                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  930   22   32    9   50   20  ---   12 |    41   81   60   45   43  ---    54
 R02  | 1023   19   17   15   55   25  ---   12 |    47   63   50   51   37  ---    45
 R03  | 3586   25   22   15   35   19  ---   11 |    29   35   31   39   29  ---    26
XR04E | 9917    6  ---  ---  ---  ---  ---    0 |   309  ---  ---  ---  ---  ---   306
 R05  |  814   26   18   21   56   32  121   14 |    64   59   57   41   56   33    52
 R06  | 1087   15   18   16   56   24  ---   11 |    51   61   47   35   57  ---    48
 R07  | 3974   22   19   19   77   23  ---   14 |    63   44   57   93   54  ---    48
 R08  | 1802   15   21   15   53   13  ---   10 |    54   76   62   62   54  ---    59
 R09  |  894   32   16   16   32   22  ---   11 |    45   48   38   54   42  ---    39
 R10  | 1094   12   28   18   59   27  ---   13 |    28   38   35   47   27  ---    25
 R11  | 1178   42   38   23   85   16  121   18 |    39   59   39   77   36   30    35
 R12  | 1052   38   22   22   56   13  ---   13 |    33   38   33   66   31  ---    28
 R13  | 2674   30   24   14   52   16  ---   12 |    34   54   38   41   40  ---    37
 R15  | 5121   26   25   23   33   10   91   11 |    44   44   36   38   38   33    36
 R16  |  745   32   15   18   28   14  ---   10 |    36   36   43   27   27  ---    31
 R17E | 2434   28   18   28   40   28  ---   13 |    34   40   40   44   48  ---    35
 R18E | 2096   26   16   14   39   14  ---   10 |    53   40   46   43   39  ---    41
 R19E | 2112   27   17   17   44   17  ---   11 |    56   45   56   61   57  ---    52
 R20E | 4441   21   23   29   89   32  ---   17 |    32   48   49  101   33  ---    34
 R21E |  877   17   13   18   27   20  ---    9 |    22   38   38   30   28  ---    27
 R22E | 1699   16   19   14   38   18  ---    9 |    32   45   34   47   33  ---    31
 R23E | 2671   11   18    7   45   14  ---    8 |    95   92   85   91   77  ---    86
 R24E | 4813   30   20   24   39   24  ---   13 |    41   38   40   44   45  ---    34
------+-----------------------------------------+-------------------------------------
 RMS  | 2545   26   22   19   52   21  112      |T   55   51   46   53   42   32    52
 WRMS | 2545   26   22   16   47   21  112      |NE  43   52   44   51   40   32    40
 MEDI | 1802   25   19   17   45   19  121      |MD  41   45   40   45   39   33    37

Table 3.1649.4  GPS week: 1649   Day: 4   MJD: 55791                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1007   16    9   12   46   10  ---    8 |    34   42   40   51   38  ---    36
 R02  | 1449   20   14   25   86   16  ---   13 |    37   50   55   62   35  ---    41
 R03  | 5896   25   19   24   48   19  ---   12 |    28   35   35   62   25  ---    25
XR04E | 6365   32   16  ---  ---   17  ---   15 |   123   22  ---  ---   29  ---   123
 R05  | 1649   32   10   12   66   20   98   12 |    47   41   34   81   37   22    37
 R06  |  848   17   17   22   68   15  ---   12 |    45   49   38   66   41  ---    39
 R07  | 3503   17   20   30  105   19  ---   16 |    56   66   40   72   65  ---    50
 R08  | 1735   14   12   17   83   24  ---   13 |    51   51   52   39   71  ---    50
 R09  |  826   29   15   13   45   10  ---   10 |    25   35   32   59   29  ---    28
 R10  | 1824   18   31   14   32   31  ---   13 |    27   51   36   43   33  ---    33
 R11  | 1297   42   27   31   29   18  138   14 |    34   45   41   48   42   17    33
 R12  |  975   36   15   21   57   25  ---   13 |    41   49   50   71   46  ---    43
 R13  | 2159   32   19   29   73   16  ---   14 |    38   47   53   61   32  ---    35
 R15  | 3915   24   23   13   44   12  100   10 |    29   30   22   49   22   20    23
 R16  |  720   41   20   15   62   12  ---   13 |    39   35   27   72   33  ---    29
 R17E | 3350   26   17   18   55   24  ---   12 |    35   51   45   56   51  ---    42
 R18E |  989   26   14   20   47   17  ---   10 |    36   33   36   43   26  ---    26
 R19E | 1663   26   17   17   79   23  ---   13 |   105  113  105  113  102  ---   104
 R20E | 3834   48   34   44   64   36  ---   21 |    50   75   62   78   46  ---    50
 R21E | 1329   25   22   26   50   22  ---   13 |    26   38   46   52   29  ---    30
 R22E | 2082   23   17   15   37   25  ---   11 |    37   44   43   54   49  ---    38
 R23E | 1674   10   22   15   52   26  ---   11 |    93   87   92   85  100  ---    90
 R24E | 2908   17   14   16   47   22  ---   10 |    26   38   33   44   29  ---    30
------+-----------------------------------------+-------------------------------------
 RMS  | 2438   27   20   22   61   21  114      |T   46   49   46   61   43   19    45
 WRMS | 2438   27   18   19   61   21  114      |NE  37   44   39   59   39   19    35
 MEDI | 1674   25   17   17   52   19  100      |MD  37   45   40   59   37   20    37

Table 3.1649.5  GPS week: 1649   Day: 5   MJD: 55792                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  |  874   19   26   19   63   15  ---   12 |    30   56   50   50   37  ---    40
 R02  | 1690   24   15   29   80   19  ---   15 |    36   32   34   59   21  ---    27
 R03  | 4202   27   12   12   32   16  ---    9 |    19   31   32   46   30  ---    24
XR04E | 6177   20   31  ---   58   30  ---   18 |    94   48  ---   52   22  ---    90
 R05  | 1251   25   18   19   48   21  105   11 |    40   41   36   55   49   15    39
 R06  | 1747   15   14   19   59   13  ---   10 |    36   53   49   40   34  ---    40
 R07  | 4266   21   14   23   74   18  ---   13 |    42   35   40  234   36  ---    28
 R08  | 2408   22   13   14   62   24  ---   12 |    51   48   44   46   58  ---    45
 R09  |  876   35   19   22   31   15  ---   11 |    25   31   30   51   24  ---    22
 R10  | 2233   19   14   16   49   15  ---   10 |    22   30   37   60   29  ---    28
 R11  | 1365   50   26   26   51   21   96   16 |    37   59   54   48   31   23    40
 R12  | 1085   32   12   20   55   21  ---   12 |    37   37   34   51   35  ---    31
 R13  | 1344   30   16   17   62   22  ---   13 |    25   31   32   50   23  ---    21
 R15  | 2577   28   14   14   32   26  113   11 |    32   37   28   42   38   26    28
 R16  | 1391   35   18   12   42   18  ---   11 |    28   26   22   35   30  ---    21
 R17E | 2713   31   36   25   37   38  ---   16 |    29   63   47   52   35  ---    38
 R18E | 1566   40   13   19   84   14  ---   15 |    28   31   40   73   28  ---    29
 R19E |  793   23   15   14   61   20  ---   11 |    82   74   74   78   63  ---    70
 R20E | 1345   28   24   45   56   52  ---   20 |    60   59   73   68   43  ---    51
 R21E | 1198   25   13   21   55   24  ---   12 |    27   24   34   53   22  ---    20
 R22E | 1128   34   32   18  106   38  ---   20 |    39   71   49  139   50  ---    53
 R23E | 1051   16   18   16   42   28  ---   11 |   156  145  147  153  143  ---   146
 R24E | 3105   18   15   14   41   29  ---   11 |    25   36   34   60   38  ---    30
------+-----------------------------------------+-------------------------------------
 RMS  | 2075   28   19   21   58   25  105      |T   43   47   46   69   39   21    41
 WRMS | 2075   26   17   17   56   25  105      |NE  32   39   37   61   33   21    31
 MEDI | 1391   25   15   19   55   21  105      |MD  36   37   37   52   35   23    31

Table 3.1649.6  GPS week: 1649   Day: 6   MJD: 55793                            

        Weighted Average                        Orbit Dynamics (7 days)
 PRN  |  brd  cod  esx  gfz  grg  iac  mcc  IGL |   cod  esx  gfz  grg  iac  mcc   IGL
------+-----------------------------------------+-------------------------------------
 R01  | 1042   19   27   20   45   25  ---   13 |    47   67   45   44   60  ---    50
 R02  | 1181   20   13   15   61   21  ---   12 |    53   41   47   42   54  ---    43
 R03  | 2403   22   15   16   35   21  ---   10 |    29   41   41   47   26  ---    32
XR04E | 2273   28   30  ---   27   23  ---   16 |   104   37  ---   22   26  ---   108
 R05  | 1034   18   11   18   35   13   88    9 |    66   61   60   59   59   27    58
 R06  | 2784   24   13   14   68   19  ---   13 |    48   47   43   46   47  ---    40
 R07  | 3615   18   17   21  846   30  ---   13 |    50   54   52  321   41  ---    44
 R08  | 1471   22   10   10   46   17  ---    9 |    60   58   53   42   51  ---    50
 R09  | 1269   39   24   23   48   17  ---   14 |    30   40   40   44   24  ---    28
 R10  | 1516   21   16   18   37   21  ---   10 |    29   32   32   40   29  ---    27
 R11  | 1182   36   28   33   41   31  102   16 |    39   57   44   41   42   24    39
 R12  | 1108   35   24   22   70   29  ---   16 |    44   46   61   93   37  ---    47
 R13  | 1607   28   16   20   44   20  ---   12 |    31   30   31   47   20  ---    23
 R15  | 2582   25   16   27   37   25  113   12 |    25   34   41   44   27   23    27
 R16  | 1332   30   14   16   32   22  ---   11 |    32   31   30   41   25  ---    23
 R17E | 3573   32   38   31   35   36  ---   17 |    34   48   46   44   38  ---    31
 R18E | 1654   22   11   13   47   17  ---   10 |    28   34   34   54   22  ---    27
 R19E | 1348   18   11   14   56   12  ---   10 |    68   70   76  105   73  ---    73
 R20E | 2259   26   18   35   20   27  ---   13 |    69   72   73   68   51  ---    63
 R21E | 1228   18   12   22   27   18  ---    9 |    19   29   35   30   30  ---    24
 R22E | 1107   19   19   14   20   24  ---    9 |    73   68   72   92   77  ---    71
 R23E |  825   19   30   15   53   25  ---   13 |   165  176  168  157  143  ---   162
 R24E | 1536   25   28   19   50   24  ---   13 |    27   42   33   38   26  ---    29
------+-----------------------------------------+-------------------------------------
 RMS  | 1884   25   20   21  185   23  102      |T   50   52   52   67   44   24    48
 WRMS | 1884   25   18   18   47   23  102      |NE  41   45   44   67   38   24    37
 MEDI | 1471   22   16   18   44   22  102      |MD  44   46   44   44   38   24    40




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