[IGSREPORT-25563] Wk 1968 IGLOS Final Orbits

acc acc at igs.org
Sun Oct 15 20:13:37 PDT 2017


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1968   (Sep 24, 2017 - Sep 30, 2017) 
                                                                               
Contact: acc at igs.org
                                                                               
                                                                               
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 2.1968.
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:
                                                                               
 igl1968[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1968 in the SP3 format.
 igl19687.sum      Combination Report for GPS Week 1968.


    
    
REMARKS concerning the IGL Orbit Combination:                                  
---------------------------------------------

Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.

 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
    
    Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
    model file has been updated to igs14.atx to be consistent with IGS14.
    See IGSMAIL #7399 for more information
        ftp://igs.org/pub/station/general/igs14.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  |      1.9 ns
                1  |     -1.9 ns
                2  |     -0.7 ns
                3  |      0.1 ns
                4  |     -1.3 ns
                5  |    -12.9 ns
                6  |      1.4 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
               ----+--------+---------------
                4  |  GRG   | R22

    
         
ORBIT COMBINATION AND EVALUATION STATISTICS:                                    
--------------------------------------------                                    
      
Table 1 summarizes all statistics for the week. It contains means and standard 
        deviations over the week of satellite ephemeris  and  clock correction
        transformation parameters for each centre (Tables 1.1968, 1a.1968).
        
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 2.1968.0-6)                                                                                
    
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 3.1968.0-6). 
        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 1968 summary.                      (Sep 24, 2017 - Sep 30, 2017)

Table 1.1968.a     GPS week : 1968   MJD: 58020.0-58026.0

         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  n/a|   -2     0    -5    18     2     2   .07   29   31 |    7328    -323   4223  11690
        |    1     1     3    19    14    29   .04           |    4348    1833
cof  n/a|   -2     0    -5    24     2    -7   .11   32   33 |    7322    -316   4225  11691
        |    1     1     2    20    12    20   .06           |    4345    1829
emx  n/a|   -1     0    -3   -17    18    19   .07   27   27 |    -886    -802   3183   9243
        |    1     1     2    19    28    58   .05           |   15325    1704
esx  n/a|    0     0     1   -18    22    -3   .19   15   14 |    -907     584   3169  11120
        |    1     1     1    12    14    48   .04           |    6244    1532
gfz  n/a|    0     0     2    27    27    53   .00   22   20 |       0    -308   3186   9809
        |    1     2     2    13    16    23   .03           |       0    2732
grg  n/a|   -1     0     5   -85     0  -124  -.44  243   26 |    5286   -2831   4906 175885
        |    2     1     4    33    13    60   .04           |   19809    4529
iac  n/a|    1     0    -1    62   -74    25  -.04   20   20 |   -1382    -740   4225  10498
        |    1     1     1    30    34    66   .04           |    4602     979
mcc  n/a|    2    -4    -1   101   -52   386  -.24  138  138 |     ---     ---    ---    ---
        |    5     6    14   103    32   268   .13           |     ---     ---


Table 1.1968.b     GPS week : 1968   MJD: 58020.0-58026.0   

         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  |   11   10   11   11   11   10   11 |
 R02  |    8    9    8    7    8    8    8 |
 R03  |    6    7   10    7    8    8    7 |
 R04  |    6    6    8    8    7    7    8 |
 R05  |   12   11   11   12   11   11   12 |
 R06  |    9   10    8   11   10   10   10 |
 R07  |    7    9    7    7    8    8    8 |
 R08  |    6   11    8    7    8    8    6 |
 R09  |   10    9    6    8   12    7   10 |
 R10  |    7    7    8    8   10    8    7 |
 R11  |   10    7    9    7    8    7    8 |
 R13  |    8    8    8    6    9    9    7 |
 R14  |   24   21   17   12   22   15   16 |
 R15  |   11   14   13   15   15   12   12 |
 R16  |   13   18   19   14   12   17   14 |
 R17  |   11   10   11   10   10    8   12 |
 R18  |    8    8    7    7    8    9    8 |
 R19  |   15   13   15   14   14   14   13 |
 R20  |   14   16   12   15   13   11   12 |
 R21  |   10    9   10   11   10   10   10 |
 R22  |   11   10   10   10   14    9   12 |
 R23  |    9    9    8    8    9    9    9 |
 R24  |   15   15   12   19   15   15   12 |


Table 1.1968.c     GPS week : 1968   MJD: 58020.0-58026.0   

         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 1968 0   |  -12    -4   -17    -770    -888    2468  83.8  1487  1487 |    1935       0
brd 1968 1   |   -5    54   -38    1996    -181    3030  83.4  2688  2688 |   -1948       0
brd 1968 2   |  -28    40   -46   -1055     124    2747  84.1  1809  1809 |    -654       0
brd 1968 3   |   -3    -5   -50     608    -197    2682  83.9  1836  1836 |     107       0
brd 1968 4   |  -71    34   -35     231   -1743    4685  83.3  1892  1892 |   -1316       0
brd 1968 5   |  -25   -16   -21    1524    -674    4239  82.4  1651  1651 |  -12892       0
brd 1968 6   |   -8    -9   -48      -3    -410    1673  82.8  1414  1414 |    1424       0
-------------+------------------------------------------------------------+----------------
brd 1968 mean|  -22    13   -36     361    -567    3074  83.4  1825  1825 |   -1906       0
brd 1968 sdev|   23    28    12    1119     617    1044    .6   420   420 |    5041       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 2.1968.0  GPS week: 1968   Day: 0   MJD: 58020                            

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  n/a|    0     0    -4    -7   -14   -36   .08   27   30 |   10990     593   6918  12040
cof  n/a|    0     0    -1    10    20   -24   .02   30   31 |   10989     584   6925  12040
emx  n/a|   -1     3     0   -44    65    71   .00   24   24 |   18987    1505   3728   8382
esx  n/a|    0     1     0   -34     6    53   .18   17   16 |    9480    2371   3729  10429
gfz  n/a|    0     0     3    20    60    63   .04   19   20 |       0    3538   3740   8942
grg  n/a|   -3    -2     4  -108     8  -229  -.42   30   23 |    3940     321   7029 177926
iac  n/a|    0    -1     0   105  -108   -22   .02   20   19 |    3061   -1706   6914  10750
mcc  n/a|   -2    -4     9     9   -49   492  -.21  165  165 |     ---     ---    ---    ---

Table 2.1968.1  GPS week: 1968   Day: 1   MJD: 58021                            

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  n/a|   -1     0    -4    18    -8    25   .07   30   32 |    8556   -2607   3693  13115
cof  n/a|    0     0    -6    36     5    10   .18   35   35 |    8540   -2566   3694  13116
emx  n/a|   -1     0     0    16    49    41  -.01   30   30 |   14529   -2752   3420   9918
esx  n/a|   -1    -1     0   -16    34     2   .26   16   13 |   -4610   -1523   3397  11161
gfz  n/a|   -2    -1     2    21    19    54  -.04   19   19 |       0   -3771   3394  10582
grg  n/a|    2     1     8   -89    -2  -158  -.45   33   27 |   -1405   -2662   3716  11623
iac  n/a|    3     0    -2    41   -77    23  -.10   20   20 |   -1592   -1403   3695  11566
mcc  n/a|    1   -17    -2    70   -76   468  -.13  135  135 |     ---     ---    ---    ---

Table 2.1968.2  GPS week: 1968   Day: 2   MJD: 58022                            

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  n/a|   -1     1    -7    44     3   -43   .11   30   34 |    8030    -467   3587  11085
cof  n/a|   -3     0    -8     5     3   -17   .10   32   35 |    8042    -496   3588  11087
emx  n/a|   -2     0    -3   -10   -10    -1   .06   27   27 |  -18809   -1876   3201   9739
esx  n/a|    0     0     3   -29    28     6   .21   15   13 |    1744     844   3176  11409
gfz  n/a|    1    -1     0    36    20    76   .00   21   18 |       0   -1261   3183  10241
grg  n/a|   -1     0     8   -95    10   -95  -.50   31   27 |    -956       0   3591   9712
iac  n/a|    2     1    -1    75   -43   -22  -.06   19   19 |    -768     239   3591   9680
mcc  n/a|    6     2   -19   229   -45   338  -.19  118  118 |     ---     ---    ---    ---

Table 2.1968.3  GPS week: 1968   Day: 3   MJD: 58023                            

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  n/a|   -3     2    -2    -6    16    18   .13   30   32 |    8877      72   3746  10432
cof  n/a|   -2     1    -1    -1   -13   -26   .13   33   35 |    8868      77   3747  10436
emx  n/a|    1     0    -5   -23    14    21   .11   30   30 |   -7594    -400   3002   9551
esx  n/a|    0    -1     1    -2    25     0   .18   14   13 |   -5797    2103   2997  11737
gfz  n/a|    0     0     2     8    10    51  -.03   23   20 |       0     756   2997  10104
grg  n/a|    0     0     1   -81   -26   -70  -.47   33   31 |     -44      49   3749   9208
iac  n/a|    0     1     0    69   -57   -30  -.02   20   19 |    1007   -1496   3748   9456
mcc  n/a|   -5    -1   -14    85   -27   467  -.05  169  169 |     ---     ---    ---    ---

Table 2.1968.4  GPS week: 1968   Day: 4   MJD: 58024                            

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  n/a|   -1    -1    -3    24    18     9  -.00   29   32 |    7241   -1138   3500  13233
cof  n/a|   -3    -1    -7    26    -5   -10   .05   32   33 |    7221   -1104   3501  13237
emx  n/a|   -1    -2    -2   -30    12    86   .12   27   27 |    9999   -2609   3023   8687
esx  n/a|    1    -1     1   -24     1  -101   .19   15   15 |    -166   -1200   3013  11550
gfz  n/a|    1     3     0    18    19     8   .02   25   19 |       0   -3117   3012   9100
grg  n/a|   -2     2     7  -137    -3   -51  -.43 1527   30 |   -1400   -3312   7649  13563
iac  n/a|    0     0    -2    55   -68    83  -.07   19   20 |   -1415    -495   3503  11883
mcc  n/a|    5    -4     4   263   -17   761  -.39  128  128 |     ---     ---    ---    ---

Table 2.1968.5  GPS week: 1968   Day: 5   MJD: 58025                            

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  n/a|   -3    -1   -11    37    16    23   .07   27   27 |   -2148   -1747   4567  10240
cof  n/a|   -2     0    -6    56    17    30   .13   30   32 |   -2143   -1759   4566  10237
emx  n/a|    0    -1    -7    -6    -1     9   .09   27   27 |  -17133    -606   3296   9197
esx  n/a|    1    -1     0    -2    18    29   .19   15   16 |    2303     101   3278  11373
gfz  n/a|    0     1     3    39    31    77   .03   23   21 |       0    -798   3299   9641
grg  n/a|    0    -1    13   -50     1  -153  -.37   25   21 |  -11981   -1627   4587   9170
iac  n/a|    1     2    -1     9   -35     0  -.04   22   22 |  -11118   -1191   4573   9702
mcc  n/a|   11    -3   -12    52  -113   297  -.41  118  118 |     ---     ---    ---    ---

Table 2.1968.6  GPS week: 1968   Day: 6   MJD: 58026                            

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  n/a|   -3    -1    -3    15   -14    18   .06   29   29 |    9750    3029   3551  11688
cof  n/a|   -2    -2    -5    36    -9   -10   .17   31   29 |    9739    3048   3556  11689
emx  n/a|   -3     1    -6   -26     1   -90   .12   27   27 |   -6183    1118   2614   9230
esx  n/a|    1    -1     2   -19    42   -12   .14   13   13 |   -9309    1398   2599  10181
gfz  n/a|    2    -4     7    45    33    38  -.01   24   25 |       0    2491   2679  10058
grg  n/a|    0     2     0   -37    15  -114  -.44   25   21 |   48848  -12586   4025 999999
iac  n/a|    0     0     0    81  -131   145  -.03   22   22 |    1150     869   3555  10452
mcc  n/a|    0    -2    21     1   -37  -118  -.31  134  134 |     ---     ---    ---    ---

       
       
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 3.1968.0  GPS week: 1968   Day: 0   MJD: 58020                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01E |  687   27   16   20   13   21   43   15  ---   10 |   121  124  130  127  133  131  127  ---   127
 R02E | 2221   16   20   14   14   18   25   15   88    7 |    51   52   48   53   50   63   46   82    49
 R03E | 1893   16   15   16   11   15   14   12  124    6 |    65   64   68   68   68   69   67   97    66
 R04E | 1275   11   12   16   12   13   15   11  ---    5 |    56   58   54   55   60   60   66  ---    57
 R05E | 2083   23   24   13   19   27   37   31  ---   11 |    68   67   73   77   77   77   73  ---    73
 R06E | 1474   22   35   22   16   13   27   22  ---    9 |    64   66   64   66   67   59   61  ---    62
 R07E | 1018   15   10   16   10   14   22    9  315    6 |    75   78   74   74   77   78   77  222    75
 R08E |  766   12   18   18   10   10   24   10  ---    6 |    42   52   55   39   45   43   44  ---    42
 R09E | 1381   14   10   18   19   11   43   17  ---    9 |    12   21   21   34   26   24   24  ---    19
 R10  | 1350   21   14   18   10   14   18   16  ---    7 |    23   25   24   30   28   25   19  ---    22
 R11  | 1227   27   21   20   20   24   15   19  113    9 |    29   33   32   38   34   29   26  103    30
 R13  | 1406   16   24   12   19   22   22   17  ---    8 |    32   35   32   33   29   33   26  ---    28
XR14  |  760   27   25  ---  ---  ---   46   26  ---   23 |    19   23  ---  ---  ---   53   21  ---    23
 R15  | 3862   45   47   20   23   12   18   19  ---   10 |    45   46   32   32   28   23   20  ---    22
 R16  |  810   35   39   33   23   16   48   22  ---   13 |    47   56   34   37   43   32   33  ---    31
 R17  |  801   31   35   32   14   26   13   25  ---   11 |    62   64   54   45   46   40   35  ---    43
 R18  |  598   23   22   16   15   22   21   12  ---    8 |    41   40   40   37   33   22   30  ---    32
 R19  |  616   48   47   37   21   25   32   34  ---   14 |    70   74   57   43   38   54   34  ---    44
 R20  |  651   37   52   38   19   11   54   21  ---   13 |    81   89   58   51   59   67   41  ---    55
 R21  | 1052   37   31   29   10   20   10   25   36   10 |    66   64   58   50   38   50   42   65    47
 R22  | 1257   30   35   27   16   27   14   30  ---   11 |    64   65   52   50   30  923   29  ---    41
 R23  | 1077   17   20   18   27   15   25   12  ---    9 |    40   41   37   56   42   37   38  ---    41
 R24  | 1196   28   52   43   18   31   57   19  ---   14 |    66   83   70   59   64   42   50  ---    55
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1486   27   30   24   17   19   30   20  165      |T   53   57   53   52   50   88   44  113    47
 WRMS | 1486   30   31   24   16   20   23   19  165      |NE  48   52   44   43   39  102   31   84    36
 MEDI | 1196   23   24   18   16   16   24   19  113      |MD  56   58   54   50   43   50   38   97    43

Table 3.1968.1  GPS week: 1968   Day: 1   MJD: 58021                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01E |  668   30   25   25   16   22   30   15  ---    9 |   100   97  100  112  110  102  100  ---   105
 R02E | 2341   16   12   14   10   15   43   16   80    8 |    50   49   52   51   48   49   51   55    47
 R03E |  633   16   15   15   14   18   16   15  111    7 |    45   43   52   52   54   44   46   53    48
 R04E | 1066   11   12   15    8   13   21   14  ---    6 |    38   36   35   45   45   45   43  ---    41
 R05E | 1286   20   27   25   11   16   34   35  ---   10 |    51   56   59   55   44   67   47  ---    50
 R06E | 1999   24   25   25   18   12   34   26  ---   10 |    45   43   48   54   46   37   42  ---    43
 R07E |  902   25   20   20   12   21   18   18  252    8 |    51   50   53   50   60   56   56  179    52
 R08E | 9816   27   49   30   29   21   21   19  ---   11 |    51   83   53   65   53   48   52  ---    51
 R09E | 1743   16   15   19   17   15   31   20  ---    8 |    12   16   15   28   29   33   22  ---    17
 R10  |  754   17   23   15   12   21   16   12  ---    7 |    19   19   19   20   23   15   12  ---    14
 R11  |  807   23   25   18    8   16   19   11   77    6 |    23   24   25   29   29   25   20   57    24
 R13  | 2230   11   10   20   12   19   31   11  ---    7 |    21   22   25   31   24   28   14  ---    21
XR14  |  872   24   28  ---  ---  ---   30   31  ---   20 |    15   14  ---  ---  ---   27   29  ---    14
 R15  | 5002   57   57   42   19   30   15   17  ---   14 |    23   25   20   20   17   16   10  ---    13
 R16  |  828   36   54   65   21   16   83   23  ---   18 |    31   46   29   43   35   39   21  ---    28
 R17  |  754   35   35   26   10   22   16   19  ---    9 |    35   35   33   32   29   32   29  ---    29
 R18  |  726   21   24   18   14   22   17   15  ---    8 |    22   27   26   22   18   19   21  ---    18
 R19  |  617   52   66   36    7   29   13   27  ---   12 |    41   53   39   36   42   40   32  ---    35
 R20  |  893   44   57   43   25   24   54   26  ---   15 |    49   67   31   34   40   37   17  ---    28
 R21  |  802   28   35   26    8   13   23   23   50    8 |    40   47   42   42   48   48   29   53    39
 R22  | 1905   35   26   31    8   18   22   23  ---   10 |    38   33   38   34   27  646   25  ---    29
 R23  | 1060   19   15   26   23   15   21   14  ---    9 |    26   30   28   43   30   41   32  ---    32
 R24  | 2462   36   44   45   20   13   59   28  ---   14 |    57   72   45   58   59   46   46  ---    48
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 2688   30   35   30   16   19   33   20  134      |T   38   42   39   43   41   66   34   79    35
 WRMS | 2688   32   35   30   13   19   27   20  134      |NE  31   36   30   34   32   75   24   55    26
 MEDI |  902   24   25   25   12   18   22   19   80      |MD  38   43   35   42   40   40   29   55    32

Table 3.1968.2  GPS week: 1968   Day: 2   MJD: 58022                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01E |  845   37   19   23   15   28   29   16  ---   10 |    79   82   86   95   97   80   95  ---    89
 R02E | 1514   16   18   18   12   20   34   11   90    8 |    45   48   46   35   42   51   42   54    38
 R03E |  915   20   18   21    9   19   39   23   45    9 |    34   38   37   32   40   53   37   53    34
 R04E | 1082   15   18   18   10   20   22   20  ---    7 |    40   41   39   38   43   43   35  ---    37
 R05E | 1144   27   34   24   22   20   28   23  ---   10 |    76   79   72   73   67   86   66  ---    71
 R06E | 3911   27   28   21   15   12   23   16  ---    8 |    41   47   39   45   43   38   42  ---    39
 R07E |  618   27   39   22    8   15   15    9  226    7 |    49   52   51   46   51   47   45  176    45
 R08E |  633   22   21   27    9   15   21   13  ---    7 |    42   45   62   41   48   40   37  ---    42
 R09E | 1598   11   17   18    9   12   22   14  ---    6 |    21   24   22   23   19   26   28  ---    18
 R10  |  684   25   22   15   14   16   20   18  ---    7 |    22   23   28   30   25   20   21  ---    21
 R11  |  638   26   22   26    6   20   27   15   61    8 |    26   30   33   30   30   33   20   35    25
 R13  | 1751   14   19   17   18   22   14   14  ---    7 |    24   24   26   29   19   24   22  ---    19
XR14  |  684   19   23  ---  ---  ---   30   21  ---   16 |    16   19  ---  ---  ---   27   25  ---    17
 R15  | 5800   56   53   32   18   24   27   25  ---   13 |    33   34   25   31   23   19   15  ---    19
 R16  | 1244   43   46   66   25   14   77   15  ---   18 |    25   33   35   30   27   35   26  ---    23
 R17  |  761   38   46   31   11   29   24   11  ---   10 |    48   54   38   30   26   24   30  ---    28
 R18  |  801   22   24   18   13   11   17    9  ---    6 |    31   35   30   28   29   19   25  ---    24
 R19  |  851   54   47   40   11   34   34   38  ---   15 |    56   52   43   30   34   31   40  ---    33
 R20  |  942   26   18   22   23   29   33   23  ---   11 |    39   37   52   33   32   30   26  ---    27
 R21  |  778   37   39   27   10   23   16   21   71    9 |    47   48   45   40   29   41   25   66    35
 R22  | 1402   29   36   24    9   14   24   28  ---    9 |    45   51   36   38   41 9999   25  ---    35
 R23  |  991   19   22   24   17   10   27   15  ---    8 |    37   35   29   38   30   21   33  ---    30
 R24  | 1218   28   52   26   20   28   45   17  ---   11 |    59   76   75   48   41   30   53  ---    47
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1808   30   32   27   15   21   31   19  118      |T   40   43   43   39   38   37   35   76    34
 WRMS | 1808   34   35   27   13   18   27   19  118      |NE  36   39   38   33   29   27   27   50    27
 MEDI |  942   26   23   23   12   20   27   16   71      |MD  40   41   38   33   32   31   30   54    33

Table 3.1968.3  GPS week: 1968   Day: 3   MJD: 58023                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01E |  618   36   32   30   16   25   19   22  ---   10 |    71   77   79   94   93   84   84  ---    84
 R02E | 1450   18   23   18    8   18   21   10  121    6 |    68   63   72   73   81   63   67   93    70
 R03E | 1401   16   20   20    9   18   26   14   71    7 |    55   55   51   54   55   42   51   97    50
 R04E | 2208   16   12   18    9   20   22   18  ---    7 |    30   32   26   32   35   34   34  ---    29
 R05E | 1006   17   27   28   10   20   47   32  ---   11 |    37   41   33   26   36   54   31  ---    28
 R06E | 2630   28   28   32   22   22   23   16  ---   10 |    32   36   29   54   42   30   36  ---    36
 R07E | 1028   25   23   22    7   16   11   14  324    7 |    40   40   46   37   42   43   45  150    39
 R08E |  922   17   15   26   10   17   21   12  ---    7 |    72   82   77   67   64   75   74  ---    70
 R09E | 1301   17   23   15   14   21   28   15  ---    8 |    14   22   19   21   33   42   27  ---    20
 R10  |  850   17   28   18   13   11   25   23  ---    8 |    24   33   21   21   19   23   15  ---    16
 R11  |  855   20   20   18    8   14   15   18   69    6 |    18   21   18   17   21   20   15   67    13
 R13  | 1888   12    9   15    7   19   16   14  ---    6 |    27   28   31   32   30   35   22  ---    27
XR14  | 2249   15   19  ---  ---  ---   24   13  ---   12 |    19   20  ---  ---  ---   30   17  ---    17
 R15  | 6154   51   57   35   22   35   38   21  ---   14 |    38   43   28   27   27   35   12  ---    21
 R16  |  992   32   33   51   21   23   51   14  ---   14 |    34   39   39   28   34   40   21  ---    23
 R17  |  645   35   35   26    8   30   18   22  ---   10 |    61   62   47   40   42   40   29  ---    40
 R18  |  519   18   15   15    8   18   27    9  ---    7 |    35   33   39   36   24   42   30  ---    31
 R19  |  703   56   59   40   15   30   22   26  ---   14 |    58   59   45   22   19   44   23  ---    28
 R20  |  792   20   28   50   27   24   51   33  ---   15 |    41   48   36   39   32   38   31  ---    28
 R21  | 1168   37   38   32    8   29   22   20  114   10 |    55   57   50   40   31   40   31   91    38
 R22  | 1286   34   32   26   10   26   25   22  ---   10 |    52   51   47   37   31 9999   26  ---    36
 R23  |  761   17   21   29   15   10   19   20  ---    8 |    32   31   30   35   35   46   29  ---    30
 R24  | 2011   52   73   45   16   41   86   25  ---   19 |    94  106   72   67   63   51   44  ---    60
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1836   30   33   30   14   23   33   20  169      |T   43   46   42   40   40   43   34   99    36
 WRMS | 1836   32   35   30   13   20   31   19  169      |NE  42   45   38   33   31   37   24   79    29
 MEDI | 1028   20   27   26   10   20   23   18  114      |MD  38   41   39   36   34   40   30   93    30

Table 3.1968.4  GPS week: 1968   Day: 4   MJD: 58024                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01E | 1442   42   34   27   11   26   22   13  ---   10 |    49   52   55   64   75   61   49  ---    57
 R02E | 1160   23   22   17   12   19   21   18   96    8 |    37   43   40   46   45   51   35   44    39
 R03E | 1209   25   35   21   13   20   19   15  102    8 |    40   47   46   45   43   51   38   71    41
 R04E | 1510   15   18   20   12   18   19   12  ---    7 |    30   32   31   35   36   36   33  ---    32
 R05E | 1293   29   30   27   14   20   29   26  ---   10 |    78   74   61   62   65   56   58  ---    61
 R06E | 1239   22   26   33   18   23   19   22  ---   10 |    37   44   48   46   45   32   44  ---    40
 R07E |  958   25   26   27    7   24   15   14  171    8 |    40   38   45   39   46   50   50  172    41
 R08E | 1228   13   16   22   16   15   24   16  ---    7 |    37   38   44   35   36   49   34  ---    34
 R09E |  880   17   15   25   15   21   62   17  ---   12 |    16   19   23   22   33   63   31  ---    22
 R10  |  821   20   22   17   24   12   27   20  ---    9 |    24   24   31   33   23   19   19  ---    19
 R11  |  952   20   28   14   14   17   23   20   97    8 |    21   29   28   23   26   26   22   46    19
 R13  | 1412   12   17   15   17   30   17   21  ---    9 |    23   29   26   28   22   20   25  ---    19
XR14  | 1622   22   29  ---  ---  ---   51   20  ---   22 |    23   31  ---  ---  ---   59   21  ---    25
 R15  | 6868   49   44   36   22   39   38   16  ---   14 |    32   32   28   25   28   38   16  ---    19
 R16  |  941   25   29   35   15   25   49   17  ---   12 |    18   28   25   23   25   34   25  ---    17
 R17  |  669   35   28   26   13   28   17   20  ---   10 |    54   54   50   46   43   55   39  ---    45
 R18  |  862   13   22   12   16   24   23   13  ---    7 |    33   39   28   39   29   25   25  ---    28
 R19  |  911   58   62   27   13   35   24   23  ---   13 |    56   62   43   36   35   33   42  ---    36
 R20  | 1345   17   43   35   17   20   45   31  ---   12 |    44   64   49   42   41   32   34  ---    34
 R21  | 1380   29   27   34    6   36   18   15  154   10 |    52   53   57   43   35   44   41   69    43
 R22  | 1071   32   30   29   14   42 7159   24  ---   13 |    44   46   44   42   33 9999   29  ---    34
 R23  | 1221   10   18   22   19    9   39   17  ---    9 |    40   49   36   41   34   50   37  ---    36
 R24  | 2268   47   52   43   14   21   61   22  ---   15 |    72   72   52   43   43   50   44  ---    43
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1892   29   32   27   15   25 1526   19  128      |T   39   43   40   39   38   42   34   80    34
 WRMS | 1892   32   33   27   15   19   30   20  128      |NE  38   43   38   35   32   37   29   57    29
 MEDI | 1221   23   28   26   14   21   24   18  102      |MD  37   43   43   39   35   44   34   69    34

Table 3.1968.5  GPS week: 1968   Day: 5   MJD: 58025                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01E | 1695   34   34   25   12   23   18   20  ---    9 |    79   76   82   90   89   75   85  ---    83
 R02E | 1680   20   14   28   10   16   17   20   96    8 |    40   41   47   41   45   45   30   42    38
 R03E | 1012   28   26   19   11   19   18   19   93    8 |    53   52   61   63   58   64   48   52    56
 R04E |  670   17   17   20   10   18   11   14  ---    6 |    42   46   44   43   49   47   41  ---    42
 R05E | 1027   36   33   23   19   23   24   27  ---   11 |    54   61   53   68   56   66   63  ---    61
 R06E |  798   23   27   31   26   13   17   19  ---   10 |    46   45   51   55   43   50   45  ---    46
 R07E |  749   21   22   20    9   28   12   13  125    7 |    65   69   65   67   78   66   69  199    67
 R08E | 1088   16   17   22   14   20   17   13  ---    7 |    51   53   54   43   51   47   37  ---    44
 R09E |  742   15   14   23    9   20   19   12  ---    7 |    12   13   28   23   32   35   24  ---    18
 R10  |  767   10    9   21   13   22   23   18  ---    8 |    24   24   21   23   30   33   16  ---    19
 R11  |  618   14   12   15   10   21   10   21  124    7 |    22   23   30   31   33   32   31   45    28
 R13  | 1942   14   20   23   19   16   25   23  ---    9 |    25   30   25   29   33   24   15  ---    21
XR14  | 1588   25   24  ---  ---  ---   25   13  ---   15 |    19   17  ---  ---  ---   17   20  ---    14
 R15  | 5648   44   51   32    7   34   15   25  ---   11 |    17   27   22   22   18   34   11  ---    13
 R16  |  963   19   34   68   19   25   58   21  ---   17 |    26   38   45   46   28   28   23  ---    28
 R17  |  825   25   34   20    9   19   16   23  ---    8 |    36   42   36   35   41   30   23  ---    32
 R18  | 1159   17   20   13   21   24   26   17  ---    9 |    26   30   24   31   16   22   15  ---    18
 R19  | 1611   54   64   22   10   36   26   33  ---   13 |    34   41   25   24   23   26   20  ---    21
 R20  | 1165   26   29   33   15   21   14   35  ---   11 |    33   47   46   32   30   26   35  ---    24
 R21  | 1541   27   30   25   17   24   20   16  146    9 |    37   40   35   33   38   38   33   66    33
 R22  |  741   33   34   21    6   22   10   29  ---    9 |    35   37   33   36   36 9999   26  ---    32
 R23  | 1318   14   14   16   21   18   22   16  ---    8 |    29   24   33   36   34   24   23  ---    27
 R24  |  782   33   38   28   22   31   59   23  ---   15 |    43   45   29   37   31   32   23  ---    26
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1651   27   30   27   15   23   25   22  118      |T   36   40   40   41   40   39   32   80    34
 WRMS | 1651   27   32   27   16   21   21   22  118      |NE  29   33   31   31   30   28   22   55    24
 MEDI | 1027   23   26   22   12   21   18   20  124      |MD  35   41   35   36   34   33   26   52    28

Table 3.1968.6  GPS week: 1968   Day: 6   MJD: 58026                            

        Weighted Average                                  Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  emx  esx  gfz  grg  iac  mcc  IGL |   cod  cof  emx  esx  gfz  grg  iac  mcc   IGL
------+---------------------------------------------------+-----------------------------------------------
 R01E | 1384   40   39   25   12   29   17   29  ---   11 |   153  152  146  152  153  145  148  ---   148
 R02E | 2026   16   15   18   10   19   27    9  119    7 |   112  110  108  108  109  103  114  123   108
 R03E |  915   27   22   18    8   17   16   16  107    7 |   134  134  132  135  134  133  132  132   132
 R04E |  711   21   16   21    9   20   23   20  ---    8 |    97   97   89   95   92   91   92  ---    92
XR05E | 1112   30   45   27   11  ---   32   29  ---   12 |    74   80   62   65  ---   68   68  ---    64
 R06E |  714   26   33   35   23   14   15   12  ---   10 |    83   83   82   91   83   76   92  ---    84
 R07E |  608   21   15   19   10   19   19   17  130    7 |   106  104   97  105  107  102  113  249   104
 R08E |  879   18   20   19    7   20   14   12  ---    6 |    66   66   64   64   64   62   68  ---    63
 R09E | 1045   14   17   23   10   16   38   30  ---   10 |    17   18   21   25   28   39   28  ---    20
 R10  |  941   16   14   16   11   20   15   13  ---    6 |    31   35   31   36   39   40   28  ---    31
 R11  |  652   15   12   17    9   32   14   20  176    8 |    36   39   42   47   44   47   37   73    41
 R13  | 2033   13   12   15   13   15   20   17  ---    7 |    21   23   26   29   28   21   21  ---    21
XR14  | 1785   30   44  ---  ---  ---   23   14  ---   16 |    27   34  ---  ---  ---   29   17  ---    17
 R15  | 3416   42   29   33   14   32   30   20  ---   12 |    42   43   31   34   18   32   17  ---    24
 R16  |  981   24   20   51    8   21   40   33  ---   13 |    29   29   44   32   37   28   25  ---    28
 R17  |  624   44   44   39    7   25   11   34  ---   12 |    63   64   53   42   34   36   37  ---    40
 R18  |  862   22   22   13   15   19   23   20  ---    8 |    41   44   36   38   26   27   27  ---    29
 R19  | 1444   51   47   28   10   29   18   40  ---   13 |    72   75   44   43   36   43   38  ---    41
 R20  | 1769   34   75   21   20   31   37   12  ---   11 |    53   72   35   39   26   38   42  ---    34
 R21  | 2222   35   34   29   11   36   13   13  125   10 |    70   69   61   48   33   51   42   68    48
 R22  |  779   40   41   31   16   29   22   26  ---   11 |    69   68   56   53   42  626   31  ---    47
 R23  |  716   13   12   21   17   19   28   16  ---    8 |    35   38   43   53   43   36   35  ---    41
 R24  | 1162   23   27   35   16   23   45   15  ---   12 |    58   60   43   54   38   41   36  ---    43
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1413   29   31   27   13   24   25   22  133      |T   64   66   61   63   57   83   56  129    56
 WRMS | 1413   29   29   27   13   25   21   22  133      |NE  46   49   41   42   34   78   30   70    34
 MEDI |  981   24   22   21   11   20   22   17  125      |MD  63   66   44   48   39   43   37  123    41




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