[IGSREPORT-23720] Wk 1850 IGLOS Final Orbits

IGS ACC igs.acc at noaa.gov
Fri Jul 10 08:49:11 PDT 2015


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1850   (Jun 21, 2015 - Jun 27, 2015) 
                                                                               
Contact: igs.acc 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 2.1850.
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:
                                                                               
 igl1850[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1850 in the SP3 format.
 igl18507.sum      Combination Report for GPS Week 1850.


    
    
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
    

 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  |     -8.6 ns
                1  |      0.9 ns
                2  |      0.0 ns
                3  |     -0.5 ns
                4  |     -0.4 ns
                5  |     -0.1 ns
                6  |      8.4 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  |  COD   | R12
                5  |  COD   | R11 R12
                6  |  COD   | R11 R12

    
         
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 1.1850, 1a.1850).
        
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 2.1850.0-6)                                                                                
    
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 3.1850.0-6). 
        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 1850 summary.                      (Jun 21, 2015 - Jun 27, 2015)

Table 1.1850.a     GPS week : 1850   MJD: 57194.0-57200.0

         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|   -1     0    -2    55   -29     2   .32   56   46 |     ---     ---    ---    ---
        |    1     2     4    34    25    29   .05           |     ---     ---
cof  n/a|   -1    -1    -3    37   -19    11   .27   59   47 |     ---     ---    ---    ---
        |    1     2     3    16    44    39   .05           |     ---     ---
emx  n/a|   -1     0     6    31   -40   -30   .26   29   28 |   -1808    -826   4536   7219
        |    1     1     2    20    24    13   .04           |    8200    1218
esx  n/a|    0     0    -1   -33     8    16  -.00   21   19 |   -3917   -1975   4245   7679
        |    0     0     1    18    17    29   .04           |    4173    1109
gfz  n/a|    0     0     0    16    54    38   .13   21   18 |       0    -778   4169   6673
        |    0     1     1    21    10    19   .07           |       0    1493
grg  n/a|   -1     1     1    -3    28   165  -.30   36   33 | -773617   -1226   9534 692784
        |    1     1     3    28    29    21   .06           |    8843    1852
iac  n/a|    2     0    -1   -17   -19   -84  -.23   20   20 |    1605    -360   4647   7459
        |    1     1     1    26    23    28   .03           |    4728    1185
mcc  n/a|    2     0    22     0  -106  -717  -.47  171  171 |     ---     ---    ---    ---
        |   10     7    28    53   155   827   .24           |     ---     ---


Table 1.1850.b     GPS week : 1850   MJD: 57194.0-57200.0   

         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  |   10   10   10    9   10   10   11 |
 R02  |    7    8    7    7    7    7    8 |
 R03  |    9    9    8    7    8    9    8 |
 R04  |    7    9    9    8    8    7    6 |
 R05  |   12   11   10   12   15   11   16 |
 R06  |    8    7   12    9   11   11   10 |
 R07  |    6    8    7    7    7    7    7 |
 R08  |    9    7    7    7    9    7    8 |
 R09  |   12   13   13   15   15   12   15 |
 R10  |    9   10    7    8    9   15    8 |
 R11  |   22   21   22   23   25   15   14 |
 R12  |   19   23   20   23   26   20   18 |
 R13  |   10   10   11   12   12   10   10 |
 R14  |   16   20   20   17   20   17   16 |
 R15  |    9    9   10    9   13   12   10 |
 R16  |   11   10   10   12   10    9   11 |
 R17  |   25   22   22   25   23   23   21 |
 R18  |   11    9    9    7    8    9   10 |
 R19  |   12   11   10   10    9   10    9 |
 R20  |   14   14   15   13   16   16   18 |
 R21  |   12   13   13   14   13   10   11 |
 R22  |   10   11   12   13   12   11   11 |
 R23  |    9   10   10   10   11   10   10 |
 R24  |   12   13   13   14   15   15   13 |


Table 1.1850.c     GPS week : 1850   MJD: 57194.0-57200.0   

         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 1850 0   |  154    55   302     416     851    1393  85.0  2258  2258 |   -8611       0
brd 1850 1   | -154   -86    30    1638    1887    -865  91.2  8571  8571 |     887       0
brd 1850 2   |   42   -31   231    1095   -1509     261  86.8  2760  2760 |       0       0
brd 1850 3   |  -36   -36   186    1231    -104     735  86.3  1697  1697 |    -465       0
brd 1850 4   | -106     8   224    -751    -461     912  87.0  1574  1574 |    -428       0
brd 1850 5   |  -49   -17   306    1660   -1248    1988  86.0  1648  1648 |    -139       0
brd 1850 6   |  -17   -79   111    -226     478    4516  86.1  1872  1872 |    8425       0
-------------+------------------------------------------------------------+----------------
brd 1850 mean|  -23   -26   198     723     -15    1277  86.9  2911  2911 |     -47       0
brd 1850 sdev|  100    49    99     938    1195    1686   2.0  2530  2530 |    4938       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 2.1850.0  GPS week: 1850   Day: 0   MJD: 57194                            

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     3   -11   -36    -8   .34   51   46 |     ---     ---    ---    ---
cof  n/a|   -4    -4     1     4   -41   -26   .31   56   47 |     ---     ---    ---    ---
emx  n/a|    0     2     7    38   -20    -9   .28   29   27 |   -8392   -2712   4299   7558
esx  n/a|    0    -1    -2   -22   -11   -20  -.00   20   19 |   -5561   -3089   4318   8728
gfz  n/a|    0     2    -1    40    53    28   .09   20   20 |       0   -2990   4275   7627
grg  n/a|    0     0     0   -10    64   157  -.38   33   29 | -780624   -3299   4376 694544
iac  n/a|    2    -1    -1   -51   -16   -70  -.27   18   18 |   -6110   -2050   4375   8002
mcc  n/a|    1   -12    15    26  -211   202  -.33  119  119 |     ---     ---    ---    ---

Table 2.1850.1  GPS week: 1850   Day: 1   MJD: 57195                            

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     0     0    49   -20   -16   .34   50   35 |     ---     ---    ---    ---
cof  n/a|   -3     0    -2    35    12    44   .33   50   35 |     ---     ---    ---    ---
emx  n/a|   -1     0     9    56   -28   -40   .31   30   28 |    2206     613   4797   8174
esx  n/a|    0    -1    -2   -44     3   -17   .06   21   18 |   -8627    -809   3806   7324
gfz  n/a|    0     0    -1    14    66    58   .23   23   21 |       0     525   3811   6293
grg  n/a|   -3     1     0    12    25   169  -.35   37   33 | -755173    1386  38291 684460
iac  n/a|    2     1     0   -19   -49   -62  -.22   18   18 |    1992    1374   4839   8140
mcc  n/a|   -3     4   -15    19  -184   524  -.62  132  132 |     ---     ---    ---    ---

Table 2.1850.2  GPS week: 1850   Day: 2   MJD: 57196                            

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     1    71     8     8   .37   49   42 |     ---     ---    ---    ---
cof  n/a|   -1    -2     0    43    63     5   .26   54   45 |     ---     ---    ---    ---
emx  n/a|    0     0     6     2   -69   -30   .26   33   32 |    5651   -1299   4788   7268
esx  n/a|    0    -1    -2   -62    31    18   .04   22   20 |   -2153   -2579   3936   6989
gfz  n/a|    0     0     1   -19    34    59   .07   19   19 |       0    -678   3969   5952
grg  n/a|   -1     0     0     7    50   179  -.29   37   34 | -772877   -2745   6251 695109
iac  n/a|    2     0     0    30   -21   -82  -.22   17   17 |    3533   -1580   5479   9187
mcc  n/a|   21    11    12    46   137  -416  -.27  143  143 |     ---     ---    ---    ---

Table 2.1850.3  GPS week: 1850   Day: 3   MJD: 57197                            

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     2     0    77   -54    47   .30   56   52 |     ---     ---    ---    ---
cof  n/a|   -3     2    -4    38   -69    10   .22   60   53 |     ---     ---    ---    ---
emx  n/a|   -2    -1     6    21   -54   -32   .22   30   27 |   -5243    -808   4404   6404
esx  n/a|    0     0    -1    -9     2    56  -.01   18   18 |   -5692   -2854   4246   7271
gfz  n/a|    1     1    -1    22    51    17   .07   19   20 |       0   -2027   4218   6155
grg  n/a|   -2     1     6   -38    28   174  -.21   38   35 | -777159   -1400   4412 694085
iac  n/a|    2     0     0   -12    20  -134  -.21   20   20 |     125     598   4406   6250
mcc  n/a|   11     3    39    24    50 -1221  -.84  148  148 |     ---     ---    ---    ---

Table 2.1850.4  GPS week: 1850   Day: 4   MJD: 57198                            

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    -4    -4    92   -46     7   .36   59   58 |     ---     ---    ---    ---
cof  n/a|    0    -3    -4    38   -25    76   .23   62   62 |     ---     ---    ---    ---
emx  n/a|   -4    -2     3    49   -66   -35   .26   28   26 |  -13604   -1795   3588   6343
esx  n/a|    0     0     0   -48    -8    50  -.03   22   20 |    -680   -2872   3580   6978
gfz  n/a|    0     0     0    44    55    28   .07   24   16 |       0   -1156   3577   6487
grg  n/a|    0     0    -1   -36    45   166  -.25   37   36 | -778172   -2726   3561 694780
iac  n/a|    2     0     0    -7   -18  -113  -.22   23   23 |     924    -378   3572   6283
mcc  n/a|   -9     0    39    35   -92 -1393  -.64  187  187 |     ---     ---    ---    ---

Table 2.1850.5  GPS week: 1850   Day: 5   MJD: 57199                            

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     1    -7    38     0    24   .29   62   42 |     ---     ---    ---    ---
cof  n/a|    0     0    -7    57   -25     4   .22   65   45 |     ---     ---    ---    ---
emx  n/a|    1     0     2    12    -5   -18   .20   28   28 |   -3121    -320   4879   6685
esx  n/a|    0     0     0   -27    14    14  -.04   19   17 |   -7740   -1072   4831   7540
gfz  n/a|    0     0     0    10    61    58   .19   20   14 |       0    -591   4823   6542
grg  n/a|   -2     3     0    43   -24   122  -.31   40   36 | -780003    -727   4870 693554
iac  n/a|    0    -2    -3   -23   -43   -69  -.27   21   21 |     939    -508   4862   6559
mcc  n/a|   -2     0    67  -101  -132 -1134  -.42  228  228 |     ---     ---    ---    ---

Table 2.1850.6  GPS week: 1850   Day: 6   MJD: 57200                            

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     2    -7    72   -53   -44   .23   62   43 |     ---     ---    ---    ---
cof  n/a|    0     0    -8    42   -51   -36   .30   65   45 |     ---     ---    ---    ---
emx  n/a|   -1     1     6    42   -35   -49   .26   29   28 |    9841     538   4997   8103
esx  n/a|    0    -1     0   -18    30    13  -.04   21   18 |    3031    -553   4999   8923
gfz  n/a|    1    -1    -1     6    55    18   .20   22   14 |       0    1468   4516   7660
grg  n/a|    0     0     7    -1     5   189  -.30   33   28 | -771315     928   4979 692961
iac  n/a|    1     0    -2   -40    -7   -61  -.21   18   18 |    9832      21   4998   7796
mcc  n/a|   -1     0    -5   -44  -312 -1582  -.15  241  241 |     ---     ---    ---    ---

       
       
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 3.1850.0  GPS week: 1850   Day: 0   MJD: 57194                            

        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
------+---------------------------------------------------+-----------------------------------------------
 R01  | 1897   28   42   31   22   20   17   13  ---    9 |    42   52   45   31   39   34   40  ---    33
 R02  | 1271   18   23   12   16   11   21   16   92    7 |    54   58   47   33   43   35   42   52    39
 R03  | 1380   16   16   18   11   22   31   16  ---    8 |    56   56   65   67   60   72   60  ---    61
 R04  | 1406   21   26   22   10   13   10   14  ---    6 |    66   69   67   54   50   54   47  ---    53
 R05  | 1466   18   16   23   31   16   43   21  ---   11 |    59   58   52   55   60   60   58  ---    55
 R06  | 1125   16   12   19   16    9   33   13  ---    8 |    52   51   58   52   50   42   51  ---    48
 R07  | 1285   19   22   12   11    8   27    8  126    6 |    68   67   70   62   58   57   61   78    61
 R08  | 1283   19   16   29   20   15   22   14  ---    8 |    60   57   66   41   46   47   56  ---    49
 R09  | 1744   15   23   28   27   23   47   18  ---   12 |    29   35   30   40   32   35   26  ---    26
 R10  | 1089   18   18   21   21   14   31   12  ---    8 |    27   30   26   36   23   28   24  ---    22
 R11  | 1568  119  110   34   22   31   56   22  ---   21 |   100   97   35   29   43   57   40  ---    27
 R12  | 1705  159  177   63   20   34   51   16  152   18 |   115  130   40   33   54   61   39   82    35
 R13  | 5272   26   30   22   18   15   34   20  ---    9 |    42   45   34   34   25   30   23  ---    23
 R14  | 3259   34   46   50   34   21   53   26  ---   16 |    33   42   30   41   30   36   26  ---    21
 R15  | 2120   13   20   24   25   14   14   18  ---    8 |    29   35   30   38   27   18   20  ---    22
 R16  | 2092   29   37   28   25   28   21   13  ---   11 |    27   37   27   36   37   23   22  ---    23
XR17E |  853   42   57   51  ---  ---   26   43  ---   24 |    47   52   45  ---  ---   45   40  ---    36
 R18E |  993   46   49   25   11   19   37   16   47   11 |    50   52   28   22   27   40   20   27    22
 R19E | 1077   40   47   28   16   17   21   31  ---   11 |    87   93   83   83   86   82   88  ---    83
 R20E | 5834   50   56   31   21   30   32   25  ---   13 |    91   89   86   91  102   98   95  ---    91
 R21E | 1435   54   65   23   15   16   34   19  148   11 |    63   72   33   29   40   44   24   47    30
 R22E | 1581   47   55   24   15   12   24   13  ---   10 |    65   69   58   56   60   76   57  ---    57
 R23E | 1204   29   31   20   14   12   27   18  ---    8 |    37   45   35   45   46   45   42  ---    40
 R24E | 1531   49   57   24   23   22   17   22  ---   11 |    50   61   36   39   36   25   32  ---    28
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 2257   51   56   29   20   20   33   18  119      |T   56   60   46   45   46   47   43   57    41
 WRMS | 2257   46   47   27   19   20   29   18  119      |NE  53   57   45   42   42   43   39   70    37
 MEDI | 1435   28   31   24   20   16   27   16  126      |MD  52   56   40   40   43   44   40   52    35

Table 3.1850.1  GPS week: 1850   Day: 1   MJD: 57195                            

        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
------+---------------------------------------------------+-----------------------------------------------
 R01  | 3337   27   31   32   21   12   34   10  ---    9 |    33   28   39   37   39   40   28  ---    30
 R02  | 2352   24   31   15   10   13   40    9  106    8 |    37   42   36   26   36   22   35   84    29
 R03  | 4751   13   13   18   18   22   33   12  ---    8 |    44   46   37   39   37   40   37  ---    36
 R04  | 7233   29   32   27   13   24   17   13  ---    8 |    43   46   45   33   31   30   29  ---    30
 R05  | 9632   29   35   21   20   15   50   15  ---   10 |    37   43   30   43   33   49   35  ---    33
 R06  | 4843   18   15   17   14   16    9   12  ---    6 |    35   29   30   23   31   46   32  ---    26
 R07  |11005   22   28   20   13   17   37   10  174    8 |    43   52   45   46   51   37   38   76    40
 R08  |10138   18   26   22   14   13   28    9  ---    7 |    37   45   44   32   35   27   38  ---    33
XR09  | 4197   23   38   22   34  ---   31   16  ---   13 |    25   43   25   40  ---   23   22  ---    20
 R10  |10349   12   30   20   27   20   33   20  ---   10 |    27   39   26   34   31   38   17  ---    22
 R11  |13401  108  105   43   33   24   67   29  ---   20 |    77   77   36   43   44   40   30  ---    29
 R12  |16063  131  107   54   21   39   67   27  119   23 |    83   69   48   43   55   48   36  106    36
 R13  |12384   28   29   23   17   26   35    7  ---    9 |    34   37   22   31   26   36   15  ---    18
 R14  | 4354   43   42   58   37   38   58   40  ---   19 |    30   37   38   57   46   40   36  ---    32
 R15  | 5374   12   12   24   21   18   19   15  ---    8 |    19   19   26   23   23   22   19  ---    16
 R16  | 2422   18   16   24   28   20   27   15  ---   10 |    23   26   21   34   31   35   18  ---    19
XR17E |13346   46   56   39  ---  ---   38   35  ---   22 |    37   53   35  ---  ---   61   38  ---    32
 R18E | 5451   43   51   20   14   15   28    9   70    8 |    41   52   24   28   28   35   21   43    21
 R19E | 4074   52   60   23   20   19   29   13  ---   10 |    57   63   36   55   53   57   40  ---    43
 R20E |13541   55   60   35   25   33   25   22  ---   13 |    98  104   93   91  103  108   83  ---    90
 R21E | 2848   66   65   30   15   27   29   17  163   12 |    69   73   30   32   40   40   30   43    29
 R22E | 7531   56   59   25   13   22   32   14  ---   11 |    67   73   48   56   64   61   42  ---    50
 R23E | 6631   37   38   24   19   13   25   18  ---    9 |    64   68   51   55   58   59   47  ---    51
 R24E | 9694   50   56   31   21   26   31   23  ---   12 |    58   62   42   41   45   47   28  ---    30
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 8570   50   50   30   21   23   37   18  132      |T   46   51   37   40   42   43   33   70    33
 WRMS | 8570   35   35   28   18   21   33   18  132      |NE  39   42   34   36   36   35   29   88    28
 MEDI | 6631   29   35   24   20   20   31   15  119      |MD  37   46   36   39   37   40   32   76    30

Table 3.1850.2  GPS week: 1850   Day: 2   MJD: 57196                            

        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
------+---------------------------------------------------+-----------------------------------------------
 R01  |  953   29   55   32   26   10   22   15  ---    9 |    29   75   53   41   37   34   36  ---    34
 R02  | 7698   24   23   19   15   13   27   10  141    7 |    42   43   45   32   37   42   42   65    36
 R03  | 1734   35   31   17   20   11   19   10  ---    7 |    49   60   63   71   59   58   60  ---    60
 R04  |  790   15   21   19   12   15   30   21  ---    8 |    50   54   61   51   56   47   39  ---    48
 R05  | 1190   18   23   25   24   19   38   15  ---   10 |    52   56   50   47   51   44   40  ---    43
 R06  | 3504   16   21   14   21   20   65   14  ---   11 |    45   51   38   40   33   60   39  ---    33
 R07  | 1061   16   18   27   15   14   14    9  169    7 |    56   46   56   53   62   60   62   51    57
 R08  |  886   18   17   23   10   10   25   15  ---    7 |    49   50   55   41   47   42   33  ---    41
 R09  | 1179   25   38   29   40   27   26   17  ---   12 |    26   51   34   45   35   30   30  ---    24
 R10  | 1364    9   16   13   18   15   23   13  ---    7 |    19   21   24   23   21   27   14  ---    14
 R11  | 1043  118  128   55   13   31   53   28  ---   21 |    84   90   41   35   39   44   30  ---    23
 R12  | 1973  113  114   40   19   27   59   24  206   19 |    81   81   23   26   31   50   29  148    22
 R13  | 1575   37   54   21   21   24   28   21  ---   10 |    46   60   33   32   21   18   21  ---    19
 R14  | 2380   35   32   91   30   12   61   25  ---   20 |    33   45   42   49   35   35   28  ---    25
 R15  | 5163   15   20   16   29   21   42   12  ---   10 |    25   31   21   33   20   28   24  ---    15
 R16  | 2981   19   25   25   29   19   37    9  ---   10 |    20   27   23   27   19   19   18  ---    14
XR17E | 1143   49   34   43  ---  ---   37   28  ---   21 |    35   29   39  ---  ---   43   40  ---    30
 R18E | 1969   33   33   29   15   14   27   14   57    9 |    41   43   27   34   29   42   21   49    24
 R19E | 1926   44   49   25   14   16   24   19  ---   10 |    58   63   44   41   47   42   47  ---    41
 R20E | 1083   68   81   34   28   20   58   18  ---   15 |    86   92   58   63   61   80   63  ---    60
 R21E | 1923   72   79   29   15   22   30   19   90   13 |    71   78   30   28   44   34   28   20    29
 R22E | 4974   59   49   23   17   23   29   20  ---   12 |    80   78   70   71   77   83   65  ---    69
 R23E |  662   47   46    8   20   18   27   17  ---    9 |    34   42   34   43   35   45   33  ---    32
 R24E | 2494   58   71   32   22   25   32   16  ---   13 |    56   80   35   47   53   32   33  ---    35
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 2760   49   54   33   22   19   37   17  143      |T   48   56   41   42   41   43   36   66    34
 WRMS | 2760   42   45   32   20   19   34   17  143      |NE  44   52   41   40   37   39   34   88    31
 MEDI | 1575   33   33   25   20   19   29   16  141      |MD  46   51   39   41   37   42   33   51    32

Table 3.1850.3  GPS week: 1850   Day: 3   MJD: 57197                            

        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
------+---------------------------------------------------+-----------------------------------------------
 R01  |  903   33   22   19   22   12   23   20  ---    9 |    53   48   53   48   53   46   46  ---    45
 R02  |  817   20   24   25   12   12   10   11  143    6 |    48   48   53   35   31   38   36   51    36
 R03  |  655   30   34   19   11   15   18   10  ---    7 |    56   51   60   66   70   67   64  ---    63
 R04  |  917   15   15   23   13   10   32   19  ---    8 |    57   54   66   51   59   41   55  ---    53
 R05  | 1202   22   35   24   25   17   55   20  ---   12 |    64   74   65   60   58   79   56  ---    58
 R06  | 1334   22   24   20    9   14   43   18  ---    9 |    59   60   59   56   44   30   57  ---    49
 R07  |  999   16   19   22   14    8   14   17  185    7 |    62   64   58   66   57   67   52   55    58
 R08  |  918   15   19   13   15   16   25   11  ---    7 |    62   62   62   47   65   66   60  ---    57
 R09  |  933   29   36   37   28   20   64   29  ---   15 |    39   41   28   35   27   42   35  ---    23
 R10  | 1412   10   33   22   25   12   17    8  ---    8 |    23   37   31   30   19   27   16  ---    18
 R11  |  649  139  131   59   12   30   54   33  ---   22 |    96   88   47   41   54   63   48  ---    36
 R12  | 1451  136  145   53   16   40   59   22  162   22 |    98  107   40   43   59   65   40   89    36
 R13  | 1728   47   51   11   28   18   38   22  ---   11 |    56   57   28   44   28   24   16  ---    25
 R14  | 2815   48   43   62   28   19   37   34  ---   16 |    43   44   48   43   45   53   28  ---    33
 R15  | 3585   23   27   21   15   20   28   14  ---    8 |    30   33   29   27   22   31   19  ---    17
 R16  | 1155   25   40   22   25   19   55   12  ---   11 |    30   43   23   35   23   40   21  ---    21
XR17E | 1539   54   70   46  ---  ---   58   30  ---   25 |    44   59   56  ---  ---   60   41  ---    37
 R18E | 2142   25   28   18    9   13   19   13   61    6 |    35   37   34   32   33   29   28   32    29
 R19E | 2228   37   33   24   11   16   37   14  ---    9 |    59   59   57   51   54   54   41  ---    48
 R20E | 1233   62   79   27   14   23   35   25  ---   12 |    97  109   92   97  107   93   88  ---    93
 R21E | 2397   87   99   35   13   21   32   19  158   14 |    86   96   41   35   46   47   30   15    35
 R22E | 1491   63   79   28   15   20   36   28  ---   12 |    93  103   84   91   99   99   69  ---    85
 R23E | 1428   54   58   18   17   18   28   16  ---   10 |    69   75   69   68   67   59   60  ---    62
 R24E | 2612   63   63   27   22   24   43   26  ---   13 |    59   67   49   46   50   51   44  ---    39
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1697   56   60   30   18   19   38   20  148      |T   59   63   51   49   50   52   43   48    44
 WRMS | 1697   52   53   27   18   20   35   20  148      |NE  54   56   46   45   44   48   40   65    39
 MEDI | 1334   30   35   23   15   18   35   19  158      |MD  57   59   53   46   53   51   41   51    37

Table 3.1850.4  GPS week: 1850   Day: 4   MJD: 57198                            

        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
------+---------------------------------------------------+-----------------------------------------------
 R01  | 1072   33   29   25   17   21   19   22  ---   10 |    47   58   50   56   65   42   56  ---    50
 R02  | 1012   18   22   19    7   10   19   14  142    6 |    43   46   32   42   46   51   33   43    39
 R03  |  509   28   25   19   20   17    9   17  ---    8 |    46   54   54   65   60   59   61  ---    58
 R04  | 1017   23   21   20   14   12   21   13  ---    7 |    57   55   56   39   48   37   44  ---    44
 R05  | 1025   23   23   25   32   25   66   17  ---   14 |    53   61   59   76   68   55   61  ---    61
 R06  | 1520   18   20   12   21   15   48   26  ---   11 |    45   55   56   56   59   39   64  ---    53
 R07  |  929   22   24   20    8   12   18   15  219    7 |    62   65   58   53   49   46   59   73    53
 R08  |  709   18   21   22   22   18   16   17  ---    8 |    54   55   58   53   32   53   43  ---    46
 R09  | 1725   23   22   37   25   27   57   20  ---   14 |    29   36   30   39   34   40   33  ---    27
 R10  | 1156   10   27   25   22   16   23   19  ---    9 |    28   34   38   30   30   59   17  ---    25
 R11  |  858  150  156   47   30   43   55   34  ---   25 |    99  103   52   60   64   51   46  ---    39
 R12  | 1204  161  171   46   22   44   58   40  152   26 |   107  114   35   54   70   69   51   38    41
 R13  | 1761   47   53   18   23   25   39   10  ---   11 |    47   54   27   33   32   29   20  ---    21
 R14  | 2385   61   66   59   29   32   47   40  ---   19 |    40   59   38   43   54   24   30  ---    29
 R15  | 2197   25   44   27   38   20   35   18  ---   12 |    37   56   25   51   28   33   26  ---    24
 R16  | 1165   29   30   26   16   20   29   15  ---    9 |    37   39   28   30   30   27   24  ---    23
XR17E |  988   62   53   40  ---  ---   37   29  ---   22 |    56   59   27  ---  ---   37   38  ---    24
 R18E | 1706   30   33   14   16   14   22   11   66    7 |    39   45   29   32   26   30   26   22    24
 R19E | 2507   32   42   22   15   15   26   18  ---    9 |    59   62   53   56   54   64   49  ---    52
 R20E | 1279   66   54   24   27   30   32   41  ---   15 |    89   81   52   73   81   77   65  ---    64
 R21E | 2589   51   53   23   17   20   49   19  281   12 |    66   69   36   48   49   55   40   22    41
 R22E | 1194   64   64   24   19   20   24   20  ---   12 |    86   86   59   66   70   61   62  ---    61
 R23E |  846   55   60   18   16   22   24   15  ---   10 |    54   57   53   50   56   45   38  ---    46
 R24E | 2762   62   60   28   26   29   30   33  ---   14 |    60   56   34   45   41   38   20  ---    27
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1574   59   62   28   22   24   37   23  187      |T   55   60   43   50   49   46   41   39    40
 WRMS | 1574   58   62   26   20   16   36   23  187      |NE  51   59   43   48   48   44   41   51    39
 MEDI | 1165   30   33   24   21   20   29   18  152      |MD  53   56   38   51   49   45   40   38    41

Table 3.1850.5  GPS week: 1850   Day: 5   MJD: 57199                            

        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
------+---------------------------------------------------+-----------------------------------------------
 R01  | 1177   20   21   31   19   14   31   15  ---    9 |    30   32   50   50   53   51   55  ---    47
 R02  |  808   22   24   20    9   11   24   17  145    7 |    34   37   35   27   24   26   25   51    25
 R03  |  813   21   29   25   15   14   28   16  ---    8 |    40   41   39   54   54   41   47  ---    46
 R04  | 1428   22   30   13   10   10   30   10  ---    6 |    47   53   43   38   38   66   46  ---    43
 R05  |  771   28   27   34   11   15   55   14  ---   11 |    38   34   52   62   61   42   57  ---    53
 R06  | 1538   27   37   25   14   17   34   30  ---   10 |    36   34   38   63   57   64   56  ---    52
 R07  | 1025   12   15   17   11    8   33   14  272    7 |    47   49   46   62   56   49   55  122    53
 R08  |  836   17   17   17   16   11   16   17  ---    7 |    41   41   42   38   34   38   47  ---    38
 R09  | 1541   14   21   32   24   25   51   18  ---   12 |    29   33   30   38   33   35   32  ---    27
 R10  | 1425   19   20   16   19   18  101   13  ---   15 |    21   26   28   33   21   91   17  ---    26
 R11  |  993  167  176   33   26   25   49   23  ---   14 |   101  113   46   54   53   40   36  ---    43
 R12  | 1195  182  183   53   35   34   59   30  155   20 |   108  114   37   67   64   37   44   33    46
 R13  | 1414   42   40   15   18   18   40   10  ---   10 |    40   36   18   28   19   27   16  ---    16
 R14  | 1692   55   38   41   33   27   25   40  ---   16 |    31   47   49   66   66   61   31  ---    46
 R15  | 2801   42   33   19   27   23   26   18  ---   11 |    36   32   26   30   33   22   20  ---    20
 R16  | 1276   33   41   21   15   17   28   12  ---    8 |    37   46   26   23   26   23   17  ---    18
XR17E | 1017   57   53   36  ---  ---   36   31  ---   22 |    58   57   51  ---  ---   54   43  ---    41
 R18E | 1757   28   35   18   15   11   33   22   72    9 |    40   45   27   31   32   41   27   49    26
 R19E | 2040   40   48   25   13   17   25   17  ---    9 |    59   68   52   51   49   37   35  ---    44
 R20E | 1768   63   69   41   20   29   45   33  ---   16 |   102  105   95   93  101   91   81  ---    87
 R21E | 3249   43   43   26   11   20   22   17  367   10 |    56   58   41   38   36   30   25   33    31
 R22E | 1668   47   54   22   13   18   36   18  ---   10 |    66   69   43   50   56   57   45  ---    47
 R23E | 2632   47   45   27   14   15   25   17  ---   10 |    55   56   38   37   34   50   27  ---    33
 R24E | 1098   64   78   26   26   30   23   29  ---   14 |    62   74   43   44   35   39   35  ---    33
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1648   62   65   28   19   20   40   21  228      |T   50   54   41   46   45   46   38   57    39
 WRMS | 1648   42   45   28   17   14   36   21  228      |NE  44   48   37   45   43   44   37   68    37
 MEDI | 1414   33   37   25   15   17   31   17  155      |MD  40   46   41   44   38   41   35   49    41

Table 3.1850.6  GPS week: 1850   Day: 6   MJD: 57200                            

        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
------+---------------------------------------------------+-----------------------------------------------
 R01  | 1028   27   25   21   33   19   26   24  ---   11 |    54   52   61   51   60   67   65  ---    56
 R02  |  890   17   17   21   15   15   11   23   90    8 |    56   55   52   47   46   48   49   82    47
 R03  | 1759   17   13   28   13   13   12   15  ---    7 |    58   61   62   69   70   65   68  ---    65
 R04  | 1556   15   15   11    8    8   26   12  ---    6 |    69   69   72   64   66   80   63  ---    66
 R05  | 1023   29   33   49   13   29   64   24  ---   16 |    61   62   68   70   69   59   74  ---    66
 R06  | 1860   29   33   17   32   11   25   13  ---    9 |    53   56   60   82   67   54   62  ---    62
 R07  |  653   19   18   16   17   11   14   15  164    7 |    76   80   87   86   87   81   86  180    84
 R08  |  864   12   17   13   19   16   19   16  ---    7 |    69   69   69   58   70   71   62  ---    64
 R09  | 1028   22   39   23   29   41   57   25  ---   15 |    31   48   26   36   44   30   31  ---    26
 R10  | 1431   15   19   26   18   11   27   12  ---    8 |    30   31   34   31   31   42   20  ---    23
 R11  |  921  170  173   47   16   30   33   12  ---   14 |   116  119   49   61   81   61   57  ---    58
 R12  | 1058  187  187   47   36   24   47   22  110   17 |   133  139   35   62   65   54   55   94    48
 R13  | 1457   40   48   15   20   17   30   11  ---    9 |    49   55   30   34   25   28   26  ---    24
 R14  | 1385   32   34   40   34   38   50   17  ---   15 |    28   46   26   56   66   43   41  ---    39
 R15  | 5658   24   35   20   28   16   26   13  ---    9 |    34   39   33   46   24   35   22  ---    25
 R16  | 1827   38   39   23   14   27   29   17  ---   11 |    44   47   24   28   35   28   20  ---    21
XR17E | 1454   57   65   45   45  ---   39   26  ---   21 |    50   60   39   13  ---   54   41  ---    33
 R18E | 2523   35   33   22   11   21   30   19  134   10 |    45   44   32   32   32   36   33   51    30
 R19E | 1105   40   45   21   10   15   19   17  ---    9 |    60   63   42   45   49   44   36  ---    42
 R20E | 1012   71   89   51   21   35   34   23  ---   17 |   107  109   98   81   81   88   79  ---    80
 R21E | 2650   39   31   23   12   22   28   19  474   10 |    54   56   44   46   49   47   39  127    41
 R22E | 1633   41   34   27   14   20   32   18  ---   11 |    73   74   76   75   83   73   69  ---    72
 R23E | 1930   37   43   23   20   16   23   21  ---   10 |    39   45   31   30   30   32   32  ---    26
 R24E | 1019   65   75   18   18   22   26   17  ---   12 |    68   87   42   48   53   54   42  ---    43
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1872   62   65   29   21   22   33   18  241      |T   60   65   49   52   55   53   48  106    47
 WRMS | 1872   43   45   28   18   14   28   18  241      |NE  60   64   49   55   56   52   50  118    48
 MEDI | 1385   32   34   23   18   19   27   17  134      |MD  54   56   42   48   60   54   42   94    43




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