[IGSREPORT-26693] Wk 2060 IGLOS Final Orbits

acc acc at igs.org
Fri Jul 19 01:03:28 PDT 2019


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 2060   (Jun 30, 2019 - Jul 06, 2019) 
                                                                               
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 2.2060.
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:
                                                                               
 igl2060[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 2060 in the SP3 format.
 igl20607.sum      Combination Report for GPS Week 2060.


    
    
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  |     -2.6 ns
                1  |     -3.2 ns
                2  |     -3.9 ns
                3  |     -2.9 ns
                4  |     -1.9 ns
                5  |     -2.1 ns
                6  |     -1.3 ns

    
         
ORBIT COMBINATION AND EVALUATION STATISTICS:                                    
--------------------------------------------                                    
      
Table 1 summarizes all statistics for the week. It contains means and standard 
        deviations over the week of satellite ephemeris  and  clock correction
        transformation parameters for each centre (Tables 1.2060, 1a.2060).
        
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 2.2060.0-6)                                                                                
    
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 3.2060.0-6). 
        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 2060 summary.                      (Jun 30, 2019 - Jul 06, 2019)

Table 1.2060.a     GPS week : 2060   MJD: 58664.0-58670.0

         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|    0     0     3     5   -13    49   .11   22   19 |   12021    -805   3441   8826
        |    1     1     2    10    19    18   .03           |    1252     945
cof  n/a|    1     1     3    19    -4    46   .11   24   21 |   12017    -814   3441   8826
        |    1     1     1    14    20    27   .05           |    1254     949
esx  n/a|    0     0    -3    29    -1    14   .09   27   22 |    1252    -408   3381  10853
        |    1     1     1    19    15    28   .02           |   12572    1376
gfz  n/a|    0     0     2   -36    -2    21   .10   27   18 |       0    -757   3366   8632
        |    0     1     4    17    16    37   .08           |       0    1334
grg  n/a|    0     0    -2   -42    28   -67  -.34   31   26 |   -2422    -924   3519   8567
        |    1     0     3    19    31    65   .06           |     542     836
iac  n/a|   -1     0    -3    20    18   -52  -.10   33   29 |   -1063    -373   3997  11006
        |    1     2     2    30    26    84   .03           |    1874     815
mcc  n/a|    0   -10     1    91    38   817  -.23  162  162 |     ---     ---    ---    ---
        |   12    12    10   111   120   613   .27           |     ---     ---


Table 1.2060.b     GPS week : 2060   MJD: 58664.0-58670.0   

         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  |   21   23   25   21   21   24   25 |
 R02  |    8    9    7    6    9    8   11 |
 R03  |    7   10    8    8    8    7   10 |
 R04  |    7    6    8    7    9    7    9 |
 R05  |   11   11    9    9   10   11   11 |
 R07  |    8    8    6    8    7    9   12 |
 R08  |    7    8    5    7    8   12   12 |
 R09  |    6   10    7    7    7    8    8 |
 R10  |    7    7    8    9   10   10   11 |
 R11  |    6    6    9    7    8    7    9 |
 R12  |    7    7    7    7    8    8    9 |
 R13  |    8    6    8    7   10   14   11 |
 R14  |    7    8    8    8    8   11    9 |
 R15  |    6    8   10    8    7    8    9 |
 R16  |   14   20   20   16   20   18   12 |
 R17  |   15   12   12   14   13   13   10 |
 R18  |    9    9   11    8   11   12   10 |
 R19  |   29   31   31   32   30   33   31 |
 R20  |   22   19   21   25   17   15   19 |
 R21  |   14   15   12   13   15   12   12 |
 R22  |   16   15   15   13   15   17   14 |
 R23  |   11   10   10   10   11   13   11 |
 R24  |   24   20   21   18   21   22   20 |
 R26  |   17   26   17   12   10   15   14 |


Table 1.2060.c     GPS week : 2060   MJD: 58664.0-58670.0   

         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 2060 0   |   38   -26    50     460     974    1806  82.5  1354  1354 |   -2630       0
brd 2060 1   |  -10   -12    43     312    1467      42  81.5  1373  1373 |   -3172       0
brd 2060 2   |    4    26   205     638     885     -35  81.9  1285  1285 |   -3907       0
brd 2060 3   |    2    34   225     534     835   -1203  83.4  1628  1628 |   -2849       0
brd 2060 4   |  -26    26   209    -125     270     390  83.2  1599  1599 |   -1870       0
brd 2060 5   |  -96   -63   213    -976    -303     885  82.9  1488  1488 |   -2134       0
brd 2060 6   |   57     2   193   -1887   -1171    -562  81.2  1376  1376 |   -1287       0
-------------+------------------------------------------------------------+----------------
brd 2060 mean|   -4    -1   163    -149     422     189  82.4  1443  1443 |   -2549       0
brd 2060 sdev|   49    35    79     946     900     975    .8   130   130 |     871       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 2.2060.0  GPS week: 2060   Day: 0   MJD: 58664                            

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     5     0   -13    66   .07   21   19 |   11964    -575   3182   9892
cof  n/a|    1     0     1    40   -11    29   .04   23   21 |   11939    -556   3181   9897
esx  n/a|   -1     0    -1    58    27     5   .10   27   25 |  -12900     220   3182  12142
gfz  n/a|    1     1     0     0     7    -3   .14   23   17 |       0    -567   3180   9728
grg  n/a|    1     0    -1   -58   -16  -125  -.29   32   25 |   -2468    -613   3167   9203
iac  n/a|   -1     0    -6     3   -13    57  -.08   29   25 |   -4550    -186   3882  14644
mcc  n/a|  -10   -17   -12    55   261   392  -.44  185  185 |     ---     ---    ---    ---

Table 2.2060.1  GPS week: 2060   Day: 1   MJD: 58665                            

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     2    16    -1    70   .11   22   19 |   13929     -17   3532   7767
cof  n/a|    0     1     4    25    26   103   .10   25   21 |   13929     -37   3532   7767
esx  n/a|   -1     0    -1    35     0    26   .10   24   19 |   -1864    1163   3372   9659
gfz  n/a|    0     0     0   -44    28    82  -.01   33   16 |       0      89   3376   7689
grg  n/a|    0     0    -1   -29   -16  -118  -.34   31   22 |   -3134     -19   3372   7069
iac  n/a|    0     0    -3   -12     5  -116  -.06   30   27 |   -1050     321   3924   8008
mcc  n/a|  -10     5    -1    34    57   894  -.43  173  173 |     ---     ---    ---    ---

Table 2.2060.2  GPS week: 2060   Day: 2   MJD: 58666                            

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    -1     4    13   -23    38   .08   22   19 |   13505   -2578   3902   8539
cof  n/a|    3     2     4    25   -11    57   .11   23   20 |   13512   -2595   3895   8534
esx  n/a|    0     1    -3    18    -8    33   .10   29   20 |   -6193   -2065   3889  10553
gfz  n/a|    0    -1    -2   -33     0    -9   .13   27   14 |       0   -2430   3848   8433
grg  n/a|    1     0     0   -20    41  -132  -.30   29   22 |   -2580   -2578   3875   7996
iac  n/a|   -2     2    -3    -9     0    30  -.13   32   29 |    -260   -1338   4432  10570
mcc  n/a|   26   -21    -1   308   -44   940   .12  180  180 |     ---     ---    ---    ---

Table 2.2060.3  GPS week: 2060   Day: 3   MJD: 58667                            

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     5    10   -15    59   .10   20   19 |   10760    -855   3553  10380
cof  n/a|    1     2     6     5   -10    50   .07   23   20 |   10765    -876   3550  10378
esx  n/a|    0     0    -4     4   -12    31   .07   29   22 |   17657   -1250   3462  12865
gfz  n/a|    0     0     0   -32   -12    49   .18   22   16 |       0   -2561   3413  10211
grg  n/a|    0     0     0   -51    49   -86  -.30   29   22 |   -2349   -1051   3472   9764
iac  n/a|   -3    -3    -5    27    43  -115  -.13   35   31 |   -2043     659   4057  10331
mcc  n/a|    0   -15    14   169    59  1977  -.18  192  192 |     ---     ---    ---    ---

Table 2.2060.4  GPS week: 2060   Day: 4   MJD: 58668                            

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     3     6   -14   -14    32   .13   21   19 |   11729    -404   3197   7632
cof  n/a|    0     1     3    21   -25    31   .14   26   22 |   11722    -407   3193   7631
esx  n/a|   -1     0    -3    47    -9    44   .04   26   24 |   12134    -327   3158   9215
gfz  n/a|    1     1     4   -42   -10    44   .02   28   16 |       0     137   3150   7492
grg  n/a|   -1     0   -11   -27    41   -20  -.32   27   23 |   -1498    -631   3149   7044
iac  n/a|   -3     0     0    24    28  -172  -.09   34   31 |    -212    -167   3490   7758
mcc  n/a|   -4    -3    15    56   -64   -13  -.13  143  143 |     ---     ---    ---    ---

Table 2.2060.5  GPS week: 2060   Day: 5   MJD: 58669                            

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     0     7   -45    58   .15   24   19 |   11531   -1412   3424   9355
cof  n/a|    0     0     2    -3   -21    25   .14   26   22 |   11526   -1429   3433   9359
esx  n/a|    0    -1    -6    27     6   -33   .10   26   26 |   12051   -1882   3325  11015
gfz  n/a|    1     1     7   -49   -16   -19   .04   28   20 |       0    -955   3315   8763
grg  n/a|    1     0    -2   -73    61    40  -.41   34   32 |   -2036   -1245   3300   8299
iac  n/a|    0     0     0    74    62   -40  -.11   34   30 |    1494    -334   3863  13637
mcc  n/a|    0     5    -3   -20   -90   672   .06  136  136 |     ---     ---    ---    ---

Table 2.2060.6  GPS week: 2060   Day: 6   MJD: 58670                            

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     2     6    17    21   .11   21   18 |   10735     200   3299   8220
cof  n/a|    1    -1     3    24    21    28   .18   23   20 |   10732     198   3304   8218
esx  n/a|   -1     1    -5    12   -16    -9   .10   26   21 |  -12118    1285   3281  10522
gfz  n/a|    0     2     7   -52   -12     7   .17   27   23 |       0     986   3285   8111
grg  n/a|    0    -2    -1   -35    36   -28  -.46   33   34 |   -2894    -337   4301  10594
iac  n/a|    0     2    -3    34     5    -9  -.09   35   31 |    -825   -1569   4337  12094
mcc  n/a|    1   -25    -2    36    88   858  -.61  128  128 |     ---     ---    ---    ---

       
       
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 3.2060.0  GPS week: 2060   Day: 0   MJD: 58664                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  esx  gfz  grg  iac  mcc  IGL |   cod  cof  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  686   51   47   54   22   25   36  ---   20 |    98   97   49   67   60   43  ---    59
 R02  | 1224   13   16   14   17   18   14  191    7 |    54   55   39   54   57   40   88    47
 R03  | 1125   10   11   12   12   18   12  154    6 |    59   62   50   62   71   50   83    58
 R04  | 2253   11   11   11    7   16   17  ---    6 |    62   63   51   60   65   49  ---    57
 R05M |  933   21   22   20   27   13   16  ---   10 |    55   60   46   63   49   46  ---    49
 R07  | 1263   17   17   14   12   17   13  178    7 |    70   69   53   70   55   49   49    59
 R08M |  687    9   11   15   16    7   20  ---    7 |    64   65   54   69   58   57  ---    59
 R09E | 3028   12   11   10   14   14   12  ---    6 |    37   39   39   47   43   37  ---    39
 R10E | 2065   12   13    9   14   20   15  ---    7 |    86   90   87   88   91   74  ---    85
 R11E | 1325    7   12    8   14   13   12  173    5 |    29   31   29   30   33   24   47    28
 R12E |  957   12   21   14   16   11   18  ---    7 |    57   57   47   59   58   49  ---    53
 R13E | 1594   14   21   10   20   19   14  ---    8 |    36   33   32   33   39   31  ---    32
 R14E | 1511   16   18   14   12   15   15  ---    7 |    52   51   48   50   46   42  ---    46
 R15E | 1049   12   11   14   11   10   14  ---    6 |    37   34   36   42   36   39  ---    36
 R16E | 1272   19   40   23   31   33   30  ---   13 |    51   55   57   73   59   48  ---    54
 R17M | 1709   23   27   36   23   26   40  ---   15 |    69   70   41   70   68   31  ---    55
 R18  |  917   15   15   25    9   20   13  ---    8 |    45   47   45   52   51   33  ---    43
 R19  |  521   45   33   60   46   64   74  ---   28 |   100  103   60   99   87   28  ---    70
 R20  |  687   26   25   40   29   64   54  ---   21 |    74   78   50   86   95   38  ---    65
 R21M |  834   23   31   28   16   25   40  221   13 |    77   81   45   71   73   43   99    61
 R22  |  731   15   23   38   30   33   43  ---   16 |    71   74   40   79   85   33  ---    61
 R23  |  474   18   22   28   21   13   20  ---   10 |    28   36   55   26   39   48  ---    35
 R24M | 1129   28   27   24   50   87   26  ---   23 |    53   65   52   68   77   44  ---    54
XR26  | 5223   15   29  ---  ---  ---   19  ---   17 |    26   37  ---  ---  ---   29  ---    25
------+----------------------------------------------+------------------------------------------
 RMS  | 1353   21   23   27   23   32   29  185      |T   57   60   48   61   60   41   73    51
 WRMS | 1353   19   21   25   17   25   25  185      |NE  62   65   49   65   66   40   73    52
 MEDI | 1125   15   21   15   16   18   17  178      |MD  55   60   48   63   58   42   83    54

Table 3.2060.1  GPS week: 2060   Day: 1   MJD: 58665                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  esx  gfz  grg  iac  mcc  IGL |   cod  cof  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  686   59   68   43   42   31   37  ---   23 |    64   73   49   42   45   31  ---    40
 R02  | 1073   11   16   20   15   18   21  218    8 |    43   45   31   41   43   32   41    35
 R03  |  861   10   10   14   10   33   23  168    9 |    46   45   39   41   53   27   27    39
 R04  | 2109    5   12    9   12   12   15  ---    5 |    53   54   52   61   57   44  ---    53
 R05M |  592   15   18   24   22   22   24  ---   10 |    47   51   67   60   41   41  ---    49
 R07  |  707   14   16   15   20   15   14  188    7 |    53   53   44   56   38   41   45    46
 R08M |  578   12   14   14   22   15   16  ---    7 |    48   52   40   55   36   47  ---    44
 R09E | 3056   13   12   12   30   11   25  ---    9 |    25   20   25   34   27   36  ---    25
 R10E | 1525    9   12   10   13   25   13  ---    7 |    85   89   93   87   79   79  ---    84
 R11E | 1433    7   11   12   10   14   13   97    5 |    33   34   40   32   44   39   34    35
 R12E | 1009   13   16   13   12    7   18  ---    6 |    51   54   46   48   44   44  ---    45
 R13E | 2500    9   12   11   14   16   12  ---    6 |    25   28   26   27   32   28  ---    25
 R14E | 1940   10    9   17   15   16   24  ---    8 |    62   63   61   64   62   53  ---    59
 R15E | 1451   18   16   16   15   14   15  ---    8 |    38   39   44   43   40   39  ---    39
 R16E | 1179   17   27   25   68   53   37  ---   20 |    43   44   44   84   59   41  ---    40
 R17M | 1257   22   23   26   24   13   34  ---   12 |    39   39   36   44   32   25  ---    33
 R18  |  798   12   18   15   12   31   18  ---    9 |    30   28   29   31   38   25  ---    28
 R19  |  771   56   56   54   85   55   63  ---   31 |    50   59   50   49   37   30  ---    35
 R20  |  797   16   24   35   37   53   50  ---   18 |    48   53   34   60   42   32  ---    39
 R21M | 1529   20   16   24   26   30   48  169   14 |    44   43   37   56   53   26   70    40
 R22  |  654   21   14   34   25   30   43  ---   15 |    42   35   26   45   41   18  ---    32
 R23  |  561   19   25   23   14   11   22  ---    9 |    24   25   37   23   26   26  ---    25
 R24M |  765   16   27   13   61   69   21  ---   19 |    34   38   32   46   30   34  ---    30
XR26  | 6220   19   50  ---  ---  ---   35  ---   26 |    18   46  ---  ---  ---   25  ---    15
------+----------------------------------------------+------------------------------------------
 RMS  | 1373   22   25   24   33   31   30  172      |T   43   46   42   49   43   35   43    38
 WRMS | 1373   19   21   19   16   22   27  172      |NE  42   46   39   44   42   30   37    35
 MEDI | 1009   14   16   16   20   18   22  169      |MD  43   45   40   46   41   32   41    39

Table 3.2060.2  GPS week: 2060   Day: 2   MJD: 58666                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  esx  gfz  grg  iac  mcc  IGL |   cod  cof  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  525   62   49   65   28   35   30  ---   24 |    67   59   46   43   43   25  ---    36
 R02  |  675   16   20   17   10   11   14  270    7 |    42   43   30   34   35   34  102    33
 R03  |  725    9   15   16   14   22   22  191    8 |    46   50   36   45   51   29   72    41
 R04  | 1423   15   13   13   10   22   21  ---    8 |    45   42   31   42   46   38  ---    39
 R05M |  676   11   14   12   21   14   29  ---    9 |    41   42   46   55   42   32  ---    42
 R07  |  761    8   11   11   14   11   19  189    6 |    55   57   55   59   47   44   89    52
 R08M |  656    8   12    6   10   12   14  ---    5 |    51   50   48   50   47   54  ---    49
 R09E | 3129   14   23   13   13   11   22  ---    7 |    24   33   22   29   24   24  ---    22
 R10E | 2155   10   12   12   14   17   22  ---    7 |    53   52   48   54   51   49  ---    50
 R11E | 1284    9   11    9   17   31   17  109    8 |    43   42   42   42   58   57   32    46
 R12E | 1338   12   21   16   11   12   20  ---    7 |    42   45   44   47   44   40  ---    42
 R13E | 1391   10   11   14   14   21   15  ---    7 |    34   34   40   36   36   31  ---    33
 R14E | 1324    8   13   11   18   14   25  ---    7 |    35   36   37   44   39   30  ---    35
 R15E |  879   11   12   28   18   19   17  ---    9 |    36   40   57   45   35   45  ---    41
 R16E |  991   26   22   35   61   34   35  ---   20 |    53   69   62  109   66   59  ---    63
 R17M | 1171   19   26   22   16   18   38  ---   11 |    48   51   34   44   39   35  ---    38
 R18  |  639   18   16   15   30   13   29  ---   11 |    31   36   37   56   35   26  ---    35
 R19  |  868   59   63   75   57   33   78  ---   31 |    81   89   47   76   48   39  ---    50
 R20  | 1586   15   29   48   30   60   46  ---   20 |    63   70   35   71   79   39  ---    56
 R21M | 1595   18   20   15   10   23   46   75   12 |    54   53   40   49   55   29   69    44
 R22  |  610   11   11   31   24   36   46  ---   15 |    49   51   41   65   67   29  ---    49
 R23  |  916   23   18   28   13   12   18  ---   10 |    19   22   41   32   19   35  ---    26
 R24M | 1029   13   22   12   53   76   30  ---   21 |    36   44   34   35   37   33  ---    31
XR26  | 3983   13   46  ---  ---  ---   22  ---   16 |    20   36  ---  ---  ---   24  ---    19
------+----------------------------------------------+------------------------------------------
 RMS  | 1284   22   23   29   27   29   32  180      |T   44   47   41   50   45   36   72    40
 WRMS | 1284   19   20   20   14   22   29  180      |NE  47   50   39   52   47   32   87    39
 MEDI |  991   13   16   15   16   19   22  189      |MD  43   44   41   45   44   34   72    41

Table 3.2060.3  GPS week: 2060   Day: 3   MJD: 58667                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  esx  gfz  grg  iac  mcc  IGL |   cod  cof  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  611   34   41   57   27   46   47  ---   21 |    72   81   46   74   71   29  ---    56
 R02  |  727    7   15   11   15   10   19  281    6 |    52   61   51   57   52   42  148    51
 R03  |  957   11   11   16   14   18   21  241    7 |    56   55   38   58   60   45  147    51
 R04  |  625   10   12   14   12   14   25  ---    7 |    49   57   49   53   53   37  ---    48
 R05M | 1212   22   22   16   11   18   23  ---    9 |    41   53   49   44   53   41  ---    42
 R07  |  805    9    9   17   21    9   19  189    7 |    64   62   48   72   60   49  127    59
 R08M |  723    8   12   10   18   20   16  ---    7 |    60   63   56   70   53   59  ---    60
 R09E | 4345   13   12   13   14   12   14  ---    6 |    27   29   29   31   29   27  ---    25
 R10E | 3483   15   16   18   14   14   28  ---    8 |    87   91   90   88   85   79  ---    85
 R11E |  576   10    9   13   17   10   22   98    7 |    44   47   50   49   48   46   56    45
 R12E | 1721   12   22   12   10   15   21  ---    7 |    35   38   40   44   35   37  ---    36
 R13E | 2530   12   15   17   10   11   16  ---    6 |    31   30   32   36   28   29  ---    29
 R14E | 1718   16   21   10   17   12   21  ---    7 |    48   50   45   51   40   46  ---    44
 R15E | 1107   11    8   17   21   13   17  ---    8 |    33   34   35   45   39   36  ---    34
 R16E | 1296   25   26   25   36   38   32  ---   15 |    50   58   52   76   78   53  ---    57
 R17M |  965   18   20   33   27   22   45  ---   14 |   205  204  184  204  193  181  ---   194
 R18  |  615   20   19    7   14    7   26  ---    8 |    38   38   37   39   38   31  ---    35
 R19  |  756   53   54   79   60   34   84  ---   31 |    77   84   42   94   61   22  ---    56
 R20  | 1402   14   33   55   27   76   66  ---   24 |    83   98   45   92  119   41  ---    76
 R21M | 2018   18   24   29   14   27   40   42   12 |    69   74   48   67   73   48   60    60
 R22  |  740   15   20   22   14   29   47  ---   12 |    63   64   46   63   74   36  ---    56
 R23  |  696   25   13   24    5   15   10  ---    9 |    24   31   54   45   43   40  ---    38
 R24M |  737   21   24   19   31   62   41  ---   18 |   124  122  114   99  127  126  ---   116
XR26  | 3788    8   97  ---  ---  ---   17  ---   12 |    27  111  ---  ---  ---   37  ---    29
------+----------------------------------------------+------------------------------------------
 RMS  | 1627   20   23   29   22   29   35  192      |T   60   68   55   67   65   50  107    57
 WRMS | 1627   19   20   22   16   22   31  192      |NE  55   67   45   64   63   37  140    50
 MEDI |  957   14   19   17   15   15   22  189      |MD  50   58   48   58   53   41  127    51

Table 3.2060.4  GPS week: 2060   Day: 4   MJD: 58668                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  esx  gfz  grg  iac  mcc  IGL |   cod  cof  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  674   38   41   50   31   40   48  ---   21 |    68   70   32   70   54   28  ---    49
 R02  | 1052   16   16   20   19   11   14  153    8 |    43   44   37   53   39   38  170    40
 R03  |  700   10   14   17   11   17   19  159    7 |    49   53   40   50   52   41   92    45
 R04  | 1334   13   12   21    8   23   23  ---    9 |    46   43   29   37   48   25  ---    36
 R05M | 1218   17   15   21   17   17   30  ---   10 |    39   43   34   39   41   30  ---    32
 R07  |  958    8   13   11   20   10   21  174    7 |    55   59   49   65   42   42  117    50
 R08M | 1134   10   11   16   16   12   26  ---    8 |    52   51   64   63   52   43  ---    54
 R09E | 4531   12   18   15   18   13   16  ---    7 |    34   34   32   39   41   37  ---    34
 R10E | 1670   14   19   15   17   24   26  ---    9 |    83   81   92   89   81   73  ---    83
 R11E | 1657   10    8   10   15   22   17  137    7 |    29   28   29   31   33   26   54    26
 R12E | 1628   17   10   14   14   15   16  ---    7 |    45   47   46   50   52   41  ---    45
 R13E | 2473   18   20   12   23   27   20  ---   10 |    40   37   43   52   44   39  ---    40
 R14E | 1570   15   16   16   12   10   23  ---    8 |    37   36   33   35   33   33  ---    32
 R15E | 1232   10   12   12   18   15   18  ---    7 |    28   29   30   38   32   30  ---    28
 R16E | 2160   39   38   26   57   30   38  ---   19 |    53   58   59   91   67   57  ---    56
 R17M |  842   20   17   28   17   24   42  ---   13 |   496  495  493  495  508  492  ---   496
 R18  |  894   12   15    9   30   25   26  ---   10 |    34   36   37   50   47   31  ---    37
 R19  |  485   52   63   58   57   43   88  ---   29 |    79   85   53   80   69   33  ---    58
 R20  | 1281   16   50   33   35   38   45  ---   16 |    57   89   44   71   65   38  ---    53
 R21M | 1518   13   16   35   28   28   42   63   14 |    61   63   38   72   72   35   38    55
 R22  |  825   17   16   34   15   37   42  ---   15 |    55   56   42   60   71   31  ---    51
 R23  |  845   20   29   30   24   13   21  ---   11 |    28   32   48   30   40   29  ---    32
 R24M |  829   22   35   26   55   59   36  ---   20 |   307  306  313  315  320  297  ---   309
XR26  | 4694    8   44  ---  ---  ---   13  ---   10 |    39   52  ---  ---  ---   30  ---    37
------+----------------------------------------------+------------------------------------------
 RMS  | 1598   21   26   26   28   27   34  143      |T   77   80   74   85   82   66   94    74
 WRMS | 1598   19   22   24   16   23   31  143      |NE  50   56   41   56   52   33  126    44
 MEDI | 1218   15   16   20   18   23   23  153      |MD  46   51   42   53   52   35   92    45

Table 3.2060.5  GPS week: 2060   Day: 5   MJD: 58669                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  esx  gfz  grg  iac  mcc  IGL |   cod  cof  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  824   50   55   51   40   43   46  ---   23 |    55   63   25   58   40   19  ---    33
 R02  |  709    9   10   14   24   14   15  118    8 |    35   35   31   53   27   26  100    33
 R03  |  551   12   12   18    7   16   10  155    7 |    40   39   29   36   36   35   49    33
 R04  | 1864   13   19   15    7   14   14  ---    6 |    38   41   32   35   33   27  ---    32
 R05M | 1403   19   21   19   14   25   32  ---   11 |    32   33   24   24   39   29  ---    23
 R07  |  985   12   14   14   17   17   25  126    8 |    51   48   38   54   51   33   83    44
 R08M | 1453   13   11   12   26   28   42  ---   12 |    56   60   52   73   62   38  ---    54
 R09E | 4523   18   10   10   16   14   21  ---    8 |    46   44   42   50   46   53  ---    44
 R10E | 1790   18   22   11   23   20   24  ---    9 |   113  111  117  120  113   96  ---   112
 R11E |  606   16   11    9   10   14   17  184    6 |    44   51   52   49   51   53   67    48
 R12E | 1379   18   20   10   14   11   20  ---    7 |    58   59   62   61   59   62  ---    59
 R13E | 1250   41   36   21   23   25   23  ---   14 |   161  162  155  156  163  158  ---   156
 R14E | 2087   21   14   18   29   18   23  ---   11 |    50   44   39   47   38   41  ---    38
 R15E |  820   14   15   14   18   14   20  ---    8 |    32   35   39   38   34   34  ---    32
 R16E | 1152   27   29   23   48   43   42  ---   18 |    81   87   84   93   89   68  ---    78
 R17M | 1000   17   18   19   26   21   43  ---   12 |   808  806  803  808  804  806  ---   805
 R18  | 1086   13   11   14   13   44   33  ---   12 |    26   29   29   29   56   21  ---    27
 R19  |  409   61   53   69   64   58   82  ---   33 |    71   72   40   77   78   21  ---    52
 R20  |  662   14   41   16   39   41   35  ---   14 |    28   38   41   43   29   28  ---    29
 R21M |  978   21   27   23   22   18   39   69   12 |    44   45   34   46   39   30   36    36
 R22  |  740   15   21   41   21   52   36  ---   17 |    38   42   23   42   64   28  ---    34
 R23  |  749   26   35   26   27   26   25  ---   13 |    21   20   35   21   30   33  ---    24
 R24M | 1489   13   19   33   42   86   27  ---   22 |   492  502  498  494  487  485  ---   493
XR26  | 3520   11   33  ---  ---  ---   19  ---   14 |    30   50  ---  ---  ---   27  ---    27
------+----------------------------------------------+------------------------------------------
 RMS  | 1488   24   26   26   28   34   34  136      |T  102  104  101  109  107   93   67    97
 WRMS | 1488   19   22   26   20   32   30  136      |NE  39   43   32   44   44   27   77    33
 MEDI | 1000   16   19   18   23   21   25  126      |MD  44   45   39   50   51   33   67    36

Table 3.2060.6  GPS week: 2060   Day: 6   MJD: 58670                            

        Weighted Average                             Orbit Dynamics (7 days)
 PRN  |  brd  cod  cof  esx  gfz  grg  iac  mcc  IGL |   cod  cof  esx  gfz  grg  iac  mcc   IGL
------+----------------------------------------------+------------------------------------------
 R01  |  644   48   43   57   40   42   59  ---   25 |    83   81   38   76   59   32  ---    49
 R02  | 1041   11   18   12   29   26   28  139   10 |    57   59   46   72   49   41  112    51
 R03  |  926    8   11   17   24   18   29  188    9 |    66   68   62   81   60   48   31    63
 R04  |  753   13   11   18   18   17   27  ---    9 |    62   58   46   63   56   44  ---    53
 R05M | 1681   17   17   27   21   22   25  ---   11 |    56   58   52   63   57   37  ---    51
 R07  |  969   12   12   24   32   16   33  101   12 |    73   73   56   90   67   57   71    67
 R08M |  628   15   15   25   21   27   29  ---   11 |    81   87   86   96   90   75  ---    83
 R09E | 4252   13   14   10   17   25   11  ---    7 |    34   34   35   41   34   34  ---    33
 R10E | 1265   14   15   13   26   35   18  ---   10 |   117  117  114  118  114  114  ---   114
 R11E |  624   12   17   10   13   36   19   99    9 |    38   41   41   49   61   42   56    41
 R12E | 1276   15   19   18   16   16   27  ---    9 |    55   61   72   67   63   61  ---    62
 R13E | 1171   23   15   22   16   18   30  ---   11 |   128  132  142  142  128  126  ---   132
 R14E | 2204   14   13   14   20   24   13  ---    8 |    61   68   73   74   67   67  ---    66
 R15E |  956   13   16   13   14   24   22  ---    8 |    46   43   45   49   37   50  ---    42
 R16E |  837   19   30   17   30   27   25  ---   11 |    69   75   77   91   82   60  ---    73
 R17M |  843   17   19   19   15   17   34  ---   10 |  9999 9999 9999 9999 9999 9999  ---  9999
 R18  |  831   12   17   14   29   15   30  ---   10 |    41   39   44   60   56   35  ---    45
 R19  |  695   51   61   59   55   53   92  ---   30 |   100  106   43  105   97   25  ---    72
 R20  |  693   18   20   34   42   59   36  ---   18 |    61   61   50   78   79   28  ---    56
 R21M |  670   16   22   19   26   16   40   83   12 |    78   83   52   82   76   43   40    66
 R22  |  607   14   14   30   23   31   39  ---   13 |    71   72   41   76   85   37  ---    60
 R23  | 1599   25   16   28   13   18   14  ---   11 |    32   45   61   36   52   45  ---    41
 R24M | 1091   16   30   25   38   81   19  ---   19 |   700  708  702  694  709  678  ---   697
XR26  | 2898   10   39  ---  ---   28   21  ---   13 |    42   47  ---  ---    8   34  ---    42
------+----------------------------------------------+------------------------------------------
 RMS  | 1376   21   23   26   27   33   35  128      |T   93   96   89  104   95   78   62    89
 WRMS | 1376   18   20   21   23   34   31  128      |NE  62   64   48   73   60   38   71    54
 MEDI |  926   14   17   19   23   24   27  101      |MD  62   68   52   76   63   44   56    60



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