[IGSREPORT-24041] Wk 1869 IGLOS Final Orbits

IGS ACC igs.acc at noaa.gov
Thu Nov 19 16:59:15 PST 2015


Author:   AC Coordinator / NOAA NGS                                               
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1869   (Nov 01, 2015 - Nov 07, 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 2.1869.
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:
                                                                               
 igl1869[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1869 in the SP3 format.
 igl18697.sum      Combination Report for GPS Week 1869.


    
    
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  |     -1.7 ns
                1  |      1.3 ns
                2  |     -2.0 ns
                3  |     -9.1 ns
                4  |    -12.9 ns
                5  |     -0.7 ns
                6  |     -9.5 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  |  ESX   | R07
                1  |  ESX   | R07
                2  |  ESX   | R07

    
         
ORBIT COMBINATION AND EVALUATION STATISTICS:                                    
--------------------------------------------                                    
      
Table 1 summarizes all statistics for the week. It contains means and standard 
        deviations over the week of satellite ephemeris  and  clock correction
        transformation parameters for each centre (Tables 1.1869, 1a.1869).
        
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 2.1869.0-6)                                                                                
    
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 3.1869.0-6). 
        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 1869 summary.                      (Nov 01, 2015 - Nov 07, 2015)

Table 1.1869.a     GPS week : 1869   MJD: 57327.0-57333.0

         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|   -3     0    -8    57   -44   -57   .33   48   48 |     ---     ---    ---    ---
        |    2     0     2    21    31    28   .05           |     ---     ---
cof  n/a|   -3     0   -10    37   -50   -26   .30   50   50 |     ---     ---    ---    ---
        |    1     2     2    23    25    43   .03           |     ---     ---
emx  n/a|    0    -1     0   -28   -56    -6   .30   29   29 |       0    -259   3984   7551
        |    2     1     2    40    41    42   .05           |       0    1138
esx  n/a|    0     0    -1   -75    30   -54  -.11   22   19 |   -4214    -115   4310   8230
        |    1     1     1    17    31    46   .04           |    9889    2576
gfz  n/a|    0     0     2    53    66    40   .13   24   23 | -432398   -1857  39204 433010
        |    1     1     0    17    30    23   .05           |  530949    1790
grg  n/a|    0     1     6    30    14   -89  -.38   40   37 | -770735   -1378   4985 822117
        |    2     1     3    25    33    50   .05           |  214482    2047
iac  n/a|    1     0     0    20   -26    50  -.08   16   16 | -431932    -811   4302 433154
        |    0     0     0    30    38    36   .03           |  531387    1325
mcc  n/a|    2     0    33    65  -135  -104  -.26  149  149 |     ---     ---    ---    ---
        |   13     7    30    68   178   428   .58           |     ---     ---


Table 1.1869.b     GPS week : 1869   MJD: 57327.0-57333.0   

         Satellite position sigmas for the combined orbits
         (coded in the IGS SP3 orbit files).
         "E" flags eclipsing satellites.
         Units: mm.

              Day of GPS week
 PRN  |    0    1    2    3    4    5    6 |  Remarks
------+------------------------------------+------------------------------------------
 R01  |   13   12   12   12   12   15   15 |
 R02  |    8    8    8    8    8    9   10 |
 R03  |    8    8    8    8    8    7    9 |
 R04  |    8    9    9    8    8    9    9 |
 R05  |   13   14   11   10   15   13   13 |
 R06  |   11   10    9    9   10    8    8 |
 R07  |   28   18   14   12   10   12   10 |
 R08  |   10   10   10   10   11   10   10 |
 R09  |   15   17   15   11   14   15   16 |
 R10  |   11   11    8    9    7    9   11 |
 R11  |   18   18   20   19   19   18   17 |
 R12  |   17   15   17   18   18   22   17 |
 R13  |   12   10   11   12   14   13   12 |
 R14  |   18   16   17   15   14   14   18 |
 R15  |   13   10   10    9   10   10   10 |
 R16  |   11   10    9   10   10   10   13 |
 R18  |    8    8   11   10    9    9   11 |
 R19  |   11    9   10   11   11    9    9 |
 R20  |   11   12   12    9   13   12   11 |
 R21  |   10    9    9   10   12   13   11 |
 R22  |   10    8    9   10   12   14   13 |
 R23  |    9    9    9    9    9   11   10 |
 R24  |   12   11   16   10   15   10   11 |
 R26  |    0    0    0    0    0    0    0 |


Table 1.1869.c     GPS week : 1869   MJD: 57327.0-57333.0   

         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 1869 0   | -106    87     0     252     -73   -6328  83.9  2110  2110 |   -1717       0
brd 1869 1   |  -40   -63     1    -639    -193   -8219  80.6  2068  2068 |    1268       0
brd 1869 2   |   36   -12     1    -738    -903   -6161  84.7  1901  1901 |   -2040       0
brd 1869 3   |   41    15    78   -2341    -364   -2530  84.3  2093  2093 |   -9080       0
brd 1869 4   |   -1     6    27    -850   -1575    3558  83.4  2009  2009 |  -12917       0
brd 1869 5   |  -11    37   -10     168    -160    3725  83.6  1438  1438 |    -679       0
brd 1869 6   |    5    75   -39    1014     327    1540  83.6  1488  1488 |   -9522       0
-------------+------------------------------------------------------------+----------------
brd 1869 mean|  -10    20     8    -447    -420   -2059  83.4  1872  1872 |   -4955       0
brd 1869 sdev|   50    51    36    1070     628    5019   1.3   288   288 |    5435       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 2.1869.0  GPS week: 1869   Day: 0   MJD: 57327                            

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    -8    36   -56   -51   .26   46   43 |     ---     ---    ---    ---
cof  n/a|    0    -1    -7   -12   -34   -84   .31   46   44 |     ---     ---    ---    ---
emx  n/a|    0     0     0   -77   -72   -32   .26   29   28 |       0     647   3251   7031
esx  n/a|    0     0     0   -99    52   -86  -.11   19   18 |    9024     230   4066   8280
gfz  n/a|   -2     0     2    45    43    65   .19   22   26 | -999999   -2549  86815 999999
grg  n/a|   -3     1     2    59    33   -29  -.42   40   35 | -999999   -2607   4105 999999
iac  n/a|    1     0     0    72   -48    83  -.14   19   19 | -999999   -2221   4075 999999
mcc  n/a|   21    -4    85   131    -7   416  -.69  174  174 |     ---     ---    ---    ---

Table 2.1869.1  GPS week: 1869   Day: 1   MJD: 57328                            

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    47   -61   -92   .27   48   48 |     ---     ---    ---    ---
cof  n/a|   -2     2   -10    57   -75    -5   .29   52   51 |     ---     ---    ---    ---
emx  n/a|    0     0     1   -68   -44    -4   .24   27   28 |       0   -1041   3847   6427
esx  n/a|    0     0     0   -89    43   -31  -.09   21   19 |    7763   -3128   4706   6848
gfz  n/a|    0     1     1    29    80    68   .09   22   22 | -999999   -4002  75756 999999
grg  n/a|   -1    -1     4    64    68  -151  -.43   41   35 | -999999   -3994   4714 999999
iac  n/a|    0     0     0    42   -40    13  -.07   15   15 | -999999   -2047   4697 999999
mcc  n/a|    5    -8    55     8   -92  -710 -1.05  133  133 |     ---     ---    ---    ---

Table 2.1869.2  GPS week: 1869   Day: 2   MJD: 57329                            

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    -8    99   -48   -18   .33   49   42 |     ---     ---    ---    ---
cof  n/a|   -1     3   -13    56   -79     7   .27   52   44 |     ---     ---    ---    ---
emx  n/a|    2    -1     1   -37   -87    59   .35   31   29 |       0    1399   3619   7494
esx  n/a|    0     0     0   -92    -7   -85  -.10   20   18 |  -10823    1249   4015   8057
gfz  n/a|   -1     1     1    70    44    50   .06   23   22 | -999999    -118  94883 999999
grg  n/a|    0     2     5    33    14  -113  -.41   41   32 | -999999     705   4059 999999
iac  n/a|    0     0     0    17    19    45  -.08   16   16 | -999999     234   4052 999999
mcc  n/a|   15    -1    41   120    12  -433  -.78  116  116 |     ---     ---    ---    ---

Table 2.1869.3  GPS week: 1869   Day: 3   MJD: 57330                            

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|   -4     0   -10    59   -66   -71   .37   49   48 |     ---     ---    ---    ---
cof  n/a|   -3    -1   -11    33   -72   -87   .26   49   47 |     ---     ---    ---    ---
emx  n/a|    1    -1    -2   -53   -21   -23   .36   29   27 |       0   -1446   4746   8092
esx  n/a|    2    -1    -1   -65    28  -123  -.10   21   18 |   -9728   -1626   4737   8697
gfz  n/a|    0     0     3    54    72    27   .12   25   24 |   -8706   -2419   4621   7857
grg  n/a|   -2     3     9    13   -30  -133  -.33   39   40 | -598899   -2653   9282 688197
iac  n/a|    0     0     0    30   -50   107  -.03   13   13 |   -7338    -232   4744   8025
mcc  n/a|    0    -7    28   149  -250    -7  -.18  101  101 |     ---     ---    ---    ---

Table 2.1869.4  GPS week: 1869   Day: 4   MJD: 57331                            

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|   -6     0   -10    41   -74   -92   .35   49   51 |     ---     ---    ---    ---
cof  n/a|   -4    -3    -7    40   -50   -20   .32   49   50 |     ---     ---    ---    ---
emx  n/a|   -4     0    -4    19    16   -54   .31   29   31 |       0   -1396   4150   8449
esx  n/a|    2    -2    -3   -57    81    10  -.18   24   22 |  -12556   -2556   4404   9176
gfz  n/a|    0     1     3    59   128    47   .14   25   23 |  -10115   -2751   4198   8102
grg  n/a|   -1     1    12    33   -23   -52  -.30   39   40 | -604424    -805   4508 688145
iac  n/a|    2     0     1   -10   -78    18  -.05   15   15 |  -10481   -1569   4297   8423
mcc  n/a|   -3    -3     9   -31  -426   173   .14  108  108 |     ---     ---    ---    ---

Table 2.1869.5  GPS week: 1869   Day: 5   MJD: 57332                            

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|   -6     0   -10    49    14   -29   .34   50   54 |     ---     ---    ---    ---
cof  n/a|   -6    -2    -8    43   -20   -23   .29   51   55 |     ---     ---    ---    ---
emx  n/a|    0    -4     0    13   -87   -30   .32   28   30 |       0     625   4507   7632
esx  n/a|    0     0    -1   -64    21   -42  -.06   22   20 |     933    4345   4493   7996
gfz  n/a|    1     0     3    77    50    12   .13   25   19 |    -938    1258   4410   7453
grg  n/a|   -2     1     3    16    22   -33  -.44   41   42 | -592705    1785   4487 689440
iac  n/a|    1     2     1    -9    -7    68  -.09   17   17 |     553    1390   4491   7678
mcc  n/a|  -20    13    16    35  -249  -448   .43  183  183 |     ---     ---    ---    ---

Table 2.1869.6  GPS week: 1869   Day: 6   MJD: 57333                            

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|   -4     1    -4    69   -18   -48   .37   49   52 |     ---     ---    ---    ---
cof  n/a|   -4     3   -10    45   -21    25   .35   53   56 |     ---     ---    ---    ---
emx  n/a|   -1    -2     0     3   -96    41   .26   30   30 |       0    -603   3774   7735
esx  n/a|    0     0    -2   -59    -5   -19  -.12   23   20 |  -14111     681   3755   8559
gfz  n/a|    0    -1     3    38    48    13   .19   24   21 |   -7032   -2420   3748   7666
grg  n/a|    4     0     5    -8    19  -114  -.36   37   37 | -599126   -2081   3743 689043
iac  n/a|    0     0     0    -2    23    16  -.06   17   17 |   -6266   -1236   3763   7958
mcc  n/a|   -3     6    -6    42    64   281   .29  225  225 |     ---     ---    ---    ---

       
       
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 3.1869.0  GPS week: 1869   Day: 0   MJD: 57327                            

        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  | 1225   73   67   31   14   22   26   12  ---   12 |    84   83   32   24   19   19   22  ---    20
 R02  | 4906   38   38   17   13   17   18    7  131    7 |    73   73   43   51   35   32   41  103    42
 R03  | 1965   22   26   23   18   20   23   10  ---    8 |    77   78   59   77   58   54   68  ---    65
 R04  | 3136   26   33   16   16   21   24   10  ---    8 |    73   78   49   63   39   40   49  ---    50
 R05  |  682   37   34   30   25   28   51   20  ---   13 |    82   83   59   70   47   30   60  ---    55
 R06  | 3366   31   36   38   20   21   21   17  ---   11 |    60   62   63   91   73   58   74  ---    73
XR07  | 3777   50   65  ---  269   19  112   21  ---   28 |   100  118  ---   80   68   82   72  ---    70
 R08  |  785   50   51   22   15   25   20   15  ---   10 |    81   82   44   45   22   24   36  ---    37
 R09  |  840   42   60   42   24   20   63   26  ---   15 |    44   57   40   37   38   40   23  ---    25
 R10  |  770   35   46   28   25   13   24   19  ---   10 |    35   43   34   32   25   18   24  ---    20
 R11  | 2279  101   95   37   14   29   45   29  ---   17 |   107  104   52   30   28   28   23  ---    26
 R12  |  745   83   84   34   17   41   47   20   75   16 |    95   95   43   37   30   37   17   27    25
 R13  |  744   64   47   20   17   27   31   16  ---   12 |    70   62   36   30   22   19   15  ---    21
 R14  |  919   37   35   59   21   23   83   18  ---   17 |    42   41   32   47   40   28   27  ---    32
 R15  | 5270   33   40   16   33   32   25   22  ---   12 |    40   50   35   38   35   31   31  ---    29
 R16  |  895   29   27   30   13   21   48   21  ---   11 |    34   34   44   37   26   29   29  ---    25
 R18  |  593   27   30   19   12   14   28   11  102    7 |    49   49   36   31   21   31   25   81    25
 R19  | 2218   39   42   38    8   26   30   11  ---   10 |    55   57   46   31   23   22   17  ---    23
 R20  |  974   19   19   18   12   18   56   25  ---   11 |    35   43   38   35   35   22   29  ---    28
 R21  | 1100   26   28   15   13   15   35   26  296    9 |    62   62   43   41   50   48   24  152    37
 R22  |  593   40   39   13   16   10   41   18  ---    9 |    65   64   40   42   30   21   23  ---    31
 R23  |  742   19   20   18   24   11   24   16  ---    8 |    25   26   31   53   35   27   34  ---    34
 R24  |  961   21   30   22   31   15   48   25  ---   12 |    56   65   41   69   45   12   43  ---    44
XR26  | ----  ---  ---  ---  ---  ---  ---    7  ---    0 |   ---  ---  ---  ---  ---  ---   54  ---    55
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 2110   46   46   29   19   22   40   19  174      |T   62   65   42   47   36   32   35   90    37
 WRMS | 2110   43   44   28   18   26   35   19  174      |NE  62   65   42   47   36   32   35   90    37
 MEDI |  961   37   38   22   17   21   31   18  102      |MD  62   62   41   41   35   29   29   81    31

Table 3.1869.1  GPS week: 1869   Day: 1   MJD: 57328                            

        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  | 1441   72   85   31   15   26   32   10  ---   12 |    71   82   30   28   19   25   19  ---    20
 R02  | 3750   38   40   16   14   16   30    7  123    7 |    64   67   46   51   37   38   39   58    42
 R03  | 1176   16   18   22   20   17   18    8  ---    7 |    62   66   51   61   49   56   53  ---    53
 R04  | 3395   30   21   17   20   26   22   12  ---    9 |    56   51   42   49   29   34   41  ---    38
 R05  |  740   33   39   32   23   27   66   21  ---   13 |    60   66   41   50   45   43   47  ---    41
 R06  | 2695   30   35   27   26   13   32   17  ---   10 |    42   40   49   70   49   45   56  ---    53
XR07  | 6771   55   51  ---  250   23   53   16  102   17 |    77   72  ---   59   36   75   56   86    49
 R08  |  866   55   51   19   14   24   25   12  ---    9 |    68   66   37   38   31   22   31  ---    32
 R09  | 1165   38   31   39   29   31   68   32  ---   16 |    42   48   58   52   48   53   29  ---    34
 R10  |  916   42   49   21   26   19   42   11  ---   10 |    38   44   31   27   29   40   20  ---    22
 R11  | 2477  106  119   48   22   36   39   16  ---   17 |    75   87   42   31   29   26   19  ---    19
 R12  |  846   94   91   31   15   33   22   25   86   15 |    74   73   38   33   30   26   21   52    24
 R13  |  974   56   88   18   17   16   30   13  ---    9 |    47   72   26   27   21   18   16  ---    18
 R14  |  895   28   23   52   25   14   74   21  ---   15 |    27   28   34   42   30   21   27  ---    23
 R15  | 5691   35   34   19   23   23   39   10  ---   10 |    40   40   33   37   31   23   25  ---    28
 R16  | 1120   22   31   19   24   24   43   12  ---   10 |    28   35   31   43   37   25   26  ---    28
 R18  |  692   32   36   23    9   16   27   13  112    8 |    32   35   29   21   23   18   15   76    17
 R19  | 2144   39   37   23    8   20   29   13  ---    8 |    39   38   28   23   22   25   19  ---    19
 R20  | 1406   14   21   26   20   13   69   18  ---   11 |    21   31   35   31   26   19   22  ---    22
 R21  |  841   51   51   21   13   15   26    9  189    8 |    51   51   34   33   41   32   31   84    31
 R22  |  707   41   38   18    9   12   17   13  ---    7 |    43   41   31   24   36   25   21  ---    24
 R23  | 1218   17   27   25   30   12   22    8  ---    9 |    21   23   18   42   24   20   26  ---    23
 R24  | 1513   34   17   17   27   18   56   15  ---   11 |    48   30   22   37   22   17   29  ---    22
XR26  | ----  ---  ---  ---  ---  ---  ---    3  ---    0 |   ---  ---  ---  ---  ---  ---   76  ---    77
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 2068   48   52   27   21   22   41   15  133      |T   48   51   35   39   32   31   31   71    31
 WRMS | 2068   48   51   28   19   22   35   15  133      |NE  48   51   35   39   32   31   31   71    31
 MEDI | 1176   38   37   22   20   19   32   13  112      |MD  47   48   34   37   30   25   26   76    24

Table 3.1869.2  GPS week: 1869   Day: 2   MJD: 57329                            

        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  | 2022   74   63   23   11   26   27   16  ---   11 |    80   73   34   30   21   25   21  ---    23
 R02  | 3301   32   29   20   16   18   20   10   99    7 |    62   61   53   47   33   32   37   37    40
 R03  | 1360   17   21   25   13   16   27   11  ---    7 |    66   66   50   62   57   49   64  ---    58
 R04  | 2896   29   34   31   19   17   20   10  ---    9 |    67   72   46   53   42   39   43  ---    45
 R05  |  632   34   35   29   24   16   34   18  ---   10 |    86   89   48   70   65   48   49  ---    57
 R06  | 1338   29   30   21   23   21   16   15  ---    9 |    51   54   65   75   48   54   65  ---    62
XR07  | 2593   55   52  ---  254   21   30    8   66   13 |    87   90  ---  112   46   64   56   32    55
 R08  |  625   52   53   15   18   24   32    8  ---    9 |    74   76   30   45   30   22   30  ---    33
 R09  | 1543   43   41   46   19   31   69   17  ---   15 |    41   36   35   37   35   31   21  ---    24
 R10  | 1183   34   39   21   14   22   21   12  ---    8 |    36   41   33   24   24   22   19  ---    20
 R11  | 1512   93   97   38   36   32   65   33  ---   19 |    87  100   57   74   58   28   24  ---    44
 R12  |  898  102  121   36   25   32   42   27   84   17 |    83  100   33   43   29   27   16   26    21
 R13  |  962   62   40   16   16   21   35   14  ---   10 |    59   45   32   25   22   37   17  ---    20
 R14  | 1198   51   50   63   32   15   67   19  ---   17 |    38   37   33   58   42   30   35  ---    33
 R15  | 5567   36   41   16   20   32   34   15  ---   10 |    37   42   33   29   32   22   20  ---    22
 R16  | 1607   28   29   16   16   20   43   11  ---    9 |    32   35   29   36   34   27   21  ---    26
 R18  |  652   38   36   29   16   33   32   12   90   10 |    42   42   32   26   22   19   11   41    14
 R19  | 1645   43   48   28   12   22   27   15  ---    9 |    51   55   36   39   28   31   26  ---    30
 R20  | 1224   23   46   32   17   19   66   14  ---   12 |    36   42   38   36   30   21   18  ---    24
 R21  |  597   46   56   25   10   18   29    7  170    8 |    50   61   42   28   28   34   27   65    28
 R22  |  733   48   53   29    9   17   20   10  ---    8 |    45   52   34   19   21   17   17  ---    18
 R23  |  998   26   24   28   24   12   20   13  ---    9 |    21   33   22   42   40   26   35  ---    31
 R24  | 1539   26   54   50   28   22   68   24  ---   15 |    51   79   57   52   35   19   40  ---    38
XR26  | ----  ---  ---  ---  ---  ---  ---    3  ---    0 |   ---  ---  ---  ---  ---  ---   47  ---    48
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1901   49   52   31   20   23   41   16  116      |T   55   60   39   46   35   31   31   40    33
 WRMS | 1901   42   44   29   18   22   32   16  116      |NE  55   60   39   46   35   31   31   40    33
 MEDI | 1338   38   41   28   18   21   32   13   90      |MD  51   55   34   42   33   28   26   37    30

Table 3.1869.3  GPS week: 1869   Day: 3   MJD: 57330                            

        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  | 1252   74   84   25   15   30   29   10  ---   11 |    85   95   39   35   34   30   22  ---    28
 R02  | 1636   37   35   21   16   19   24   11  100    8 |    74   76   48   57   39   33   45   32    46
 R03  |  800   19   15   19   19   18   37   10  ---    8 |    77   74   54   77   61   55   67  ---    65
 R04  | 1776   32   31   30   14   21   20    5  ---    8 |    82   84   58   61   51   46   53  ---    55
 R05  |  694   32   28   33   18   16   22   16  ---    9 |    87   90   69   71   62   67   63  ---    65
 R06  | 1404   24   26   27   21   18   28    9  ---    8 |    65   67   75   92   67   62   78  ---    76
 R07  | 1567   52   51   48   15   25   33    9  133   12 |    97   93   53  120   41   55   51   54    55
 R08  |  442   56   53   21   17   22   34    9  ---    9 |    83   83   43   51   34   32   40  ---    41
 R09  | 1257   38   41   29   11   21   60    9  ---   10 |    39   49   37   40   39   37   27  ---    31
 R10  | 1375   31   35   22   19   14   38    8  ---    8 |    42   46   39   38   32   23   29  ---    29
 R11  |  766   94   90   38   37   34   80   18  ---   18 |    93   93   51   64   57   34   33  ---    40
 R12  | 1052   92   83   35   42   35   56   25   90   18 |    91   88   54   79   49   27   28   33    43
 R13  |  644   68   71   23   16   28   37   16  ---   11 |    54   58   31   26   31   40   22  ---    21
 R14  | 1574   51   47   54   29   34   49   13  ---   15 |    47   49   37   54   38   26   23  ---    30
 R15  | 8440   33   37   15   17   20   30   14  ---    8 |    43   50   29   28   29   28   23  ---    22
 R16  |  847   30   27   17   25   24   40   12  ---   10 |    36   34   29   40   28   32   26  ---    25
 R18  |  734   35   39   24   19   21   33   14   71    9 |    37   40   28   29   30   23   11   47    15
 R19  | 1006   54   58   31   11   35   22    8  ---   10 |    52   55   37   19   32   20   15  ---    14
 R20  | 1055   22   47   22   18   19   40   15  ---    9 |    37   64   33   34   31    8   19  ---    22
 R21  |  530   48   40   25   17   21   29   16  102   10 |    60   54   48   40   30   19   20   59    26
 R22  |  818   43   37   18   19   36   29   12  ---   10 |    56   52   37   38   26   21   34  ---    28
 R23  | 1762   22   24   26   24   13   31   10  ---    9 |    21   27   30   46   37   31   30  ---    31
 R24  |  900   25   22   33   18   19   35   17  ---   10 |    42   48   66   44   47   33   30  ---    38
XR26  | ----  ---  ---  ---  ---  ---  ---    6  ---    0 |   ---  ---  ---  ---  ---  ---   92  ---    92
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 2092   49   49   29   21   25   39   13  101      |T   60   63   44   51   40   34   36   45    39
 WRMS | 2092   48   47   27   18   24   40   13  101      |NE  60   63   44   51   40   34   36   45    39
 MEDI | 1052   37   39   25   18   21   33   11  100      |MD  56   58   39   44   37   32   29   47    31

Table 3.1869.4  GPS week: 1869   Day: 4   MJD: 57331                            

        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  | 1119   65   80   26   30   24   24   14  ---   12 |    72   85   36   50   38   23   24  ---    30
 R02  |  942   39   46   16   16   21   23    9   92    8 |    76   82   46   58   51   36   50   32    49
 R03  | 1419   21   31   14   16   16   31   13  ---    7 |    62   76   60   69   56   39   63  ---    58
 R04  |  882   34   40   19   13   14   23   10  ---    7 |    73   77   51   54   43   37   43  ---    46
 R05  |  924   34   38   48   24   27   51   18  ---   14 |    78   83   51   70   68   52   63  ---    58
 R06  | 1311   19   18   26   25   13   30   14  ---    9 |    65   72   69   89   76   51   69  ---    71
 R07  | 1707   50   50   19   19   26   25   12  191   10 |    87   87   36   74   40   55   49   97    55
 R08  |  586   51   57   24   17   26   22   15  ---   10 |    76   80   51   48   26   29   36  ---    38
 R09  |  845   40   37   33   26   26   61   19  ---   14 |    39   41   28   38   29   29   24  ---    20
 R10  |  902   25   19   12   17   16   25   11  ---    7 |    32   29   26   34   28   19   20  ---    23
 R11  | 1571   99   92   41   36   37   58   18  ---   18 |    75   72   37   57   47   26   24  ---    29
 R12  | 1128   87   89   44   30   45   46   22   85   18 |    77   82   43   56   48   24   27   79    33
 R13  |  752   79   69   22   27   22   52   17  ---   14 |    71   65   36   44   30   37   21  ---    27
 R14  | 1571   55   50   27   40   22   40   17  ---   13 |    48   50   44   49   25   30   19  ---    27
 R15  | 7809   34   25   17   22   30   39    9  ---   10 |    32   31   23   26   33   36   17  ---    19
 R16  |  997   31   29   12   23   27   37   16  ---   10 |    31   32   31   43   46   30   24  ---    29
 R18  |  863   43   39   27   12   16   19   13   64    9 |    36   36   29   21   28   24   16   85    16
 R19  | 1085   49   53   20   22   30   35   12  ---   11 |    44   47   28   30   34   37   16  ---    17
 R20  |  939   32   26   39   27   27   42   16  ---   13 |    42   41   32   32   37   15   21  ---    20
 R21  |  658   46   47   40   13   26   15   17   50   11 |    41   40   34   26   30   22   16   71    17
 R22  |  720   40   45   33   20   24   39   19  ---   12 |    48   53   45   39   27   25   16  ---    24
 R23  | 2635   23   32   19   28   19   25   10  ---    9 |    20   23   24   46   25   25   27  ---    25
 R24  | 1040   19   19   44   22   21   72   15  ---   14 |    38   35   40   47   39   36   29  ---    32
XR26  | ----  ---  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---  ---  200  ---   201
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 2009   49   49   29   24   25   39   15  108      |T   54   57   39   47   39   32   38   72    40
 WRMS | 2009   51   50   31   22   23   40   15  108      |NE  54   57   39   47   39   32   38   72    40
 MEDI |  997   40   40   26   22   24   35   14   85      |MD  48   53   36   47   37   30   24   79    29

Table 3.1869.5  GPS week: 1869   Day: 5   MJD: 57332                            

        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  |  922   65   55   35   27   34   24   23  ---   14 |    64   59   37   42   38   14   18  ---    24
 R02  |  910   49   55   14   17   18   24   13  108    9 |    68   75   41   48   40   31   37   40    39
 R03  | 2247   11   12   17   18   15   23   11  ---    7 |    60   55   50   64   53   52   59  ---    55
 R04  | 1473   38   39   23   19   18   22   14  ---    9 |    71   70   54   55   44   34   43  ---    46
 R05  | 1892   33   31   27   26   24   57   23  ---   13 |    71   70   45   61   51   36   55  ---    49
 R06  | 1610   25   19   20   18   12   32   10  ---    8 |    55   61   60   64   60   52   59  ---    58
 R07  | 2622   52   51   32   21   16   36   16  237   11 |    84   82   27   69   54   41   46   69    52
 R08  |  629   54   53   18   19   21   18   15  ---   10 |    72   70   39   47   32   30   28  ---    35
 R09  |  810   25   32   33   30   22   82   20  ---   15 |    32   36   28   42   34   22   30  ---    28
 R10  |  914   25   25    8   27   14   34   10  ---    8 |    24   25   23   34   24   33   19  ---    20
 R11  | 1078   98   96   42   19   42   41   26  ---   18 |    72   70   38   39   46   27   17  ---    25
 R12  | 1348  106   95   51   37   53   50   25   96   21 |    71   66   44   70   69   19   27   35    38
 R13  |  594   75   93   29   18   24   37   18  ---   13 |    65   81   40   40   33   27   19  ---    29
 R14  | 1262   57   51   22   34   22   56   19  ---   14 |    54   53   38   40   36   47   20  ---    27
 R15  | 2603   26   35   16   21   34   30    8  ---    9 |    26   34   25   23   30   25   15  ---    16
 R16  | 1313   32   31   18   21   18   38   16  ---    9 |    34   38   26   34   26   32   23  ---    23
 R18  |  596   36   37   21   10   17   32   15  226    8 |    28   31   22   18   25   27   14   89    12
 R19  |  920   47   45   18   13   18   23   12  ---    8 |    37   35   14   23   21   18   15  ---    13
 R20  |  777   20   35   29   26   19   61   15  ---   12 |    27   41   27   28   22   20   21  ---    15
 R21  |  778   46   52   39   21   38   28   14  195   13 |    44   51   36   36   40   33   22   63    26
 R22  | 1062   58   58   39   16   28   37   28  ---   14 |    42   41   30   25   29   23   31  ---    20
 R23  | 2185   23   24   25   21   14   45   18  ---   10 |    18   19   20   30   18   38   22  ---    18
 R24  | 1408   18   30   23   18   16   54   14  ---   10 |    25   36   35   34   27   15   33  ---    26
XR26  | ----  ---  ---  ---  ---  ---  ---    4  ---    0 |   ---  ---  ---  ---  ---  ---   76  ---    76
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1438   50   51   28   22   25   41   17  182      |T   49   52   34   42   37   30   31   59    32
 WRMS | 1438   54   55   30   20   19   42   17  182      |NE  49   52   34   42   37   30   31   59    32
 MEDI | 1078   38   39   23   21   19   36   15  195      |MD  54   53   36   40   34   30   23   63    26

Table 3.1869.6  GPS week: 1869   Day: 6   MJD: 57333                            

        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  |  629   67   71   35   29   35   35   24  ---   15 |    83   90   51   51   40   14   20  ---    29
 R02  |  529   56   52   16   14   21   33    8  105   10 |    96   94   61   61   44   40   49   44    53
 R03  | 1879   19   18   20   21   22   27   10  ---    8 |    81   83   72   88   69   61   77  ---    75
 R04  | 2057   42   48   17   18   19   25   11  ---    9 |    91   95   54   68   47   40   54  ---    55
 R05  | 1517   42   44   30   20   26   47   21  ---   12 |   101   98   68   72   51   49   68  ---    63
 R06  | 3669   20   31   23   23   11   16    9  ---    7 |    74   73   73  102   84   82   87  ---    85
 R07  | 2072   57   63   24   11   20   21   14  268   10 |   109  114   34   84   51   62   60   65    64
 R08  |  897   51   55   24   19   11   22   16  ---    9 |    98  102   69   64   42   35   41  ---    52
 R09  |  703   44   32   53   27   21   51   20  ---   15 |    36   40   23   36   34   24   26  ---    23
 R10  | 1049   22   31   25   31   25   27   19  ---   11 |    34   34   28   37   33   26   21  ---    23
 R11  |  737   98   97   36   22   34   46   23  ---   17 |    94   93   51   41   32   25   21  ---    28
 R12  |  794   92  105   42   29   33   40   21  186   17 |    96  103   48   50   49   22   23   42    30
 R13  |  696   64   75   25   23   28   29   12  ---   12 |    68   80   37   37   29   16   21  ---    23
 R14  | 1472   39   46   53   27   30   73   24  ---   17 |    46   56   44   53   41   20   27  ---    31
 R15  | 2476   23   29   11   24   31   19   15  ---    9 |    32   37   23   35   28   23   18  ---    22
 R16  | 1351   26   35   19   35   24   63   12  ---   13 |    37   43   32   38   28   38   23  ---    23
 R18  |  892   48   49   31    9   18   23   19  195   10 |    41   43   26   15   23   23   22   46    13
 R19  | 1176   43   42   20   11   11   26   18  ---    9 |    53   54   27   22   30   27   15  ---    15
 R20  |  862   24   27   18   27   15   48   16  ---   10 |    32   33   21   41   27   23   20  ---    19
 R21  |  794   46   47   23   17   23   37   15  313   10 |    52   52   32   24   28   23   26   73    20
 R22  |  650   55   59   35   20   34   28   18  ---   13 |    57   61   43   29   33   25   24  ---    22
 R23  | 1676   18   19   32   28   13   19   14  ---    9 |    22   22   22   47   25   27   30  ---    26
 R24  | 1198   21   37   27   30   17   35   17  ---   11 |    38   41   37   61   38   31   39  ---    39
XR26  | ----  ---  ---  ---  ---  ---  ---    2  ---    0 |   ---  ---  ---  ---  ---  ---   57  ---    57
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1487   49   53   30   23   24   37   17  225      |T   63   67   42   50   39   32   36   54    37
 WRMS | 1487   52   56   30   20   21   37   17  225      |NE  63   67   42   50   39   32   36   54    37
 MEDI | 1049   43   46   25   23   22   29   16  195      |MD  57   61   37   47   34   26   26   46    28




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