[IGSREPORT-24242] Wk 1881 IGLOS Final Orbits

IGS ACC acc at igs.org
Tue Feb 16 17:11:36 PST 2016


Author:   AC Coordinator / GA MIT                                              
sum-file Version 2.0
                                                                               
IGLOS Orbit Combination - Week 1881   (Jan 24, 2016 - Jan 30, 2016) 
                                                                               
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 2.1881.
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:
                                                                               
 igl1881[0-6].sp3  IGLOS-PP Glonass ephemerides files for days 0-6
                   of GPS Week 1881 in the SP3 format.
 igl18817.sum      Combination Report for GPS Week 1881.


    
    
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  |     -3.2 ns
                1  |      5.2 ns
                2  |      4.3 ns
                3  |     15.8 ns
                4  |      0.3 ns
                5  |     -4.2 ns
                6  |     -8.6 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
               ----+--------+---------------
                3  |  COD   | R10

    
         
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 1.1881, 1a.1881).
        
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 2.1881.0-6)                                                                                
    
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 3.1881.0-6). 
        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 1881 summary.                      (Jan 24, 2016 - Jan 30, 2016)

Table 1.1881.a     GPS week : 1881   MJD: 57411.0-57417.0

         Mean and standard deviations of transformation parameters to the 
         combined IGL orbit.
         WRMS - orbit RMS weighted by the SP3 header accuracy codes.
         STA  - Mean number of stations in the daily solutions.
   
CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
cod  n/a|   -2     0    -3    25    -3    -9   .37   35   29 |     ---     ---    ---    ---
        |    1     1     2    13    20    39   .04           |     ---     ---
cof  n/a|   -2     0    -4     7   -20     0   .29   38   31 |     ---     ---    ---    ---
        |    1     0     3    25    25    68   .07           |     ---     ---
emx  n/a|    0     0    -2   -59   -33   -82   .29   26   27 |       0    1294   3789   7605
        |    1     1     3    27    36    33   .02           |       0     989
esx  n/a|    0     0     5   -22   -29   -15  -.08   20   18 |    -535    1557   4029   8259
        |    1     1     1    16    15    55   .02           |    8372    2169
gfz  n/a|    0    -1    -6    39    60    41  -.00   22   18 | -141610    1755   4828 432828
        |    1     1     1    12    20    30   .05           |  155966    2173
grg  n/a|   -1     2    -1   -11    -3    15  -.38   41   35 | -656522    1202   7226 778679
        |    1     2     4    36    21    40   .07           |  119721    1830
iac  n/a|    2     0     4    25     4     6  -.12   21   21 | -118908    -829   4155 432911
        |    0     0     2    28    35    85   .02           |  157644    1115
mcc  n/a|    1     0    11    16    -8   357  -.33  149  149 |     ---     ---    ---    ---
        |    6     6    15    88    86   437   .35           |     ---     ---


Table 1.1881.b     GPS week : 1881   MJD: 57411.0-57417.0   

         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  |    9   11    9    8    8   10   11 |
 R02  |    8   10    7    8    6    6    5 |
 R03  |    7    8    8    7    7    7    6 |
 R04  |    6    7    6    9    7    7    5 |
 R05  |   15   13   16   11   12   13   15 |
 R06  |    7    9    7    7   10    8   16 |
 R07  |    9    8   10    9    8    7   11 |
 R08  |    7    9    9    8    9    8   10 |
 R09  |   12   13   13   13   14   15   13 |
 R10  |    9    9  187 2850   29   13   11 |
 R11  |   16   16   16   16   16   15   14 |
 R12  |   18   14   14   15   15   16   15 |
 R13  |    9    9    9   30    9    9   10 |
 R14  |   13   17   15   15   16   19   25 |
 R15  |   11   11   12   12   11   11   11 |
 R16  |   11    9   11   10   11   10   10 |
 R17  |  ---  ---  ---    0  105   76   92 |
 R18  |    8    9   12   11   12   12    9 |
 R19  |   10    8   10   11   10   11   12 |
 R20  |   12   13   15   16   13   13   18 |
 R21  |   11   10    9    9   11   11   12 |
 R22  |   12   11   10   13   11   12   13 |
 R23  |   11   11   10    9   10   11   11 |
 R24  |   12   14   12   10   11   13   16 |
 R26  | 1441    0 2445  115 2054 2790  339 |
 R27  |    0    0    0    0  ---  ---  --- |


Table 1.1881.c     GPS week : 1881   MJD: 57411.0-57417.0   

         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 1881 0   |  -23   -25    -3     677     727     739  85.0  3222  3222 |   -3156       0
brd 1881 1   |  -23   -37   -24    1107    -875    -667  84.8  2297  2297 |    5209       0
brd 1881 2   |   55   -48    17     472   -1081   -1774  84.5  1523  1523 |    4274       0
brd 1881 3   |   50    62    -8     114    -357   -1580  84.7  1203  1203 |   15769       0
brd 1881 4   |  -25   -94    55     355     200   -2990  84.6  1351  1351 |     293       0
brd 1881 5   |   18    23    81     -47     856   -5627  83.3  1526  1526 |   -4186       0
brd 1881 6   |  101    31    78     230    1596   -3176  84.8  1312  1312 |   -8599       0
-------------+------------------------------------------------------------+----------------
brd 1881 mean|   21   -12    28     415     152   -2153  84.5  1776  1776 |    1372       0
brd 1881 sdev|   49    54    43     385     978    2035    .6   731   731 |    7983       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 2.1881.0  GPS week: 1881   Day: 0   MJD: 57411                            

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    -4    40     3    38   .40   35   27 |     ---     ---    ---    ---
cof  n/a|   -1    -1    -2    35   -25    56   .40   38   30 |     ---     ---    ---    ---
emx  n/a|    0     0    -3   -57   -97   -58   .28   22   22 |       0     -18   3983   9313
esx  n/a|    1    -1     5   -11   -29    60  -.08   23   21 |   -4454   -1160   3981   9980
gfz  n/a|   -2     0    -5    52    65    71  -.02   20   14 |  -22827    -590   3959   9461
grg  n/a|    0     0     0   -58     0     4  -.32   34   32 | -585284   -1113  10193 688730
iac  n/a|    2     1     4    11    62  -121  -.12   20   20 |     953   -2770   3991   9698
mcc  n/a|    1     8   -18   -96    77   -82   .27  193  193 |     ---     ---    ---    ---

Table 2.1881.1  GPS week: 1881   Day: 1   MJD: 57412                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
cod  n/a|   -2     0    -5     4     1   -46   .37   35   27 |     ---     ---    ---    ---
cof  n/a|   -3    -1    -5    -7    14    14   .37   37   28 |     ---     ---    ---    ---
emx  n/a|    0    -2    -2   -53   -27   -67   .26   23   24 |       0    1529   4178   7442
esx  n/a|    0     0     6   -14   -24    62  -.08   21   19 |    2895    2082   4178   8115
gfz  n/a|    0    -3    -7    16    28    55   .03   22   18 |  -14808    1947   4109   7259
grg  n/a|    0     3     3   -27     2    33  -.42   34   32 | -578060    1636   8917 688907
iac  n/a|    1     0     3    45    22   -55  -.16   19   19 |    5940     -65   4192   7318
mcc  n/a|    1    11    20    29   -26   137  -.63  120  120 |     ---     ---    ---    ---

Table 2.1881.2  GPS week: 1881   Day: 2   MJD: 57413                            

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    -7    19   -24    -9   .41   36   30 |     ---     ---    ---    ---
cof  n/a|   -2     0    -4    20   -14   -26   .28   38   32 |     ---     ---    ---    ---
emx  n/a|    0     0     1   -91   -13  -145   .30   26   26 |       0     539   3932   6645
esx  n/a|    1     0     4    -5   -49   -38  -.07   17   16 |    3021   -1030   3945   7163
gfz  n/a|    0    -3    -9    45    89    34   .05   25   20 |  -15906      78   3843   6496
grg  n/a|   -1     1    -8    10     0    -2  -.44   38   37 | -582115      -9   8154 690255
iac  n/a|    1     0     3    58    -4    90  -.12   19   19 |    5998   -1208   3949   6700
mcc  n/a|  -12    -4    28   -19    40   -69  -.50  108  108 |     ---     ---    ---    ---

Table 2.1881.3  GPS week: 1881   Day: 3   MJD: 57414                            

CENT STA|   DX    DY    DZ    RX    RY    RZ   SCL  RMS  WRMS|    TOFT   TDRFT   SDEV    RMS
        |  [mm]  [mm]  [mm] [uas] [uas] [uas] [ppb] [mm] [mm]|    [ps]  [ps/d]   [ps]   [ps]
--------+----------------------------------------------------+------------------------------
cod  n/a|    0     0    -4    39     4   -16   .31   37   32 |     ---     ---    ---    ---
cof  n/a|    0     0   -10    32    -2    27   .25   41   35 |     ---     ---    ---    ---
emx  n/a|    1    -1    -6   -31   -43   -59   .30   27   28 |       0    2259   3694   6999
esx  n/a|    0     1     3   -52   -15   -75  -.11   19   18 |   12206    1277   3710   7375
gfz  n/a|    1     0    -3    46    40    63   .01   21   17 |  -12874    3017   3606   6585
grg  n/a|   -3     2     0    23     5    71  -.45   58   33 | -587790    3588   3702 691341
iac  n/a|    1     0     5   -14     4   -56  -.12   21   21 |   16782    -359   3707   6668
mcc  n/a|    2    -7    22   -48    -6    87  -.63  123  123 |     ---     ---    ---    ---

Table 2.1881.4  GPS week: 1881   Day: 4   MJD: 57415                            

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    -3    23    23   -30   .36   35   28 |     ---     ---    ---    ---
cof  n/a|   -2     0    -2   -38   -13  -141   .29   40   31 |     ---     ---    ---    ---
emx  n/a|    3    -1    -7   -40   -58   -89   .31   27   29 |       0    1187   4012   7266
esx  n/a|   -2     1     4   -19   -51   -25  -.05   19   16 |     864    4701   5027   7866
gfz  n/a|    0     0    -4    37    76   -21  -.01   19   17 | -308795    5170   6465 999999
grg  n/a|   -3     1     1     4   -46    35  -.41   34   35 | -599415    1138   4016 691523
iac  n/a|    3     0     8    10    21    92  -.11   21   21 | -290949   -1087   4209 999999
mcc  n/a|    3     0    16     6   -62   909  -.56  154  154 |     ---     ---    ---    ---

Table 2.1881.5  GPS week: 1881   Day: 5   MJD: 57416                            

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    -1    32     1   -52   .34   34   29 |     ---     ---    ---    ---
cof  n/a|   -2     0     0     9   -36    25   .18   35   29 |     ---     ---    ---    ---
emx  n/a|    0     0     0  -101    -8  -103   .29   26   27 |       0    2809   3490   7954
esx  n/a|    0    -2     4   -13   -18   -33  -.06   22   20 |   -3287    3540   3958   8919
gfz  n/a|   -2     0    -5    49    68    47  -.09   22   14 | -312905    3119   6473 999999
grg  n/a|   -1     5    -7   -59    -9    28  -.27   37   36 | -828830    3473   3888 999999
iac  n/a|    1     0     6    58   -46    80  -.09   20   20 | -283095     787   4399 999999
mcc  n/a|    6    -2     8    64    80   653  -.22  162  162 |     ---     ---    ---    ---

Table 2.1881.6  GPS week: 1881   Day: 6   MJD: 57417                            

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    16   -37    48   .40   36   29 |     ---     ---    ---    ---
cof  n/a|   -2     0    -3     0   -63    47   .25   41   32 |     ---     ---    ---    ---
emx  n/a|    1     0     0   -36    12   -53   .26   30   30 |       0     753   3235   7618
esx  n/a|    0    -1     5   -37   -14   -59  -.11   20   17 |  -14990    1493   3410   8399
gfz  n/a|   -2    -2    -5    31    58    40   .02   25   23 | -303161    -454   5344 999999
grg  n/a|    1     5    -2    25    25   -58  -.34   53   40 | -834164    -294  11712 999999
iac  n/a|    3     0     0     9   -25    13  -.11   24   24 | -287987   -1102   4638 999999
mcc  n/a|    6     0     5   179  -162   869  -.04  184  184 |     ---     ---    ---    ---

       
       
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 3.1881.0  GPS week: 1881   Day: 0   MJD: 57411                            

        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  | 1135   21   41   14   30   12   21   16  ---    8 |    74   88   71   53   60   58  ---  ---     0
 R02  |  596   12   13   20   23   18   18   14  321    8 |    58   60   67   41   54   54  ---  134     0
 R03  | 1199   14   18   17   13   10   31   10  ---    7 |    67   68   85   68   74   69  ---  ---     0
 R04  | 1301   12   16   15   14    8   11   18  ---    6 |    64   63   69   67   72   58  ---  ---     0
 R05  | 1292   35   27   24   24   30   63   29  ---   14 |    57   58   52   65   78   50  ---  ---     0
 R06  | 2772   14    9   13   13   10   23   18  ---    6 |    53   60   66   62   65   73  ---  ---     0
 R07  |  975   15   26   17   16   13   48   14  243    9 |    82   88   83   74   82   69  ---  103     0
 R08  |  615   16   24    8   18   10   25   17  ---    7 |    75   83   74   77   78   63  ---  ---     0
 R09  | 1065   30   51   22   29   26   38   23  ---   12 |    47   68   32   60   55   50  ---  ---     0
 R10  | 3199   29   33   22   15   12   17   19  ---    8 |  9999 9999   26 9999 9999 9999  ---  ---     0
 R11  |  696   60   62   34   34   26   50   28  ---   16 |    69   69   29   46   48   65  ---  ---     0
 R12  | 1897   61   42   48   34   34   48   23   92   18 |    67   56   40   56   68   67  ---   49     0
 R13  | 1612   32   50   18   13   17   33   11  ---    9 |    39   51   24   31   38   56  ---  ---     0
 R14  | 1511   31   28   28   27   24   37   30  ---   13 |    68   69   55   53   60   46  ---  ---     0
 R15  |13634   32   33   18   21   25   34   26  ---   11 |    36   33   30   35   43   22  ---  ---     0
 R16  | 1790   39   40   20   25   18   20   23  ---   10 |    40   38   27   27   31   31  ---  ---     0
 R18  |  623   30   33   10   17   16   22   10   68    7 |    64   68   38   48   29   32  ---   59     0
 R19  | 1937   44   50   12   20   16   28   18  ---   10 |    72   77   42   49   33   23  ---  ---     0
 R20  |  720   46   51   19   26   25   35   21  ---   12 |    64   69   36   41   31   29  ---  ---     0
 R21  |  483   51   44   12   16   19   33   13  109   10 |    64   63   43   47   32   25  ---   82     0
 R22  |  830   55   61   20   14   24   37   16  ---   12 |    84   86   54   49   37   28  ---  ---     0
 R23  | 1753   27   26   30   29   11   23   20  ---   10 |    40   44   41   76   52   47  ---  ---     0
 R24  | 2290   26   30   22   35   18   45   22  ---   12 |    55   56   53   74   46   36  ---  ---     0
XR26  | ---- 2138 2141  ---  ---  ---  ---  971  --- 1440 |    84  839  ---  ---  ---  ---  ---  ---     0
XR27  | ----  ---  ---  ---  ---  ---  ---    8  ---    0 |   ---  ---  ---  ---  ---  ---  ---  ---     0
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 3222   35   38   22   23   20   34   20  193      |T   61   98   49   54   53   47  ---   85   ---
 WRMS | 3222   27   30   22   21   14   32   20  193      |NE  61   98   49   54   53   47  ---   85   ---
 MEDI | 1292   30   33   19   21   18   33   18  109      |MD  64   68   43   53   52   50  ---   82   ---

Table 3.1881.1  GPS week: 1881   Day: 1   MJD: 57412                            

        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  | 1624   22   25   26   16   31   27   18  ---   10 |    59   63   42   47   68   55  ---  ---     0
 R02  |  650   12   16   20   26   23   22   18  106    9 |    42   45   45   27   50   36  ---   74     0
 R03  | 1890   14   14   17   15   24   19   16  ---    8 |    41   47   52   40   60   46  ---  ---     0
 R04  | 1118   11   18   16   17   11   32   10  ---    7 |    32   36   41   29   29   30  ---  ---     0
 R05  | 1070   29   40   28   32   18   53   22  ---   13 |    29   49   27   40   47   35  ---  ---     0
 R06  | 1776   21   23   11   26   12   18   20  ---    8 |    31   29   42   66   55   48  ---  ---     0
 R07  |  951   13   12   10   16   16   26   17  119    7 |    56   58   53   68   69   56  ---  126     0
 R08  |  696   18   13   15   18   19   40   14  ---    9 |    56   53   50   56   64   41  ---  ---     0
 R09  |  646   36   26   26   29   26   46   19  ---   13 |    68   68   47   61   61   63  ---  ---     0
 R10  | 3226   31   36   17   18   16   18   15  ---    8 |  9999 9999   19 9999 9999 9999  ---  ---     0
 R11  |  619   64   64   33   24   29   43   25  ---   15 |    68   69   32   54   54   57  ---  ---     0
 R12  | 1672   55   50   26   19   27   43   23  164   13 |    59   64   52   56   59   55  ---   59     0
 R13  | 1152   30   38   23   16   14   25   12  ---    8 |    42   50   25   29   30   46  ---  ---     0
 R14  | 1905   45   74   42   26   39   43   31  ---   16 |    45   58   52   53   65   42  ---  ---     0
 R15  | 8671   38   35   21   21   24   32   21  ---   11 |    38   42   37   32   42   28  ---  ---     0
 R16  |  945   35   37   23   19   15   19   16  ---    9 |    37   43   25   40   28   34  ---  ---     0
 R18  |  681   38   40   13   16   17   23   12   95    8 |    45   44   25   35   25   19  ---   35     0
 R19  | 1609   37   40   12   13   14   27   12  ---    8 |    54   55   41   42   37   32  ---  ---     0
 R20  | 1293   50   44   26   23   25   43   19  ---   13 |    41   45   34   37   37   49  ---  ---     0
 R21  |  516   39   37   19   12   20   31   16  102    9 |    51   52   41   38   37   37  ---   72     0
 R22  |  784   48   35   19   17   28   31   11  ---   11 |    59   54   46   54   49   43  ---  ---     0
 R23  | 1841   24   30   18   25   18   40   25  ---   11 |    27   30   39   50   30   36  ---  ---     0
 R24  | 1919   25   16   35   30   24   47   22  ---   13 |    34   34   52   44   26   29  ---  ---     0
XR26  | ----  ---  ---  ---  ---  ---  ---  ---  ---    0 |    85 9999  ---  ---  ---  ---  ---  ---     0
XR27  | ----  ---  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---  ---  ---  ---     0
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 2296   35   37   23   21   22   34   19  120      |T   47   49   39   45   46   41  ---   73   ---
 WRMS | 2296   27   28   24   19   18   32   19  120      |NE  47   49   39   45   46   41  ---   73   ---
 MEDI | 1152   31   35   20   19   20   31   17  106      |MD  45   49   41   42   47   41  ---   72   ---

Table 3.1881.2  GPS week: 1881   Day: 2   MJD: 57413                            

        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  | 2054   20   16   22   16   18   31   13  ---    8 |    58   43   46   41   63   55  ---  ---     0
 R02  |  949   16   17   15   12   15   25   18   84    7 |    48   54   43   48   51   39  ---   44     0
 R03  | 2622   13   14   27   10   20   25   10  ---    8 |    53   50   63   44   50   38  ---  ---     0
 R04  | 1142   17   16   13    6   16   20   13  ---    6 |    48   45   42   47   61   66  ---  ---     0
 R05  |  610   30   18   34   22   23   90   19  ---   16 |    40   53   44   57   51   48  ---  ---     0
 R06  |  802   16   18   14   13   13   20   15  ---    6 |    35   34   48   52   41   65  ---  ---     0
 R07  | 1354   15   11   20   14   14   32   28  132    9 |    57   56   56   55   50   85  ---   51     0
 R08  |  735   24   27   18   16   19   41   13  ---    9 |    60   65   55   48   63   27  ---  ---     0
 R09  |  769   31   47   23   23   28   41   29  ---   12 |    71   74   68   86   64  100  ---  ---     0
XR10  | 7151  863  702   25  ---  376  317   17  ---  186 |  9999 9999   19  --- 9999 9999  ---  ---     0
 R11  |  691   71   51   31   17   38   43   25  ---   16 |    80   75   30   46   61   63  ---  ---     0
 R12  | 1420   60   60   39   16   31   36   20  104   14 |    64   63   31   47   52   60  ---   36     0
 R13  |  577   27   35   17   15   17   36   10  ---    8 |    45   49   22   34   34   82  ---  ---     0
 R14  |  842   46   47   34   17   34   39   33  ---   14 |    57   63   52   54   54   40  ---  ---     0
 R15  | 4046   30   55   25   14   43   29   21  ---   12 |    42   59   37   31   55   28  ---  ---     0
 R16  |  949   33   29   26   19   18   38   20  ---   11 |    34   36   32   41   34   35  ---  ---     0
 R18  |  573   46   47   33   20   24   32   13   93   12 |    52   55   35   37   25   32  ---   34     0
 R19  | 1143   39   43   17   15   20   33   14  ---    9 |    53   55   33   38   23   25  ---  ---     0
 R20  | 1748   58   62   38   31   33   23   20  ---   15 |    61   73   37   48   40   37  ---  ---     0
 R21  |  581   26   25   15   19   15   32   11  118    8 |    46   46   34   44   32   28  ---   60     0
 R22  |  517   50   55   16    9   26   30   14  ---   10 |    59   65   42   45   40   39  ---  ---     0
 R23  | 2108   30   31   17   20   19   28   18  ---    9 |    29   33   38   54   35   30  ---  ---     0
 R24  | 1775   14   30   37   12   29   48   24  ---   12 |    41   42   61   41   26   40  ---  ---     0
XR26  | ---- 3770 3754  ---  ---  ---  --- 1585  --- 2444 |    99  593  ---  ---  ---  ---  ---  ---     0
XR27  | ----  ---  ---  ---  ---  ---  ---    6  ---    0 |   ---  ---  ---  ---  ---  ---  ---  ---     0
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1522   36   38   26   17   25   38   19  108      |T   53   77   42   47   45   48  ---   45   ---
 WRMS | 1522   30   32   26   16   20   37   19  108      |NE  53   77   42   47   45   48  ---   45   ---
 MEDI |  949   30   31   23   16   20   32   18  104      |MD  53   55   42   46   50   39  ---   44   ---

Table 3.1881.3  GPS week: 1881   Day: 3   MJD: 57414                            

        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  | 1456   21   22   17   16   16   27   18  ---    8 |    52   73   65   69   71   45  ---  ---     0
 R02  |  940   17   22   19   11   10   29   18  114    7 |    58   63   60   45   49   41  ---   23     0
 R03  | 1918   13   21   16   12   12   22   22  ---    7 |    60   70   65   52   58   40  ---  ---     0
 R04  |  930   23   28   27   19   14   26   11  ---    8 |    53   62   60   35   41   40  ---  ---     0
 R05  |  542   36   35   31   16   15   47   16  ---   11 |    29   35   56   36   28   38  ---  ---     0
 R06  |  700    5   14   25   13    9   27   11  ---    7 |    43   47   60   38   40   52  ---  ---     0
 R07  |  839   13   12   22   17   15   27   24  169    8 |    61   66   69   63   47   60  ---   89     0
 R08  |  999   18   23   17   15    8   26   21  ---    7 |    61   70   69   59   54   76  ---  ---     0
 R09  | 1839   29   48   38   22   22   46   26  ---   13 |    53   61   50   50   52   51  ---  ---     0
XR10  |12542 5906 9226  ---  --- 2729  --- 2976  --- 2850 |  9999 9999  ---  --- 9999  ---  ---  ---     0
 R11  |  705   69   56   38   14   29   31   36  ---   16 |    71   63   33   35   53   49  ---  ---     0
 R12  | 1443   67   41   37   15   24   42   26   96   15 |    73   65   39   46   53   64  ---   29     0
 R13  |  716   34   29   23   31   33  222   17  ---   29 |    41   40   25   32   33  170  ---  ---     0
 R14  |  871   34   38   34   35   27   44   34  ---   15 |    37   50   31   39   35   27  ---  ---     0
 R15  | 1865   29   29   24   24   34   21   18  ---   11 |    44   46   26   33   52   24  ---  ---     0
 R16  |  676   21   49   20   18   16   25   28  ---    9 |    40   61   34   47   40   40  ---  ---     0
XR17  | 9738    5  556  ---  ---  ---  ---  ---  ---    0 |    60  246  ---  ---  ---  ---  ---  ---     0
 R18  |  863   46   51   25   15   21   26   12   72   10 |    63   65   37   36   26   23  ---   32     0
 R19  | 1208   46   51   22   15   22   37   12  ---   11 |    60   62   39   44   28   32  ---  ---     0
 R20  | 1785   58   88   34   23   29   53   21  ---   15 |    75  101   44   44   35   36  ---  ---     0
 R21  |  634   31   38   21   18   16   24   18  140    9 |    62   68   57   57   45   45  ---   65     0
 R22  |  680   60   54   17   20   19   48   18  ---   13 |    73   69   39   40   32   41  ---  ---     0
 R23  | 1611   29   35   24   20   16   24   15  ---    9 |    29   30   26   48   39   41  ---  ---     0
 R24  | 1328   16   29   33   19   18   29   17  ---   10 |    29   40   43   43   38   31  ---  ---     0
XR26  | ----  160  297  ---  ---  ---  ---   83  ---  115 |    72  409  ---  ---  ---  ---  ---  ---     0
XR27  | ----  ---  ---  ---  ---  ---  ---    5  ---    0 |   ---  ---  ---  ---  ---  ---  ---  ---     0
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1202   37   41   27   19   21   58   21  123      |T   54   81   46   45   43   48  ---   47   ---
 WRMS | 1202   32   35   28   18   17   33   21  123      |NE  54   81   46   45   43   48  ---   47   ---
 MEDI |  940   29   38   24   17   18   27   18  114      |MD  58   63   43   44   40   41  ---   32   ---

Table 3.1881.4  GPS week: 1881   Day: 4   MJD: 57415                            

        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  |  811   17   21   28   11   11   16   18  ---    7 |    46   42   68   51   49   54  ---  ---     0
 R02  | 1005   18   18    8    8    9   23   16  161    6 |    49   49   39   35   40   42  ---   37     0
 R03  |  726   18   17   16   12   11   22   14  ---    6 |    58   58   55   50   43   36  ---  ---     0
 R04  | 1083   14   17   13   15   10   29   19  ---    7 |    55   56   60   58   49   30  ---  ---     0
 R05  |  872   28   36   29   13   17   53   21  ---   11 |    37   44   60   43   41   34  ---  ---     0
 R06  | 1469   11   13   33   16   17   27   22  ---    9 |    39   41   53   30   44   32  ---  ---     0
 R07  | 1167    7   17   23   14   11   31   18  223    8 |    51   56   62   57   59   50  ---  153     0
 R08  |  826   14   13   30   16    7   42   12  ---    9 |    52   48   66   51   48   45  ---  ---     0
 R09  | 2947   36   63   39   27   23   32   31  ---   13 |    83  100   69   87   76   75  ---  ---     0
XR10  |23028   43   44  ---   30   31  ---   81  ---   29 |  9999 9999  --- 9999 9999  ---  ---  ---     0
 R11  | 1226   61   68   48   17   29   36   27  ---   15 |    66   69   36   48   63   58  ---  ---     0
 R12  |  970   65   53   33   13   24   34   29  105   14 |    71   65   30   43   49   54  ---   42     0
 R13  |  777   34   41   24   14   12   22   17  ---    8 |    47   56   34   36   35   67  ---  ---     0
 R14  | 1376   35   42   39   42   28   47   30  ---   16 |    38   68   44   69   47   38  ---  ---     0
 R15  | 2512   28   34   24   15   27   26   22  ---   10 |    38   43   30   32   39   33  ---  ---     0
 R16  |  953   23   34   28   19   16   36   26  ---   10 |    38   57   28   41   34   25  ---  ---     0
XR17  | 2913  202  207  ---  144  121  ---  ---  ---  104 |    26  100  ---  138   97  ---  ---  ---     0
 R18  |  785   50   50   21   12   24   37   12   63   11 |    60   64   37   35   27   24  ---   29     0
 R19  | 1593   47   51   11   13   27   22    8  ---   10 |    54   58   26   34   24   31  ---  ---     0
 R20  | 1831   48   42   29   21   15   46   27  ---   13 |    60   55   40   39   33   27  ---  ---     0
 R21  |  674   31   42   17   26   18   39   20  165   11 |    53   60   41   57   41   25  ---  138     0
 R22  | 1230   50   65   16   19   18   29   17  ---   10 |    63   79   27   44   32   24  ---  ---     0
 R23  | 1186   29   34   27   24   17   29   16  ---   10 |    33   37   34   50   32   29  ---  ---     0
 R24  | 1036   24   28   19   23   22   39   23  ---   11 |    39   43   35   40   29   27  ---  ---     0
XR26  | ---- 2871 2857  ---  ---  ---  --- 1469  --- 2054 |    61  286  ---  ---  ---  ---  ---  ---     0
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1351   35   40   27   19   19   34   21  153      |T   50   68   44   50   44   39  ---   79   ---
 WRMS | 1351   28   31   29   16   17   35   21  153      |NE  50   68   44   50   44   39  ---   79   ---
 MEDI | 1083   31   41   24   16   17   31   20  161      |MD  51   56   39   44   41   33  ---   42   ---

Table 3.1881.5  GPS week: 1881   Day: 5   MJD: 57416                            

        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  | 1012   20   21   32   15   12   25   22  ---    9 |    40   45   60   37   36   50  ---  ---     0
 R02  |  689   16   14   13    9    9   23   16  217    6 |    37   35   35   23   30   45  ---   23     0
 R03  |  885   10   15    9   15   10   23   20  ---    6 |    44   47   38   48   44   40  ---  ---     0
 R04  |  846   15   21   10   13   13   24   17  ---    7 |    43   45   40   44   44   33  ---  ---     0
 R05  | 1536   27   31   25   24   19   66   20  ---   13 |    32   55   59   55   58   42  ---  ---     0
 R06  |  971   10   16   24   13   14   28   18  ---    8 |    34   38   38   34   39   53  ---  ---     0
 R07  | 1533   10   16   23   14   10   20   15  168    7 |    43   47   52   37   47   61  ---  139     0
 R08  |  443   11   10   17   13   12   45    9  ---    8 |    38   42   50   47   44   41  ---  ---     0
 R09  | 1316   42   39   33   29   24   34   39  ---   15 |    77   89   79   97   75   73  ---  ---     0
XR10  |48743   42   45  ---   24   15   27   22  ---   12 |  9999 9999  --- 9999 9999  992  ---  ---     0
 R11  | 1702   60   42   34   22   26   44   20  ---   15 |    65   57   36   55   65   58  ---  ---     0
 R12  | 1425   59   42   47   17   26   35   28   69   16 |    64   58   36   47   60   54  ---   54     0
 R13  | 1012   30   27   19   16   15   28   15  ---    8 |    44   42   24   33   33   44  ---  ---     0
 R14  |  961   44   67   33   43   46   57   36  ---   19 |    39   93   33   70   84   31  ---  ---     0
 R15  | 4490   23   33   18   25   36   24   18  ---   11 |    37   47   22   34   49   30  ---  ---     0
 R16  | 1958   21   32   30   22   14   25   21  ---   10 |    26   34   42   37   27   41  ---  ---     0
XR17  | 3294  246  245  ---  111  140  110  141  ---   76 |    26   49  ---  153   92   62  ---  ---     0
 R18  |  514   42   41   17   16   26   42   17   50   11 |    53   52   38   34   27   23  ---   31     0
 R19  | 1513   48   49   19   13   22   33   16  ---   11 |    65   66   49   52   41   33  ---  ---     0
 R20  | 1539   43   56   27   24   20   49   21  ---   13 |    52   65   35   38   25   26  ---  ---     0
 R21  |  675   36   30   17   23   20   47   11  219   11 |    52   47   39   48   31   37  ---  132     0
 R22  | 1099   49   41   16   17   21   39   13  ---   11 |    64   59   40   40   38   26  ---  ---     0
 R23  |  578   20   22   35   25   20   20   14  ---   10 |    29   40   32   50   46   24  ---  ---     0
 R24  | 1684   26   29   28   38   21   42   19  ---   13 |    44   34   35   45   31   32  ---  ---     0
XR26  | ---- 2674 2668  ---  ---  ---  --- 2848  --- 2789 |    33  254  ---  ---  ---  ---  ---  ---     0
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1526   34   35   25   22   22   37   20  162      |T   45   60   41   50   46   81  ---   75   ---
 WRMS | 1526   29   29   27   20   14   36   20  162      |NE  45   60   41   50   46   81  ---   75   ---
 MEDI | 1099   30   32   23   17   20   33   19  168      |MD  43   47   38   45   44   41  ---   54   ---

Table 3.1881.6  GPS week: 1881   Day: 6   MJD: 57417                            

        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  | 1302   28   21   24   21   30   38   12  ---   11 |    60   66   68   55   76   63  ---  ---     0
 R02  |  778   12   12   14   10    9   16   10  299    5 |    55   55   64   56   58   53  ---   33     0
 R03  | 1087   11    9   16    7   12   29   13  ---    6 |    68   68   71   63   72   74  ---  ---     0
 R04  | 1561   11   16    9   12   14   19    8  ---    5 |    67   70   65   59   69   58  ---  ---     0
 R05  |  736   44   31   38   18   21   75   17  ---   14 |    51   51   58   47   46   31  ---  ---     0
 R06  |  970   12   10   16   13    8  122   20  ---   15 |    50   51   58   49   56   72  ---  ---     0
 R07  | 1499   18   20   38   10   18   47   15  194   10 |    71   74   79   64   68   52  ---   58     0
 R08  |  792   20   20   24   24   12   39   15  ---    9 |    73   75   76   61   70   48  ---  ---     0
 R09  | 1761   33   46   24   24   26   34   37  ---   13 |    68   70   63   59   61   64  ---  ---     0
XR10  |78099   33   41  ---   16   14   42   17  ---   11 |  9999 9999  --- 9999 9999 9999  ---  ---     0
 R11  |  832   48   60   34   17   30   48   23  ---   14 |    54   79   31   50   64   64  ---  ---     0
 R12  | 1003   57   70   44   12   19   50   25  112   14 |    61   83   42   49   57   63  ---   35     0
 R13  |  611   35   47   18   18   17   26   19  ---    9 |    45   54   26   31   35   40  ---  ---     0
 R14  | 1067   59   40   57   36   53   42   70  ---   24 |    99   83   60   78   72   85  ---  ---     0
 R15  | 2937   28   59   17   22   37   22   17  ---   11 |    37   73   27   37   44   31  ---  ---     0
 R16  | 2024   26   46   23   17   13   44   24  ---   10 |    33   45   30   30   28   33  ---  ---     0
XR17  | 2505  178  179  ---  247   61  174  175  ---   91 |    22   64  ---  223   68   63  ---  ---     0
 R18  |  795   36   44   13   11   20   34   11   43    9 |    70   75   46   42   31   25  ---   36     0
 R19  | 1544   47   46   14   10   27   61   16  ---   12 |    69   67   52   51   41   63  ---  ---     0
 R20  | 1016   44   31   39   13   30  118   16  ---   18 |    64   55   39   37   25   32  ---  ---     0
 R21  |  544   46   56   30   13   30   38   17  165   12 |    67   76   38   46   28   30  ---   88     0
 R22  |  504   52   58   31   13   28   39   14  ---   12 |    79   82   40   46   28   24  ---  ---     0
 R23  |  913   27   22   31   29   18   13   14  ---   10 |    38   42   37   77   51   48  ---  ---     0
 R24  | 1756   33   41   41   41   27   47   31  ---   16 |    55   79   44   74   51   32  ---  ---     0
XR26  | ----  490  594  ---  ---  ---  ---  234  ---  338 |    39  367  ---  ---  ---  ---  ---  ---     0
------+---------------------------------------------------+-----------------------------------------------
 RMS  | 1311   36   41   30   20   25   53   24  184      |T   58   79   50   60   52   49  ---   50   ---
 WRMS | 1311   29   32   30   17   23   40   24  184      |NE  58   79   50   60   52   49  ---   50   ---
 MEDI | 1016   33   41   24   16   20   39   17  165      |MD  60   70   46   51   56   52  ---   36   ---




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