[IGSREPORT-25145] Wk 1938 IGLOS Final Orbits
acc
acc at igs.org
Sun Mar 19 16:14:10 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1938 (Feb 26, 2017 - Mar 04, 2017)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1938.
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:
igl1938[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1938 in the SP3 format.
igl19387.sum Combination Report for GPS Week 1938.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 13.5 ns
1 | 15.7 ns
2 | 4.3 ns
3 | 13.7 ns
4 | -1.3 ns
5 | 15.1 ns
6 | -25.4 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1938, 1a.1938).
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 2.1938.0-6)
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 3.1938.0-6).
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 1938 summary. (Feb 26, 2017 - Mar 04, 2017)
Table 1.1938.a GPS week : 1938 MJD: 57810.0-57816.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -5 2 -7 -44 .13 34 32 | -113426 -61 3321 152572
| 1 1 2 24 37 30 .06 | 297985 960
cof n/a| -2 -1 -7 6 2 -49 .08 37 34 | -113433 -54 3321 152574
| 2 1 4 35 35 54 .05 | 297991 952
emx n/a| 0 -1 6 5 -48 -67 .12 24 24 | 0 888 3181 10562
| 1 0 2 18 26 34 .03 | 0 757
esx n/a| 1 0 -2 4 -17 6 .13 17 16 | 1328 -813 3179 12666
| 1 1 1 14 10 33 .03 | 16116 2164
gfz n/a| 0 0 3 0 21 35 -.00 24 23 | -100423 170 3307 152152
| 1 1 3 13 27 47 .07 | 296638 706
grg n/a| 0 1 3 -58 53 -30 -.32 34 30 | -88497 -48230 3343 152465
| 1 1 4 28 20 115 .04 | 338298 143089
iac n/a| 0 1 -3 13 15 47 -.12 19 19 | -107751 -20 3304 151922
| 0 0 2 29 27 50 .03 | 296500 869
mcc n/a| -1 2 3 92 49 230 -.60 108 108 | --- --- --- ---
| 2 6 7 85 84 556 .43 | --- ---
Table 1.1938.b GPS week : 1938 MJD: 57810.0-57816.0
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 10 11 12 12 12 |
R02 | 7 9 8 8 9 8 9 |
R03 | 10 9 10 10 10 10 9 |
R04 | 9 10 11 11 10 10 8 |
R05 | 13 17 15 12 14 15 15 |
R07 | 9 11 11 9 10 10 10 |
R08 | 8 9 9 8 9 9 9 |
R09 | 7 7 8 9 8 8 9 |
R10 | 9 7 10 8 8 8 7 |
R11 | 7 8 7 8 7 8 8 |
R13 | 10 8 9 10 9 9 8 |
R14 | 12 10 12 13 16 15 12 |
R15 | 10 11 20 10 10 9 10 |
R16 | 12 13 11 12 12 15 14 |
R17 | 8 11 9 7 9 11 8 |
R18 | 7 9 8 8 6 10 9 |
R19 | 16 13 14 10 10 9 10 |
R20 | 11 17 17 17 17 16 16 |
R21 | 9 11 11 9 9 10 8 |
R22 | 8 10 9 9 8 8 10 |
R23 | 13 10 9 9 8 9 9 |
R24 | 16 17 14 14 20 19 21 |
Table 1.1938.c GPS week : 1938 MJD: 57810.0-57816.0
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 1938 0 | -20 -10 19 847 134 1579 83.9 1392 1392 | 13470 0
brd 1938 1 | -3 8 25 840 352 1714 85.2 1253 1253 | 15661 0
brd 1938 2 | 9 -7 15 -1280 285 953 85.3 1125 1125 | 4290 0
brd 1938 3 | -34 62 30 -1105 -1940 165 84.6 1006 1006 | 13742 0
brd 1938 4 | 21 -6 150 -556 -1723 1635 84.5 1060 1060 | -1271 0
brd 1938 5 | 14 5 132 192 -1738 1560 84.5 1062 1062 | 15063 0
brd 1938 6 | -7 45 74 599 -369 1258 85.8 1046 1046 | -25361 0
-------------+------------------------------------------------------------+----------------
brd 1938 mean| -3 14 64 -65 -714 1266 84.8 1135 1135 | 5084 0
brd 1938 sdev| 20 28 56 909 1044 552 .6 138 138 | 14858 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 2.1938.0 GPS week: 1938 Day: 0 MJD: 57810
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| -5 0 -4 37 23 -65 .08 37 35 | -788463 -468 3382 999999
cof n/a| -4 -3 -14 9 26 -114 .12 36 34 | -788481 -431 3382 999999
emx n/a| 1 -2 5 35 -24 -73 .14 22 22 | 0 1070 3414 10979
esx n/a| 1 0 -3 -7 -34 -13 .13 14 13 | 8687 -344 3372 10349
gfz n/a| 0 0 5 10 80 -27 .02 25 23 | -772361 -351 3335 999999
grg n/a| -1 2 -3 -46 57 98 -.37 31 27 | -834740 32695 3425 999999
iac n/a| 0 1 0 -15 -26 59 -.08 21 21 | -779376 -477 3371 999999
mcc n/a| 0 -1 12 156 101 -6 -.64 96 96 | --- --- --- ---
Table 2.1938.1 GPS week: 1938 Day: 1 MJD: 57811
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 25 45 -42 .21 35 34 | 11784 -779 3931 11341
cof n/a| 0 -2 -7 41 59 -33 .09 38 36 | 11792 -799 3933 11341
emx n/a| 0 0 10 -9 -98 -45 .14 25 25 | 0 979 3039 10578
esx n/a| 0 1 0 7 -15 -25 .12 17 15 | 16269 821 2992 12062
gfz n/a| -1 1 5 -13 28 85 -.10 26 25 | 24039 -593 3940 10884
grg n/a| -1 2 6 -94 76 89 -.28 39 34 | 208981 -371559 4039 11214
iac n/a| 0 0 -7 36 17 5 -.11 18 18 | 17076 -768 3914 10718
mcc n/a| 2 3 12 107 76 160 -.72 125 125 | --- --- --- ---
Table 2.1938.2 GPS week: 1938 Day: 2 MJD: 57812
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -2 -4 18 -2 -69 .11 32 30 | -203 -1173 3222 11554
cof n/a| -4 -1 -1 -5 8 -109 .14 33 29 | -217 -1153 3226 11554
emx n/a| -1 0 6 15 -54 -41 .08 22 22 | 0 -607 3213 10824
esx n/a| 1 1 -4 -14 -26 -14 .16 20 18 | -1546 -3472 3222 13460
gfz n/a| 0 1 -1 3 14 3 .08 23 24 | 11905 -115 3216 11128
grg n/a| 0 -1 9 -44 39 47 -.31 35 30 | 4800 -809 3221 11416
iac n/a| 0 1 -4 27 34 70 -.14 19 19 | 4923 -627 3218 10892
mcc n/a| -2 5 4 108 62 654 .02 125 125 | --- --- --- ---
Table 2.1938.3 GPS week: 1938 Day: 3 MJD: 57813
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 2 -3 -20 -16 -81 .15 33 32 | 8376 1485 3031 11453
cof n/a| 0 -1 -11 15 -39 -87 .08 36 36 | 8379 1467 3030 11454
emx n/a| -1 0 5 21 -26 -140 .14 26 26 | 0 1881 2995 10679
esx n/a| 1 0 -3 30 -12 -4 .17 16 16 | 19886 1562 3011 13333
gfz n/a| 0 0 5 18 2 0 -.00 23 21 | 21056 1427 3004 10930
grg n/a| 1 1 1 -22 22 -45 -.32 28 23 | 12949 1654 3030 11693
iac n/a| 0 0 -1 -39 39 135 -.13 19 19 | 13471 1142 3006 10641
mcc n/a| -4 6 4 -1 -44 1171 -.54 148 148 | --- --- --- ---
Table 2.1938.4 GPS week: 1938 Day: 4 MJD: 57814
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 -7 -6 -5 -38 .03 34 31 | -6122 -159 2984 11040
cof n/a| -3 0 -3 -33 -7 14 -.03 40 35 | -6128 -154 2982 11045
emx n/a| 0 -1 7 -3 -24 -69 .09 27 27 | 0 835 2962 10268
esx n/a| 0 -1 0 0 -12 7 .11 18 16 | -10323 -4165 2992 13074
gfz n/a| 0 0 0 3 16 90 .03 21 18 | 7100 -268 2978 10513
grg n/a| -1 2 2 -94 54 -64 -.37 34 30 | -800 -439 2952 10769
iac n/a| 0 1 -2 27 -19 -15 -.12 20 20 | -925 1155 2972 10283
mcc n/a| 2 -11 -6 -33 -67 139 -1.23 88 88 | --- --- --- ---
Table 2.1938.5 GPS week: 1938 Day: 5 MJD: 57815
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 -1 -12 -73 -2 .16 34 31 | 9359 1006 3219 11060
cof n/a| -1 0 -4 56 -38 -24 .05 34 31 | 9350 1016 3226 11063
emx n/a| -1 -1 5 -7 -52 -65 .13 23 23 | 0 1289 3198 9989
esx n/a| 4 0 -3 7 -1 20 .08 18 15 | 3096 182 3218 12912
gfz n/a| -2 1 0 -17 9 74 -.11 24 22 | 22550 557 3245 10649
grg n/a| 0 0 4 -71 43 -214 -.32 40 33 | 14493 1186 3240 10989
iac n/a| 0 1 -3 38 36 58 -.10 19 19 | 15002 228 3204 10169
mcc n/a| -4 9 -4 97 40 -613 -.94 78 78 | --- --- --- ---
Table 2.1938.6 GPS week: 1938 Day: 6 MJD: 57816
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -8 -25 -20 -8 .16 36 32 | -28716 -343 3479 11558
cof n/a| -1 -1 -6 -37 4 7 .07 39 35 | -28729 -326 3473 11562
emx n/a| 0 0 1 -10 -56 -39 .12 23 23 | 0 773 3450 10617
esx n/a| 0 1 0 7 -22 75 .14 17 15 | -26771 -280 3446 13475
gfz n/a| 1 0 6 -11 1 19 .05 26 26 | -17256 539 3435 10967
grg n/a| -1 0 4 -36 80 -121 -.31 32 30 | -25162 -340 3496 11176
iac n/a| -1 1 0 19 24 19 -.17 20 20 | -24430 -797 3448 10758
mcc n/a| -1 2 3 214 180 108 -.13 99 99 | --- --- --- ---
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 3.1938.0 GPS week: 1938 Day: 0 MJD: 57810
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 | 628 76 67 18 5 43 24 14 --- 13 | 3 4 2 4 6 1 2 --- 3
R02 | 751 23 31 17 7 22 18 10 66 6 | 2 3 3 3 3 3 2 2 2
R03 | 957 38 35 19 15 25 26 18 73 9 | 3 3 4 5 5 3 4 3 3
R04 | 745 42 39 17 9 22 16 15 --- 8 | 2 5 3 2 3 3 2 --- 2
R05 | 1454 54 49 29 21 24 32 28 --- 13 | 3 7 4 5 14 3 3 --- 3
R07 | 684 47 49 15 9 31 20 9 110 9 | 2 2 3 4 3 3 2 2 2
R08 | 1303 33 33 17 10 24 18 7 --- 7 | 2 3 2 7 3 4 2 --- 3
XR09 | 1867 21 25 14 11 13 --- 12 --- 6 | 1 2 1 3 3 --- 2 --- 2
R10 | 1924 20 29 25 14 18 27 18 --- 8 | 2 4 3 3 3 2 2 --- 2
R11 | 1042 21 22 10 10 23 21 16 155 7 | 2 2 3 2 2 4 2 4 2
R13 | 1008 17 19 22 17 24 32 15 --- 9 | 2 2 2 2 2 2 2 --- 1
R14 | 2222 14 23 22 19 16 34 39 --- 11 | 3 5 2 5 3 3 3 --- 2
R15 | 2318 32 32 22 19 18 24 21 --- 9 | 2 2 2 145 3 3 2 --- 2
R16 | 1421 25 26 29 23 16 42 19 --- 11 | 3 4 3 4 3 3 3 --- 2
R17 | 1238 32 35 15 6 14 13 23 --- 7 | 1 3 1 4 4 2 2 --- 2
R18 | 564 25 29 13 9 14 17 17 --- 6 | 1 3 2 4 3 3 2 --- 2
R19 | 928 59 47 36 14 35 41 38 --- 15 | 1 5 2 4 5 7 3 --- 3
R20 | 784 15 30 26 17 26 50 11 --- 11 | 4 5 3 5 6 2 3 --- 3
R21 | 553 34 27 19 9 16 21 25 30 8 | 1 2 1 2 4 4 2 1 2
R22 | 482 28 30 13 10 12 30 18 --- 7 | 1 2 1 2 2 2 1 --- 1
XR23 | 1380 29 37 --- 25 28 27 20 --- 12 | 1 5 --- 7 5 3 1 --- 3
R24 | 3165 31 37 29 23 40 63 26 --- 15 | 2 6 6 3 3 7 3 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS | 1391 37 36 22 14 25 31 21 96 |T 2 3 2 10 4 3 2 2 2
WRMS | 1391 35 34 22 13 23 27 21 96 |NE 2 3 2 10 4 3 2 2 2
MEDI | 1008 29 31 19 11 22 26 18 73 |MD 2 3 2 4 3 3 2 2 2
Table 3.1938.1 GPS week: 1938 Day: 1 MJD: 57811
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 | 549 57 74 21 9 29 25 16 --- 11 | 3 6 3 5 6 3 3 --- 3
R02 | 1471 18 18 15 18 25 28 18 77 9 | 4 5 4 6 4 5 4 9 4
R03 | 747 36 44 13 8 31 14 13 88 8 | 4 5 5 5 4 4 5 4 3
R04 | 674 44 45 15 10 31 23 12 --- 9 | 2 4 3 5 4 3 3 --- 2
R05 | 1320 41 51 32 31 29 72 23 --- 16 | 3 7 7 5 14 3 4 --- 3
R07 | 880 44 42 19 12 30 35 15 131 10 | 2 3 4 4 5 6 2 6 3
R08 | 1450 34 30 15 12 29 22 8 --- 8 | 2 4 3 6 5 4 3 --- 3
XR09 | 2015 18 17 18 8 15 --- 9 --- 6 | 1 3 3 4 4 --- 2 --- 2
R10 | 1544 18 22 16 11 19 20 13 --- 6 | 4 4 4 7 4 3 3 --- 4
R11 | 1224 20 23 14 13 24 26 11 212 7 | 2 3 3 2 3 4 1 16 2
R13 | 875 17 14 17 16 14 27 15 --- 7 | 2 3 2 6 3 4 2 --- 2
R14 | 1645 19 21 21 21 15 29 27 --- 10 | 2 4 5 5 7 4 4 --- 3
R15 | 596 34 38 25 19 28 32 19 --- 11 | 2 4 3 142 4 3 2 --- 2
R16 | 1282 26 29 35 30 17 48 20 --- 13 | 3 7 3 5 9 4 3 --- 3
R17 | 902 38 32 24 12 28 25 21 --- 10 | 1 2 2 5 3 3 2 --- 2
R18 | 495 31 28 22 16 10 29 14 --- 8 | 1 2 2 5 4 4 2 --- 2
R19 | 991 51 62 14 20 29 48 21 --- 13 | 1 5 3 8 6 7 3 --- 3
R20 | 693 35 24 55 24 32 55 28 --- 16 | 3 9 8 10 10 5 2 --- 6
R21 | 444 39 36 25 10 32 31 13 46 10 | 1 3 2 4 5 6 2 6 2
R22 | 613 38 33 17 11 22 36 15 --- 9 | 2 3 2 3 3 5 2 --- 2
XR23 | 1461 18 19 --- 25 17 25 15 --- 10 | 1 5 --- 9 4 2 1 --- 4
R24 | 3295 21 28 43 20 39 77 26 --- 16 | 2 6 6 6 4 7 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1253 35 38 25 17 26 39 18 125 |T 2 4 3 11 5 4 2 8 2
WRMS | 1253 34 36 25 15 25 34 18 125 |NE 2 4 3 11 5 4 2 8 2
MEDI | 902 34 29 19 13 28 29 15 88 |MD 2 4 3 5 4 4 2 6 3
Table 3.1938.2 GPS week: 1938 Day: 2 MJD: 57812
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 | 505 45 19 16 13 25 21 17 --- 10 | 4 12 3 4 5 4 2 --- 3
R02 | 1638 23 28 15 13 19 15 18 94 7 | 6 7 7 7 7 8 6 14 6
R03 | 737 48 49 12 8 28 22 19 142 10 | 4 6 5 5 4 5 5 5 4
R04 | 614 44 48 17 11 31 22 19 --- 10 | 2 3 4 5 4 2 4 --- 2
R05 | 1405 20 27 23 26 24 69 27 --- 14 | 3 9 5 5 15 3 5 --- 3
R07 | 1045 45 55 15 12 35 25 20 146 11 | 2 3 3 3 5 4 2 9 2
R08 | 1382 33 47 14 14 19 32 12 --- 8 | 2 6 4 5 6 4 3 --- 3
XR09 | 1864 17 24 17 15 17 --- 10 --- 7 | 2 4 4 4 4 --- 2 --- 2
R10 | 1101 23 19 26 26 18 17 13 --- 9 | 6 7 6 8 6 6 6 --- 6
R11 | 1097 19 22 11 12 19 21 10 161 6 | 2 4 3 3 3 3 2 25 2
R13 | 801 23 23 18 16 22 29 17 --- 9 | 2 3 2 5 3 7 2 --- 3
R14 | 1130 21 24 26 26 13 39 32 --- 12 | 2 5 6 9 8 7 3 --- 5
XR15 | 8876 56 54 32 --- 32 47 34 --- 19 | 2 5 2 --- 3 3 3 --- 2
R16 | 625 18 18 30 25 14 34 18 --- 10 | 3 8 4 7 7 2 3 --- 3
R17 | 1066 26 26 15 8 22 28 24 --- 9 | 1 2 3 3 3 3 4 --- 2
R18 | 691 27 23 15 17 18 18 14 --- 8 | 2 3 2 6 4 4 3 --- 3
R19 | 810 49 44 24 33 22 39 18 --- 13 | 2 5 2 8 4 3 2 --- 3
R20 | 750 42 43 47 21 27 74 13 --- 17 | 3 8 6 9 9 6 2 --- 5
R21 | 489 40 35 15 13 40 18 21 39 11 | 1 3 2 4 7 5 2 10 3
R22 | 835 32 31 14 15 23 17 16 --- 8 | 2 5 2 5 4 4 2 --- 3
R23 | 1606 13 12 17 32 12 18 12 --- 8 | 2 5 1 7 3 3 1 --- 2
R24 | 2317 18 20 38 32 9 58 16 --- 14 | 3 6 6 11 6 5 4 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1124 32 33 22 20 23 35 19 125 |T 2 5 3 5 5 4 3 12 3
WRMS | 1124 30 29 22 18 24 30 19 125 |NE 2 5 3 5 5 4 3 12 3
MEDI | 1045 26 26 17 15 22 25 17 142 |MD 2 5 3 5 4 4 3 10 3
Table 3.1938.3 GPS week: 1938 Day: 3 MJD: 57813
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 | 560 41 46 15 16 25 30 18 --- 10 | 4 7 2 3 4 4 3 --- 2
R02 | 1305 29 23 19 14 11 22 13 181 7 | 9 10 9 9 10 10 9 9 9
R03 | 727 49 54 16 10 27 22 14 196 10 | 4 6 5 5 7 5 5 4 5
R04 | 984 51 44 23 7 32 20 12 --- 10 | 2 3 3 5 5 4 3 --- 3
R05 | 708 23 17 26 18 23 39 24 --- 11 | 4 10 4 5 14 4 4 --- 3
R07 | 1435 47 42 17 11 23 13 12 133 9 | 2 3 2 2 4 3 2 1 2
R08 | 784 32 33 16 12 21 15 14 --- 8 | 2 8 4 6 5 3 2 --- 3
XR09 | 1598 21 20 26 12 20 --- 12 --- 9 | 1 5 3 3 4 --- 2 --- 2
R10 | 1004 25 31 20 18 14 19 11 --- 8 | 9 10 9 9 9 9 8 --- 9
R11 | 907 20 21 14 17 20 16 17 138 7 | 2 3 2 2 3 4 2 2 2
R13 | 1411 28 28 22 14 27 26 19 --- 9 | 2 6 3 6 5 7 2 --- 3
R14 | 820 21 25 28 25 21 42 34 --- 13 | 3 13 4 12 11 5 4 --- 6
R15 | 939 25 28 21 18 18 37 18 --- 10 | 2 4 2 9999 6 5 2 --- 3
R16 | 1499 22 32 44 13 17 28 23 --- 11 | 2 8 5 6 6 3 3 --- 3
R17 | 605 21 26 15 11 17 20 15 --- 7 | 1 4 3 6 4 3 4 --- 3
R18 | 680 22 26 20 15 24 19 10 --- 8 | 3 4 3 5 4 3 3 --- 3
R19 | 579 33 36 15 16 25 18 25 --- 9 | 1 4 3 5 2 4 2 --- 2
R20 | 892 56 65 57 26 19 51 21 --- 17 | 3 6 3 7 8 4 3 --- 4
R21 | 476 35 47 13 12 27 14 14 34 8 | 1 5 2 4 5 3 3 1 2
R22 | 528 33 42 22 11 24 17 20 --- 9 | 2 5 2 5 3 6 2 --- 3
R23 | 931 14 24 26 16 26 19 15 --- 8 | 1 4 1 2 3 4 1 --- 1
R24 | 1907 20 28 39 24 24 45 28 --- 14 | 3 9 4 8 6 5 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1007 33 36 26 16 23 28 19 148 |T 2 6 3 5 5 4 3 3 3
WRMS | 1007 32 36 26 16 21 23 19 148 |NE 2 6 3 5 5 4 3 3 3
MEDI | 892 25 28 20 14 23 20 15 138 |MD 2 5 3 5 5 4 3 2 3
Table 3.1938.4 GPS week: 1938 Day: 4 MJD: 57814
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 | 585 56 69 20 10 26 26 18 --- 11 | 3 7 3 3 4 3 4 --- 2
R02 | 1780 26 42 17 19 20 21 17 94 8 | 12 15 12 15 15 12 12 12 13
R03 | 1001 48 49 26 12 16 20 13 92 10 | 5 6 5 7 9 6 6 5 6
R04 | 1405 42 50 20 12 24 19 18 --- 9 | 2 3 3 5 4 5 3 --- 2
R05 | 907 32 46 16 19 23 61 36 --- 14 | 3 7 4 5 13 4 3 --- 2
R07 | 788 45 49 19 11 20 23 14 104 9 | 2 3 3 5 5 4 2 1 2
R08 | 1065 30 36 16 18 17 21 19 --- 8 | 2 6 4 5 4 2 3 --- 2
XR09 | 1699 16 13 16 11 22 --- 14 --- 8 | 2 3 2 4 4 --- 3 --- 2
R10 | 642 18 31 21 21 12 22 9 --- 8 | 11 13 11 11 11 12 11 --- 11
R11 | 493 23 25 16 10 21 17 13 81 7 | 2 3 3 3 3 4 3 2 2
R13 | 2522 28 32 32 13 19 21 10 --- 9 | 2 6 3 6 4 5 2 --- 3
R14 | 736 27 34 26 34 26 55 33 --- 15 | 2 15 6 15 14 6 4 --- 8
R15 | 739 30 38 18 16 26 29 23 --- 10 | 2 5 4 9999 5 4 2 --- 3
R16 | 902 22 29 43 24 19 25 19 --- 11 | 2 7 5 4 5 5 3 --- 2
R17 | 508 28 33 16 15 17 25 18 --- 8 | 1 6 2 5 5 4 2 --- 2
R18 | 612 19 23 11 9 18 14 11 --- 6 | 3 4 4 5 5 4 4 --- 4
R19 | 819 38 40 12 15 20 25 22 --- 9 | 1 5 5 4 3 5 2 --- 2
R20 | 962 50 59 52 19 25 48 33 --- 16 | 4 8 4 7 6 5 4 --- 4
R21 | 701 37 32 24 10 16 21 18 66 9 | 1 4 2 6 4 4 3 1 2
R22 | 899 32 32 21 11 19 17 15 --- 8 | 1 2 2 6 5 5 1 --- 2
R23 | 811 15 12 20 20 12 22 10 --- 7 | 1 5 1 5 6 3 2 --- 3
R24 | 1192 25 31 64 26 29 86 26 --- 20 | 3 9 8 5 6 5 5 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1060 34 40 27 18 21 34 20 88 |T 3 6 4 6 6 5 3 4 3
WRMS | 1060 31 35 27 16 18 30 20 88 |NE 3 6 4 6 6 5 3 4 3
MEDI | 819 28 33 20 15 20 22 18 92 |MD 2 6 4 5 5 5 3 2 2
Table 3.1938.5 GPS week: 1938 Day: 5 MJD: 57815
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 | 636 58 56 23 11 27 25 17 --- 11 | 3 5 4 5 8 4 3 --- 3
R02 | 1187 24 12 18 15 19 12 15 32 7 | 15 17 14 15 15 15 15 15 14
R03 | 918 52 54 17 8 27 16 15 24 10 | 6 8 7 6 7 6 6 7 6
R04 | 968 47 47 16 16 18 19 11 --- 9 | 3 5 4 7 5 5 4 --- 3
XR05 | 859 54 69 21 20 --- 33 28 --- 14 | 4 10 4 6 --- 5 4 --- 3
R07 | 996 52 58 19 11 25 18 13 108 10 | 3 5 4 5 5 5 4 5 3
R08 | 1629 32 41 15 14 17 31 14 --- 8 | 3 5 4 5 5 4 4 --- 3
XR09 | 1017 18 28 18 9 23 --- 11 --- 7 | 3 4 3 5 5 --- 4 --- 4
R10 | 657 22 32 19 16 24 16 13 --- 8 | 14 16 14 15 14 14 14 --- 14
R11 | 545 25 31 12 8 27 25 14 72 8 | 3 4 3 4 4 4 3 6 3
R13 | 2793 27 22 15 16 21 32 15 --- 9 | 4 7 4 6 5 6 4 --- 4
R14 | 759 26 29 20 40 20 59 33 --- 15 | 4 12 8 16 14 6 5 --- 8
R15 | 1218 17 19 16 11 22 37 17 --- 8 | 3 5 5 1 5 5 3 --- 3
R16 | 599 39 30 46 22 28 40 30 --- 15 | 3 7 4 6 7 5 5 --- 3
R17 | 692 31 27 25 20 37 18 20 --- 11 | 3 8 3 9 6 4 3 --- 4
R18 | 916 19 15 15 21 22 16 26 --- 9 | 5 6 5 5 6 5 5 --- 5
R19 | 811 39 24 9 14 17 19 17 --- 8 | 3 6 5 4 5 5 3 --- 3
R20 | 659 24 27 40 20 16 79 21 --- 15 | 5 10 6 6 6 6 5 --- 5
R21 | 774 25 21 16 17 22 32 20 111 9 | 3 5 3 6 4 5 3 4 3
R22 | 725 32 30 12 12 10 24 17 --- 7 | 3 3 3 6 7 4 3 --- 3
R23 | 539 22 24 27 16 18 33 12 --- 9 | 3 5 1 8 8 3 4 --- 5
R24 | 724 23 30 36 29 37 104 22 --- 19 | 4 12 8 6 7 4 3 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1061 34 34 23 18 24 40 19 78 |T 4 7 5 6 7 5 4 7 4
WRMS | 1061 31 31 23 15 22 33 19 78 |NE 4 7 5 6 7 5 4 7 4
MEDI | 774 26 29 18 16 22 25 17 72 |MD 3 6 4 6 6 5 4 6 3
Table 3.1938.6 GPS week: 1938 Day: 6 MJD: 57816
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 | 528 65 62 25 14 27 26 16 --- 12 | 5 4 4 4 6 4 3 --- 3
R02 | 900 23 33 17 14 27 19 20 62 8 | 17 18 18 18 18 18 17 18 18
R03 | 1568 44 41 17 10 26 20 13 139 9 | 7 7 7 6 7 6 7 9 6
R04 | 929 37 39 13 9 24 19 15 --- 8 | 4 5 4 6 4 3 4 --- 3
R05 | 687 48 44 21 21 20 54 33 --- 14 | 4 7 4 6 9999 4 5 --- 4
R07 | 676 49 52 16 10 27 15 18 127 9 | 4 4 3 4 4 4 4 8 3
R08 | 1659 28 25 21 18 22 18 15 --- 8 | 4 5 4 4 4 4 5 --- 3
XR09 | 1275 18 22 14 17 17 --- 17 --- 8 | 3 4 3 4 4 --- 3 --- 3
R10 | 828 23 15 12 13 15 22 16 --- 7 | 17 17 17 18 17 16 17 --- 17
R11 | 476 33 30 14 8 28 14 7 62 7 | 3 3 3 3 3 3 3 9 3
R13 | 1968 28 38 14 13 17 21 16 --- 7 | 4 5 3 4 4 6 3 --- 4
R14 | 1301 35 41 19 20 29 37 26 --- 11 | 4 9 6 10 8 4 4 --- 5
R15 | 989 18 18 15 15 30 41 11 --- 9 | 3 5 3 1 5 5 3 --- 3
R16 | 722 45 48 37 21 25 30 29 --- 13 | 3 5 4 5 5 4 4 --- 3
R17 | 721 23 24 14 11 31 14 19 --- 8 | 3 6 3 7 5 3 3 --- 4
R18 | 1549 25 23 19 14 29 16 17 --- 8 | 5 6 6 5 6 5 5 --- 5
R19 | 756 54 61 21 12 21 24 14 --- 10 | 3 4 3 3 4 3 3 --- 2
R20 | 831 20 34 50 30 17 58 17 --- 16 | 6 8 5 5 6 6 5 --- 5
R21 | 1023 20 25 18 11 23 13 16 75 7 | 3 4 3 4 3 4 4 8 3
R22 | 842 35 36 19 14 35 24 14 --- 10 | 3 3 3 4 5 4 3 --- 3
R23 | 690 21 18 22 20 19 21 15 --- 9 | 3 3 1 5 5 2 3 --- 3
R24 | 690 39 59 45 37 43 76 37 --- 20 | 4 11 6 4 5 2 3 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1046 36 39 23 17 26 32 20 99 |T 5 6 5 5 6 5 5 10 4
WRMS | 1046 32 35 23 15 26 30 20 99 |NE 5 6 5 5 6 5 5 10 4
MEDI | 831 28 34 18 14 25 21 16 75 |MD 4 5 4 4 5 4 4 9 3
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