[IGSREPORT-25179] Wk 1940 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 3 22:27:46 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1940 (Mar 12, 2017 - Mar 18, 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 2.1940.
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:
igl1940[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1940 in the SP3 format.
igl19407.sum Combination Report for GPS Week 1940.
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 | -12.1 ns
1 | -11.5 ns
2 | -13.6 ns
3 | -12.6 ns
4 | -10.5 ns
5 | -10.9 ns
6 | -10.8 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 1.1940, 1a.1940).
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 2.1940.0-6)
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 3.1940.0-6).
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 1940 summary. (Mar 12, 2017 - Mar 18, 2017)
Table 1.1940.a GPS week : 1940 MJD: 57824.0-57830.0
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 1 -8 -14 32 .09 28 27 | -11903 570 3246 11362
| 1 1 2 26 24 17 .04 | 1570 1321
cof n/a| -2 0 0 -6 3 26 .13 33 30 | -11904 571 3245 11363
| 1 1 2 22 31 27 .05 | 1574 1335
emx n/a| 0 0 6 -12 -60 -48 .12 25 25 | -19616 897 3226 10570
| 1 1 1 15 19 46 .05 | 8670 862
esx n/a| 1 0 0 21 20 21 .12 17 16 | -14323 329 3239 13290
| 1 1 1 17 14 29 .03 | 12117 1495
gfz n/a| 0 0 1 25 17 7 .04 24 20 | 0 620 3228 10685
| 1 1 2 16 12 43 .07 | 0 1432
grg n/a| 0 0 3 -49 28 -101 -.39 34 32 | 15619 -52750 3282 11144
| 1 1 2 20 26 106 .11 | 58916 112637
iac n/a| 0 0 -9 9 -4 29 -.14 22 22 | -11110 -145 3238 10513
| 1 1 1 32 20 46 .05 | 876 721
mcc n/a| -10 2 2 -45 -52 327 -1.07 239 239 | --- --- --- ---
| 8 5 12 145 90 1203 .85 | --- ---
Table 1.1940.b GPS week : 1940 MJD: 57824.0-57830.0
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 | 18 13 13 13 11 10 12 |
R02 | 11 11 8 7 9 9 8 |
R03 | 18 12 9 9 11 8 8 |
R04 | 9 8 8 8 11 8 7 |
R05 | 14 14 13 16 14 14 12 |
R07 | 10 12 9 8 8 10 8 |
R08 | 10 11 11 10 9 9 9 |
R09 | 8 8 8 7 9 8 8 |
R10 | 9 9 8 8 8 7 8 |
R11 | 10 7 8 10 8 8 7 |
R13 | 8 8 9 9 9 12 8 |
R14 | 11 11 14 12 14 15 14 |
R15 | 11 9 11 12 12 11 11 |
R16 | 17 12 10 10 11 11 16 |
R17 | 9 9 10 9 8 7 9 |
R18 | 7 8 7 8 6 7 7 |
R19 | 13 13 14 13 12 10 8 |
R20 | 14 14 14 15 17 16 15 |
R21 | 7 9 9 10 9 7 9 |
R22 | 9 8 7 10 11 8 7 |
R23 | 7 8 6 9 8 7 9 |
R24 | 21 12 14 19 18 13 19 |
R26 | --- --- --- --- 0 0 0 |
Table 1.1940.c GPS week : 1940 MJD: 57824.0-57830.0
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 1940 0 | -18 17 -4 -168 615 351 85.2 1169 1169 | -12133 0
brd 1940 1 | 17 -64 30 608 267 -1095 83.9 1048 1048 | -11541 0
brd 1940 2 | 43 -8 82 1218 1235 1111 85.0 985 985 | -13592 0
brd 1940 3 | -60 44 139 -870 610 2316 87.7 1272 1272 | -12554 0
brd 1940 4 | 28 73 160 -1315 507 6160 87.2 1468 1468 | -10531 0
brd 1940 5 | 10 2 151 -338 -389 2316 87.0 1705 1705 | -10895 0
brd 1940 6 | 38 -13 41 -1077 707 2230 85.0 1689 1689 | -10808 0
-------------+------------------------------------------------------------+----------------
brd 1940 mean| 8 7 86 -277 507 1912 85.9 1333 1333 | -11722 0
brd 1940 sdev| 36 44 65 922 492 2257 1.4 293 293 | 1105 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 2.1940.0 GPS week: 1940 Day: 0 MJD: 57824
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 -45 -24 39 .13 31 28 | -11846 434 3209 11263
cof n/a| -3 0 3 25 30 8 .13 40 31 | -11860 459 3203 11270
emx n/a| -2 0 4 5 -55 -38 .15 25 25 | -5773 1374 3176 10525
esx n/a| 1 1 0 48 8 36 .14 18 17 | 5965 836 3203 13267
gfz n/a| 0 2 5 45 35 -15 -.10 28 23 | 0 281 3207 10593
grg n/a| 0 1 2 -47 15 -88 -.63 37 33 | -12321 250 3233 10849
iac n/a| 2 0 -11 -37 -19 43 -.12 31 31 | -11897 -154 3183 10645
mcc n/a| -11 -3 -7 -143 -78 1858 -1.16 290 290 | --- --- --- ---
Table 2.1940.1 GPS week: 1940 Day: 1 MJD: 57825
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 39 25 12 .05 33 28 | -14507 1928 3193 12537
cof n/a| -2 0 -2 18 19 58 .12 36 32 | -14509 1935 3195 12533
emx n/a| 1 -3 5 -33 -43 -80 .12 23 23 | -10144 1260 3162 11382
esx n/a| 0 0 1 6 -5 15 .15 14 13 | -4268 1934 3186 14709
gfz n/a| 0 -1 2 34 3 -30 .09 23 21 | 0 2328 3170 11880
grg n/a| 0 0 -1 -66 74 -109 -.36 33 33 | -12946 2423 3198 12281
iac n/a| 0 2 -11 14 21 103 -.24 22 22 | -10838 -396 3204 11722
mcc n/a| 1 12 6 -299 -156 886 -2.18 256 256 | --- --- --- ---
Table 2.1940.2 GPS week: 1940 Day: 2 MJD: 57826
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -3 0 10 -21 35 .10 30 30 | -13433 748 3169 11253
cof n/a| 0 -3 -1 -9 0 25 .18 32 30 | -13441 766 3169 11252
emx n/a| 0 0 6 -18 -61 -69 .20 28 28 | -24948 1419 3160 10483
esx n/a| 1 1 -1 39 34 5 .12 13 11 | -16263 1585 3163 13736
gfz n/a| 1 -2 3 32 13 -1 .05 25 22 | 0 990 3164 10564
grg n/a| 0 -1 6 -46 20 -9 -.34 29 27 | -14122 831 3159 11116
iac n/a| 0 0 -10 -25 -33 16 -.12 21 21 | -12334 -754 3162 10343
mcc n/a| -20 0 0 -114 -105 -578 -1.70 293 293 | --- --- --- ---
Table 2.1940.3 GPS week: 1940 Day: 3 MJD: 57827
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 2 -9 12 47 .09 28 28 | -11100 -1619 3305 10804
cof n/a| -4 0 -2 -15 28 29 .11 30 30 | -11086 -1650 3307 10801
emx n/a| -1 0 7 -2 -95 -23 .11 25 25 | -20183 -662 3292 10106
esx n/a| 2 1 0 31 33 10 .07 17 17 | -12939 -2193 3303 12723
gfz n/a| 1 0 1 19 23 15 -.01 24 17 | 0 -1467 3301 10154
grg n/a| -4 0 3 -68 -2 -188 -.35 37 33 | -11751 -1493 3307 10713
iac n/a| 0 0 -11 8 -14 42 -.11 20 20 | -11728 -772 3311 9925
mcc n/a| -15 -1 27 50 66 -1834 -1.79 360 360 | --- --- --- ---
Table 2.1940.4 GPS week: 1940 Day: 4 MJD: 57828
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 -17 -15 56 .12 27 26 | -9871 910 3091 11405
cof n/a| -1 0 2 -13 22 62 .20 31 29 | -9867 894 3088 11407
emx n/a| -2 -1 9 -32 -47 26 .10 25 25 | -20268 1146 3065 10819
esx n/a| 2 0 -1 17 32 78 .13 21 20 | -27028 -1137 3101 13218
gfz n/a| 0 0 0 35 18 75 .07 25 20 | 0 838 3074 10639
grg n/a| 1 -2 5 -68 36 -287 -.34 34 35 | -10932 946 3119 11239
iac n/a| 0 2 -7 44 -8 -51 -.13 19 19 | -10195 1143 3089 10429
mcc n/a| 1 4 -11 96 83 349 -.23 158 158 | --- --- --- ---
Table 2.1940.5 GPS week: 1940 Day: 5 MJD: 57829
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 4 -18 -34 7 .04 27 27 | -11021 -541 3024 11875
cof n/a| -1 1 3 -40 -24 -16 .04 30 28 | -11017 -553 3022 11880
emx n/a| 0 0 5 -9 -41 -119 .04 24 24 | -27974 55 3002 10888
esx n/a| 0 -1 0 9 23 18 .15 17 15 | -17612 253 3001 13692
gfz n/a| 1 1 0 10 0 -44 .08 21 18 | 0 -853 2999 11206
grg n/a| 0 0 5 -14 7 16 -.32 34 31 | 145152 -300826 3201 11882
iac n/a| 1 1 -8 13 17 41 -.15 18 18 | -10110 -601 3002 10893
mcc n/a| -16 6 -3 2 -91 603 -.14 153 153 | --- --- --- ---
Table 2.1940.6 GPS week: 1940 Day: 6 MJD: 57830
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 2 -16 -42 25 .13 23 23 | -11543 2131 3731 10403
cof n/a| -3 0 -1 -9 -53 18 .14 30 29 | -11552 2150 3736 10402
emx n/a| 0 0 5 0 -74 -31 .08 24 24 | -28024 1689 3725 9793
esx n/a| 0 0 -3 0 20 -16 .12 19 18 | -28121 1029 3716 11685
gfz n/a| 2 1 0 -1 24 50 .07 22 17 | 0 2224 3683 9765
grg n/a| -1 0 3 -30 51 -43 -.40 35 31 | 26257 -71387 3761 9931
iac n/a| 0 0 -8 49 3 9 -.14 20 20 | -10670 513 3715 9639
mcc n/a| -10 1 4 85 -84 1008 -.29 165 165 | --- --- --- ---
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 3.1940.0 GPS week: 1940 Day: 0 MJD: 57824
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 461 44 44 23 20 47 38 69 --- 18 | 3 6 5 4 11 4 4 --- 4
R02 | 2735 12 21 19 23 17 30 40 332 11 | 5 5 4 5 3 9 3 22 2
R03 | 733 43 53 26 26 30 29 69 423 17 | 3 9 8 8 6 6 3 27 4
R04E | 752 28 37 20 9 18 31 18 --- 9 | 3 8 8 6 3 3 3 --- 3
R05E | 649 41 46 23 19 39 47 32 --- 14 | 4 5 5 3 6 5 5 --- 3
R07E | 1163 33 37 19 11 23 21 23 --- 9 | 3 5 4 6 5 4 5 --- 2
R08E | 647 27 21 25 14 24 21 18 --- 9 | 3 5 4 4 6 4 3 --- 3
XR09 | 1638 20 22 15 12 18 --- 14 --- 7 | 2 4 3 4 5 --- 2 --- 2
R10 | 648 28 23 13 15 20 24 13 --- 8 | 3 5 2 2 5 5 2 --- 2
R11 | 827 34 46 22 8 28 13 30 94 10 | 3 4 3 4 4 4 2 16 1
R13 | 690 28 30 17 9 16 17 21 --- 8 | 2 5 2 2 5 4 2 --- 2
R14 | 1634 26 29 13 21 29 36 29 --- 11 | 3 5 3 6 6 4 3 --- 3
R15 | 827 28 31 27 23 32 18 17 --- 11 | 3 3 2 3 2 4 2 --- 2
R16 | 1016 29 62 37 32 23 70 31 --- 17 | 3 8 2 4 5 4 3 --- 3
R17 | 580 23 22 21 12 28 21 16 --- 9 | 2 2 4 2 5 3 2 --- 2
R18 | 1286 17 14 9 9 21 26 14 --- 7 | 2 3 3 3 4 3 2 --- 1
R19 | 2150 51 49 23 23 25 27 26 --- 13 | 3 3 4 4 4 5 2 --- 2
R20 | 1653 40 65 25 28 22 55 13 --- 14 | 5 8 4 8 6 2 3 --- 5
R21 | 517 11 12 8 16 22 21 18 194 7 | 2 3 3 4 4 2 2 19 2
R22 | 553 20 23 12 13 29 33 15 --- 9 | 2 2 3 3 3 3 2 --- 2
R23 | 581 13 20 13 7 10 29 15 --- 6 | 2 3 5 7 4 4 1 --- 3
R24 | 1209 35 71 64 16 46 84 31 --- 21 | 3 11 5 5 3 5 3 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS | 1168 31 40 25 18 28 37 31 289 |T 2 5 3 4 4 4 2 21 2
WRMS | 1168 28 31 25 17 23 33 31 289 |NE 2 4 3 4 4 3 2 17 2
MEDI | 752 28 30 20 15 23 29 18 194 |MD 3 5 4 4 5 4 2 19 2
Table 3.1940.1 GPS week: 1940 Day: 1 MJD: 57825
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 568 48 57 29 11 37 36 23 --- 13 | 3 7 5 8 11 4 6 --- 5
R02E | 2454 37 20 27 13 27 16 24 179 10 | 4 8 9 7 9 8 5 5 5
R03E | 474 42 38 32 20 26 24 18 324 11 | 4 9 8 8 7 6 4 5 4
R04E | 703 28 29 18 10 25 23 14 --- 8 | 3 8 7 6 7 6 4 --- 3
R05E | 1034 40 40 30 18 33 42 29 --- 13 | 4 7 10 8 12 6 5 --- 4
R07E | 778 37 45 30 14 20 23 32 406 11 | 3 7 6 7 5 4 8 9999 3
R08E | 831 23 27 19 11 25 37 30 --- 10 | 3 5 5 7 6 4 4 --- 4
XR09 | 1543 19 20 14 14 17 --- 18 --- 8 | 3 4 3 4 5 --- 2 --- 2
R10 | 654 27 46 13 13 27 30 18 --- 9 | 3 6 2 3 5 5 2 --- 2
R11 | 602 25 27 12 10 21 19 16 74 7 | 3 4 3 4 4 5 2 2 2
R13 | 576 26 25 18 10 26 16 16 --- 8 | 3 5 3 5 8 3 3 --- 3
R14 | 1769 29 33 25 17 15 35 32 --- 11 | 3 11 4 7 7 4 3 --- 4
R15 | 1674 28 37 22 17 20 17 14 --- 8 | 3 4 3 3 5 7 2 --- 3
R16 | 858 38 46 17 20 11 50 22 --- 11 | 3 9 3 5 5 3 3 --- 3
R17 | 454 21 21 17 10 26 37 20 --- 9 | 2 3 3 4 6 5 2 --- 2
R18 | 741 20 24 18 7 16 29 18 --- 7 | 2 4 3 3 4 4 2 --- 2
R19 | 1353 50 55 39 14 28 16 20 --- 12 | 3 6 5 6 5 5 2 --- 3
R20 | 1178 28 39 26 16 17 73 19 --- 13 | 6 8 5 9 7 5 4 --- 6
R21 | 633 21 30 12 17 15 29 24 145 8 | 3 4 3 4 5 4 2 2 2
R22 | 535 21 22 9 15 17 16 25 --- 7 | 3 5 3 4 4 4 1 --- 2
R23 | 729 12 16 11 13 17 33 14 --- 7 | 3 3 4 6 5 4 1 --- 2
R24 | 806 52 38 30 17 17 26 21 --- 11 | 4 9 4 10 5 6 2 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1048 33 36 23 14 23 33 22 256 |T 3 6 4 5 6 4 3 3 3
WRMS | 1048 28 32 23 13 21 33 22 256 |NE 3 5 3 5 5 4 2 2 2
MEDI | 741 28 30 18 14 20 29 20 179 |MD 3 6 4 6 5 5 2 2 3
Table 3.1940.2 GPS week: 1940 Day: 2 MJD: 57826
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 583 48 38 39 14 25 42 15 --- 13 | 5 3 5 9 7 4 5 --- 4
R02E | 2030 24 20 19 9 26 19 13 374 7 | 5 6 7 6 9 4 5 5 5
R03E | 1230 35 28 18 12 24 26 12 218 9 | 4 6 6 5 7 6 5 5 4
R04E | 800 31 38 17 7 25 17 9 --- 7 | 5 6 4 5 7 5 5 --- 3
R05E | 1095 23 28 21 21 30 37 36 --- 12 | 4 9 8 10 12 5 5 --- 5
R07E | 902 33 42 28 8 28 15 14 467 8 | 4 8 5 6 6 5 6 9999 3
R08E | 707 19 30 27 16 23 24 36 --- 11 | 4 4 6 8 6 5 6 --- 4
XR09 | 1599 19 21 19 15 10 --- 14 --- 7 | 4 2 4 4 5 --- 2 --- 2
R10 | 760 24 38 13 11 24 14 23 --- 8 | 4 6 3 5 6 3 2 --- 3
R11 | 662 24 23 18 5 29 24 14 123 8 | 4 4 3 4 6 3 1 2 2
R13 | 793 31 23 23 9 24 20 18 --- 8 | 4 4 4 5 8 2 2 --- 3
R14 | 956 19 30 23 26 23 49 39 --- 14 | 4 11 4 7 9 3 2 --- 3
R15 | 1241 35 28 32 8 17 37 15 --- 10 | 4 5 2 4 6 6 2 --- 3
R16 | 799 29 33 34 17 13 28 16 --- 10 | 5 8 5 4 7 3 2 --- 2
R17 | 615 37 35 29 15 17 19 17 --- 9 | 4 3 2 5 6 4 3 --- 2
R18 | 554 16 15 19 10 12 18 22 --- 7 | 4 2 2 2 4 3 2 --- 2
R19 | 1247 47 44 40 17 51 22 20 --- 14 | 4 6 4 9 9 4 2 --- 4
R20 | 942 33 33 47 12 24 58 17 --- 14 | 6 7 5 6 7 6 4 --- 4
R21 | 802 28 21 21 8 21 17 23 92 8 | 4 5 4 3 7 5 3 2 2
R22 | 714 29 34 16 7 15 8 18 --- 6 | 4 4 2 4 5 4 1 --- 2
R23 | 1287 6 10 14 10 13 19 10 --- 5 | 4 2 3 6 6 3 1 --- 2
R24 | 755 34 49 44 19 35 42 24 --- 14 | 4 8 4 8 5 7 4 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 985 30 32 28 13 25 29 21 293 |T 4 5 4 5 6 4 3 3 3
WRMS | 985 30 30 28 11 22 27 21 293 |NE 4 5 3 5 6 4 2 2 2
MEDI | 800 29 30 21 11 24 22 17 218 |MD 4 5 4 5 6 4 2 2 3
Table 3.1940.3 GPS week: 1940 Day: 3 MJD: 57827
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 986 42 37 29 13 30 39 21 --- 12 | 6 3 6 7 8 6 4 --- 4
R02E | 2829 16 24 15 8 20 20 12 354 6 | 6 5 4 7 8 5 4 15 4
R03E | 1928 32 28 19 11 25 16 13 398 8 | 6 4 6 7 8 4 4 48 4
R04E | 866 22 23 17 10 24 24 10 --- 7 | 5 2 5 5 9 5 5 --- 4
R05E | 1199 27 23 31 28 42 52 31 --- 15 | 6 11 5 14 21 7 6 --- 7
R07E | 1330 29 23 17 14 19 23 12 559 8 | 6 5 4 6 8 5 5 9999 4
R08E | 1317 25 26 22 15 23 35 17 --- 9 | 6 3 6 5 7 4 6 --- 4
XR09 | 2145 16 14 18 10 15 --- 11 --- 7 | 5 2 3 4 7 --- 2 --- 2
R10 | 523 19 22 14 16 13 22 18 --- 7 | 5 5 3 4 7 5 2 --- 2
R11 | 730 25 23 15 20 24 12 24 202 9 | 5 4 3 4 6 3 2 4 2
R13 | 2283 29 28 18 13 20 29 15 --- 8 | 5 4 3 3 7 5 2 --- 2
R14 | 817 30 33 27 14 19 51 23 --- 11 | 5 9 6 7 11 5 4 --- 4
R15 | 805 32 36 30 23 32 25 11 --- 11 | 5 4 2 5 8 3 2 --- 2
R16 | 1095 25 41 23 17 17 38 17 --- 10 | 6 8 5 6 8 3 2 --- 3
R17 | 752 27 34 18 12 28 15 17 --- 8 | 5 3 3 4 6 5 2 --- 2
R18 | 546 24 22 20 10 14 15 16 --- 7 | 5 3 4 4 6 2 3 --- 2
R19 | 1441 39 40 21 28 18 40 22 --- 12 | 5 4 3 10 9 3 1 --- 4
R20 | 806 34 41 48 12 21 63 16 --- 14 | 6 7 7 4 7 5 3 --- 3
R21 | 845 27 35 24 10 28 34 15 105 10 | 5 4 3 4 8 6 3 3 3
R22 | 580 24 24 17 13 16 16 31 --- 9 | 5 4 4 4 7 3 2 --- 2
R23 | 1168 18 13 20 23 17 24 12 --- 8 | 5 2 3 6 6 2 1 --- 2
R24 | 1023 35 39 39 28 29 85 37 --- 18 | 6 6 4 7 8 5 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1272 28 30 24 17 24 37 20 360 |T 5 4 4 5 8 4 3 17 3
WRMS | 1272 28 30 24 17 17 33 20 360 |NE 5 4 3 5 7 3 2 3 2
MEDI | 986 27 26 20 13 20 25 16 354 |MD 5 4 4 5 8 5 3 4 3
Table 3.1940.4 GPS week: 1940 Day: 4 MJD: 57828
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 706 34 34 28 13 30 29 19 --- 11 | 6 3 6 5 7 7 4 --- 3
R02E | 3341 22 27 18 14 21 33 15 61 9 | 6 7 3 8 10 5 4 24 4
R03E | 1159 24 31 22 14 18 28 29 227 10 | 6 5 7 13 8 5 5 79 5
R04E | 720 23 18 22 16 31 17 29 --- 10 | 6 5 7 11 10 4 5 --- 5
R05E | 1587 24 23 34 25 37 48 27 --- 14 | 6 9 4 11 17 7 6 --- 5
R07E | 2060 22 22 16 11 16 24 13 155 7 | 6 6 4 9 8 5 5 9999 3
R08E | 1780 24 25 21 10 21 28 12 --- 8 | 6 3 4 6 7 5 4 --- 3
XR09 | 1730 15 19 15 18 10 --- 21 --- 8 | 6 3 3 4 7 --- 2 --- 2
R10 | 613 16 16 15 23 11 20 12 --- 7 | 6 7 2 3 7 5 2 --- 2
R11 | 577 21 25 11 11 26 19 13 197 7 | 6 4 2 3 7 7 2 7 2
R13 | 3214 31 40 20 12 23 11 21 --- 9 | 6 3 2 3 7 7 1 --- 2
R14 | 952 43 42 29 27 29 45 21 --- 14 | 6 8 5 9 17 9 3 --- 7
R15 | 831 36 31 22 23 28 34 15 --- 11 | 6 3 2 6 8 7 2 --- 2
R16 | 2009 22 31 15 25 13 53 12 --- 11 | 6 6 4 9 8 2 2 --- 3
R17 | 796 20 20 14 17 20 25 16 --- 8 | 6 3 3 3 6 5 2 --- 2
R18 | 590 10 21 12 8 21 16 10 --- 5 | 6 3 3 6 7 5 3 --- 2
R19 | 729 41 40 22 23 38 24 14 --- 12 | 6 3 3 8 7 7 1 --- 3
R20 | 752 38 60 56 29 27 54 25 --- 17 | 6 9 8 6 8 6 3 --- 4
R21 | 764 28 27 18 11 23 21 20 84 9 | 6 2 2 3 7 5 2 3 3
R22 | 1018 23 31 27 13 34 27 23 --- 11 | 6 4 4 5 7 5 3 --- 2
R23 | 680 14 22 13 27 15 16 9 --- 7 | 6 4 3 5 8 7 1 --- 1
R24 | 964 25 25 42 48 27 73 21 --- 18 | 6 9 6 13 11 7 2 --- 6
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 9999 --- 1
------+---------------------------------------------------+-----------------------------------------------
RMS | 1467 27 31 25 21 25 34 19 158 |T 6 4 3 6 8 5 2 28 3
WRMS | 1467 26 29 25 20 20 35 19 158 |NE 6 4 3 5 8 6 2 5 2
MEDI | 831 23 25 20 16 23 27 16 155 |MD 6 4 3 6 7 5 2 7 3
Table 3.1940.5 GPS week: 1940 Day: 5 MJD: 57829
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 502 27 27 22 13 22 40 16 --- 10 | 5 8 5 7 9 8 6 --- 4
R02E | 2735 22 17 24 9 24 31 16 99 9 | 5 7 6 8 8 6 4 5 3
R03E | 1196 22 23 22 9 24 22 12 153 8 | 5 7 5 11 8 5 5 5 4
R04E | 756 18 13 22 12 17 19 21 --- 8 | 5 6 5 12 8 4 5 --- 5
R05E | 1560 22 25 28 30 27 47 30 --- 13 | 6 6 4 7 9 5 7 --- 4
R07E | 2571 27 29 31 11 30 21 15 107 10 | 5 9 8 9 8 6 5 9999 4
R08E | 3017 23 23 22 9 15 40 9 --- 8 | 5 6 3 9 7 5 5 --- 3
XR09 | 1721 16 17 16 12 18 --- 13 --- 7 | 5 3 2 3 6 --- 2 --- 2
R10 | 783 17 25 23 15 10 19 13 --- 7 | 5 5 3 4 6 4 2 --- 2
R11 | ---- 22 21 15 17 18 16 20 267 8 | 5 6 2 4 7 10 1 2 3
R13 | 4151 35 31 21 20 31 32 22 --- 11 | 5 5 3 3 6 5 2 --- 2
R14 | 2354 40 46 22 34 33 38 29 --- 14 | 5 11 3 9 15 8 4 --- 6
R15 | 695 43 46 27 11 22 26 24 --- 11 | 5 6 3 6 7 9 2 --- 3
R16 | 1199 20 26 27 19 17 48 20 --- 11 | 5 8 4 8 6 5 2 --- 2
R17 | 538 17 23 17 9 16 16 12 --- 6 | 5 3 2 3 6 5 2 --- 2
R18 | 690 20 17 14 14 11 23 10 --- 6 | 5 2 2 5 7 8 2 --- 3
R19 | 968 30 31 30 17 23 16 15 --- 9 | 5 5 2 6 6 6 2 --- 2
R20 | 515 40 31 47 20 18 69 24 --- 16 | 5 9 5 8 9 6 3 --- 4
R21 | 661 29 30 13 10 16 11 15 42 7 | 5 4 2 2 6 5 2 2 2
R22 | 691 24 21 23 8 18 15 14 --- 7 | 5 4 2 4 5 5 2 --- 2
R23 | 570 16 19 15 22 10 15 11 --- 7 | 5 6 2 5 7 7 2 --- 2
R24 | 1318 22 61 24 22 23 63 20 --- 13 | 5 11 4 12 9 9 3 --- 5
XR26 | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 9999 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1705 27 30 24 17 21 34 18 153 |T 5 6 3 6 7 6 3 3 3
WRMS | 1705 27 28 24 15 18 31 18 153 |NE 5 5 2 5 7 6 2 2 2
MEDI | 968 22 25 22 13 18 23 15 107 |MD 5 6 3 6 7 6 2 2 3
Table 3.1940.6 GPS week: 1940 Day: 6 MJD: 57830
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 997 30 35 32 13 30 36 17 --- 11 | 4 6 3 6 7 5 5 --- 4
R02E | 1044 11 21 23 16 17 27 18 83 8 | 5 5 5 6 7 5 5 6 3
R03E | 1839 21 23 16 12 20 25 10 135 7 | 4 5 3 6 5 3 4 5 3
R04E | 805 13 21 17 12 13 29 15 --- 7 | 5 3 3 7 5 4 4 --- 3
R05E | 847 20 25 23 20 21 44 28 --- 11 | 5 5 3 5 8 5 6 --- 4
R07E | 1300 22 24 18 8 24 19 15 90 8 | 4 6 6 6 6 5 4 9999 3
R08E | 3513 19 26 24 13 24 17 19 --- 8 | 4 5 3 7 6 4 4 --- 3
XR09 | 1496 20 17 16 13 20 --- 11 --- 8 | 3 3 1 1 4 --- 2 --- 1
R10 | 1080 19 19 22 15 18 23 12 --- 8 | 4 3 2 3 4 3 2 --- 1
R11 | 648 24 33 14 10 12 19 16 318 7 | 3 5 1 3 5 7 2 2 2
R13 | 3626 26 29 15 12 19 13 20 --- 8 | 4 4 2 3 4 3 2 --- 2
R14 | 2344 28 47 27 31 34 41 24 --- 13 | 4 9 2 5 6 4 3 --- 3
R15 | 1198 34 43 17 22 22 27 27 --- 11 | 3 5 2 4 5 6 2 --- 2
R16 | 592 24 34 56 26 19 50 33 --- 16 | 4 6 3 3 4 4 2 --- 2
R17 | 1573 24 22 24 15 16 22 14 --- 8 | 3 3 1 2 5 4 1 --- 2
R18 | 872 15 15 13 12 16 31 12 --- 7 | 3 2 1 3 5 6 2 --- 2
R19 | 1634 23 23 14 10 19 18 14 --- 7 | 3 4 1 4 5 3 2 --- 2
R20 | 706 21 32 28 39 19 57 32 --- 15 | 4 6 2 6 7 3 3 --- 3
R21 | 978 27 34 15 11 17 22 23 40 9 | 3 3 2 2 5 4 1 2 2
R22 | 944 20 30 15 6 12 22 18 --- 7 | 3 3 2 1 4 3 2 --- 1
R23 | 562 11 16 26 26 13 19 13 --- 8 | 3 4 2 3 4 4 2 --- 1
R24 | 2906 38 49 29 28 49 86 17 --- 18 | 4 5 2 5 4 6 3 --- 2
XR26 | ---- --- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- 9999 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1689 23 30 24 19 22 35 20 165 |T 3 4 2 4 5 4 2 3 2
WRMS | 1689 23 29 24 18 17 31 20 165 |NE 3 4 1 3 4 4 2 2 1
MEDI | 1044 21 25 18 13 19 25 17 90 |MD 4 5 2 4 5 4 2 2 2
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