[IGSREPORT-25390] Wk 1955 IGLOS Final Orbits
acc
acc at igs.org
Sun Jul 16 21:58:31 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1955 (Jun 25, 2017 - Jul 01, 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 2.1955.
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:
igl1955[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1955 in the SP3 format.
igl19557.sum Combination Report for GPS Week 1955.
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 | 19.1 ns
1 | -15.0 ns
2 | 26.9 ns
3 | 9.2 ns
4 | 1.3 ns
5 | 23.5 ns
6 | 10.3 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1955, 1a.1955).
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 2.1955.0-6)
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 3.1955.0-6).
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 1955 summary. (Jun 25, 2017 - Jul 01, 2017)
Table 1.1955.a GPS week : 1955 MJD: 57929.0-57935.0
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 -2 -10 0 21 .25 26 26 | 694192 116 146449 436066
| 0 1 3 17 11 14 .09 | 2758658 4287
cof n/a| 0 0 -3 -14 8 12 .16 29 28 | 694189 108 146451 436069
| 1 1 2 20 15 12 .12 | 2758660 4300
emx n/a| 0 0 6 6 -13 -9 .22 22 21 | 0 -395 3347 10803
| 0 0 2 19 30 20 .12 | 0 879
esx n/a| 0 0 -1 23 14 -5 .05 21 18 | 6670 -1473 3657 12692
| 1 1 2 9 14 21 .12 | 19106 3070
gfz n/a| 0 1 3 -30 37 40 -.12 25 22 | -272310 1269 288209 294094
| 1 0 2 26 17 26 .16 | 497302 4508
grg n/a| 0 0 -1 -37 32 -88 -.44 28 26 | -132185 1747 145974 152561
| 1 1 5 20 23 55 .21 | 382940 6408
iac n/a| 0 0 -2 33 -38 23 -.13 22 21 | 703247 871 146470 435721
| 1 1 3 27 16 32 .06 | 2762094 3545
mcc n/a| -3 -1 -37 74 1 508 -.01 288 288 | --- --- --- ---
| 15 16 26 212 112 1020 .85 | --- ---
Table 1.1955.b GPS week : 1955 MJD: 57929.0-57935.0
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 | 16 16 12 12 13 8 10 |
R02 | 10 11 10 9 7 7 6 |
R03 | 7 9 9 7 8 5 8 |
R04 | 8 7 7 7 6 7 5 |
R05 | 20 15 19 14 13 16 13 |
R06 | 12 9 8 9 9 11 11 |
R07 | 9 8 7 6 8 9 6 |
R08 | 8 15 9 9 8 9 6 |
R09 | 8 7 8 9 10 8 11 |
R10 | 10 8 10 8 9 8 8 |
R11 | 9 7 7 7 8 6 6 |
R13 | 8 7 8 8 8 9 7 |
R14 | 20 65 1544 2008 1523 374 61 |
R15 | 10 10 8 10 8 7 8 |
R16 | 17 14 13 15 19 16 15 |
R17 | 10 9 9 9 11 10 10 |
R18 | 10 8 8 8 8 8 9 |
R19 | 12 15 571 95 66 14 14 |
R20 | 16 15 16 15 15 14 12 |
R21 | 8 12 11 10 9 9 9 |
R22 | 13 10 12 10 11 10 9 |
R23 | 13 9 10 8 10 10 9 |
R24 | 20 15 12 15 15 15 14 |
R26 | 22 26 20 21 13 19 27 |
Table 1.1955.c GPS week : 1955 MJD: 57929.0-57935.0
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 1955 0 | 27 7 214 1616 305 -607 83.5 1135 1135 | 19053 0
brd 1955 1 | 8 -4 268 899 295 -21 83.3 1307 1307 | -14978 0
brd 1955 2 | 102 67 334 900 510 -497 86.1 1368 1368 | 26934 0
brd 1955 3 | -10 -43 364 802 -1048 509 85.7 1280 1280 | 9163 0
brd 1955 4 | -26 -4 306 -1119 -1232 2826 85.9 1341 1341 | 1286 0
brd 1955 5 | 31 22 243 -400 -1710 3992 84.8 1384 1384 | 23466 0
brd 1955 6 | 41 64 213 525 -902 3229 86.1 1223 1223 | 10305 0
-------------+------------------------------------------------------------+----------------
brd 1955 mean| 24 15 277 460 -540 1347 85.1 1291 1291 | 10747 0
brd 1955 sdev| 41 39 59 920 890 1937 1.2 87 87 | 14415 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 2.1955.0 GPS week: 1955 Day: 0 MJD: 57929
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 1 -3 12 12 .26 29 26 | 7193 772 3368 12376
cof n/a| -3 0 -1 -11 34 19 .30 30 25 | 7166 777 3369 12389
emx n/a| -1 0 6 2 -39 -13 .29 26 27 | 0 617 3394 11559
esx n/a| 0 -1 -1 30 7 -15 .14 23 20 | 10853 -4946 3356 14565
gfz n/a| 1 1 6 -27 29 48 -.27 27 25 | 28616 1071 3390 12074
grg n/a| 1 0 -4 -56 46 -5 -.85 34 31 | 18868 505 3385 11831
iac n/a| 1 2 -6 9 -54 8 -.12 32 32 | 19750 202 3360 11410
mcc n/a| -8 6 -30 439 148 -210 .00 283 283 | --- --- --- ---
Table 2.1955.1 GPS week: 1955 Day: 1 MJD: 57930
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 0 9 8 .25 24 22 | -30673 -3701 5898 16983
cof n/a| 0 0 -1 -10 9 19 .02 28 24 | -30682 -3721 5903 16981
emx n/a| 0 0 8 31 -20 -11 .34 19 17 | 0 -473 2997 11543
esx n/a| 1 1 -4 25 28 22 -.09 25 21 | -33051 -678 4408 16058
gfz n/a| 1 2 4 -21 49 45 .05 30 25 | -7736 -1325 4000 13419
grg n/a| 1 -4 -4 -56 30 -100 -.56 32 31 | -15212 -1528 4252 13421
iac n/a| 0 0 -5 11 -36 -10 -.10 21 20 | -21347 -2383 5918 17306
mcc n/a| -22 0 -64 -110 14 -636 -1.86 310 310 | --- --- --- ---
Table 2.1955.2 GPS week: 1955 Day: 2 MJD: 57931
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 0 -25 -3 38 .29 23 25 | 12552 -2975 3482 11868
cof n/a| 0 -2 0 -45 4 32 .12 26 27 | 12543 -2980 3478 11864
emx n/a| -1 0 11 12 8 -6 .31 24 24 | 0 -1391 3481 10854
esx n/a| 0 2 -2 27 -11 16 -.10 22 18 | 13389 -3674 3483 13473
gfz n/a| 0 1 2 -12 33 7 -.09 25 23 | 35728 -2358 3487 11298
grg n/a| 1 -1 -10 -9 26 -81 -.42 29 28 | 28541 -3149 3545 10682
iac n/a| -1 0 1 18 -34 -14 -.03 20 19 | 25693 -309 3491 10906
mcc n/a| 9 11 -75 -191 -198 -393 .11 281 281 | --- --- --- ---
Table 2.1955.3 GPS week: 1955 Day: 3 MJD: 57932
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -3 -9 11 2 .28 27 26 | -999999 9157 999999 999999
cof n/a| 0 -1 -5 8 1 -7 .03 29 27 | -999999 9173 999999 999999
emx n/a| 0 1 4 0 -47 -31 .22 21 21 | 0 923 3868 10393
esx n/a| 1 -1 -3 34 29 -42 .04 21 19 | 5433 4013 4289 4451
gfz n/a| 0 2 4 -85 47 38 -.23 25 23 | -999999 8315 999999 999999
grg n/a| 1 0 1 -15 -7 -35 -.21 24 24 | 7309 3614 3935 10212
iac n/a| 1 0 0 35 -17 62 -.16 18 16 | -999999 8573 999999 999999
mcc n/a| -10 -19 -7 215 100 425 .63 355 355 | --- --- --- ---
Table 2.1955.4 GPS week: 1955 Day: 4 MJD: 57933
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 -6 -16 0 22 .41 26 26 | -999999 69 5799 999999
cof n/a| -1 0 -5 -1 22 11 .32 31 27 | -999999 93 5804 999999
emx n/a| 0 1 6 24 -30 20 .25 23 18 | 0 -855 3128 9708
esx n/a| 1 1 -2 25 19 -3 .05 19 17 | 4182 591 3496 13464
gfz n/a| 0 0 0 -32 61 3 -.33 22 19 | -999999 6958 999999 999999
grg n/a| 0 0 5 -38 68 -114 -.35 31 28 | -999999 15437 999999 999999
iac n/a| 0 0 0 18 -56 22 -.10 21 21 | -999999 972 5906 999999
mcc n/a| -15 -13 -12 94 -57 810 .28 252 252 | --- --- --- ---
Table 2.1955.5 GPS week: 1955 Day: 5 MJD: 57934
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 -7 15 -5 30 .13 29 30 | 12195 -891 3601 11242
cof n/a| -1 -1 -7 -1 0 5 .15 34 34 | 12220 -954 3605 11252
emx n/a| 0 0 6 -27 -9 11 .17 22 19 | 0 -1214 3577 10762
esx n/a| -1 0 2 6 18 -12 .07 20 17 | 25462 -2065 3581 13201
gfz n/a| -2 0 4 -31 6 70 .00 22 20 | 25216 -2098 3595 10685
grg n/a| 2 0 -2 -31 18 -104 -.32 26 22 | 24586 -1781 3728 10982
iac n/a| 0 0 -4 83 -17 30 -.16 20 20 | 25884 -363 3603 10432
mcc n/a| 8 -16 -24 110 18 1418 .15 291 291 | --- --- --- ---
Table 2.1955.6 GPS week: 1955 Day: 6 MJD: 57935
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 -3 -36 -20 37 .16 27 29 | 6858077 -1619 3000 999999
cof n/a| 0 0 -3 -40 -12 6 .20 28 30 | 6858079 -1632 3003 999999
emx n/a| -1 0 3 0 41 -35 -.02 20 18 | 0 -374 2989 10803
esx n/a| 0 1 -1 12 12 -1 .22 18 16 | 20425 -3553 2987 13638
gfz n/a| 0 0 4 -3 37 71 .06 23 20 | 12003 -1677 2994 11186
grg n/a| -1 0 1 -56 45 -175 -.36 24 20 | 10609 -863 2978 10804
iac n/a| 0 -1 -1 55 -54 67 -.22 18 18 | 6872752 -590 3017 999999
mcc n/a| 17 23 -48 -36 -14 2148 .60 247 247 | --- --- --- ---
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 3.1955.0 GPS week: 1955 Day: 0 MJD: 57929
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 | 801 26 34 44 23 44 46 31 --- 16 | 49 76 41 64 91 75 58 --- 56
R02 | 829 23 19 14 24 28 26 16 176 10 | 51 53 56 64 65 52 57 260 54
R03 | 1299 10 14 13 10 18 31 14 380 7 | 53 56 55 55 54 39 50 207 50
R04 | 928 12 9 21 18 20 18 17 --- 8 | 49 52 45 55 52 44 42 --- 46
R05 | 679 49 39 53 33 35 55 33 --- 19 | 44 51 57 69 75 59 52 --- 53
R06 | 789 23 25 20 26 37 28 28 --- 12 | 31 44 44 61 61 43 34 --- 42
R07 | 593 14 21 20 12 17 35 23 418 9 | 60 59 60 55 56 60 60 404 56
R08 | 813 17 34 14 13 24 15 20 --- 8 | 51 56 66 65 62 46 54 --- 55
XR09E | 4386 14 18 16 6 20 --- 19 --- 7 | 34 36 43 37 37 --- 47 --- 37
R10E | 747 15 21 19 14 20 20 43 --- 10 | 64 79 70 77 73 65 62 --- 67
R11E | 1602 16 16 15 15 15 28 33 163 9 | 56 54 48 55 52 50 51 78 49
R13E | 1431 10 10 17 13 17 28 19 --- 7 | 83 83 83 81 82 87 82 --- 82
R14E | 906 48 33 43 45 31 50 42 --- 19 | 546 817 15 42 38 87 777 --- 600
R15E | 747 19 15 21 16 21 23 27 --- 9 | 68 71 69 75 84 85 81 --- 74
R16E | 1237 38 42 33 31 38 46 40 --- 16 | 90 93 101 87 100 88 93 --- 89
R17E | 686 30 32 17 11 20 19 29 --- 9 | 60 65 35 40 24 41 38 --- 36
R18 | 522 20 21 17 19 24 24 34 --- 10 | 72 75 59 65 59 69 40 --- 57
R19E | 1367 41 48 22 22 28 24 22 --- 12 | 121 147 20 67 113 47 58 --- 86
R20E | 2237 46 52 30 29 35 31 34 --- 15 | 85 97 67 95 90 92 75 --- 80
R21 | 678 26 28 16 10 20 23 16 157 8 | 86 85 66 65 65 64 60 138 65
R22 | 926 36 34 21 18 29 32 39 --- 13 | 90 92 64 68 62 82 82 --- 69
R23 | 881 36 36 29 29 17 32 24 --- 13 | 132 124 123 143 137 140 136 --- 133
R24 | 2133 30 30 33 27 31 65 72 --- 19 | 111 116 113 116 101 101 70 --- 98
XR26E | ---- 21 38 --- --- --- --- 23 --- 22 | 40 54 --- --- --- --- 54 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 1134 29 30 26 23 27 34 32 283 |T 88 105 60 69 71 68 92 217 86
WRMS | 1134 26 25 27 20 25 31 32 283 |NE 67 72 65 72 72 67 61 252 64
MEDI | 881 23 28 20 18 24 28 27 176 |MD 60 71 59 65 65 64 58 207 56
Table 3.1955.1 GPS week: 1955 Day: 1 MJD: 57930
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 | 1197 18 15 33 26 61 39 28 --- 15 | 30 37 36 59 83 34 41 --- 39
R02 | 1648 17 20 18 22 28 50 14 365 11 | 32 36 41 44 44 28 35 374 32
R03 | 995 12 14 16 27 28 23 11 386 9 | 32 38 34 50 44 26 29 127 32
R04 | 1032 10 12 12 17 19 15 21 --- 7 | 33 36 35 45 48 32 31 --- 34
R05 | 659 33 36 14 42 37 53 15 --- 14 | 35 49 51 54 58 51 29 --- 38
R06 | 856 19 21 14 13 28 23 22 --- 8 | 28 29 36 32 46 26 26 --- 26
R07 | 764 14 34 12 27 14 19 14 --- 7 | 37 49 38 33 31 41 29 --- 30
R08 | 867 18 28 10 60 35 33 25 --- 14 | 35 49 43 74 59 25 38 --- 39
XR09E | 4706 14 12 15 9 19 --- 12 --- 7 | 19 21 19 23 31 --- 25 --- 19
R10E | 630 15 22 14 19 15 26 15 --- 7 | 66 67 67 71 69 67 74 --- 67
R11E | 939 16 19 16 15 18 15 14 296 7 | 50 54 47 55 51 48 47 80 48
R13E | 2927 10 13 15 16 16 24 12 --- 7 | 61 63 58 62 63 57 63 --- 60
XR14E | 1121 104 252 --- --- --- 114 64 --- 65 | 411 776 --- --- --- 83 924 --- 569
R15E | 785 10 14 16 19 37 26 22 --- 10 | 48 48 48 44 64 49 46 --- 46
R16E | 1672 31 38 25 26 39 40 28 --- 13 | 73 72 74 61 69 67 68 --- 63
R17E | 674 32 35 17 13 21 20 13 --- 9 | 37 42 31 33 29 41 30 --- 30
R18 | 694 23 21 20 15 17 17 13 --- 8 | 35 29 21 34 28 34 30 --- 25
XR19E | 1055 42 44 --- 22 30 21 23 --- 14 | 273 301 --- 122 231 59 58 --- 161
R20E | 1189 44 41 22 24 40 37 27 --- 14 | 55 63 47 58 62 51 50 --- 46
R21 | 762 37 38 18 17 29 34 21 116 11 | 65 64 55 52 47 56 47 116 51
R22 | 1211 36 42 19 8 25 22 16 --- 10 | 48 47 25 30 23 33 27 --- 26
R23 | 1420 21 20 15 24 12 26 21 --- 9 | 50 50 51 62 54 54 59 --- 52
R24 | 2399 22 29 32 26 29 47 35 --- 14 | 38 66 54 54 61 45 54 --- 44
XR26E | ---- 28 49 --- --- --- --- 23 --- 25 | 30 45 --- --- --- --- 47 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1306 24 28 19 25 30 32 21 310 |T 67 88 43 52 58 45 79 174 67
WRMS | 1306 22 24 17 21 25 31 20 310 |NE 38 44 40 47 48 37 36 205 36
MEDI | 1032 19 22 16 19 28 26 21 296 |MD 37 49 43 52 51 45 41 116 39
Table 3.1955.2 GPS week: 1955 Day: 2 MJD: 57931
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 | 1029 22 26 29 34 19 19 28 --- 12 | 39 44 43 53 46 46 48 --- 38
R02 | 1614 16 24 23 26 31 22 19 --- 10 | 43 40 39 44 54 34 48 --- 40
R03 | 704 14 13 19 14 28 22 13 342 8 | 40 39 41 39 53 36 38 179 36
R04 | 888 10 19 16 17 10 17 15 --- 6 | 42 46 51 41 45 31 38 --- 40
R05 | 594 37 32 48 37 35 65 28 --- 18 | 43 43 63 60 64 32 43 --- 45
R06 | 835 13 22 25 13 16 21 19 --- 8 | 31 36 34 38 29 31 29 --- 29
R07 | 859 13 9 10 16 16 16 14 --- 6 | 47 42 45 51 44 45 38 --- 42
R08 | 673 15 14 13 11 29 21 21 --- 8 | 43 47 50 48 60 38 33 --- 42
XR09E | 3038 13 12 18 10 18 --- 13 --- 7 | 18 19 19 18 23 --- 27 --- 17
R10E | 751 12 18 20 20 27 39 18 --- 10 | 44 41 39 40 46 43 35 --- 38
R11E | 735 14 13 15 15 21 17 12 335 7 | 46 41 38 47 42 46 38 158 41
R13E | 2970 16 15 20 16 13 32 12 --- 8 | 48 49 49 51 48 45 47 --- 46
XR14E | ---- 1678 1806 --- --- --- --- 1420 --- 1543 | 9999 9999 --- --- --- --- 9999 --- 988
R15E | 918 12 12 15 21 22 18 10 --- 7 | 47 50 45 52 48 51 42 --- 46
R16E | 1760 18 26 34 27 16 39 32 --- 13 | 69 79 64 66 74 72 83 --- 68
R17E | 643 30 42 14 15 22 23 16 --- 9 | 46 54 23 31 22 41 31 --- 28
R18 | 669 23 25 13 11 19 20 14 --- 7 | 45 46 32 36 32 36 29 --- 33
XR19E |>>>>> 795 1111 --- --- 462 --- 988 --- 570 | 9999 9999 --- --- 9999 --- 148 --- 9999
R20E | 930 37 38 34 28 48 40 28 --- 16 | 59 62 41 61 71 62 44 --- 47
R21 | 1274 37 36 23 12 25 22 17 92 10 | 59 58 37 44 32 32 32 95 37
R22 | 1194 46 41 22 11 28 12 15 --- 11 | 64 58 34 35 23 35 25 --- 33
R23 | 1977 18 24 18 30 15 28 14 --- 9 | 42 35 41 67 48 40 48 --- 46
R24 | 2766 19 37 30 31 22 35 27 --- 12 | 40 44 49 54 48 34 42 --- 38
XR26E | ---- 22 56 --- --- --- --- 17 --- 19 | 41 41 --- --- --- --- 35 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1367 23 26 24 22 25 29 20 281 |T 45 46 41 46 45 41 44 144 80
WRMS | 1367 25 27 24 18 23 28 19 281 |NE 44 44 43 46 44 36 37 137 38
MEDI | 918 18 24 20 16 22 22 17 335 |MD 43 44 41 47 46 38 38 158 40
Table 3.1955.3 GPS week: 1955 Day: 3 MJD: 57932
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 | 485 23 47 39 25 27 18 17 --- 11 | 45 70 36 50 58 51 47 --- 43
R02 | 960 14 22 16 27 18 24 18 430 9 | 42 45 44 39 38 36 47 410 38
R03 | 1229 10 12 13 9 25 18 13 244 7 | 47 48 41 51 48 54 55 115 47
R04 | 718 7 18 10 28 12 14 14 --- 7 | 35 35 37 32 34 46 42 --- 35
R05 | 1053 43 33 29 24 29 39 18 --- 13 | 39 53 59 59 68 59 62 --- 55
R06 | 1259 23 25 17 13 24 16 19 --- 8 | 27 24 26 33 49 25 24 --- 27
R07 | 659 13 13 18 14 12 13 9 608 6 | 50 50 43 63 63 64 52 350 54
R08 | 830 14 15 11 29 14 24 13 --- 8 | 44 43 46 66 57 39 47 --- 47
XR09E | 2977 17 16 19 8 20 --- 18 --- 8 | 19 19 17 25 29 --- 28 --- 20
R10E | 795 19 22 16 16 12 23 21 --- 8 | 55 57 65 60 51 60 60 --- 58
R11E | 711 11 18 16 15 20 11 14 110 6 | 39 46 38 36 45 35 38 168 36
R13E | 2673 13 17 16 16 19 24 11 --- 7 | 36 37 31 44 39 51 42 --- 38
XR14E | 2157 2642 6108 --- --- --- --- 1524 --- 2007 | 9999 9999 --- --- --- --- 9999 --- 9999
R15E | 1476 16 22 18 18 33 32 15 --- 10 | 40 45 34 47 60 39 47 --- 41
R16E | 1962 28 13 32 31 40 38 29 --- 14 | 45 48 66 41 60 41 47 --- 41
R17E | 922 34 27 14 12 23 23 8 --- 8 | 44 41 29 34 21 28 24 --- 26
R18 | 1183 24 33 17 15 24 20 11 --- 8 | 41 47 32 35 23 32 29 --- 28
XR19E | 1070 113 108 --- 261 108 --- 101 --- 94 | 324 371 --- 124 244 --- 33 --- 217
R20E | 1015 46 35 26 24 37 27 40 --- 15 | 65 59 33 51 37 32 54 --- 38
R21 | 1244 35 38 12 16 30 17 19 76 9 | 62 60 36 45 26 35 34 87 37
R22 | 817 44 54 17 11 26 13 13 --- 9 | 66 75 33 43 24 34 28 --- 34
R23 | 1588 28 28 14 22 14 17 11 --- 8 | 39 45 44 61 46 46 57 --- 48
R24 | 1843 32 35 39 33 37 36 22 --- 15 | 55 64 47 57 36 51 38 --- 40
XR26E | ---- 28 86 --- --- --- --- 14 --- 20 | 18 101 --- --- --- --- 34 --- 24
------+---------------------------------------------------+-----------------------------------------------
RMS | 1279 27 29 21 21 25 24 18 355 |T 55 64 39 49 52 42 42 226 46
WRMS | 1279 26 27 21 19 23 24 16 355 |NE 45 50 40 48 43 44 43 240 41
MEDI | 1070 23 25 17 16 24 20 15 244 |MD 44 48 37 45 45 39 42 168 38
Table 3.1955.4 GPS week: 1955 Day: 4 MJD: 57933
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 | 891 21 19 21 38 12 50 16 --- 12 | 46 36 42 38 42 79 43 --- 40
R02 | 643 11 21 16 17 16 17 15 325 7 | 39 50 48 47 43 45 44 147 42
R03 | 1563 10 12 11 10 17 29 21 156 7 | 42 43 46 47 41 42 57 74 44
R04 | 910 10 7 16 10 14 15 6 --- 5 | 35 33 39 34 29 33 33 --- 32
R05 | 1831 36 41 22 25 20 50 17 --- 12 | 36 38 58 41 35 49 40 --- 39
R06 | 1037 26 27 12 14 15 25 22 --- 8 | 21 33 31 30 32 38 31 --- 26
R07 | 642 15 14 17 7 21 17 19 426 7 | 42 47 44 49 64 54 63 171 50
R08 | 705 14 27 17 10 14 22 25 --- 7 | 40 45 43 42 48 60 39 --- 42
XR09E | 2500 16 21 24 12 23 --- 18 --- 9 | 22 33 24 29 35 --- 26 --- 22
R10E | 818 18 24 17 19 13 24 21 --- 8 | 36 46 42 40 41 50 41 --- 38
R11E | 777 17 16 15 16 16 26 18 55 8 | 25 26 22 29 29 28 19 89 21
R13E | 2845 18 19 18 15 18 21 12 --- 7 | 37 39 29 38 40 39 37 --- 35
XR14E | 3907 1760 4373 --- --- --- --- 1317 --- 1522 | 9999 9999 --- --- --- --- 9999 --- 9999
R15E | 1970 15 25 19 14 14 29 16 --- 8 | 30 39 30 34 33 33 31 --- 29
R16E | 1717 24 44 63 24 35 55 41 --- 19 | 56 71 68 59 65 50 52 --- 53
R17E | 1105 36 37 20 18 23 27 21 --- 10 | 48 47 28 36 21 38 34 --- 29
R18 | 1150 25 25 19 12 23 18 11 --- 8 | 40 40 39 34 36 34 32 --- 32
XR19E | 1733 93 85 --- 217 91 75 87 --- 66 | 298 322 --- 182 231 67 40 --- 190
R20E | 699 44 64 23 25 38 39 32 --- 15 | 65 85 39 38 51 42 44 --- 39
R21 | 1395 32 31 18 8 19 14 20 59 8 | 58 58 40 43 39 37 37 78 40
R22 | 1034 45 38 17 8 33 22 12 --- 11 | 64 56 31 32 27 39 30 --- 32
R23 | 1622 32 34 13 32 12 16 10 --- 9 | 32 34 46 74 49 47 52 --- 50
R24 | 1106 21 39 29 29 30 45 38 --- 14 | 47 64 42 51 47 43 46 --- 35
XR26E | ---- 15 49 --- --- --- --- 10 --- 13 | 42 65 --- --- --- --- 30 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1340 26 31 23 19 22 31 21 252 |T 52 58 39 47 49 45 39 111 43
WRMS | 1340 26 27 18 17 19 28 21 252 |NE 41 44 42 43 40 46 42 117 38
MEDI | 1106 21 27 18 15 18 25 18 156 |MD 40 45 40 38 40 42 39 89 38
Table 3.1955.5 GPS week: 1955 Day: 5 MJD: 57934
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 | 1541 19 25 24 15 13 20 13 --- 8 | 38 49 42 59 55 48 47 --- 47
R02 | 699 16 13 15 16 17 20 10 527 7 | 34 31 44 42 43 41 36 239 38
R03 | 849 13 14 15 10 11 9 11 266 5 | 37 40 38 44 34 49 40 134 39
R04 | 1059 13 21 17 12 20 15 16 --- 7 | 38 40 41 38 43 40 33 --- 36
R05 | 953 46 44 29 25 20 57 29 --- 15 | 53 59 44 69 46 58 33 --- 47
R06 | 1009 20 23 18 29 33 24 22 --- 11 | 29 33 26 42 33 22 22 --- 22
R07 | 821 18 22 19 25 23 15 17 250 9 | 39 40 44 64 56 42 44 99 46
R08 | 1616 12 21 9 20 25 27 16 --- 8 | 35 50 41 52 57 26 32 --- 39
XR09E | 1562 12 20 24 10 12 --- 15 --- 8 | 18 19 20 22 25 --- 22 --- 18
R10E | 1220 12 15 13 15 12 24 20 --- 7 | 55 60 61 63 57 68 60 --- 59
R11E | 1185 16 22 17 13 13 12 11 96 6 | 47 50 40 49 46 53 46 77 45
R13E | 4008 17 17 15 16 22 28 17 --- 8 | 70 75 76 68 71 62 73 --- 69
XR14E | 3313 467 1068 --- --- --- --- 298 --- 374 | 9999 9999 --- --- --- --- 9999 --- 9999
R15E | 1423 15 19 14 15 20 16 13 --- 7 | 52 51 46 53 55 47 54 --- 50
R16E | 788 19 27 53 26 33 33 34 --- 15 | 74 77 87 74 77 75 82 --- 75
R17E | 1051 45 49 18 11 24 13 15 --- 10 | 48 51 26 24 21 30 25 --- 24
R18 | 654 23 23 18 17 15 16 19 --- 8 | 60 62 51 57 50 58 51 --- 53
R19E | 903 55 57 28 14 29 34 27 --- 14 | 171 191 28 85 153 35 63 --- 98
R20E | 709 37 71 24 34 24 40 31 --- 14 | 50 84 30 48 55 47 49 --- 40
R21 | 1440 37 39 16 11 25 16 13 61 9 | 46 49 28 25 23 26 33 85 26
R22 | 1299 43 48 14 11 23 16 17 --- 9 | 65 67 44 45 40 48 39 --- 44
R23 | 765 29 29 15 26 23 17 18 --- 9 | 31 30 40 53 47 32 51 --- 42
R24 | 1210 35 41 31 29 29 36 35 --- 14 | 37 48 41 47 40 31 45 --- 33
XR26E | ---- 22 31 --- --- --- --- 16 --- 18 | 31 50 --- --- --- --- 40 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1383 29 34 22 20 22 26 20 291 |T 50 56 42 51 51 44 44 126 44
WRMS | 1383 30 34 19 17 20 22 20 291 |NE 41 46 40 49 43 40 38 139 39
MEDI | 1059 19 23 17 15 22 20 17 250 |MD 46 50 41 49 46 47 44 99 42
Table 3.1955.6 GPS week: 1955 Day: 6 MJD: 57935
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 | 2574 18 13 22 13 30 18 23 --- 9 | 51 57 46 58 71 62 65 --- 56
R02 | 733 8 12 14 11 10 16 12 --- 5 | 61 59 65 64 64 57 64 --- 61
R03 | 671 10 10 12 16 22 21 15 412 7 | 57 58 62 69 71 58 60 210 61
R04 | 960 8 12 10 9 13 17 12 --- 5 | 56 59 57 54 53 51 50 --- 52
R05 | 928 33 31 13 32 25 48 13 --- 12 | 56 58 66 63 62 64 51 --- 58
R06 | 1090 27 31 28 27 23 19 16 --- 10 | 36 42 30 50 39 41 37 --- 36
R07 | 675 8 11 12 14 14 15 10 201 5 | 62 63 60 68 68 68 65 152 64
R08 | 1302 8 12 7 12 14 15 15 --- 5 | 57 61 62 67 68 55 52 --- 58
XR09E | 1595 17 22 25 10 19 --- 32 --- 11 | 18 22 24 20 23 --- 27 --- 19
R10E | 880 11 12 15 15 20 22 18 --- 7 | 66 67 64 68 66 73 65 --- 66
R11E | 1244 10 14 13 13 17 16 10 173 6 | 65 68 61 64 56 63 62 69 61
R13E | 2905 15 16 16 12 22 15 12 --- 6 | 92 92 92 92 95 94 91 --- 92
XR14E | 1114 77 131 --- --- --- --- 47 --- 60 | 570 667 --- --- --- --- 871 --- 728
R15E | 1161 11 12 19 18 20 20 12 --- 7 | 60 65 55 63 69 53 58 --- 58
R16E | 564 27 26 44 20 30 33 39 --- 15 | 86 84 98 85 91 88 96 --- 89
R17E | 560 38 45 17 16 28 15 13 --- 9 | 61 66 34 38 28 40 32 --- 34
R18 | 691 29 34 23 13 22 14 14 --- 8 | 58 61 53 42 42 44 42 --- 43
R19E | 721 64 67 19 14 31 33 18 --- 14 | 200 218 17 66 174 30 58 --- 124
R20E | 675 41 27 16 22 23 21 28 --- 11 | 68 71 42 50 52 42 47 --- 44
R21 | 1090 33 36 13 11 23 20 18 58 8 | 71 73 46 49 40 44 47 113 47
R22 | 1269 44 40 12 7 22 12 13 --- 9 | 88 87 55 57 45 62 50 --- 57
R23 | 652 23 29 20 22 13 23 19 --- 9 | 44 44 54 75 56 47 72 --- 59
R24 | 1106 20 15 29 33 33 47 24 --- 14 | 41 44 40 59 41 45 56 --- 43
XR26E | ---- 31 67 --- --- --- --- 23 --- 26 | 37 57 --- --- --- --- 39 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1222 27 28 20 18 23 24 18 247 |T 85 93 53 60 62 56 89 136 85
WRMS | 1222 29 30 18 16 20 20 18 247 |NE 56 58 53 59 55 53 54 158 53
MEDI | 960 20 22 16 14 22 19 15 173 |MD 60 61 55 63 56 55 56 113 58
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