[IGSREPORT-21064] Wk 1698 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Aug 10 09:10:15 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1698 (Jul 22, 2012 - Jul 28, 2012)
Contact: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1698.
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:
igl1698[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1698 in the SP3 format.
igl16987.sum Combination Report for GPS Week 1698.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
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 | 183.2 ns
1 | 182.5 ns
2 | 183.4 ns
3 | 187.2 ns
4 | 184.8 ns
5 | 184.6 ns
6 | 186.7 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
----+--------+---------------
2 | COD | R18
2 | EMX | R18
2 | GRG | R18
4 | IAC | R18
5 | GRG | R24
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 1.1698, 1a.1698).
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 2.1698.0-6)
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 3.1698.0-6).
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 1698 summary. (Jul 22, 2012 - Jul 28, 2012)
Table 1.1698.a GPS week : 1698 MJD: 56130.0-56136.0
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 261| -2 1 -5 113 -7 -82 -.19 34 34 | --- --- --- ---
| 2 1 1 39 22 33 .04 | --- ---
emx 139| 0 0 -2 -19 0 55 -.20 29 29 | 184033 -1115 3999 6993
| 2 2 4 42 21 35 .04 | 1804 2849
esx 175| 0 0 -1 -34 -2 -47 .46 18 16 | 184915 -1679 4004 4396
| 1 1 1 23 31 40 .04 | 2216 3931
gfz 196| 0 -1 -2 -9 -4 -2 -.25 18 15 | 0 -1380 3998 6824
| 1 1 2 45 31 31 .04 | 0 3691
grg 124| 0 3 -1 26 -37 57 -.04 48 37 | 131813 -1048 4016 19417
| 1 2 5 34 30 43 .07 | 13370 3230
iac n/a| 1 1 10 -2 34 31 -.02 24 24 | 185759 -907 3997 6936
| 1 1 6 23 28 90 .05 | 1902 1225
mcc n/a| 1 2 23 43 56 346 -.27 123 123 | --- --- --- ---
| 4 5 14 82 48 211 .33 | --- ---
Table 1.1698.b GPS week : 1698 MJD: 56130.0-56136.0
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 15 12 13 13 14 14 |
R02 | 14 10 12 13 14 20 13 |
R03 | 12 15 11 9 11 12 10 |
R04 | 11 10 11 10 12 10 10 |
R05 | 9 11 8 11 11 10 9 |
R06 | 8 8 9 10 12 8 10 |
R07 | 9 11 10 9 12 12 9 |
R08 | 10 7 9 9 9 11 12 |
R09 | 10 12 10 8 8 11 11 |
R10 | 13 10 8 8 7 8 7 |
R11 | 17 17 15 18 15 14 12 |
R12 | 12 11 10 11 12 9 8 |
R13 | 8 10 9 11 11 9 10 |
R14 | 12 13 13 16 14 11 12 |
R15 | 10 6 7 8 9 10 10 |
R16 | 12 11 11 8 11 10 12 |
R17 | 12 13 12 10 13 12 12 |
R18 | 11 11 14 0 434 14 11 |
R19 | 0 21 16 34 30 27 20 |
R20 | 0 0 26 27 40 36 38 |
R21 | 13 13 13 15 18 15 15 |
R22 | 11 12 10 10 12 14 12 |
R23 | 10 9 10 10 11 8 9 |
R24 | 11 11 10 12 12 9 10 |
R26 | --- --- --- --- 0 0 0 |
Table 1.1698.c GPS week : 1698 MJD: 56130.0-56136.0
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 1698 0 | 28 43 252 490 -285 -4066 83.6 1743 1743 | 183226 0
brd 1698 1 | -73 66 259 -211 -474 -1514 84.7 1500 1500 | 182547 0
brd 1698 2 | -43 -20 267 589 -591 -4431 82.7 1316 1316 | 183354 0
brd 1698 3 | -10 95 346 1395 -919 -8753 83.6 1329 1329 | 187191 0
brd 1698 4 | -55 -15 318 123 332 -4376 82.6 1391 1391 | 184750 0
brd 1698 5 | -21 -51 406 586 -222 -11880 83.8 1385 1385 | 184600 0
brd 1698 6 | 19 86 303 -127 -763 -10190 85.0 2032 2032 | 186715 0
-------------+------------------------------------------------------------+----------------
brd 1698 mean| -22 29 307 406 -417 -6458 83.7 1528 1528 | 184626 0
brd 1698 sdev| 37 58 55 547 412 3812 .9 266 266 | 1772 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 2.1698.0 GPS week: 1698 Day: 0 MJD: 56130
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 261| 0 0 -9 87 -15 -78 -.22 33 35 | --- --- --- ---
emx 139| -2 -2 -7 -8 31 39 -.14 27 27 | 182718 -635 3658 6002
esx 175| 1 1 -1 -30 -27 -65 .45 18 17 | 182231 1006 3651 3799
gfz 196| -1 -3 -5 -27 -19 18 -.21 20 14 | 0 35 3652 5900
grg 124| 1 4 0 -6 -61 93 .04 36 36 | 143549 -202 3660 17532
iac n/a| 3 2 19 35 74 5 -.12 25 25 | 183631 581 3637 6321
mcc n/a| 0 -6 34 25 0 397 .04 137 137 | --- --- --- ---
Table 2.1698.1 GPS week: 1698 Day: 1 MJD: 56131
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 261| -3 0 -4 149 10 -62 -.23 34 34 | --- --- --- ---
emx 139| 1 -2 -9 -24 -11 55 -.18 29 29 | 181656 -1444 3747 7305
esx 175| 0 -2 -1 2 3 -16 .48 19 15 | 182751 -1711 3765 3906
gfz 196| 0 1 -3 -43 -16 28 -.26 17 16 | 0 -2486 3750 7059
grg 124| -2 1 2 -24 -30 20 -.05 40 35 | 117804 -1472 3764 23317
iac n/a| 1 1 13 -26 24 -44 -.03 23 23 | 183711 -1274 3760 7105
mcc n/a| 7 1 42 101 18 613 -.19 141 141 | --- --- --- ---
Table 2.1698.2 GPS week: 1698 Day: 2 MJD: 56132
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 261| 1 2 -5 162 19 -82 -.18 35 34 | --- --- --- ---
emx 139| 1 -2 -4 63 0 -8 -.20 26 26 | 182927 -2242 4263 7395
esx 175| 0 0 0 -14 -14 -9 .52 17 15 | 184560 -3863 4238 4400
gfz 196| -2 0 1 -78 10 41 -.25 17 17 | 0 -2883 4234 7298
grg 124| 0 0 2 67 -33 87 -.04 38 35 | 133552 -3831 4245 20861
iac n/a| 2 0 1 -20 28 -69 .01 21 21 | 185381 -2545 4241 7638
mcc n/a| 4 4 4 57 98 264 -.24 95 95 | --- --- --- ---
Table 2.1698.3 GPS week: 1698 Day: 3 MJD: 56133
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 261| -2 1 -4 134 12 -123 -.22 35 36 | --- --- --- ---
emx 139| 0 3 0 -30 -22 81 -.27 28 29 | 183967 4667 4206 8533
esx 175| 2 -2 -1 -46 22 -116 .45 16 13 | 184584 5637 4209 4514
gfz 196| 0 -1 0 25 26 -38 -.31 20 16 | 0 6277 4204 8217
grg 124| -3 5 -9 2 -93 12 -.07 36 35 | 120254 5675 4220 18821
iac n/a| 1 0 10 -22 -1 208 -.03 24 24 | 185630 632 4204 8120
mcc n/a| 7 11 14 126 20 461 -.38 95 95 | --- --- --- ---
Table 2.1698.4 GPS week: 1698 Day: 4 MJD: 56134
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 261| -3 -1 -4 122 -43 -104 -.14 33 34 | --- --- --- ---
emx 139| 0 0 0 -20 -25 103 -.16 29 31 | 184362 -828 4054 6873
esx 175| 0 -1 1 -47 -49 -14 .46 21 19 | 184960 -2158 4063 4331
gfz 196| 1 -2 -1 -21 29 -29 -.20 19 15 | 0 -2087 4055 6611
grg 124| 0 2 -5 43 -3 2 -.17 38 41 | 131050 -1279 4062 21871
iac n/a| 1 3 5 -13 55 64 -.02 27 27 | 188537 -1963 4057 6616
mcc n/a| -1 -2 24 57 127 351 -.41 116 116 | --- --- --- ---
Table 2.1698.5 GPS week: 1698 Day: 5 MJD: 56135
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 261| -4 2 -6 59 -20 -22 -.13 32 34 | --- --- --- ---
emx 139| 2 3 0 -74 1 60 -.22 29 28 | 185787 -4223 4001 6715
esx 175| 1 -1 -1 -37 -1 -78 .48 21 20 | 186600 -4949 4038 5582
gfz 196| 1 -1 0 44 0 -15 -.22 16 12 | 0 -4799 4035 6536
grg 124| -1 2 4 47 -22 99 .01 115 45 | 154348 -3393 4112 17502
iac n/a| 0 0 5 5 53 15 -.02 24 24 | 185430 -389 4028 6563
mcc n/a| -2 6 33 64 88 404 -.86 134 134 | --- --- --- ---
Table 2.1698.6 GPS week: 1698 Day: 6 MJD: 56136
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 261| -4 2 -4 76 -15 -103 -.22 32 30 | --- --- --- ---
emx 139| -1 0 0 -41 20 55 -.22 32 32 | 186815 -3100 4065 6132
esx 175| 0 -2 -2 -67 47 -27 .38 17 15 | 188725 -5719 4067 4242
gfz 196| 0 -1 -6 32 -62 -21 -.25 18 18 | 0 -3717 4061 6148
grg 124| 1 7 -6 50 -16 83 -.00 36 31 | 122137 -2840 4051 16016
iac n/a| 0 1 16 20 4 41 .03 22 22 | 187999 -1391 4058 6191
mcc n/a| -1 1 9 -129 40 -67 .12 145 145 | --- --- --- ---
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 3.1698.0 GPS week: 1698 Day: 0 MJD: 56130
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1653 49 29 23 27 34 12 --- 12 | 70 39 41 61 42 40 --- 42
R02 | 1497 49 20 23 25 50 22 --- 13 | 65 16 40 46 48 21 --- 32
R03 | 1070 35 38 13 18 45 21 --- 12 | 80 82 86 86 96 69 --- 81
R04 | 1161 33 23 22 21 36 20 --- 11 | 55 39 33 40 31 32 --- 35
R05 | 757 35 18 14 17 27 16 88 9 | 48 39 46 45 30 31 14 38
R06 | 986 23 11 15 17 21 17 --- 7 | 42 26 34 32 40 30 --- 30
R07 | 1145 21 20 10 14 16 31 --- 8 | 62 57 54 53 45 33 --- 49
R08 | 2874 21 27 22 10 30 23 74 10 | 49 56 54 50 44 46 34 47
R09 | 1415 35 20 16 11 28 28 --- 10 | 27 35 30 24 40 18 --- 22
R10 | 1977 25 43 18 15 38 29 --- 12 | 16 24 34 27 41 22 --- 20
R11 | 1339 51 26 29 39 55 35 107 17 | 28 49 57 52 39 33 28 37
R12 | 1168 36 24 17 27 35 21 --- 11 | 24 25 42 53 32 20 --- 31
R13 | 2598 30 20 13 13 23 14 --- 8 | 22 30 39 36 31 19 --- 27
R14 | 1781 42 35 19 18 28 16 --- 11 | 16 34 40 36 35 23 --- 25
R15 | 947 26 23 14 20 36 14 79 9 | 27 22 26 28 28 20 35 18
R16 | 1499 33 16 15 14 52 28 --- 11 | 34 45 39 37 57 19 --- 32
R17E | 1859 24 35 18 14 37 29 264 11 | 44 51 58 55 55 43 86 47
R18E | 1253 26 26 15 17 39 30 111 11 | 9999 992 544 9999 677 936 577 9999
XR19E | ---- 9 --- --- --- --- --- --- 0 | 199 --- --- --- --- --- --- 208
XR20E | ---- 9 --- --- --- --- --- --- 0 | 43 --- --- --- --- --- --- 35
R21E | 3424 45 32 24 26 30 23 --- 13 | 45 62 74 71 79 46 --- 60
R22E | 2458 26 31 16 22 25 27 --- 11 | 28 48 56 57 55 35 --- 45
R23E | 1626 17 29 19 10 27 30 --- 10 | 113 116 124 126 112 111 --- 118
R24E | 801 22 26 10 17 41 35 --- 11 | 43 45 57 59 71 45 --- 51
------+----------------------------------------------+------------------------------------------
RMS | 1742 33 27 18 20 36 25 137 |T 51 87 73 51 78 76 129 49
WRMS | 1742 35 27 17 14 36 25 137 |NE 41 38 43 44 42 29 27 35
MEDI | 1415 26 26 16 17 34 23 88 |MD 43 39 42 50 42 32 34 37
Table 3.1698.1 GPS week: 1698 Day: 1 MJD: 56131
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2276 66 20 41 11 32 20 --- 14 | 44 14 44 24 32 22 --- 15
R02 | 1267 41 18 16 12 22 28 --- 10 | 47 38 30 34 35 25 --- 29
R03 | 992 22 32 15 21 78 28 --- 14 | 66 65 69 71 77 53 --- 61
R04 | 891 37 26 18 10 38 19 --- 10 | 37 42 20 28 21 19 --- 21
R05 | 782 43 24 19 17 48 13 63 11 | 28 26 19 24 31 15 19 10
R06 | 697 28 24 14 13 18 14 --- 8 | 27 25 22 24 30 22 --- 19
R07 | 1379 21 23 15 18 28 35 --- 10 | 33 37 37 37 37 21 --- 29
R08 | 1929 14 24 10 11 10 16 94 6 | 35 43 39 37 38 34 47 35
R09 | 1577 29 14 19 25 52 28 --- 12 | 27 22 30 35 44 16 --- 22
R10 | 953 20 18 15 14 47 19 --- 9 | 15 27 23 22 36 18 --- 13
R11 | 2254 72 33 30 17 59 21 116 16 | 22 63 70 47 73 34 47 45
R12 | 1284 35 28 9 13 52 18 --- 10 | 22 15 21 18 51 15 --- 14
R13 | 2008 29 21 14 20 29 22 --- 9 | 21 28 20 31 27 20 --- 18
R14 | 1306 27 44 23 20 41 24 --- 12 | 15 30 38 29 26 21 --- 21
R15 | 1031 15 16 6 13 17 18 79 6 | 20 20 19 16 25 16 28 13
R16 | 1149 37 22 13 21 34 25 --- 10 | 20 32 25 31 31 14 --- 19
R17E | 1324 27 39 26 19 35 27 145 12 | 32 39 44 39 32 28 67 29
R18E | 969 21 42 14 13 25 27 257 10 | 9999 9999 575 9999 591 899 700 9999
XR19E | ---- 26 --- --- --- --- 18 --- 21 | 169 --- --- --- --- 132 --- 171
XR20E | ---- 10 --- --- --- --- --- --- 0 | 39 --- --- --- --- --- --- 32
R21E | 2693 36 34 22 20 49 22 --- 12 | 29 33 58 48 72 38 --- 42
R22E | 1965 24 34 22 27 35 26 --- 12 | 36 61 58 64 41 37 --- 48
R23E | 915 20 33 12 17 27 19 --- 9 | 101 105 103 111 98 97 --- 102
R24E | 1142 28 44 12 14 40 19 --- 11 | 28 35 48 51 71 37 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1500 34 29 19 17 40 23 141 |T 39 38 64 39 69 71 151 36
WRMS | 1500 34 29 15 16 35 23 141 |NE 29 32 32 31 38 22 35 24
MEDI | 1267 27 24 15 17 35 21 94 |MD 29 33 37 34 36 22 47 29
Table 3.1698.2 GPS week: 1698 Day: 2 MJD: 56132
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2213 54 29 16 28 21 20 --- 12 | 54 22 55 68 42 25 --- 42
R02 | 1155 58 23 17 11 18 30 --- 11 | 50 32 24 27 23 24 --- 18
R03 | 1050 18 27 12 25 37 27 --- 10 | 59 55 48 67 57 34 --- 50
R04 | 881 23 25 16 15 51 22 --- 10 | 45 40 45 43 58 21 --- 36
R05 | 972 35 15 9 18 31 11 87 8 | 44 30 41 49 21 18 17 34
R06 | 1207 35 10 22 14 34 13 --- 9 | 34 21 32 27 40 16 --- 20
R07 | 1493 31 26 16 12 28 27 --- 10 | 50 33 39 42 32 23 --- 34
R08 | 1069 23 11 16 18 31 17 85 8 | 36 41 55 49 36 34 56 42
R09 | 991 33 16 17 13 48 14 --- 9 | 27 17 30 27 30 16 --- 17
R10 | 1194 19 16 15 13 29 15 --- 7 | 23 22 25 17 31 24 --- 14
R11 | 1272 67 41 17 18 59 21 80 15 | 26 64 56 45 66 37 40 42
R12 | 1045 44 21 14 16 39 15 --- 10 | 23 23 38 44 49 18 --- 27
R13 | 1298 27 19 11 14 25 22 --- 8 | 24 38 32 36 45 24 --- 28
R14 | 1409 34 43 20 18 47 28 --- 13 | 19 16 34 34 39 20 --- 19
R15 | 1270 14 17 11 12 18 22 105 7 | 17 25 23 22 21 16 28 15
R16 | 1667 36 17 14 20 44 21 --- 10 | 26 26 29 43 59 15 --- 26
R17E | 1361 29 37 27 18 29 23 114 12 | 35 33 54 46 51 31 52 37
XR18E | 4458 889 1549 --- 11 3316 17 --- 14 | 9999 9999 --- 9999 742 9999 --- 9999
XR19E | ---- 24 --- --- --- --- 9 --- 15 | 151 --- --- --- --- 105 --- 154
XR20E | ---- 39 --- --- --- --- 15 --- 25 | 37 --- --- --- --- 40 --- 39
R21E | 1867 28 29 23 24 57 24 --- 13 | 20 25 51 53 71 33 --- 37
R22E | 1451 23 24 19 19 36 21 --- 10 | 34 26 44 33 53 38 --- 30
R23E | 1098 23 22 19 15 50 18 --- 10 | 120 116 112 115 104 113 --- 112
R24E | 787 19 37 13 14 38 17 --- 10 | 48 51 52 56 79 56 --- 51
------+----------------------------------------------+------------------------------------------
RMS | 1315 35 26 17 17 38 21 95 |T 43 36 43 44 79 33 38 40
WRMS | 1315 34 26 15 17 35 21 95 |NE 34 31 37 40 40 22 35 29
MEDI | 1207 29 23 16 15 36 20 87 |MD 35 30 41 43 45 24 40 34
Table 3.1698.3 GPS week: 1698 Day: 3 MJD: 56133
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1569 51 28 24 23 21 26 --- 12 | 66 27 42 48 31 26 --- 34
R02 | 1177 45 31 16 22 29 38 --- 13 | 60 38 42 50 42 28 --- 35
R03 | 1003 24 22 11 12 20 33 --- 9 | 73 83 80 72 55 54 --- 69
R04 | 896 38 30 13 12 31 17 --- 9 | 49 46 23 24 24 27 --- 25
R05 | 1287 31 26 11 15 37 32 90 10 | 51 55 44 43 38 25 8 36
R06 | 1888 24 20 12 20 42 18 --- 9 | 40 40 37 40 39 27 --- 33
R07 | 1447 41 23 9 16 14 17 --- 8 | 57 37 27 25 36 34 --- 30
R08 | 1796 22 16 6 19 35 24 62 9 | 50 34 39 45 23 38 31 36
R09 | 955 27 12 11 9 33 16 --- 7 | 23 25 26 24 30 29 --- 22
R10 | 1117 22 21 8 16 28 19 --- 8 | 22 22 20 28 31 26 --- 18
R11 | 1606 62 43 25 41 52 21 75 17 | 24 33 56 66 45 38 31 38
R12 | 1405 52 28 12 14 37 12 --- 11 | 25 31 36 30 39 29 --- 25
R13 | 807 44 30 12 11 34 21 --- 10 | 22 40 37 36 40 26 --- 29
R14 | 1833 38 61 18 29 47 30 --- 16 | 15 40 36 44 49 28 --- 27
R15 | 1067 14 20 10 18 28 19 115 8 | 13 29 24 26 29 23 19 17
R16 | 1243 32 17 13 11 22 21 --- 8 | 20 27 35 26 25 26 --- 22
R17E | 1217 23 24 16 17 38 23 121 10 | 29 37 52 51 56 34 37 40
XR18E |10922 --- --- --- --- --- 13 --- 0 | --- --- --- --- --- 9999 --- 9999
XR19E | ---- 45 --- --- --- --- 25 --- 34 | 154 --- --- --- --- 98 --- 146
XR20E | ---- 33 --- --- --- --- 21 --- 26 | 44 --- --- --- --- 30 --- 37
R21E | 1955 34 33 27 22 68 29 --- 15 | 17 20 55 49 75 32 --- 37
R22E | 914 19 19 20 18 37 22 --- 10 | 46 52 63 66 61 46 --- 53
R23E | 755 19 23 13 22 30 26 --- 9 | 132 120 129 145 163 116 --- 131
R24E | 857 32 30 24 20 35 21 --- 11 | 56 58 79 67 71 60 --- 62
------+----------------------------------------------+------------------------------------------
RMS | 1328 35 28 16 20 36 24 95 |T 47 42 46 47 47 39 25 43
WRMS | 1328 36 29 13 16 35 24 95 |NE 38 37 37 39 36 30 22 31
MEDI | 1217 32 24 13 18 34 21 90 |MD 44 37 39 44 39 29 31 35
Table 3.1698.4 GPS week: 1698 Day: 4 MJD: 56134
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1107 57 43 14 13 24 15 --- 13 | 45 28 24 22 24 21 --- 14
R02 | 969 40 35 13 22 49 40 --- 14 | 53 33 41 43 84 12 --- 34
R03 | 753 25 18 31 14 15 35 --- 11 | 62 66 89 60 54 43 --- 62
R04 | 855 33 26 23 10 34 37 --- 12 | 47 46 21 33 31 33 --- 27
R05 | 898 27 25 9 15 42 35 85 11 | 44 54 39 36 27 22 8 30
R06 | 1013 24 23 21 24 51 18 --- 12 | 37 35 54 45 65 31 --- 41
R07 | 1147 31 29 23 22 25 26 --- 11 | 55 42 51 30 32 23 --- 35
R08 | 1914 22 20 17 17 28 16 85 8 | 32 28 26 25 51 20 22 24
R09 | 754 24 12 14 13 31 20 --- 8 | 23 27 29 24 28 17 --- 19
R10 | 1414 15 16 13 12 27 15 --- 7 | 21 20 29 28 30 21 --- 21
R11 | 1268 46 43 32 20 41 26 81 15 | 20 37 44 34 47 38 27 28
R12 | 1290 47 19 9 28 38 21 --- 12 | 29 39 28 44 39 21 --- 25
R13 | 616 38 19 14 12 41 21 --- 10 | 31 31 42 37 47 34 --- 32
R14 | 987 37 32 22 21 54 23 --- 13 | 17 34 38 35 49 24 --- 23
R15 | 2134 16 32 11 12 17 27 145 8 | 11 24 28 22 20 18 18 17
R16 | 1226 30 23 24 12 37 19 --- 10 | 17 32 36 24 37 17 --- 20
R17E | 1565 39 23 29 22 32 31 157 12 | 33 43 70 60 50 32 36 46
XR18E |23530 640 --- --- 293 --- 3298 --- 433 | 9999 --- --- 9999 --- 9999 --- 9999
XR19E | ---- 34 --- --- --- --- 26 --- 30 | 121 --- --- --- --- 112 --- 120
XR20E | ---- 46 --- --- --- --- 33 --- 39 | 44 --- --- --- --- 36 --- 29
R21E | 2870 36 53 30 30 65 33 --- 17 | 18 46 59 54 77 33 --- 40
R22E | 1304 21 30 21 22 45 29 --- 12 | 27 46 51 42 54 46 --- 38
R23E | 1041 17 36 15 16 42 21 --- 10 | 120 114 120 125 124 113 --- 117
R24E | 1893 26 25 25 18 20 39 --- 11 | 84 83 106 89 202 74 --- 84
XR26E | ---- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- 154 --- 155
------+----------------------------------------------+------------------------------------------
RMS | 1390 33 29 21 19 38 27 115 |T 43 43 48 43 55 41 22 45
WRMS | 1390 34 31 19 15 41 27 115 |NE 34 36 38 33 41 24 18 28
MEDI | 1147 31 25 21 17 37 26 85 |MD 33 37 41 36 47 31 22 30
Table 3.1698.5 GPS week: 1698 Day: 5 MJD: 56135
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1071 60 31 25 14 48 23 --- 14 | 50 31 42 37 45 31 --- 32
R02 | 1061 54 22 19 19 129 23 --- 19 | 46 20 22 36 86 24 --- 22
R03 | 1085 39 37 20 14 51 16 --- 12 | 55 76 73 70 28 58 --- 63
R04 | 775 19 24 16 10 17 39 --- 10 | 38 55 52 43 49 26 --- 39
R05 | 839 42 25 27 8 12 16 87 10 | 37 42 37 29 27 24 10 26
R06 | 1313 12 22 14 14 29 17 --- 7 | 29 25 44 41 49 28 --- 32
R07 | 796 30 19 31 25 27 27 --- 12 | 45 38 47 31 52 25 --- 34
R08 | 839 11 21 21 9 72 14 129 11 | 37 47 54 42 46 34 51 38
R09 | 838 30 23 27 12 46 18 --- 10 | 16 28 42 28 32 21 --- 23
R10 | 1578 10 17 19 12 29 22 --- 8 | 12 16 29 13 29 15 --- 13
R11 | 1120 41 45 29 14 44 22 91 13 | 30 45 35 31 33 28 42 24
R12 | 964 32 23 14 14 27 14 --- 8 | 21 28 21 26 39 15 --- 18
R13 | 949 37 11 13 15 22 17 --- 8 | 20 19 33 34 25 21 --- 23
R14 | 1225 21 40 19 15 33 28 --- 11 | 18 29 34 31 29 27 --- 22
R15 | 2480 22 31 16 11 34 22 156 9 | 26 30 30 23 40 16 17 20
R16 | 1346 33 20 18 9 44 23 --- 10 | 16 33 39 27 31 31 --- 24
R17E | 1844 32 33 26 19 39 22 183 12 | 35 43 56 49 42 31 40 38
XR18E |20091 28 --- 21 19 --- 31 --- 14 | 9999 --- 616 9999 --- 819 --- 9999
XR19E | ---- 34 --- --- --- --- 20 --- 26 | 109 --- --- --- --- 101 --- 115
XR20E | 9008 46 --- --- --- --- 28 --- 36 | 38 --- --- --- --- 29 --- 21
R21E | 1998 35 44 18 28 51 38 --- 15 | 32 34 51 58 69 35 --- 41
R22E | 1209 26 46 23 22 34 40 --- 14 | 62 95 73 74 81 52 --- 68
R23E | 1667 20 23 15 13 25 20 --- 8 | 111 122 105 113 108 100 --- 108
R24E | 2254 17 15 25 17 481 15 --- 9 | 49 51 40 55 300 40 --- 44
XR26E | ---- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- 277 --- 276
------+----------------------------------------------+------------------------------------------
RMS | 1385 32 29 21 16 115 24 134 |T 40 43 71 42 59 76 32 48
WRMS | 1385 34 28 20 12 45 24 134 |NE 31 35 39 33 40 26 30 28
MEDI | 1209 30 23 19 14 34 22 129 |MD 37 34 42 36 42 29 40 32
Table 3.1698.6 GPS week: 1698 Day: 6 MJD: 56136
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1183 54 27 15 28 47 25 --- 14 | 68 31 45 43 19 24 --- 33
R02 | 1089 57 26 20 13 35 20 --- 12 | 68 25 27 31 40 22 --- 23
R03 | 1231 30 43 15 14 32 11 --- 10 | 76 82 86 77 63 70 --- 76
R04 | 883 26 21 20 15 32 20 --- 9 | 57 53 62 59 46 36 --- 51
R05 | 1081 23 23 19 17 20 19 --- 8 | 64 49 65 50 64 46 --- 53
R06 | 1741 29 20 11 19 39 17 --- 9 | 54 38 43 36 48 45 --- 38
R07 | 839 29 23 8 17 26 21 --- 8 | 67 57 52 37 55 37 --- 46
R08 | 1755 15 28 13 24 64 13 96 11 | 49 57 47 40 63 47 41 45
R09 | 1010 28 51 18 12 17 17 --- 11 | 19 26 27 23 27 31 --- 20
R10 | 2820 18 21 11 13 20 16 --- 7 | 15 19 26 22 25 19 --- 17
R11 | 2009 40 40 13 14 50 18 85 12 | 24 49 36 39 34 44 58 33
R12 | 1188 25 18 9 16 33 12 --- 8 | 26 20 25 29 33 20 --- 18
R13 | 812 30 32 15 15 31 20 --- 10 | 26 29 35 32 39 24 --- 24
R14 | 2457 41 37 17 24 30 25 --- 12 | 29 28 32 41 43 24 --- 25
R15 | 2723 21 25 15 10 37 27 138 9 | 26 28 29 26 27 24 39 22
R16 | 2259 37 42 15 13 32 29 --- 12 | 15 47 37 31 31 27 --- 26
R17E | 2001 27 34 32 12 35 22 181 12 | 38 41 62 44 47 38 88 42
R18E | 4771 31 25 11 18 46 28 193 11 | 9999 9999 530 9999 773 939 392 9999
XR19E | 4643 26 --- --- --- --- 14 --- 20 | 114 --- --- --- --- 113 --- 111
XR20E | 1950 52 --- --- --- --- 25 --- 37 | 54 --- --- --- --- 27 --- 34
R21E | 2017 34 47 22 30 36 36 --- 14 | 21 31 59 64 68 33 --- 43
R22E | 867 25 34 15 23 43 28 --- 12 | 63 75 65 71 68 72 --- 65
R23E | 3282 18 29 12 18 33 20 --- 9 | 113 123 110 119 113 105 --- 112
R24E | 1392 21 20 21 17 28 30 --- 10 | 56 69 75 59 123 57 --- 63
XR26E | ---- --- --- --- --- --- 10 --- 0 | --- --- --- --- --- 237 --- 236
------+----------------------------------------------+------------------------------------------
RMS | 2031 32 32 17 18 36 22 145 |T 49 46 71 46 84 86 123 52
WRMS | 2031 30 32 15 18 31 22 145 |NE 42 39 42 38 41 33 46 34
MEDI | 1741 28 27 15 16 33 20 138 |MD 54 41 45 40 46 37 58 38
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