[IGSREPORT-20282] Wk 1658 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Nov 3 07:00:38 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1658 (Oct 16, 2011 - Oct 22, 2011)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths 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 2.1658.
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:
igl1658[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1658 in the SP3 format.
igl16587.sum Combination Report for GPS Week 1658.
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 | 162.8 ns
1 | 162.9 ns
2 | 160.8 ns
3 | 158.5 ns
4 | 162.1 ns
5 | 162.8 ns
6 | 164.2 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
----+--------+---------------
4 | GFZ | R12
4 | GRG | R12
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 1.1658, 1a.1658).
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 2.1658.0-6)
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 3.1658.0-6).
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 1658 summary. (Oct 16, 2011 - Oct 22, 2011)
Table 1.1658.a GPS week : 1658 MJD: 55850.0-55856.0
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 259| -1 0 2 25 -72 -39 -.18 29 25 | --- --- --- ---
| 1 1 3 27 22 25 .06 | --- ---
emx 141| 0 -1 -3 -82 10 3 -.25 33 30 | 161914 -426 4671 7737
| 1 2 5 19 60 54 .06 | 1386 1633
esx 141| -1 0 -7 24 -8 0 .38 20 18 | 162773 -617 4738 4932
| 1 1 4 22 26 23 .05 | 1003 2663
gfz 199| 0 -1 -10 30 27 59 -.20 24 22 | 0 -352 4642 7545
| 2 2 4 30 70 31 .05 | 0 2450
grg 131| 0 0 0 17 13 8 .13 51 47 | --- --- --- ---
| 2 2 5 69 27 95 .09 | --- ---
iac n/a| 2 1 13 2 36 -58 -.03 25 25 | 147375 -1078 4720 79304
| 2 1 19 18 20 52 .13 | 41140 1442
mcc n/a| 5 0 44 20 103 550 .12 98 98 | --- --- --- ---
| 4 4 12 75 145 640 .25 | --- ---
Table 1.1658.b GPS week : 1658 MJD: 55850.0-55856.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 9 8 9 8 9 11 10 |
R02 | 9 8 9 8 11 11 11 |
R04 | --- --- --- 0 0 0 40 |
R05 | 10 11 12 9 8 11 7 |
R06 | 9 9 11 10 8 8 12 |
R07 | 11 11 14 11 9 9 11 |
R08 | 10 8 8 11 10 8 9 |
R09 | 10 11 11 11 10 12 16 |
R10 | 11 11 14 9 10 10 10 |
R11 | 21 18 21 21 23 21 24 |
R12 | 9 10 12 23 30 23 18 |
R13 | 11 12 12 15 14 14 12 |
R14 | 11 11 12 13 14 15 13 |
R15 | 12 13 12 13 12 11 15 |
R16 | 11 12 13 12 10 14 17 |
R17 | 13 12 15 12 13 15 17 |
R18 | 10 11 10 9 10 12 13 |
R19 | 12 12 10 11 11 11 18 |
R20 | 20 17 20 18 21 20 19 |
R21 | 9 11 10 13 9 10 15 |
R22 | 11 11 13 12 9 10 17 |
R23 | 12 8 10 12 10 10 11 |
R24 | 8 8 12 11 10 15 14 |
Table 1.1658.c GPS week : 1658 MJD: 55850.0-55856.0
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 1658 0 | 73 37 124 1265 -219 235 83.0 3032 3032 | 162802 0
brd 1658 1 | 49 33 51 669 405 3665 84.4 2128 2128 | 162948 0
brd 1658 2 | -33 105 -46 921 -240 -1955 85.5 2566 2566 | 160807 0
brd 1658 3 | -25 182 16 -377 -1650 -10120 85.6 2172 2172 | 158530 0
brd 1658 4 | -26 106 54 -807 -1430 -7541 85.9 1996 1996 | 162120 0
brd 1658 5 | -64 134 -2 -1149 -1744 -4456 85.9 2168 2168 | 162847 0
brd 1658 6 | 3 -63 69 939 -885 -1297 86.9 2258 2258 | 164168 0
-------------+------------------------------------------------------------+----------------
brd 1658 mean| -3 76 38 208 -823 -3066 85.3 2331 2331 | 162031 0
brd 1658 sdev| 49 81 54 965 828 4695 1.3 355 355 | 1845 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 2.1658.0 GPS week: 1658 Day: 0 MJD: 55850
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 259| -1 0 4 25 -90 7 -.22 28 26 | --- --- --- ---
emx 141| 1 -2 0 -100 -40 47 -.31 35 29 | 162050 550 4016 8112
esx 141| 0 0 -6 23 -48 30 .41 16 16 | 162487 280 4006 4173
gfz 199| 1 0 -10 36 100 50 -.20 22 18 | 0 751 4020 8090
grg 131| -4 -2 1 -39 -5 -128 .27 52 49 | --- --- --- ---
iac n/a| 0 1 12 -8 35 -122 -.16 22 22 | 163146 1269 4001 8765
mcc n/a| 12 -7 27 104 96 1281 -.15 119 119 | --- --- --- ---
Table 2.1658.1 GPS week: 1658 Day: 1 MJD: 55851
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 259| -1 1 4 48 -108 -28 -.28 27 23 | --- --- --- ---
emx 141| 0 1 -5 -97 -45 83 -.24 31 30 | 163040 -199 4927 8392
esx 141| 0 0 -10 0 -30 -8 .40 16 15 | 162954 -641 4909 5101
gfz 199| -2 -3 -13 43 132 107 -.20 23 23 | 0 239 4642 7648
grg 131| 2 2 -4 78 -15 -55 .21 46 41 | --- --- --- ---
iac n/a| 0 0 21 5 31 -125 -.12 21 21 | 163274 -153 4922 8445
mcc n/a| 0 0 47 120 395 1410 .23 144 144 | --- --- --- ---
Table 2.1658.2 GPS week: 1658 Day: 2 MJD: 55852
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 259| -2 -1 -3 32 -48 -28 -.14 29 28 | --- --- --- ---
emx 141| -1 0 -8 -71 -37 35 -.21 32 31 | 161539 -2169 5650 8979
esx 141| -4 -1 -10 29 -22 -1 .38 22 21 | 161241 -1459 5648 5816
gfz 199| 0 0 -15 57 50 11 -.20 25 19 | 0 -2164 5620 8805
grg 131| 0 0 -4 -31 41 46 .15 45 41 | --- --- --- ---
iac n/a| 1 0 32 6 43 -37 -.07 23 23 | 162794 -650 5619 9161
mcc n/a| 7 -2 48 10 48 -90 -.30 95 95 | --- --- --- ---
Table 2.1658.3 GPS week: 1658 Day: 3 MJD: 55853
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 259| -2 -1 0 38 -45 -53 -.12 31 27 | --- --- --- ---
emx 141| 0 -2 -4 -59 17 -7 -.21 31 27 | 159307 -2544 6093 8527
esx 141| -1 0 -5 53 11 -36 .42 20 17 | 162975 -6081 6093 6357
gfz 199| 0 0 -13 -31 12 59 -.12 21 16 | 0 -4232 6100 8425
grg 131| 2 0 2 18 -11 -66 .09 53 46 | --- --- --- ---
iac n/a| 3 0 20 -9 33 21 -.16 29 29 | 159197 -2520 6095 9229
mcc n/a| 3 5 38 -26 -3 -136 .31 77 77 | --- --- --- ---
Table 2.1658.4 GPS week: 1658 Day: 4 MJD: 55854
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 259| 0 -1 2 -22 -61 -51 -.20 30 25 | --- --- --- ---
emx 141| -1 2 -2 -107 57 -66 -.32 34 27 | 161265 1729 4578 7185
esx 141| -2 0 -10 36 16 25 .37 20 18 | 163690 339 4519 4723
gfz 199| 0 0 -10 13 -47 90 -.19 21 17 | 0 3274 4673 7048
grg 131| -4 -3 0 141 26 24 .02 54 54 | --- --- --- ---
iac n/a| 3 2 19 -5 16 -32 .09 21 21 | 164009 -690 4676 7446
mcc n/a| 0 3 36 -24 -25 97 .12 80 80 | --- --- --- ---
Table 2.1658.5 GPS week: 1658 Day: 5 MJD: 55855
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 259| -1 0 0 0 -74 -65 -.19 30 24 | --- --- --- ---
emx 141| 0 -4 -11 -77 116 -23 -.16 36 37 | 163289 -1340 3619 5082
esx 141| -4 1 -8 36 -1 -19 .28 21 19 | 161900 1248 3783 3976
gfz 199| 0 -4 -9 47 -47 42 -.29 24 26 | 0 -1373 3615 5005
grg 131| 0 0 0 -2 54 136 .05 54 53 | --- --- --- ---
iac n/a| 2 3 15 -13 18 -41 .16 20 20 | 54168 -2719 3784 503944
mcc n/a| 7 0 46 -89 33 438 .27 89 89 | --- --- --- ---
Table 2.1658.6 GPS week: 1658 Day: 6 MJD: 55856
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 259| 0 3 8 52 -82 -57 -.13 29 23 | --- --- --- ---
emx 141| 1 -3 3 -64 6 -49 -.30 33 31 | 162910 987 3815 7887
esx 141| 0 0 1 -10 19 10 .37 23 18 | 164165 1992 4210 4378
gfz 199| -4 -4 -1 44 -8 54 -.23 29 33 | 0 1038 3825 7797
grg 131| 0 4 10 -40 1 100 .12 50 44 | --- --- --- ---
iac n/a| 6 3 -27 39 77 -69 .06 37 37 | 165039 -2088 3943 8141
mcc n/a| 8 3 66 50 182 852 .35 85 85 | --- --- --- ---
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 3.1658.0 GPS week: 1658 Day: 0 MJD: 55850
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 | 686 17 20 14 11 40 26 --- 9 | 32 40 38 31 29 35 --- 30
R02 | 1360 15 27 16 12 47 18 --- 9 | 35 38 35 31 35 35 --- 29
R05 | 860 28 25 15 19 43 18 63 10 | 35 18 23 30 38 19 27 16
R06 | 1964 27 13 12 17 26 24 --- 8 | 30 23 17 30 29 25 --- 16
R07 |10724 26 29 15 31 35 12 --- 10 | 29 31 25 30 27 27 --- 20
R08 | 927 27 27 9 20 50 10 94 9 | 37 34 25 28 32 31 44 23
R09E | 2032 22 30 20 18 34 18 --- 9 | 45 39 52 51 50 54 --- 46
R10E | 2190 20 26 26 20 28 24 --- 10 | 41 37 35 34 52 49 --- 36
R11E | 2931 61 77 24 40 46 42 131 21 | 48 62 61 67 67 47 64 48
R12E | 2037 17 21 14 20 39 21 --- 9 | 44 31 39 42 90 44 --- 41
R13E | 2556 25 29 13 16 51 28 --- 11 | 32 38 37 40 48 34 --- 32
R14E | 3589 22 31 9 21 45 25 --- 10 | 32 52 36 44 43 39 --- 34
R15E | 1255 22 27 24 29 44 25 63 12 | 41 43 41 34 47 47 50 35
R16E | 988 28 26 15 19 57 19 --- 10 | 37 43 44 46 61 51 --- 41
R17 | 1598 32 32 19 32 52 17 --- 12 | 30 28 25 42 40 32 --- 23
R18 | 2139 26 16 19 24 53 13 191 10 | 63 62 54 63 54 39 101 51
R19 | 1469 27 23 10 19 88 14 --- 12 | 63 54 53 55 33 38 --- 47
R20 | 4400 43 97 18 26 66 34 --- 20 | 61 63 63 57 64 43 --- 52
R21 | 1269 18 11 9 20 52 17 --- 8 | 81 66 72 79 49 52 --- 67
R22 | 2129 14 19 18 17 82 15 --- 11 | 88 84 90 90 57 60 --- 79
R23 | 772 32 36 13 21 66 20 --- 12 | 64 59 49 57 47 42 --- 48
R24 | 608 17 17 9 14 47 9 --- 7 | 56 51 50 51 34 36 --- 43
------+----------------------------------------------+------------------------------------------
RMS | 3031 28 35 16 22 52 22 119 |T 46 45 43 46 46 39 57 38
WRMS | 3031 26 29 16 18 49 22 119 |NE 50 46 44 48 40 36 57 38
MEDI | 1598 25 26 15 20 47 18 94 |MD 41 40 39 42 47 39 50 36
Table 3.1658.1 GPS week: 1658 Day: 1 MJD: 55851
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 | 878 10 13 12 16 33 21 --- 7 | 29 23 27 31 32 33 --- 24
R02 | 1052 14 29 12 12 31 17 --- 8 | 31 43 22 25 21 34 --- 24
R05 | 900 39 17 19 27 38 15 118 11 | 33 18 22 27 29 17 23 12
R06 | 1169 20 21 11 24 36 18 --- 9 | 31 14 22 32 36 22 --- 18
XR07 | 9788 20 25 17 --- 30 22 --- 10 | 28 22 23 --- 30 25 --- 16
R08 | 649 18 15 14 26 25 14 87 8 | 23 21 25 35 31 33 60 23
R09E | 1826 23 26 13 29 41 20 --- 10 | 29 27 39 40 51 39 --- 32
R10E | 2174 26 31 19 21 42 24 --- 11 | 35 22 30 32 43 35 --- 25
R11E | 3449 48 57 30 32 45 32 157 17 | 52 45 70 65 51 45 90 50
R12E | 1105 23 27 15 18 37 18 --- 9 | 35 31 41 45 79 34 --- 38
R13E | 3700 40 33 13 22 37 24 --- 12 | 39 36 43 49 48 34 --- 35
R14E | 3514 21 28 16 18 59 20 --- 11 | 26 40 35 40 49 35 --- 31
R15E | 3474 33 26 22 32 53 20 152 12 | 30 37 36 39 36 30 93 26
R16E | 1156 25 27 20 22 63 20 --- 12 | 33 37 45 36 57 30 --- 30
R17 | 1674 30 22 18 23 42 29 --- 11 | 37 28 30 32 37 42 --- 21
R18 | 3468 22 14 17 24 60 18 186 10 | 44 44 52 37 51 20 154 37
R19 | 1674 32 23 11 14 78 16 --- 12 | 45 42 38 45 81 19 --- 34
R20 | 2423 43 84 13 19 29 21 --- 17 | 41 52 53 53 48 39 --- 45
R21 | 735 17 25 13 34 49 22 --- 11 | 53 45 64 70 33 31 --- 49
R22 | 1112 16 25 13 23 48 31 --- 11 | 54 65 47 58 50 27 --- 44
R23 | 2034 11 12 15 16 34 19 --- 7 | 45 45 55 54 35 43 --- 45
R24 | 723 24 14 10 16 39 14 --- 8 | 37 28 27 27 30 29 --- 23
------+----------------------------------------------+------------------------------------------
RMS | 2127 27 31 16 23 46 21 144 |T 36 34 38 41 43 31 84 31
WRMS | 2127 23 30 15 23 41 21 144 |NE 37 35 36 40 38 29 79 29
MEDI | 1674 23 25 14 22 39 20 152 |MD 35 36 36 39 37 33 90 30
Table 3.1658.2 GPS week: 1658 Day: 2 MJD: 55852
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 | 1334 19 17 17 20 23 24 --- 9 | 23 18 29 23 32 34 --- 18
R02 | 1284 26 16 10 15 42 20 --- 9 | 29 22 27 23 31 22 --- 17
R05 | 1103 35 15 26 27 32 24 100 12 | 27 15 28 35 36 19 36 13
R06 | 3219 36 17 20 20 29 25 --- 11 | 29 22 25 18 31 21 --- 11
R07 | 6899 12 30 25 44 43 27 --- 14 | 20 26 30 53 45 34 --- 20
R08 | 758 17 17 13 13 21 21 20 7 | 22 21 30 33 29 28 69 21
R09E | 1191 20 28 22 23 43 20 --- 11 | 34 39 45 45 39 42 --- 36
R10E | 2256 22 26 22 21 73 25 --- 13 | 38 31 37 36 68 40 --- 32
R11E | 1398 60 65 39 33 48 28 99 20 | 39 45 56 58 61 39 71 39
R12E | 2651 31 31 16 18 39 25 --- 11 | 43 37 41 45 86 49 --- 42
R13E | 2193 30 29 16 24 42 20 --- 11 | 40 44 58 54 57 43 --- 45
R14E | 5171 22 21 15 27 51 23 --- 11 | 41 45 41 51 56 46 --- 41
R15E | 3910 27 29 18 21 42 23 85 11 | 39 39 35 28 35 47 74 31
R16E | 999 21 17 18 23 63 30 --- 12 | 32 35 36 44 37 41 --- 33
R17 | 2128 33 49 28 37 30 20 --- 15 | 26 31 41 52 26 29 --- 28
R18 | 2207 15 16 13 18 40 28 133 9 | 50 56 55 47 63 21 172 44
R19 | 1369 12 20 12 21 51 22 --- 10 | 51 52 48 53 64 37 --- 45
R20 | 1710 50 79 36 30 37 24 --- 20 | 54 84 23 34 46 29 --- 28
R21 | 864 25 13 19 21 47 16 --- 10 | 63 48 50 53 43 38 --- 46
R22 | 991 21 23 20 24 73 22 --- 13 | 65 57 72 68 51 44 --- 56
R23 | 1181 18 11 28 19 32 22 --- 10 | 55 47 37 56 39 44 --- 43
R24 | 1015 34 33 23 17 39 22 --- 12 | 52 43 38 43 21 30 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 2566 29 32 22 25 45 23 95 |T 39 38 40 43 45 35 84 32
WRMS | 2566 28 31 21 19 41 23 95 |NE 40 38 38 42 39 30 92 30
MEDI | 1369 22 21 19 21 42 23 99 |MD 39 39 37 45 39 37 71 32
Table 3.1658.3 GPS week: 1658 Day: 3 MJD: 55853
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 | 1179 14 18 9 9 30 29 --- 8 | 29 26 36 29 29 35 --- 26
R02 | 1002 24 15 10 9 33 16 --- 7 | 27 20 29 22 44 22 --- 20
XR04 | ---- 5 --- --- --- --- --- --- 0 | 70 --- --- --- --- --- --- 71
R05 | 1006 29 17 14 15 26 18 67 8 | 30 25 19 24 25 30 28 17
R06 | 2984 41 19 11 15 36 19 --- 10 | 32 26 16 22 31 24 --- 11
R07 | 4551 29 15 24 16 40 20 --- 10 | 29 24 37 27 33 24 --- 18
R08 | 2145 16 18 23 17 37 38 40 11 | 19 18 36 24 30 29 51 16
R09E | 1087 25 23 12 20 48 29 --- 10 | 42 44 48 52 73 55 --- 46
R10E | 1335 22 28 11 15 39 17 --- 9 | 37 40 38 40 56 42 --- 35
R11E | 1357 64 57 32 43 53 38 89 21 | 37 52 57 61 72 39 44 41
R12E | 1981 43 36 46 26 124 46 --- 22 | 81 38 96 104 227 53 --- 77
R13E | 2195 30 41 28 21 58 40 --- 15 | 61 50 70 72 89 47 --- 58
R14E | 4637 33 31 21 23 53 28 --- 13 | 38 42 38 41 43 44 --- 34
R15E | 2597 28 37 18 27 54 26 74 13 | 39 36 33 41 51 47 52 31
R16E | 1474 25 26 17 21 38 38 --- 11 | 31 36 31 33 43 43 --- 26
R17 | 2177 50 24 17 22 25 14 --- 11 | 29 40 39 37 39 35 --- 31
R18 | 1941 31 19 13 13 35 16 102 9 | 51 51 34 38 42 36 108 37
R19 | 1560 19 20 20 21 47 23 --- 10 | 58 55 32 50 35 50 --- 43
R20 | 2872 28 70 15 17 62 50 --- 18 | 55 65 50 40 33 32 --- 42
R21 | 950 26 11 15 36 57 23 --- 12 | 66 57 48 69 34 53 --- 51
R22 | 786 14 14 10 11 81 26 --- 11 | 61 55 54 63 53 59 --- 54
R23 | 888 11 33 22 19 57 26 --- 12 | 56 37 68 62 49 50 --- 52
R24 | 831 34 30 9 20 47 16 --- 11 | 71 32 42 57 29 44 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 2172 31 31 20 21 53 29 77 |T 45 39 43 45 52 40 56 38
WRMS | 2172 27 27 17 16 46 29 77 |NE 45 37 38 40 36 37 62 35
MEDI | 1474 28 23 15 19 47 26 74 |MD 39 38 38 40 42 42 51 37
Table 3.1658.4 GPS week: 1658 Day: 4 MJD: 55854
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 | 1533 18 23 16 16 40 22 --- 9 | 35 29 36 33 42 42 --- 29
R02 | 973 28 17 15 13 73 15 --- 10 | 26 26 26 25 49 28 --- 21
XR04 | ---- 6 --- --- --- --- --- --- 0 | 61 --- --- --- --- --- --- 63
R05 | 818 18 19 9 13 53 14 41 8 | 24 24 23 31 49 26 21 21
R06 | 1564 25 15 11 13 43 10 --- 7 | 21 25 25 25 39 25 --- 19
R07 | 2496 21 20 22 14 42 17 --- 9 | 24 30 28 29 39 24 --- 18
R08 | 2636 22 20 20 16 42 20 29 9 | 24 30 27 23 41 25 29 16
R09E | 1837 24 28 17 19 34 23 --- 10 | 55 44 59 61 77 62 --- 54
R10E | 1243 15 26 15 20 52 17 --- 9 | 31 29 39 32 57 38 --- 30
R11E | 1054 66 70 40 47 66 26 71 22 | 26 37 63 58 78 42 30 37
XR12E |13185 31 --- --- 348 855 28 --- 29 | 58 --- --- 209 338 66 --- 67
R13E | 1458 30 30 28 21 75 20 --- 13 | 35 39 48 38 65 31 --- 32
R14E | 1759 36 33 35 17 51 29 --- 14 | 55 58 67 56 69 35 --- 49
R15E | 3139 27 34 14 18 72 23 88 12 | 41 39 37 40 53 40 35 33
R16E | 1803 26 24 13 24 44 19 --- 10 | 29 26 30 36 50 36 --- 26
R17 | 1677 51 22 23 25 46 18 --- 13 | 25 35 48 35 39 42 --- 31
R18 | 1395 20 23 16 20 51 12 130 9 | 46 35 50 43 44 42 54 39
R19 | 2346 37 27 17 22 52 15 --- 11 | 41 38 26 30 48 25 --- 23
R20 | 5092 38 92 16 27 59 48 --- 21 | 52 57 48 42 51 23 --- 38
R21 | 874 14 22 19 10 56 11 --- 8 | 58 54 73 57 40 47 --- 55
R22 | 881 11 23 13 14 58 14 --- 8 | 54 58 58 57 51 50 --- 52
R23 | 1254 16 19 14 23 55 16 --- 9 | 44 36 38 62 56 36 --- 41
R24 | 591 26 20 19 13 51 21 --- 10 | 58 41 59 50 50 23 --- 42
------+----------------------------------------------+------------------------------------------
RMS | 1995 30 34 20 21 54 21 80 |T 40 37 43 48 64 36 33 36
WRMS | 1995 25 27 18 17 54 21 80 |NE 39 37 40 38 45 32 34 33
MEDI | 1533 25 23 16 18 52 18 71 |MD 41 36 39 38 50 36 30 33
Table 3.1658.5 GPS week: 1658 Day: 5 MJD: 55855
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 | 1705 15 35 23 20 33 21 --- 10 | 27 42 36 34 27 40 --- 30
R02 | 838 23 17 10 12 75 16 --- 10 | 26 23 24 18 43 31 --- 18
XR04 | ---- 6 --- --- --- --- --- --- 0 | 54 --- --- --- --- --- --- 58
R05 | 981 24 23 12 22 54 21 36 10 | 16 17 24 25 43 20 18 14
R06 | 1743 15 19 13 16 40 15 --- 8 | 19 17 21 24 38 24 --- 16
R07 | 2478 21 19 15 24 26 13 --- 8 | 19 22 33 36 38 27 --- 23
R08 | 1316 18 19 21 9 31 14 48 8 | 19 25 22 19 34 25 32 17
R09E | 1822 28 35 22 20 50 22 --- 12 | 52 53 61 50 73 44 --- 48
R10E | 1567 19 30 22 20 44 14 --- 10 | 25 24 32 25 36 35 --- 23
R11E | 1422 61 67 33 36 70 38 71 21 | 38 36 61 66 80 38 41 41
XR12E | 2271 41 --- 32 --- --- 23 --- 22 | 33 --- 44 --- --- 43 --- 33
R13E | 1050 29 37 21 24 74 18 --- 13 | 32 29 43 38 58 34 --- 29
R14E | 1395 39 44 37 24 41 19 --- 14 | 33 43 49 38 59 28 --- 32
R15E | 4859 29 30 18 22 31 21 125 10 | 32 33 33 28 39 30 39 25
R16E | 1109 31 39 27 24 56 24 --- 13 | 31 37 47 33 55 35 --- 29
R17 | 1614 52 40 29 26 48 20 --- 15 | 33 15 42 34 53 19 --- 23
R18 | 2065 17 17 17 28 76 20 124 12 | 41 42 49 45 40 35 29 37
R19 | 2433 27 18 17 20 53 21 --- 10 | 39 41 26 35 38 30 --- 25
R20 | 5404 44 87 15 18 94 20 --- 20 | 45 26 30 34 60 24 --- 24
R21 | 1006 21 17 16 20 41 24 --- 10 | 47 46 39 41 43 22 --- 31
R22 | 1074 22 31 17 17 56 10 --- 10 | 52 59 51 41 37 42 --- 42
R23 | 1714 27 29 25 14 32 15 --- 10 | 46 53 25 42 37 25 --- 30
R24 | 646 28 17 11 55 54 22 --- 14 | 59 46 48 49 64 46 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 2168 30 36 21 24 54 20 89 |T 35 34 38 35 47 31 31 30
WRMS | 2168 24 37 19 26 53 20 89 |NE 36 33 33 34 42 29 26 28
MEDI | 1567 27 30 18 20 50 20 71 |MD 33 36 36 35 43 30 32 29
Table 3.1658.6 GPS week: 1658 Day: 6 MJD: 55856
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 | 1082 18 27 14 23 32 21 --- 9 | 34 37 36 41 30 47 --- 34
R02 | 1300 25 18 13 22 36 35 --- 10 | 37 32 34 30 32 41 --- 29
XR04 | 4399 37 --- --- --- --- 43 --- 40 | 65 --- --- --- --- 8 --- 60
R05 | 903 19 11 12 12 26 14 56 6 | 33 16 23 22 42 29 28 21
R06 | 1703 27 15 16 17 43 47 --- 12 | 32 22 25 30 37 37 --- 23
R07 | 2063 17 20 26 22 44 25 --- 11 | 33 28 29 27 39 31 --- 23
R08 | 1004 22 11 14 12 27 27 51 8 | 34 34 37 34 37 37 44 30
R09E | 2299 34 44 17 23 31 56 --- 15 | 54 50 65 64 61 83 --- 59
R10E | 2583 22 19 14 19 27 30 --- 9 | 42 42 36 32 46 57 --- 37
R11E | 1420 44 67 41 52 57 58 51 23 | 39 64 80 82 78 53 45 57
XR12E | 2646 31 --- 20 --- 57 22 --- 17 | 26 --- 41 --- 200 34 --- 33
R13E | 1603 23 30 24 21 44 27 --- 12 | 36 32 49 45 59 42 --- 36
R14E | 2132 25 31 26 21 42 35 --- 13 | 39 47 53 43 51 42 --- 39
R15E | 6010 29 40 31 24 42 41 119 15 | 44 36 54 42 58 48 45 40
R16E | 803 40 38 28 19 60 44 --- 16 | 36 36 43 41 70 56 --- 37
R17 | 4141 51 46 36 25 32 27 --- 17 | 29 33 59 52 31 40 --- 35
R18 | 2654 16 12 13 20 86 21 117 13 | 71 64 78 72 47 68 85 64
R19 | 1292 16 17 19 41 96 54 --- 18 | 62 50 53 63 77 61 --- 51
R20 | 1644 46 63 26 19 58 33 --- 18 | 58 51 44 45 54 44 --- 38
R21 | 1742 29 32 26 47 40 23 --- 14 | 71 64 55 63 45 50 --- 53
R22 | 1965 25 31 10 39 73 52 --- 16 | 76 74 62 71 50 49 --- 58
R23 | 1021 23 21 17 16 32 39 --- 10 | 62 67 47 52 56 29 --- 48
R24 | 907 19 15 19 54 45 25 --- 14 | 63 63 53 72 35 45 --- 54
------+----------------------------------------------+------------------------------------------
RMS | 2257 29 33 23 29 50 37 85 |T 46 44 48 48 56 44 49 41
WRMS | 2257 23 31 18 33 44 37 85 |NE 50 45 45 48 43 41 52 41
MEDI | 1703 25 27 19 22 42 33 56 |MD 39 42 47 45 47 44 45 38
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