[IGSREPORT-21716] Wk 1732 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat Apr 6 16:58:06 PDT 2013
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1732 (Mar 17, 2013 - Mar 23, 2013)
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 2.1732.
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:
igl1732[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1732 in the SP3 format.
igl17327.sum Combination Report for GPS Week 1732.
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
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 | 180.4 ns
1 | 178.5 ns
2 | 183.9 ns
3 | 192.6 ns
4 | 198.2 ns
5 | 202.9 ns
6 | 206.6 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
----+--------+---------------
0 | IAC | R08
1 | IAC | R08
2 | IAC | R08
3 | IAC | R08
4 | IAC | R08
5 | IAC | R08
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 1.1732, 1a.1732).
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 2.1732.0-6)
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 3.1732.0-6).
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 1732 summary. (Mar 17, 2013 - Mar 23, 2013)
Table 1.1732.a GPS week : 1732 MJD: 56368.0-56374.0
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| -2 3 -5 68 -12 -33 -.22 35 36 | --- --- --- ---
| 1 2 2 21 53 32 .06 | --- ---
cof n/a| -2 4 -2 58 18 -26 -.31 38 38 | --- --- --- ---
| 2 1 2 21 42 49 .06 | --- ---
emx n/a| 0 0 -1 -75 -21 -79 -.31 32 32 | 192493 -1344 3803 6691
| 1 1 2 24 40 45 .04 | 11047 2336
esx n/a| 0 -2 3 -49 27 18 .31 21 18 | 188976 -569 3785 6420
| 1 1 1 28 36 17 .03 | 9523 3402
gfz n/a| 0 -2 -2 39 -28 9 -.33 20 17 | 0 -1802 3780 6639
| 0 0 1 44 52 24 .04 | 0 2836
grg n/a| -2 2 0 40 -28 102 .09 39 37 | -190953 -1967 3766 7518
| 3 1 1 24 33 50 .06 | 8607 3338
iac n/a| 2 2 4 7 57 -45 .29 26 26 | 193151 -974 3792 7416
| 1 1 2 20 31 45 .03 | 11584 1867
mcc n/a| 2 -2 26 -1 64 200 .09 127 127 | --- --- --- ---
| 4 4 9 96 57 466 .38 | --- ---
Table 1.1732.b GPS week : 1732 MJD: 56368.0-56374.0
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 13 16 17 17 14 17 |
R02 | 14 13 13 16 14 16 16 |
R03 | 11 12 10 12 11 11 12 |
R04 | 11 12 14 11 9 12 12 |
R05 | 13 16 13 13 8 10 10 |
R06 | 12 9 11 10 12 8 8 |
R07 | 10 14 12 10 13 11 12 |
R08 | 13 16 19 14 15 16 14 |
R09 | 10 10 8 10 9 8 10 |
R10 | 9 10 9 9 10 7 9 |
R11 | 14 18 17 20 18 23 17 |
R12 | 8 9 7 9 8 9 19 |
R13 | 9 10 10 11 9 10 10 |
R14 | 18 18 40 23 17 15 18 |
R15 | 9 11 12 13 10 8 11 |
R16 | 11 11 10 10 10 10 10 |
R17 | 11 10 10 8 7 7 8 |
R18 | 12 12 10 12 15 9 8 |
R19 | 10 12 12 11 9 9 8 |
R20 | 14 15 24 20 13 16 18 |
R21 | 15 16 16 22 19 14 16 |
R22 | 15 11 10 11 13 14 12 |
R23 | 13 9 8 8 8 12 8 |
R24 | 10 10 10 11 9 7 9 |
Table 1.1732.c GPS week : 1732 MJD: 56368.0-56374.0
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 1732 0 | 58 42 22 1068 2138 -21720 85.5 1687 1687 | 180413 0
brd 1732 1 | -23 -146 26 1495 37 -26850 86.3 1945 1945 | 178546 0
brd 1732 2 | 153 -46 53 1043 -2200 -20170 85.1 1804 1804 | 183905 0
brd 1732 3 | -81 50 36 -876 -1363 -25400 84.7 1973 1973 | 192600 0
brd 1732 4 | -106 60 237 -849 -3301 -25850 86.0 1730 1730 | 198234 0
brd 1732 5 | -1 71 121 -1645 761 -17490 88.2 1558 1558 | 202916 0
brd 1732 6 | -44 10 111 -1585 1022 -12840 84.9 1310 1310 | 206582 0
-------------+------------------------------------------------------------+----------------
brd 1732 mean| -6 5 87 -192 -414 -21474 85.8 1715 1715 | 191885 0
brd 1732 sdev| 88 78 77 1348 1940 5093 1.2 229 229 | 11193 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 2.1732.0 GPS week: 1732 Day: 0 MJD: 56368
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 2 -3 70 -85 -41 -.26 34 37 | --- --- --- ---
cof n/a| 0 4 -2 66 -26 -72 -.30 41 41 | --- --- --- ---
emx n/a| 1 0 -2 -52 -43 -6 -.34 31 31 | 179807 832 3885 6484
esx n/a| -1 -2 2 -43 -15 -3 .33 20 18 | 180425 -155 3900 6205
gfz n/a| -1 -1 -3 -11 52 -17 -.28 18 15 | 0 -2169 3892 6390
grg n/a| 1 5 -1 46 -4 96 .15 40 40 | -197505 -652 3916 7096
iac n/a| 2 0 4 36 62 -5 .31 27 27 | 183269 -1770 3883 7230
mcc n/a| 6 -1 36 100 11 340 .35 158 158 | --- --- --- ---
Table 2.1732.1 GPS week: 1732 Day: 1 MJD: 56369
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 -2 90 -48 -70 -.29 33 36 | --- --- --- ---
cof n/a| -1 1 0 63 -24 -71 -.29 35 37 | --- --- --- ---
emx n/a| 0 -1 -1 -42 -65 -67 -.38 31 32 | 181031 -5513 4106 7250
esx n/a| 1 -2 0 -36 38 13 .36 23 21 | 182251 -6771 4090 7364
gfz n/a| 0 -2 -2 -18 4 4 -.35 20 20 | 0 -6482 4090 7226
grg n/a| -1 3 0 84 -52 154 .09 32 31 | -198817 -7637 3954 11620
iac n/a| 0 3 5 6 81 -66 .33 27 27 | 179082 -3542 4110 7817
mcc n/a| 3 2 22 12 96 535 .23 126 126 | --- --- --- ---
Table 2.1732.2 GPS week: 1732 Day: 2 MJD: 56370
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -5 2 -5 63 20 -79 -.19 36 38 | --- --- --- ---
cof n/a| -6 4 -3 39 30 -84 -.39 36 38 | --- --- --- ---
emx n/a| 0 2 0 -77 -45 -72 -.27 33 33 | 184905 -1680 3780 6156
esx n/a| 0 0 2 -92 5 42 .30 20 20 | 180057 -39 3785 5465
gfz n/a| 0 -1 -6 103 -7 28 -.35 20 17 | 0 -2459 3777 6140
grg n/a| 1 2 0 12 -53 84 .07 45 42 | -198756 -2440 3825 6091
iac n/a| 1 0 8 33 63 -60 .25 22 22 | 183706 908 3788 6973
mcc n/a| 4 1 7 45 129 628 .33 115 115 | --- --- --- ---
Table 2.1732.3 GPS week: 1732 Day: 3 MJD: 56371
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 4 -4 30 38 -33 -.10 39 37 | --- --- --- ---
cof n/a| -2 5 0 22 27 16 -.23 41 40 | --- --- --- ---
emx n/a| 2 0 1 -76 45 -47 -.25 37 35 | 193071 -1259 3758 6149
esx n/a| 0 -3 4 -76 75 20 .29 26 21 | 185357 931 3753 5841
gfz n/a| -1 -1 -2 67 -80 -17 -.33 20 16 | 0 -1888 3753 5967
grg n/a| -6 2 0 14 -45 11 .14 44 45 | -194558 -1574 3779 5973
iac n/a| 3 3 2 -18 36 40 .28 26 26 | 192611 1273 3777 6699
mcc n/a| -7 -2 32 -141 75 741 .59 121 121 | --- --- --- ---
Table 2.1732.4 GPS week: 1732 Day: 4 MJD: 56372
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 5 -8 63 43 -8 -.24 36 40 | --- --- --- ---
cof n/a| -3 4 -7 54 86 30 -.30 38 41 | --- --- --- ---
emx n/a| 2 0 0 -116 23 -109 -.30 33 32 | 197584 1432 3680 7540
esx n/a| 0 -3 4 -52 74 2 .33 21 18 | 192213 4612 3581 7367
gfz n/a| -1 -2 -1 67 -94 35 -.28 20 16 | 0 3242 3581 7619
grg n/a| -5 0 4 45 -66 121 -.04 33 33 | -187709 3680 3553 7655
iac n/a| 3 2 2 5 8 -69 .28 26 26 | 199843 500 3576 8521
mcc n/a| -1 0 31 -119 -33 -234 -.20 135 135 | --- --- --- ---
Table 2.1732.5 GPS week: 1732 Day: 5 MJD: 56373
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 4 -6 65 12 9 -.24 35 35 | --- --- --- ---
cof n/a| -4 2 -2 77 51 -19 -.41 37 37 | --- --- --- ---
emx n/a| -2 0 -2 -66 -21 -138 -.29 32 33 | 202678 -456 3710 6839
esx n/a| 0 0 4 -36 12 41 .28 17 14 | 198056 -809 3703 6614
gfz n/a| 0 -2 -1 38 -58 -4 -.39 22 20 | 0 -1641 3697 6870
grg n/a| -3 0 1 40 0 159 .12 34 30 | -180194 -2624 3687 7110
iac n/a| 4 2 1 0 104 -88 .27 27 27 | 205347 -2556 3725 7668
mcc n/a| 3 -10 32 0 64 -340 -.32 117 117 | --- --- --- ---
Table 2.1732.6 GPS week: 1732 Day: 6 MJD: 56374
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 6 -8 96 -66 -11 -.23 34 30 | --- --- --- ---
cof n/a| -1 5 -6 85 -15 18 -.27 38 33 | --- --- --- ---
emx n/a| 0 1 -5 -94 -45 -115 -.29 28 29 | 208380 -2770 3705 6420
esx n/a| -1 -1 5 -6 1 12 .30 18 16 | 204475 -1755 3685 6090
gfz n/a| 0 -3 0 29 -13 38 -.29 19 16 | 0 -1221 3671 6266
grg n/a| -3 1 0 40 22 88 .08 46 36 | -179137 -2526 3650 7085
iac n/a| 2 1 5 -11 43 -68 .31 27 27 | 208202 -1635 3687 7008
mcc n/a| 5 -3 25 94 109 -264 -.37 120 120 | --- --- --- ---
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 3.1732.0 GPS week: 1732 Day: 0 MJD: 56368
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 | 1145 51 47 25 23 12 52 14 --- 13 | 79 79 62 39 44 36 41 --- 43
R02 | 1325 61 79 37 20 21 31 16 --- 14 | 69 81 48 18 27 25 24 --- 25
R03 | 1751 29 45 46 21 11 19 16 --- 11 | 49 57 54 31 34 27 30 --- 34
R04 | 1527 20 21 29 20 12 34 35 --- 11 | 66 67 72 37 53 75 25 --- 48
R05 | 701 38 38 38 23 23 43 22 188 13 | 64 65 74 36 39 54 30 29 41
R06 | 1580 22 21 28 23 18 54 27 --- 12 | 51 54 55 31 35 70 32 --- 37
R07 | 1137 17 34 34 10 20 22 29 287 10 | 62 72 70 50 47 62 38 48 50
XR08 | 1057 25 28 30 23 16 --- 213 --- 13 | 66 67 71 40 48 --- 58 --- 51
R09E | 1687 14 13 17 13 9 42 40 --- 10 | 18 30 28 27 28 38 31 --- 23
R10E | 2221 24 31 17 16 13 39 16 --- 8 | 22 23 26 16 22 26 25 --- 17
R11E | 1769 33 36 38 18 26 49 34 75 14 | 27 46 36 57 68 61 39 36 47
R12E | 1237 18 18 15 14 15 22 25 --- 8 | 55 56 55 46 62 64 49 --- 53
R13E | 1428 16 21 27 7 20 35 21 --- 9 | 67 68 74 69 74 61 69 --- 68
R14E | 4124 29 46 37 34 42 42 48 --- 17 | 39 68 43 70 60 35 31 --- 43
R15E | 1874 25 33 16 11 12 43 20 93 9 | 21 26 25 21 25 27 26 37 18
R16E | 2011 23 37 22 21 18 34 30 --- 10 | 17 31 28 25 16 33 29 --- 18
R17 | 1809 38 51 20 14 15 37 27 104 10 | 81 90 68 55 56 57 51 35 57
R18 | 878 42 47 31 22 19 46 14 79 12 | 66 66 58 34 26 45 33 45 34
R19 | 1312 34 36 23 14 9 42 12 --- 9 | 68 67 59 37 41 42 41 --- 43
R20 | 1038 37 42 46 19 10 48 31 --- 13 | 59 66 72 46 44 22 32 --- 42
R21 | 1629 58 66 37 29 14 37 24 --- 14 | 79 80 66 26 36 41 39 --- 39
R22 | 1054 43 43 37 23 20 51 36 --- 14 | 53 56 49 38 32 43 31 --- 31
R23 | 1025 38 40 32 20 16 40 35 --- 12 | 51 55 52 43 41 56 39 --- 41
R24 | 1395 26 46 29 18 14 34 22 --- 10 | 45 51 49 34 42 42 35 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1686 34 41 31 20 18 40 27 158 |T 53 59 53 38 41 45 36 38 39
WRMS | 1686 37 41 31 18 15 40 27 158 |NE 63 67 61 37 40 46 36 39 40
MEDI | 1395 29 37 29 20 15 40 25 93 |MD 55 65 55 37 41 42 32 36 41
Table 3.1732.1 GPS week: 1732 Day: 1 MJD: 56369
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 | 1571 38 53 31 16 17 26 40 --- 12 | 50 61 47 44 47 42 25 --- 39
R02 | 1571 39 33 33 27 12 33 24 --- 12 | 51 44 49 29 39 42 22 --- 33
R03 | 1240 31 28 37 22 25 27 14 --- 11 | 40 39 48 41 26 28 44 --- 34
R04 | 925 35 44 33 20 14 22 30 --- 11 | 47 52 43 28 36 40 14 --- 29
R05 | 957 55 58 41 30 18 26 37 166 15 | 47 57 50 35 36 29 28 20 28
R06 | 1697 23 31 24 14 16 22 21 --- 9 | 40 43 49 31 37 35 25 --- 32
R07 | 1657 30 26 50 28 19 25 25 176 13 | 47 46 61 37 43 45 37 24 39
XR08 | 1111 25 35 39 21 24 --- 229 --- 15 | 46 55 58 44 41 --- 59 --- 44
R09E | 1626 13 24 12 12 12 42 29 --- 9 | 18 19 22 23 29 48 24 --- 21
R10E | 3826 28 39 14 11 17 31 24 --- 9 | 28 36 23 27 34 24 21 --- 21
R11E | 2312 38 25 38 28 36 67 33 86 18 | 26 52 39 65 64 74 42 28 47
R12E | 2719 15 19 16 11 16 38 17 --- 8 | 19 24 27 33 33 36 31 --- 25
R13E | 1007 18 14 22 14 11 44 22 --- 10 | 61 66 60 71 76 74 62 --- 65
R14E | 2210 30 31 35 44 34 42 46 --- 17 | 43 53 40 57 80 66 40 --- 49
R15E | 1454 15 26 27 13 27 28 22 69 10 | 19 35 32 20 39 31 27 33 19
R16E | 3891 33 39 26 21 16 24 25 --- 10 | 20 27 20 33 24 32 26 --- 18
R17 | 2304 25 31 25 26 14 20 23 99 9 | 46 50 49 46 40 37 25 28 38
R18 | 652 45 47 33 23 19 28 16 122 12 | 37 40 29 27 19 17 18 35 16
R19 | 977 32 34 28 26 16 34 18 --- 11 | 40 44 41 22 19 42 23 --- 21
R20 | 958 39 33 45 21 27 28 38 --- 14 | 47 47 63 27 48 50 39 --- 38
R21 | 2259 58 53 45 36 20 36 21 --- 16 | 51 53 46 41 40 26 27 --- 32
R22 | 990 34 32 29 20 13 22 23 --- 10 | 30 40 42 41 37 42 30 --- 33
R23 | 1831 22 24 22 17 17 21 22 --- 9 | 35 38 37 42 26 40 38 --- 33
R24 | 1687 29 27 19 20 19 19 23 --- 9 | 36 31 31 25 34 30 18 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1944 33 35 31 23 20 32 27 126 |T 38 43 41 37 39 40 31 28 32
WRMS | 1944 36 37 32 21 20 31 27 126 |NE 43 46 46 35 35 36 29 26 32
MEDI | 1571 30 31 29 21 17 28 23 99 |MD 40 44 42 33 37 40 27 28 32
Table 3.1732.2 GPS week: 1732 Day: 2 MJD: 56370
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 | 1508 54 44 41 33 31 27 21 --- 15 | 54 51 59 44 27 19 24 --- 29
R02 | 1060 37 48 38 19 18 36 33 --- 13 | 49 58 53 36 44 35 16 --- 31
R03 | 1284 32 35 27 16 13 32 13 --- 9 | 38 46 41 34 31 36 30 --- 30
R04 | 871 37 34 33 25 15 63 13 --- 13 | 47 44 40 21 28 38 26 --- 23
R05 | 1049 50 47 40 22 23 25 16 150 13 | 44 45 37 31 34 33 19 25 22
R06 | 1244 32 36 24 10 16 37 31 --- 11 | 45 53 45 42 40 49 24 --- 35
R07 | 1581 29 22 40 22 28 29 16 83 12 | 37 38 51 42 45 28 31 34 34
XR08 | 1090 42 25 43 27 20 --- 240 --- 18 | 54 43 54 58 44 --- 42 --- 47
R09E | 1560 21 30 20 10 16 26 21 --- 8 | 20 31 29 27 37 33 28 --- 23
R10E | 3202 25 35 20 14 12 18 25 --- 8 | 25 33 28 38 29 37 24 --- 26
R11E | 3049 41 29 52 22 29 68 32 102 17 | 28 47 44 59 65 71 32 37 43
R12E | 2759 20 18 14 12 11 18 18 --- 7 | 32 28 31 34 32 35 30 --- 28
R13E | 1313 25 30 19 11 19 42 24 --- 10 | 80 81 75 63 70 81 71 --- 69
XR14E | 2466 59 58 --- 50 105 62 87 --- 39 | 72 117 --- 122 183 96 65 --- 103
R15E | 1026 26 22 25 22 19 37 28 74 11 | 25 42 30 41 44 31 25 46 24
R16E | 1976 27 32 28 13 12 37 24 --- 10 | 22 32 22 27 24 41 31 --- 20
R17 | 2509 30 34 23 24 18 23 22 72 10 | 62 63 68 50 42 61 53 29 51
R18 | 1183 34 37 33 18 14 24 14 170 10 | 56 58 56 35 32 44 32 35 37
R19 | 1150 42 40 34 13 23 35 21 --- 12 | 54 51 48 33 38 43 32 --- 34
R20 | 713 51 54 67 27 24 134 19 --- 24 | 53 56 60 29 27 114 31 --- 25
R21 | 1999 57 58 42 34 21 38 18 --- 15 | 55 60 53 36 36 31 33 --- 31
R22 | 980 32 29 27 16 17 26 22 --- 10 | 42 43 43 42 20 31 28 --- 29
R23 | 1720 15 19 15 12 17 33 13 --- 7 | 37 43 41 46 30 62 36 --- 37
R24 | 2626 23 36 15 24 19 32 14 --- 9 | 46 55 45 24 31 53 43 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1803 36 36 33 20 20 45 22 115 |T 44 50 45 42 43 47 33 34 36
WRMS | 1803 38 38 33 20 17 42 22 115 |NE 48 50 49 37 34 45 31 30 33
MEDI | 1313 32 34 28 19 18 33 21 83 |MD 45 46 45 36 34 38 31 34 31
Table 3.1732.3 GPS week: 1732 Day: 3 MJD: 56371
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 | 1130 55 65 60 37 16 43 21 --- 17 | 59 66 57 46 31 22 22 --- 24
R02 | 1623 52 54 54 23 22 44 22 --- 15 | 57 57 56 26 25 30 13 --- 21
R03 | 1186 36 32 38 12 21 31 29 --- 12 | 44 41 49 34 41 36 30 --- 32
R04 | 1194 35 37 32 13 12 41 22 --- 11 | 53 53 48 23 29 41 20 --- 27
R05 | 1878 42 45 32 30 27 34 19 129 13 | 49 50 42 21 27 46 44 44 26
R06 | 2066 37 34 28 17 17 27 14 --- 10 | 44 41 38 29 29 39 26 --- 26
R07 | 1408 35 33 33 21 9 27 16 74 10 | 51 52 54 43 49 59 39 64 44
XR08 | 1162 34 55 36 17 17 --- 231 --- 14 | 55 67 58 40 47 --- 52 --- 45
R09E | 1971 21 25 20 17 20 28 25 --- 9 | 15 24 26 28 35 44 30 --- 22
R10E | 2749 29 39 20 16 13 22 25 --- 9 | 28 43 31 26 29 27 33 --- 23
R11E | 3477 41 36 50 33 38 75 38 121 20 | 31 46 38 64 81 74 38 59 47
R12E | 3283 24 28 20 12 13 33 16 --- 8 | 31 34 22 23 26 36 27 --- 20
R13E | 1567 21 14 21 14 18 30 37 --- 11 | 94 98 96 100 101 101 78 --- 92
R14E | 2893 47 34 68 51 34 73 47 --- 23 | 45 90 113 108 77 76 49 --- 69
R15E | 1557 30 29 24 20 26 37 35 74 12 | 30 38 22 27 47 41 28 68 22
R16E | 1381 22 27 28 18 16 26 23 --- 9 | 15 23 32 21 28 38 29 --- 17
R17 | 2317 23 23 17 13 9 32 11 76 7 | 63 63 64 50 52 50 57 49 53
R18 | 1588 42 54 45 24 16 20 18 200 12 | 58 68 63 31 32 33 26 102 33
R19 | 1672 29 36 26 24 8 55 9 --- 11 | 54 62 54 39 35 42 33 --- 34
R20 | 891 48 51 53 18 24 96 36 --- 20 | 55 61 79 34 37 108 16 --- 31
R21 | 1463 81 83 46 63 30 46 26 --- 21 | 72 74 52 69 51 36 17 --- 32
R22 | 1199 42 50 29 12 16 31 21 --- 11 | 55 60 49 33 29 29 28 --- 30
R23 | 1202 20 21 22 11 13 29 20 --- 8 | 40 37 43 39 29 38 37 --- 32
R24 | 2649 28 29 24 25 9 27 28 --- 10 | 44 49 43 44 37 47 34 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 1973 39 41 37 26 20 43 26 121 |T 47 54 51 41 41 47 33 64 34
WRMS | 1973 37 40 35 21 16 45 26 121 |NE 53 56 53 37 36 43 30 64 32
MEDI | 1567 35 34 29 18 16 32 22 76 |MD 49 52 49 34 35 41 30 59 31
Table 3.1732.4 GPS week: 1732 Day: 4 MJD: 56372
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 | 1926 67 72 45 31 18 32 41 --- 17 | 53 60 44 51 43 35 32 --- 33
R02 | 2294 51 47 47 20 21 27 28 --- 14 | 53 48 49 24 28 13 14 --- 22
R03 | 959 30 36 40 20 12 25 25 --- 11 | 41 52 51 37 38 32 29 --- 32
R04 | 1287 24 32 26 10 15 21 24 --- 9 | 43 52 49 32 35 26 22 --- 31
R05 | 2938 33 36 15 17 11 23 11 54 8 | 48 51 36 34 39 49 31 69 35
R06 | 1238 27 33 31 17 18 46 23 --- 12 | 42 49 48 23 29 44 42 --- 27
R07 | 1733 43 42 48 23 22 19 21 143 13 | 44 47 51 20 28 26 28 98 22
XR08 | 1241 36 37 31 19 21 --- 251 --- 15 | 52 56 47 31 24 --- 78 --- 32
R09E | 2601 17 14 15 17 19 32 23 --- 9 | 13 23 17 29 31 38 29 --- 19
R10E | 1341 18 35 17 16 15 47 18 --- 10 | 31 40 34 46 37 36 36 --- 33
R11E | 2915 47 33 44 32 43 53 28 201 18 | 26 55 33 67 80 72 35 64 46
R12E | 1257 18 31 25 12 12 27 16 --- 8 | 16 29 26 20 21 30 26 --- 18
R13E | 1701 23 29 24 13 16 33 17 --- 9 | 123 122 128 127 129 134 127 --- 126
R14E | 2276 25 31 33 41 30 52 36 --- 16 | 52 56 33 73 57 67 58 --- 51
R15E | 1067 26 35 24 13 15 26 34 187 10 | 36 54 34 33 43 45 30 105 31
R16E | 1393 16 23 15 17 16 38 31 --- 10 | 35 45 28 34 41 55 24 --- 29
R17 | 1778 16 24 19 8 10 24 11 77 6 | 56 62 58 54 52 41 48 36 50
R18 | 1580 43 42 44 19 29 39 23 64 14 | 50 49 55 34 19 23 29 98 23
R19 | 1492 26 24 18 14 18 23 19 --- 8 | 46 40 42 34 37 42 48 --- 38
R20 | 1442 40 44 46 11 12 16 35 --- 12 | 44 42 64 36 31 57 14 --- 33
R21 | 683 71 66 43 37 36 35 31 --- 18 | 73 68 55 28 41 48 21 --- 30
R22 | 1068 47 49 42 29 9 24 22 --- 13 | 49 51 51 35 26 23 18 --- 25
R23 | 772 15 19 17 13 16 24 22 --- 8 | 28 33 36 39 40 29 36 --- 32
R24 | 1452 23 20 22 21 10 26 22 --- 9 | 43 40 39 31 34 37 19 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1729 36 38 33 21 20 33 26 135 |T 45 51 46 40 40 43 36 78 35
WRMS | 1729 40 41 32 18 16 33 26 135 |NE 47 50 48 33 34 35 31 75 30
MEDI | 1442 26 33 26 17 16 27 23 77 |MD 44 49 44 34 37 38 29 69 31
Table 3.1732.5 GPS week: 1732 Day: 5 MJD: 56373
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 | 3241 60 60 34 21 17 34 30 --- 14 | 46 57 38 45 48 42 26 --- 34
R02 | 2297 55 62 49 23 28 43 26 --- 16 | 47 54 48 26 41 22 21 --- 24
R03 | 957 37 32 26 18 15 27 25 --- 10 | 30 29 31 23 27 29 27 --- 21
R04 | 1506 37 36 33 10 17 48 23 --- 12 | 38 36 34 20 23 40 28 --- 19
R05 | 2034 36 37 17 9 21 23 25 64 9 | 38 40 29 26 40 25 24 29 26
R06 | 939 21 19 22 10 17 25 18 --- 8 | 30 28 32 24 27 30 35 --- 24
R07 | 1871 38 49 25 16 23 19 25 115 10 | 42 51 35 30 25 35 45 38 29
XR08 | 1439 43 47 31 17 23 --- 255 --- 15 | 41 42 33 27 28 --- 122 --- 25
R09E | 1665 18 19 16 11 15 27 20 --- 7 | 15 34 21 30 31 44 25 --- 23
R10E | 1063 12 20 20 11 12 19 18 --- 6 | 23 33 17 25 25 33 25 --- 19
R11E | 1223 55 36 63 41 50 69 43 205 23 | 34 67 56 93 101 72 34 39 61
R12E | 1148 18 19 22 18 13 24 23 --- 8 | 23 27 20 39 33 48 25 --- 27
R13E | 1131 16 27 24 9 19 38 31 --- 10 | 142 147 141 142 144 154 130 --- 140
R14E | 2256 31 37 32 25 38 44 33 --- 15 | 56 60 27 56 75 77 51 --- 54
R15E | 1009 18 12 24 17 14 17 22 114 8 | 25 26 38 28 30 41 33 54 27
R16E | 1296 24 24 23 14 23 31 21 --- 9 | 28 36 29 32 25 41 27 --- 23
R17 | 1259 24 27 18 8 14 25 14 76 7 | 49 50 47 48 42 35 49 34 43
R18 | 999 29 29 19 12 14 24 24 67 8 | 43 42 37 36 29 29 32 32 32
R19 | 1471 19 26 19 8 14 39 13 --- 8 | 45 53 45 46 37 52 39 --- 41
R20 | 710 43 47 66 14 19 51 20 --- 16 | 42 48 55 24 26 38 21 --- 21
R21 | 1633 48 60 36 14 25 28 37 --- 13 | 64 73 62 53 56 35 26 --- 46
R22 | 1094 47 45 36 20 18 24 45 --- 14 | 48 49 42 32 24 31 22 --- 23
R23 | 1045 31 31 25 21 20 24 36 --- 11 | 36 35 35 34 34 19 50 --- 30
R24 | 1523 17 25 19 13 10 17 15 --- 6 | 30 40 38 27 28 26 26 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1557 35 37 32 17 22 34 27 117 |T 42 48 41 40 41 43 39 37 34
WRMS | 1557 35 37 33 14 20 30 27 117 |NE 41 45 40 32 33 32 37 33 29
MEDI | 1259 31 31 24 14 17 27 24 76 |MD 38 42 35 30 30 35 27 34 26
Table 3.1732.6 GPS week: 1732 Day: 6 MJD: 56374
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 | 1126 65 76 50 31 26 41 21 --- 17 | 66 70 45 39 37 43 21 --- 29
R02 | 1961 48 61 34 26 29 43 40 --- 15 | 67 81 58 30 47 24 22 --- 30
R03 | 1086 29 32 35 12 28 21 25 --- 11 | 53 57 61 39 39 31 35 --- 38
R04 | 1408 34 42 37 21 17 24 22 --- 11 | 59 63 60 38 41 24 28 --- 37
R05 | 806 34 30 19 16 19 28 16 87 9 | 59 59 51 33 34 38 32 40 36
R06 | 869 15 21 10 8 18 27 26 --- 7 | 55 54 53 38 45 53 38 --- 42
R07 | 1659 34 28 29 17 14 54 15 82 11 | 60 63 59 37 43 65 45 55 44
XR08 | 1139 37 36 35 20 25 --- 23 --- 13 | 64 65 65 37 33 --- 109 --- 41
R09E | 1653 17 23 19 17 18 39 27 --- 9 | 17 23 23 30 30 45 38 --- 24
R10E | 1447 18 32 18 8 22 41 22 --- 9 | 20 23 19 17 36 31 18 --- 16
R11E | 1432 42 48 44 24 27 67 29 200 16 | 22 46 29 61 70 70 28 29 45
R12E | 1489 17 18 20 15 14 127 30 --- 18 | 18 21 27 26 25 114 25 --- 21
R13E | 1591 26 29 18 18 15 39 28 --- 10 | 122 108 119 130 116 126 128 --- 122
XR14E | 2248 45 46 --- 31 34 49 31 --- 18 | 76 87 --- 103 77 97 71 --- 82
R15E | 1182 26 34 22 22 15 38 27 112 10 | 19 37 29 30 36 34 21 48 24
R16E | 878 23 27 14 17 15 32 29 --- 9 | 18 26 23 25 29 47 36 --- 23
R17 | 905 18 19 21 13 15 18 21 74 7 | 67 70 63 51 57 49 45 34 54
R18 | 517 22 22 15 10 16 28 22 117 8 | 59 57 54 46 32 40 39 31 41
R19 | 1448 19 21 21 7 14 22 20 --- 7 | 64 63 59 53 50 61 43 --- 52
R20 | 971 57 54 41 27 22 65 39 --- 17 | 56 59 62 30 29 48 24 --- 26
R21 | 1408 55 55 36 26 26 31 39 --- 15 | 92 94 79 45 40 63 31 --- 48
R22 | 973 36 46 33 11 18 38 31 --- 11 | 61 65 55 43 50 37 27 --- 41
R23 | 1452 19 24 15 13 13 29 22 --- 8 | 47 51 50 35 36 40 39 --- 38
R24 | 1525 24 22 25 10 12 15 26 --- 8 | 42 38 43 26 32 35 25 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1309 34 38 28 18 19 46 27 120 |T 53 57 51 43 44 52 40 39 41
WRMS | 1309 30 33 29 16 16 36 27 120 |NE 60 63 57 38 40 43 37 40 39
MEDI | 1408 26 30 22 17 18 38 26 87 |MD 59 59 54 37 37 45 32 34 38
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