[IGSREPORT-26090] Wk 2013 IGLOS Final Orbits
acc
acc at igs.org
Sat Aug 25 06:43:45 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2013 (Aug 05, 2018 - Aug 11, 2018)
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 2.2013.
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:
igl2013[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2013 in the SP3 format.
igl20137.sum Combination Report for GPS Week 2013.
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 | 5.9 ns
1 | 6.8 ns
2 | 3.5 ns
3 | 1.9 ns
4 | 3.7 ns
5 | 2.8 ns
6 | 4.2 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 1.2013, 1a.2013).
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 2.2013.0-6)
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 3.2013.0-6).
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 2013 summary. (Aug 05, 2018 - Aug 11, 2018)
Table 1.2013.a GPS week : 2013 MJD: 58335.0-58341.0
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 10 1 -14 -7 -.02 40 35 | 4262 -891 3587 9539
| 1 0 2 15 18 46 .06 | 1897 1987
cof n/a| -1 1 13 5 8 -12 -.01 43 37 | 4264 -903 3587 9538
| 1 1 3 22 12 41 .07 | 1889 1993
emx n/a| -1 1 0 10 -22 49 .04 23 23 | 726 -1084 3603 9047
| 1 1 0 30 20 27 .03 | 11301 1555
esx n/a| 0 0 0 -10 3 -7 .11 15 13 | 4034 -675 3601 11378
| 0 0 0 13 15 16 .03 | 12492 2192
gfz n/a| -2 0 -8 -4 46 24 .10 29 24 | 178 -913 3609 9228
| 1 1 2 12 17 50 .09 | 680 2468
grg n/a| 0 0 7 -37 -15 -126 -.31 51 41 | 4265 -750 3605 8897
| 1 1 6 25 14 50 .06 | 1903 2186
iac n/a| 0 0 -4 12 -2 -13 -.18 22 21 | 5980 -1122 3600 8962
| 1 0 2 16 20 42 .03 | 1985 1101
mcc n/a| 0 2 34 72 11 61 -.86 213 213 | --- --- --- ---
| 7 9 21 89 127 507 .49 | --- ---
Table 1.2013.b GPS week : 2013 MJD: 58335.0-58341.0
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 | 20 24 23 19 19 19 19 |
R02 | 12 10 12 10 10 9 9 |
R03 | 10 9 11 10 12 13 12 |
R04 | 8 8 8 10 9 9 8 |
R05 | 35 0 0 0 --- 0 0 |
R07 | 11 10 12 9 10 11 13 |
R08 | 11 9 13 9 11 11 12 |
R09 | 6 5 8 6 7 8 7 |
R10 | 6 6 10 9 11 8 9 |
R11 | 6 7 7 7 9 9 8 |
R13 | 9 6 8 8 7 10 10 |
R14 | 7 7 9 7 9 9 10 |
R15 | 12 13 12 12 13 14 16 |
R16 | 14 11 14 13 13 12 14 |
R17 | 9 9 11 10 9 10 12 |
R18 | 9 7 9 8 8 8 8 |
R19 | 23 20 20 19 21 19 19 |
R20 | 18 14 17 14 18 16 15 |
R21 | 12 11 13 11 11 8 10 |
R22 | 10 8 10 10 10 9 9 |
R23 | 7 7 10 9 8 10 10 |
R24 | 19 21 16 14 17 17 17 |
R26 | 27 20 12 20 22 29 14 |
Table 1.2013.c GPS week : 2013 MJD: 58335.0-58341.0
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 2013 0 | -23 2311 -1327 -595 -3963 -5155 4.9 >>>>> >>>>> | 5931 0
brd 2013 1 | 59 148 207 1600 -448 -673 68.8 >>>>> >>>>> | 6833 0
brd 2013 2 | 1867 2379 -9224 7586 -58240 -9466 <<<< >>>>> >>>>> | 3500 0
brd 2013 3 | 100 33 -1132 -307 -1636 499 86.3 >>>>> >>>>> | 1859 0
brd 2013 4 | 131 100 2405 4734 -3525 -1289 97.4 >>>>> >>>>> | 3657 0
brd 2013 5 | 613 ---- 262 -1061 -3845 -5548 89.6 >>>>> >>>>> | 2785 0
brd 2013 6 | 294 -12 532 733 -3450 -885 123.1 >>>>> >>>>> | 4202 0
-------------+------------------------------------------------------------+----------------
brd 2013 mean| 434 -910 -1182 1812 -10729 -3216 50.4 >>>>> >>>>> | 4109 0
brd 2013 sdev| 665 4718 3753 3204 20990 3597 82.5 27300 27300 | 1738 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 2.2013.0 GPS week: 2013 Day: 0 MJD: 58335
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 7 13 -31 48 .08 39 31 | 3952 -1407 3484 10011
cof n/a| 0 0 10 29 9 4 .11 44 34 | 3949 -1409 3484 10009
emx n/a| 0 0 0 15 -1 22 .08 28 28 | -1514 -1688 3482 9187
esx n/a| 0 0 0 -8 7 -16 .09 14 12 | 7938 -544 3496 12242
gfz n/a| -4 0 -6 -7 14 125 .21 31 23 | 307 -1811 3500 9559
grg n/a| 0 -1 3 -17 -12 -114 -.34 48 33 | 7004 -1899 3498 8978
iac n/a| -2 0 -7 28 -4 -56 -.16 21 21 | 7928 -2150 3494 9187
mcc n/a| -6 -8 60 164 -111 624 -1.64 183 183 | --- --- --- ---
Table 2.2013.1 GPS week: 2013 Day: 1 MJD: 58336
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 8 6 -23 60 -.04 42 32 | 6627 2353 3665 10049
cof n/a| -2 0 10 21 -3 35 -.02 45 34 | 6615 2371 3663 10051
emx n/a| -1 0 1 10 -12 28 .05 23 23 | 20877 1268 3698 9626
esx n/a| 0 0 0 -6 -1 3 .10 12 9 | 20069 2297 3694 11650
gfz n/a| -1 1 -5 -9 51 15 .13 28 24 | 693 3194 3704 9579
grg n/a| 0 -2 0 -31 -33 -119 -.34 58 35 | 5951 2897 3733 9201
iac n/a| 0 0 -6 3 0 -64 -.22 20 20 | 8768 721 3690 9357
mcc n/a| -4 -4 39 -77 117 -882 -.67 143 143 | --- --- --- ---
Table 2.2013.2 GPS week: 2013 Day: 2 MJD: 58337
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 7 8 -31 -12 .06 42 39 | 5826 -3955 4031 10882
cof n/a| -2 0 11 15 12 -1 -.01 46 41 | 5825 -3960 4040 10885
emx n/a| -2 0 0 -44 -16 79 .04 22 22 | -14467 -3208 4053 10359
esx n/a| 0 -1 0 8 34 -11 .17 18 16 | 19093 -3846 4047 12582
gfz n/a| -3 -1 -7 15 68 29 -.05 31 25 | 249 -4156 4057 10451
grg n/a| 0 0 0 -24 0 -95 -.25 50 43 | 5363 -3734 4038 10022
iac n/a| 2 -1 -1 26 -42 -45 -.18 21 20 | 6387 -2251 4043 10218
mcc n/a| 1 6 51 126 -51 -290 -.18 151 151 | --- --- --- ---
Table 2.2013.3 GPS week: 2013 Day: 3 MJD: 58338
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 10 6 16 -24 -.05 40 38 | 1313 -2362 3492 8726
cof n/a| 0 2 13 -8 9 20 .08 44 39 | 1328 -2388 3492 8724
emx n/a| -1 1 -1 -4 -37 82 .07 21 21 | 8254 -2514 3516 8470
esx n/a| 0 0 0 -10 -5 -24 .11 14 13 | -11026 -2776 3506 10570
gfz n/a| -3 -1 -9 9 59 -30 .18 28 28 | -911 -2397 3530 8619
grg n/a| -3 0 6 -12 -10 -238 -.34 49 45 | 2121 -2324 3480 8067
iac n/a| 1 0 0 19 -11 27 -.19 19 18 | 2982 -1805 3497 8295
mcc n/a| 7 -2 49 129 85 411 -.54 172 172 | --- --- --- ---
Table 2.2013.4 GPS week: 2013 Day: 4 MJD: 58339
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 14 8 -12 -62 -.06 40 34 | 2485 42 3461 8665
cof n/a| 0 3 18 20 6 -88 -.07 40 35 | 2494 13 3457 8663
emx n/a| -2 2 0 8 -33 70 .04 27 27 | 1988 325 3480 8278
esx n/a| 0 -1 0 -15 2 -10 .07 15 11 | -6036 1659 3466 10462
gfz n/a| -1 0 -9 -21 36 -19 .11 26 21 | -574 493 3485 8510
grg n/a| -1 0 15 -36 0 -119 -.28 48 42 | 2096 614 3458 8283
iac n/a| 0 0 -7 -4 15 27 -.16 22 22 | 4374 -217 3482 8248
mcc n/a| 14 3 22 -20 158 214 -.67 203 203 | --- --- --- ---
Table 2.2013.5 GPS week: 2013 Day: 5 MJD: 58340
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| -4 0 9 0 2 -51 -.04 38 32 | 4108 -703 3518 9672
cof n/a| -2 1 17 -6 30 -40 -.06 42 35 | 4114 -728 3522 9672
emx n/a| -1 2 0 31 -53 17 .03 23 23 | -5106 -957 3515 9137
esx n/a| 0 0 -1 -6 1 23 .10 14 13 | 4598 -596 3539 11696
gfz n/a| -3 0 -9 -10 44 19 .06 29 23 | 971 -2303 3540 9449
grg n/a| -1 1 11 -58 -36 -95 -.25 48 41 | 3381 -943 3536 9292
iac n/a| 4 0 -3 -13 2 -16 -.22 24 24 | 5381 -1441 3530 9185
mcc n/a| -1 19 2 118 66 35 -1.23 209 209 | --- --- --- ---
Table 2.2013.6 GPS week: 2013 Day: 6 MJD: 58341
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 13 -33 -23 -12 -.07 39 36 | 5527 -211 3461 8771
cof n/a| 0 0 16 -33 -8 -18 -.06 42 38 | 5526 -225 3456 8766
emx n/a| 0 3 0 54 0 44 -.02 21 21 | -4950 -818 3480 8273
esx n/a| 0 0 0 -35 -12 -18 .10 17 14 | -6396 -922 3463 10450
gfz n/a| -2 2 -14 -8 48 35 .08 31 25 | 512 587 3450 8433
grg n/a| 2 2 13 -84 -18 -103 -.40 55 48 | 3945 134 3497 8441
iac n/a| 0 -1 -2 23 22 29 -.14 24 24 | 6045 -711 3465 8244
mcc n/a| -6 4 15 64 -181 318 -1.09 428 428 | --- --- --- ---
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 3.2013.0 GPS week: 2013 Day: 0 MJD: 58335
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 |>>>>> 74 68 38 21 31 88 32 --- 19 | 79 82 35 29 39 77 40 --- 25
XR02 |>>>>> 40 44 16 11 30 --- 30 180 12 | 76 81 41 52 32 --- 32 152 44
R03 |>>>>> 42 37 19 6 30 15 21 186 9 | 83 80 59 55 45 64 39 90 53
R04 |>>>>> 29 27 15 6 34 18 15 --- 8 | 75 73 59 51 39 65 44 --- 52
XR05 | ---- 63 179 48 --- 94 124 24 --- 34 | --- --- --- --- --- --- --- --- 0
R07E |>>>>> 43 43 26 8 34 19 24 137 11 | 82 83 63 50 37 57 32 177 49
R08E |>>>>> 36 43 20 13 25 42 19 --- 10 | 78 81 57 51 39 84 42 --- 52
R09 |>>>>> 12 11 13 9 11 16 16 --- 5 | 49 47 48 42 45 43 49 --- 44
R10 |>>>>> 10 13 16 12 16 19 11 --- 6 | 62 65 47 62 43 68 49 --- 54
R11 |>>>>> 22 19 12 9 22 17 10 235 6 | 64 60 49 52 37 52 41 88 47
R13 |>>>>> 14 14 22 13 14 43 14 --- 8 | 57 60 43 61 58 83 46 --- 55
R14 |>>>>> 25 26 12 9 25 20 15 --- 7 | 65 65 44 53 52 56 46 --- 50
R15E |>>>>> 51 59 25 12 37 22 22 --- 12 | 77 79 39 32 39 39 24 --- 33
R16E |>>>>> 49 74 31 19 32 52 24 --- 14 | 84 100 69 73 55 97 70 --- 70
R17E |>>>>> 35 37 14 12 23 25 22 --- 9 | 49 51 37 43 30 49 30 --- 38
R18 |>>>>> 19 19 20 14 27 27 25 --- 9 | 35 37 33 41 32 41 29 --- 34
R19 |>>>>> 92 112 45 30 57 61 40 --- 22 | 94 104 69 49 41 83 35 --- 52
R20 |>>>>> 18 18 55 20 37 85 23 --- 17 | 61 69 42 54 47 60 29 --- 41
R21 |>>>>> 30 37 17 11 46 43 25 161 11 | 55 58 49 47 41 45 35 94 43
R22 |>>>>> 28 27 18 13 36 43 13 --- 10 | 44 45 41 38 30 46 30 --- 35
R23E |>>>>> 14 23 24 13 11 20 14 --- 7 | 26 35 24 33 30 30 29 --- 27
R24 |>>>>> 33 32 52 16 21 113 14 --- 19 | 59 58 43 37 51 61 34 --- 40
XR26 | ---- 35 77 --- --- --- --- 20 --- 26 | 22 53 --- --- --- --- 28 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 39 44 28 14 31 48 21 183 |T 62 66 47 47 41 60 37 120 43
WRMS |>>>>> 31 34 28 12 23 33 21 183 |NE 61 64 46 48 42 60 37 106 43
MEDI |>>>>> 33 37 20 12 30 27 21 180 |MD 62 65 44 50 39 57 35 94 44
Table 3.2013.1 GPS week: 2013 Day: 1 MJD: 58336
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 |>>>>> 91 100 27 29 41 140 32 --- 23 | 65 79 46 44 44 99 36 --- 31
R02 |>>>>> 37 38 19 10 32 45 14 84 10 | 63 60 36 46 43 68 38 98 43
R03 |>>>>> 36 38 14 5 25 29 26 86 9 | 72 69 61 60 53 63 44 99 57
R04 |>>>>> 27 20 15 5 28 38 15 --- 8 | 62 57 49 45 39 72 40 --- 47
XR05 | ---- 6 >>>> --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07E |>>>>> 47 57 20 7 31 14 21 223 9 | 70 78 48 46 39 38 32 141 42
R08E |>>>>> 35 39 13 5 31 39 19 --- 9 | 60 60 41 42 28 54 38 --- 40
R09 |>>>>> 12 13 9 8 9 10 18 --- 5 | 44 42 44 37 40 34 43 --- 39
R10 |>>>>> 11 14 15 11 15 16 11 --- 5 | 45 44 40 47 36 42 32 --- 41
R11 |>>>>> 16 20 20 12 22 22 11 152 7 | 43 45 42 36 37 45 32 53 36
R13 |>>>>> 10 7 16 8 15 26 9 --- 5 | 41 39 36 44 38 44 37 --- 39
R14 |>>>>> 25 32 12 9 16 27 10 --- 6 | 47 52 38 43 41 38 34 --- 38
R15E |>>>>> 65 58 29 9 29 46 17 --- 13 | 56 53 38 27 37 42 21 --- 26
R16E |>>>>> 39 62 24 14 28 32 25 --- 10 | 63 71 44 51 39 41 49 --- 46
R17E |>>>>> 32 31 13 9 18 44 20 --- 8 | 28 29 21 37 33 39 24 --- 28
R18 | ---- 22 24 17 6 21 21 19 --- 7 | 23 25 24 25 29 29 23 --- 24
R19 |>>>>> 92 84 35 24 53 75 31 --- 20 | 43 45 42 36 34 40 23 --- 31
R20 |>>>>> 45 33 40 15 25 67 19 --- 14 | 23 44 45 40 32 28 23 --- 32
R21 |>>>>> 40 37 21 9 29 20 31 119 10 | 30 32 32 37 27 29 32 82 31
R22 |>>>>> 30 36 13 6 29 25 21 --- 8 | 25 30 27 29 26 15 22 --- 24
R23E |>>>>> 14 12 21 13 13 14 8 --- 6 | 28 32 20 33 24 27 19 --- 23
R24 |>>>>> 26 48 42 8 36 159 18 --- 21 | 33 62 32 29 38 92 23 --- 29
XR26 | ---- 26 41 --- --- --- --- 14 --- 19 | 17 55 --- --- --- --- 29 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 42 45 23 12 28 58 20 143 |T 44 50 38 39 36 46 31 94 35
WRMS |>>>>> 32 34 23 9 24 35 20 143 |NE 42 48 39 39 37 49 31 83 35
MEDI |>>>>> 30 37 19 9 28 29 18 119 |MD 43 45 40 40 37 41 32 98 32
Table 3.2013.2 GPS week: 2013 Day: 2 MJD: 58337
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 |>>>>> 94 102 35 21 48 100 34 --- 22 | 76 83 22 34 50 64 37 --- 21
R02 |>>>>> 39 36 20 14 30 50 15 70 11 | 59 58 37 26 22 49 26 73 30
R03 |>>>>> 33 38 21 14 33 32 21 81 10 | 60 64 47 43 32 58 31 58 40
R04 |>>>>> 26 33 17 6 30 27 15 --- 8 | 63 68 54 46 35 63 39 --- 47
XR05 | ---- 5 68 --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07E |>>>>> 49 51 23 20 22 17 22 249 11 | 68 71 43 36 38 40 32 163 36
R08E |>>>>> 34 38 15 9 33 70 21 --- 12 | 57 62 35 38 30 86 32 --- 38
R09 |>>>>> 15 16 15 13 21 20 20 --- 7 | 29 33 32 38 39 40 34 --- 32
R10 |>>>>> 13 16 17 18 25 40 21 --- 9 | 50 54 39 57 34 70 43 --- 46
R11 |>>>>> 25 21 11 13 16 12 11 170 6 | 49 49 38 41 32 32 27 72 35
R13 |>>>>> 15 17 19 16 18 30 16 --- 8 | 48 51 37 52 41 57 48 --- 44
R14 |>>>>> 29 31 12 16 27 28 14 --- 8 | 48 51 34 36 31 43 35 --- 33
R15E |>>>>> 59 66 19 10 38 21 17 --- 12 | 63 71 35 25 20 24 20 --- 26
R16E |>>>>> 25 29 32 25 33 53 25 --- 13 | 58 51 38 64 52 59 51 --- 48
R17E |>>>>> 35 36 13 14 29 52 21 --- 11 | 35 38 27 32 25 51 22 --- 27
R18 |>>>>> 19 24 19 18 17 36 14 --- 8 | 30 29 30 38 34 31 30 --- 30
R19 | ---- 83 77 21 22 50 74 35 --- 19 | 56 56 58 52 45 58 29 --- 44
R20 |>>>>> 53 77 44 25 34 61 15 --- 16 | 46 58 46 39 36 34 29 --- 27
R21 |>>>>> 43 50 25 14 28 43 34 104 13 | 34 40 36 35 35 31 28 48 30
R22 |>>>>> 36 37 12 17 31 26 19 --- 9 | 37 35 33 32 30 28 36 --- 30
R23E |>>>>> 8 13 28 26 22 21 11 --- 9 | 20 25 27 28 26 32 19 --- 21
R24 | ---- 22 24 23 22 38 97 25 --- 16 | 46 43 61 35 38 25 24 --- 32
XR26 | ---- 17 37 --- --- --- --- 7 --- 12 | 41 60 --- --- --- --- 22 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 42 46 22 18 31 50 21 151 |T 48 52 38 39 34 46 31 82 33
WRMS |>>>>> 39 41 22 16 25 43 20 151 |NE 48 52 40 40 35 45 32 62 34
MEDI |>>>>> 29 36 19 16 30 36 19 104 |MD 48 51 37 38 34 43 30 72 32
Table 3.2013.3 GPS week: 2013 Day: 3 MJD: 58338
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 |>>>>> 82 87 31 23 40 79 33 --- 19 | 68 76 44 54 62 50 36 --- 38
R02 |>>>>> 41 47 13 7 28 35 22 94 9 | 64 69 33 36 33 44 21 49 32
R03 |>>>>> 39 33 14 8 19 48 20 82 9 | 68 66 48 53 48 85 44 32 51
R04 |>>>>> 34 39 14 13 29 36 17 --- 9 | 62 65 38 36 38 63 29 --- 36
XR05 | ---- 6 154 --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07E |>>>>> 46 45 15 6 28 24 14 289 9 | 74 73 40 40 31 49 32 204 39
R08E | ---- 31 31 18 12 18 41 16 --- 9 | 67 65 36 47 34 73 37 --- 43
R09 |>>>>> 11 14 13 10 11 17 14 --- 5 | 31 35 30 26 31 38 34 --- 28
R10 |>>>>> 10 12 24 13 23 43 15 --- 9 | 62 63 48 63 47 85 48 --- 55
R11 |>>>>> 21 17 12 12 21 21 15 198 7 | 58 52 41 51 34 46 31 107 43
R13 |>>>>> 17 18 19 11 24 27 14 --- 7 | 60 60 48 54 39 69 50 --- 50
R14 |>>>>> 28 32 14 10 26 18 10 --- 7 | 61 64 36 50 27 49 46 --- 43
R15E |>>>>> 59 55 19 12 45 26 16 --- 12 | 69 65 31 25 32 36 30 --- 28
R16E |>>>>> 26 63 29 12 28 73 24 --- 13 | 72 103 47 58 59 96 57 --- 56
R17E |>>>>> 39 42 12 9 31 38 20 --- 9 | 43 45 30 38 29 48 24 --- 33
R18 |>>>>> 16 23 14 9 21 42 16 --- 7 | 30 35 26 30 27 44 23 --- 27
R19 |>>>>> 80 81 25 33 27 72 32 --- 18 | 66 69 41 59 48 62 28 --- 43
R20 |>>>>> 53 63 29 7 24 77 14 --- 13 | 53 55 37 37 40 41 31 --- 36
R21 |>>>>> 41 43 14 10 34 56 21 95 11 | 45 48 33 34 31 42 31 20 33
R22 |>>>>> 34 32 15 10 28 58 14 --- 10 | 38 42 32 34 26 47 31 --- 31
R23E |>>>>> 16 18 29 17 24 19 13 --- 9 | 24 28 28 29 21 18 24 --- 22
R24 |>>>>> 19 22 37 20 34 75 19 --- 14 | 37 40 35 34 26 56 33 --- 30
XR26 | ---- 27 65 --- --- --- --- 15 --- 20 | 28 51 --- --- --- --- 27 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 40 44 21 14 28 49 19 172 |T 53 57 37 42 36 54 33 82 37
WRMS |>>>>> 38 39 21 13 28 45 18 172 |NE 51 55 38 43 37 54 33 52 37
MEDI |>>>>> 31 39 15 11 27 41 16 95 |MD 60 60 36 38 33 49 31 49 36
Table 3.2013.4 GPS week: 2013 Day: 4 MJD: 58339
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 | ---- 83 77 35 26 33 65 31 --- 19 | 76 75 42 54 44 57 43 --- 38
R02 |>>>>> 38 46 18 14 23 31 17 139 9 | 63 73 33 52 37 50 33 55 43
R03 |>>>>> 37 38 18 9 32 43 35 135 12 | 65 66 47 47 36 70 25 75 42
R04 |>>>>> 36 32 16 6 20 28 19 --- 8 | 69 68 55 56 51 70 47 --- 54
R07E | ---- 45 40 16 8 25 32 16 319 9 | 73 72 44 44 45 58 38 251 45
R08E | ---- 32 32 16 10 32 53 13 --- 10 | 64 65 45 52 43 82 54 --- 50
R09 |>>>>> 11 11 15 10 10 26 20 --- 6 | 36 35 40 37 36 27 39 --- 35
R10 |>>>>> 21 22 31 17 16 41 18 --- 10 | 60 63 49 59 43 82 43 --- 52
R11 |>>>>> 22 35 20 9 28 48 12 242 9 | 62 74 50 46 47 80 39 175 48
R13 |>>>>> 17 18 13 5 16 32 20 --- 7 | 56 58 50 47 39 61 40 --- 46
R14 |>>>>> 30 27 15 13 22 36 12 --- 8 | 60 58 49 50 42 47 44 --- 47
R15E |>>>>> 53 49 15 12 42 31 26 --- 12 | 64 66 44 44 43 40 32 --- 41
R16E |>>>>> 38 41 32 19 19 48 24 --- 12 | 93 100 51 71 60 83 56 --- 64
R17E |>>>>> 35 38 11 8 28 19 18 --- 8 | 36 38 32 36 28 42 27 --- 30
R18 |>>>>> 17 26 9 11 27 34 15 --- 7 | 41 49 38 46 49 32 38 --- 40
R19 |>>>>> 78 84 38 37 38 81 25 --- 20 | 63 63 38 49 36 64 31 --- 38
R20 |>>>>> 42 22 61 17 20 85 30 --- 18 | 50 37 56 47 51 54 33 --- 42
R21 | ---- 35 35 14 10 29 42 30 94 10 | 36 37 33 37 30 29 27 39 31
R22 |>>>>> 31 38 13 6 31 47 23 --- 10 | 39 45 34 39 43 51 38 --- 38
R23E |>>>>> 15 18 24 16 11 23 15 --- 7 | 30 33 28 31 31 37 28 --- 29
R24 |>>>>> 22 24 56 20 17 79 25 --- 16 | 32 40 48 43 33 55 22 --- 34
XR26 | ---- 27 43 --- --- --- --- 18 --- 22 | 36 42 --- --- --- --- 33 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 40 40 27 15 26 48 22 203 |T 54 57 43 47 41 55 36 119 41
WRMS |>>>>> 34 35 27 11 21 42 22 203 |NE 52 55 44 47 41 55 35 86 41
MEDI |>>>>> 32 35 16 11 25 41 19 139 |MD 60 58 44 47 43 55 38 75 41
Table 3.2013.5 GPS week: 2013 Day: 5 MJD: 58340
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 | ---- 85 85 30 25 37 68 32 --- 19 | 53 59 41 46 41 30 31 --- 27
R02 | ---- 29 37 19 9 25 38 14 107 9 | 45 52 19 38 29 45 29 42 31
R03 |>>>>> 38 44 17 7 41 55 30 106 12 | 51 59 30 31 24 73 23 26 30
R04 |>>>>> 35 37 15 12 26 19 17 --- 8 | 49 53 34 35 25 33 31 --- 32
XR05 |>>>>> 6 3039 --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07E |>>>>> 39 37 12 12 26 38 32 410 10 | 55 55 37 36 26 56 22 354 33
R08E | ---- 34 30 12 7 28 57 23 --- 10 | 52 48 29 29 23 62 24 --- 30
R09 |>>>>> 13 15 15 14 16 26 28 --- 8 | 23 24 27 22 27 29 30 --- 21
R10 |>>>>> 13 14 18 8 17 39 15 --- 7 | 50 53 39 45 43 72 43 --- 44
R11 |>>>>> 29 21 18 12 25 37 16 118 9 | 48 42 32 30 24 56 23 161 30
R13 |>>>>> 18 20 14 10 24 60 18 --- 10 | 43 48 34 40 36 69 31 --- 36
R14 |>>>>> 32 36 12 14 22 27 22 --- 9 | 46 49 35 42 45 59 39 --- 40
R15E |>>>>> 50 47 20 13 41 40 36 --- 13 | 50 51 31 31 25 49 18 --- 27
R16E |>>>>> 38 48 30 14 19 43 25 --- 11 | 73 81 43 51 52 53 53 --- 48
R17E | ---- 40 41 22 11 24 13 26 --- 10 | 29 28 26 25 19 24 18 --- 21
R18 |>>>>> 16 19 9 10 33 33 20 --- 8 | 18 18 19 20 21 25 21 --- 16
R19 |>>>>> 61 65 40 21 50 72 38 --- 18 | 37 40 51 38 30 46 29 --- 36
R20 |>>>>> 52 78 20 18 28 83 26 --- 15 | 48 67 51 32 43 51 26 --- 36
R21 |>>>>> 29 37 14 10 18 27 21 115 8 | 45 49 46 36 51 35 50 52 43
R22 | ---- 29 28 16 8 32 17 26 --- 9 | 26 23 32 29 21 24 23 --- 25
R23E |>>>>> 19 22 25 25 15 27 7 --- 9 | 15 19 21 27 20 17 16 --- 18
R24 |>>>>> 20 16 50 20 29 86 16 --- 16 | 27 28 37 41 47 37 20 --- 28
XR26 | ---- 32 58 --- --- --- --- 25 --- 28 | 55 82 --- --- --- --- 28 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 38 42 23 14 29 48 24 209 |T 42 46 34 34 32 45 28 127 31
WRMS |>>>>> 32 35 23 13 23 41 24 209 |NE 41 46 35 35 33 45 29 70 31
MEDI |>>>>> 32 37 18 12 26 38 23 115 |MD 46 49 34 35 27 46 26 52 30
Table 3.2013.6 GPS week: 2013 Day: 6 MJD: 58341
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 | ---- 81 91 32 22 31 79 31 --- 19 | 73 83 40 45 48 60 43 --- 31
R02 | ---- 32 32 19 8 30 36 13 142 9 | 64 67 32 42 27 59 34 59 37
R03 | ---- 42 38 19 9 21 49 31 103 11 | 77 75 42 43 28 83 24 55 42
R04 |>>>>> 31 35 14 7 25 19 18 --- 8 | 69 73 51 47 34 58 41 --- 47
XR05 | ---- 7 3556 --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07E |>>>>> 44 49 19 19 31 42 28 824 12 | 86 88 49 49 44 75 30 370 48
R08E |>>>>> 31 36 13 9 29 72 29 --- 12 | 73 77 40 42 27 100 30 --- 43
R09 |>>>>> 12 15 12 13 15 22 22 --- 7 | 33 33 34 30 37 32 42 --- 32
R10 |>>>>> 15 16 20 14 21 39 14 --- 8 | 68 68 51 71 48 95 64 --- 63
R11 |>>>>> 23 23 19 7 22 23 16 153 7 | 69 69 51 51 35 66 43 137 49
R13 |>>>>> 17 20 15 10 25 68 19 --- 10 | 60 61 45 51 42 99 43 --- 49
R14 |>>>>> 31 31 12 11 34 39 19 --- 9 | 63 67 43 52 45 67 43 --- 46
R15E |>>>>> 60 59 23 28 34 41 34 --- 15 | 79 80 44 32 27 56 22 --- 33
R16E |>>>>> 32 51 29 20 25 71 27 --- 13 | 83 102 65 79 62 100 61 --- 70
R17E |>>>>> 39 38 21 13 42 35 29 --- 12 | 70 71 67 66 62 71 61 --- 64
R18 |>>>>> 21 20 18 15 24 27 13 --- 8 | 36 37 25 41 37 39 34 --- 33
R19 |>>>>> 69 68 28 28 55 66 39 --- 19 | 88 89 60 66 44 85 38 --- 56
R20 |>>>>> 41 54 31 27 35 54 27 --- 14 | 52 55 58 37 39 59 38 --- 39
XR21 |>>>>> 35 36 15 12 28 --- 13 96 9 | 64 67 58 57 53 --- 56 52 56
R22 |>>>>> 23 25 12 9 21 48 22 --- 9 | 48 50 39 47 48 48 35 --- 41
R23E | ---- 15 24 27 23 14 32 15 --- 10 | 22 25 19 34 33 30 30 --- 25
R24 |>>>>> 25 32 23 15 55 120 15 --- 17 | 45 50 48 41 49 56 35 --- 39
XR26 | ---- 17 143 --- --- --- --- 10 --- 14 | 47 133 --- --- --- --- 32 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 39 42 21 17 31 55 24 428 |T 62 69 45 48 41 66 39 134 44
WRMS |>>>>> 36 38 21 14 25 48 24 428 |NE 59 67 45 48 40 64 40 75 43
MEDI |>>>>> 31 36 19 13 28 41 19 142 |MD 64 68 45 47 42 60 38 59 42
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