[IGSREPORT-26029] Wk 2008 IGLOS Final Orbits
acc
acc at igs.org
Sun Jul 22 05:41:41 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2008 (Jul 01, 2018 - Jul 07, 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 2.2008.
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:
igl2008[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2008 in the SP3 format.
igl20087.sum Combination Report for GPS Week 2008.
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 | 2.4 ns
1 | 5.9 ns
2 | 5.2 ns
3 | 5.4 ns
4 | 6.9 ns
5 | 5.8 ns
6 | 6.2 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 1.2008, 1a.2008).
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 2.2008.0-6)
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 3.2008.0-6).
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 2008 summary. (Jul 01, 2018 - Jul 07, 2018)
Table 1.2008.a GPS week : 2008 MJD: 58300.0-58306.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -2 16 -21 -3 .07 31 29 | 5259 -392 3778 10372
| 0 1 1 13 16 25 .02 | 866 2215
cof n/a| 0 0 -2 6 3 -9 .12 34 31 | 5258 -399 3774 10370
| 0 1 1 32 18 36 .06 | 862 2230
emx n/a| -1 0 2 -2 -25 31 -.02 21 21 | 3614 -354 3726 9725
| 0 1 2 18 15 32 .03 | 7634 1367
esx n/a| 0 0 1 11 11 -32 .14 20 17 | 4525 557 3725 12195
| 0 1 0 22 13 40 .03 | 7878 2449
gfz n/a| 0 0 2 4 28 22 .00 27 19 | 0 -292 3711 9914
| 2 1 0 31 22 34 .04 | 0 2429
grg n/a| 0 0 0 -54 7 -5 -.33 42 33 | 5457 -280 3733 9668
| 1 1 3 18 16 48 .04 | 562 2278
iac n/a| 0 0 -1 -8 8 13 -.03 24 23 | 6739 213 5178 12097
| 1 1 2 59 58 52 .04 | 1816 2151
mcc n/a| -2 0 -11 39 -32 308 -.09 166 166 | --- --- --- ---
| 11 7 18 120 92 245 .15 | --- ---
Table 1.2008.b GPS week : 2008 MJD: 58300.0-58306.0
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 | 17 11 12 14 16 13 14 |
R02 | 7 6 8 8 6 5 6 |
R03 | 5 6 7 8 6 6 5 |
R04 | 6 5 6 5 5 6 8 |
R05 | 26 19 17 25 27 16 18 |
R07 | 6 6 6 7 7 5 7 |
R08 | 7 7 6 6 8 7 6 |
R09 | 6 7 7 7 7 6 7 |
R10 | 8 9 8 7 7 7 7 |
R11 | 9 7 6 8 8 6 7 |
R13 | 8 8 7 7 8 7 8 |
R14 | 12 9 9 8 7 8 7 |
R15 | 10 12 11 10 9 10 12 |
R16 | 14 11 11 10 12 10 11 |
R17 | 12 12 13 11 11 11 11 |
R18 | 19 7 8 10 9 8 7 |
R19 | 18 15 19 28 30 29 31 |
R20 | 18 15 14 16 19 16 17 |
R21 | 11 11 12 11 12 12 12 |
R22 | 14 13 13 13 10 12 14 |
R23 | 11 12 12 10 12 11 11 |
R24 | 14 17 17 22 19 15 13 |
R26 | 40 27 17 23 31 18 14 |
Table 1.2008.c GPS week : 2008 MJD: 58300.0-58306.0
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 2008 0 | 63 -20 84 683 -1083 -1528 83.1 1985 1985 | 2381 0
brd 2008 1 | 7 -39 276 1349 45 -1595 84.3 1546 1546 | 5919 0
brd 2008 2 | -73 11 275 1269 -1866 493 83.2 1743 1743 | 5154 0
brd 2008 3 | 10 -40 227 -624 -1804 1783 85.7 1563 1563 | 5400 0
brd 2008 4 | -3 27 199 -673 -999 3508 85.4 1939 1939 | 6910 0
brd 2008 5 | 22 4 141 -465 -31 2573 85.4 2039 2039 | 5773 0
brd 2008 6 | -13 -23 96 -859 944 2000 83.2 1791 1791 | 6234 0
-------------+------------------------------------------------------------+----------------
brd 2008 mean| 1 -11 185 96 -684 1033 84.4 1800 1800 | 5395 0
brd 2008 sdev| 41 26 79 968 1042 1989 1.2 197 197 | 1446 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 2.2008.0 GPS week: 2008 Day: 0 MJD: 58300
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 2 -2 37 -34 -10 .05 28 30 | 5559 -4448 4260 10680
cof n/a| -1 2 0 58 1 -4 .10 30 30 | 5574 -4489 4252 10672
emx n/a| -1 0 4 12 1 77 -.01 22 22 | 7582 -2603 4005 10057
esx n/a| 1 0 2 32 7 -11 .17 22 22 | 17762 -3977 3999 12372
gfz n/a| 0 0 1 -3 46 -29 -.06 25 24 | 0 -4776 4075 10272
grg n/a| -1 1 0 -49 9 16 -.31 37 30 | 4569 -4283 4028 10202
iac n/a| 0 -1 -2 -70 -8 -36 .06 27 24 | 5011 -1148 4400 9957
mcc n/a| 8 12 -40 -161 -106 106 -.27 158 158 | --- --- --- ---
Table 2.2008.1 GPS week: 2008 Day: 1 MJD: 58301
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 -5 31 -28 -31 .06 26 29 | 4316 647 3376 10362
cof n/a| 0 2 -1 5 14 -58 .13 31 31 | 4316 652 3374 10360
emx n/a| -1 -1 0 -24 -13 51 -.02 19 19 | 6630 585 3375 9880
esx n/a| 0 1 1 37 9 -25 .14 20 19 | -4056 1769 3382 12340
gfz n/a| 1 0 2 23 38 32 .06 25 19 | 0 365 3371 10024
grg n/a| 0 0 2 -34 11 -71 -.28 35 28 | 5560 900 3361 10042
iac n/a| 1 0 0 -31 -4 45 -.04 22 22 | 6882 47 4324 9944
mcc n/a| 5 -2 -22 59 5 337 -.08 105 105 | --- --- --- ---
Table 2.2008.2 GPS week: 2008 Day: 2 MJD: 58302
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 13 -29 -39 .09 30 29 | 4557 -224 3403 11176
cof n/a| 0 2 -5 9 -30 -41 .11 33 31 | 4546 -208 3401 11170
emx n/a| -1 1 2 0 -43 -1 -.01 20 20 | -10217 -175 3307 9849
esx n/a| 0 0 1 3 -4 -62 .16 17 15 | 3942 765 3307 12179
gfz n/a| 0 -1 2 2 -8 -15 -.01 25 19 | 0 -553 3321 10141
grg n/a| 1 2 3 -88 -14 52 -.40 39 30 | 5593 -721 3282 9835
iac n/a| 0 -2 -3 33 125 99 -.01 22 22 | 4926 4359 7419 11659
mcc n/a| -14 1 -2 91 79 262 -.27 118 118 | --- --- --- ---
Table 2.2008.3 GPS week: 2008 Day: 3 MJD: 58303
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 -3 13 -40 0 .09 31 28 | 4851 -1569 3639 9306
cof n/a| 0 0 -3 -36 7 37 .21 34 30 | 4870 -1610 3630 9305
emx n/a| -2 -1 0 -29 -27 45 -.07 28 28 | 865 -1553 3639 8785
esx n/a| 0 -1 1 -26 0 -108 .16 20 17 | 11044 360 3623 11486
gfz n/a| 0 1 3 -22 57 26 .01 27 19 | 0 -1180 3609 8961
grg n/a| 0 0 0 -64 -7 51 -.30 44 33 | 5881 -1155 3607 8523
iac n/a| 0 0 -4 88 4 36 -.01 26 25 | 10147 -1256 4624 16796
mcc n/a| -2 2 16 187 -196 604 -.08 157 157 | --- --- --- ---
Table 2.2008.4 GPS week: 2008 Day: 4 MJD: 58304
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 0 -3 10 -1 31 .06 35 31 | 4767 2236 4397 9896
cof n/a| 0 0 -5 10 31 32 .18 37 32 | 4766 2230 4398 9894
emx n/a| -1 -1 -1 0 -31 51 -.04 24 24 | 11995 1490 4409 9519
esx n/a| 0 0 1 26 37 -28 .10 22 18 | 3883 4057 4399 12323
gfz n/a| 1 -1 1 40 37 55 .02 28 20 | 0 2719 4416 9586
grg n/a| 1 0 1 -63 34 -6 -.35 49 34 | 5288 2759 4423 8825
iac n/a| 2 1 1 -49 -55 -51 -.05 25 23 | 5626 942 6041 15777
mcc n/a| -20 -6 -13 21 11 -49 .12 178 178 | --- --- --- ---
Table 2.2008.5 GPS week: 2008 Day: 5 MJD: 58305
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 -2 17 -14 11 .10 34 30 | 6157 -838 3461 11308
cof n/a| -1 -2 -2 29 -2 -32 .11 36 32 | 6138 -819 3461 11312
emx n/a| 0 0 4 22 -39 -5 -.03 18 18 | 9468 -496 3460 10456
esx n/a| 0 -1 0 10 13 4 .12 18 15 | 3475 -438 3458 13021
gfz n/a| -3 0 2 37 18 21 .05 28 18 | 0 -546 3351 10935
grg n/a| 0 0 2 -36 1 -46 -.32 43 35 | 6286 -941 3533 10834
iac n/a| 0 0 -1 -58 32 18 -.08 21 22 | 7430 -2182 4820 11074
mcc n/a| 2 5 -20 -63 -39 267 .07 204 204 | --- --- --- ---
Table 2.2008.6 GPS week: 2008 Day: 6 MJD: 58306
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 0 -4 0 12 .05 33 29 | 6609 1449 3910 9880
cof n/a| 0 0 -2 -28 1 4 .03 35 30 | 6599 1450 3907 9880
emx n/a| -1 2 6 0 -24 4 .01 18 18 | -1021 270 3891 9532
esx n/a| 0 -2 2 0 17 0 .15 22 17 | -4373 1366 3911 11644
gfz n/a| -2 -1 1 -46 13 65 -.03 29 17 | 0 1922 3840 9481
grg n/a| 2 0 -6 -46 15 -38 -.31 47 40 | 5024 1480 3899 9418
iac n/a| 1 0 -3 29 -32 -17 -.07 22 23 | 7152 731 4619 9478
mcc n/a| 5 -7 0 141 18 626 -.12 245 245 | --- --- --- ---
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 3.2008.0 GPS week: 2008 Day: 0 MJD: 58300
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 | 724 30 35 45 39 21 54 39 --- 17 | 56 60 52 48 49 64 56 --- 42
R02 | 2697 11 19 11 14 14 15 19 114 6 | 67 72 62 63 61 66 70 121 63
R03 | 2527 10 14 9 6 10 25 8 155 5 | 71 68 71 72 70 84 71 53 71
R04 | 1197 9 18 11 9 13 14 21 --- 5 | 72 70 73 71 72 70 62 --- 69
XR05 | 742 40 39 51 29 --- 105 29 --- 25 | 80 64 61 80 --- 76 53 --- 62
R07 | 844 13 15 11 6 15 13 14 152 5 | 71 75 72 78 83 75 75 178 75
R08 | 830 14 16 10 17 15 20 11 --- 6 | 64 69 66 79 77 68 66 --- 70
R09E | 3250 12 11 15 11 18 15 12 --- 6 | 49 47 45 43 49 51 47 --- 45
R10E | 1263 14 32 19 12 16 27 22 --- 8 | 28 41 27 36 34 40 41 --- 30
R11E | 1028 17 21 20 32 16 13 11 237 9 | 79 81 79 97 92 89 83 67 85
R13E | 1031 13 22 19 15 20 22 14 --- 7 | 35 41 34 36 34 35 32 --- 32
R14E | 701 18 29 16 40 20 31 17 --- 11 | 43 45 42 63 43 40 49 --- 44
R15E | 6501 22 21 18 12 22 36 20 --- 9 | 39 42 37 46 53 42 40 --- 40
R16E | 1451 19 35 24 20 38 59 26 --- 13 | 39 57 34 46 37 72 41 --- 37
R17 | 961 38 33 15 12 27 32 27 --- 11 | 76 76 47 45 35 62 33 --- 46
R18 | 844 37 29 35 19 30 57 70 --- 19 | 96 90 97 89 86 70 97 --- 83
R19 | 766 60 61 27 34 39 47 29 --- 17 | 173 170 141 130 137 166 141 --- 141
R20 | 813 46 51 24 27 39 73 35 --- 18 | 81 85 38 55 34 85 39 --- 45
R21 | 792 36 31 17 14 31 27 16 90 10 | 86 83 66 60 46 70 64 57 62
R22 | 740 40 41 22 13 38 42 23 --- 13 | 81 82 46 53 37 86 46 --- 53
R23 | 1169 25 22 30 32 6 17 22 --- 11 | 47 46 58 80 65 46 69 --- 60
R24 | 1080 28 27 20 31 30 47 30 --- 13 | 63 73 58 81 70 72 63 --- 63
XR26 | 4090 40 100 --- --- --- --- 39 --- 40 | 32 75 --- --- --- --- 42 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1985 28 30 22 22 25 37 27 158 |T 66 70 59 65 60 69 60 95 58
WRMS | 1985 30 30 22 22 24 30 24 158 |NE 76 78 67 72 65 77 65 102 65
MEDI | 1028 22 29 19 15 20 27 22 152 |MD 67 70 58 63 53 70 56 67 60
Table 3.2008.1 GPS week: 2008 Day: 1 MJD: 58301
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 | 1055 18 32 19 24 25 45 20 --- 11 | 42 60 52 48 46 49 41 --- 41
R02 | 1615 13 12 15 16 13 9 9 103 6 | 50 44 46 38 52 48 53 61 45
R03 | 1796 7 9 9 10 19 19 10 136 5 | 52 54 51 47 48 55 52 32 49
R04 | 1502 12 19 7 7 6 12 19 --- 5 | 55 51 58 57 59 61 67 --- 58
R05 | 909 22 33 41 36 26 86 34 --- 19 | 63 85 66 84 59 58 33 --- 59
R07 | 898 13 13 6 11 15 12 14 103 5 | 56 57 63 64 72 65 55 118 61
R08 | 820 11 14 12 21 14 15 15 --- 7 | 47 50 49 54 58 45 46 --- 49
R09E | 3767 14 22 15 14 18 24 14 --- 7 | 27 32 25 33 34 29 25 --- 26
R10E | 2089 11 33 18 15 20 43 16 --- 9 | 27 39 28 25 24 48 24 --- 23
R11E | 802 13 15 18 12 16 16 14 114 6 | 71 72 77 67 73 74 68 76 70
R13E | 1328 16 23 21 15 21 17 14 --- 8 | 34 38 36 34 35 35 37 --- 32
R14E | 642 15 9 17 27 16 14 26 --- 9 | 36 36 34 37 45 30 47 --- 35
R15E | 3197 31 11 20 24 23 35 29 --- 12 | 41 41 53 51 51 57 35 --- 43
R16E | 1037 17 31 22 24 22 25 34 --- 11 | 22 39 28 40 38 29 33 --- 25
R17 | 1072 39 47 20 13 30 21 26 --- 11 | 48 53 38 30 24 38 24 --- 31
R18 | 952 18 21 13 17 19 13 15 --- 7 | 46 43 42 46 41 38 41 --- 40
R19 | 1412 58 55 19 16 36 31 28 --- 14 | 114 111 103 99 101 103 106 --- 103
R20 | 632 46 64 23 29 28 36 31 --- 14 | 50 67 33 40 33 36 37 --- 31
R21 | 940 37 38 13 12 31 35 15 51 11 | 73 72 65 63 57 66 64 51 63
R22 | 1012 32 28 14 17 34 50 21 --- 12 | 50 44 41 41 36 59 45 --- 42
R23 | 708 30 37 26 30 15 24 30 --- 12 | 35 38 48 54 51 41 55 --- 45
R24 | 1226 27 29 26 27 51 68 25 --- 16 | 36 40 29 52 51 63 49 --- 39
XR26 | 3719 28 90 --- --- --- --- 24 --- 26 | 29 80 --- --- --- --- 44 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1545 26 31 19 20 24 35 22 105 |T 48 54 48 50 49 51 47 67 45
WRMS | 1545 29 31 19 19 19 28 22 105 |NE 52 59 52 54 52 55 50 65 49
MEDI | 1055 18 28 18 16 20 24 20 103 |MD 47 50 46 47 48 48 45 61 42
Table 3.2008.2 GPS week: 2008 Day: 2 MJD: 58302
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 | 1314 19 20 23 15 16 62 17 --- 11 | 52 50 42 43 53 66 39 --- 44
R02 | 1191 18 18 16 20 15 16 17 166 8 | 45 45 50 67 62 56 53 71 55
R03 | 565 17 17 15 12 17 17 10 129 6 | 57 53 55 49 58 59 50 25 52
R04 | 905 13 10 11 6 13 22 12 --- 5 | 47 50 50 52 47 61 55 --- 50
R05 | 1241 21 28 28 31 28 81 37 --- 16 | 35 44 38 37 30 55 39 --- 31
R07 | 779 11 18 10 7 15 15 17 92 5 | 48 43 48 52 60 56 52 104 51
R08 | 628 9 10 9 11 19 16 15 --- 5 | 44 42 46 47 55 50 39 --- 44
R09E | 4904 13 15 15 7 17 19 17 --- 6 | 40 40 37 43 49 43 39 --- 39
R10E | 1490 11 47 22 15 22 24 14 --- 8 | 44 61 54 51 45 43 40 --- 45
R11E | 1011 13 26 13 9 13 20 11 113 5 | 43 45 47 48 51 62 50 80 48
R13E | 3429 15 17 17 11 13 14 16 --- 6 | 31 33 36 35 34 26 31 --- 31
R14E | 1298 12 15 18 15 23 16 25 --- 8 | 33 32 34 38 39 36 35 --- 33
R15E | 2453 30 22 21 19 21 35 21 --- 10 | 40 43 43 52 54 55 44 --- 44
R16E | 1101 24 36 23 18 21 36 31 --- 11 | 37 50 39 38 39 35 33 --- 31
R17 | 680 37 39 21 14 36 39 25 --- 12 | 61 62 42 40 38 59 33 --- 40
R18 | 1307 15 18 15 11 18 19 24 --- 7 | 38 40 33 38 33 33 35 --- 33
R19 | 747 78 72 19 22 40 58 36 --- 19 | 168 170 167 173 171 182 159 --- 168
R20 | 1006 50 49 38 17 21 32 26 --- 14 | 59 56 39 47 38 39 38 --- 35
R21 | 889 44 50 21 19 35 17 20 61 12 | 64 66 43 43 27 45 47 35 40
R22 | 1418 41 49 16 16 31 52 15 --- 12 | 63 69 35 38 35 69 44 --- 41
R23 | 2115 29 31 23 23 21 41 23 --- 11 | 38 36 39 54 53 37 55 --- 44
R24 | 982 32 26 25 26 51 75 30 --- 17 | 56 56 46 64 53 70 57 --- 52
XR26 | 4023 19 83 --- --- --- --- 14 --- 17 | 45 93 --- --- --- --- 35 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1742 30 33 20 17 25 39 22 117 |T 51 55 48 52 51 56 47 63 47
WRMS | 1742 29 31 20 15 19 30 22 117 |NE 57 60 51 56 54 62 51 58 51
MEDI | 1191 19 26 18 15 21 22 17 113 |MD 45 50 42 47 47 55 40 71 44
Table 3.2008.3 GPS week: 2008 Day: 3 MJD: 58303
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 | 1367 26 22 45 14 31 48 24 --- 14 | 48 52 41 52 75 64 58 --- 51
R02 | 1101 15 16 16 22 10 11 24 252 8 | 54 58 53 75 61 60 60 169 60
R03 | 577 13 19 13 21 14 21 22 170 8 | 58 59 66 82 76 61 58 70 67
R04 | 961 9 11 13 9 7 14 12 --- 4 | 55 48 56 52 53 53 44 --- 51
R05 | 894 22 32 53 46 50 108 53 --- 24 | 43 46 47 58 40 54 32 --- 41
R07 | 720 13 15 12 17 15 11 17 126 6 | 49 54 53 71 63 57 55 124 58
R08 | 1038 14 16 13 14 9 15 15 --- 6 | 51 55 50 60 55 62 51 --- 54
R09E | 4354 14 19 14 12 14 14 24 --- 7 | 38 41 39 45 45 37 37 --- 39
R10E | 1330 14 18 18 12 14 22 15 --- 6 | 39 40 45 41 40 47 39 --- 38
R11E | 1291 10 17 16 11 17 23 24 109 7 | 80 78 80 78 85 77 88 132 80
R13E | 2930 10 11 13 15 12 20 20 --- 6 | 42 43 37 47 38 44 49 --- 41
R14E | 1555 15 16 17 18 20 14 16 --- 7 | 41 40 36 46 39 36 52 --- 40
R15E | 1521 29 17 23 18 25 17 21 --- 10 | 43 44 46 55 53 45 44 --- 45
R16E | 1045 19 43 26 19 26 28 18 --- 10 | 38 53 40 45 34 37 43 --- 35
R17 | 841 36 35 16 12 30 26 23 --- 11 | 71 72 56 47 41 62 47 --- 51
R18 | 1574 12 12 17 14 24 30 32 --- 9 | 46 49 38 56 45 55 43 --- 44
R19 | 580 95 105 38 34 56 93 51 --- 27 | 121 128 87 71 66 110 58 --- 72
R20 | 859 40 34 41 23 27 61 30 --- 16 | 62 63 41 53 36 59 42 --- 41
R21 | 837 34 36 17 9 32 21 23 48 10 | 67 68 51 52 34 61 45 44 48
R22 | 754 42 44 15 18 33 36 21 --- 12 | 68 70 43 55 34 67 42 --- 47
R23 | 1509 23 24 23 22 7 20 26 --- 9 | 45 50 53 73 62 44 63 --- 57
R24 | 1548 40 42 65 26 40 97 24 --- 21 | 74 93 71 89 79 60 74 --- 72
XR26 | 3252 22 62 --- --- --- --- 23 --- 22 | 39 80 --- --- --- --- 47 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1563 31 34 28 20 27 44 26 157 |T 55 60 51 59 52 56 50 107 50
WRMS | 1563 28 30 28 17 19 33 25 157 |NE 59 65 53 63 54 61 51 101 53
MEDI | 1101 19 19 17 17 20 21 23 126 |MD 49 54 47 55 45 57 47 124 48
Table 3.2008.4 GPS week: 2008 Day: 4 MJD: 58304
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 | 751 33 28 48 25 31 53 28 --- 16 | 38 31 33 39 51 42 37 --- 30
R02 | 740 13 10 13 17 12 15 13 123 6 | 42 42 44 45 45 57 47 103 44
R03 | 1433 17 15 11 13 18 13 10 135 6 | 46 49 45 59 63 53 54 28 53
R04 | 1368 8 17 12 10 12 20 11 --- 5 | 40 46 40 46 35 51 43 --- 41
R05 | 832 29 17 50 57 46 125 56 --- 26 | 24 35 45 58 43 58 32 --- 32
R07 | 719 10 9 19 8 17 20 16 267 6 | 47 49 54 52 54 38 45 111 48
R08 | 718 23 21 20 18 15 10 15 --- 8 | 45 49 41 66 61 53 59 --- 53
R09E | 5865 15 17 13 14 16 24 16 --- 7 | 28 31 34 31 43 43 33 --- 32
R10E | 920 11 13 11 16 19 20 17 --- 7 | 27 31 29 39 41 24 25 --- 29
R11E | 2873 15 17 13 15 14 16 25 223 7 | 49 51 48 42 42 43 33 124 42
R13E | 1748 10 17 16 16 19 25 16 --- 7 | 26 29 27 31 27 30 25 --- 24
R14E | 1314 13 16 19 8 19 23 13 --- 7 | 32 34 29 30 33 37 39 --- 30
R15E | 3933 26 32 20 15 24 21 20 --- 9 | 33 36 36 40 38 34 38 --- 32
R16E | 1544 20 22 28 27 26 36 20 --- 11 | 29 42 36 46 37 41 31 --- 31
R17 | 940 40 41 15 11 25 18 24 --- 10 | 63 64 40 39 25 40 28 --- 37
R18 | 1683 17 13 21 17 21 20 16 --- 8 | 40 37 34 41 27 33 33 --- 32
R19 | 971 118 127 22 30 65 98 49 --- 29 | 187 190 161 150 167 163 153 --- 155
R20 | 1075 46 42 33 25 35 83 36 --- 18 | 50 51 32 49 49 75 30 --- 32
R21 | 693 42 40 17 13 37 27 20 64 12 | 66 70 54 50 44 56 49 49 50
R22 | 502 35 33 12 8 29 34 17 --- 10 | 55 52 35 39 29 48 38 --- 37
R23 | 1278 19 22 26 33 14 33 21 --- 11 | 33 36 40 63 41 20 46 --- 42
R24 | 1262 39 52 40 20 31 97 25 --- 18 | 75 86 56 57 52 63 59 --- 56
XR26 | 2987 33 31 --- --- --- --- 28 --- 30 | 36 37 --- --- --- --- 34 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1938 35 37 24 22 28 49 25 178 |T 48 51 45 50 47 50 43 83 42
WRMS | 1938 31 32 24 18 20 34 23 178 |NE 55 57 50 56 52 56 49 72 47
MEDI | 1262 20 21 19 16 19 23 20 135 |MD 40 42 40 45 42 43 38 103 37
Table 3.2008.5 GPS week: 2008 Day: 5 MJD: 58305
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 | 816 26 40 23 31 18 50 26 --- 12 | 31 51 19 43 32 53 31 --- 25
R02 | 824 10 14 10 8 9 12 9 68 4 | 40 41 32 37 36 42 34 52 34
R03 | 1986 12 15 9 12 21 10 19 137 6 | 39 40 40 47 54 39 30 27 40
R04 | 2660 9 9 13 7 12 14 21 --- 6 | 35 32 35 35 38 39 28 --- 33
R05 | 1029 24 27 21 18 34 90 29 --- 15 | 29 42 48 30 34 34 39 --- 29
R07 | 927 9 9 6 12 16 13 12 303 5 | 38 42 39 39 30 45 41 143 37
R08 | 688 15 14 10 13 19 29 15 --- 7 | 44 46 35 36 42 55 49 --- 39
R09E | 6531 13 14 12 13 15 13 15 --- 6 | 45 42 35 52 47 45 40 --- 42
R10E | 854 13 12 15 14 21 21 16 --- 7 | 43 45 44 42 48 41 50 --- 43
R11E | 2404 9 12 12 12 14 10 15 297 5 | 65 66 64 64 73 66 74 97 66
R13E | 976 12 18 16 14 16 15 19 --- 7 | 41 44 46 43 42 42 44 --- 41
R14E | 1704 20 14 17 17 22 9 13 --- 7 | 22 22 24 34 35 19 24 --- 23
R15E | 3608 33 24 20 25 25 18 13 --- 10 | 45 47 47 53 54 48 51 --- 47
R16E | 1132 18 34 20 19 33 32 15 --- 10 | 32 43 29 34 36 43 30 --- 28
R17 | 759 42 48 13 13 27 33 23 --- 11 | 50 55 31 28 29 43 24 --- 30
R18 | 1508 20 18 19 17 25 17 14 --- 8 | 30 31 25 28 32 27 26 --- 24
R19 | 1253 113 109 30 36 68 91 47 --- 28 | 162 159 130 109 120 143 125 --- 123
R20 | 1385 41 53 27 17 41 77 24 --- 16 | 43 53 37 41 43 64 32 --- 32
R21 | 707 42 48 16 11 34 38 26 67 12 | 51 57 34 35 28 49 30 24 33
R22 | 656 39 41 13 11 37 47 22 --- 12 | 49 50 33 35 24 58 31 --- 34
R23 | 1039 13 19 19 29 12 44 17 --- 10 | 33 30 31 41 32 19 33 --- 29
R24 | 1008 22 25 22 24 38 73 26 --- 14 | 52 60 63 53 49 45 50 --- 49
XR26 | 2764 19 55 --- --- --- --- 17 --- 18 | 40 71 --- --- --- --- 36 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 2039 34 36 18 18 28 43 21 204 |T 46 50 41 43 43 48 41 68 39
WRMS | 2039 30 32 18 15 18 35 22 204 |NE 47 53 42 42 41 50 39 61 39
MEDI | 1039 19 19 16 14 21 21 17 137 |MD 41 45 35 39 36 43 34 52 34
Table 3.2008.6 GPS week: 2008 Day: 6 MJD: 58306
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 | 822 25 28 20 34 37 49 31 --- 14 | 42 42 40 47 50 64 40 --- 37
R02 | 533 9 16 10 12 14 14 14 107 5 | 57 58 52 58 52 54 53 100 53
R03 | 1208 8 17 12 7 13 10 14 149 5 | 61 58 58 61 61 64 52 40 58
R04 | 1371 5 11 16 15 10 18 27 --- 7 | 53 53 58 50 54 58 46 --- 51
R05 | 1090 26 21 20 18 34 119 26 --- 18 | 33 38 52 48 42 30 50 --- 40
R07 | 794 10 17 11 16 13 14 21 362 6 | 59 58 56 61 61 55 56 176 57
R08 | 565 11 17 11 12 13 13 14 --- 5 | 54 59 49 56 55 54 51 --- 52
R09E | 4947 12 11 12 14 18 12 18 --- 6 | 54 58 51 61 65 57 51 --- 55
R10E | 1885 13 9 12 16 16 29 14 --- 7 | 47 51 44 49 50 49 51 --- 46
R11E | 1551 13 15 14 18 16 17 15 354 7 | 85 76 81 83 86 82 90 91 84
R13E | 1748 18 22 17 15 17 17 15 --- 7 | 42 45 44 41 40 40 37 --- 39
R14E | 1393 15 21 15 13 19 19 16 --- 7 | 46 45 40 48 47 39 53 --- 44
R15E | 4494 30 21 29 16 30 30 18 --- 11 | 61 64 54 64 66 54 55 --- 56
R16E | 1070 19 29 23 23 29 40 20 --- 11 | 47 52 43 68 62 53 49 --- 49
R17 | 821 37 36 13 14 35 29 21 --- 11 | 80 80 47 49 30 70 38 --- 49
R18 | 953 13 15 15 18 16 28 10 --- 7 | 52 55 36 54 42 60 44 --- 45
R19 | 916 117 120 26 52 69 102 46 --- 31 | 199 199 145 128 137 184 144 --- 143
R20 | 1462 42 42 23 29 50 68 28 --- 16 | 71 74 31 47 37 81 38 --- 41
R21 | 743 39 39 14 12 37 40 24 98 12 | 79 78 48 43 32 75 41 51 48
R22 | 730 41 49 14 17 36 61 19 --- 13 | 79 85 43 41 27 90 42 --- 48
R23 | 682 21 14 24 30 16 30 21 --- 11 | 39 45 46 71 50 29 60 --- 49
R24 | 1090 14 18 23 24 28 68 26 --- 13 | 66 74 73 79 65 73 66 --- 67
XR26 | 2369 13 54 --- --- --- --- 14 --- 13 | 38 40 --- --- --- --- 43 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 1790 33 35 18 22 29 47 22 245 |T 62 64 54 59 55 64 54 91 54
WRMS | 1790 29 30 18 17 17 40 23 245 |NE 66 68 55 59 53 69 54 91 54
MEDI | 1090 15 21 15 16 18 29 19 149 |MD 54 58 48 54 50 57 51 91 49
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