[IGSREPORT-25207] Wk 1942 IGLOS Final Orbits
acc
acc at igs.org
Sun Apr 16 05:32:23 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1942 (Mar 26, 2017 - Apr 01, 2017)
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 2.1942.
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:
igl1942[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1942 in the SP3 format.
igl19427.sum Combination Report for GPS Week 1942.
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 | -11.8 ns
1 | 2.0 ns
2 | -11.5 ns
3 | -1.3 ns
4 | -10.6 ns
5 | 7.3 ns
6 | 0.8 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
----+--------+---------------
5 | GFZ | R06
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 1.1942, 1a.1942).
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 2.1942.0-6)
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 3.1942.0-6).
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 1942 summary. (Mar 26, 2017 - Apr 01, 2017)
Table 1.1942.a GPS week : 1942 MJD: 57838.0-57844.0
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| 0 0 6 -36 6 58 .14 25 26 | -1730 297 3303 11838
| 1 1 2 13 25 17 .03 | 6720 2839
cof n/a| 0 0 6 -38 22 38 .14 28 28 | -1733 295 3300 11835
| 1 1 1 26 33 28 .06 | 6723 2836
emx n/a| 0 0 4 -9 -42 -81 .02 25 25 | -3494 924 3287 11040
| 2 2 1 41 25 46 .05 | 18207 2012
esx n/a| 0 0 -3 9 11 -9 .14 18 18 | -5679 -570 3296 13827
| 1 0 1 23 25 29 .02 | 13701 3510
gfz n/a| -1 0 -4 -9 34 -1 .01 21 19 | 0 39 3294 11601
| 1 1 2 16 23 31 .03 | 0 2403
grg n/a| 0 0 12 -46 23 7 -.47 33 31 | -20538 32751 3340 11584
| 2 2 5 18 29 91 .05 | 30600 64708
iac n/a| 0 0 -7 46 -19 21 .02 19 19 | -3465 273 3295 11000
| 1 1 0 46 49 62 .06 | 7319 1158
mcc n/a| -2 1 8 112 72 322 -.17 138 138 | --- --- --- ---
| 8 7 28 103 191 552 .42 | --- ---
Table 1.1942.b GPS week : 1942 MJD: 57838.0-57844.0
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 | 11 10 11 13 14 16 12 |
R02 | 8 8 9 7 7 7 8 |
R03 | 7 6 6 8 8 7 8 |
R04 | 9 8 7 7 8 7 8 |
R05 | 9 11 11 10 11 13 12 |
R06 | --- --- --- --- --- 42 8 |
R07 | 8 7 10 8 9 8 7 |
R08 | 10 8 9 8 10 10 8 |
R09 | 7 7 7 8 9 7 6 |
R10 | 8 9 8 10 8 9 8 |
R11 | 8 8 10 9 8 10 7 |
R13 | 10 8 9 7 7 8 10 |
R14 | 14 12 11 11 13 12 15 |
R15 | 11 9 9 10 11 11 9 |
R16 | 15 14 15 12 13 16 11 |
R17 | 9 10 11 10 10 9 9 |
R18 | 8 7 8 10 7 8 8 |
R19 | 10 11 14 15 13 13 15 |
R20 | 13 13 14 12 15 17 14 |
R21 | 9 9 8 8 9 11 9 |
R22 | 8 10 9 8 8 9 12 |
R23 | 8 9 7 8 7 9 9 |
R24 | 16 17 18 15 14 17 16 |
R26 | 21 18 36 20 21 20 18 |
Table 1.1942.c GPS week : 1942 MJD: 57838.0-57844.0
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 1942 0 | -14 21 108 307 -399 4624 85.3 1367 1367 | -11802 0
brd 1942 1 | -53 -9 105 -1228 -259 5587 85.9 1289 1289 | 1979 0
brd 1942 2 | 13 -8 116 -914 212 5627 85.6 1036 1036 | -11546 0
brd 1942 3 | 18 2 104 112 429 2589 85.5 1168 1168 | -1338 0
brd 1942 4 | -44 -5 119 86 369 -458 85.9 1227 1227 | -10570 0
brd 1942 5 | 10 36 188 675 1050 1565 87.0 1327 1327 | 7331 0
brd 1942 6 | -75 -49 74 -246 -184 1478 86.5 1153 1153 | 777 0
-------------+------------------------------------------------------------+----------------
brd 1942 mean| -20 -1 116 -172 174 3001 86.0 1223 1223 | -3595 0
brd 1942 sdev| 37 27 34 679 502 2335 .6 114 114 | 7679 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 2.1942.0 GPS week: 1942 Day: 0 MJD: 57838
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 4 -22 -26 50 .13 24 25 | -10562 367 3235 11481
cof n/a| 0 0 7 -8 -36 31 .11 29 27 | -10558 351 3234 11484
emx n/a| -4 1 5 -58 -54 -88 -.05 24 24 | -10650 583 3217 11005
esx n/a| 1 0 0 7 21 -17 .17 18 15 | -23631 1685 3235 13870
gfz n/a| -2 0 -2 -22 20 -23 .01 20 19 | 0 36 3222 10985
grg n/a| 0 0 5 -71 7 102 -.42 35 30 | -11796 441 3240 11364
iac n/a| 4 0 -6 101 -1 12 .08 18 18 | -11248 -967 3225 10698
mcc n/a| -1 0 -11 261 -219 498 -.14 100 100 | --- --- --- ---
Table 2.1942.1 GPS week: 1942 Day: 1 MJD: 57839
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 8 -25 -24 56 .12 25 26 | 4064 3887 3266 11305
cof n/a| 1 0 7 -26 3 28 .02 27 27 | 4044 3906 3256 11295
emx n/a| 2 2 3 -24 -64 -21 -.02 24 24 | -10255 3402 3263 10652
esx n/a| 0 0 -3 11 20 -17 .16 16 15 | -7494 2591 3266 13318
gfz n/a| -1 0 -1 10 47 -44 -.01 21 20 | 0 3333 3251 11383
grg n/a| 1 -2 6 -65 37 79 -.52 34 26 | 185 3668 3303 11017
iac n/a| -1 1 -6 45 -12 -2 .10 18 18 | 1700 1334 3263 10556
mcc n/a| -8 8 -31 86 -35 463 -.69 111 111 | --- --- --- ---
Table 2.1942.2 GPS week: 1942 Day: 2 MJD: 57840
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 5 -38 28 60 .13 26 27 | -5849 -2280 3660 12255
cof n/a| 0 0 8 -40 28 14 .15 29 28 | -5854 -2287 3657 12251
emx n/a| 0 0 4 61 -72 -124 -.02 23 23 | -10519 -1647 3604 11236
esx n/a| 0 0 -2 3 0 -42 .14 20 20 | 6897 -5759 3651 14466
gfz n/a| -2 0 -2 -30 20 -9 .06 20 20 | 0 -2203 3651 11970
grg n/a| -2 1 8 -53 11 73 -.44 34 31 | -10415 -2315 3858 11705
iac n/a| 1 -1 -8 12 11 63 .00 22 22 | -10334 -963 3667 11449
mcc n/a| -13 10 7 134 342 -465 .08 159 159 | --- --- --- ---
Table 2.1942.3 GPS week: 1942 Day: 3 MJD: 57841
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 6 -43 9 75 .18 23 24 | 1679 -3837 3220 12814
cof n/a| 0 1 7 -58 42 65 .20 27 27 | 1677 -3828 3220 12809
emx n/a| 0 0 3 -14 -27 -86 .09 25 25 | -4186 -1254 3244 11294
esx n/a| -2 -1 -5 20 53 -8 .10 19 18 | 16217 -4231 3215 14606
gfz n/a| -1 1 -4 6 77 -10 -.04 21 17 | 0 -3076 3213 12606
grg n/a| 0 -1 16 -32 50 48 -.55 31 27 | 382 -3413 3218 12565
iac n/a| 0 0 -7 46 -115 -12 .07 18 18 | -1719 -552 3222 11843
mcc n/a| 11 -5 21 183 175 -326 .32 97 97 | --- --- --- ---
Table 2.1942.4 GPS week: 1942 Day: 4 MJD: 57842
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 4 -48 0 79 .18 24 24 | -9424 -746 3084 11278
cof n/a| 2 0 4 -39 36 90 .14 26 26 | -9440 -727 3085 11277
emx n/a| 1 -4 3 24 -4 -15 .06 26 26 | -29185 374 3088 10802
esx n/a| 0 0 -4 -7 8 2 .14 16 16 | -13328 -2411 3090 13092
gfz n/a| 0 3 -6 5 31 38 -.00 24 23 | 0 -1053 3080 11004
grg n/a| 0 0 17 -50 14 -27 -.45 31 31 | -9887 -1179 3111 10958
iac n/a| 0 -1 -7 3 -25 -83 -.02 20 20 | -10525 345 3082 10532
mcc n/a| -6 -9 30 106 233 278 -.22 152 152 | --- --- --- ---
Table 2.1942.5 GPS week: 1942 Day: 5 MJD: 57843
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 2 9 -53 42 61 .16 29 31 | 5755 3409 3274 11799
cof n/a| -2 1 5 -83 17 12 .21 30 32 | 5765 3388 3269 11794
emx n/a| 0 2 5 -45 -18 -109 -.01 31 31 | 25760 3337 3254 11026
esx n/a| 0 0 -2 -23 -32 -33 .14 17 19 | -2893 2854 3267 13450
gfz n/a| -3 0 -5 -18 5 -2 .02 21 19 | 0 2820 3299 11421
grg n/a| 1 0 14 -20 -21 -92 -.48 37 38 | -25077 62768 3299 11606
iac n/a| 1 -1 -7 114 42 90 -.07 21 21 | 7443 2000 3269 10953
mcc n/a| -5 3 51 92 -37 1073 -.75 205 205 | --- --- --- ---
Table 2.1942.6 GPS week: 1942 Day: 6 MJD: 57844
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 3 -21 17 26 .08 27 27 | 2224 1282 3385 11940
cof n/a| 2 0 5 -10 67 29 .15 27 26 | 2234 1265 3384 11939
emx n/a| -2 0 5 -8 -57 -126 .05 21 21 | 14577 1673 3344 11265
esx n/a| 0 0 -3 52 9 49 .13 20 21 | -15524 1281 3351 13988
gfz n/a| -1 0 -8 -17 34 40 .03 21 17 | 0 420 3342 11838
grg n/a| 4 -4 20 -33 66 -130 -.41 31 31 | -87158 169293 3352 11877
iac n/a| 0 1 -8 -1 -36 84 .01 19 19 | 425 719 3342 10975
mcc n/a| 3 6 -9 -76 48 738 .19 140 140 | --- --- --- ---
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 3.1942.0 GPS week: 1942 Day: 0 MJD: 57838
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 705 25 33 23 18 18 40 26 --- 11 | 6 15 6 4 5 6 7 --- 4
R02E | 3230 14 16 15 15 18 38 9 83 8 | 4 3 3 5 4 14 4 6 3
R03E | 629 15 22 14 8 18 22 12 96 6 | 3 5 3 5 4 4 5 7 3
R04E | 1156 14 16 11 21 26 38 14 --- 9 | 3 3 3 6 6 7 4 --- 3
R05E | 830 19 37 24 15 18 29 15 --- 8 | 4 6 3 8 8 5 5 --- 5
R07E | 1239 18 21 25 8 14 24 19 111 8 | 3 3 3 5 4 4 5 4 3
R08E | 1699 22 23 32 13 15 28 18 --- 9 | 3 3 3 5 5 5 6 --- 3
XR09 | 3664 20 19 13 11 16 --- 9 --- 7 | 1 4 1 2 4 --- 2 --- 1
R10 | 1099 29 22 17 16 14 15 11 --- 8 | 1 5 3 4 5 5 2 --- 3
R11 | 1029 25 29 22 12 14 11 16 86 8 | 1 3 2 4 4 2 2 3 2
R13 | 729 18 23 18 28 25 22 18 --- 10 | 2 4 3 6 3 3 1 --- 3
R14 | 2084 26 42 28 31 23 53 21 --- 13 | 2 4 4 6 7 4 3 --- 3
R15 | 970 26 33 23 16 28 22 23 --- 10 | 2 3 3 2 3 2 2 --- 2
R16 | 1663 28 37 56 24 20 44 25 --- 15 | 2 6 4 7 6 4 3 --- 3
R17 | 757 25 22 19 10 18 19 27 --- 9 | 1 2 4 2 5 2 2 --- 1
R18 | 568 16 21 17 13 25 15 14 --- 7 | 1 3 2 4 4 5 2 --- 2
R19 | 1348 37 35 15 12 18 29 15 --- 9 | 1 3 2 5 5 2 2 --- 2
R20 | 1271 20 27 20 36 19 51 17 --- 12 | 2 6 4 4 3 2 4 --- 2
R21 | 847 25 22 22 10 27 20 13 119 9 | 1 2 2 3 2 3 2 1 1
R22 | 559 22 24 16 13 14 16 21 --- 8 | 1 4 2 4 3 2 2 --- 2
R23 | 901 16 19 22 16 20 22 12 --- 8 | 1 3 1 4 3 5 1 --- 2
R24 | 2109 36 57 23 17 25 87 17 --- 15 | 2 4 8 2 4 3 3 --- 2
XR26 | ---- 24 35 --- --- --- --- 17 --- 20 | 3 12 --- --- --- --- 2 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS | 1367 24 29 24 18 20 35 18 100 |T 2 4 3 4 4 4 3 4 2
WRMS | 1367 25 27 24 15 19 30 18 100 |NE 1 3 4 2 4 3 2 --- 1
MEDI | 1029 22 23 20 15 18 24 17 96 |MD 2 4 3 4 4 4 2 4 2
Table 3.1942.1 GPS week: 1942 Day: 1 MJD: 57839
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 893 36 19 24 12 21 30 19 --- 10 | 3 8 6 8 9 7 7 --- 6
R02E | 2839 17 11 28 15 13 22 10 105 8 | 3 6 3 9 7 13 4 19 4
R03E | 1055 15 15 14 9 13 17 11 118 5 | 2 8 3 6 6 4 4 13 4
R04E | 1338 18 22 16 11 25 17 12 --- 7 | 3 5 4 6 6 6 4 --- 4
R05E | 1237 28 49 27 14 28 30 19 --- 10 | 8 11 4 9 7 7 6 --- 5
R07E | 799 24 11 14 8 17 16 12 66 6 | 3 6 4 6 5 5 5 21 4
R08E | 1625 20 17 19 13 16 22 17 --- 7 | 2 6 4 7 5 5 5 --- 4
XR09 | 2941 18 22 13 14 14 --- 13 --- 7 | 1 3 1 2 4 --- 2 --- 1
R10M | 951 27 34 29 13 17 21 17 --- 9 | 2 4 2 4 6 6 4 --- 3
R11M | 786 22 24 15 9 21 17 16 129 7 | 2 5 3 4 5 4 3 8 2
R13 | 711 14 18 17 13 13 30 15 --- 7 | 1 4 2 5 3 5 1 --- 2
R14 | 1833 23 21 19 19 27 54 17 --- 11 | 2 5 4 5 6 4 3 --- 3
R15 | 1358 22 20 26 13 19 26 19 --- 9 | 2 5 3 5 4 6 1 --- 2
R16 | 1748 22 16 40 27 25 43 28 --- 13 | 2 8 4 6 6 5 2 --- 3
R17 | 611 28 31 28 11 26 17 25 --- 10 | 1 4 4 7 7 3 2 --- 3
R18 | 585 17 10 15 12 23 15 14 --- 7 | 1 7 3 8 4 4 2 --- 3
R19M | 1409 46 48 18 15 25 18 14 --- 10 | 1 6 5 7 5 3 3 --- 2
R20M | 1003 23 21 27 32 15 55 20 --- 13 | 3 6 4 7 5 3 2 --- 3
R21 | 514 24 25 28 11 20 15 21 125 9 | 2 3 2 3 4 5 2 7 2
R22 | 581 28 34 18 13 18 34 22 --- 9 | 2 3 3 4 3 6 2 --- 2
R23 | 1050 16 15 21 14 9 39 15 --- 8 | 1 4 3 5 4 7 2 --- 3
R24 | 1610 38 50 43 21 33 80 23 --- 17 | 3 7 7 6 5 3 3 --- 3
XR26 | ---- 21 65 --- --- --- --- 14 --- 17 | 3 47 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1288 25 27 24 16 21 34 18 111 |T 2 7 3 5 5 5 3 13 3
WRMS | 1288 26 27 24 15 20 26 18 111 |NE 1 6 4 7 5 3 2 --- 3
MEDI | 1050 22 21 19 13 19 22 17 118 |MD 2 6 3 6 5 5 3 13 3
Table 3.1942.2 GPS week: 1942 Day: 2 MJD: 57840
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1382 38 25 21 14 24 20 28 --- 11 | 2 4 6 9 10 4 6 --- 5
XR02E | 2726 19 10 20 18 19 --- 12 154 9 | 2 6 3 8 7 --- 6 31 4
R03E | 1234 12 17 17 14 13 15 11 133 6 | 3 8 3 7 5 4 5 20 4
R04E | 668 12 13 19 10 13 28 14 --- 7 | 2 5 4 5 4 5 4 --- 3
R05E | 1059 21 46 26 19 23 40 21 --- 11 | 4 16 6 8 7 8 6 --- 5
R07E | 534 25 22 21 17 22 18 29 252 10 | 3 5 5 7 6 4 5 35 4
R08E | 2296 20 14 18 14 17 21 22 --- 8 | 2 4 4 6 6 4 5 --- 4
XR09M | 2075 21 23 14 6 18 --- 10 --- 7 | 2 2 1 3 4 --- 2 --- 2
R10 | 797 22 17 20 17 19 19 14 --- 8 | 2 4 3 8 5 5 3 --- 3
R11 | 642 28 28 25 9 16 21 30 82 10 | 2 4 4 3 4 6 3 12 2
R13M | 572 16 15 18 11 16 44 16 --- 9 | 1 5 2 3 3 6 2 --- 1
R14M | 709 32 39 19 23 20 34 20 --- 11 | 2 4 3 3 5 7 3 --- 2
R15M | 1255 25 24 17 20 23 21 13 --- 9 | 2 3 3 6 5 6 1 --- 2
R16M | 1010 33 52 23 35 22 55 36 --- 15 | 3 8 4 6 5 6 3 --- 3
R17 | 644 24 27 22 23 23 32 20 --- 10 | 1 3 2 8 7 3 1 --- 3
R18 | 556 24 23 17 13 20 19 14 --- 8 | 1 5 2 8 6 5 2 --- 3
R19 | 1149 53 52 25 21 32 21 25 --- 14 | 2 5 5 6 4 5 2 --- 2
R20M | 632 23 28 29 28 15 65 15 --- 13 | 3 8 4 15 12 5 3 --- 6
R21M | 413 15 22 16 18 10 25 23 113 8 | 1 4 3 5 6 5 2 11 2
R22M | 732 29 26 17 12 21 22 17 --- 9 | 1 3 2 4 4 6 2 --- 2
R23M | 1032 12 14 15 16 11 19 19 --- 7 | 1 4 3 4 4 5 2 --- 2
R24 | 1478 25 31 50 37 29 66 33 --- 18 | 3 5 4 7 5 5 2 --- 3
XR26M | ---- 38 222 --- --- --- --- 33 --- 36 | 5 41 --- --- --- --- 6 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1035 26 29 23 20 20 34 22 159 |T 2 6 3 6 5 5 3 21 3
WRMS | 1035 27 28 23 20 20 31 22 159 |NE 1 4 2 7 6 4 1 --- 3
MEDI | 797 24 24 19 17 19 21 20 133 |MD 2 5 3 6 5 5 3 20 3
Table 3.1942.3 GPS week: 1942 Day: 3 MJD: 57841
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1327 39 38 39 25 31 25 16 --- 13 | 3 8 7 10 9 4 8 --- 6
R02E | 2819 13 14 21 15 16 22 11 94 7 | 2 5 4 5 5 9999 4 5 3
R03E | 2367 15 14 22 17 16 20 14 97 7 | 2 6 5 7 5 5 5 5 4
R04E | 807 10 13 17 17 11 26 13 --- 7 | 2 4 3 6 4 7 4 --- 3
R05E | 1227 14 25 26 21 17 40 15 --- 10 | 3 12 6 11 7 7 4 --- 4
R07E | 798 19 25 17 12 20 19 16 111 7 | 3 6 5 6 8 5 5 7 4
R08E | 1090 22 17 20 13 17 21 17 --- 8 | 2 4 4 8 8 5 5 --- 4
XR09 | 2162 21 28 15 11 21 --- 9 --- 8 | 1 2 2 3 3 --- 2 --- 2
R10 | 677 12 11 23 20 17 44 19 --- 10 | 2 5 4 7 4 7 2 --- 3
R11 | 696 22 27 13 14 18 32 14 96 8 | 4 5 4 5 5 7 4 4 4
R13 | 1363 16 25 14 16 19 16 9 --- 7 | 2 4 3 3 3 4 3 --- 2
R14 | 876 23 33 19 20 11 33 31 --- 10 | 3 10 3 9 4 6 2 --- 3
R15 | 682 24 31 19 26 20 33 14 --- 10 | 2 4 3 6 7 4 2 --- 3
R16 | 795 23 32 37 24 21 43 18 --- 12 | 3 6 6 5 4 4 4 --- 3
R17 | 552 29 26 23 17 25 30 15 --- 10 | 2 3 3 5 5 4 2 --- 2
R18 | 447 21 24 24 13 19 22 26 --- 9 | 1 3 2 4 5 6 2 --- 2
R19 | 613 46 42 40 16 38 21 28 --- 14 | 2 5 5 7 6 4 2 --- 3
R20 | 689 20 35 29 29 26 30 25 --- 12 | 3 11 8 13 11 5 4 --- 6
R21 | 821 23 22 16 11 23 13 12 88 7 | 2 4 3 6 6 3 3 1 3
R22 | 710 20 34 14 13 17 19 18 --- 7 | 1 5 2 4 5 3 2 --- 2
R23 | 969 11 10 12 22 8 39 10 --- 8 | 2 3 2 2 3 3 3 --- 1
R24 | 1098 24 27 40 14 29 64 21 --- 14 | 3 5 5 5 4 5 3 --- 2
XR26 | ---- 22 70 --- --- --- --- 17 --- 19 | 5 12 --- --- --- --- 5 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1168 23 27 25 19 21 31 18 97 |T 2 5 4 6 5 4 3 4 3
WRMS | 1168 24 27 25 18 17 27 18 97 |NE 2 3 3 4 4 5 2 --- 2
MEDI | 807 21 26 20 16 19 26 16 96 |MD 2 5 4 6 5 5 3 5 3
Table 3.1942.4 GPS week: 1942 Day: 4 MJD: 57842
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1156 37 30 31 20 32 27 35 --- 13 | 4 6 6 8 7 4 9 --- 5
R02E | 2004 10 11 16 11 18 24 14 66 7 | 3 6 5 6 6 9999 5 5 4
R03E | 2098 16 14 17 9 21 25 13 72 7 | 3 4 5 6 5 6 5 5 4
R04E | 1070 14 15 24 15 15 24 11 --- 7 | 3 5 6 6 6 7 5 --- 4
R05E | 816 19 25 22 21 22 38 25 --- 11 | 5 10 5 18 12 6 6 --- 8
R07E | 773 20 18 20 15 28 20 18 238 9 | 4 6 6 6 7 7 5 7 5
R08E | 911 23 19 23 16 21 31 22 --- 10 | 3 6 5 8 9 7 5 --- 4
XR09 | 2007 13 12 18 14 28 --- 16 --- 9 | 2 4 3 4 3 --- 2 --- 1
R10 | 528 13 22 17 19 13 29 18 --- 8 | 3 5 5 6 5 6 3 --- 3
R11 | 758 19 22 17 7 27 19 12 180 7 | 6 6 6 7 9 6 6 6 6
R13 | 2090 10 8 12 13 13 29 9 --- 6 | 4 5 4 5 4 4 4 --- 3
R14 | 1850 35 32 29 18 26 48 25 --- 13 | 4 10 4 8 6 3 3 --- 3
R15 | 776 32 32 25 21 32 18 20 --- 11 | 3 4 4 7 9 4 3 --- 4
R16 | 638 24 23 50 15 25 35 24 --- 13 | 4 6 5 5 6 5 3 --- 3
R17 | 770 32 41 22 15 34 21 13 --- 10 | 3 4 4 5 4 3 2 --- 2
R18 | 423 20 22 18 10 15 12 18 --- 7 | 3 4 3 3 3 5 2 --- 2
R19 | 984 40 50 33 13 32 22 27 --- 12 | 3 6 4 8 7 2 1 --- 3
R20 | 728 28 42 35 24 25 60 28 --- 15 | 4 10 8 6 7 4 4 --- 3
R21 | 649 25 32 23 12 24 15 19 129 9 | 3 7 5 5 5 2 3 1 2
R22 | 1183 23 20 12 12 27 14 9 --- 7 | 3 5 3 7 7 4 3 --- 4
R23 | 1273 15 16 15 18 13 21 13 --- 7 | 3 5 3 4 4 2 2 --- 2
R24 | 1791 13 16 38 22 29 61 16 --- 13 | 3 6 5 4 5 4 4 --- 2
XR26 | ---- 24 64 --- --- --- --- 17 --- 21 | 5 11 --- --- --- --- 2 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1226 24 26 26 16 24 31 20 152 |T 3 6 4 6 6 4 3 4 3
WRMS | 1226 24 26 26 16 23 31 20 152 |NE 3 4 4 4 4 4 2 --- 2
MEDI | 911 20 22 22 15 25 24 18 129 |MD 3 6 5 6 6 4 3 5 3
Table 3.1942.5 GPS week: 1942 Day: 5 MJD: 57843
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1761 39 33 40 15 32 36 47 --- 15 | 4 7 7 6 6 5 7 --- 5
R02E | 2078 17 16 21 9 16 21 16 143 7 | 4 8 5 7 7 9999 4 7 4
R03E | 1821 19 17 19 10 18 12 14 157 7 | 5 5 6 8 8 6 5 10 4
R04E | 1860 14 14 21 10 17 22 14 --- 7 | 4 5 7 8 7 5 4 --- 4
R05E | 908 32 33 33 26 25 37 22 --- 12 | 5 10 6 17 14 6 7 --- 8
XR06 | 1571 41 591 --- --- 7672 43 --- --- 42 | 1 1 --- --- 1 1 --- --- 1
R07E | 1027 17 14 20 15 18 24 16 268 8 | 6 9 8 10 9 9 7 14 7
R08E | 1335 25 23 27 20 20 18 15 --- 9 | 4 6 6 6 8 7 4 --- 4
XR09 | 1645 15 20 17 11 17 --- 12 --- 7 | 4 5 4 6 6 --- 2 --- 2
R10 | 827 20 32 25 20 14 21 18 --- 8 | 5 6 6 8 7 7 4 --- 4
R11 | 798 23 20 19 11 29 25 20 258 9 | 8 9 8 10 10 9 7 25 8
R13 | 1044 17 22 22 14 17 19 15 --- 7 | 5 6 5 7 5 6 5 --- 4
R14 | 1703 44 44 28 17 11 42 19 --- 12 | 4 9 6 6 6 3 4 --- 3
R15 | 793 32 29 28 21 20 30 18 --- 11 | 4 5 5 8 8 4 4 --- 3
R16 | 727 25 34 51 24 15 80 20 --- 16 | 5 8 5 11 7 4 3 --- 5
R17 | 665 36 30 20 10 16 12 22 --- 9 | 4 5 4 6 5 5 2 --- 2
R18 | 836 24 22 20 9 21 12 11 --- 7 | 4 4 4 5 5 5 2 --- 2
R19 | 755 50 46 34 19 15 35 20 --- 12 | 4 6 5 8 6 5 1 --- 3
R20 | 566 41 44 59 16 33 70 18 --- 17 | 5 8 7 6 7 4 3 --- 3
R21 | 428 30 29 22 19 23 22 25 166 10 | 4 7 5 7 8 4 3 8 3
R22 | 871 27 30 22 14 20 23 18 --- 9 | 4 5 5 10 6 8 4 --- 4
R23 | 1844 22 30 24 26 12 19 9 --- 8 | 4 6 5 5 5 4 2 --- 2
R24 | 2507 21 30 44 22 22 80 29 --- 16 | 5 9 7 10 9 4 3 --- 5
XR26 | ---- 23 99 --- --- --- --- 17 --- 20 | 4 16 --- --- --- --- 2 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS | 1327 29 30 31 17 21 37 21 205 |T 4 6 5 7 6 5 3 12 3
WRMS | 1327 31 32 31 19 19 38 21 205 |NE 4 6 5 7 6 4 2 --- 3
MEDI | 1027 24 30 22 15 18 23 18 166 |MD 4 6 5 7 7 5 4 10 4
Table 3.1942.6 GPS week: 1942 Day: 6 MJD: 57844
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1887 29 29 24 20 30 30 21 --- 11 | 5 7 6 6 6 5 9 --- 4
R02E | 1503 17 24 16 15 19 30 15 66 8 | 4 7 4 6 6 9999 5 10 3
R03E | 1169 19 22 18 10 23 21 14 107 8 | 5 6 5 7 7 5 5 15 4
R04E | 1278 18 21 18 17 18 21 11 --- 7 | 5 5 6 7 7 5 5 --- 4
R05E | 1388 24 28 24 27 25 36 22 --- 11 | 5 9 6 10 10 5 7 --- 5
R06 | 713 17 15 17 13 16 17 18 --- 7 | 9999 1 9999 9999 9999 1 1 --- 1
R07E | 864 13 13 12 11 14 20 16 144 6 | 9 9 10 10 10 9 8 22 8
R08E | 731 20 25 20 12 15 27 11 --- 7 | 5 6 5 7 7 5 5 --- 4
XR09 | 2252 10 12 12 14 12 --- 11 --- 6 | 4 4 4 5 5 --- 2 --- 1
R10 | 665 16 11 16 22 10 19 14 --- 7 | 5 5 5 6 6 5 4 --- 3
R11 | 588 19 19 12 16 18 18 13 239 7 | 10 10 10 10 10 9 9 40 9
R13 | 1064 16 17 19 11 22 35 21 --- 9 | 6 6 6 7 6 6 5 --- 5
R14 | 2048 57 44 27 37 16 39 24 --- 15 | 4 7 5 5 5 3 4 --- 2
R15 | 1089 26 27 17 16 19 31 12 --- 9 | 4 4 5 5 5 4 3 --- 2
R16 | 568 18 21 25 22 16 43 13 --- 10 | 5 6 5 9 6 4 4 --- 4
R17 | 610 20 21 16 14 13 18 30 --- 9 | 4 4 4 5 5 4 1 --- 2
R18 | 932 13 10 13 19 15 14 20 --- 7 | 4 4 4 5 5 4 2 --- 2
R19 | 1369 48 52 26 19 31 42 33 --- 14 | 4 5 5 5 5 4 2 --- 2
R20 | 898 40 45 25 25 31 46 24 --- 14 | 5 6 5 5 5 2 2 --- 2
R21 | 740 27 29 17 8 29 16 17 70 9 | 4 5 4 6 7 3 2 13 3
R22 | 556 36 34 29 19 32 16 25 --- 12 | 4 4 4 7 5 6 4 --- 3
R23 | 1017 27 21 19 29 9 16 8 --- 9 | 4 4 5 4 4 4 1 --- 1
R24 | 1810 30 19 31 36 22 70 20 --- 16 | 6 6 6 8 6 3 3 --- 3
XR26 | ---- 19 51 --- --- --- --- 16 --- 17 | 4 13 --- --- --- --- 2 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS | 1153 27 27 21 20 21 31 19 140 |T 5 5 5 6 6 4 3 20 3
WRMS | 1153 27 26 21 21 17 31 19 140 |NE 4 4 4 6 5 3 2 --- 2
MEDI | 1017 19 21 18 17 18 21 16 107 |MD 5 6 5 6 6 4 4 15 3
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