[IGSREPORT-27113] Wk 2092 IGLOS Final Orbits
acc
acc at igs.org
Mon Mar 2 03:14:14 PST 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2092 (Feb 09, 2020 - Feb 15, 2020)
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 2.2092.
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:
igl2092[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2092 in the SP3 format.
igl20927.sum Combination Report for GPS Week 2092.
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 | -4.9 ns
1 | -4.0 ns
2 | -3.0 ns
3 | -4.2 ns
4 | -3.9 ns
5 | -4.4 ns
6 | -2.8 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 1.2092, 1a.2092).
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 2.2092.0-6)
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 3.2092.0-6).
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 2092 summary. (Feb 09, 2020 - Feb 15, 2020)
Table 1.2092.a GPS week : 2092 MJD: 58888.0-58894.0
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 -2 3 -8 65 .06 20 18 | 19610 32 3018 8269
| 1 0 2 15 10 22 .03 | 483 2071
cof n/a| 1 0 -2 7 12 64 .05 23 20 | 19606 28 3016 8267
| 1 0 2 29 13 30 .06 | 486 2086
emx n/a| 1 0 5 24 -5 -32 .09 31 31 | -8187 350 2998 8414
| 1 1 3 18 25 33 .03 | 10424 1465
esx n/a| 0 1 0 9 -8 -41 .09 32 29 | -10810 1272 3018 10268
| 0 2 2 32 18 20 .04 | 11833 1841
gfz n/a| 0 -1 -1 -19 11 -21 .13 22 16 | 0 -60 3064 7861
| 1 0 2 20 21 24 .08 | 0 1819
grg n/a| 0 0 3 -33 5 -12 -.43 30 26 | -3880 129 3012 7459
| 0 1 8 15 21 104 .07 | 610 1721
iac n/a| 0 0 0 20 2 -12 -.05 20 18 | -2409 -100 3020 8438
| 1 0 2 25 26 43 .05 | 516 1638
mcc n/a| 1 4 -11 29 -124 -179 -.61 290 290 | --- --- --- ---
| 13 13 16 267 187 827 .31 | --- ---
Table 1.2092.b GPS week : 2092 MJD: 58888.0-58894.0
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 | 19 18 14 20 19 20 15 |
R02 | 20 9 7 8 7 9 7 |
R03 | 8 13 9 8 7 7 7 |
R04 | 12 9 10 8 8 9 9 |
R05 | 11 9 10 8 10 10 8 |
R07 | 20 11 7 7 8 8 9 |
R08 | 13 11 9 8 7 7 7 |
R09 | 7 7 7 6 6 7 8 |
R11 | 6 6 6 7 11 7 5 |
R12 | 10 8 9 11 12 10 10 |
R13 | 17 15 17 16 15 13 13 |
R14 | 7 7 8 7 6 8 6 |
R15 | 9 10 8 9 9 6 6 |
R16 | 12 11 12 15 12 12 10 |
R17 | 8 7 7 10 11 8 9 |
R18 | 8 8 8 8 7 8 8 |
R19 | 23 22 21 19 19 19 19 |
R20 | 18 20 17 17 15 18 15 |
R21 | 12 10 10 9 7 11 9 |
R22 | 12 11 8 9 10 9 11 |
R23 | 7 11 9 10 8 8 8 |
R26 | 13 32 39 27 21 13 23 |
Table 1.2092.c GPS week : 2092 MJD: 58888.0-58894.0
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 2092 0 | 4 -9 210 1258 537 1240 82.7 1421 1421 | -4934 0
brd 2092 1 | 38 29 211 -541 -1044 4490 81.7 1574 1574 | -4011 0
brd 2092 2 | 38 81 122 503 -70 4104 83.4 1424 1424 | -3048 0
brd 2092 3 | 24 99 148 -1917 1014 920 80.7 1445 1445 | -4215 0
brd 2092 4 | -36 5 140 -35 -281 3058 83.0 1507 1507 | -3863 0
brd 2092 5 | 20 71 155 -215 2226 1705 82.7 1363 1363 | -4380 0
brd 2092 6 | -18 54 104 385 1712 -898 81.1 1371 1371 | -2789 0
-------------+------------------------------------------------------------+----------------
brd 2092 mean| 10 47 156 -80 584 2088 82.2 1443 1443 | -3891 0
brd 2092 sdev| 28 40 41 996 1153 1911 1.0 74 74 | 749 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 2.2092.0 GPS week: 2092 Day: 0 MJD: 58888
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 -2 11 -15 56 .09 23 17 | 19358 -1100 2912 8462
cof n/a| 1 0 -7 -36 -6 64 .14 23 18 | 19352 -1099 2918 8460
emx n/a| 2 0 5 22 15 -89 .03 29 28 | -7085 -17 2901 8623
esx n/a| 0 2 -3 -31 -21 -48 .05 32 29 | 10964 584 2920 9781
gfz n/a| 0 0 0 -24 27 -46 -.00 32 21 | 0 -1509 2971 8217
grg n/a| -1 -1 -2 -36 -30 149 -.46 36 33 | -4431 -1119 2907 7871
iac n/a| 0 0 3 54 3 -10 -.07 27 27 | -3364 567 2927 8621
mcc n/a| -15 -4 -20 329 -338 -104 -.63 408 408 | --- --- --- ---
Table 2.2092.1 GPS week: 2092 Day: 1 MJD: 58889
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 -16 0 71 .07 19 15 | 19371 -2109 2994 8438
cof n/a| 2 0 1 59 22 88 -.03 24 19 | 19390 -2164 2993 8439
emx n/a| 2 0 7 42 23 -41 .12 33 33 | 5039 -1384 2956 8481
esx n/a| 0 3 4 36 -20 -62 .17 35 30 | -12385 -699 2976 10351
gfz n/a| 1 -2 0 -14 -15 -48 .10 20 15 | 0 -1025 3027 8063
grg n/a| 0 1 -6 -39 4 75 -.36 35 30 | -3403 -1050 2995 7831
iac n/a| -1 0 0 16 7 -36 -.09 23 22 | -2321 -547 2995 8503
mcc n/a| -9 30 -21 -389 -105 -743 -1.04 312 312 | --- --- --- ---
Table 2.2092.2 GPS week: 2092 Day: 2 MJD: 58890
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 -1 1 35 .04 21 18 | 18980 1912 3047 7624
cof n/a| 0 0 0 -6 20 27 .03 24 21 | 18957 1936 3049 7622
emx n/a| 0 -1 9 15 -49 -27 .10 31 31 | -12583 1004 3038 7622
esx n/a| -2 4 1 -22 -25 -32 .12 31 28 | -14042 2633 3056 9240
gfz n/a| 0 -1 -4 -16 -7 -36 .18 23 13 | 0 1796 3113 7169
grg n/a| 0 2 -5 -14 -11 -5 -.34 25 19 | -3693 1235 3059 7031
iac n/a| 0 0 2 20 58 37 -.05 18 16 | -1890 917 3054 7754
mcc n/a| 12 1 -37 -151 -265 -1547 -.32 204 204 | --- --- --- ---
Table 2.2092.3 GPS week: 2092 Day: 3 MJD: 58891
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 -1 25 -3 48 .08 23 23 | 19456 -414 3252 7597
cof n/a| 4 0 0 26 16 55 .07 26 25 | 19451 -408 3245 7595
emx n/a| 0 0 7 15 15 -3 .10 37 37 | -24687 -484 3219 7732
esx n/a| 0 3 2 53 -10 -52 .07 33 29 | -1417 936 3226 9715
gfz n/a| 1 -2 -3 -58 17 12 .15 23 14 | 0 -975 3265 7243
grg n/a| 0 0 4 -56 19 7 -.36 25 21 | -3951 -288 3229 6752
iac n/a| -1 0 -1 38 -8 -12 -.07 17 15 | -2655 -1041 3225 7717
mcc n/a| 26 12 3 313 168 -559 -.56 252 252 | --- --- --- ---
Table 2.2092.4 GPS week: 2092 Day: 4 MJD: 58892
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 -3 17 -29 81 .06 19 18 | 19991 1811 2785 8602
cof n/a| 0 0 -1 12 2 105 .02 24 22 | 19982 1815 2780 8601
emx n/a| 1 -3 4 2 -18 -23 .06 33 33 | -12453 1775 2780 8896
esx n/a| 0 -1 0 37 28 -52 .08 34 31 | -22877 3259 2833 10935
gfz n/a| -1 0 -2 -23 48 -13 .09 18 15 | 0 1239 2852 8001
grg n/a| 0 0 12 -44 2 -45 -.49 28 25 | -4910 2192 2797 7475
iac n/a| -1 1 -4 35 -15 -64 .07 19 17 | -2376 1662 2806 8935
mcc n/a| -1 -6 -10 73 -297 307 -.12 248 248 | --- --- --- ---
Table 2.2092.5 GPS week: 2092 Day: 5 MJD: 58893
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 -3 -15 -6 102 .01 19 15 | 20455 -2485 3052 8731
cof n/a| 2 1 -2 -2 29 82 .01 21 17 | 20454 -2492 3047 8730
emx n/a| 0 0 2 55 -17 11 .09 29 30 | -10103 -985 3026 8934
esx n/a| -1 0 0 2 -4 0 .05 33 30 | -15032 -1140 3041 11015
gfz n/a| -1 -1 -2 0 2 6 .23 20 15 | 0 -2303 3087 8077
grg n/a| 0 0 11 -11 25 -122 -.52 31 28 | -3142 -2170 3063 7721
iac n/a| -1 0 0 -8 -24 -53 -.05 19 17 | -2438 -3170 3056 8944
mcc n/a| 1 5 11 -140 -76 728 -.71 274 274 | --- --- --- ---
Table 2.2092.6 GPS week: 2092 Day: 6 MJD: 58894
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 -6 7 -4 62 .04 17 17 | 19661 2611 3090 8429
cof n/a| 1 0 -4 0 1 26 .10 20 20 | 19662 2610 3083 8428
emx n/a| 2 0 -1 13 -7 -56 .11 28 28 | 4559 2542 3072 8616
esx n/a| 0 0 -2 -4 -6 -46 .08 29 28 | -20885 3334 3080 10843
gfz n/a| 0 -2 2 2 10 -23 .15 22 18 | 0 2355 3137 8262
grg n/a| 0 1 12 -33 30 -146 -.49 30 28 | -3631 2105 3039 7538
iac n/a| 1 0 0 -15 -1 49 -.05 16 15 | -1820 906 3077 8597
mcc n/a| 0 -6 -2 169 39 664 -.86 332 332 | --- --- --- ---
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 3.2092.0 GPS week: 2092 Day: 0 MJD: 58888
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 | 812 44 32 53 38 35 58 28 --- 19 | 81 76 77 73 80 93 64 --- 71
R02E | 1141 31 30 35 13 64 41 62 279 20 | 84 102 84 90 110 109 80 70 86
R03E | 472 16 21 25 13 20 19 15 405 8 | 162 164 160 164 169 169 159 105 162
XR04E | 2006 18 20 26 16 --- 32 29 --- 12 | 84 80 85 86 --- 89 94 --- 86
R05E | 2022 14 24 28 24 26 27 25 --- 10 | 65 67 69 71 68 69 69 --- 65
R07E | 721 32 35 34 18 75 39 48 710 20 | 187 193 183 198 219 203 210 128 196
R08E | 2760 21 27 39 24 23 38 20 --- 12 | 156 155 148 150 161 153 158 --- 153
R09 | 1060 12 16 11 13 15 25 14 --- 6 | 24 24 25 28 30 33 30 --- 24
R11 | 1128 9 12 15 14 11 17 13 147 6 | 48 50 42 43 50 56 47 52 47
R12 | 587 17 28 18 40 9 15 20 --- 9 | 92 95 73 59 79 87 87 --- 80
R13 | 2661 43 23 21 30 50 41 24 --- 16 | 82 83 61 46 66 72 67 --- 64
R14 | 922 17 16 11 19 12 19 13 --- 7 | 64 64 47 45 51 65 52 --- 54
R15 | 1743 12 9 15 30 12 29 18 --- 8 | 78 77 67 54 71 87 80 --- 72
R16 | 659 23 33 24 26 27 41 15 --- 11 | 50 49 42 67 63 65 50 --- 53
R17 | 1509 19 15 21 26 13 19 8 --- 8 | 35 39 33 29 32 41 34 --- 33
R18 | 744 11 16 22 15 16 20 15 --- 7 | 21 24 21 23 26 21 28 --- 20
R19 | 949 32 34 38 85 44 59 39 --- 22 | 36 40 30 47 37 43 50 --- 32
R20 | 805 22 26 60 19 27 64 36 --- 18 | 26 31 26 32 39 36 42 --- 26
R21 | 742 9 10 22 48 14 26 32 256 12 | 42 45 36 38 47 48 51 83 41
R22 | 2361 7 8 20 42 19 36 23 --- 11 | 39 38 31 26 38 42 37 --- 33
R23 | 1153 9 11 13 25 15 15 13 --- 7 | 22 26 23 32 36 26 24 --- 25
XR26 | ---- 11 31 --- --- --- --- 15 --- 13 | 22 35 --- --- --- --- 27 --- 16
------+---------------------------------------------------+-----------------------------------------------
RMS | 1421 23 23 29 32 32 36 27 408 |T 68 70 64 66 73 76 70 87 65
WRMS | 1421 17 18 28 29 21 33 27 408 |NE 45 48 39 40 47 51 47 67 41
MEDI | 1060 17 21 22 24 19 29 20 279 |MD 50 50 47 47 51 65 51 83 53
Table 3.2092.1 GPS week: 2092 Day: 1 MJD: 58889
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 | 588 41 37 40 40 39 54 26 --- 18 | 77 76 72 78 83 85 67 --- 73
R02E | 1117 13 16 37 11 15 23 14 297 8 | 50 50 47 42 54 45 44 52 45
R03E | 523 16 16 35 29 17 25 45 279 12 | 155 159 162 168 165 158 153 131 158
XR04E | 1392 15 21 28 17 --- 16 12 --- 9 | 59 61 54 63 --- 69 57 --- 59
R05E | 2107 14 25 32 20 22 13 12 --- 8 | 74 82 74 79 83 79 79 --- 76
R07E | 855 19 13 30 23 14 34 25 491 10 | 183 184 180 184 177 184 183 76 181
R08E | 3329 17 17 32 19 20 32 28 --- 10 | 113 119 105 120 116 123 102 --- 111
R09 | 1538 15 18 16 15 8 13 24 --- 7 | 19 18 24 27 27 23 28 --- 20
R11 | 766 8 8 12 10 18 19 14 109 6 | 31 30 27 30 40 28 33 28 30
R12 | 842 20 26 23 24 10 15 14 --- 8 | 69 65 51 45 58 58 60 --- 58
R13 | 1553 41 57 28 47 30 37 12 --- 15 | 56 77 47 44 66 55 52 --- 51
R14 | 2186 10 10 15 9 11 31 13 --- 6 | 38 37 31 32 29 55 32 --- 33
R15 | 1093 20 20 16 44 14 14 14 --- 9 | 49 48 43 34 44 48 42 --- 41
R16 | 866 21 34 26 29 20 40 16 --- 11 | 20 34 32 37 30 48 35 --- 28
R17 | 1602 11 19 23 24 12 18 14 --- 7 | 29 33 28 28 25 24 34 --- 26
R18 | 1495 10 11 28 10 14 21 22 --- 8 | 19 22 19 23 22 19 25 --- 17
R19 | 2008 29 31 43 90 32 42 53 --- 21 | 22 37 28 40 30 27 31 --- 15
R20 | 776 9 16 85 28 23 84 16 --- 19 | 21 23 35 26 30 34 29 --- 21
R21 | 520 8 10 26 40 14 17 22 258 9 | 22 23 26 28 24 25 28 60 21
R22 | 2602 8 13 23 48 17 27 18 --- 10 | 21 26 23 18 26 20 23 --- 19
R23 | 1453 11 18 13 36 21 45 16 --- 10 | 22 26 24 22 32 29 27 --- 21
XR26 | ---- 28 45 --- --- --- --- 36 --- 32 | 30 44 --- --- --- --- 27 --- 18
------+---------------------------------------------------+-----------------------------------------------
RMS | 1573 19 24 33 35 20 35 23 312 |T 53 57 53 55 58 58 54 69 51
WRMS | 1573 15 19 33 30 15 30 22 312 |NE 31 36 31 31 34 35 33 44 27
MEDI | 1392 15 18 28 24 17 25 16 279 |MD 31 37 35 37 32 48 34 60 30
Table 3.2092.2 GPS week: 2092 Day: 2 MJD: 58890
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 | 860 40 40 39 33 29 16 21 --- 13 | 62 60 49 33 49 51 39 --- 41
R02E | 1558 10 17 26 13 15 13 18 181 7 | 41 37 35 41 49 42 41 51 38
R03E | 726 13 15 36 15 21 16 13 252 8 | 97 97 102 100 108 98 106 110 101
XR04E | 1270 16 16 24 12 --- 25 15 --- 9 | 37 38 34 30 --- 45 38 --- 34
R05E | 1622 16 15 36 15 20 25 16 --- 9 | 60 59 68 59 65 60 66 --- 61
R07E | 1317 14 19 26 17 18 9 10 189 7 | 126 129 126 129 128 122 143 156 128
R08E | 3199 11 11 32 17 13 28 13 --- 8 | 75 71 69 72 79 81 80 --- 75
R09 | 1101 11 18 28 15 12 11 17 --- 7 | 20 26 30 21 24 27 23 --- 18
R11 | 841 13 13 10 18 6 11 18 158 6 | 32 33 38 35 36 42 48 31 37
R12 | 780 22 19 26 21 21 17 19 --- 9 | 69 69 49 66 72 66 54 --- 60
R13 | 811 48 53 22 48 52 27 20 --- 17 | 68 71 51 39 42 60 70 --- 53
R14 | 2021 18 13 18 29 9 18 12 --- 8 | 54 49 32 37 46 49 51 --- 45
R15 | 683 18 24 14 25 10 18 15 --- 7 | 66 71 57 51 57 69 52 --- 57
R16 | 663 20 19 30 22 30 39 21 --- 12 | 39 38 41 43 48 50 31 --- 38
R17 | 1005 14 16 17 20 15 8 13 --- 6 | 19 22 20 21 20 20 25 --- 17
R18 | 1424 9 13 24 23 22 10 19 --- 8 | 18 22 19 24 26 16 24 --- 16
R19 | 2257 26 32 49 88 33 34 39 --- 20 | 27 39 43 28 39 23 38 --- 24
R20 | 647 29 39 60 20 20 65 14 --- 17 | 24 34 33 31 29 24 23 --- 22
R21 | 863 8 8 32 33 27 17 14 225 10 | 28 31 26 35 44 30 36 65 32
R22 | 1991 6 8 23 27 14 14 17 --- 7 | 25 26 27 28 26 26 27 --- 23
R23 | 900 19 25 23 25 19 26 10 --- 9 | 19 21 24 30 31 16 19 --- 19
XR26 | ---- 40 48 --- --- --- --- 37 --- 38 | 33 45 --- --- --- --- 34 --- 16
------+---------------------------------------------------+-----------------------------------------------
RMS | 1424 21 24 31 31 23 25 18 204 |T 47 49 46 45 50 48 48 82 43
WRMS | 1424 18 21 31 28 13 19 16 204 |NE 36 39 35 34 38 37 37 48 31
MEDI | 1005 16 17 26 21 19 17 16 189 |MD 37 38 38 35 44 45 38 65 37
Table 3.2092.3 GPS week: 2092 Day: 3 MJD: 58891
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 | 1005 39 42 70 54 51 25 35 --- 20 | 93 102 101 120 123 108 81 --- 97
R02E | 1532 13 19 28 13 13 15 18 122 7 | 70 76 72 72 74 59 62 125 67
R03E | 545 14 15 31 17 16 15 11 372 7 | 97 96 88 96 101 90 100 365 95
XR04E | 676 15 16 30 14 --- 14 11 --- 8 | 33 33 25 34 --- 30 26 --- 28
R05E | 430 16 20 35 15 17 19 11 --- 8 | 88 93 87 89 90 100 87 --- 88
R07E | 963 13 12 26 16 16 17 9 282 7 | 107 108 109 104 108 120 112 278 108
R08E | 3157 14 15 26 16 15 23 13 --- 8 | 52 53 54 58 64 56 56 --- 55
R09 | 1083 13 19 11 14 12 11 16 --- 6 | 18 18 20 21 33 18 31 --- 22
R11 | 1646 18 20 23 13 13 19 13 134 7 | 39 39 31 45 57 56 56 35 48
R12 | 1899 24 26 49 30 10 14 18 --- 11 | 63 63 44 51 57 52 58 --- 52
R13 | 1149 42 38 36 36 43 30 26 --- 16 | 64 70 61 46 81 67 53 --- 59
R14 | 2349 13 21 18 17 14 15 10 --- 6 | 50 57 33 41 53 43 48 --- 45
R15 | 546 24 26 24 37 13 11 9 --- 9 | 64 62 52 32 41 51 48 --- 47
R16 | 1015 36 47 33 27 42 44 13 --- 15 | 42 55 43 46 49 43 35 --- 38
R17 | 706 9 18 23 40 15 32 16 --- 10 | 23 30 24 20 28 40 32 --- 24
R18 | 1051 13 16 16 13 12 21 19 --- 7 | 17 21 19 20 22 24 21 --- 14
R19 | 1991 26 36 63 80 29 32 24 --- 18 | 30 40 41 36 45 38 35 --- 33
R20 | 1406 39 33 66 22 20 57 15 --- 16 | 24 27 33 29 31 32 35 --- 23
R21 | 649 9 11 25 42 12 14 16 256 9 | 30 31 31 21 27 31 32 115 26
R22 | 1536 10 8 29 33 15 19 10 --- 8 | 27 26 29 27 29 26 30 --- 26
R23 | 1020 29 26 33 30 14 16 13 --- 10 | 17 20 26 38 37 18 28 --- 23
XR26 | ---- 33 56 --- --- --- --- 22 --- 27 | 26 49 --- --- --- --- 22 --- 16
------+---------------------------------------------------+-----------------------------------------------
RMS | 1445 23 26 37 33 23 25 17 252 |T 48 53 48 49 57 52 49 183 47
WRMS | 1445 23 25 37 29 14 21 15 252 |NE 35 40 34 33 42 38 37 75 33
MEDI | 1051 15 20 29 22 15 19 13 256 |MD 39 49 41 41 49 43 35 125 38
Table 3.2092.4 GPS week: 2092 Day: 4 MJD: 58892
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 | 588 36 47 64 59 36 25 31 --- 18 | 55 66 58 84 83 57 54 --- 58
R02E | 2272 8 14 23 9 15 20 17 77 7 | 50 52 51 52 52 62 43 56 49
R03E | 818 14 17 25 11 9 15 20 112 7 | 56 54 48 49 55 51 66 128 54
XR04E | 1294 10 19 27 13 --- 16 11 --- 7 | 36 40 33 35 --- 38 42 --- 35
R05E | 523 15 17 36 13 25 18 16 --- 9 | 57 56 61 64 67 60 59 --- 59
R07E | 675 11 11 29 17 15 16 12 424 7 | 68 67 68 60 65 68 65 255 64
R08E | 3073 15 13 23 13 16 15 10 --- 7 | 54 51 48 59 58 53 53 --- 53
R09 | 951 11 13 17 17 14 16 11 --- 6 | 21 25 29 19 32 22 19 --- 20
XR11 | 8729 13 11 22 --- 19 38 18 118 11 | 30 30 28 --- 25 57 47 56 33
R12 | 2433 13 17 42 36 14 39 23 --- 12 | 58 59 45 53 57 82 75 --- 59
R13 | 1032 31 41 29 39 29 51 20 --- 14 | 67 75 58 36 65 64 64 --- 59
R14 | 1413 8 19 15 17 10 16 13 --- 5 | 52 60 43 47 57 39 57 --- 50
R15 | 873 12 19 15 35 16 18 20 --- 8 | 56 57 45 46 67 58 55 --- 55
R16 | 953 31 31 28 28 24 25 17 --- 11 | 31 29 31 37 37 25 41 --- 29
R17 | 1060 11 14 22 47 12 14 28 --- 10 | 24 27 21 23 22 26 36 --- 20
R18 | 1451 10 15 18 18 14 21 16 --- 7 | 18 23 19 28 29 20 24 --- 17
R19 | 2044 30 38 62 81 19 31 29 --- 18 | 31 37 39 33 30 27 31 --- 25
R20 | 1940 31 38 46 14 12 65 22 --- 15 | 30 36 29 27 40 29 29 --- 27
R21 | 1005 7 11 22 30 14 16 7 220 7 | 22 25 21 22 25 28 29 160 22
R22 | 1547 10 13 27 48 15 21 12 --- 10 | 26 27 20 25 23 22 22 --- 20
R23 | 806 19 17 26 18 12 15 18 --- 8 | 21 25 29 28 28 26 29 --- 23
XR26 | ---- 21 47 --- --- --- --- 20 --- 20 | 20 46 --- --- --- --- 25 --- 17
------+---------------------------------------------------+-----------------------------------------------
RMS | 1507 19 24 33 34 18 28 19 248 |T 40 43 39 41 45 43 43 131 38
WRMS | 1507 18 22 33 31 15 25 17 248 |NE 33 38 32 32 38 37 38 108 31
MEDI | 1060 13 17 26 18 15 18 17 118 |MD 31 40 39 36 40 39 42 128 33
Table 3.2092.5 GPS week: 2092 Day: 5 MJD: 58893
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 | 1058 42 31 49 47 55 36 27 --- 19 | 74 71 64 59 86 63 63 --- 63
R02E | 1167 9 11 25 13 17 26 22 107 8 | 35 35 31 37 42 43 31 64 33
R03E | 1297 8 14 27 20 12 15 11 107 7 | 103 104 99 103 102 103 102 146 101
XR04E | 1751 10 12 24 19 --- 17 20 --- 9 | 56 56 53 55 --- 63 60 --- 56
R05E | 781 14 20 27 19 26 24 19 --- 9 | 58 59 56 53 61 60 62 --- 56
R07E | 613 14 17 28 14 18 22 15 561 8 | 120 125 118 127 132 133 130 127 126
R08E | 2018 15 16 22 11 11 12 15 --- 6 | 91 89 93 88 91 99 102 --- 94
R09 | 805 14 20 20 16 10 17 12 --- 6 | 25 25 30 26 21 27 26 --- 21
R11 | 1076 7 8 11 21 12 26 13 102 6 | 30 34 30 27 36 43 25 29 29
R12 | 2272 17 20 17 31 13 27 22 --- 9 | 52 48 41 40 48 61 56 --- 48
R13 | 1412 20 26 38 45 12 38 18 --- 12 | 52 58 47 36 42 57 58 --- 46
R14 | 1319 13 10 18 20 11 20 19 --- 7 | 51 47 37 38 41 36 61 --- 44
R15 | 615 11 7 15 22 10 16 10 --- 6 | 56 57 56 56 59 64 65 --- 59
R16 | 1024 30 29 16 46 24 23 22 --- 12 | 38 38 41 57 40 35 37 --- 35
R17 | 874 14 12 23 30 17 13 15 --- 8 | 16 19 19 22 21 16 15 --- 15
R18 | 1687 13 18 22 21 20 21 11 --- 8 | 19 20 21 25 26 29 22 --- 21
R19 | 1627 31 32 50 84 18 50 27 --- 19 | 25 36 33 29 32 42 25 --- 20
R20 | 2439 30 44 50 12 17 82 33 --- 18 | 19 40 25 21 27 53 21 --- 17
R21 | 809 11 13 32 44 23 16 23 161 11 | 17 22 19 23 32 22 29 83 21
R22 | 1617 8 12 28 36 12 29 12 --- 9 | 17 19 18 18 20 26 19 --- 16
R23 | 553 8 11 22 22 13 23 14 --- 7 | 17 20 17 20 24 22 22 --- 16
XR26 | ---- 12 32 --- --- --- --- 13 --- 13 | 25 31 --- --- --- --- 26 --- 17
------+---------------------------------------------------+-----------------------------------------------
RMS | 1362 19 21 29 33 20 31 19 274 |T 45 47 45 45 49 52 48 89 43
WRMS | 1362 15 17 30 30 15 28 17 274 |NE 30 34 31 31 33 38 33 56 28
MEDI | 1167 13 16 24 21 13 23 15 107 |MD 35 38 37 37 40 43 31 83 33
Table 3.2092.6 GPS week: 2092 Day: 6 MJD: 58894
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 | 1714 23 23 45 40 40 32 27 --- 15 | 73 74 71 72 91 81 65 --- 70
R02E | 1184 11 9 25 11 15 13 12 133 6 | 45 47 41 44 47 46 40 67 42
R03E | 2649 8 10 28 15 19 17 11 154 7 | 116 116 108 113 120 117 111 140 113
XR04E | 1568 8 14 26 18 --- 18 19 --- 9 | 79 82 74 76 --- 87 75 --- 77
R05E | 660 14 17 28 20 15 19 14 --- 8 | 61 61 60 58 60 63 61 --- 59
R07E | 570 11 14 33 19 24 18 14 699 9 | 133 134 133 132 133 144 138 80 134
R08E | 1320 11 13 27 9 17 20 12 --- 7 | 121 123 118 120 123 136 127 --- 123
R09 | 758 15 17 20 9 21 22 17 --- 8 | 30 30 31 28 30 33 31 --- 27
R11 | 676 7 13 9 9 8 17 11 114 4 | 48 47 45 42 48 55 48 56 47
R12 | 1464 21 30 17 34 16 17 19 --- 9 | 81 84 69 55 70 79 76 --- 71
R13 | 1515 22 21 24 37 30 54 13 --- 13 | 82 85 62 53 63 75 64 --- 66
R14 | 1354 12 19 18 15 12 18 8 --- 6 | 68 72 50 53 54 56 65 --- 59
R15 | 1446 10 12 9 22 18 12 11 --- 6 | 81 84 73 68 73 83 84 --- 77
R16 | 1171 20 28 11 19 29 39 15 --- 10 | 46 47 48 58 57 60 50 --- 50
R17 | 952 21 21 18 33 18 15 10 --- 8 | 31 33 22 24 29 29 26 --- 24
R18 | 944 11 13 21 22 17 25 11 --- 7 | 22 21 18 23 18 31 24 --- 19
R19 | 1704 32 41 51 70 23 49 33 --- 19 | 42 51 39 30 43 48 45 --- 35
R20 | 2161 32 31 39 15 31 63 15 --- 15 | 25 24 23 20 22 20 27 --- 19
R21 | 698 6 7 29 36 16 22 16 91 9 | 35 39 31 29 42 40 43 115 35
R22 | 1641 8 11 34 36 21 29 19 --- 10 | 36 35 27 29 41 46 37 --- 34
R23 | 618 10 17 18 26 16 17 14 --- 7 | 21 23 24 33 35 24 18 --- 22
XR26 | ---- 21 53 --- --- --- --- 23 --- 22 | 49 73 --- --- --- --- 27 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1370 17 20 28 29 22 30 16 332 |T 60 62 55 55 59 64 58 91 56
WRMS | 1370 17 20 28 28 18 28 15 332 |NE 46 49 40 38 44 48 44 85 40
MEDI | 1320 11 17 25 20 18 19 14 133 |MD 48 51 48 53 48 56 48 80 47
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