[IGSREPORT-28719] Wk 2211 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 13 02:59:28 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2211 (May 22, 2022 - May 28, 2022)
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 2.2211.
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:
igl2211[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2211 in the SP3 format.
igl22117.sum Combination Report for GPS Week 2211.
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/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
https://files.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 | -1.4 ns
1 | 1.2 ns
2 | -0.3 ns
3 | 0.5 ns
4 | -0.1 ns
5 | 1.0 ns
6 | -1.5 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 1.2211, 1a.2211).
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 2.2211.0-6)
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 3.2211.0-6).
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 2211 summary. (May 22, 2022 - May 28, 2022)
Table 1.2211.a GPS week : 2211 MJD: 59721.0-59727.0
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 -1 -17 -27 13 .12 21 17 | 36562 -152 3306 8674
| 0 0 1 9 14 31 .05 | 490 1845
emx n/a| 0 0 -3 20 -1 -28 -.08 50 32 | -5271 392 3239 8365
| 2 2 2 30 32 43 .05 | 9906 1014
esx n/a| 0 0 -1 49 16 10 -.09 40 27 | -4041 905 3250 11140
| 1 1 1 10 16 29 .04 | 11353 1890
gfz n/a| -1 0 1 -11 5 11 -.06 30 16 | 0 -417 3269 8267
| 1 1 3 20 19 22 .04 | 0 1956
grg n/a| 2 -1 5 -34 33 -41 .30 32 23 | -108 -305 3237 7940
| 1 1 2 22 21 52 .03 | 219 1693
iac n/a| 0 0 -4 19 4 14 -.24 24 23 | 1978 -220 3247 9113
| 2 1 3 32 29 64 .05 | 644 1004
Table 1.2211.b GPS week : 2211 MJD: 59721.0-59727.0
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 | 15 16 15 17 13 15 17 |
R02 | 8 7 7 8 6 6 11 |
R03 | 9 7 7 9 7 6 8 |
R04 | 10 10 8 7 8 7 9 |
R05 | 8 6 8 9 9 9 11 |
R07 | 7 7 5 7 8 6 5 |
R08 | 7 6 6 7 9 6 7 |
R09 | 7 7 8 7 7 9 9 |
R11 | 10 9 9 6 10 9 9 |
R12 | 8 7 9 7 7 7 7 |
R13 | 19 18 20 18 14 19 19 |
R14 | 8 7 6 7 8 8 9 |
R15 | 8 8 7 8 6 8 8 |
R17 | 8 14 10 8 9 9 10 |
R18 | 8 8 7 9 9 10 9 |
R19 | 24 26 26 22 27 24 24 |
R20 | 26 25 25 26 23 28 29 |
R21 | 8 8 9 9 10 8 8 |
R22 | 37 33 32 31 30 30 31 |
R24 | 11 9 10 13 12 12 12 |
Table 1.2211.c GPS week : 2211 MJD: 59721.0-59727.0
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 2211 0 | 65 5 157 -1499 -1756 9753 82.2 1744 1744 | -1353 0
brd 2211 1 | -43 78 180 -2968 -332 13070 82.7 1347 1347 | 1232 0
brd 2211 2 | 31 -10 175 -458 449 2216 84.4 1275 1275 | -256 0
brd 2211 3 | -4 10 140 -324 -238 2055 81.8 1395 1395 | 521 0
brd 2211 4 | 1 -13 134 146 1344 -142 82.1 1538 1538 | -132 0
brd 2211 5 | -5 -62 227 2349 954 -449 80.6 1594 1594 | 969 0
brd 2211 6 | -42 -6 105 -318 -1066 3933 82.2 1435 1435 | -1486 0
-------------+------------------------------------------------------------+----------------
brd 2211 mean| 0 0 160 -438 -92 4347 82.3 1475 1475 | -72 0
brd 2211 sdev| 38 42 39 1615 1099 5138 1.1 160 160 | 1065 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 2.2211.0 GPS week: 2211 Day: 0 MJD: 59721
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 -8 -31 -15 .09 17 14 | 35669 -2735 3386 8521
emx n/a| 1 -1 -7 55 -16 -101 -.14 49 32 | 11621 -809 3285 8394
esx n/a| -1 0 -2 61 11 25 -.10 32 23 | 1235 -1526 3359 10588
gfz n/a| 0 0 -4 -23 16 -10 -.06 26 18 | 0 -2655 3344 8185
grg n/a| 1 0 9 -35 0 2 .25 28 21 | -179 -2561 3341 7816
iac n/a| 1 0 -1 14 34 20 -.29 24 22 | 859 -1588 3337 8866
Table 2.2211.1 GPS week: 2211 Day: 1 MJD: 59722
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 0 -5 -26 40 .06 16 13 | 36662 2012 3643 9742
emx n/a| -2 3 -3 7 34 -23 -.11 50 30 | -16458 1521 3575 9301
esx n/a| 0 2 -1 36 49 55 -.14 45 31 | -1438 3440 3587 12114
gfz n/a| -1 -1 0 -36 -14 5 -.01 32 16 | 0 1804 3654 9047
grg n/a| 0 -2 8 -4 36 -14 .28 33 23 | 23 1762 3536 8970
iac n/a| 5 -1 -5 39 11 -64 -.25 29 29 | 2831 862 3578 10241
Table 2.2211.2 GPS week: 2211 Day: 2 MJD: 59723
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 -20 -7 46 .23 22 16 | 36576 -568 3145 8641
emx n/a| -1 4 -2 -23 31 11 -.04 51 31 | -16294 -332 3087 8333
esx n/a| 0 0 -1 56 14 19 -.09 42 27 | 13358 866 3092 10873
gfz n/a| 0 0 0 26 13 51 -.05 30 15 | 0 -1008 3138 8331
grg n/a| 0 -2 2 -14 33 -63 .34 34 24 | 50 -1128 3081 8081
iac n/a| 0 -1 0 -34 -30 -59 -.26 21 20 | 1612 -474 3084 9152
Table 2.2211.3 GPS week: 2211 Day: 3 MJD: 59724
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 -18 -23 3 .14 23 17 | 37291 1074 3477 8137
emx n/a| 2 0 -2 16 -54 18 -.00 47 35 | -6520 1414 3405 7839
esx n/a| 0 0 -3 52 -1 -40 -.05 39 28 | -17299 2118 3391 10916
gfz n/a| -3 0 0 -9 -17 25 -.03 30 14 | 0 501 3413 7670
grg n/a| 2 0 4 -34 56 -19 .32 31 21 | -63 863 3396 7444
iac n/a| 1 0 0 -11 46 41 -.32 24 22 | 2369 199 3387 8626
Table 2.2211.4 GPS week: 2211 Day: 4 MJD: 59725
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 -46 -24 .11 20 17 | 36641 -214 3099 9097
emx n/a| 2 -1 -7 0 -27 -64 -.10 48 31 | -1987 -403 3037 8740
esx n/a| 0 1 0 33 26 1 -.03 39 30 | -19032 546 3057 11991
gfz n/a| -1 1 7 0 -1 -3 -.05 28 17 | 0 57 3074 8672
grg n/a| 2 -2 5 -42 50 -148 .33 37 25 | -299 5 3063 8215
iac n/a| -1 -1 -2 36 -17 125 -.24 22 19 | 2239 5 3058 9520
Table 2.2211.5 GPS week: 2211 Day: 5 MJD: 59726
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 1 -32 -14 -7 .11 22 20 | 36327 1599 3056 7770
emx n/a| 1 0 -1 60 3 -40 -.12 52 35 | -8056 1416 3003 7437
esx n/a| 2 -2 -1 51 8 15 -.15 41 29 | -6509 2329 2982 9932
gfz n/a| -1 0 2 -23 2 -6 -.06 31 13 | 0 1569 2994 7554
grg n/a| 3 -4 4 -33 51 -1 .29 32 23 | 171 1133 2959 6947
iac n/a| -2 3 -8 52 -23 25 -.17 23 23 | 2250 893 2995 8231
Table 2.2211.6 GPS week: 2211 Day: 6 MJD: 59727
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 0 -20 -44 49 .12 25 19 | 36774 -2234 3340 8813
emx n/a| -1 0 -2 29 15 3 -.07 50 33 | 793 -60 3286 8515
esx n/a| 0 -1 -1 52 8 -1 -.07 40 25 | 1394 -1438 3284 11570
gfz n/a| 0 2 4 -13 39 19 -.12 34 18 | 0 -3187 3268 8416
grg n/a| 3 0 5 -74 8 -45 .29 30 23 | -461 -2212 3288 8112
iac n/a| 0 0 -9 40 13 15 -.19 25 24 | 1687 -1439 3294 9159
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 3.2211.0 GPS week: 2211 Day: 0 MJD: 59721
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 620 23 25 40 35 35 39 15 | 85 60 55 68 69 103 73
R02 | 4184 11 25 17 13 11 27 7 | 59 50 61 65 66 84 64
R03 | 664 9 21 17 24 13 34 9 | 68 59 69 82 77 75 70
XR04 | 834 19 26 14 --- 18 24 10 | 65 65 51 --- 50 51 55
R05 | 806 18 23 18 13 18 21 8 | 50 60 52 54 58 54 51
R07 | 750 15 19 16 20 10 12 7 | 60 53 70 76 69 65 65
R08 | 891 15 17 10 13 21 19 7 | 60 50 63 66 76 56 61
R09E | 4399 11 16 17 19 17 15 7 | 18 24 29 38 24 32 24
XR11E | 3343 --- 19 10 19 30 17 10 | --- 26 28 40 27 24 28
R12E | 860 10 26 16 17 19 17 7 | 38 29 37 46 45 40 38
R13E | 1171 34 58 37 58 33 38 18 | 68 62 69 94 67 63 66
R14E | 975 9 18 18 14 17 25 7 | 71 66 75 72 73 68 70
R15E | 1279 11 29 15 18 16 18 7 | 156 152 158 158 156 152 155
R17 | 832 8 39 16 17 9 16 7 | 76 51 70 86 82 86 76
R18 | 887 15 34 17 15 21 11 8 | 66 46 68 61 65 67 62
R19 | 709 26 122 52 42 65 29 24 | 99 31 64 115 97 94 86
R20 | 1559 29 102 89 43 58 18 25 | 111 54 51 126 127 104 97
R21 | 851 11 30 16 16 20 22 8 | 70 50 61 69 75 66 66
XR22 | 2026 37 --- 116 68 85 54 36 | 38 --- 104 32 52 55 36
R24 | 1474 14 54 25 15 20 26 11 | 81 45 68 82 93 91 78
------+-----------------------------------------+-------------------------------------
RMS | 1744 17 49 32 26 28 24 |T 70 54 65 75 72 71 66
WRMS | 1744 14 32 23 18 21 22 |NE 70 51 64 75 75 75 67
MEDI | 887 15 26 17 18 19 21 |MD 68 51 63 69 69 66 65
Table 3.2211.1 GPS week: 2211 Day: 1 MJD: 59722
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 687 19 21 54 30 40 48 16 | 63 52 32 54 54 90 58
R02 | 1875 10 15 12 12 10 24 6 | 40 37 45 49 49 59 44
R03 | 758 11 16 11 8 17 22 6 | 46 45 50 43 53 41 45
XR04 | 559 14 25 25 --- 12 23 9 | 48 53 38 --- 42 40 42
R05 | 727 12 18 16 15 13 13 6 | 34 38 32 34 44 35 33
R07 | 1019 7 19 15 19 17 17 6 | 42 40 45 54 44 42 43
R08 | 816 9 14 20 16 12 13 6 | 43 42 56 49 47 37 44
R09E | 3523 11 19 9 20 16 22 7 | 16 26 23 38 26 31 22
XR11E | 3125 --- 20 11 17 19 17 8 | --- 25 24 35 24 29 25
R12E | 1235 8 28 13 15 15 22 7 | 32 29 35 39 36 40 33
R13E | 860 22 60 45 61 33 27 18 | 52 42 68 83 56 49 52
R14E | 1025 13 18 20 9 15 18 6 | 54 53 60 57 56 62 55
R15E | 1801 16 24 21 11 15 23 8 | 136 139 135 135 143 130 135
R17 | 906 15 31 13 25 21 63 14 | 34 26 33 43 39 67 33
R18 | 915 13 34 14 16 14 14 7 | 39 32 32 44 34 33 34
R19 | 781 25 138 43 31 78 30 25 | 49 35 44 53 60 53 45
R20 | 946 29 98 94 54 42 24 25 | 57 37 33 67 63 44 48
R21 | 839 13 26 17 16 22 15 7 | 41 32 38 39 49 34 37
R22 | 1082 22 72 132 86 79 50 33 | 43 70 69 43 39 43 34
R24 | 1351 13 43 16 12 14 21 8 | 35 36 33 34 37 33 32
------+-----------------------------------------+-------------------------------------
RMS | 1346 16 50 45 32 33 29 |T 47 44 46 52 49 49 44
WRMS | 1346 13 30 31 16 23 29 |NE 43 41 41 46 46 46 40
MEDI | 915 13 24 16 16 16 22 |MD 43 37 38 44 44 41 42
Table 3.2211.2 GPS week: 2211 Day: 2 MJD: 59723
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 578 33 24 31 39 40 32 15 | 67 50 50 73 38 62 55
R02 | 1843 12 15 16 8 14 20 6 | 47 45 52 48 44 65 49
R03 | 787 7 13 13 19 12 22 7 | 57 49 49 55 60 64 55
XR04 | 610 7 15 27 --- 10 14 7 | 53 55 42 --- 52 54 49
R05 | 1101 14 24 26 12 18 15 8 | 40 48 47 50 41 36 39
R07 | 734 9 14 14 9 10 13 5 | 48 44 41 49 52 51 46
R08 | 917 13 12 10 10 14 17 6 | 42 46 43 43 45 34 39
R09E | 2683 12 16 8 19 16 25 7 | 17 25 27 32 23 30 22
XR11E | 3295 --- 17 10 16 25 18 9 | --- 24 27 32 27 26 23
R12E | 1368 14 35 20 17 17 15 8 | 34 29 39 41 39 42 34
R13E | 838 25 47 31 74 41 32 19 | 37 47 41 95 42 44 38
R14E | 841 10 23 16 10 16 12 6 | 41 36 37 43 50 46 41
R15E | 2245 13 26 17 13 13 14 7 | 64 67 63 70 70 70 66
R17 | 808 10 39 20 10 14 32 9 | 55 41 50 57 65 75 57
R18 | 875 10 32 17 11 11 16 7 | 47 39 58 49 56 47 47
R19 | 574 44 132 43 31 78 27 26 | 69 27 52 70 54 64 55
R20 | 776 33 92 102 31 49 27 25 | 79 41 33 69 75 71 59
R21 | 607 14 34 17 20 27 15 9 | 51 35 43 50 55 42 45
R22 | 865 51 86 120 70 77 19 32 | 28 64 81 34 30 40 33
R24 | 1825 10 51 16 21 18 13 9 | 58 38 62 71 72 52 58
------+-----------------------------------------+-------------------------------------
RMS | 1275 22 51 42 30 34 21 |T 49 42 46 54 49 50 45
WRMS | 1275 16 31 27 15 24 20 |NE 52 44 50 55 52 54 49
MEDI | 841 13 24 17 17 16 17 |MD 48 41 43 50 50 47 46
Table 3.2211.3 GPS week: 2211 Day: 3 MJD: 59724
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 799 38 27 54 24 41 29 16 | 71 53 34 68 34 60 49
R02 | 1750 9 10 9 23 18 27 8 | 43 42 47 61 44 42 44
R03 | 738 18 17 14 21 18 22 8 | 55 58 69 79 74 77 68
XR04 | 991 6 13 14 --- 13 21 7 | 52 49 45 --- 53 68 53
R05 | 776 17 23 22 18 15 26 9 | 42 49 63 56 50 65 52
R07 | 1067 6 17 14 9 13 28 7 | 50 51 46 52 53 74 53
R08 | 629 13 15 9 10 22 14 6 | 40 38 46 51 63 51 47
R09E | 2995 12 16 16 15 16 20 7 | 22 30 26 28 30 33 24
XR11E | 3375 --- 12 9 8 15 12 5 | --- 27 25 28 23 26 24
R12E | 1258 13 31 15 13 9 9 6 | 33 27 33 34 37 33 30
R13E | 929 34 59 33 61 18 26 18 | 39 26 41 90 45 41 40
R14E | 1563 15 22 13 17 14 15 7 | 33 32 36 38 38 34 33
R15E | 2441 11 29 17 10 14 22 7 | 93 93 92 95 94 87 91
R17 | 983 6 37 11 11 17 16 7 | 54 33 54 54 66 52 52
R18 | 1295 10 39 18 19 22 15 9 | 51 29 54 51 64 50 49
R19 | 535 39 106 31 28 59 25 21 | 89 74 58 76 56 66 64
R20 | 1183 40 95 92 40 34 38 25 | 85 51 51 89 80 83 69
R21 | 516 11 34 18 21 16 19 8 | 41 32 31 46 40 37 35
R22 | 678 47 63 102 76 80 40 31 | 36 56 71 37 28 48 29
R24 | 1937 14 54 19 18 36 26 12 | 53 35 50 47 75 64 51
------+-----------------------------------------+-------------------------------------
RMS | 1395 23 47 39 30 31 24 |T 51 44 48 56 52 54 47
WRMS | 1395 17 35 28 14 21 22 |NE 54 46 51 59 55 59 51
MEDI | 991 13 27 16 18 17 22 |MD 50 38 46 52 50 51 49
Table 3.2211.4 GPS week: 2211 Day: 4 MJD: 59725
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 665 26 28 43 27 28 18 13 | 67 68 51 66 60 63 60
R02 | 1993 9 14 5 20 16 14 6 | 52 46 47 62 58 48 50
R03 | 529 14 21 20 19 12 12 7 | 56 55 71 76 69 64 63
XR04 | 1280 7 12 22 --- 20 18 8 | 55 55 52 --- 50 58 52
R05 | 1125 21 15 16 18 16 24 8 | 42 45 54 61 48 63 50
R07 | 1260 8 26 17 22 19 16 7 | 57 52 58 71 63 62 59
R08 | 780 18 21 17 21 23 17 8 | 49 51 63 67 69 47 54
R09E | 3539 15 21 11 15 16 18 7 | 23 25 27 32 26 32 24
XR11E | 3818 --- 16 11 21 26 22 10 | --- 26 25 32 25 25 23
R12E | 598 11 25 14 19 17 14 7 | 31 26 26 38 38 26 27
R13E | 2069 22 41 33 43 31 19 13 | 43 47 51 69 45 38 41
R14E | 1580 11 23 17 12 20 19 7 | 36 32 33 32 39 39 33
R15E | 2769 8 26 14 10 17 12 6 | 55 51 61 60 58 54 55
R17 | 778 12 32 12 14 27 23 8 | 46 37 38 45 61 40 41
R18 | 1410 14 34 26 20 25 11 9 | 41 29 40 33 50 33 34
R19 | 1076 36 124 42 43 89 39 26 | 59 45 62 80 52 65 57
R20 | 1034 31 96 79 28 40 40 23 | 71 41 39 65 68 80 58
R21 | 487 12 43 24 16 17 26 10 | 51 37 48 50 58 55 49
R22 | 712 37 52 112 71 92 21 30 | 56 54 49 48 65 47 42
R24 | 1236 22 58 20 12 20 21 11 | 45 39 59 48 62 44 46
------+-----------------------------------------+-------------------------------------
RMS | 1538 20 48 39 28 37 22 |T 49 43 47 54 53 49 45
WRMS | 1538 17 31 30 17 25 19 |NE 53 46 52 59 59 54 51
MEDI | 1125 14 26 17 20 20 18 |MD 51 45 49 60 58 47 49
Table 3.2211.5 GPS week: 2211 Day: 5 MJD: 59726
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 398 38 32 41 34 25 28 15 | 54 46 43 44 42 38 38
R02 | 1648 10 13 16 11 18 16 6 | 43 39 44 43 50 37 41
R03 | 500 8 11 15 8 16 19 6 | 54 49 56 47 50 48 49
XR04 | 956 11 16 9 --- 22 10 7 | 51 51 41 --- 38 44 44
R05 | 1322 19 14 26 21 14 14 8 | 36 47 57 50 37 34 40
R07 | 707 11 18 10 10 11 14 5 | 50 50 46 42 49 50 46
R08 | 726 10 13 13 11 14 19 6 | 38 33 38 42 42 42 37
R09E | 4249 13 27 15 19 17 29 9 | 19 25 23 29 25 39 23
XR11E | 3673 --- 22 16 8 24 19 9 | --- 23 25 24 25 24 21
R12E | 649 9 27 12 13 12 16 6 | 31 26 29 37 41 27 30
R13E | 2183 34 52 44 61 29 38 19 | 42 40 55 80 57 46 43
R14E | 1479 16 28 16 14 14 17 7 | 50 45 45 49 52 55 48
R15E | 2636 12 33 15 16 15 20 8 | 90 91 96 96 96 87 91
R17 | 1437 9 31 19 13 18 30 9 | 36 31 39 28 43 33 33
R18 | 909 5 49 17 13 30 23 10 | 40 38 42 43 56 50 43
R19 | 868 31 107 44 36 82 22 23 | 42 40 42 53 50 48 41
R20 | 974 32 114 97 68 38 23 27 | 53 29 40 87 66 59 54
R21 | 639 9 36 13 9 21 20 8 | 35 28 31 36 43 34 33
R22 | 1342 47 86 110 64 70 31 30 | 36 58 47 41 27 35 28
R24 | 803 15 68 25 14 19 27 12 | 46 31 35 48 45 53 42
------+-----------------------------------------+-------------------------------------
RMS | 1594 22 52 41 31 32 23 |T 44 41 43 48 46 44 41
WRMS | 1594 20 35 29 13 23 23 |NE 43 40 42 46 45 43 40
MEDI | 956 12 28 16 14 18 20 |MD 42 39 42 43 43 42 41
Table 3.2211.6 GPS week: 2211 Day: 6 MJD: 59727
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 505 46 32 47 38 23 27 16 | 87 69 56 73 64 76 68
R02 | 1282 14 11 10 24 17 42 10 | 55 47 54 65 60 64 54
R03 | 571 10 11 13 12 26 18 7 | 69 60 70 69 80 65 68
XR04 | 604 19 18 11 --- 19 19 9 | 67 64 53 --- 57 59 59
R05 | 1439 25 18 21 35 11 21 10 | 48 55 62 74 53 61 55
R07 | 772 6 12 15 12 10 13 5 | 70 66 66 78 72 74 71
R08 | 1180 9 14 12 8 22 19 7 | 57 54 69 61 80 56 62
R09E | 3273 14 19 10 17 19 27 8 | 21 26 30 35 26 35 25
XR11E | 2419 --- 14 16 14 14 21 8 | --- 26 27 32 24 27 23
R12E | 609 9 29 13 18 12 18 7 | 37 33 33 41 42 36 35
R13E | 1518 34 50 42 65 34 30 19 | 34 43 52 70 40 39 36
R14E | 929 14 23 19 22 9 25 8 | 73 71 80 82 77 70 73
R15E | 2390 11 31 18 19 16 14 8 | 88 93 87 94 91 90 89
R17 | 1346 10 36 22 22 11 27 9 | 57 39 47 63 59 61 53
R18 | 744 13 31 15 13 18 28 9 | 55 42 63 58 59 66 56
R19 | 751 40 122 50 43 43 25 24 | 86 38 56 93 82 70 67
R20 | 2020 29 116 93 63 60 28 29 | 112 66 42 125 124 111 97
R21 | 779 10 30 13 24 18 11 8 | 45 31 37 43 48 43 40
R22 | 1556 58 55 103 70 76 28 30 | 45 58 71 55 42 50 32
R24 | 861 17 65 22 12 17 20 11 | 62 29 49 58 64 68 56
------+-----------------------------------------+-------------------------------------
RMS | 1434 25 50 40 34 30 25 |T 61 50 55 66 62 61 55
WRMS | 1434 19 33 25 18 23 24 |NE 65 51 56 70 67 66 59
MEDI | 929 14 29 16 22 18 21 |MD 57 47 54 65 59 61 56
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