[IGSREPORT-28521] Wk 2197 IGLOS Final Orbits
acc
acc at igs.org
Tue Mar 8 04:02:55 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2197 (Feb 13, 2022 - Feb 19, 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 2.2197.
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:
igl2197[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2197 in the SP3 format.
igl21977.sum Combination Report for GPS Week 2197.
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 | 2.0 ns
1 | -1.7 ns
2 | 1.5 ns
3 | 0.7 ns
4 | 2.1 ns
5 | -4.6 ns
6 | -6.0 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 1.2197, 1a.2197).
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 2.2197.0-6)
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 3.2197.0-6).
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 2197 summary. (Feb 13, 2022 - Feb 19, 2022)
Table 1.2197.a GPS week : 2197 MJD: 59623.0-59629.0
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 5 3 -4 47 .13 24 20 | 19801 1044 3484 8978
| 1 0 2 12 20 18 .05 | 4431 3755
emx n/a| -1 1 -10 6 40 -8 -.05 44 34 | 1180 1154 3504 8932
| 1 1 6 34 38 30 .09 | 9692 2376
esx n/a| -1 0 -1 -1 -20 -44 -.15 35 24 | 6188 929 3479 9675
| 0 1 2 16 16 41 .06 | 7944 3900
gfz n/a| 0 0 4 -11 1 -29 -.17 30 17 | 0 1314 3480 8729
| 2 0 2 25 23 19 .07 | 0 3862
grg n/a| 1 -4 -3 -6 5 55 .25 29 23 | -1662 1274 3475 8606
| 0 2 4 20 16 45 .07 | 2045 3799
iac n/a| 2 6 0 46 24 -121 -.25 31 29 | -2866 -697 3092 8702
| 0 1 0 8 24 59 .05 | 852 1004
mcc n/a| -7 2 -9 -1 30 360 -1.06 214 214 | --- --- --- ---
| 13 15 68 160 164 310 .98 | --- ---
Table 1.2197.b GPS week : 2197 MJD: 59623.0-59629.0
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 | 18 22 22 23 21 16 15 |
R02 | 10 12 9 9 10 8 9 |
R03 | 10 10 10 14 10 9 10 |
R04 | 11 10 11 15 11 8 9 |
R05 | 10 13 10 13 12 9 9 |
R07 | 7 10 12 10 10 8 11 |
R08 | 9 8 12 11 11 9 10 |
R09 | 8 8 9 10 8 7 7 |
R11 | 9 13 12 11 9 12 7 |
R12 | 6 7 10 5 6 9 9 |
R13 | 18 18 19 20 12 12 18 |
R14 | 6 8 7 7 6 9 10 |
R15 | 7 8 7 6 6 8 8 |
R17 | 12 9 9 9 9 8 9 |
R18 | 10 10 10 10 8 9 9 |
R19 | 22 24 30 33 31 21 19 |
R20 | 36 34 32 32 36 31 30 |
R21 | 9 10 11 11 10 13 10 |
R22 | 28 27 25 29 26 24 27 |
R24 | 12 15 16 13 14 12 11 |
Table 1.2197.c GPS week : 2197 MJD: 59623.0-59629.0
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 2197 0 | -22 49 -48 -436 519 -3831 79.9 1396 1396 | 1953 0
brd 2197 1 | -34 -1 -21 -817 642 -10180 80.7 1266 1266 | -1671 0
brd 2197 2 | -6 -88 -21 -40 -3719 -18030 80.3 1550 1550 | 1491 0
brd 2197 3 | 50 -54 66 -1290 -2074 -15790 79.0 1923 1923 | 649 0
brd 2197 4 | -39 0 119 -2033 -606 -10160 81.2 1858 1858 | 2109 0
brd 2197 5 | -8 -69 47 -2454 -995 -12040 82.8 2082 2082 | -4586 0
brd 2197 6 | 62 -49 160 -476 1029 -9703 83.6 1842 1842 | -5956 0
-------------+------------------------------------------------------------+----------------
brd 2197 mean| 0 -30 43 -1078 -743 -11390 81.1 1702 1702 | -858 0
brd 2197 sdev| 40 48 78 891 1701 4597 1.6 301 301 | 3292 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 2.2197.0 GPS week: 2197 Day: 0 MJD: 59623
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 25 22 25 .09 20 15 | 13901 4492 4157 9894
emx n/a| -2 0 -2 -25 1 -22 -.05 42 32 | -1296 2544 4234 9822
esx n/a| 0 0 -1 10 -41 -27 -.17 36 24 | 13296 4773 4150 9083
gfz n/a| 1 -1 3 8 23 -22 -.16 30 18 | 0 4830 4125 9502
grg n/a| 2 -2 -8 -31 0 0 .28 30 23 | -621 4479 4175 9816
mcc n/a| -10 -10 -48 72 21 113 -1.81 285 285 | --- --- --- ---
Table 2.2197.1 GPS week: 2197 Day: 1 MJD: 59624
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 2 1 62 .10 25 24 | 15128 -940 4190 10859
emx n/a| -2 1 -3 57 42 -54 -.04 44 34 | -6890 -216 4217 10868
esx n/a| -1 -1 0 20 -41 -76 -.25 35 26 | 15222 -1148 4190 12614
gfz n/a| 2 0 2 -2 15 -47 -.14 30 17 | 0 -1292 4210 10604
grg n/a| 2 -2 -9 -18 5 62 .28 27 23 | -1341 -1197 4188 10746
mcc n/a| -12 -10 -10 204 269 569 -1.41 134 134 | --- --- --- ---
Table 2.2197.2 GPS week: 2197 Day: 2 MJD: 59625
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 8 12 1 61 .20 26 21 | 17423 6602 3170 9266
emx n/a| -2 2 -9 42 37 23 .03 44 35 | -11609 4578 3206 9205
esx n/a| 0 1 -1 -5 -28 -47 -.16 38 28 | 1452 6541 3185 8843
gfz n/a| -1 0 8 -43 -41 -9 -.29 28 20 | 0 6945 3192 8750
grg n/a| 1 -1 -5 -24 34 -14 .25 28 21 | -2136 6907 3155 8880
mcc n/a| -34 8 -24 -149 238 712 -2.19 201 201 | --- --- --- ---
Table 2.2197.3 GPS week: 2197 Day: 3 MJD: 59626
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 5 5 4 40 .14 23 19 | 23027 -53 3528 7841
emx n/a| 0 3 -20 21 66 13 -.23 46 36 | 4233 943 3533 7795
esx n/a| -1 1 -1 -30 -7 -78 -.07 37 25 | 14313 -580 3536 9710
gfz n/a| 0 0 2 -37 -13 -59 -.09 32 16 | 0 289 3548 7594
grg n/a| 0 -6 2 17 2 78 .11 31 24 | 449 -37 3531 7084
mcc n/a| -6 -11 -68 -126 -166 362 -1.75 268 268 | --- --- --- ---
Table 2.2197.4 GPS week: 2197 Day: 4 MJD: 59627
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 4 -8 -23 48 .16 28 22 | 25917 1965 3122 8562
emx n/a| -1 0 -15 -23 106 -42 -.04 44 34 | 18864 2646 3084 8293
esx n/a| -2 1 -5 -4 -3 -33 -.17 31 23 | -4477 2250 3102 10867
gfz n/a| 0 0 3 26 5 -31 -.18 30 16 | 0 2723 3100 8563
grg n/a| 1 -6 2 -10 -4 68 .22 27 26 | 597 3006 3110 8165
mcc n/a| 1 -1 -73 -163 -58 606 -.52 196 196 | --- --- --- ---
Table 2.2197.5 GPS week: 2197 Day: 5 MJD: 59628
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 5 -1 1 70 .08 24 18 | 22370 117 3331 8568
emx n/a| -1 -1 -12 -8 -4 11 .03 43 35 | 3800 364 3360 8554
esx n/a| -3 1 -1 -10 -14 -82 -.11 33 23 | 3351 -339 3332 8996
gfz n/a| -3 0 5 -28 -2 -5 -.12 30 15 | 0 268 3354 8494
grg n/a| 1 -6 -4 0 -15 108 .29 29 23 | -4678 201 3313 8066
iac n/a| 2 5 0 40 42 -79 -.22 30 28 | -2264 13 3318 9080
mcc n/a| 6 30 117 202 -6 336 .46 240 240 | --- --- --- ---
Table 2.2197.6 GPS week: 2197 Day: 6 MJD: 59629
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 -8 -38 23 .18 26 18 | 20846 -4873 2893 7861
emx n/a| -3 4 -10 -21 30 8 -.08 44 35 | 1158 -2777 2895 7991
esx n/a| -1 0 -3 9 -7 34 -.13 36 22 | 161 -4991 2863 7612
gfz n/a| -1 1 7 -3 23 -32 -.26 29 16 | 0 -4562 2837 7602
grg n/a| 1 -4 -1 20 19 83 .35 27 20 | -3905 -4438 2855 7485
iac n/a| 3 6 0 52 7 -163 -.28 32 30 | -3469 -1407 2866 8324
mcc n/a| 1 11 39 -48 -84 -178 -.22 175 175 | --- --- --- ---
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 3.2197.0 GPS week: 2197 Day: 0 MJD: 59623
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg mcc IGL | cod emx esx gfz grg mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1687 31 47 44 40 19 --- 18 | 81 66 81 90 72 --- 74
R02E | 1366 6 35 15 21 16 --- 9 | 60 57 63 65 67 --- 61
R03E | 992 13 33 21 14 18 --- 9 | 84 81 82 85 88 --- 82
XR04E | 4811 8 26 24 --- 18 --- 10 | 46 44 46 --- 52 --- 45
R05E | 2551 19 24 16 21 13 294 9 | 71 68 56 67 75 167 66
R07E | 1756 11 25 12 16 9 --- 7 | 162 165 168 166 170 --- 166
R08E | 1563 11 29 19 17 17 --- 9 | 71 73 70 71 74 --- 70
R09 | 1137 13 9 9 20 20 --- 7 | 20 23 23 31 19 --- 20
XR11 | 1120 10 --- 19 16 13 --- 8 | 10 --- 23 21 25 --- 17
R12 | 1001 10 15 10 14 10 313 6 | 23 15 26 24 15 315 17
R13 | 932 30 19 34 37 48 --- 17 | 23 27 27 27 28 --- 20
R14 | 1145 7 20 14 9 8 --- 5 | 14 23 18 16 16 --- 14
R15 | 558 7 16 13 13 16 368 6 | 16 18 19 16 24 272 16
R17 | 561 15 36 25 20 26 --- 12 | 74 48 60 76 83 --- 68
R18 | 1380 11 38 19 11 25 --- 10 | 57 39 73 66 79 --- 62
R19 | 1278 30 82 39 21 48 --- 22 | 94 41 40 81 90 --- 65
R20 | 1158 25 104 84 89 54 --- 35 | 104 32 48 141 120 --- 88
R21 | 1630 14 32 13 11 16 --- 8 | 80 53 64 77 83 --- 72
R22 | 1971 41 33 89 33 70 --- 28 | 61 78 127 76 73 --- 71
R24 | 904 13 48 25 20 16 77 12 | 84 40 56 82 83 59 71
------+-----------------------------------------+-------------------------------------
RMS | 1396 20 42 36 30 30 285 |T 61 52 58 67 66 203 58
WRMS | 1396 15 32 24 18 23 285 |NE 50 36 46 56 56 215 46
MEDI | 1158 13 32 19 20 17 294 |MD 61 44 56 71 73 167 65
Table 3.2197.1 GPS week: 2197 Day: 1 MJD: 59624
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg mcc IGL | cod emx esx gfz grg mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 957 38 51 47 53 33 --- 22 | 92 60 74 93 75 --- 74
R02E | 877 18 36 21 27 15 --- 11 | 53 49 64 70 71 --- 60
R03E | 1539 13 32 14 17 17 --- 9 | 102 101 103 108 109 --- 104
XR04E | 4817 11 32 13 --- 13 --- 10 | 43 43 41 --- 46 --- 42
R05E | 2080 17 28 30 25 26 112 12 | 47 40 53 54 50 159 46
R07E | 1311 24 24 13 18 18 --- 10 | 158 156 159 155 158 --- 156
R08E | 1658 11 24 14 13 13 --- 7 | 78 73 84 80 85 --- 79
R09 | 1214 16 11 15 13 21 --- 8 | 22 23 26 30 14 --- 19
XR11 | 1133 14 --- 24 13 30 --- 12 | 20 --- 32 24 16 --- 17
R12 | 595 14 16 12 11 13 187 6 | 13 16 23 20 20 92 15
R13 | 582 34 20 40 33 39 --- 17 | 20 28 16 20 16 --- 12
R14 | 718 14 11 9 18 18 --- 7 | 15 25 21 24 18 --- 16
R15 | 829 16 17 16 18 9 143 7 | 16 23 24 28 14 153 18
R17 | 871 16 30 15 16 11 --- 9 | 46 35 37 47 42 --- 40
R18 | 1042 13 30 16 15 22 --- 9 | 38 32 43 34 53 --- 38
R19 | 1558 45 93 31 40 26 --- 24 | 64 44 40 57 53 --- 43
R20 | 1567 43 95 74 76 54 --- 33 | 68 39 35 73 83 --- 53
R21 | 1792 9 37 15 26 13 --- 10 | 45 36 42 64 48 --- 46
R22 | 1334 39 47 87 23 52 --- 27 | 47 53 92 61 41 --- 50
R24 | 954 17 62 25 19 25 63 15 | 50 33 33 49 57 15 42
------+-----------------------------------------+-------------------------------------
RMS | 1266 25 44 35 30 27 134 |T 51 47 52 57 53 104 48
WRMS | 1266 24 34 26 17 23 134 |NE 35 32 35 40 36 86 31
MEDI | 1133 16 30 16 18 18 112 |MD 46 39 40 54 48 92 42
Table 3.2197.2 GPS week: 2197 Day: 2 MJD: 59625
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg mcc IGL | cod emx esx gfz grg mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1369 35 61 56 38 35 --- 22 | 82 71 70 77 88 --- 71
R02E | 973 9 29 19 18 17 --- 9 | 59 55 52 57 63 --- 56
R03E | 2178 13 34 11 21 20 --- 10 | 69 67 64 68 76 --- 67
XR04E | 4271 15 28 15 --- 19 --- 11 | 60 53 55 --- 57 --- 54
R05E | 3626 13 26 20 20 20 168 9 | 51 49 53 57 53 110 50
R07E | 1707 19 37 13 19 27 --- 11 | 237 238 240 235 244 --- 238
R08E | 795 19 21 19 26 28 --- 11 | 108 102 116 119 111 --- 110
R09 | 2077 18 23 10 17 15 --- 8 | 19 25 23 24 15 --- 18
XR11 | 1671 16 --- 23 14 29 --- 12 | 21 --- 33 32 16 --- 20
R12 | 683 21 9 31 16 15 320 10 | 25 26 45 28 26 218 25
R13 | 1174 33 18 37 40 52 --- 19 | 37 23 31 30 22 --- 23
R14 | 1417 10 13 20 15 11 --- 7 | 18 29 37 29 22 --- 22
R15 | 682 14 20 13 14 8 154 7 | 18 24 16 15 14 139 15
R17 | 572 15 30 18 11 18 --- 9 | 58 36 47 48 51 --- 47
R18 | 800 16 38 15 14 18 --- 10 | 45 30 50 56 56 --- 46
R19 | 863 54 98 53 43 46 --- 29 | 94 31 44 86 59 --- 59
R20 | 1112 43 84 90 64 39 --- 32 | 89 44 38 113 82 --- 70
R21 | 1820 9 39 19 18 19 --- 10 | 58 42 49 69 72 --- 58
R22 | 1880 47 41 76 34 41 --- 24 | 44 63 106 90 49 --- 63
R24 | 738 16 56 32 24 27 82 15 | 65 37 47 69 69 33 56
------+-----------------------------------------+-------------------------------------
RMS | 1550 26 44 38 28 28 201 |T 62 55 60 68 62 125 58
WRMS | 1550 21 35 28 20 20 201 |NE 45 34 43 53 42 130 40
MEDI | 1174 16 30 19 19 20 154 |MD 58 42 47 57 56 110 54
Table 3.2197.3 GPS week: 2197 Day: 3 MJD: 59626
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg mcc IGL | cod emx esx gfz grg mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 3447 39 60 52 47 23 --- 22 | 77 37 56 83 63 --- 59
R02E | 1789 10 34 12 17 20 --- 9 | 61 59 68 65 77 --- 64
R03E | 2289 12 44 17 17 42 --- 13 | 70 87 76 78 76 --- 72
XR04E | 2616 10 39 19 --- 33 --- 14 | 62 51 58 --- 85 --- 62
R05E | 4217 14 40 17 35 17 413 12 | 60 55 57 69 61 174 58
R07E | 1244 16 35 17 11 21 --- 10 | 159 161 169 168 167 --- 164
R08E | 1610 15 36 14 20 25 --- 11 | 83 79 91 96 105 --- 89
R09 | 1698 16 26 17 12 30 --- 10 | 24 27 23 24 20 --- 16
R11 | 1364 12 25 23 24 28 --- 11 | 17 11 24 34 18 --- 18
R12 | 985 8 14 12 10 8 --- 5 | 18 19 26 26 16 --- 18
R13 | 1943 20 20 33 36 68 --- 19 | 29 33 30 26 26 --- 23
R14 | 2241 8 17 11 14 17 --- 6 | 17 18 19 21 27 --- 17
R15 | 1296 7 13 10 12 16 208 5 | 14 14 27 25 15 156 16
R17 | 509 11 31 15 13 16 --- 8 | 63 37 52 63 65 --- 57
R18 | 459 11 36 15 16 20 --- 9 | 55 32 55 58 63 --- 53
R19 | 797 47 114 64 55 55 --- 32 | 102 18 40 104 95 --- 72
R20 | 1416 49 77 71 75 46 --- 31 | 91 36 34 99 60 --- 61
R21 | 1392 13 38 21 16 24 --- 11 | 65 37 52 67 76 --- 60
R22 | 2123 41 31 94 57 29 --- 28 | 43 62 121 48 51 --- 53
R24 | 1501 18 52 21 17 19 49 13 | 76 39 58 73 73 48 65
------+-----------------------------------------+-------------------------------------
RMS | 1923 23 46 37 32 31 268 |T 59 45 56 64 61 126 54
WRMS | 1923 19 36 25 16 24 268 |NE 47 29 43 51 46 102 40
MEDI | 1501 13 35 17 17 23 208 |MD 61 37 52 65 63 156 58
Table 3.2197.4 GPS week: 2197 Day: 4 MJD: 59627
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg mcc IGL | cod emx esx gfz grg mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 3154 46 60 41 39 25 --- 21 | 72 30 36 65 42 --- 43
R02E | 1345 12 30 10 25 16 --- 9 | 51 40 50 64 68 --- 54
R03E | 2315 19 36 15 9 16 --- 9 | 66 70 66 68 71 --- 66
XR04E | 1531 14 33 13 --- 15 --- 10 | 78 67 78 --- 79 --- 75
R05E | 4003 18 37 16 20 25 --- 11 | 57 51 58 63 69 --- 57
R07E | 1081 11 34 13 12 25 --- 9 | 181 181 181 184 184 --- 182
R08E | 2383 14 33 17 14 27 --- 10 | 51 43 54 55 61 --- 50
R09 | 1597 10 20 16 15 15 --- 7 | 21 23 21 24 24 --- 19
R11 | 1007 17 15 19 13 22 --- 9 | 16 15 20 19 17 --- 13
R12 | 702 9 17 12 12 10 --- 5 | 23 27 39 35 29 --- 27
R13 | 1683 17 21 20 18 38 --- 12 | 27 27 21 21 25 --- 19
R14 | 1718 10 13 18 10 9 --- 6 | 19 17 32 23 19 --- 20
R15 | 1260 13 14 11 7 11 273 5 | 18 17 22 21 22 192 18
R17 | 962 15 35 15 13 12 --- 9 | 60 39 59 58 60 --- 55
R18 | 1202 7 30 13 10 14 --- 7 | 52 33 52 49 54 --- 48
R19 | 1316 54 111 55 40 56 --- 31 | 85 33 28 62 76 --- 47
R20 | 851 51 83 73 97 52 --- 36 | 73 49 31 103 50 --- 53
R21 | 742 11 37 18 11 22 --- 10 | 62 42 53 57 68 --- 55
R22 | 2856 60 27 70 44 40 --- 26 | 39 53 88 47 88 --- 57
R24 | 798 25 55 21 16 19 44 13 | 67 32 41 58 66 67 52
------+-----------------------------------------+-------------------------------------
RMS | 1858 28 44 31 30 27 196 |T 55 44 51 56 58 129 50
WRMS | 1858 22 34 23 16 26 196 |NE 43 31 39 44 46 129 37
MEDI | 1316 14 33 16 14 19 44 |MD 52 33 41 57 60 67 50
Table 3.2197.5 GPS week: 2197 Day: 5 MJD: 59628
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 3349 33 55 49 34 16 19 --- 16 | 68 27 41 72 66 98 --- 53
R02E | 2093 11 26 18 17 17 22 --- 8 | 30 23 35 32 32 28 --- 27
R03E | 2051 15 35 18 26 13 18 --- 9 | 64 63 64 70 69 22 --- 64
XR04E | 1208 7 31 12 --- 13 13 --- 7 | 48 36 50 --- 51 18 --- 47
R05E | 2881 13 34 20 19 17 22 --- 9 | 35 30 36 35 44 20 --- 33
R07E | 2872 15 33 12 15 18 15 --- 8 | 153 162 156 152 159 22 --- 156
R08E | 1829 12 34 14 20 22 11 --- 8 | 40 32 41 43 51 18 --- 40
R09 | 1132 15 13 10 16 12 22 --- 6 | 18 16 30 31 23 25 --- 21
XR11 | 1066 13 --- 24 23 28 26 --- 11 | 12 --- 26 18 20 15 --- 13
R12 | 672 10 14 16 24 13 33 239 8 | 16 20 24 30 14 14 256 14
R13 | 1462 17 20 18 30 41 19 --- 11 | 26 30 21 21 20 15 --- 16
R14 | 775 15 12 12 9 20 39 --- 9 | 14 10 18 17 21 15 --- 12
R15 | 1580 15 20 12 17 15 21 242 7 | 13 17 22 24 19 23 302 17
R17 | 1937 14 34 13 11 13 15 --- 7 | 43 27 39 37 44 21 --- 39
R18 | 2648 14 33 17 14 18 28 --- 9 | 40 29 48 42 52 33 --- 41
R19 | 2030 42 81 38 27 49 40 --- 20 | 42 26 28 29 52 261 --- 33
R20 | 989 44 94 72 83 72 57 --- 31 | 51 46 22 70 33 25 --- 36
R21 | 621 10 41 31 12 15 49 --- 12 | 53 35 43 55 54 28 --- 52
R22 | 2840 50 37 81 51 42 37 --- 23 | 44 62 85 61 77 25 --- 55
R24 | 2651 20 59 16 11 18 27 239 11 | 47 32 37 34 45 31 154 38
------+----------------------------------------------+------------------------------------------
RMS | 2082 24 43 33 30 29 30 240 |T 42 38 43 45 47 37 237 40
WRMS | 2082 18 35 23 15 23 28 240 |NE 32 29 34 36 36 40 237 29
MEDI | 1829 15 34 17 19 17 22 239 |MD 40 30 36 35 44 22 256 36
Table 3.2197.6 GPS week: 2197 Day: 6 MJD: 59629
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 2209 37 49 40 37 14 25 --- 15 | 86 44 41 83 65 96 --- 62
R02E | 1121 16 36 17 18 12 18 --- 8 | 50 44 59 64 60 25 --- 55
R03E | 2596 21 36 19 20 19 26 --- 10 | 65 66 65 68 68 28 --- 63
XR04E | 1309 14 30 13 --- 12 21 --- 8 | 70 59 61 --- 70 20 --- 65
R05E | 1698 8 32 24 15 13 23 105 8 | 59 48 54 55 59 20 138 54
R07E | 3288 15 38 20 29 14 26 --- 10 | 160 165 167 161 169 20 --- 164
R08E | 2218 15 35 18 12 25 30 --- 10 | 60 51 68 70 74 19 --- 64
R09 | 849 14 13 20 15 13 11 --- 6 | 20 28 25 26 27 19 --- 21
XR11 | 1478 11 --- 16 14 7 19 --- 6 | 16 --- 26 18 27 9 --- 16
R12 | 605 12 11 18 15 11 38 139 8 | 19 21 28 28 19 16 125 20
R13 | 2019 27 30 34 34 58 36 --- 17 | 34 36 33 28 34 13 --- 27
R14 | 572 16 11 14 15 18 42 --- 9 | 19 22 22 22 26 20 --- 18
R15 | 1302 15 15 18 15 12 30 274 8 | 25 20 22 25 20 14 263 19
R17 | 907 17 39 20 18 12 18 --- 9 | 78 44 64 75 74 19 --- 69
R18 | 2209 17 40 10 10 15 25 --- 8 | 62 46 76 73 76 28 --- 68
R19 | 2021 46 66 30 27 37 42 --- 18 | 91 30 38 79 82 247 --- 62
R20 | 632 49 105 72 68 56 64 --- 30 | 100 41 52 120 73 22 --- 76
R21 | 565 8 41 19 9 10 39 --- 9 | 79 56 65 82 84 22 --- 77
R22 | 2182 51 45 99 56 46 32 --- 26 | 69 101 150 81 83 19 --- 86
R24 | 2659 9 51 20 22 20 22 129 11 | 83 47 60 84 84 22 98 74
------+----------------------------------------------+------------------------------------------
RMS | 1841 26 44 36 29 27 32 175 |T 62 51 58 65 63 34 156 58
WRMS | 1841 18 35 22 16 20 30 175 |NE 53 41 50 57 54 36 162 48
MEDI | 1478 15 36 19 18 14 26 129 |MD 62 44 54 70 68 20 125 62
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