[IGSREPORT-28507] Wk 2196 IGLOS Final Orbits
acc
acc at igs.org
Tue Mar 1 00:14:01 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2196 (Feb 06, 2022 - Feb 12, 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 2.2196.
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:
igl2196[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2196 in the SP3 format.
igl21967.sum Combination Report for GPS Week 2196.
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 | -0.8 ns
3 | 0.1 ns
4 | -1.6 ns
5 | -1.7 ns
6 | -0.5 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 1.2196, 1a.2196).
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 2.2196.0-6)
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 3.2196.0-6).
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 2196 summary. (Feb 06, 2022 - Feb 12, 2022)
Table 1.2196.a GPS week : 2196 MJD: 59616.0-59622.0
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 3 1 -10 42 .15 23 19 | 12996 -375 2896 8312
| 0 0 2 14 11 19 .04 | 742 1535
emx n/a| -1 2 -2 -2 15 -45 -.08 48 37 | -6567 90 2915 8323
| 2 1 3 23 21 59 .07 | 11048 1140
esx n/a| -1 1 -1 3 -26 -26 -.13 40 28 | 6507 -930 2902 8792
| 1 1 1 20 11 11 .04 | 5492 1366
gfz n/a| 0 1 4 3 5 -18 -.06 27 18 | 0 -390 2886 8054
| 1 1 2 16 10 39 .06 | 0 1300
grg n/a| 2 -2 -2 -27 15 15 .28 28 22 | -1118 -305 2899 7856
| 0 1 2 13 19 35 .06 | 298 1197
iac n/a| 0 -1 -4 22 7 -4 -.25 22 19 | 562 167 2813 8471
| 1 2 2 29 22 42 .02 | 809 555
mcc n/a| 2 2 -29 -69 99 17 -1.10 173 173 | --- --- --- ---
| 11 8 7 165 160 337 .32 | --- ---
Table 1.2196.b GPS week : 2196 MJD: 59616.0-59622.0
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 | 21 20 20 20 18 20 20 |
R02 | 8 8 7 7 6 8 8 |
R03 | 8 8 7 7 7 8 9 |
R04 | 8 9 9 10 9 9 11 |
R05 | 8 8 9 8 7 7 9 |
R07 | 8 7 7 8 9 10 8 |
R08 | 7 7 7 8 8 12 10 |
R09 | 7 7 9 9 11 9 9 |
R11 | 9 11 8 8 8 7 11 |
R12 | 8 8 9 8 6 6 8 |
R13 | 15 13 17 14 14 19 21 |
R14 | 8 7 6 8 6 7 5 |
R15 | 9 9 6 7 6 6 7 |
R17 | 8 9 9 7 9 9 10 |
R18 | 9 10 10 9 8 10 10 |
R19 | 19 23 25 25 19 23 21 |
R20 | 28 26 27 31 30 35 35 |
R21 | 10 9 11 9 10 12 11 |
R22 | 23 24 22 21 27 35 32 |
R24 | 13 13 12 13 12 14 12 |
Table 1.2196.c GPS week : 2196 MJD: 59616.0-59622.0
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 2196 0 | 21 -19 192 665 715 -12970 81.9 1698 1698 | -1991 0
brd 2196 1 | 37 -24 141 -795 -885 -19700 83.5 2072 2072 | -1720 0
brd 2196 2 | 49 17 132 1406 1068 27930 79.1 1671 1671 | -782 0
brd 2196 3 | -28 16 99 139 1640 -5757 80.2 1603 1603 | 88 0
brd 2196 4 | -7 -5 27 -283 2510 -18150 83.0 1461 1461 | -1551 0
brd 2196 5 | -54 89 -39 553 1860 -9064 81.6 1631 1631 | -1715 0
brd 2196 6 | -63 -35 -28 -965 57 -4597 79.3 1459 1459 | -541 0
-------------+------------------------------------------------------------+----------------
brd 2196 mean| -6 5 75 102 995 -6044 81.2 1656 1656 | -1173 0
brd 2196 sdev| 44 42 89 848 1151 16054 1.7 206 206 | 768 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 2.2196.0 GPS week: 2196 Day: 0 MJD: 59616
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 -6 -29 36 .11 23 19 | 13688 -1005 2821 7270
emx n/a| -2 2 3 28 2 -116 -.20 48 35 | -11211 -348 2794 7291
esx n/a| 0 2 0 6 -34 -27 -.14 40 26 | 5443 -1558 2817 9539
gfz n/a| -1 2 3 -4 -5 -51 .00 24 20 | 0 -1365 2811 6890
grg n/a| 1 -1 -3 -39 15 -14 .38 28 22 | -1488 -1222 2829 7053
iac n/a| 0 -5 -4 55 29 50 -.27 24 22 | -468 -379 2813 7905
mcc n/a| 1 7 -38 104 73 -115 -.72 146 146 | --- --- --- ---
Table 2.2196.1 GPS week: 2196 Day: 1 MJD: 59617
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 -1 49 .18 23 19 | 13783 -1812 2491 7699
emx n/a| 0 2 2 5 26 -129 -.05 51 42 | -18194 -742 2509 7853
esx n/a| -1 0 0 19 -29 -25 -.15 41 34 | 4290 -1587 2513 6040
gfz n/a| -2 1 9 -4 13 47 -.06 29 20 | 0 -788 2490 7561
grg n/a| 2 -2 -3 -43 24 -16 .25 23 17 | -1451 -803 2502 7220
iac n/a| -1 -1 -8 24 -22 18 -.23 22 18 | 35 448 2502 8427
mcc n/a| 7 16 -25 -282 44 317 -.72 129 129 | --- --- --- ---
Table 2.2196.2 GPS week: 2196 Day: 2 MJD: 59618
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 -17 -9 68 .19 23 17 | 12846 -144 3105 7179
emx n/a| 0 0 -4 11 35 -29 .04 51 41 | 3356 674 3092 7060
esx n/a| 1 0 -2 17 -22 -42 -.06 42 32 | 13533 -1667 3115 9367
gfz n/a| -1 3 3 -4 -1 -7 -.01 30 18 | 0 -1286 3026 6829
grg n/a| 2 -3 0 -8 28 14 .27 29 19 | -767 -471 3120 6906
iac n/a| 0 0 -3 -7 -1 -46 -.24 18 16 | 926 -53 3114 7802
mcc n/a| 0 -4 -24 -103 -4 463 -.88 160 160 | --- --- --- ---
Table 2.2196.3 GPS week: 2196 Day: 3 MJD: 59619
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 1 12 -20 15 .11 24 19 | 12825 2346 3101 8149
emx n/a| -2 1 -5 0 -26 5 -.04 53 37 | 6265 1874 3112 7999
esx n/a| -3 3 -2 -24 -20 -7 -.15 39 31 | 10893 2065 3105 8564
gfz n/a| 0 0 5 22 21 -35 -.05 26 14 | 0 2270 3121 7627
grg n/a| 1 -3 0 -21 -12 -9 .32 28 24 | -1111 2149 3091 7491
iac n/a| 1 0 -4 -6 31 4 -.22 22 18 | 1628 997 3094 8737
mcc n/a| 8 -2 -20 -11 -36 258 -1.37 219 219 | --- --- --- ---
Table 2.2196.4 GPS week: 2196 Day: 4 MJD: 59620
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 6 -2 -7 51 .16 23 19 | 13527 -874 2538 8931
emx n/a| 1 1 -6 5 27 -4 -.12 46 36 | -19417 -67 2585 8966
esx n/a| -2 2 -3 -27 -8 -40 -.14 41 29 | 210 -1312 2541 9258
gfz n/a| 0 1 3 -15 -1 -8 -.04 26 15 | 0 -803 2557 8759
grg n/a| 1 -4 0 -30 31 26 .23 26 22 | -1073 -1016 2539 8333
iac n/a| -1 1 -3 46 1 -48 -.26 26 19 | 689 -178 2542 9486
mcc n/a| 21 3 -27 97 13 -58 -1.41 167 167 | --- --- --- ---
Table 2.2196.5 GPS week: 2196 Day: 5 MJD: 59621
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 16 -7 20 .11 21 19 | 12630 -1968 3070 8719
emx n/a| -4 3 -2 -36 15 17 -.08 46 37 | 4586 -1590 3122 8706
esx n/a| -2 0 -3 13 -27 -23 -.08 42 24 | -112 -1751 3066 8193
gfz n/a| 2 -1 3 0 12 -3 -.17 29 19 | 0 -1083 3026 8668
grg n/a| 2 -3 -5 -13 31 27 .22 30 22 | -1208 -1075 3069 8209
mcc n/a| -9 6 -31 8 427 -442 -1.37 178 178 | --- --- --- ---
Table 2.2196.6 GPS week: 2196 Day: 6 MJD: 59622
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 -8 4 56 .21 26 19 | 11675 826 3146 10237
emx n/a| -2 2 -1 -33 26 -63 -.12 40 33 | -11360 831 3197 10387
esx n/a| 0 0 0 16 -45 -21 -.16 33 22 | 11295 -706 3160 10585
gfz n/a| 0 1 0 32 -1 -74 -.12 28 18 | 0 325 3172 10049
grg n/a| 3 -1 -3 -35 -11 84 .32 34 24 | -728 297 3148 9786
mcc n/a| -11 -9 -41 -296 179 -298 -1.26 212 212 | --- --- --- ---
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 3.2196.0 GPS week: 2196 Day: 0 MJD: 59616
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 | 1404 28 65 63 58 27 34 --- 20 | 119 111 137 143 119 92 --- 123
R02E | 2189 14 30 14 10 18 21 --- 7 | 44 38 52 46 54 48 --- 46
R03E | 1217 8 31 13 15 18 22 --- 8 | 78 75 77 76 82 54 --- 76
XR04 | 786 9 31 15 --- 11 18 --- 8 | 95 92 98 --- 95 54 --- 96
R05E | 1529 14 26 19 14 13 19 174 7 | 65 63 65 65 67 41 108 62
R07E | 1650 10 23 13 15 9 27 --- 7 | 64 61 60 60 67 50 --- 62
R08E | 2459 11 23 18 18 13 13 --- 7 | 43 36 41 44 47 35 --- 40
R09 | 1270 12 16 14 14 22 14 --- 7 | 37 45 34 32 25 37 --- 32
XR11 | 974 10 --- 30 16 11 24 --- 9 | 33 --- 37 40 41 35 --- 36
R12 | 652 12 14 24 10 16 25 219 7 | 61 59 50 57 54 47 203 57
R13 | 1824 27 30 43 26 49 20 --- 14 | 67 66 51 59 45 39 --- 55
R14 | 1326 11 7 10 11 28 26 --- 8 | 51 43 42 40 41 36 --- 44
R15 | 757 19 29 21 22 11 18 112 9 | 54 52 39 39 44 37 135 44
R17 | 711 8 29 18 20 13 17 --- 7 | 69 45 55 73 64 45 --- 64
R18 | 1087 17 24 14 14 26 19 --- 8 | 53 36 57 57 67 36 --- 52
R19 | 1027 36 83 39 33 38 28 --- 18 | 93 39 38 71 91 48 --- 64
R20 | 1416 55 127 81 34 55 35 --- 28 | 109 44 44 104 91 55 --- 76
R21 | 1433 6 38 26 25 12 17 59 9 | 68 37 50 79 67 48 46 65
R22 | 4176 42 36 99 25 50 34 --- 22 | 30 56 118 48 36 50 --- 43
R24 | 777 14 66 32 18 24 27 109 13 | 78 48 60 87 90 54 34 77
------+----------------------------------------------+------------------------------------------
RMS | 1698 23 48 40 24 28 24 146 |T 65 55 60 64 64 47 105 60
WRMS | 1698 19 35 25 20 22 22 146 |NE 64 50 55 60 60 44 104 57
MEDI | 1270 12 30 19 18 18 21 112 |MD 64 48 51 59 64 47 108 57
Table 3.2196.1 GPS week: 2196 Day: 1 MJD: 59617
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 | 1752 32 66 64 48 26 37 --- 19 | 95 86 86 103 92 61 --- 85
R02E | 2098 12 34 21 16 10 17 --- 7 | 38 33 46 40 47 40 --- 41
R03E | 1553 10 33 13 12 15 19 --- 7 | 71 69 66 71 77 50 --- 71
XR04 | 1529 8 40 14 --- 15 14 --- 8 | 59 60 60 --- 63 37 --- 59
R05E | 2321 16 31 22 18 16 14 176 8 | 68 62 61 65 76 52 98 68
R07E | 2301 13 29 14 17 14 14 --- 7 | 51 46 49 47 64 37 --- 51
R08E | 2956 10 24 13 26 9 11 --- 6 | 45 40 46 42 48 42 --- 44
R09 | 2041 12 22 14 20 12 12 --- 6 | 31 42 29 30 19 33 --- 29
XR11 | 2243 13 --- 21 25 18 26 --- 10 | 22 --- 28 29 19 25 --- 20
R12 | 1414 13 18 29 12 10 15 137 7 | 23 18 27 35 34 32 92 28
R13 | 1924 16 24 31 36 36 27 --- 13 | 36 33 43 42 48 52 --- 42
R14 | 1187 9 12 6 15 15 20 --- 6 | 29 22 27 22 21 35 --- 27
R15 | 743 20 23 24 25 11 17 130 8 | 26 25 22 20 14 23 74 16
R17 | 2327 5 41 23 20 18 11 --- 8 | 39 25 36 48 49 30 --- 40
R18 | 1655 19 44 14 21 20 20 --- 10 | 33 21 37 44 45 29 --- 34
R19 | 1808 45 102 68 45 37 22 --- 22 | 75 30 34 85 65 31 --- 57
R20 | 2773 42 107 87 57 42 22 --- 25 | 74 44 49 85 80 33 --- 59
R21 | 1466 15 46 22 17 12 18 80 9 | 39 25 29 43 43 29 18 36
R22 | 3820 51 60 84 36 44 43 --- 23 | 27 57 83 76 41 45 --- 42
R24 | 536 9 73 36 19 18 27 102 13 | 41 37 29 47 44 36 20 40
------+----------------------------------------------+------------------------------------------
RMS | 2072 23 51 41 29 23 22 129 |T 46 40 44 51 49 37 60 44
WRMS | 2072 19 42 34 20 17 18 129 |NE 39 33 38 46 41 33 51 37
MEDI | 1808 13 34 22 20 15 18 130 |MD 39 37 37 44 47 35 74 41
Table 3.2196.2 GPS week: 2196 Day: 2 MJD: 59618
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 | 1475 40 61 51 52 22 39 --- 19 | 88 89 110 107 86 72 --- 86
R02E | 1599 10 32 14 12 20 11 --- 7 | 41 43 46 41 55 35 --- 41
R03E | 1463 9 30 14 15 12 12 --- 6 | 60 50 63 69 64 44 --- 61
XR04 | 1244 12 36 16 --- 14 15 --- 8 | 45 44 51 --- 53 44 --- 47
R05E | 1830 18 37 18 20 15 13 116 8 | 57 51 51 56 62 42 102 55
R07E | 1733 10 34 17 16 11 12 --- 7 | 42 35 41 44 43 40 --- 39
R08E | 1872 11 31 18 14 18 12 --- 7 | 72 80 83 75 72 61 --- 75
R09 | 626 15 31 21 19 22 21 --- 9 | 30 52 35 32 35 28 --- 31
R11 | 2691 12 25 13 23 17 11 --- 7 | 28 14 34 49 35 34 --- 34
R12 | 864 23 12 26 24 10 8 259 8 | 49 42 39 42 36 33 121 38
R13 | 3282 38 40 32 34 56 21 --- 16 | 53 57 39 41 45 28 --- 38
R14 | 1402 12 20 15 10 14 6 --- 5 | 38 32 35 34 29 26 --- 33
R15 | 958 10 18 8 12 9 15 158 5 | 27 37 35 32 34 33 43 31
R17 | 1200 12 35 30 16 21 13 --- 9 | 45 31 26 47 62 37 --- 43
R18 | 644 10 52 19 12 24 19 --- 9 | 40 35 30 38 55 42 --- 41
R19 | 1188 47 119 70 38 60 28 --- 25 | 83 25 32 84 95 34 --- 60
R20 | 1214 41 101 94 73 55 16 --- 27 | 72 41 34 92 67 45 --- 58
R21 | 997 17 52 20 25 19 21 107 11 | 50 22 46 66 62 45 17 52
R22 | 1392 30 37 101 52 43 18 --- 22 | 30 43 88 47 31 33 --- 33
R24 | 2574 7 67 28 15 21 20 102 11 | 53 24 42 54 63 47 25 52
------+----------------------------------------------+------------------------------------------
RMS | 1671 23 51 42 30 29 18 160 |T 50 42 48 55 54 40 61 47
WRMS | 1671 17 41 32 18 19 16 160 |NE 45 35 40 50 50 36 51 42
MEDI | 1392 12 35 19 19 19 15 116 |MD 45 41 39 47 55 37 43 41
Table 3.2196.3 GPS week: 2196 Day: 3 MJD: 59619
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 | 877 41 68 45 49 32 35 --- 19 | 79 69 75 80 72 65 --- 65
R02E | 2523 10 25 16 15 10 14 --- 6 | 54 45 54 55 64 39 --- 54
R03E | 1019 10 27 14 14 12 20 --- 7 | 52 47 51 56 56 47 --- 50
XR04 | 2045 10 37 17 --- 20 14 --- 9 | 38 33 42 --- 46 43 --- 38
R05E | 1076 16 37 21 13 13 12 87 8 | 41 31 39 42 48 46 131 40
R07E | 828 11 29 17 18 14 20 --- 8 | 51 51 60 62 58 37 --- 53
R08E | 1137 12 30 17 16 11 20 --- 7 | 43 42 44 41 45 38 --- 40
R09 | 2810 12 20 26 17 27 20 --- 9 | 28 36 36 32 23 28 --- 25
R11 | 1746 14 21 19 8 25 16 --- 7 | 21 12 25 25 34 28 --- 23
R12 | 733 16 19 15 17 15 18 404 7 | 46 48 53 39 33 26 241 39
R13 | 1688 29 21 23 26 59 11 --- 14 | 51 54 43 36 28 22 --- 39
R14 | 780 22 17 15 13 21 9 --- 7 | 39 32 32 33 26 21 --- 29
R15 | 1119 16 20 15 16 7 14 210 6 | 35 33 20 22 26 16 77 25
R17 | 853 15 33 12 11 14 15 --- 7 | 59 36 49 56 64 29 --- 54
R18 | 1471 13 45 15 14 26 14 --- 9 | 45 36 41 56 62 31 --- 48
R19 | 1219 59 125 58 27 39 38 --- 25 | 96 32 32 72 67 29 --- 57
R20 | 2011 38 129 94 72 53 43 --- 31 | 77 47 30 107 60 43 --- 63
R21 | 976 12 38 17 14 18 18 116 8 | 52 25 42 54 53 29 41 48
R22 | 2899 34 27 97 25 32 30 --- 20 | 23 43 80 33 36 33 --- 28
R24 | 1878 12 72 34 14 25 19 108 13 | 61 25 42 68 77 32 30 60
------+----------------------------------------------+------------------------------------------
RMS | 1603 24 53 39 26 28 22 219 |T 49 38 44 51 48 34 104 43
WRMS | 1603 19 37 31 14 24 18 219 |NE 47 35 40 48 45 29 97 41
MEDI | 1137 14 29 17 16 20 18 116 |MD 46 36 42 54 48 31 77 40
Table 3.2196.4 GPS week: 2196 Day: 4 MJD: 59620
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 | 850 34 58 49 39 21 35 --- 17 | 62 53 80 79 72 62 --- 61
R02E | 3489 11 29 12 11 13 8 --- 6 | 51 50 54 54 54 45 --- 51
R03E | 1095 12 29 14 12 12 13 --- 6 | 63 51 54 55 64 68 --- 57
XR04 | 2592 10 32 15 --- 13 16 --- 8 | 42 37 45 --- 49 49 --- 43
R05E | 1139 15 28 15 12 12 14 191 7 | 51 39 48 49 56 58 86 47
R07E | 785 10 34 21 17 25 14 --- 9 | 66 61 62 72 79 51 --- 66
R08E | 1625 12 29 17 14 25 12 --- 8 | 69 65 67 63 71 46 --- 64
R09 | 2731 27 20 13 22 25 27 --- 10 | 29 42 38 42 17 43 --- 30
XR11 | 1515 12 --- 14 12 16 19 --- 7 | 21 --- 24 29 22 30 --- 22
R12 | 819 15 20 21 8 10 10 167 6 | 34 33 23 32 27 30 244 29
R13 | 1278 32 37 27 21 33 34 --- 13 | 40 51 44 37 31 44 --- 31
R14 | 603 13 6 12 14 10 18 --- 6 | 31 32 29 27 32 29 --- 27
R15 | 974 15 10 12 14 9 20 196 6 | 29 25 29 32 29 22 60 24
R17 | 1259 11 33 11 21 22 21 --- 9 | 53 35 43 54 45 43 --- 45
R18 | 785 10 34 21 10 15 17 --- 7 | 46 32 53 46 50 32 --- 42
R19 | 1535 42 80 46 23 37 33 --- 19 | 64 48 30 49 61 37 --- 44
R20 | 1190 43 116 94 70 47 37 --- 30 | 80 53 29 88 57 48 --- 57
R21 | 1001 12 39 27 11 19 24 --- 9 | 47 27 37 46 54 48 --- 44
R22 | 647 37 36 111 48 49 58 --- 27 | 28 32 72 47 48 65 --- 29
R24 | 1136 16 62 19 11 28 16 93 11 | 59 27 43 45 64 45 44 48
------+----------------------------------------------+------------------------------------------
RMS | 1461 23 46 41 26 26 26 167 |T 48 41 45 49 49 44 108 43
WRMS | 1461 19 36 29 15 22 19 167 |NE 43 36 38 44 41 40 116 36
MEDI | 1136 13 33 17 14 19 18 167 |MD 47 39 43 47 50 45 60 44
Table 3.2196.5 GPS week: 2196 Day: 5 MJD: 59621
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg mcc IGL | cod emx esx gfz grg mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1720 25 61 44 46 24 --- 19 | 73 64 72 95 76 --- 72
R02E | 3581 7 27 19 9 14 --- 7 | 33 22 31 32 43 --- 31
R03E | 1444 9 32 14 13 14 --- 8 | 65 63 63 69 67 --- 64
XR04 | 2789 10 25 17 --- 16 --- 9 | 84 79 85 --- 77 --- 81
R05E | 1779 6 26 18 9 14 230 7 | 65 60 62 63 66 96 62
R07E | 1758 10 31 26 14 19 --- 9 | 53 46 56 58 61 --- 53
R08E | 1671 14 33 24 23 28 --- 12 | 65 70 79 79 69 --- 69
R09 | 1530 13 14 17 17 23 --- 8 | 28 31 37 29 19 --- 25
XR11 | 1942 9 --- 12 14 10 --- 6 | 18 --- 25 17 21 --- 18
R12 | 700 8 21 12 14 7 91 6 | 22 30 31 27 25 145 23
R13 | 2402 27 38 37 37 51 --- 19 | 23 37 29 21 20 --- 18
R14 | 785 9 16 10 19 13 --- 6 | 18 23 21 18 23 --- 15
R15 | 1912 7 7 15 12 11 238 5 | 17 20 36 25 24 80 22
R17 | 612 13 35 11 8 15 --- 8 | 40 23 31 29 33 --- 31
R18 | 1300 13 33 14 20 19 --- 9 | 36 24 32 41 33 --- 31
R19 | 933 34 84 42 25 51 --- 23 | 33 29 38 42 41 --- 30
R20 | 1030 51 102 86 74 44 --- 34 | 42 41 45 58 38 --- 33
R21 | 1142 11 43 30 17 19 --- 11 | 42 33 27 36 47 --- 35
R22 | 1215 40 54 125 49 61 --- 34 | 37 52 86 60 61 --- 41
R24 | 1143 8 57 21 25 28 97 13 | 35 26 34 48 48 30 35
------+-----------------------------------------+-------------------------------------
RMS | 1631 21 46 42 29 30 178 |T 41 40 46 44 44 87 39
WRMS | 1631 19 37 24 19 22 178 |NE 33 34 39 34 36 85 31
MEDI | 1444 10 33 18 17 19 97 |MD 36 33 36 41 41 80 31
Table 3.2196.6 GPS week: 2196 Day: 6 MJD: 59622
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg mcc IGL | cod emx esx gfz grg mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2701 41 48 34 41 36 --- 20 | 97 88 102 110 104 --- 98
R02E | 2385 8 31 11 11 11 --- 7 | 32 34 30 34 36 --- 29
R03E | 1025 14 29 17 17 16 --- 9 | 85 75 85 88 91 --- 85
XR04 | 4120 11 28 18 --- 18 --- 10 | 99 99 97 --- 97 --- 97
R05E | 2033 13 24 18 14 18 254 8 | 75 71 66 72 76 148 71
R07E | 1037 7 30 14 12 16 --- 8 | 59 61 63 62 63 --- 60
R08E | 2074 11 36 17 16 15 --- 9 | 79 76 74 82 85 --- 77
R09 | 691 20 17 12 13 21 --- 8 | 24 37 35 29 27 --- 26
XR11 | 916 21 --- 17 12 20 --- 10 | 26 --- 40 32 40 --- 31
R12 | 592 19 20 9 15 18 183 8 | 47 45 46 43 41 218 42
R13 | 1349 24 26 27 37 78 --- 20 | 51 56 41 38 34 --- 40
R14 | 1148 6 12 10 7 9 --- 4 | 41 39 36 35 38 --- 37
R15 | 1971 11 15 9 15 18 271 7 | 42 41 39 34 33 136 36
R17 | 593 8 39 13 17 17 --- 9 | 71 46 58 74 73 --- 65
R18 | 1185 13 36 22 8 22 --- 10 | 58 33 66 64 70 --- 58
R19 | 918 34 74 32 30 47 --- 21 | 92 38 53 84 77 --- 68
R20 | 1045 51 90 73 78 64 --- 35 | 104 25 46 123 87 --- 79
R21 | 1190 10 38 21 21 17 --- 10 | 65 33 46 70 73 --- 60
R22 | 1065 65 38 94 30 59 --- 31 | 42 53 108 35 46 --- 40
R24 | 804 11 44 16 16 26 88 11 | 69 31 54 75 83 37 65
------+-----------------------------------------+-------------------------------------
RMS | 1458 26 40 33 28 34 212 |T 62 51 59 62 63 134 58
WRMS | 1458 19 33 22 18 24 212 |NE 59 44 54 56 58 130 53
MEDI | 1065 13 31 17 16 18 183 |MD 59 45 53 64 70 136 60
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