[IGSREPORT-28433] Wk 2191 IGLOS Final Orbits
acc
acc at igs.org
Fri Jan 21 05:19:17 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2191 (Jan 02, 2022 - Jan 08, 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 2.2191.
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:
igl2191[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2191 in the SP3 format.
igl21917.sum Combination Report for GPS Week 2191.
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 | -0.9 ns
1 | -1.5 ns
2 | -93.4 ns
3 | -1.6 ns
4 | -0.4 ns
5 | -1.7 ns
6 | -1.6 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
1 | BKG | R07
1 | COD | R07
1 | COF | R07
1 | EMX | R07
1 | ESX | R07
1 | GFZ | R07
1 | GRG | R07
1 | IAC | R07
1 | MCC | R07
2 | BKG | R07
2 | COD | R07
2 | COF | R07
2 | EMX | R07
2 | ESX | R07
2 | GFZ | R07
2 | GRG | R07
2 | IAC | R07
2 | MCC | R07
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 1.2191, 1a.2191).
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 2.2191.0-6)
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 3.2191.0-6).
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 2191 summary. (Jan 02, 2022 - Jan 08, 2022)
Table 1.2191.a GPS week : 2191 MJD: 59581.0-59587.0
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 -3 -8 55 .17 22 19 | 2176 -782 3057 8041
| 1 1 1 16 17 10 .04 | 35366 1795
emx n/a| 0 1 13 27 -16 -31 -.00 49 37 | -12661 -590 3029 8466
| 2 2 2 27 11 62 .08 | 33996 1313
esx n/a| 1 0 0 0 -4 -38 -.15 39 28 | -14195 -558 3020 7624
| 1 1 2 14 17 31 .06 | 30666 1818
gfz n/a| 0 1 0 -29 -15 -17 -.08 24 16 | 0 -579 2927 7519
| 0 1 2 24 14 26 .04 | 0 1301
grg n/a| 1 -5 5 19 -19 -3 .22 37 27 | -14489 -320 3021 7574
| 1 2 3 26 20 30 .05 | 35172 1731
iac n/a| -1 0 -4 34 60 -14 -.31 34 33 | -12579 -286 3059 8541
| 2 2 4 41 85 124 .12 | 34963 760
Table 1.2191.b GPS week : 2191 MJD: 59581.0-59587.0
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 | 16 15 18 18 15 17 19 |
R02 | 7 9 10 8 9 7 11 |
R03 | 10 15 11 9 10 10 9 |
R04 | 11 11 12 10 13 11 10 |
R05 | 9 9 9 8 9 11 10 |
R07 | 11 --- --- 23 10 9 10 |
R08 | 9 8 11 9 11 9 7 |
R09 | 9 12 9 10 10 7 7 |
R11 | 10 9 10 9 9 8 8 |
R12 | 9 9 11 12 10 8 7 |
R13 | 16 17 16 14 14 15 15 |
R14 | 9 9 8 9 8 7 6 |
R15 | 10 7 9 7 8 7 6 |
R17 | 11 11 8 9 8 10 8 |
R18 | 10 9 9 10 9 11 7 |
R19 | 23 29 26 23 29 30 26 |
R20 | 21 28 30 27 22 25 23 |
R21 | 11 9 8 12 11 10 9 |
R22 | 27 25 24 28 28 24 27 |
R24 | 13 13 14 12 10 11 11 |
Table 1.2191.c GPS week : 2191 MJD: 59581.0-59587.0
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 2191 0 | 7 -35 -11 -1381 1369 -13660 83.7 1528 1528 | -931 0
brd 2191 1 | 64 1 24 -682 -190 -4833 85.4 1779 1779 | -1509 0
brd 2191 2 | 13 34 61 -2101 -3250 -4003 83.1 2192 2192 | -93352 0
brd 2191 3 | -20 71 3 -3118 -1892 -5836 81.1 2550 2550 | -1650 0
brd 2191 4 | 74 92 62 -2408 -839 -1344 80.9 1409 1409 | -409 0
brd 2191 5 | 0 72 4 -1754 4 -411 81.9 1499 1499 | -1705 0
brd 2191 6 | -56 -70 113 1418 3078 5821 80.9 1218 1218 | -1610 0
-------------+------------------------------------------------------------+----------------
brd 2191 mean| 12 23 36 -1432 -245 -3466 82.4 1739 1739 | -14452 0
brd 2191 sdev| 45 60 44 1473 2073 5940 1.7 473 473 | 34794 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 2.2191.0 GPS week: 2191 Day: 0 MJD: 59581
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 -1 -43 60 .19 20 17 | 17081 -1948 2633 7231
emx n/a| -2 0 9 -3 -5 9 -.02 42 37 | 8213 -1110 2660 7889
esx n/a| 1 2 -1 -6 -7 8 -.23 39 37 | -16250 -2315 2631 9308
gfz n/a| 0 -1 5 -23 -6 11 -.05 22 16 | 0 -2080 2640 7003
grg n/a| -1 -2 8 49 -42 -16 .25 38 30 | 97 -2344 2646 6842
iac n/a| 1 1 -9 27 131 -174 -.45 36 36 | 1462 -1294 2646 7800
Table 2.2191.1 GPS week: 2191 Day: 1 MJD: 59582
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 15 0 65 .19 22 18 | 14790 -2570 2722 7575
emx n/a| 0 0 14 35 -4 -60 -.10 55 41 | 6038 -2124 2686 7583
esx n/a| 3 -1 -3 -15 -29 -85 -.08 39 27 | -779 -2039 2725 2775
gfz n/a| 0 3 1 -63 -28 -32 -.08 25 13 | 0 -1971 2734 7526
grg n/a| 0 -11 11 50 -29 35 .29 46 33 | -817 -1541 2718 6854
iac n/a| 3 2 -10 118 199 189 -.34 47 46 | 343 -563 2743 7942
Table 2.2191.2 GPS week: 2191 Day: 2 MJD: 59583
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 -1 -7 5 58 .15 24 23 | -77925 716 2561 8987
emx n/a| -2 1 12 34 -32 -74 -.05 51 37 | -88617 145 2587 9606
esx n/a| 1 1 0 10 -3 -15 -.13 37 26 | -81779 1517 2545 8905
gfz n/a| 2 0 -1 -54 1 19 -.16 24 20 | 0 765 2434 8205
grg n/a| 3 -3 3 -18 17 -36 .14 41 31 | -94204 1357 2555 8569
iac n/a| -3 -4 0 41 -49 -14 -.10 36 37 | -91831 162 2562 9474
Table 2.2191.3 GPS week: 2191 Day: 3 MJD: 59584
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 11 -6 42 .19 21 19 | 15339 1023 2758 8575
emx n/a| 4 4 13 59 -11 -16 -.06 47 36 | -145 704 2492 9066
esx n/a| 1 -1 1 20 16 -18 -.13 38 25 | -5160 1148 2518 8608
gfz n/a| 1 0 -1 -43 -4 -3 -.08 21 17 | 0 1156 2718 6983
grg n/a| 2 -3 6 34 -4 6 .23 39 30 | -2384 1632 2508 8133
iac n/a| -1 -1 -4 -5 -12 -145 -.39 35 37 | 1214 -730 2740 9167
Table 2.2191.4 GPS week: 2191 Day: 4 MJD: 59585
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -4 8 -20 47 .23 22 19 | 18552 -3355 3684 8027
emx n/a| -1 0 19 26 -30 -125 .07 50 37 | -3303 -2491 3782 8517
esx n/a| 0 2 4 -12 7 -49 -.19 40 27 | -194 -2911 3700 7348
gfz n/a| 0 0 -2 -5 -5 -29 -.09 22 14 | 0 -1333 3368 7786
grg n/a| 3 -7 0 -1 -27 -36 .23 38 25 | 563 -2285 3688 7758
iac n/a| -3 0 -3 24 77 76 -.39 31 28 | 2008 -834 3704 8567
Table 2.2191.5 GPS week: 2191 Day: 5 MJD: 59586
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 -1 -4 -23 -5 47 .11 18 16 | 13502 27 3466 7755
emx n/a| -1 0 12 52 -13 -18 .04 49 37 | -1518 520 3441 8103
esx n/a| 0 1 0 15 -24 -59 -.18 43 27 | -3199 57 3461 7862
gfz n/a| 0 3 -1 -4 -27 -38 -.09 24 17 | 0 -756 3238 7773
grg n/a| 2 -5 2 15 -13 -10 .18 31 20 | -2398 -114 3438 7214
iac n/a| -5 0 0 -4 56 3 -.24 33 29 | -1246 583 3453 8173
Table 2.2191.6 GPS week: 2191 Day: 6 MJD: 59587
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 -26 9 69 .16 24 18 | 13899 633 3576 8143
emx n/a| -1 4 13 -14 -15 66 .11 47 34 | -9295 226 3557 8499
esx n/a| 1 0 1 -5 7 -49 -.09 37 25 | 7993 636 3561 8567
gfz n/a| 0 0 0 -13 -33 -47 -.04 29 18 | 0 164 3359 7360
grg n/a| 0 -6 3 5 -32 36 .22 29 23 | -2282 1053 3599 7652
iac n/a| -1 0 -5 36 21 -35 -.26 22 20 | -9 673 3566 8667
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 3.2191.0 GPS week: 2191 Day: 0 MJD: 59581
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 580 40 34 40 28 28 31 15 | 110 68 65 78 75 91 81
R02M | 2454 9 27 16 11 9 20 6 | 68 53 79 73 64 68 68
R03M | 946 13 30 16 13 35 29 9 | 84 64 71 83 96 102 82
XR04M | 1284 18 24 20 --- 15 33 10 | 84 71 83 --- 84 62 78
R05 | 822 18 22 19 16 17 25 8 | 83 57 84 68 66 72 71
R07M | 1328 20 28 12 26 20 42 11 | 116 68 115 101 76 125 86
R08M | 810 11 34 14 13 17 35 8 | 93 77 99 94 95 116 94
R09 | 2309 13 13 19 15 13 45 9 | 38 41 45 42 39 36 37
XR11M | 1028 21 --- 13 13 15 34 9 | 26 --- 28 28 20 39 24
R12M | 872 14 43 10 14 15 17 8 | 73 46 58 64 65 72 63
R13 | 950 35 30 32 26 52 29 15 | 96 73 72 77 74 74 77
R14M | 830 19 23 14 18 17 31 9 | 57 38 62 49 50 62 51
R15M | 1542 16 33 15 14 19 43 10 | 72 48 64 65 64 68 63
R17 | 537 6 39 23 7 14 50 10 | 38 31 43 38 38 50 36
R18 | 1261 6 53 18 15 10 30 10 | 37 35 38 39 37 54 37
R19 | 1299 31 79 71 45 60 32 23 | 46 42 47 44 54 54 41
R20 | 1071 26 64 79 16 55 48 21 | 41 60 50 61 47 42 45
R21 | 1295 9 45 23 17 30 34 11 | 39 44 39 38 48 42 38
R22 | 3760 25 39 95 46 96 50 27 | 59 58 47 54 54 52 49
R24 | 1045 11 60 22 15 40 34 13 | 36 37 35 34 48 33 34
------+-----------------------------------------+-------------------------------------
RMS | 1528 20 42 39 22 38 36 |T 64 53 61 59 59 65 57
WRMS | 1528 17 37 37 16 30 36 |NE 51 47 50 49 50 50 46
MEDI | 1045 16 34 19 15 17 33 |MD 59 53 58 61 54 62 51
Table 3.2191.1 GPS week: 2191 Day: 1 MJD: 59582
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 730 34 48 35 26 37 33 15 | 74 41 42 64 50 74 58
R02M | 2427 8 17 27 12 28 27 8 | 46 42 67 42 43 70 48
R03M | 541 8 33 19 12 29 96 15 | 78 63 74 71 79 131 76
XR04M | 1852 17 26 10 --- 17 45 11 | 66 56 62 --- 71 81 64
R05 | 683 13 27 20 14 22 36 8 | 49 36 59 44 53 75 47
XR08M | 755 14 --- 13 11 17 27 7 | 106 --- 111 109 118 132 111
R09 | 4244 15 16 14 15 25 69 11 | 26 27 32 34 39 55 29
XR11M | 1060 16 --- 20 13 15 33 9 | 28 --- 41 30 26 29 26
R12M | 979 15 35 13 17 25 24 9 | 70 52 49 58 54 74 59
R13 | 1579 39 38 22 33 60 38 17 | 75 41 63 61 57 63 59
R14M | 1232 11 32 15 19 12 36 8 | 43 30 46 37 39 49 38
R15M | 1560 10 33 13 10 14 24 7 | 65 50 61 70 65 55 62
R17 | 635 11 40 16 12 18 58 10 | 29 29 42 35 36 41 30
R18 | 1025 12 50 11 11 19 30 9 | 35 36 33 34 35 54 34
R19 | 1945 29 125 75 45 102 46 29 | 43 54 52 29 45 61 32
R20 | 1585 35 98 81 59 65 56 27 | 36 90 70 57 35 31 41
R21 | 972 7 36 22 11 16 44 9 | 26 24 32 32 30 38 26
R22 | 2561 29 68 86 29 94 36 24 | 41 47 40 39 44 32 33
R24 | 1667 24 59 20 9 40 32 12 | 32 32 29 26 41 26 26
------+-----------------------------------------+-------------------------------------
RMS | 1779 21 55 39 25 46 47 |T 53 44 55 50 50 64 47
WRMS | 1779 18 41 27 13 33 46 |NE 39 41 45 39 41 47 35
MEDI | 1232 15 36 20 13 25 36 |MD 43 41 49 42 44 55 41
Table 3.2191.2 GPS week: 2191 Day: 2 MJD: 59583
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 1027 46 43 38 30 39 44 17 | 82 41 43 63 62 60 56
R02M | 1829 8 30 23 11 34 28 9 | 61 47 77 70 55 66 63
R03M | 1137 10 36 11 11 30 45 10 | 80 56 74 83 67 111 78
XR04M | 2155 19 32 14 --- 15 37 11 | 142 125 136 --- 132 131 134
R05 | 807 19 36 16 18 17 24 9 | 62 39 62 70 53 68 59
R08M | 1109 8 40 12 21 21 48 11 | 95 93 92 106 102 77 93
R09 | 7103 17 16 17 14 24 34 9 | 50 53 54 53 56 59 50
XR11M | 991 13 --- 16 12 16 44 10 | 34 --- 44 42 37 56 39
R12M | 525 17 23 17 10 33 44 10 | 62 49 54 55 46 83 55
R13 | 1335 42 27 25 32 37 39 15 | 85 53 58 63 52 68 62
R14M | 1449 10 31 15 10 19 27 7 | 64 48 71 63 69 71 63
R15M | 920 16 22 7 17 25 34 9 | 106 90 97 85 99 115 97
R17 | 986 11 27 10 13 13 36 8 | 38 31 37 39 40 42 36
R18 | 757 10 43 20 7 13 24 8 | 39 47 40 37 40 49 39
R19 | 1198 42 115 70 36 63 39 26 | 49 73 62 59 49 45 51
R20 | 2120 29 102 91 64 81 39 30 | 46 53 55 50 40 67 44
R21 | 938 10 31 13 16 12 21 7 | 35 36 40 41 37 42 37
R22 | 2093 34 50 77 17 90 30 23 | 52 65 59 43 46 61 47
R24 | 2426 18 64 20 14 27 46 13 | 41 38 38 38 39 40 37
------+-----------------------------------------+-------------------------------------
RMS | 2192 24 51 37 24 41 36 |T 65 57 63 62 59 69 60
WRMS | 2192 23 37 26 20 31 37 |NE 49 48 50 49 45 54 46
MEDI | 1137 17 32 17 14 25 37 |MD 61 49 58 59 52 66 55
Table 3.2191.3 GPS week: 2191 Day: 3 MJD: 59584
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 466 45 41 47 36 43 27 18 | 93 50 42 84 50 54 64
R02M | 1363 11 26 20 7 18 24 7 | 72 48 76 67 66 50 65
R03M | 748 18 45 12 8 18 22 9 | 87 56 67 76 70 78 74
XR04M | 2126 15 29 12 --- 20 25 9 | 319 317 313 --- 318 319 317
R05 | 705 16 31 9 9 15 29 8 | 73 53 66 60 70 71 64
XR07M | 1041 24 --- 73 25 --- 30 23 | 133 --- 167 140 --- 136 116
R08M | 1200 11 32 11 23 16 27 9 | 154 145 146 154 151 135 148
R09 | 9605 22 18 13 13 14 45 10 | 42 44 38 43 36 59 39
R11M | 2188 13 30 17 15 20 28 8 | 34 34 42 40 40 38 35
R12M | 1219 10 37 17 18 24 50 11 | 70 53 71 79 61 98 71
R13 | 716 29 32 29 24 42 28 13 | 71 64 60 63 51 50 58
R14M | 1111 13 35 11 14 22 26 8 | 69 46 72 70 64 68 66
R15M | 962 16 25 10 11 15 22 7 | 142 136 132 135 134 149 137
R17 | 542 8 35 17 15 21 24 8 | 40 39 43 46 44 38 40
R18 | 478 12 26 20 11 17 46 10 | 43 46 47 39 51 60 43
R19 | 684 35 111 53 19 58 40 22 | 43 29 42 39 41 34 33
R20 | 2670 28 92 94 36 69 45 26 | 39 51 55 44 41 47 39
R21 | 599 11 35 18 22 21 48 11 | 42 40 40 44 50 65 42
R22 | 804 31 43 94 43 107 28 28 | 57 67 66 57 57 55 54
R24 | 1465 16 54 18 7 29 43 12 | 40 47 41 41 43 43 41
------+-----------------------------------------+-------------------------------------
RMS | 2550 21 47 38 21 39 35 |T 83 71 81 69 75 82 77
WRMS | 2550 19 36 25 17 30 37 |NE 49 48 49 47 48 52 45
MEDI | 962 16 35 17 15 21 28 |MD 69 50 60 60 51 59 58
Table 3.2191.4 GPS week: 2191 Day: 4 MJD: 59585
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 448 38 49 43 22 22 33 15 | 79 45 43 64 54 39 53
R02M | 1870 13 29 17 8 16 33 8 | 63 35 62 53 52 59 54
R03M | 1107 21 39 20 11 17 32 10 | 140 128 133 136 132 132 134
XR04M | 2579 22 31 11 --- 39 24 13 | 373 376 378 --- 372 384 376
R05 | 635 12 30 16 10 28 22 8 | 71 46 66 65 49 63 60
R07M | 1326 8 32 24 17 21 32 9 | 277 181 317 276 208 295 258
R08M | 1346 12 36 14 22 28 32 10 | 323 318 327 329 334 349 329
R09 | 1704 23 16 18 13 11 42 10 | 30 37 30 34 43 46 31
XR11M | 2731 11 --- 23 8 18 31 9 | 13 --- 24 18 25 31 14
R12M | 1574 11 46 21 12 8 38 10 | 112 102 108 117 112 121 111
R13 | 812 24 30 20 32 49 27 14 | 74 54 67 80 59 53 66
R14M | 890 14 25 17 11 23 19 7 | 100 101 105 96 92 106 98
R15M | 988 12 31 15 16 17 23 8 | 227 225 227 240 225 218 228
R17 | 1200 12 33 18 10 13 25 8 | 28 24 23 29 30 28 25
R18 | 729 12 34 19 11 14 28 8 | 30 24 28 25 30 35 26
R19 | 1246 36 125 81 50 69 44 29 | 47 41 51 57 48 40 46
R20 | 2753 20 89 79 29 54 30 22 | 36 26 40 42 38 37 35
R21 | 639 14 45 21 12 29 31 10 | 30 33 29 30 39 39 28
R22 | 946 49 41 94 38 101 25 28 | 44 55 69 60 30 47 42
R24 | 2569 17 45 21 9 22 17 9 | 27 33 25 28 39 32 26
------+-----------------------------------------+-------------------------------------
RMS | 1408 22 50 40 22 38 31 |T 106 99 107 93 100 107 102
WRMS | 1408 19 37 27 14 25 28 |NE 41 37 42 45 40 42 38
MEDI | 1200 14 34 20 12 22 30 |MD 63 46 62 60 49 47 53
Table 3.2191.5 GPS week: 2191 Day: 5 MJD: 59586
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 541 39 58 46 34 31 27 17 | 79 47 59 77 63 57 64
R02M | 1891 11 28 15 8 14 16 6 | 56 34 56 53 49 46 50
R03M | 2044 13 37 21 20 19 32 10 | 203 195 201 206 207 196 202
XR04M | 1004 23 32 14 --- 18 25 11 | 428 436 434 --- 429 421 429
R05 | 1052 15 34 15 24 37 20 11 | 66 40 57 75 43 64 57
R07M | 1726 13 33 23 15 11 35 9 | 343 314 356 337 296 349 334
R08M | 756 12 33 13 11 30 29 9 | 442 444 449 451 456 470 451
R09 | 1616 17 13 21 13 17 14 7 | 21 33 30 29 20 24 21
R11M | 2472 10 16 15 18 18 28 7 | 18 20 21 32 16 34 19
R12M | 2216 14 35 13 15 12 16 7 | 129 120 123 117 130 115 122
R13 | 883 21 50 37 26 46 26 14 | 84 93 60 80 67 73 73
R14M | 757 13 19 12 10 17 23 6 | 135 126 132 132 123 117 128
R15M | 754 10 27 12 9 16 21 6 | 293 288 291 296 289 296 292
R17 | 1441 9 37 20 7 15 47 10 | 21 21 21 17 25 30 20
R18 | 729 10 33 14 18 22 45 10 | 25 27 17 26 27 47 21
R19 | 1889 31 135 86 40 80 48 30 | 39 38 39 50 39 66 42
R20 | 2247 24 82 102 45 43 40 24 | 28 33 29 38 27 37 27
R21 | 599 8 46 20 19 15 33 10 | 26 23 28 28 24 41 25
R22 | 863 29 28 98 47 44 61 23 | 34 34 51 54 44 53 29
R24 | 1449 14 47 21 15 17 33 10 | 31 37 31 23 35 37 27
------+-----------------------------------------+-------------------------------------
RMS | 1499 18 49 43 24 31 33 |T 125 120 124 111 120 128 121
WRMS | 1499 16 37 27 17 20 29 |NE 37 37 36 42 35 47 34
MEDI | 1052 13 33 20 18 18 28 |MD 56 38 56 54 44 57 50
Table 3.2191.6 GPS week: 2191 Day: 6 MJD: 59587
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 845 55 45 39 50 40 23 19 | 104 55 71 112 58 67 77
R02M | 1444 11 27 28 15 18 34 10 | 73 43 84 73 69 59 67
R03M | 840 16 31 17 22 14 22 9 | 143 129 132 146 144 133 138
XR04M | 1529 24 34 15 --- 12 15 10 | 555 557 555 --- 551 557 555
R05 | 1322 27 41 15 16 19 15 10 | 90 58 80 83 66 81 77
R07M | 922 19 29 14 16 30 17 9 | 269 296 247 270 301 257 276
R08M | 1653 13 26 11 14 13 16 6 | 363 354 358 362 357 339 356
R09 | 975 14 19 9 12 17 22 7 | 33 34 33 33 35 30 30
R11M | 1494 13 17 13 21 10 21 7 | 30 22 34 31 33 43 31
R12M | 2066 14 27 17 12 12 14 7 | 102 84 86 94 92 107 95
R13 | 1557 29 50 41 24 40 23 15 | 105 75 68 93 76 92 84
R14M | 519 11 21 13 9 9 14 5 | 102 84 94 90 97 100 95
R15M | 671 8 20 9 15 12 17 6 | 284 279 280 276 283 288 281
R17 | 1490 17 27 11 12 15 24 8 | 31 28 31 29 36 41 31
R18 | 890 11 36 8 20 14 8 7 | 33 28 35 37 40 43 34
R19 | 1297 40 125 68 36 60 27 26 | 47 31 38 44 40 49 39
R20 | 1301 31 79 81 43 45 32 23 | 44 42 35 48 41 47 39
R21 | 762 13 40 20 24 12 14 9 | 45 43 44 49 46 39 43
R22 | 923 33 37 90 77 55 41 26 | 46 59 56 55 44 60 44
R24 | 960 15 51 20 9 30 12 10 | 29 35 32 29 40 40 31
------+-----------------------------------------+-------------------------------------
RMS | 1218 24 47 37 29 29 22 |T 126 116 119 102 122 123 121
WRMS | 1218 18 34 25 18 23 20 |NE 50 43 45 50 46 52 45
MEDI | 975 15 31 15 16 15 17 |MD 73 55 68 73 58 60 67
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