[IGSREPORT-27632] Wk 2132 IGLOS Final Orbits
acc
acc at igs.org
Thu Dec 3 18:36:07 PST 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2132 (Nov 15, 2020 - Nov 21, 2020)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.2132.
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:
igl2132[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2132 in the SP3 format.
igl21327.sum Combination Report for GPS Week 2132.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 0.3 ns
1 | 1.0 ns
2 | 1.5 ns
3 | 0.6 ns
4 | -0.0 ns
5 | 0.5 ns
6 | -0.1 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
----+--------+---------------
0 | IAC | R23
1 | IAC | R23
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 1.2132, 1a.2132).
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 2.2132.0-6)
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 3.2132.0-6).
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 2132 summary. (Nov 15, 2020 - Nov 21, 2020)
Table 1.2132.a GPS week : 2132 MJD: 59168.0-59174.0
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 -1 3 3 14 15 .26 26 22 | 18112 -869 3069 7704
| 1 1 1 14 15 17 .07 | 1192 1406
emx n/a| 0 0 -10 -37 0 -7 .18 33 32 | -1368 -815 3062 7789
| 1 1 1 34 24 43 .07 | 9920 856
esx n/a| 0 2 0 18 -45 26 .08 31 26 | 596 -1721 3066 9982
| 2 1 1 17 17 25 .09 | 10960 1487
gfz n/a| -1 -1 0 -12 -17 -37 .00 32 19 | 0 -261 3071 7457
| 2 1 1 18 14 16 .06 | 0 1264
grg n/a| 2 0 2 13 7 -61 -.37 24 20 | 772 -525 3064 7071
| 1 1 3 19 24 34 .08 | 640 1408
iac n/a| -1 0 2 18 38 96 -.05 98 71 | 2616 -464 3065 7934
| 2 1 3 40 38 78 .28 | 1039 809
mcc n/a| 5 -2 -8 53 46 -14 -.30 204 204 | --- --- --- ---
| 7 15 8 124 190 755 .50 | --- ---
Table 1.2132.b GPS week : 2132 MJD: 59168.0-59174.0
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 18 18 14 16 14 16 |
R02 | 7 7 7 7 7 9 8 |
R03 | 6 8 9 8 6 8 5 |
R04 | 10 10 8 9 10 9 10 |
R05 | 11 12 10 8 12 11 11 |
R07 | 9 8 9 8 8 7 7 |
R08 | 9 8 8 10 9 8 7 |
R09 | 8 9 12 8 8 7 9 |
R11 | 7 7 9 10 0 --- --- |
R12 | 8 8 11 11 9 10 11 |
R13 | 15 16 18 17 17 15 16 |
R14 | 7 8 11 16 9 8 8 |
R15 | 10 11 13 10 10 9 8 |
R16 | 12 13 17 11 12 13 13 |
R17 | 12 8 9 9 9 9 9 |
R18 | 10 8 7 7 9 8 9 |
R19 | 26 25 26 28 29 24 28 |
R20 | 25 25 26 24 24 21 23 |
R21 | 8 10 10 10 10 11 9 |
R22 | 17 18 22 23 17 13 10 |
R23 | 13 15 11 12 14 12 11 |
R24 | 12 9 9 8 9 8 12 |
R25 | --- 0 0 0 23 18 43 |
Table 1.2132.c GPS week : 2132 MJD: 59168.0-59174.0
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 2132 0 | -38 42 114 91 2856 3104 80.3 4774 4774 | 328 0
brd 2132 1 | 66 32 113 240 1608 1732 82.4 1843 1843 | 1028 0
brd 2132 2 | 17 -15 129 -800 730 2543 80.3 1660 1660 | 1472 0
brd 2132 3 | 17 97 168 -1357 1026 -4 80.8 1709 1709 | 567 0
brd 2132 4 | -64 25 59 -262 -1268 1658 80.2 1667 1667 | -30 0
brd 2132 5 | -17 -43 98 715 611 713 80.9 1581 1581 | 486 0
brd 2132 6 | -30 -15 64 89 -1465 3971 81.2 1532 1532 | -148 0
-------------+------------------------------------------------------------+----------------
brd 2132 mean| -7 17 107 -183 585 1959 80.9 2109 2109 | 529 0
brd 2132 sdev| 43 47 37 695 1530 1369 .8 1179 1179 | 570 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 2.2132.0 GPS week: 2132 Day: 0 MJD: 59168
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 -9 17 9 .20 23 18 | 16637 -2167 2880 7661
emx n/a| -2 -1 -9 -62 -12 -4 .12 31 28 | -10717 -1185 2892 7681
esx n/a| 0 2 0 46 -33 0 .11 31 21 | -9519 -2690 2897 10123
gfz n/a| -4 0 0 2 2 -21 .08 27 19 | 0 -1405 2928 7066
grg n/a| 3 1 -3 28 20 -25 -.42 26 19 | 1041 -1300 2883 6856
iac n/a| -2 0 3 -17 19 47 -.06 454 265 | 1492 761 2894 7917
mcc n/a| 1 -11 -17 -75 111 -885 -.50 185 185 | --- --- --- ---
Table 2.2132.1 GPS week: 2132 Day: 1 MJD: 59169
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 -3 4 -4 19 -1 .27 24 20 | 16749 -1116 3022 7725
emx n/a| 0 1 -9 -24 2 12 .23 33 33 | 6093 -1271 3009 7616
esx n/a| -2 2 0 25 -60 42 .19 28 20 | 6732 -2460 3017 9450
gfz n/a| 0 -3 0 2 -5 -41 -.07 28 17 | 0 -591 3082 7473
grg n/a| 4 2 0 11 43 -59 -.29 25 22 | 1570 -778 3016 6622
iac n/a| 0 0 6 29 -28 68 -.28 80 88 | 3636 -517 3021 7843
mcc n/a| 2 -10 0 74 48 -187 -.70 202 202 | --- --- --- ---
Table 2.2132.2 GPS week: 2132 Day: 2 MJD: 59170
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 -3 3 29 37 -2 .35 25 22 | 18113 114 3403 8211
emx n/a| 0 -1 -10 -24 30 19 .27 32 33 | 5867 -401 3385 8342
esx n/a| -3 2 -2 1 -66 40 .18 34 29 | 6995 -1249 3390 10496
gfz n/a| 0 0 0 -1 -35 -15 .07 35 16 | 0 1520 3277 8154
grg n/a| 1 2 4 -5 -14 -44 -.42 26 22 | 1306 269 3406 7620
iac n/a| -2 0 5 -39 55 53 -.49 38 36 | 4237 -1011 3395 8353
mcc n/a| 19 -20 0 34 22 739 -.10 159 159 | --- --- --- ---
Table 2.2132.3 GPS week: 2132 Day: 3 MJD: 59171
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 14 19 1 .34 25 23 | 17728 760 3456 8253
emx n/a| 1 0 -9 -19 -34 -97 .26 33 33 | 12951 182 3462 8409
esx n/a| -1 3 -1 -6 -36 12 .07 32 33 | 2743 992 3448 10808
gfz n/a| -3 0 0 -32 -21 -45 .01 35 23 | 0 279 3340 8150
grg n/a| 0 0 1 30 -4 -47 -.48 24 21 | -92 938 3446 7846
iac n/a| 4 -1 0 50 95 260 .02 35 35 | 2990 -536 3440 8429
mcc n/a| 7 25 -20 38 23 1106 .73 199 199 | --- --- --- ---
Table 2.2132.4 GPS week: 2132 Day: 4 MJD: 59172
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -2 0 -2 8 36 .17 29 28 | 19165 -2061 3345 7763
emx n/a| 1 0 -12 -54 -5 -13 .09 35 36 | -13409 -1833 3323 7911
esx n/a| -1 1 1 14 -23 37 -.03 32 29 | -14539 -2969 3335 9750
gfz n/a| 0 0 1 -43 -6 -48 .02 32 19 | 0 -1176 3392 7530
grg n/a| 1 -1 3 8 13 -105 -.39 21 16 | 681 -1868 3327 7200
iac n/a| -4 1 0 79 38 123 .36 31 29 | 2372 -1587 3329 8077
mcc n/a| 0 4 -3 143 -336 320 -.62 160 160 | --- --- --- ---
Table 2.2132.5 GPS week: 2132 Day: 5 MJD: 59173
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 -2 2 6 -11 35 .24 28 23 | 18535 783 2625 7325
emx n/a| -1 -2 -9 11 34 38 .14 32 32 | -2358 338 2604 7361
esx n/a| 1 3 0 20 -36 61 -.02 28 24 | -5307 -694 2629 9334
gfz n/a| 0 -2 -3 -5 -31 -27 -.01 32 20 | 0 1165 2673 7157
grg n/a| 2 0 5 -16 22 -111 -.37 18 16 | -52 1354 2622 6962
iac n/a| -3 -1 0 16 30 29 .17 26 25 | 1786 411 2608 7538
mcc n/a| 0 -10 -12 261 227 -700 -.62 214 214 | --- --- --- ---
Table 2.2132.6 GPS week: 2132 Day: 6 MJD: 59174
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 -6 8 25 .24 24 20 | 19862 -2401 2757 6990
emx n/a| 0 0 -11 -92 -14 -9 .16 31 31 | -8004 -1541 2760 7207
esx n/a| 2 0 -2 28 -63 -8 .03 28 23 | 17068 -2983 2751 9915
gfz n/a| 0 0 0 -6 -21 -61 -.08 33 19 | 0 -1619 2808 6674
grg n/a| 0 1 7 36 -26 -35 -.23 27 21 | 951 -2295 2754 6391
iac n/a| 0 -1 3 6 57 94 -.08 25 22 | 1800 -772 2773 7383
mcc n/a| 4 2 -2 -103 227 -494 -.29 311 311 | --- --- --- ---
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 3.2132.0 GPS week: 2132 Day: 0 MJD: 59168
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 622 31 42 38 39 26 21 --- 15 | 34 43 30 36 35 53 --- 32
R02 | 979 10 12 14 10 14 29 --- 6 | 23 20 25 25 17 33 --- 20
R03 | 956 8 12 11 10 16 16 104 5 | 20 19 25 21 22 23 74 18
XR04 | 911 7 6 19 --- 26 35 --- 10 | 27 29 26 --- 36 30 --- 25
R05M | 1064 18 24 27 27 18 29 --- 10 | 23 24 36 32 30 32 --- 21
R07 | 579 14 14 12 32 12 24 302 8 | 22 20 23 34 23 21 221 19
R08M | 1198 15 19 22 18 20 32 --- 9 | 18 17 33 35 31 33 --- 21
R09E | 3919 15 18 14 17 21 25 --- 8 | 93 93 96 96 93 87 --- 92
R11E | 1655 17 12 10 11 18 24 130 7 | 27 25 24 25 29 44 103 27
R12E | 1438 17 21 10 18 17 21 --- 8 | 130 126 127 132 125 128 --- 127
R13E | 678 40 30 35 28 21 42 --- 14 | 66 53 61 61 63 71 --- 56
R14E | 486 14 18 17 12 13 22 --- 7 | 57 55 70 66 64 68 --- 61
R15E | 1115 18 30 23 18 13 23 --- 9 | 68 67 63 72 64 78 --- 65
R16E | 2220 22 24 29 28 30 21 --- 11 | 119 108 111 106 122 105 --- 111
R17M | 2138 14 33 23 16 15 48 --- 11 | 77 60 60 74 70 90 --- 70
R18M | 1711 15 22 18 12 11 47 --- 10 | 65 61 71 69 70 93 --- 68
R19M | 1311 53 69 69 61 44 56 --- 26 | 87 38 59 96 61 82 --- 59
R20M |20681 28 68 82 37 56 46 --- 24 | 92 52 50 73 97 77 --- 64
R21 | 478 18 25 15 18 11 18 135 8 | 75 55 57 72 67 71 56 65
R22 | 1332 20 27 21 39 51 58 --- 17 | 63 58 74 66 78 67 --- 64
R23M | 2285 24 24 29 27 21 2078 --- 12 | 69 54 81 53 74 9999 --- 64
R24M | 1523 17 31 23 19 31 32 --- 11 | 62 49 48 65 67 69 --- 57
------+----------------------------------------------+------------------------------------------
RMS | 4774 23 31 31 27 26 454 185 |T 59 51 56 62 60 64 113 54
WRMS | 4774 18 28 21 19 19 265 185 |NE 37 34 37 42 39 42 117 34
MEDI | 1198 17 24 21 18 18 29 130 |MD 63 52 57 66 64 69 74 59
Table 3.2132.1 GPS week: 2132 Day: 1 MJD: 59169
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 881 37 41 27 47 33 52 --- 17 | 28 32 26 63 25 56 --- 26
R02 | 972 12 21 12 15 10 23 357 7 | 20 19 32 32 22 33 413 22
R03 | 632 12 14 10 15 16 35 88 7 | 24 22 27 22 22 45 50 21
XR04 | 942 10 9 14 --- 22 34 --- 9 | 27 27 28 --- 35 32 --- 25
R05M | 2770 29 24 21 31 11 42 --- 12 | 29 29 37 49 26 42 --- 27
R07 | 1091 6 10 16 15 27 26 179 8 | 27 27 23 21 38 29 97 22
R08M | 1411 11 17 10 15 15 35 --- 7 | 26 25 34 33 30 33 --- 26
R09E | 3196 18 17 10 22 22 23 --- 8 | 75 77 77 81 75 77 --- 75
R11E | 977 11 18 10 13 20 18 147 6 | 37 39 40 34 32 39 53 36
R12E | 1568 20 27 14 15 15 18 --- 8 | 106 98 100 104 97 104 --- 100
R13E | 786 40 38 36 37 31 30 --- 16 | 59 49 48 59 60 68 --- 50
R14E | 924 14 22 19 12 13 23 --- 7 | 39 39 45 42 38 40 --- 37
R15E | 1225 17 27 14 17 23 52 --- 11 | 83 82 86 84 89 66 --- 81
R16E | 2083 23 28 20 19 39 44 --- 13 | 131 124 141 131 143 115 --- 130
R17M | 3079 18 22 21 14 11 19 --- 8 | 48 44 42 49 48 50 --- 45
R18M | 1741 18 21 16 16 15 27 --- 8 | 43 45 52 55 53 52 --- 48
R19M | 2019 51 69 60 53 37 57 --- 24 | 53 48 49 52 47 80 --- 45
R20M | 1754 38 80 69 48 34 52 --- 24 | 64 38 47 71 61 78 --- 52
R21 | 567 10 30 19 19 20 32 125 9 | 52 40 47 55 45 68 30 48
R22 | 1267 24 27 39 52 46 38 --- 17 | 51 48 64 44 55 60 --- 46
R23M | 2335 29 15 36 31 27 332 --- 14 | 69 62 71 58 78 656 --- 66
R24M | 3214 16 27 20 11 20 27 --- 9 | 43 40 43 38 46 39 --- 38
XR25E | ---- 5 --- --- --- --- --- --- 0 | 101 --- --- --- --- --- --- 102
------+----------------------------------------------+------------------------------------------
RMS | 1842 24 33 28 28 25 80 202 |T 53 47 52 56 52 84 128 50
WRMS | 1842 20 33 20 17 22 88 202 |NE 32 30 35 39 34 46 147 30
MEDI | 1267 18 22 19 17 20 32 147 |MD 48 40 45 52 46 52 53 45
Table 3.2132.2 GPS week: 2132 Day: 2 MJD: 59170
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1786 43 43 37 49 23 33 --- 17 | 24 38 46 61 38 44 --- 32
R02 | 1323 10 11 12 10 17 30 208 7 | 23 22 33 30 34 25 221 24
R03 | 525 9 12 25 21 15 33 85 8 | 18 20 41 22 26 44 59 21
XR04 | 840 14 13 14 --- 13 22 --- 7 | 18 21 23 --- 16 29 --- 14
R05M | 2250 20 17 28 21 16 37 --- 10 | 22 19 37 34 15 44 --- 18
R07 | 1435 13 12 25 12 15 34 138 8 | 21 26 37 26 33 42 59 22
R08M | 892 16 12 17 11 19 35 --- 8 | 20 24 34 22 37 36 --- 22
R09E | 2622 19 23 23 14 21 53 --- 11 | 52 56 60 60 65 78 --- 56
R11E | 467 11 26 16 12 16 40 197 9 | 46 44 32 36 42 57 89 41
R12E | 1345 14 29 22 18 27 34 --- 10 | 129 123 126 124 136 137 --- 127
R13E | 1133 42 46 40 35 32 40 --- 17 | 60 53 60 54 60 64 --- 51
R14E | 2024 14 26 23 21 19 40 --- 10 | 71 69 78 74 79 66 --- 70
R15E | 1771 17 22 15 19 44 46 --- 13 | 140 143 145 148 129 153 --- 139
R16E | 1027 28 22 48 47 43 32 --- 17 | 92 100 115 121 88 99 --- 96
R17M | 3069 22 24 20 15 12 27 --- 9 | 53 37 37 46 40 57 --- 42
R18M | 1044 10 16 19 18 13 21 --- 7 | 42 39 54 58 42 59 --- 46
R19M | 1021 39 60 58 80 47 57 --- 25 | 61 59 45 73 38 80 --- 47
R20M | 1175 48 77 80 57 33 42 --- 26 | 75 58 40 61 43 62 --- 46
R21 | 575 19 31 20 9 22 34 137 10 | 57 39 40 44 59 65 34 48
R22 | 1349 29 38 48 79 37 44 --- 21 | 48 44 76 66 71 60 --- 51
R23M | 1930 27 21 29 23 22 28 --- 11 | 29 37 55 49 53 277 --- 42
R24M | 2723 19 24 14 14 13 31 --- 8 | 42 27 27 31 26 40 --- 28
XR25E | ---- 7 --- --- --- --- --- --- 0 | 81 --- --- --- --- --- --- 82
------+----------------------------------------------+------------------------------------------
RMS | 1659 25 32 34 35 26 38 159 |T 53 49 56 59 53 73 92 50
WRMS | 1659 22 33 29 16 22 36 159 |NE 29 30 42 41 39 44 93 30
MEDI | 1323 19 23 23 19 19 34 138 |MD 48 39 41 54 42 59 59 46
Table 3.2132.3 GPS week: 2132 Day: 3 MJD: 59171
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2027 38 27 43 24 14 38 --- 14 | 50 59 62 66 47 46 --- 50
R02 | 1879 14 11 13 19 14 25 256 7 | 37 45 42 43 41 39 100 38
R03 | 609 9 8 18 19 18 33 89 8 | 41 41 43 37 40 47 49 39
XR04 | 937 11 12 13 --- 13 35 --- 8 | 46 48 51 --- 52 46 --- 46
R05M | 1372 17 13 23 15 10 30 --- 8 | 45 45 56 51 47 47 --- 45
R07 | 855 17 19 15 12 10 32 209 8 | 41 43 48 40 45 45 174 41
R08M | 1531 13 15 24 23 8 48 --- 10 | 40 39 48 42 36 60 --- 39
R09E | 2838 15 15 22 16 15 25 --- 8 | 61 67 66 66 64 59 --- 62
R11E | 844 13 26 15 13 19 37 238 9 | 51 51 48 46 53 49 144 42
R12E | 487 20 30 15 15 27 34 --- 11 | 133 131 128 125 135 136 --- 130
R13E | 1159 48 43 35 34 22 32 --- 16 | 70 69 72 74 73 74 --- 66
R14E | 2491 16 40 18 26 30 72 --- 16 | 89 81 81 82 99 101 --- 83
R15E | 2149 14 27 19 26 23 16 --- 9 | 256 260 255 250 261 273 --- 258
R16E | 2085 16 19 30 26 26 33 --- 11 | 130 122 120 128 139 129 --- 126
R17M | 2390 22 25 22 19 12 17 --- 9 | 71 58 56 66 57 61 --- 60
R18M | 1694 14 19 11 11 17 23 --- 7 | 69 64 68 64 73 73 --- 67
R19M | 613 41 80 65 90 49 33 --- 28 | 91 88 74 120 83 87 --- 82
R20M | 1135 51 70 72 57 21 35 --- 23 | 86 37 47 79 55 47 --- 52
R21 | 564 27 28 22 10 11 36 158 10 | 73 53 52 64 56 72 64 59
R22 | 2120 25 33 49 74 55 51 --- 22 | 56 79 89 71 70 89 --- 66
R23M | 1642 26 19 36 37 20 23 --- 12 | 77 84 95 76 86 146 --- 81
R24M | 2249 12 24 16 19 10 24 --- 7 | 60 53 55 57 49 57 --- 52
XR25E | ---- 6 --- --- --- --- --- --- 0 | 38 --- --- --- --- --- --- 37
------+----------------------------------------------+------------------------------------------
RMS | 1708 25 33 32 35 24 35 199 |T 74 73 75 78 75 81 106 70
WRMS | 1708 23 33 33 23 21 35 199 |NE 49 52 55 53 50 54 96 48
MEDI | 1531 16 24 22 19 17 33 209 |MD 61 58 56 66 56 60 100 59
Table 3.2132.4 GPS week: 2132 Day: 4 MJD: 59172
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1872 53 26 44 38 16 25 --- 16 | 49 45 62 53 45 46 --- 45
R02 | 2325 14 10 11 12 12 29 200 7 | 39 40 46 42 37 48 98 40
R03 | 940 14 10 11 6 9 22 45 5 | 39 40 42 40 45 50 75 40
XR04 | 892 13 20 13 --- 9 39 --- 10 | 41 42 35 --- 41 51 --- 39
R05M | 633 25 23 31 25 16 32 --- 11 | 42 46 58 44 50 41 --- 43
R07 | 582 19 16 7 15 13 30 114 7 | 46 47 39 40 51 46 106 42
R08M | 812 12 15 23 27 15 27 --- 9 | 42 38 48 50 51 53 --- 44
R09E | 2698 16 13 10 22 19 25 --- 8 | 73 75 75 70 76 70 --- 71
XR11E |19186 --- --- --- --- --- 9 86 0 | --- --- --- --- --- 47 72 42
R12E | 533 12 30 20 19 21 18 --- 9 | 164 166 160 159 162 168 --- 162
R13E | 1245 34 54 38 36 29 36 --- 17 | 51 57 49 59 61 57 --- 48
R14E | 1572 16 25 13 21 18 30 --- 9 | 58 60 65 64 68 69 --- 61
R15E | 2231 15 33 20 19 16 33 --- 10 | 379 378 384 378 380 367 --- 378
R16E | 3105 22 26 26 39 19 23 --- 11 | 60 57 62 68 61 75 --- 59
R17M | 2137 19 25 17 17 11 29 --- 8 | 63 54 56 63 57 65 --- 57
R18M | 2007 19 15 16 23 13 33 --- 9 | 62 60 63 61 56 71 --- 59
R19M | 1146 57 97 57 76 50 40 --- 28 | 104 63 86 102 104 125 --- 90
R20M | 1510 61 65 70 52 18 48 --- 23 | 77 42 46 67 58 57 --- 47
R21 | 462 30 21 18 13 12 33 218 9 | 70 51 54 57 53 62 44 55
R22 | 1439 28 28 38 41 42 40 --- 16 | 62 57 77 65 78 58 --- 63
R23M | 1067 25 14 48 44 19 28 --- 14 | 63 70 101 66 64 181 --- 68
R24M | 1593 14 33 15 16 11 24 --- 8 | 58 53 56 61 53 61 --- 55
XR25E | ---- 20 --- --- --- --- 24 --- 22 | 45 --- --- --- --- 45 --- 52
------+----------------------------------------------+------------------------------------------
RMS | 1666 29 35 32 32 21 31 160 |T 76 73 79 80 78 83 79 72
WRMS | 1666 28 36 29 19 16 29 160 |NE 49 46 50 49 50 51 80 46
MEDI | 1439 19 25 20 22 16 29 114 |MD 58 54 58 61 57 58 75 55
Table 3.2132.5 GPS week: 2132 Day: 5 MJD: 59173
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 877 48 19 44 32 11 19 --- 14 | 24 35 51 53 40 35 --- 35
R02 | 2392 11 12 17 12 12 37 348 8 | 16 16 26 21 20 31 182 16
R03 | 1337 15 14 16 10 26 17 94 8 | 20 17 24 21 26 22 69 18
XR04 | 888 13 18 11 --- 14 27 --- 8 | 22 19 26 --- 19 19 --- 18
R05M | 645 23 28 26 29 18 28 --- 11 | 23 28 49 46 30 30 --- 28
R07 | 1233 10 12 17 10 13 28 44 7 | 17 21 25 22 14 28 65 16
R08M | 1041 16 10 15 25 16 22 --- 8 | 19 26 23 31 22 33 --- 22
R09E | 1320 15 16 11 18 14 18 --- 6 | 57 54 60 64 63 65 --- 59
R12E | 1326 10 33 22 17 23 23 --- 10 | 112 110 118 116 112 117 --- 112
R13E | 907 33 51 32 31 20 34 --- 14 | 45 36 47 50 45 48 --- 40
R14E | 1019 8 28 10 14 15 22 --- 7 | 32 31 34 39 35 39 --- 32
R15E | 2119 10 32 17 23 13 23 --- 9 | 395 410 402 400 401 405 --- 401
R16E | 3459 25 40 18 32 16 38 --- 12 | 80 95 88 95 84 93 --- 85
R17M | 2041 10 30 18 20 15 22 --- 8 | 45 37 45 52 54 44 --- 45
R18M | 1704 15 24 10 20 14 17 --- 7 | 56 58 57 62 56 61 --- 56
R19M | 1627 60 70 50 70 31 43 --- 24 | 85 87 85 109 63 92 --- 78
R20M | 1884 58 54 65 59 15 23 --- 21 | 63 37 45 60 27 33 --- 33
R21 | 536 22 25 25 35 16 28 225 11 | 49 35 36 55 34 32 32 35
R22 | 1045 22 15 25 47 28 19 --- 12 | 41 56 52 52 51 41 --- 46
R23M | 1371 25 24 37 35 12 22 --- 11 | 40 53 63 45 46 172 --- 48
R24M | 591 27 27 14 15 10 14 --- 8 | 46 25 38 29 28 38 --- 32
XR25E | ---- 17 --- --- --- --- 18 --- 18 | 48 --- --- --- --- 35 --- 45
------+----------------------------------------------+------------------------------------------
RMS | 1581 28 32 28 32 18 26 214 |T 60 61 66 71 60 68 80 59
WRMS | 1581 23 32 24 20 16 25 214 |NE 27 28 34 37 29 29 87 26
MEDI | 1320 16 25 18 23 15 22 94 |MD 45 36 47 52 40 38 65 35
Table 3.2132.6 GPS week: 2132 Day: 6 MJD: 59174
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 536 31 45 27 34 31 48 --- 16 | 53 66 50 61 39 53 --- 46
R02 | 3171 11 15 10 13 19 27 548 7 | 28 38 40 41 41 38 389 34
R03 | 1084 6 11 9 8 8 20 125 5 | 30 31 36 31 45 43 93 34
XR04 | 1012 8 14 14 --- 29 29 --- 10 | 33 38 35 --- 54 42 --- 36
R05M | 681 17 13 23 39 26 24 --- 11 | 36 40 52 66 49 38 --- 41
R07 | 994 7 11 27 15 12 18 146 7 | 34 34 51 38 42 36 153 37
R08M | 668 14 16 17 14 12 15 --- 6 | 32 35 33 33 34 41 --- 31
R09E | 976 18 12 8 19 20 30 --- 8 | 62 68 67 63 62 77 --- 65
R12E | 1864 10 36 24 24 26 15 --- 10 | 122 127 116 125 120 118 --- 120
R13E | 574 22 41 31 50 34 28 --- 15 | 55 60 61 67 50 57 --- 50
R14E | 1258 11 22 15 17 19 17 --- 7 | 36 42 35 38 37 43 --- 35
R15E | 1522 15 23 11 13 16 18 --- 7 | 453 463 459 451 452 457 --- 455
R16E | 3533 21 32 26 39 29 28 --- 13 | 97 95 88 86 94 97 --- 90
R17M | 1358 20 28 17 11 15 23 --- 8 | 69 48 46 59 48 64 --- 55
R18M | 1118 13 21 17 30 16 22 --- 9 | 73 72 76 58 71 88 --- 72
R19M | 1680 43 72 68 97 41 33 --- 27 | 110 96 94 150 105 88 --- 98
R20M | 1770 68 48 49 29 62 32 --- 23 | 87 39 42 64 70 42 --- 45
R21 | 485 22 28 24 16 13 14 220 9 | 68 45 43 64 52 54 43 53
R22 | 1311 17 15 23 35 24 19 --- 10 | 53 53 63 60 69 60 --- 55
R23M | 1050 13 19 39 24 25 18 --- 11 | 65 79 93 59 53 209 --- 69
R24M | 488 26 40 22 13 26 19 --- 11 | 62 41 39 46 34 57 --- 45
XR25E | ---- 35 --- --- --- --- 49 --- 42 | 54 --- --- --- --- 49 --- 61
------+----------------------------------------------+------------------------------------------
RMS | 1531 24 31 28 33 27 25 311 |T 77 76 77 83 77 84 148 73
WRMS | 1531 20 31 23 19 21 22 311 |NE 42 43 45 49 48 46 169 42
MEDI | 1084 17 22 23 19 24 22 146 |MD 55 48 51 60 52 54 93 50
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