[IGSREPORT-26619] Wk 2054 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 10 18:06:43 PDT 2019
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2054 (May 19, 2019 - May 25, 2019)
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 2.2054.
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:
igl2054[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2054 in the SP3 format.
igl20547.sum Combination Report for GPS Week 2054.
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 | -2.0 ns
1 | -2.8 ns
2 | -2.7 ns
3 | -1.5 ns
4 | -2.7 ns
5 | -3.1 ns
6 | -2.1 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 1.2054, 1a.2054).
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 2.2054.0-6)
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 3.2054.0-6).
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 2054 summary. (May 19, 2019 - May 25, 2019)
Table 1.2054.a GPS week : 2054 MJD: 58622.0-58628.0
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 22 -22 27 .11 19 16 | 12847 -802 3138 11780
| 0 0 1 21 11 20 .05 | 988 1340
cof n/a| 0 0 1 23 -3 20 .13 24 18 | 12841 -795 3139 11786
| 1 0 3 20 23 33 .09 | 979 1331
emx n/a| 0 0 3 7 6 40 -.01 23 23 | 1434 -389 3144 11565
| 1 1 2 16 23 30 .07 | 13818 824
esx n/a| 0 0 -1 26 0 21 .12 19 15 | 6022 -463 3137 14190
| 0 1 2 12 7 24 .05 | 14906 1483
gfz n/a| 0 0 -2 -16 9 -19 .13 27 19 | 0 -699 3135 11567
| 1 1 2 24 8 31 .07 | 0 1213
grg n/a| 1 0 -4 -59 20 -100 -.30 22 20 | -2061 -679 3134 11178
| 1 1 2 18 13 59 .06 | 294 1141
iac n/a| -2 0 1 -1 -5 15 -.07 22 20 | -1259 -585 3137 11466
| 2 1 3 34 24 29 .05 | 220 789
mcc n/a| 0 -1 -16 95 -103 564 -.07 177 177 | --- --- --- ---
| 13 5 21 227 77 542 .37 | --- ---
Table 1.2054.b GPS week : 2054 MJD: 58622.0-58628.0
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 | 12 18 18 20 16 14 12 |
R02 | 8 8 7 7 7 6 6 |
R03 | 5 6 6 7 6 7 9 |
R04 | 5 5 6 6 6 6 6 |
R05 | 10 7 8 10 7 9 9 |
R07 | 6 7 7 6 6 7 6 |
R08 | 6 8 6 6 6 7 6 |
R09 | 6 6 8 8 8 7 9 |
R10 | 7 8 7 9 7 7 8 |
R11 | 8 9 8 7 6 7 6 |
R13 | 10 8 7 8 8 10 9 |
R14 | 8 8 8 8 10 7 8 |
R15 | 9 9 8 9 9 9 10 |
R16 | 15 14 14 15 14 14 14 |
R17 | 7 7 7 7 7 7 8 |
R18 | 7 7 5 7 6 6 7 |
R19 | 20 17 19 20 21 22 15 |
R20 | 13 11 13 14 11 12 12 |
R21 | 9 8 9 7 10 7 7 |
R22 | 8 8 9 10 8 9 8 |
R23 | 9 11 10 9 11 10 9 |
R24 | 13 12 12 13 13 14 13 |
R26 | 17 32 18 18 14 15 35 |
Table 1.2054.c GPS week : 2054 MJD: 58622.0-58628.0
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 2054 0 | 10 15 114 -1327 1072 5521 81.5 1505 1505 | -1986 0
brd 2054 1 | 51 -21 102 255 1159 3773 83.6 1594 1594 | -2843 0
brd 2054 2 | -36 -32 133 288 -1334 4864 82.6 1599 1599 | -2742 0
brd 2054 3 | 11 29 143 513 -40 3738 82.4 1674 1674 | -1533 0
brd 2054 4 | -69 -47 126 1125 -39 1771 83.9 1539 1539 | -2731 0
brd 2054 5 | 35 69 227 112 -422 2640 82.7 1498 1498 | -3079 0
brd 2054 6 | -36 55 197 -590 -176 2085 83.2 1509 1509 | -2131 0
-------------+------------------------------------------------------------+----------------
brd 2054 mean| -4 9 149 53 31 3484 82.8 1559 1559 | -2435 0
brd 2054 sdev| 43 45 45 793 863 1402 .8 65 65 | 558 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 2.2054.0 GPS week: 2054 Day: 0 MJD: 58622
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 56 -29 59 .05 21 19 | 11894 964 3467 11866
cof n/a| 1 0 1 49 -3 57 .13 24 20 | 11909 945 3470 11870
emx n/a| 0 2 2 22 26 91 -.00 25 25 | 13731 581 3474 11567
esx n/a| 0 0 -3 14 -5 24 .14 16 14 | 17098 1064 3461 13837
gfz n/a| 0 -1 -5 -42 11 -34 .14 26 19 | 0 82 3460 11715
grg n/a| 3 -2 -6 -75 23 -171 -.26 22 21 | -2283 438 3475 11408
iac n/a| -3 -2 6 12 -18 16 -.05 21 20 | -1451 -468 3463 11580
mcc n/a| 0 0 -1 62 -120 501 -.08 191 191 | --- --- --- ---
Table 2.2054.1 GPS week: 2054 Day: 1 MJD: 58623
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 15 -28 5 .06 21 16 | 13550 -1792 3280 11619
cof n/a| 0 -1 3 37 -9 -4 .01 25 20 | 13539 -1775 3283 11618
emx n/a| -1 0 7 -24 -41 23 -.12 23 23 | -3843 -1024 3293 11410
esx n/a| 1 0 -4 50 5 67 .11 17 14 | 1600 -1351 3290 14461
gfz n/a| 2 0 -5 30 5 -5 .21 23 18 | 0 -1199 3290 11353
grg n/a| 1 -1 -4 -39 32 -183 -.27 22 20 | -2092 -1048 3271 11101
iac n/a| -2 1 1 -63 -2 32 -.05 21 19 | -1229 -985 3274 11284
mcc n/a| 25 7 -20 -98 -140 981 .43 151 151 | --- --- --- ---
Table 2.2054.2 GPS week: 2054 Day: 2 MJD: 58624
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 17 -19 21 .09 18 14 | 13501 -1756 3103 12355
cof n/a| 1 -1 0 -1 30 -33 .02 25 18 | 13477 -1747 3109 12361
emx n/a| 0 0 2 2 10 21 .04 24 24 | 20496 -890 3107 12186
esx n/a| 0 0 1 12 -16 29 .07 17 13 | -13895 -1652 3096 14906
gfz n/a| 0 2 -4 -29 -6 -40 .14 29 17 | 0 -1255 3096 12159
grg n/a| 0 1 -2 -35 -2 -98 -.31 22 21 | -1746 -1854 3105 11724
iac n/a| -3 0 2 -18 25 59 -.07 24 22 | -1531 -859 3116 12023
mcc n/a| -5 1 -9 98 50 1152 -.56 155 155 | --- --- --- ---
Table 2.2054.3 GPS week: 2054 Day: 3 MJD: 58625
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 2 5 -4 48 .15 21 16 | 14337 313 2870 11546
cof n/a| 1 -2 -2 29 18 53 .15 27 17 | 14326 321 2878 11560
emx n/a| 0 0 1 26 9 16 -.06 24 24 | -9089 78 2870 11478
esx n/a| 0 0 0 25 2 13 .06 20 15 | 1221 1457 2886 13617
gfz n/a| 0 0 0 -34 5 1 .02 29 17 | 0 1196 2887 11336
grg n/a| 2 -1 -2 -80 9 -107 -.24 27 23 | -1909 793 2862 10955
iac n/a| -3 0 1 11 10 -37 -.03 21 18 | -862 847 2874 11233
mcc n/a| -6 -8 -28 46 -94 351 -.21 142 142 | --- --- --- ---
Table 2.2054.4 GPS week: 2054 Day: 4 MJD: 58626
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 44 -42 31 .13 19 16 | 12739 -484 3077 11130
cof n/a| 1 -1 6 37 -41 41 .18 22 19 | 12730 -460 3067 11132
emx n/a| 1 2 3 13 26 43 .07 22 22 | 12782 -207 3085 10878
esx n/a| 0 -1 0 25 3 8 .12 21 16 | 25803 -103 3064 13705
gfz n/a| 0 -1 1 -21 12 35 .16 28 19 | 0 -569 3062 10868
grg n/a| 2 -1 -10 -73 22 -65 -.27 19 15 | -2582 -431 3071 10385
iac n/a| -5 1 1 2 14 13 -.13 23 21 | -1172 -507 3075 10866
mcc n/a| 9 1 -45 75 -130 -108 .15 168 168 | --- --- --- ---
Table 2.2054.5 GPS week: 2054 Day: 5 MJD: 58627
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 4 23 -19 3 .07 18 14 | 12278 -2779 3198 11408
cof n/a| 0 0 2 19 -8 18 .28 22 17 | 12278 -2767 3198 11419
emx n/a| -1 1 6 1 1 13 -.07 22 22 | -13011 -1661 3209 11241
esx n/a| 0 0 0 27 5 17 .22 21 17 | 18923 -2626 3197 13811
gfz n/a| 0 0 -3 -7 17 -53 .18 29 19 | 0 -2699 3194 11201
grg n/a| 3 0 -4 -46 18 -36 -.36 23 20 | -1783 -2324 3181 10619
iac n/a| 0 2 -3 -6 -21 24 -.15 22 20 | -1364 -1760 3190 11100
mcc n/a| -15 -7 -30 -95 -201 -75 -.46 224 224 | --- --- --- ---
Table 2.2054.6 GPS week: 2054 Day: 6 MJD: 58628
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 -3 -15 19 .19 17 14 | 11634 -86 2976 12541
cof n/a| -1 0 0 -5 -14 10 .16 20 16 | 11630 -85 2974 12545
emx n/a| -1 0 0 6 12 74 .04 21 21 | -11022 398 2976 12198
esx n/a| 0 -1 -2 26 0 -11 .12 21 18 | -8592 -34 2967 14999
gfz n/a| 1 -2 0 -8 17 -42 .06 25 25 | 0 -453 2957 12337
grg n/a| 0 1 -2 -62 36 -40 -.41 19 18 | -2036 -327 2975 12060
iac n/a| 0 2 0 50 -45 0 -.04 22 21 | -1207 -363 2970 12179
mcc n/a| -8 -5 19 576 -87 1145 .25 207 207 | --- --- --- ---
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 3.2054.0 GPS week: 2054 Day: 0 MJD: 58622
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 805 41 30 29 23 17 23 15 --- 11 | 77 72 59 31 41 36 55 --- 46
R02 | 649 12 12 19 15 13 10 29 251 8 | 41 41 48 43 40 43 28 205 38
R03 | 1000 9 11 8 7 11 12 13 143 4 | 55 55 54 56 51 55 47 68 52
R04 | 580 7 10 8 8 18 12 12 --- 5 | 53 54 51 49 45 55 50 --- 49
R05 | 502 20 19 19 26 24 27 19 --- 10 | 44 48 55 61 55 55 57 --- 50
R07 | 634 8 8 12 8 12 18 22 277 6 | 58 59 59 58 61 57 68 150 58
R08 | 841 10 7 17 17 13 12 13 --- 6 | 44 43 51 43 46 45 50 --- 44
R09 | 3129 10 16 15 10 15 16 11 --- 6 | 58 57 58 61 64 57 62 --- 58
R10 | 1857 11 14 22 9 16 19 17 --- 7 | 66 68 55 71 75 72 53 --- 65
R11 | 751 18 20 23 11 12 21 13 118 7 | 59 58 46 53 56 45 39 98 48
R13 | 1041 23 23 26 13 17 26 23 --- 9 | 60 69 52 74 61 80 57 --- 64
R14 | 1176 20 25 19 12 21 15 13 --- 7 | 96 99 92 82 77 85 85 --- 85
R15 | 1139 23 29 18 9 15 15 28 --- 8 | 71 75 48 49 62 57 43 --- 54
R16 | 690 42 51 42 20 28 43 19 --- 15 | 73 89 61 69 82 83 62 --- 68
R17E | 1311 14 15 18 15 13 11 15 --- 6 | 89 86 85 92 95 93 89 --- 90
R18E | 2154 12 13 23 16 15 14 15 --- 7 | 33 36 38 37 32 30 38 --- 32
R19E | 1076 39 55 51 23 72 40 45 --- 20 | 61 65 61 55 80 54 72 --- 55
R20E | 1554 24 27 34 24 33 28 26 --- 12 | 100 104 98 101 111 94 95 --- 97
R21E | 1531 12 15 24 14 26 15 23 91 8 | 57 58 55 60 69 61 64 77 59
R22E | 1411 14 16 22 13 22 19 19 --- 8 | 103 103 100 104 112 105 105 --- 104
R23E | 2368 21 19 22 20 20 18 24 --- 9 | 82 82 74 78 76 79 69 --- 75
R24E | 2847 24 28 29 20 48 31 18 --- 13 | 31 38 31 47 66 54 46 --- 41
XR26E | ---- 23 60 --- --- --- 21 26 --- 17 | 31 63 --- --- --- 41 36 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1504 21 24 25 16 26 22 21 191 |T 62 66 60 62 66 62 59 119 59
WRMS | 1504 19 20 25 14 19 21 20 191 |NE 61 63 56 57 58 58 54 130 55
MEDI | 1076 18 19 22 14 17 18 19 143 |MD 59 63 55 58 62 57 57 98 55
Table 3.2054.1 GPS week: 2054 Day: 1 MJD: 58623
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 770 50 55 29 31 29 60 28 --- 17 | 59 66 42 39 48 33 40 --- 33
R02 | 729 12 15 19 16 14 18 22 155 7 | 34 33 40 21 29 36 18 136 26
R03 | 1471 15 17 11 12 7 11 18 144 5 | 37 37 35 34 30 31 25 34 30
R04 | 1383 7 10 9 8 9 16 12 --- 4 | 35 32 33 31 32 42 27 --- 31
R05 | 539 15 21 15 18 14 17 10 --- 6 | 30 29 35 40 35 46 32 --- 34
R07 | 1047 7 12 16 19 17 15 18 198 7 | 41 45 45 37 43 39 44 106 39
R08 | 868 15 16 16 14 23 14 16 --- 7 | 31 28 31 29 36 27 32 --- 28
R09 | 3581 11 11 13 15 13 11 14 --- 6 | 71 68 69 75 73 68 73 --- 71
R10 | 2601 12 15 18 10 22 23 18 --- 7 | 45 50 38 42 61 58 35 --- 44
R11 | 793 11 20 23 8 26 17 26 142 8 | 44 50 38 41 59 51 33 70 42
R13 | 1336 11 15 25 13 17 19 12 --- 7 | 47 42 40 46 40 54 40 --- 43
R14 | 683 22 23 22 12 21 12 14 --- 8 | 114 116 115 109 106 114 100 --- 109
R15 | 942 23 21 21 9 14 17 26 --- 8 | 52 48 41 38 43 43 33 --- 40
R16 | 626 29 45 40 20 30 34 26 --- 13 | 50 63 43 40 48 67 47 --- 41
R17E | 1246 13 9 21 11 14 18 14 --- 6 | 63 65 58 62 67 64 60 --- 61
R18E | 1424 11 12 14 13 20 13 13 --- 6 | 25 27 26 29 24 25 30 --- 24
R19E | 1555 29 49 40 30 56 25 43 --- 17 | 52 63 56 54 65 66 62 --- 53
R20E | 1387 22 22 30 23 25 25 23 --- 11 | 76 71 70 72 73 80 68 --- 70
R21E | 1775 18 20 24 10 18 12 17 96 7 | 49 51 42 46 55 46 48 72 46
R22E | 1888 15 18 25 17 16 16 21 --- 8 | 90 94 81 92 89 87 86 --- 87
R23E | 2966 31 29 23 16 30 20 23 --- 11 | 66 66 52 57 68 58 55 --- 56
R24E | 1175 28 34 31 22 29 23 19 --- 11 | 37 44 43 50 51 42 51 --- 40
XR26E | ---- 34 61 --- --- --- 63 33 --- 32 | 25 51 --- --- --- 78 27 --- 32
------+---------------------------------------------------+-----------------------------------------------
RMS | 1594 21 25 23 17 23 22 21 151 |T 51 53 48 49 53 54 46 83 46
WRMS | 1594 16 20 23 14 17 20 19 151 |NE 49 50 46 44 48 50 41 86 43
MEDI | 1246 15 20 21 14 18 17 18 144 |MD 47 50 42 41 48 51 40 72 41
Table 3.2054.2 GPS week: 2054 Day: 2 MJD: 58624
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 703 46 67 41 39 36 49 26 --- 18 | 66 95 61 53 69 29 44 --- 46
R02 | 650 13 12 21 11 13 7 23 117 6 | 40 42 53 37 42 39 33 172 38
R03 | 1654 9 15 8 11 11 13 27 107 6 | 48 51 48 52 53 55 38 59 48
R04 | 771 5 12 8 15 9 21 14 --- 6 | 42 45 43 55 44 29 32 --- 41
R05 | 586 17 20 23 11 23 22 13 --- 8 | 38 39 44 37 38 32 40 --- 34
R07 | 934 10 11 13 15 24 15 20 199 7 | 50 51 50 71 60 63 51 90 57
R08 | 892 8 10 11 7 23 12 14 --- 5 | 42 48 48 47 57 45 46 --- 46
R09 | 3262 13 19 10 13 20 23 24 --- 7 | 39 45 40 47 51 43 41 --- 41
R10 | 3465 11 11 19 12 18 15 21 --- 7 | 96 98 88 100 101 91 89 --- 94
R11 | 777 14 17 17 10 25 13 25 216 7 | 68 74 60 63 78 64 40 144 61
R13 | 1803 13 25 18 10 20 16 12 --- 6 | 62 74 56 66 67 60 59 --- 61
R14 | 642 14 20 16 9 16 23 25 --- 7 | 78 80 75 79 73 71 59 --- 73
R15 | 561 18 24 19 13 16 14 24 --- 7 | 55 61 46 42 54 52 38 --- 47
R16 | 604 24 27 40 19 36 42 26 --- 13 | 50 46 48 48 46 50 32 --- 40
R17E | 1483 11 10 20 10 26 9 18 --- 7 | 61 65 60 58 74 59 55 --- 59
R18E | 1568 10 9 13 10 9 11 16 --- 5 | 27 30 22 32 32 24 29 --- 26
R19E | 978 28 33 42 32 79 27 48 --- 19 | 39 47 43 54 75 48 59 --- 41
R20E | 1382 24 39 36 24 34 26 28 --- 12 | 77 95 76 68 85 58 63 --- 67
R21E | 847 14 15 29 12 29 13 24 92 9 | 47 51 49 41 57 43 47 61 44
R22E | 1706 17 16 29 14 23 18 15 --- 8 | 86 89 79 86 82 88 80 --- 82
R23E | 3217 19 28 16 19 33 19 23 --- 9 | 49 57 47 54 50 50 49 --- 47
R24E | 936 16 31 23 21 42 33 28 --- 12 | 30 39 27 36 47 39 37 --- 29
XR26E | ---- 12 29 --- --- --- --- 24 --- 18 | 21 28 --- --- --- --- 32 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1598 18 25 24 17 29 22 24 155 |T 52 58 52 55 60 51 47 105 49
WRMS | 1598 14 18 24 13 17 21 22 155 |NE 55 60 54 56 59 51 45 116 51
MEDI | 934 14 19 19 12 23 16 24 117 |MD 49 51 48 53 57 50 44 90 46
Table 3.2054.3 GPS week: 2054 Day: 3 MJD: 58625
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 708 50 58 50 48 52 39 20 --- 20 | 73 92 78 51 63 30 45 --- 49
R02 | 835 9 25 27 12 13 21 9 135 7 | 37 47 47 29 35 32 31 82 33
R03 | 983 7 9 12 9 16 21 19 105 6 | 50 50 47 53 59 68 40 55 51
R04 | 978 10 13 15 15 12 10 16 --- 6 | 46 44 47 38 47 51 33 --- 41
R05 | 736 23 25 16 17 34 33 12 --- 10 | 46 51 45 51 60 26 47 --- 42
R07 | 1063 12 13 10 8 12 12 17 165 5 | 49 44 52 55 50 56 46 58 50
R08 | 1036 7 11 16 12 17 17 11 --- 6 | 44 39 43 49 42 52 45 --- 45
R09 | 3045 15 13 16 14 16 28 14 --- 7 | 25 21 24 27 33 27 27 --- 23
R10 | 4527 14 12 20 27 19 20 17 --- 9 | 65 62 57 66 54 46 58 --- 57
R11 | 944 10 14 19 12 20 16 17 197 7 | 68 69 66 64 67 58 64 67 63
R13 | 1762 13 10 24 12 25 17 20 --- 8 | 77 82 84 84 86 76 70 --- 78
R14 | 629 17 17 18 8 23 27 15 --- 8 | 159 163 166 167 152 165 156 --- 160
R15 | 711 25 25 18 10 13 13 25 --- 8 | 68 69 45 45 52 52 42 --- 49
R16 | 781 23 57 46 23 19 51 28 --- 14 | 68 88 46 63 65 79 48 --- 55
R17E | 1280 14 15 19 11 23 14 14 --- 7 | 32 30 25 29 41 30 31 --- 28
R18E | 1743 15 15 10 15 13 13 21 --- 6 | 20 20 20 25 21 18 25 --- 19
R19E | 1192 41 42 34 38 69 37 47 --- 20 | 48 58 39 64 79 56 72 --- 51
R20E | 1457 22 29 33 21 39 45 32 --- 14 | 34 46 37 34 56 61 46 --- 34
R21E | 1581 15 17 18 14 15 13 19 75 7 | 31 36 31 31 37 28 32 39 29
R22E | 1072 19 24 21 14 30 29 19 --- 9 | 77 78 74 79 92 66 73 --- 74
R23E | 1769 17 24 17 17 30 23 13 --- 8 | 30 36 32 40 36 37 32 --- 32
R24E | 2347 27 39 18 25 43 40 25 --- 13 | 31 54 32 54 63 52 50 --- 39
XR26E | ---- 17 42 --- --- --- --- 18 --- 17 | 33 60 --- --- --- --- 35 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1674 21 27 24 20 29 27 21 142 |T 52 58 51 54 58 53 49 60 49
WRMS | 1674 16 17 24 15 17 23 18 142 |NE 62 65 60 60 61 58 53 65 56
MEDI | 1063 15 17 18 14 19 21 18 135 |MD 46 51 45 51 54 52 45 58 45
Table 3.2054.4 GPS week: 2054 Day: 4 MJD: 58626
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 812 37 28 25 49 49 13 29 --- 16 | 64 57 57 37 44 52 66 --- 48
R02 | 1048 14 12 9 12 11 20 23 290 7 | 35 33 32 35 33 28 47 127 30
R03 | 725 10 11 12 15 18 9 10 75 5 | 44 46 44 52 51 33 49 44 44
R04 | 828 13 15 16 14 14 8 16 --- 6 | 46 48 47 37 32 32 33 --- 36
R05 | 926 14 17 16 19 24 10 14 --- 7 | 47 46 46 50 50 41 42 --- 43
R07 | 1853 9 12 11 8 12 11 24 142 6 | 55 57 55 49 60 51 43 99 50
R08 | 664 14 15 9 13 16 13 16 --- 6 | 41 44 43 56 59 50 45 --- 47
R09 | 2700 18 26 17 13 19 17 18 --- 7 | 43 47 43 55 47 45 50 --- 45
R10 | 3810 10 15 10 24 18 14 18 --- 7 | 86 91 81 90 98 80 88 --- 85
R11 | 845 7 10 15 10 12 14 14 165 5 | 64 66 59 64 68 62 59 38 62
R13 | 1319 12 11 23 17 11 19 16 --- 7 | 66 68 69 60 71 68 52 --- 62
R14 | 730 19 20 29 17 22 15 24 --- 9 | 83 81 95 64 77 70 73 --- 74
R15 | 949 27 30 18 12 11 13 26 --- 8 | 62 65 49 47 48 38 41 --- 46
R16 | 983 30 42 42 18 29 40 24 --- 14 | 66 89 51 53 67 82 59 --- 59
R17E | 915 14 15 19 13 19 15 18 --- 7 | 62 59 60 58 71 59 58 --- 59
R18E | 1583 8 13 16 15 13 16 11 --- 6 | 28 30 31 29 29 20 27 --- 24
R19E | 999 39 43 38 39 82 26 49 --- 20 | 36 44 33 51 73 37 49 --- 34
R20E | 1661 14 21 29 17 30 19 31 --- 10 | 73 77 68 63 82 75 66 --- 67
R21E | 1076 16 16 24 23 23 14 27 67 9 | 44 47 36 37 45 43 50 42 39
R22E | 803 19 23 21 12 20 13 21 --- 8 | 82 84 79 77 90 77 78 --- 78
R23E | 721 20 22 27 19 26 23 24 --- 10 | 47 49 51 48 48 44 53 --- 44
R24E | 2887 16 30 29 29 34 38 25 --- 13 | 31 41 38 42 46 51 43 --- 31
XR26E | ---- 12 76 --- --- --- --- 16 --- 13 | 24 78 --- --- --- --- 25 --- 21
------+---------------------------------------------------+-----------------------------------------------
RMS | 1539 19 22 22 21 28 19 23 168 |T 53 58 53 52 58 51 52 70 49
WRMS | 1539 16 19 22 16 19 15 21 168 |NE 57 59 55 53 57 52 53 77 52
MEDI | 949 14 17 18 15 19 14 21 142 |MD 47 57 49 51 51 50 50 44 46
Table 3.2054.5 GPS week: 2054 Day: 5 MJD: 58627
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 586 29 35 22 45 37 32 13 --- 14 | 48 54 47 34 42 64 34 --- 37
R02 | 1074 6 13 12 15 19 15 16 410 6 | 32 36 31 32 25 35 38 240 29
R03 | 431 15 15 16 13 14 8 17 104 6 | 39 43 36 54 44 48 52 112 44
R04 | 751 11 11 13 12 17 7 16 --- 5 | 40 41 37 31 32 29 36 --- 32
R05 | 748 16 13 20 24 22 19 17 --- 9 | 37 35 41 53 50 30 35 --- 38
R07 | 2054 9 15 12 10 19 10 23 159 6 | 42 49 44 46 54 44 33 159 42
R08 | 928 9 13 13 20 12 14 24 --- 7 | 35 38 41 48 43 29 26 --- 35
R09 | 2461 12 17 11 13 19 16 19 --- 6 | 36 38 38 53 55 32 43 --- 41
R10 | 3443 11 15 18 20 14 13 18 --- 7 | 60 63 60 75 60 62 63 --- 63
R11 | 852 11 14 18 10 9 16 22 184 6 | 59 57 59 57 52 58 46 90 55
R13 | 2386 7 8 26 12 25 35 24 --- 10 | 84 83 81 87 92 105 79 --- 86
R14 | 818 14 18 17 18 18 13 17 --- 7 | 119 120 113 121 120 119 118 --- 118
R15 | 915 21 27 19 13 23 11 31 --- 9 | 48 54 36 35 54 37 35 --- 39
R16 | 1298 28 47 27 12 34 53 15 --- 13 | 46 43 40 36 39 30 35 --- 32
R17E | 724 17 14 22 7 16 13 11 --- 6 | 70 73 75 73 80 76 79 --- 74
R18E | 1301 11 14 15 13 14 14 15 --- 6 | 28 30 26 26 28 27 30 --- 25
R19E | 1018 36 34 42 46 84 34 46 --- 21 | 39 44 42 59 72 46 47 --- 36
R20E | 1675 17 22 30 27 25 38 20 --- 12 | 73 72 77 77 67 68 81 --- 71
R21E | 1136 15 9 18 16 18 10 16 108 7 | 56 61 58 72 68 61 64 71 61
R22E | 567 20 17 23 11 21 16 29 --- 9 | 106 106 97 108 111 109 117 --- 107
R23E | 1081 19 26 20 25 22 28 18 --- 10 | 69 76 63 69 62 70 65 --- 64
R24E | 2263 21 30 34 26 53 29 23 --- 14 | 35 42 38 39 45 28 35 --- 29
XR26E | ---- 20 83 --- --- --- 15 28 --- 15 | 46 91 --- --- --- 40 30 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1498 18 22 22 21 29 23 22 223 |T 54 58 53 58 58 54 53 134 51
WRMS | 1498 14 17 22 17 19 20 20 223 |NE 51 53 50 54 54 51 48 150 49
MEDI | 1018 15 15 18 13 19 15 18 159 |MD 46 54 42 53 54 46 43 112 41
Table 3.2054.6 GPS week: 2054 Day: 6 MJD: 58628
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 757 26 30 28 34 24 23 27 --- 12 | 83 86 70 52 62 58 62 --- 61
R02 | 1175 13 16 13 9 17 13 18 285 6 | 46 47 44 36 34 40 37 153 38
R03 | 563 7 9 9 25 16 19 36 185 9 | 57 58 55 59 64 65 60 128 58
R04 | 1310 8 18 9 13 20 9 20 --- 6 | 58 59 52 45 44 52 61 --- 51
R05 | 731 14 19 23 25 22 18 16 --- 8 | 50 58 55 61 61 45 57 --- 52
R07 | 1901 10 12 15 13 12 14 15 197 6 | 66 65 64 74 75 75 59 95 68
R08 | 946 5 10 11 15 10 18 13 --- 5 | 52 55 56 59 56 49 46 --- 52
R09 | 3062 12 11 12 10 17 34 25 --- 9 | 43 44 40 45 49 41 50 --- 41
R10 | 2472 13 13 17 19 26 15 11 --- 7 | 83 85 76 90 77 79 76 --- 80
R11 | 799 10 15 10 12 16 12 14 --- 5 | 70 73 61 67 58 65 53 --- 62
R13 | 2280 8 13 16 17 27 30 16 --- 9 | 94 97 92 102 95 100 92 --- 95
R14 | 1116 17 16 16 20 21 13 21 --- 8 | 90 97 83 100 93 87 80 --- 88
R15 | 1602 25 20 19 19 22 13 34 --- 10 | 76 73 47 47 72 58 42 --- 56
R16 | 1243 26 30 32 29 45 25 26 --- 13 | 61 69 40 64 65 63 54 --- 53
R17E | 699 14 17 26 15 25 10 13 --- 8 | 90 90 88 96 103 97 89 --- 92
R18E | 1512 7 11 21 15 15 20 12 --- 7 | 24 23 24 26 25 24 26 --- 21
R19E | 1428 31 35 36 39 44 21 28 --- 15 | 43 46 28 60 74 34 37 --- 35
R20E | 2039 23 27 28 21 35 17 40 --- 12 | 95 102 96 90 95 88 89 --- 89
R21E | 1032 13 17 18 11 28 9 14 133 7 | 53 54 50 53 62 51 58 117 53
R22E | 798 13 14 19 12 28 11 20 --- 7 | 106 108 106 106 106 106 118 --- 106
R23E | 1358 18 22 18 25 25 14 16 --- 8 | 70 69 66 73 65 67 68 --- 66
R24E | 1347 24 31 28 33 30 30 25 --- 12 | 42 42 39 48 45 42 41 --- 38
XR26E | ---- 38 54 --- --- --- 66 38 --- 35 | 56 76 --- --- --- 62 42 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 1508 17 20 21 21 25 19 22 207 |T 65 68 60 66 67 62 60 123 60
WRMS | 1508 14 16 21 18 25 18 21 207 |NE 66 69 59 64 64 62 59 125 61
MEDI | 1243 13 17 18 17 22 17 20 185 |MD 61 69 55 60 64 62 58 117 56
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