[IGSREPORT-27140] Wk 2094 IGLOS Final Orbits
acc
acc at igs.org
Sun Mar 15 15:54:00 PDT 2020
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2094 (Feb 23, 2020 - Feb 29, 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 2.2094.
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:
igl2094[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2094 in the SP3 format.
igl20947.sum Combination Report for GPS Week 2094.
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 | -5.4 ns
1 | -4.4 ns
2 | -6.3 ns
3 | -4.8 ns
4 | -3.6 ns
5 | -3.5 ns
6 | -4.6 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 1.2094, 1a.2094).
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 2.2094.0-6)
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 3.2094.0-6).
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 2094 summary. (Feb 23, 2020 - Feb 29, 2020)
Table 1.2094.a GPS week : 2094 MJD: 58902.0-58908.0
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 0 14 -23 72 .04 18 16 | 20060 -6 3115 7933
| 0 0 0 20 21 24 .03 | 585 1218
cof n/a| 0 0 0 4 0 65 .05 21 19 | 20053 -1 3112 7932
| 1 0 1 26 28 33 .03 | 578 1221
emx n/a| 1 -1 -1 81 15 -52 -.01 29 29 | -7442 308 3103 7985
| 0 1 3 12 26 32 .03 | 3428 922
esx n/a| -1 0 -4 -6 -45 -33 .09 31 28 | -7432 414 3111 9646
| 0 0 2 17 21 32 .03 | 13587 1377
gfz n/a| 0 0 1 -36 23 -23 .18 22 16 | 0 -139 3179 7609
| 0 0 1 19 10 27 .06 | 0 1409
grg n/a| 1 0 3 -57 -9 -19 -.41 28 23 | -4565 -17 3119 7151
| 1 1 3 15 15 26 .04 | 454 1334
iac n/a| 0 0 0 12 27 -4 -.03 18 16 | -3240 48 3115 8066
| 1 1 1 13 24 57 .07 | 717 778
mcc n/a| -2 0 -27 2 4 -89 -.73 152 152 | --- --- --- ---
| 9 9 14 168 96 624 .18 | --- ---
Table 1.2094.b GPS week : 2094 MJD: 58902.0-58908.0
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 | 19 16 16 19 20 19 20 |
R02 | 11 7 8 7 6 5 5 |
R03 | 7 8 7 8 8 11 7 |
R04 | 9 7 8 9 9 10 10 |
R05 | 9 8 8 8 8 7 8 |
R07 | 7 7 7 6 6 8 8 |
R08 | 8 9 9 7 8 8 7 |
R09 | 8 6 10 7 8 8 7 |
R11 | 7 7 6 7 5 8 7 |
R12 | 8 8 8 7 7 8 9 |
R13 | 13 14 18 16 16 13 15 |
R14 | 6 8 8 7 6 6 8 |
R15 | 8 6 5 8 9 7 7 |
R16 | 11 15 12 12 11 14 12 |
R17 | 11 8 7 9 7 8 10 |
R18 | 8 8 7 8 6 6 8 |
R19 | 19 18 20 16 16 17 19 |
R20 | 17 15 15 16 16 17 17 |
R21 | 10 11 11 10 10 10 9 |
R22 | 9 8 10 12 9 9 9 |
R23 | 7 8 9 10 11 10 7 |
R26 | 13 12 21 17 17 21 14 |
Table 1.2094.c GPS week : 2094 MJD: 58902.0-58908.0
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 2094 0 | -11 15 190 -904 -605 811 81.6 1316 1316 | -5391 0
brd 2094 1 | -20 2 194 -1049 -1193 -153 82.2 1228 1228 | -4355 0
brd 2094 2 | 32 14 192 -2007 -1070 -1053 82.4 1339 1339 | -6312 0
brd 2094 3 | -50 32 228 -1858 181 144 83.5 1443 1443 | -4753 0
brd 2094 4 | 14 83 275 -1573 -1403 319 81.4 1448 1448 | -3568 0
brd 2094 5 | 12 17 174 -750 366 2329 80.5 1812 1812 | -3529 0
brd 2094 6 | 28 100 159 -1702 1804 645 82.5 1674 1674 | -4568 0
-------------+------------------------------------------------------------+----------------
brd 2094 mean| 1 38 202 -1406 -274 434 82.0 1465 1465 | -4639 0
brd 2094 sdev| 29 38 38 498 1140 1035 1.0 207 207 | 986 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 2.2094.0 GPS week: 2094 Day: 0 MJD: 58902
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 0 22 -48 80 .02 20 17 | 20294 -618 3191 8251
cof n/a| -2 0 3 0 -17 45 .04 22 20 | 20280 -598 3188 8252
emx n/a| 1 0 -4 65 9 -8 -.04 25 25 | -8033 242 3173 8392
esx n/a| 0 0 -1 -36 -14 -71 .11 30 28 | -3786 -1493 3200 10260
gfz n/a| 0 -1 4 -24 22 -23 .19 24 19 | 0 -1312 3264 8040
grg n/a| 0 0 0 -57 1 -8 -.37 25 19 | -5031 -536 3216 7590
iac n/a| -1 0 1 27 58 -18 .01 20 19 | -3288 -866 3200 8441
mcc n/a| 9 18 -15 147 -7 -776 -.51 162 162 | --- --- --- ---
Table 2.2094.1 GPS week: 2094 Day: 1 MJD: 58903
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 0 -20 -41 85 .01 17 15 | 20306 833 2869 8330
cof n/a| 3 0 -1 -44 -17 85 .08 21 19 | 20301 845 2871 8331
emx n/a| 1 -1 -6 69 7 -28 .00 31 31 | -13441 1588 2872 8436
esx n/a| -1 0 -5 -6 -30 -5 .05 32 28 | -10793 2010 2873 9891
gfz n/a| -1 -1 2 -4 23 -20 .23 21 17 | 0 815 2921 8395
grg n/a| 0 -1 7 -53 9 3 -.39 29 25 | -4777 857 2864 7754
iac n/a| -2 1 1 22 39 -46 -.04 15 14 | -3568 375 2855 8544
mcc n/a| -12 -5 -18 58 -36 -928 -1.01 145 145 | --- --- --- ---
Table 2.2094.2 GPS week: 2094 Day: 2 MJD: 58904
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 45 -2 99 .06 19 18 | 20892 -2039 3207 8053
cof n/a| 0 0 0 37 21 102 .03 21 18 | 20881 -2027 3197 8051
emx n/a| 1 0 0 86 3 -28 -.06 29 29 | -9786 -1027 3186 8021
esx n/a| 0 1 0 -17 -62 6 .11 31 26 | 12710 -1496 3191 9089
gfz n/a| 1 -1 -1 -55 24 -2 .26 21 15 | 0 -2277 3315 7869
grg n/a| 2 1 1 -35 -13 -55 -.45 32 24 | -5130 -2306 3210 7646
iac n/a| -1 0 2 -11 34 -31 -.10 16 15 | -3975 -1104 3198 8137
mcc n/a| 0 -7 -47 100 -71 246 -.54 163 163 | --- --- --- ---
Table 2.2094.3 GPS week: 2094 Day: 3 MJD: 58905
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 27 12 40 .08 17 13 | 19200 -990 3323 8463
cof n/a| 0 0 -1 26 35 51 .07 22 18 | 19216 -1020 3321 8459
emx n/a| 1 0 -1 91 -11 -82 -.00 29 29 | -5570 -702 3299 8452
esx n/a| -1 0 -2 -1 -78 -47 .09 33 29 | -19739 701 3317 9820
gfz n/a| 0 0 0 -61 28 -80 .20 23 17 | 0 -987 3371 8085
grg n/a| 2 4 2 -42 -23 -50 -.40 28 24 | -4114 -1067 3319 7688
iac n/a| 2 0 0 0 30 59 -.13 17 16 | -4210 370 3320 8476
mcc n/a| -9 -1 -25 -360 104 585 -.77 180 180 | --- --- --- ---
Table 2.2094.4 GPS week: 2094 Day: 4 MJD: 58906
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 0 1 -25 36 .00 16 15 | 19604 1009 2786 7021
cof n/a| 0 0 0 12 0 7 .07 19 19 | 19590 1025 2790 7018
emx n/a| 0 -1 2 91 23 -98 -.03 29 29 | -7344 384 2774 7160
esx n/a| 0 2 -8 16 -34 -77 .04 28 26 | 8185 760 2768 9407
gfz n/a| -1 0 0 -36 35 -27 .15 22 16 | 0 1237 2817 6479
grg n/a| 0 0 5 -64 2 -26 -.47 29 25 | -4060 1288 2776 5889
iac n/a| 1 -1 0 19 -2 89 .07 20 17 | -2672 1141 2796 7231
mcc n/a| 1 -9 -14 -16 -146 326 -.59 152 152 | --- --- --- ---
Table 2.2094.5 GPS week: 2094 Day: 5 MJD: 58907
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 13 -24 88 .06 18 17 | 19675 1137 3243 7201
cof n/a| 1 -1 0 1 22 97 .01 21 21 | 19670 1127 3233 7200
emx n/a| 1 0 1 97 6 -51 .03 28 28 | -4659 1055 3240 7208
esx n/a| 0 1 -5 -7 -40 -14 .12 32 27 | -18925 1405 3258 9205
gfz n/a| 0 0 0 -34 26 -10 .13 22 15 | 0 1403 3331 6597
grg n/a| 1 0 8 -80 -7 15 -.37 26 22 | -4140 1132 3220 6287
iac n/a| 0 1 0 15 -10 -63 -.01 19 17 | -2354 110 3244 7309
mcc n/a| -12 3 -23 33 104 416 -.79 117 117 | --- --- --- ---
Table 2.2094.6 GPS week: 2094 Day: 6 MJD: 58908
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 7 -32 78 .06 19 15 | 20449 624 3192 8215
cof n/a| 1 0 0 -2 -46 69 .02 21 19 | 20436 640 3188 8213
emx n/a| 0 -3 0 69 71 -68 .03 28 28 | -3264 619 3177 8226
esx n/a| -2 0 -3 11 -60 -22 .10 32 30 | -19681 1015 3176 9853
gfz n/a| 0 0 1 -35 1 -1 .09 21 17 | 0 146 3240 7803
grg n/a| 1 0 -1 -68 -34 -14 -.46 29 24 | -4707 513 3228 7203
iac n/a| 1 0 0 17 39 -24 .00 20 17 | -2616 311 3193 8326
mcc n/a| 9 4 -47 53 80 -495 -.86 147 147 | --- --- --- ---
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 3.2094.0 GPS week: 2094 Day: 0 MJD: 58902
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 821 30 29 41 36 48 56 33 --- 18 | 57 61 60 63 66 76 63 --- 57
R02E | 2791 13 15 32 11 38 20 11 146 10 | 24 31 31 25 51 31 29 103 28
R03E | 2174 12 11 26 14 14 13 14 122 7 | 62 63 55 59 63 62 68 77 61
XR04E | 979 17 15 12 15 --- 28 11 --- 9 | 37 34 46 36 --- 55 42 --- 39
R05E | 722 18 18 24 24 14 20 15 --- 8 | 38 38 33 33 38 37 33 --- 32
R07E | 691 12 13 15 10 16 18 15 229 6 | 44 43 45 48 52 43 44 92 44
R08E | 1856 17 24 21 12 14 17 20 --- 7 | 34 37 31 35 41 38 43 --- 35
R09 | 717 19 24 12 12 13 12 28 --- 8 | 28 28 20 30 32 33 39 --- 26
R11 | 674 9 12 14 12 17 20 14 194 6 | 44 48 46 47 51 49 46 92 46
R12 | 1348 12 18 17 26 16 11 20 --- 7 | 60 60 62 50 58 58 67 --- 58
R13 | 753 34 30 13 27 43 34 10 --- 13 | 62 62 56 45 59 49 50 --- 51
R14 | 1699 15 18 10 18 11 12 16 --- 6 | 57 58 48 53 54 52 50 --- 51
R15 | 1799 12 14 14 28 16 16 12 --- 7 | 61 61 55 55 58 65 53 --- 56
R16 | 681 29 30 21 19 24 25 25 --- 11 | 54 57 54 59 56 62 46 --- 51
R17 | 611 9 11 28 43 23 11 19 --- 10 | 68 68 55 46 74 74 78 --- 66
R18 | 996 12 15 29 15 17 19 16 --- 8 | 52 53 56 48 60 65 61 --- 56
R19 | 570 36 41 45 78 21 31 34 --- 19 | 92 92 65 55 85 78 92 --- 76
R20 | 1349 39 39 39 22 40 53 15 --- 16 | 55 59 56 46 68 53 52 --- 50
R21 | 1090 6 11 25 37 10 19 27 67 10 | 65 67 44 47 68 76 79 63 63
R22 | 1425 13 15 26 35 9 13 22 --- 9 | 68 71 44 45 67 71 72 --- 61
R23 | 544 8 16 15 31 15 12 9 --- 7 | 41 47 39 56 41 40 44 --- 41
XR26 | ---- 13 44 --- --- --- --- 13 --- 13 | 34 59 --- --- --- --- 40 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1315 20 22 25 30 24 25 20 162 |T 51 54 47 46 57 55 54 85 49
WRMS | 1315 17 20 25 28 19 19 19 162 |NE 56 59 50 48 59 58 57 77 52
MEDI | 979 13 16 21 22 16 19 15 146 |MD 54 58 48 47 58 55 50 92 51
Table 3.2094.1 GPS week: 2094 Day: 1 MJD: 58903
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 694 25 29 54 38 32 49 22 --- 15 | 53 51 44 63 65 67 57 --- 53
R02E | 637 9 14 29 15 15 20 11 172 7 | 17 19 22 24 28 24 22 114 19
R03E | 2168 8 9 32 10 18 18 11 90 7 | 51 49 43 53 58 53 54 68 51
XR04E | 1087 10 16 20 16 --- 14 11 --- 6 | 28 34 33 32 --- 33 33 --- 30
R05E | 1036 13 13 30 14 22 18 14 --- 8 | 23 28 29 27 32 21 25 --- 22
R07E | 743 10 14 23 10 16 20 16 100 7 | 32 31 36 32 37 33 29 115 30
R08E | 809 12 13 29 16 23 22 13 --- 8 | 30 31 31 41 44 35 35 --- 33
R09 | 965 12 21 13 18 10 23 10 --- 6 | 22 23 24 28 26 31 23 --- 22
R11 | 616 7 8 13 12 20 19 14 231 6 | 34 33 29 35 38 36 34 97 32
R12 | 1155 14 20 20 30 15 11 10 --- 7 | 47 49 43 34 37 40 38 --- 39
R13 | 723 30 43 20 42 34 48 15 --- 14 | 30 34 31 40 31 27 30 --- 27
R14 | 1423 20 22 15 16 17 20 11 --- 7 | 32 36 35 34 28 32 23 --- 26
R15 | 2330 12 18 12 18 10 12 9 --- 5 | 37 42 34 35 35 39 29 --- 33
R16 | 668 19 21 57 36 18 61 20 --- 15 | 42 42 39 39 36 54 38 --- 35
R17 | 813 9 10 23 34 10 11 11 --- 7 | 45 48 38 41 45 52 45 --- 44
R18 | 1035 15 18 25 16 24 17 14 --- 8 | 37 39 35 40 51 38 39 --- 38
R19 | 1009 35 26 47 84 27 31 21 --- 18 | 47 39 54 42 44 51 42 --- 40
R20 | 1371 29 40 47 35 27 50 21 --- 14 | 33 48 33 31 37 20 23 --- 24
R21 | 1054 9 15 30 43 12 29 22 68 10 | 36 36 32 31 42 51 40 46 37
R22 | 2264 9 15 28 32 11 19 14 --- 8 | 39 43 25 35 36 43 38 --- 36
R23 | 588 9 19 12 32 25 18 13 --- 8 | 34 36 30 33 34 34 32 --- 29
XR26 | ---- 12 45 --- --- --- --- 11 --- 11 | 31 40 --- --- --- --- 25 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1228 17 21 31 32 21 29 15 145 |T 35 37 34 36 39 38 34 88 33
WRMS | 1228 15 19 31 28 17 25 14 145 |NE 36 39 34 35 37 39 33 71 32
MEDI | 1009 12 18 25 18 18 20 13 100 |MD 34 36 33 35 37 36 33 97 32
Table 3.2094.2 GPS week: 2094 Day: 2 MJD: 58904
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1058 30 29 46 42 42 36 24 --- 16 | 47 49 39 54 60 51 45 --- 42
R02E | 1043 12 14 26 9 14 28 10 112 7 | 21 27 20 25 26 35 23 109 21
R03E | 1650 10 13 32 13 14 16 10 85 7 | 75 71 65 69 72 77 70 68 70
XR04E | 1621 11 23 27 10 --- 16 14 --- 8 | 22 35 28 25 --- 25 28 --- 23
R05E | 941 17 14 31 16 9 14 13 --- 7 | 28 27 33 33 32 29 33 --- 29
R07E | 1309 11 10 23 11 18 14 10 267 6 | 35 33 35 33 36 39 33 113 32
R08E | 1034 14 15 26 11 25 27 12 --- 8 | 38 37 35 38 46 48 41 --- 39
R09 | 924 22 23 17 16 23 28 17 --- 9 | 14 15 27 32 34 33 20 --- 20
R11 | 1016 9 9 14 11 20 13 10 194 6 | 27 29 26 31 42 25 23 75 27
R12 | 1115 14 12 20 30 14 17 16 --- 8 | 48 46 48 40 44 37 49 --- 43
R13 | 685 33 20 26 39 40 75 18 --- 17 | 38 39 44 28 28 33 37 --- 29
R14 | 697 19 15 10 15 19 20 15 --- 7 | 29 27 21 30 24 28 24 --- 22
R15 | 2405 7 13 9 7 11 20 7 --- 4 | 37 36 28 36 33 38 34 --- 33
R16 | 641 26 25 23 32 15 44 15 --- 11 | 32 40 32 54 54 46 30 --- 36
R17 | 1357 12 13 24 20 10 20 11 --- 7 | 49 47 43 38 45 56 47 --- 45
R18 | 1350 13 14 20 14 10 12 20 --- 7 | 38 39 33 38 41 36 51 --- 39
R19 | 1290 34 48 43 82 33 55 26 --- 20 | 68 80 77 58 73 34 49 --- 55
R20 | 991 24 46 57 29 25 50 15 --- 14 | 38 50 26 37 50 28 37 --- 34
R21 | 906 4 10 31 46 15 19 21 68 10 | 42 44 33 24 45 46 49 62 40
R22 | 3048 10 14 27 42 13 17 21 --- 10 | 43 43 33 28 45 46 49 --- 40
R23 | 724 18 17 22 32 14 17 11 --- 8 | 22 24 22 38 27 26 30 --- 24
XR26 | ---- 22 44 --- --- --- --- 20 --- 21 | 26 58 --- --- --- --- 27 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS | 1338 19 21 29 31 21 32 16 163 |T 37 40 35 37 42 38 37 85 34
WRMS | 1338 18 18 29 26 15 24 15 163 |NE 36 41 35 36 41 36 37 68 33
MEDI | 1043 14 14 26 16 15 20 15 112 |MD 37 39 33 36 42 36 34 75 33
Table 3.2094.3 GPS week: 2094 Day: 3 MJD: 58905
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1365 30 22 51 48 60 39 23 --- 18 | 65 72 61 84 88 59 52 --- 61
R02E | 1814 10 11 26 11 21 15 11 90 7 | 34 35 36 35 41 38 33 77 33
R03E | 1734 12 18 25 10 13 21 20 50 7 | 71 77 71 75 77 74 74 54 72
XR04E | 1394 14 15 25 12 --- 23 13 --- 8 | 35 34 33 31 --- 29 38 --- 31
R05E | 660 13 12 30 12 20 21 12 --- 8 | 39 36 40 38 47 34 37 --- 36
R07E | 2296 10 7 21 10 15 12 10 333 6 | 44 44 43 45 42 51 42 72 43
R08E | 846 9 14 27 10 23 19 9 --- 7 | 45 45 39 45 50 38 38 --- 41
R09 | 1637 13 15 24 12 22 12 12 --- 7 | 24 24 25 37 39 30 30 --- 27
R11 | 839 6 7 10 15 7 26 18 190 6 | 30 30 30 30 28 40 33 42 27
R12 | 899 9 10 17 17 14 24 19 --- 7 | 44 47 43 48 55 36 51 --- 45
R13 | 1779 35 48 17 55 40 41 16 --- 15 | 46 52 41 34 46 37 38 --- 36
R14 | 577 10 18 11 20 11 23 13 --- 6 | 43 49 39 41 41 54 37 --- 39
R15 | 1234 13 15 17 14 12 25 21 --- 8 | 46 50 43 46 49 57 44 --- 45
R16 | 629 18 38 34 32 25 41 12 --- 11 | 39 51 51 53 42 57 39 --- 41
R17 | 1148 5 8 26 34 15 12 18 --- 8 | 54 54 44 44 59 55 63 --- 53
R18 | 1735 17 18 23 16 13 20 21 --- 8 | 41 42 40 38 47 52 52 --- 43
R19 | 1704 28 35 41 71 21 35 24 --- 16 | 60 67 58 44 57 61 61 --- 52
R20 | 911 22 40 55 41 19 61 18 --- 15 | 52 55 44 39 61 55 60 --- 50
R21 | 631 4 8 28 42 19 17 17 74 9 | 55 53 44 51 67 59 62 34 55
R22 | 2766 10 12 33 48 24 23 19 --- 11 | 55 61 44 44 72 69 66 --- 58
R23 | 1144 17 20 21 34 16 31 14 --- 9 | 34 37 33 46 38 49 40 --- 35
XR26 | ---- 16 36 --- --- --- --- 16 --- 16 | 32 41 --- --- --- --- 35 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1442 17 22 29 33 23 28 17 180 |T 44 48 42 45 52 49 46 55 43
WRMS | 1442 13 18 29 29 17 24 16 180 |NE 43 47 41 42 50 50 47 38 42
MEDI | 1234 13 15 25 17 19 23 16 90 |MD 44 47 43 44 47 52 40 54 41
Table 3.2094.4 GPS week: 2094 Day: 4 MJD: 58906
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1263 34 33 60 50 47 30 42 --- 19 | 55 48 46 60 68 50 52 --- 46
R02E | 1720 7 10 21 16 14 14 13 43 6 | 32 35 36 33 35 32 31 45 31
R03E | 708 9 13 27 13 18 28 15 75 8 | 63 67 62 71 62 80 69 45 66
XR04E | 1763 10 12 29 11 --- 24 15 --- 8 | 42 45 43 49 --- 56 54 --- 47
R05E | 1144 12 15 28 15 18 26 11 --- 8 | 35 40 34 34 34 41 35 --- 32
R07E | 1493 10 7 19 9 12 10 17 219 6 | 45 47 47 47 51 49 46 42 46
R08E | 1103 11 16 24 9 19 22 18 --- 7 | 41 43 38 40 49 46 42 --- 41
R09 | 923 9 11 22 17 14 31 20 --- 8 | 32 33 43 46 42 49 43 --- 38
R11 | 565 8 12 12 11 9 14 12 228 4 | 40 41 43 47 45 36 41 36 41
R12 | 679 11 17 18 19 19 19 9 --- 7 | 49 56 47 56 56 43 57 --- 50
R13 | 3969 26 23 34 41 47 48 21 --- 16 | 46 54 54 51 64 46 53 --- 47
R14 | 924 10 10 9 24 7 14 14 --- 6 | 46 45 48 44 48 42 41 --- 43
R15 | 608 15 15 20 21 11 24 26 --- 8 | 55 56 55 52 47 55 51 --- 50
R16 | 689 11 16 31 28 25 36 21 --- 11 | 61 69 40 57 56 57 57 --- 53
R17 | 675 11 20 19 27 12 13 16 --- 7 | 65 72 60 46 57 59 60 --- 57
R18 | 1681 10 9 16 12 15 10 14 --- 5 | 53 55 50 54 58 49 48 --- 51
R19 | 1658 28 35 37 59 20 38 35 --- 16 | 71 77 84 62 78 58 76 --- 67
R20 | 1649 19 29 61 25 19 66 24 --- 16 | 50 63 38 42 49 59 48 --- 45
R21 | 503 9 10 26 35 24 11 16 86 9 | 55 60 47 44 66 48 54 28 52
R22 | 1751 6 8 26 39 14 17 13 --- 8 | 54 50 42 44 56 58 53 --- 51
R23 | 962 26 31 19 23 20 39 9 --- 10 | 36 42 40 46 44 61 38 --- 39
XR26 | ---- 13 61 --- --- --- --- 20 --- 16 | 37 72 --- --- --- --- 39 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1447 16 19 29 28 22 29 20 152 |T 48 53 47 48 53 51 49 39 46
WRMS | 1447 15 19 29 26 16 25 17 152 |NE 50 56 49 49 54 51 50 32 48
MEDI | 1103 11 15 24 21 18 24 16 86 |MD 46 50 46 47 51 49 48 42 46
Table 3.2094.5 GPS week: 2094 Day: 5 MJD: 58907
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 3063 36 32 50 61 50 29 31 --- 19 | 85 94 89 115 109 87 83 --- 89
R02E | 1351 5 9 22 10 10 8 11 57 5 | 21 25 19 26 27 26 18 48 21
R03E | 1303 15 9 30 18 27 26 27 66 11 | 51 48 47 54 66 49 50 52 49
XR04E | 1369 9 9 36 16 --- 14 17 --- 9 | 20 21 23 25 --- 20 27 --- 20
R05E | 1512 10 11 26 13 15 17 14 --- 7 | 32 36 30 35 37 34 33 --- 31
R07E | 3800 11 10 32 9 12 16 13 72 7 | 53 54 60 51 49 45 53 61 50
R08E | 1136 16 11 27 16 14 17 12 --- 7 | 44 41 36 36 38 36 36 --- 37
R09 | 837 16 22 21 15 24 19 14 --- 8 | 10 17 13 22 27 20 20 --- 14
R11 | 699 14 11 12 12 11 34 14 223 7 | 17 20 19 32 27 39 21 39 22
R12 | 1354 13 29 16 27 17 15 16 --- 7 | 28 36 31 21 22 25 34 --- 23
R13 | 3638 24 37 28 28 38 36 12 --- 12 | 34 41 41 43 40 37 34 --- 35
R14 | 1360 9 15 11 13 12 18 10 --- 5 | 23 27 20 27 31 19 26 --- 22
R15 | 652 11 11 14 21 8 17 15 --- 6 | 29 27 23 24 27 26 23 --- 24
R16 | 1075 26 26 29 36 30 44 15 --- 13 | 27 41 45 43 38 22 30 --- 27
R17 | 1181 11 7 20 31 7 14 19 --- 7 | 33 25 31 24 27 32 37 --- 28
R18 | 1182 9 12 15 12 14 10 15 --- 5 | 32 33 33 32 31 27 33 --- 30
R19 | 1449 21 37 43 74 29 31 32 --- 17 | 43 47 44 36 58 33 60 --- 43
R20 | 2138 30 35 49 23 19 65 27 --- 16 | 35 36 41 31 37 52 37 --- 34
R21 | 972 6 8 27 45 9 19 24 82 10 | 31 28 23 28 31 34 40 34 29
R22 | 1994 7 9 28 36 16 14 16 --- 8 | 30 30 27 30 34 37 36 --- 31
R23 | 790 24 26 22 33 16 8 17 --- 9 | 20 21 26 32 34 20 28 --- 22
XR26 | ---- 19 58 --- --- --- --- 23 --- 21 | 30 64 --- --- --- --- 25 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1811 18 21 28 32 22 26 19 117 |T 33 36 34 36 39 34 35 46 31
WRMS | 1811 17 21 28 27 15 22 17 117 |NE 28 32 29 30 33 30 32 36 27
MEDI | 1351 13 11 27 21 15 17 15 72 |MD 30 33 31 32 34 33 33 48 28
Table 3.2094.6 GPS week: 2094 Day: 6 MJD: 58908
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 3134 48 33 45 53 53 22 33 --- 20 | 98 93 87 96 108 96 99 --- 90
R02E | 966 8 14 18 11 8 14 8 67 5 | 36 40 41 35 41 40 36 60 37
R03E | 1265 7 12 23 13 19 12 14 96 6 | 86 87 80 80 95 82 84 56 84
XR04E | 1543 11 15 31 14 --- 20 18 --- 9 | 33 34 36 33 --- 34 37 --- 32
R05E | 1453 8 14 32 13 21 15 14 --- 8 | 52 53 48 48 61 45 53 --- 51
R07E | 974 11 14 26 15 16 17 13 108 7 | 37 39 33 38 39 37 38 61 35
R08E | 1234 15 15 26 8 14 14 13 --- 7 | 63 61 65 67 74 65 63 --- 65
R09 | 723 16 17 17 7 22 10 10 --- 7 | 19 23 23 24 28 24 19 --- 18
R11 | 1135 9 15 11 13 18 29 11 272 7 | 36 38 33 40 37 46 36 36 36
R12 | 1300 17 23 15 20 22 27 12 --- 8 | 49 52 46 39 47 51 54 --- 45
R13 | 4128 24 27 28 41 21 59 26 --- 14 | 53 52 52 28 42 40 47 --- 41
R14 | 1631 12 16 13 23 9 29 20 --- 8 | 37 40 30 30 37 32 39 --- 32
R15 | 576 8 13 15 26 9 17 17 --- 7 | 46 48 44 35 41 49 44 --- 42
R16 | 1412 32 41 26 26 23 28 27 --- 12 | 43 51 34 54 45 48 45 --- 41
R17 | 1008 8 14 26 42 16 14 18 --- 9 | 67 67 60 45 69 71 75 --- 64
R18 | 924 12 22 20 18 7 24 22 --- 7 | 52 52 50 51 56 65 62 --- 54
R19 | 1417 27 31 48 84 26 41 23 --- 18 | 85 86 56 44 89 84 96 --- 75
R20 | 1724 24 25 53 15 19 70 33 --- 16 | 47 52 48 45 63 63 57 --- 51
R21 | 1666 10 13 26 33 11 18 23 97 9 | 66 65 51 46 73 76 81 45 66
R22 | 1912 9 15 29 33 16 16 17 --- 9 | 67 66 48 48 71 74 72 --- 64
R23 | 508 12 14 19 28 11 13 14 --- 7 | 31 34 40 56 43 46 45 --- 40
XR26 | ---- 12 41 --- --- --- --- 15 --- 14 | 31 46 --- --- --- --- 29 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1673 19 21 28 32 21 29 20 147 |T 51 53 47 46 57 55 55 51 49
WRMS | 1673 15 19 28 30 17 24 17 147 |NE 48 51 43 41 52 54 53 40 46
MEDI | 1300 12 15 26 20 16 18 17 97 |MD 47 52 48 45 47 49 47 56 42
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