[IGSREPORT-24264] Wk 1883 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Feb 25 15:42:18 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1883 (Feb 07, 2016 - Feb 13, 2016)
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 2.1883.
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:
igl1883[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1883 in the SP3 format.
igl18837.sum Combination Report for GPS Week 1883.
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
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 | -27.1 ns
1 | -29.3 ns
2 | -19.5 ns
3 | -11.7 ns
4 | -10.8 ns
5 | -7.5 ns
6 | -3.3 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 | ESX | R17
0 | GRG | R17
1 | ESX | R17
1 | GRG | R17
2 | ESX | R17
2 | GRG | R17
3 | ESX | R17
3 | GRG | R17
4 | ESX | R17
4 | GRG | R17
5 | ESX | R17
5 | GRG | R17
6 | ESX | R17
6 | GRG | R17
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 1.1883, 1a.1883).
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 2.1883.0-6)
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 3.1883.0-6).
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 1883 summary. (Feb 07, 2016 - Feb 13, 2016)
Table 1.1883.a GPS week : 1883 MJD: 57425.0-57431.0
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| -2 2 -17 27 -4 -119 .24 39 37 | --- --- --- ---
| 1 2 3 19 23 34 .03 | --- ---
cof n/a| -1 1 -18 28 4 -104 .24 42 39 | --- --- --- ---
| 2 2 3 16 26 31 .07 | --- ---
emx n/a| 0 0 -4 -1 -47 -81 .26 29 29 | -18314 -901 3831 7210
| 1 1 2 26 18 30 .05 | 13007 1011
esx n/a| 0 0 3 -32 -14 15 -.12 22 20 | 1322951 -5302 573153 574652
| 0 1 2 23 25 24 .03 | 1263976 1581
gfz n/a| 0 0 3 38 61 66 .04 24 21 | 0 -2090 3708 6969
| 1 1 2 27 25 54 .04 | 0 1730
grg n/a| -3 2 7 -32 29 30 -.33 38 36 | -568279 -2020 4376 684544
| 1 1 5 17 22 66 .07 | 28571 1366
iac n/a| 1 1 0 -5 -15 28 -.06 24 24 | -14232 -327 3808 7214
| 0 1 1 47 45 45 .03 | 10019 750
mcc n/a| -1 0 0 25 99 711 -.15 140 140 | --- --- --- ---
| 8 18 13 95 86 601 .53 | --- ---
Table 1.1883.b GPS week : 1883 MJD: 57425.0-57431.0
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 | 13 14 13 10 10 10 11 |
R02 | 10 9 10 10 9 10 18 |
R03 | 10 10 13 10 11 11 9 |
R04 | 7 9 9 9 10 11 12 |
R05 | 13 16 13 14 14 13 12 |
R06 | 8 9 8 10 9 9 8 |
R07 | 11 8 9 11 9 11 12 |
R08 | 9 10 9 9 10 12 10 |
R09 | 13 12 12 11 12 13 14 |
R10 | 8 9 7 9 9 10 9 |
R11 | 19 28 19 16 13 17 25 |
R12 | 17 24 20 13 15 20 20 |
R13 | 10 9 10 9 9 9 15 |
R14 | 17 15 16 15 13 17 17 |
R15 | 10 10 15 11 12 11 17 |
R16 | 12 12 10 9 12 11 12 |
R17 | 12 13 14 15 14 13 10 |
R18 | 11 11 8 11 14 11 10 |
R19 | 12 12 11 11 11 11 12 |
R20 | 13 15 14 15 21 17 23 |
R21 | 12 12 13 13 21 12 13 |
R22 | 14 13 13 12 13 16 13 |
R23 | 9 10 10 9 8 12 9 |
R24 | 15 16 12 15 16 14 14 |
R26 | 18 54 54 30 19 27 26 |
Table 1.1883.c GPS week : 1883 MJD: 57425.0-57431.0
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 1883 0 | 2 -5 -4 41 -157 2352 86.8 1540 1540 | -27092 0
brd 1883 1 | 5 -8 6 460 -203 -304 85.5 1428 1428 | -29270 0
brd 1883 2 | -1 47 52 -1026 227 -3470 84.2 1526 1526 | -19521 0
brd 1883 3 | -51 -9 68 37 -884 -4167 83.6 1473 1473 | -11664 0
brd 1883 4 | 33 -150 91 -123 -228 -3605 82.6 10170 10170 | -10787 0
brd 1883 5 | 81 -15 69 -416 -311 -2089 85.5 1455 1455 | -7532 0
brd 1883 6 | 75 14 77 723 320 -3143 83.6 1352 1352 | -3288 0
-------------+------------------------------------------------------------+----------------
brd 1883 mean| 20 -17 51 -43 -176 -2060 84.6 2706 2706 | -15593 0
brd 1883 sdev| 46 62 36 572 394 2328 1.4 3291 3291 | 9913 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 2.1883.0 GPS week: 1883 Day: 0 MJD: 57425
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 3 -17 -6 -51 -178 .24 40 36 | --- --- --- ---
cof n/a| 1 3 -18 24 -40 -143 .31 43 38 | --- --- --- ---
emx n/a| 2 0 -1 13 -50 -80 .30 31 32 | -28699 -1693 4418 7416
esx n/a| 0 1 7 -25 -35 -20 -.09 20 19 | -26994 -3950 4326 7391
gfz n/a| -1 -2 1 61 64 17 .11 27 23 | 0 -3864 4109 7154
grg n/a| -5 2 -1 -55 29 55 -.20 37 33 | -575773 -2249 4380 682930
iac n/a| 1 1 0 -16 51 90 -.10 18 18 | -25955 -209 4315 7426
mcc n/a| -9 5 -23 -1 -6 1858 .68 243 243 | --- --- --- ---
Table 2.1883.1 GPS week: 1883 Day: 1 MJD: 57426
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 4 -22 21 6 -86 .18 41 39 | --- --- --- ---
cof n/a| 0 4 -21 37 34 -75 .11 47 42 | --- --- --- ---
emx n/a| 0 0 -5 24 -71 -59 .19 26 26 | -36110 -1861 3657 6681
esx n/a| 0 0 3 3 -7 7 -.12 22 20 | -27342 -4154 3529 8115
gfz n/a| 0 0 0 57 66 104 .06 25 21 | 0 -4533 3587 6974
grg n/a| -3 2 11 0 58 22 -.30 37 34 | -581726 -4507 4493 687168
iac n/a| 1 0 2 -62 -5 25 -.07 24 24 | -27455 -1069 3621 7292
mcc n/a| -3 21 -7 13 190 933 -.61 117 117 | --- --- --- ---
Table 2.1883.2 GPS week: 1883 Day: 2 MJD: 57427
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| -3 0 -21 20 9 -125 .24 39 40 | --- --- --- ---
cof n/a| -1 0 -24 2 25 -116 .23 43 43 | --- --- --- ---
emx n/a| 0 -1 -4 7 -50 -39 .25 24 23 | -22035 68 4186 6829
esx n/a| 0 -1 3 -23 14 19 -.12 23 21 | -22720 -3469 4226 7066
gfz n/a| 0 -1 1 14 83 10 -.02 25 19 | 0 -1191 4034 6514
grg n/a| -4 0 7 -34 -10 47 -.32 33 33 | -577087 -1622 7119 685624
iac n/a| 3 3 1 -10 -47 25 -.05 22 22 | -19017 -451 4198 6887
mcc n/a| -15 -1 -7 27 222 998 -.92 101 101 | --- --- --- ---
Table 2.1883.3 GPS week: 1883 Day: 3 MJD: 57428
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 -21 39 -11 -127 .25 38 39 | --- --- --- ---
cof n/a| -3 -2 -21 44 18 -51 .28 38 39 | --- --- --- ---
emx n/a| 1 0 -8 -7 -16 -109 .33 30 32 | 3039 -139 3614 7638
esx n/a| 1 0 2 -41 11 21 -.12 21 19 | 2235443 -6241 999999 999999
gfz n/a| 0 0 6 25 94 20 .02 20 17 | 0 -864 3453 6895
grg n/a| -5 3 5 -29 40 -44 -.40 36 34 | -567024 -1277 3571 683248
iac n/a| 1 2 0 -1 -84 90 -.08 19 19 | -10381 -140 3564 7069
mcc n/a| 0 -13 2 -116 136 121 -.20 120 120 | --- --- --- ---
Table 2.1883.4 GPS week: 1883 Day: 4 MJD: 57429
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| -3 1 -13 32 20 -69 .24 37 35 | --- --- --- ---
cof n/a| 0 2 -13 22 14 -113 .32 38 38 | --- --- --- ---
emx n/a| 0 2 -4 -14 -28 -109 .24 31 32 | -14806 -2326 3411 6892
esx n/a| 1 0 0 -58 -51 -2 -.07 26 21 | 2275665 -7718 999999 999999
gfz n/a| 0 0 5 65 14 92 .06 22 22 | 0 -2992 3386 6583
grg n/a| -4 3 7 -39 48 144 -.35 36 38 | -612343 -3000 3542 694405
iac n/a| 1 -2 0 -4 1 -14 -.04 21 21 | -9378 -345 3449 6687
mcc n/a| 4 14 11 -35 79 322 .20 103 103 | --- --- --- ---
Table 2.1883.5 GPS week: 1883 Day: 5 MJD: 57430
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| -3 4 -14 28 -4 -123 .26 38 36 | --- --- --- ---
cof n/a| -4 0 -20 17 3 -124 .21 42 39 | --- --- --- ---
emx n/a| 1 -1 -5 -52 -56 -116 .30 32 31 | -21268 -216 3662 8525
esx n/a| 1 0 2 -63 0 54 -.16 23 21 | 2338139 -4983 999999 999999
gfz n/a| -1 0 4 -6 51 62 .04 24 22 | 0 198 3591 8304
grg n/a| -2 3 15 -23 15 38 -.33 38 37 | -534005 -593 3650 680325
iac n/a| 0 1 0 89 -38 -10 -.07 23 23 | -5701 -1178 3654 8578
mcc n/a| 4 3 13 113 59 399 -.31 110 110 | --- --- --- ---
Table 2.1883.6 GPS week: 1883 Day: 6 MJD: 57431
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 -14 56 3 -125 .29 40 34 | --- --- --- ---
cof n/a| -2 4 -13 49 -21 -104 .21 42 37 | --- --- --- ---
emx n/a| 1 0 -3 17 -58 -57 .25 28 28 | -8325 -146 3870 6492
esx n/a| 1 -1 2 -19 -34 30 -.14 20 20 | 2488467 -6602 999999 999999
gfz n/a| -2 1 5 48 53 156 .03 26 26 | 0 -1390 3799 6365
grg n/a| -1 1 6 -45 23 -54 -.42 49 42 | -529996 -897 3877 678108
iac n/a| 1 1 2 -33 14 -5 -.02 39 39 | -1740 1102 3856 6560
mcc n/a| 6 -35 5 175 13 351 .08 189 189 | --- --- --- ---
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 3.1883.0 GPS week: 1883 Day: 0 MJD: 57425
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 | 1266 36 18 25 18 37 49 11 --- 12 | 74 67 64 53 63 47 42 --- 49
R02 | 521 20 20 33 16 11 28 21 --- 9 | 64 65 69 53 46 41 37 --- 48
R03 | 1016 25 31 33 12 16 14 22 127 9 | 67 71 73 56 43 51 33 30 49
R04 | 790 23 31 12 15 17 13 13 --- 6 | 73 80 55 58 58 50 44 --- 53
R05 | 523 56 21 15 28 27 39 20 --- 13 | 62 60 41 58 43 39 30 --- 40
R06 | 1962 14 13 19 17 19 21 11 --- 7 | 59 59 58 58 45 49 46 --- 50
R07 | 917 25 26 44 18 13 24 12 126 10 | 72 74 74 46 47 43 45 34 49
R08 | 1228 22 20 31 15 10 31 14 --- 9 | 69 68 69 51 50 38 44 --- 49
R09E | 2325 29 35 32 26 26 41 22 --- 12 | 39 41 31 46 45 43 42 --- 34
R10E | 1912 27 43 20 16 18 20 15 --- 8 | 40 50 36 30 32 31 35 --- 30
R11E | 1078 66 59 56 21 55 54 18 --- 19 | 77 78 51 70 84 93 70 --- 60
R12E | 955 56 83 47 24 39 44 27 438 16 | 105 111 96 93 101 119 93 173 94
R13E | 1418 41 47 24 12 17 28 15 --- 9 | 137 138 124 129 134 132 118 --- 127
R14E | 2364 50 44 42 38 32 47 30 --- 17 | 83 78 57 41 43 71 64 --- 49
R15E | 4255 29 37 28 18 30 24 16 --- 10 | 41 46 30 29 37 37 27 --- 27
R16E | 1377 27 34 41 16 13 37 22 --- 11 | 42 42 30 31 33 27 29 --- 26
XR17E | 2909 27 27 --- 319 17 300 9 --- 11 | 21 29 --- 1 33 124 31 --- 27
R18 | 747 44 49 21 13 30 35 11 --- 10 | 64 72 37 48 32 27 36 --- 36
R19 | 1076 52 50 17 13 21 39 21 --- 11 | 51 51 33 39 41 56 32 --- 35
R20 | 732 48 71 39 14 31 46 12 --- 13 | 75 86 60 63 64 64 53 --- 57
R21 | 636 55 52 24 14 29 35 11 116 11 | 58 60 34 44 43 36 35 50 35
R22 | 1042 63 60 29 12 37 37 13 --- 13 | 71 67 37 32 33 20 24 --- 26
R23 | 757 26 22 20 23 17 26 12 --- 9 | 26 29 28 52 30 22 36 --- 32
R24 | 1215 25 44 30 36 28 63 19 --- 15 | 55 68 46 65 38 41 33 --- 41
XR26 | ---- 31 144 --- --- --- --- 10 --- 18 | 51 279 --- --- --- --- 54 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1540 40 43 31 20 27 37 18 243 |T 63 74 53 51 50 54 45 71 46
WRMS | 1540 36 38 32 19 23 33 18 243 |NE 64 64 55 50 45 38 37 32 43
MEDI | 1076 29 37 29 16 21 35 15 126 |MD 64 67 51 51 43 43 37 34 48
Table 3.1883.1 GPS week: 1883 Day: 1 MJD: 57426
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 | 1701 45 53 33 29 20 45 17 --- 13 | 63 77 49 54 48 18 35 --- 39
R02M | 553 21 22 30 10 14 31 13 --- 8 | 47 49 54 41 43 45 38 --- 41
R03 | 1265 19 21 30 14 17 15 24 128 9 | 44 40 53 38 31 39 23 24 35
R04 | 865 32 40 17 13 13 24 20 --- 8 | 54 56 37 33 44 33 22 --- 32
R05 | 846 61 83 22 24 29 57 29 --- 15 | 50 87 32 43 59 30 21 --- 34
R06M | 1387 21 25 19 8 10 50 14 --- 9 | 51 53 46 40 44 37 44 --- 40
R07 | 1419 24 25 17 13 13 23 14 76 7 | 53 54 41 43 35 35 35 53 38
R08 | 547 36 37 27 20 18 19 14 --- 9 | 49 49 39 28 24 22 21 --- 24
R09E | 1673 26 30 32 23 19 39 20 --- 11 | 44 49 36 45 55 46 52 --- 42
R10E | 1501 28 31 22 17 14 27 13 --- 8 | 38 43 30 26 27 28 31 --- 25
XR11E |12395 89 66 43 --- 61 59 42 --- 28 | 135 137 136 --- 137 131 119 --- 117
R12E | 911 68 75 38 45 48 46 73 --- 24 | 247 256 219 257 222 202 167 --- 214
R13E | 721 43 60 18 16 16 26 13 --- 9 | 150 160 140 150 145 145 132 --- 142
R14E | 1000 31 39 35 20 50 41 24 --- 15 | 71 79 52 60 82 69 51 --- 56
R15E | 4381 18 26 27 14 27 23 20 --- 10 | 43 44 29 38 61 40 25 --- 34
R16E | 1479 30 41 29 22 17 49 21 --- 12 | 46 47 30 39 34 37 29 --- 28
XR17E | 2226 --- --- --- 282 13 303 12 --- 12 | --- --- --- 1 36 106 31 --- 31
R18M | 627 37 35 14 28 14 43 19 --- 11 | 42 39 26 48 36 33 24 --- 31
R19M | 822 55 57 25 11 29 38 13 --- 12 | 54 64 50 48 52 55 39 --- 44
R20M | 946 54 43 32 20 28 39 36 --- 15 | 99 102 97 113 114 93 84 --- 97
R21M | 503 55 69 22 16 18 37 19 136 11 | 61 71 49 49 48 48 40 65 45
R22 | 941 67 69 17 16 25 43 14 --- 12 | 46 51 21 28 27 29 20 --- 20
R23 | 1043 29 34 20 28 16 25 9 --- 9 | 21 23 22 31 21 19 20 --- 17
R24M | 1180 40 47 33 34 46 45 17 --- 15 | 48 57 41 50 39 30 30 --- 31
XR26M | ---- 90 856 --- --- --- --- 31 --- 54 | 96 720 --- --- --- --- 81 --- 76
------+---------------------------------------------------+-----------------------------------------------
RMS | 1428 41 47 26 22 25 37 24 116 |T 68 100 57 56 61 57 48 47 53
WRMS | 1428 39 42 26 20 21 34 24 116 |NE 47 54 36 37 36 28 24 38 29
MEDI | 1000 36 40 27 20 18 39 19 128 |MD 50 54 41 43 44 37 35 53 38
Table 3.1883.2 GPS week: 1883 Day: 2 MJD: 57427
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 | 2315 48 67 38 20 28 27 16 --- 13 | 68 88 49 32 43 28 27 --- 31
R02 | 607 23 24 24 18 16 23 23 --- 9 | 42 45 43 38 45 31 26 --- 33
R03 | 1688 19 22 34 21 23 48 26 107 13 | 56 62 66 57 50 16 28 26 43
R04 | 1495 28 36 18 15 11 14 25 --- 8 | 54 57 41 39 32 35 15 --- 31
R05 | 1005 51 50 14 25 12 43 29 --- 12 | 49 54 34 43 40 36 21 --- 32
R06 | 1683 22 31 19 11 14 25 15 --- 7 | 47 55 41 40 39 37 34 --- 35
R07 | 650 29 38 15 17 18 32 17 109 9 | 59 69 42 46 47 20 27 42 37
R08 | 790 29 34 13 24 14 21 22 --- 9 | 56 61 37 52 29 35 22 --- 34
R09E | 1270 23 29 27 27 24 29 27 --- 12 | 43 43 26 40 29 35 44 --- 29
R10E | 1605 23 24 17 16 9 23 11 --- 7 | 39 38 31 29 31 30 32 --- 28
XR11E |10885 52 53 33 --- 38 43 31 --- 19 | 82 98 77 --- 91 92 64 --- 72
R12E | 1562 54 50 33 57 30 50 41 --- 19 | 116 99 98 104 101 123 108 --- 99
R13E | 1366 34 38 22 16 22 22 19 --- 9 | 112 123 105 107 114 96 91 --- 102
R14E | 1639 39 50 34 21 47 34 28 --- 15 | 46 60 46 52 74 51 43 --- 43
R15E | 4000 21 29 28 20 54 25 25 --- 14 | 41 50 42 46 65 45 28 --- 36
R16E | 1323 34 31 28 18 14 28 17 --- 10 | 47 52 29 31 34 38 24 --- 26
XR17E | 2207 --- --- --- 278 15 259 13 --- 14 | --- --- --- 1 33 99 26 --- 27
R18 | 664 39 46 11 16 16 23 9 --- 8 | 131 132 127 123 128 116 117 --- 122
R19 | 798 47 48 20 13 23 34 14 --- 10 | 48 50 33 33 31 46 23 --- 28
R20 | 943 61 65 22 29 27 40 22 --- 14 | 63 66 69 73 71 72 57 --- 63
R21 | 571 59 57 25 13 25 44 17 86 13 | 55 52 29 31 25 29 25 69 24
R22 | 1302 65 66 26 13 23 44 13 --- 13 | 57 58 42 33 24 23 22 --- 27
R23 | 729 27 31 11 28 14 33 10 --- 9 | 19 22 25 38 26 22 20 --- 20
R24 | 1435 32 40 20 31 29 34 22 --- 12 | 47 56 52 57 31 23 26 --- 36
XR26 | ---- 88 907 --- --- --- --- 31 --- 53 | 86 748 --- --- --- --- 58 --- 53
------+---------------------------------------------------+-----------------------------------------------
RMS | 1526 39 43 24 23 25 33 22 101 |T 60 93 51 49 51 49 40 45 44
WRMS | 1526 40 43 23 21 19 33 22 101 |NE 52 58 42 42 36 26 22 34 31
MEDI | 1323 34 38 22 20 22 32 22 107 |MD 54 57 42 40 39 35 27 42 34
Table 3.1883.3 GPS week: 1883 Day: 3 MJD: 57428
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 | 925 32 34 19 22 23 27 14 --- 9 | 53 52 27 42 24 31 20 --- 24
R02 | 715 29 28 37 12 14 25 14 --- 9 | 52 52 54 38 33 44 35 --- 35
R03 | 1648 21 27 37 16 11 31 13 94 9 | 59 60 67 43 41 34 37 32 42
R04 | 1834 18 21 23 12 14 48 10 --- 9 | 54 54 48 39 30 34 39 --- 35
R05 | 1505 29 20 24 29 14 59 29 --- 13 | 46 46 57 61 48 52 26 --- 43
R06 | 2164 29 26 21 14 16 38 19 --- 9 | 53 50 54 53 43 71 39 --- 47
R07 | 781 47 39 33 17 15 31 17 87 11 | 69 60 49 32 32 23 18 54 28
R08 | 1049 33 28 13 22 8 31 17 --- 9 | 65 59 46 46 38 33 26 --- 36
R09E | 704 25 23 29 20 20 23 24 --- 10 | 37 40 27 36 35 40 51 --- 33
R10E | 1277 30 32 28 14 11 25 19 --- 9 | 41 44 40 35 32 35 32 --- 31
R11E | 1509 49 30 41 27 28 51 28 --- 15 | 99 100 94 70 99 104 110 --- 97
R12E | 1640 45 34 38 22 23 38 23 176 13 | 146 146 122 139 152 138 140 164 139
R13E | 2720 26 27 27 17 16 33 13 --- 9 | 121 119 122 119 124 142 120 --- 122
R14E | 1464 40 32 46 26 33 33 21 --- 14 | 79 79 51 73 96 83 70 --- 70
R15E | 2960 22 48 25 15 32 24 20 --- 10 | 46 61 40 38 61 43 29 --- 37
R16E | 1294 30 38 22 19 17 18 14 --- 8 | 39 45 33 35 29 26 24 --- 24
XR17E | 2907 --- --- --- >>>> 13 260 16 --- 14 | --- --- --- 1 31 106 31 --- 29
R18 | 780 42 41 21 20 18 41 10 --- 10 | 261 261 255 261 253 262 245 --- 254
R19 | 634 44 43 25 19 14 43 16 --- 11 | 54 56 49 38 37 44 39 --- 38
R20 | 958 57 64 34 29 27 40 27 --- 15 | 79 85 60 67 66 78 54 --- 60
R21 | 593 57 63 25 21 27 39 17 99 13 | 72 74 60 66 47 54 44 87 51
R22 | 1356 65 71 24 14 18 38 13 --- 12 | 61 65 35 28 28 25 21 --- 25
R23 | 729 28 26 8 25 12 29 12 --- 8 | 26 25 30 49 31 26 31 --- 30
R24 | 1423 30 32 55 29 23 41 29 --- 15 | 43 45 61 60 25 39 22 --- 34
XR26 | ---- 52 1674 --- --- --- --- 16 --- 30 | 85 9999 --- --- --- --- 57 --- 65
------+---------------------------------------------------+-----------------------------------------------
RMS | 1472 38 38 30 21 20 36 19 120 |T 72 72 64 61 59 65 54 84 57
WRMS | 1472 39 39 32 19 17 34 19 120 |NE 54 52 44 42 34 32 27 43 32
MEDI | 1294 30 32 25 20 16 33 17 94 |MD 54 59 51 43 37 43 37 54 37
Table 3.1883.4 GPS week: 1883 Day: 4 MJD: 57429
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
------+---------------------------------------------------+-----------------------------------------------
XR01 | 669 25 20 19 23 14 --- 17 --- 9 | 35 30 29 41 29 --- 18 --- 26
R02 | 1277 24 21 29 17 23 21 12 --- 9 | 52 48 43 41 41 44 37 --- 38
R03 | 879 31 32 37 11 24 22 14 78 10 | 55 55 59 33 23 36 32 20 34
R04 | 1114 22 24 33 13 17 39 11 --- 9 | 50 50 59 37 40 21 36 --- 37
R05 | 1538 24 22 38 20 12 64 26 --- 14 | 48 59 61 57 45 37 31 --- 43
R06 | 1381 14 21 25 19 9 18 23 --- 8 | 49 53 50 46 34 53 25 --- 37
R07 | 947 24 35 23 11 10 22 27 94 9 | 55 64 45 34 40 53 23 27 36
XR08 | 1403 29 35 22 16 7 --- 22 --- 9 | 53 59 43 41 34 --- 21 --- 33
R09E | 546 30 34 25 31 16 35 26 --- 12 | 34 38 38 58 42 50 47 --- 38
R10E | 1656 40 38 15 14 13 22 11 --- 8 | 45 47 49 47 46 59 40 --- 44
R11E | 1501 50 42 24 25 25 32 27 --- 13 | 64 72 68 56 65 67 62 --- 56
R12E | 1814 57 58 30 21 26 43 29 144 14 | 78 79 73 61 84 90 73 75 69
R13E | 2482 31 26 16 16 12 36 17 --- 9 | 69 69 58 69 59 69 64 --- 61
R14E | 1297 40 42 30 21 30 34 27 --- 13 | 75 74 51 47 63 57 49 --- 50
R15E | 2921 34 37 29 18 28 23 27 --- 12 | 45 51 53 43 47 43 22 --- 34
R16E | 543 33 27 38 27 20 31 18 --- 12 | 39 36 34 47 33 34 30 --- 28
XR17E | 2055 --- --- --- >>>> 13 290 14 --- 13 | --- --- --- 1 31 112 26 --- 26
R18 | 828 38 39 48 24 21 46 17 --- 14 | 372 374 357 371 373 371 376 --- 371
R19 | 845 37 45 17 22 12 47 15 --- 10 | 42 48 32 38 23 34 28 --- 27
XR20 | 629 54 49 69 21 20 --- 44 --- 21 | 69 63 61 59 57 --- 44 --- 52
R21 |45011 44 54 25 82 34 34 29 83 21 | 48 54 28 80 25 33 25 46 32
R22 | 893 66 66 20 12 32 35 6 --- 13 | 56 56 22 20 28 30 20 --- 18
R23 | 1125 24 26 9 13 16 30 16 --- 7 | 24 26 24 25 29 28 21 --- 21
R24 | 2439 30 29 62 19 27 53 11 --- 15 | 31 29 36 29 35 36 18 --- 21
XR26 | ---- 30 138 --- --- --- --- 10 --- 18 | 54 470 --- --- --- --- 42 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS |10172 37 38 31 26 22 36 21 103 |T 64 83 59 57 55 64 48 42 51
WRMS |10172 35 38 32 21 22 38 21 103 |NE 47 49 42 36 33 34 25 23 31
MEDI | 1277 31 35 25 19 17 34 17 83 |MD 50 54 49 43 40 44 31 27 37
Table 3.1883.5 GPS week: 1883 Day: 5 MJD: 57430
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 | 1033 23 42 23 15 15 33 24 --- 9 | 29 51 47 45 41 23 23 --- 31
R02 | 1311 28 35 16 20 14 33 20 --- 9 | 40 50 37 43 35 48 23 --- 29
R03 | 1290 29 33 22 21 30 28 12 75 10 | 48 52 39 43 25 30 32 19 31
R04 | 1164 35 45 38 10 23 31 11 --- 10 | 44 51 43 31 23 20 18 --- 23
R05 | 1052 33 51 34 22 13 47 22 --- 12 | 29 51 34 36 24 32 34 --- 25
R06 | 1320 19 17 12 12 23 39 14 --- 9 | 32 35 28 32 34 42 26 --- 27
R07 | 939 28 31 32 20 14 24 30 105 11 | 46 48 46 42 35 45 28 23 35
R08 | 736 26 25 42 20 10 29 26 --- 11 | 44 45 58 43 29 28 15 --- 31
R09E | 714 27 34 35 29 26 29 23 --- 12 | 34 46 38 47 46 37 45 --- 35
R10E | 1809 31 29 16 18 17 21 25 --- 9 | 54 55 45 50 54 50 32 --- 43
R11E | 1212 66 54 37 19 26 59 32 --- 16 | 100 100 85 64 89 91 88 --- 85
R12E | 2558 59 62 33 53 37 36 46 138 20 | 127 133 109 94 109 115 99 44 101
R13E | 3077 30 29 22 16 13 22 15 --- 8 | 98 93 86 93 90 93 89 --- 89
R14E | 1001 37 35 54 30 30 53 27 --- 16 | 67 69 57 76 76 65 53 --- 61
R15E | 2550 24 36 27 22 35 22 13 --- 11 | 41 49 24 38 38 37 32 --- 27
R16E | 528 44 43 29 18 18 24 20 --- 11 | 37 49 30 33 30 28 30 --- 26
XR17E | 1919 --- --- --- >>>> 12 308 13 --- 12 | --- --- --- 1 32 113 21 --- 24
R18 | 998 39 37 18 19 25 38 14 --- 11 | 492 491 503 488 486 485 486 --- 489
R19 | 1268 49 44 19 12 20 44 10 --- 11 | 41 33 29 35 32 30 26 --- 27
R20 | 886 52 72 39 27 33 68 21 --- 17 | 70 90 70 71 65 97 47 --- 63
R21 | 504 38 38 24 17 15 36 28 113 11 | 57 57 54 48 47 41 34 31 41
R22 | 559 59 62 30 24 35 39 29 --- 15 | 53 54 41 53 47 38 19 --- 34
R23 | 1235 33 36 36 26 19 24 18 --- 11 | 29 33 42 43 32 38 28 --- 30
R24 | 2007 23 23 47 15 24 56 14 --- 13 | 29 29 33 33 36 31 19 --- 26
XR26 | ---- 39 83 --- --- --- --- 19 --- 27 | 48 220 --- --- --- --- 36 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1454 38 42 32 23 24 38 23 110 |T 70 82 68 65 64 69 55 29 58
WRMS | 1454 36 39 31 21 22 37 23 110 |NE 40 48 43 42 32 31 24 21 30
MEDI | 1164 33 36 30 20 20 33 20 105 |MD 44 51 43 43 36 38 32 23 31
Table 3.1883.6 GPS week: 1883 Day: 6 MJD: 57431
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 | 2219 31 34 29 20 17 15 28 --- 10 | 55 62 50 50 37 25 32 --- 36
R02 | 823 35 38 22 18 13 114 21 --- 18 | 63 65 51 45 37 46 36 --- 41
R03 | 1420 31 33 15 17 20 24 20 88 9 | 69 72 60 55 33 29 37 22 44
R04 | 573 38 39 23 16 37 17 18 --- 11 | 66 67 59 40 38 27 32 --- 37
R05 | 863 39 41 15 25 22 43 23 --- 12 | 61 65 39 54 44 36 33 --- 40
R06 | 1198 20 27 20 15 16 27 12 --- 8 | 61 67 53 53 39 53 44 --- 46
R07 | 962 24 26 42 11 25 35 18 165 12 | 73 75 75 48 41 42 37 32 48
R08 | 1123 23 24 34 14 22 21 22 --- 10 | 67 71 71 49 42 28 31 --- 46
R09E | 981 33 38 35 24 28 28 40 --- 14 | 82 91 74 96 86 82 101 --- 85
R10E | 1643 26 28 19 15 14 24 22 --- 8 | 43 38 47 35 41 42 43 --- 38
R11E | 672 72 76 41 27 42 32 105 --- 25 | 107 112 85 71 95 120 173 --- 104
R12E | 1619 72 70 42 16 29 57 62 290 20 | 182 179 176 191 187 165 169 59 177
R13E | 3550 26 31 28 19 19 22 65 --- 14 | 97 106 96 99 98 98 68 --- 89
R14E | 1329 50 52 32 18 48 51 25 --- 16 | 60 65 20 28 60 52 40 --- 30
R15E | 2055 36 34 40 20 30 23 66 --- 16 | 44 47 45 45 57 44 43 --- 34
R16E | 687 21 32 33 20 18 29 37 --- 12 | 43 46 25 46 46 44 45 --- 38
XR17E | 3448 17 15 --- >>>> 14 290 13 --- 10 | 14 15 --- 1 29 132 22 --- 22
R18 | 735 42 47 16 13 23 31 11 --- 10 | 627 629 622 625 621 621 616 --- 621
R19 | 546 39 45 18 18 27 38 18 --- 11 | 60 65 45 42 25 31 36 --- 35
R20 | 1102 65 55 22 26 24 130 28 --- 22 | 88 82 66 72 62 75 51 --- 60
R21 | 543 33 41 26 26 18 46 23 152 12 | 57 63 46 40 29 42 29 63 32
R22 | 569 44 49 22 18 18 47 33 --- 13 | 65 68 37 40 35 26 19 --- 29
R23 | 802 26 25 21 18 17 21 19 --- 9 | 23 24 38 43 30 28 31 --- 30
R24 | 757 36 43 29 22 31 57 15 --- 13 | 33 44 49 39 25 26 24 --- 27
XR26 | ---- 33 112 --- --- --- --- 19 --- 26 | 54 197 --- --- --- --- 42 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1351 40 42 28 20 26 49 39 188 |T 87 96 83 79 76 79 73 44 73
WRMS | 1351 34 37 28 20 26 42 39 188 |NE 59 63 53 47 37 30 31 27 38
MEDI | 962 33 38 26 18 22 31 22 152 |MD 61 67 51 46 41 42 37 32 40
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