[IGSREPORT-24287] Wk 1884 IGLOS Final Orbits
IGS ACC
acc at igs.org
Tue Mar 8 19:00:42 PST 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1884 (Feb 14, 2016 - Feb 20, 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 2.1884.
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:
igl1884[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1884 in the SP3 format.
igl18847.sum Combination Report for GPS Week 1884.
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 | -9.6 ns
1 | -0.3 ns
2 | -2.2 ns
3 | 7.6 ns
4 | 10.5 ns
5 | 0.4 ns
6 | 8.7 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 | COD | R12 R16
0 | GRG | R16
3 | EMX | R09
5 | EMX | R09
6 | EMX | R09
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 1.1884, 1a.1884).
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 2.1884.0-6)
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 3.1884.0-6).
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 1884 summary. (Feb 14, 2016 - Feb 20, 2016)
Table 1.1884.a GPS week : 1884 MJD: 57432.0-57438.0
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 -15 36 -4 -24 .27 42 41 | --- --- --- ---
| 2 1 3 32 27 33 .07 | --- ---
cof n/a| -1 0 -16 36 8 -28 .25 45 43 | --- --- --- ---
| 3 1 3 33 29 35 .11 | --- ---
emx n/a| 0 -1 -5 -6 -51 -53 .30 29 30 | 0 -88 3766 7037
| 1 1 2 21 16 56 .07 | 0 1068
esx n/a| 1 1 1 -37 -13 -10 -.10 20 18 | -2901 -290 3627 7326
| 1 1 1 12 22 19 .03 | 9935 2427
gfz n/a| -1 0 4 55 66 82 .08 25 22 | 4718 -696 3484 6452
| 1 1 1 37 25 19 .04 | 8162 2164
grg n/a| -3 0 11 -56 17 4 -.44 44 38 | -482002 -776 4213 624402
| 1 1 4 48 33 65 .07 | 6216 2411
iac n/a| 0 0 0 2 -3 3 -.15 22 22 | 3174 117 3875 7683
| 0 1 1 36 39 42 .04 | 7103 1368
mcc n/a| 1 4 -1 3 -2 973 -.47 205 205 | --- --- --- ---
| 6 4 18 76 220 290 .61 | --- ---
Table 1.1884.b GPS week : 1884 MJD: 57432.0-57438.0
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 12 14 15 12 11 11 |
R02 | 10 9 10 9 9 9 9 |
R03 | 8 9 17 11 11 11 12 |
R04 | 9 9 11 9 10 11 9 |
R05 | 14 17 13 11 14 15 16 |
R06 | 9 10 10 8 8 9 10 |
R07 | 13 13 12 10 11 12 11 |
R08 | 12 12 13 12 11 11 10 |
R09 | 57 0 48 119 120 148 150 |
R10 | 10 8 10 9 9 11 9 |
R11 | 17 29 16 14 15 14 15 |
R12 | 500 --- --- --- --- --- --- |
R13 | 11 11 11 10 17 9 8 |
R14 | 20 16 13 16 12 16 15 |
R15 | 14 26 12 10 12 12 12 |
R16 | 19 --- --- --- --- --- --- |
R17 | 124 18 0 84 86 89 87 |
R18 | 11 12 10 10 11 11 10 |
R19 | 11 11 16 11 13 10 10 |
R20 | 16 19 12 14 13 15 19 |
R21 | 11 10 12 10 10 12 12 |
R22 | 11 12 12 11 12 13 12 |
R23 | 8 11 10 9 8 9 14 |
R24 | 19 16 22 15 16 13 15 |
R26 | 39 68 27 70 115 20 40 |
Table 1.1884.c GPS week : 1884 MJD: 57432.0-57438.0
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 1884 0 | -33 83 111 -611 -375 -3237 84.5 1624 1624 | -9560 0
brd 1884 1 | 15 -18 86 -771 -588 -5175 83.8 2709 2709 | -326 0
brd 1884 2 | -23 0 5 488 19 -6870 83.8 2496 2496 | -2158 0
brd 1884 3 | -6 18 72 -343 631 -5105 82.7 1979 1979 | 7634 0
brd 1884 4 | 9 22 101 -1187 1097 -3663 82.1 1542 1542 | 10543 0
brd 1884 5 | 0 -7 48 -1738 82 1154 84.8 1573 1573 | 371 0
brd 1884 6 | 33 -38 149 20 703 3884 85.5 1522 1522 | 8720 0
-------------+------------------------------------------------------------+----------------
brd 1884 mean| 0 8 82 -591 224 -2716 83.9 1920 1920 | 2174 0
brd 1884 sdev| 22 39 46 742 610 3845 1.2 494 494 | 7172 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 2.1884.0 GPS week: 1884 Day: 0 MJD: 57432
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 70 9 -29 .26 42 40 | --- --- --- ---
cof n/a| 0 0 -20 25 21 -13 .27 46 41 | --- --- --- ---
emx n/a| 1 -2 -4 0 -64 -80 .39 29 28 | 0 -2121 3151 6043
esx n/a| 0 2 1 -32 19 -3 -.06 19 16 | -17098 -5014 3061 6324
gfz n/a| 0 0 5 45 70 78 .11 26 21 | -7197 -4295 2967 7992
grg n/a| 0 0 11 -75 9 -89 -.31 39 34 | -490448 -5391 7166 623029
iac n/a| 1 2 0 12 -46 50 -.12 26 26 | -7868 -808 3129 8086
Table 2.1884.1 GPS week: 1884 Day: 1 MJD: 57433
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 36 -15 0 .23 43 40 | --- --- --- ---
cof n/a| 2 0 -19 84 -23 -70 .25 45 43 | --- --- --- ---
emx n/a| 0 -1 -8 6 -46 -148 .30 33 38 | 0 1429 4055 5876
esx n/a| 2 2 1 -59 -12 10 -.10 20 18 | -9653 455 4049 7370
gfz n/a| -2 0 5 115 69 72 .08 29 26 | 3807 1608 3830 5393
grg n/a| -4 1 8 -44 -52 6 -.44 53 43 | -485128 1880 4070 625000
iac n/a| 0 0 2 -20 16 69 -.24 32 32 | -680 2247 3976 5437
mcc n/a| 0 3 19 -47 228 1134 .34 146 146 | --- --- --- ---
Table 2.1884.2 GPS week: 1884 Day: 2 MJD: 57434
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 2 -18 -30 -8 -82 .16 42 42 | --- --- --- ---
cof n/a| 0 1 -18 6 53 -38 .13 45 44 | --- --- --- ---
emx n/a| 1 0 -5 -41 -38 11 .27 27 25 | 0 131 3480 6544
esx n/a| 0 1 3 -23 -23 -33 -.17 22 20 | -8546 2333 3497 7967
gfz n/a| -2 -3 7 68 99 61 .07 26 24 | 1215 185 3400 6311
grg n/a| -3 2 17 -92 36 -31 -.37 54 40 | -486766 -153 3462 624762
iac n/a| 1 0 -2 17 -22 -5 -.12 21 21 | -1437 265 3474 6241
mcc n/a| 1 11 -5 80 -19 1170 -.33 180 180 | --- --- --- ---
Table 2.1884.3 GPS week: 1884 Day: 3 MJD: 57435
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 3 -18 32 2 -37 .21 41 39 | --- --- --- ---
cof n/a| 0 0 -20 -2 -24 -57 .19 47 42 | --- --- --- ---
emx n/a| -1 -1 -7 -21 -24 -32 .20 27 28 | 0 -101 4239 7452
esx n/a| 2 1 3 -28 12 12 -.10 19 19 | 7665 1867 3610 6930
gfz n/a| -2 1 6 7 59 123 .13 24 18 | 9870 427 3370 5836
grg n/a| -1 0 13 -15 39 24 -.49 37 33 | -476834 667 3615 625254
iac n/a| 0 0 0 56 -41 -52 -.17 19 19 | 9305 243 4229 7150
mcc n/a| 8 9 23 52 -387 1299 -1.45 235 235 | --- --- --- ---
Table 2.1884.4 GPS week: 1884 Day: 4 MJD: 57436
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| -6 0 -13 33 43 -1 .37 44 42 | --- --- --- ---
cof n/a| -2 1 -11 25 25 -40 .46 43 43 | --- --- --- ---
emx n/a| 0 -2 -9 -9 -61 11 .38 29 28 | 0 451 3700 7405
esx n/a| 0 0 3 -28 -14 -15 -.09 18 16 | 9907 -345 3565 6333
gfz n/a| 0 -1 2 36 87 77 -.01 26 24 | 18333 1007 3482 5841
grg n/a| -5 3 12 -121 10 -39 -.48 40 37 | -473987 669 3554 623820
iac n/a| 1 0 0 -1 -16 -20 -.13 21 21 | 10297 -252 4144 9714
mcc n/a| 9 4 -21 79 70 631 -.25 132 132 | --- --- --- ---
Table 2.1884.5 GPS week: 1884 Day: 5 MJD: 57437
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 -10 46 -14 -38 .29 43 42 | --- --- --- ---
cof n/a| -5 3 -13 77 20 -18 .26 48 45 | --- --- --- ---
emx n/a| 0 0 -4 27 -73 -69 .31 29 26 | 0 -361 4397 8140
esx n/a| 1 2 0 -41 -43 -35 -.09 19 19 | -5316 -84 4274 7686
gfz n/a| 0 0 2 87 18 83 .10 22 17 | -362 -908 4183 6404
grg n/a| -4 0 10 -67 37 52 -.51 41 40 | -484435 -934 4292 624572
iac n/a| 1 0 -1 -62 65 3 -.12 21 21 | 2011 1153 4722 9130
mcc n/a| -3 0 -16 -51 174 996 -.84 220 220 | --- --- --- ---
Table 2.1884.6 GPS week: 1884 Day: 6 MJD: 57438
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| -4 2 -11 61 -46 17 .35 43 43 | --- --- --- ---
cof n/a| -5 -2 -14 42 -12 36 .18 43 42 | --- --- --- ---
emx n/a| 0 1 -2 -10 -53 -70 .25 32 37 | 0 -50 3345 7804
esx n/a| 2 0 0 -46 -30 -9 -.09 20 20 | 2733 -1247 3336 8673
gfz n/a| 0 0 4 25 60 83 .09 23 25 | 7364 -2900 3156 7390
grg n/a| -3 -1 4 21 40 108 -.47 46 40 | -476419 -2170 3332 624380
iac n/a| 0 0 0 14 18 -17 -.17 18 18 | 10591 -2027 3456 8028
mcc n/a| -8 1 -11 -94 -79 607 -.30 317 317 | --- --- --- ---
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 3.1884.0 GPS week: 1884 Day: 0 MJD: 57432
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac IGL | cod cof emx esx gfz grg iac IGL
------+----------------------------------------------+------------------------------------------
R01 | 2031 30 35 33 20 18 22 38 12 | 80 88 63 64 55 46 36 51
R02 | 732 22 28 12 20 10 26 33 10 | 80 83 72 78 62 44 43 63
R03 | 629 35 41 17 12 13 29 13 8 | 91 97 76 63 61 60 55 63
R04 | 701 40 40 23 8 22 22 13 9 | 92 98 77 65 52 52 57 62
R05 | 1020 44 53 20 28 27 54 24 14 | 82 96 65 73 46 54 52 58
R06 | 1414 30 27 18 11 21 25 17 8 | 74 69 61 63 49 47 48 55
R07 | 1217 40 40 47 14 24 24 20 12 | 86 84 86 54 42 44 43 53
R08 | 951 36 31 38 13 25 37 17 12 | 82 80 81 54 42 35 40 51
XR09E | 772 --- --- --- --- 60 --- 53 57 | --- --- --- --- 16 --- 29 34
R10E | 1682 32 35 21 15 16 40 20 10 | 66 72 68 75 71 93 71 72
R11E | 835 68 81 24 19 42 40 36 16 | 237 243 238 260 277 233 238 248
XR12E |13287 >>>> >>>> --- --- 345 --- 601 499 | 48 699 --- --- 9 --- 7 264
R13E | 3584 36 22 20 15 19 26 35 11 | 181 182 186 186 194 202 199 190
R14E | 1144 50 35 37 39 43 47 54 20 | 134 120 113 113 119 128 127 114
R15E | 4497 25 25 39 25 36 33 20 13 | 273 278 274 283 270 286 273 276
XR16E |12295 1798 1275 --- --- 15 1250 21 18 | 16 14 --- --- 11 6 2 12
XR17E | 3607 --- --- --- 205 152 --- 145 123 | --- --- --- 16 16 --- 14 46
R18 | 841 54 56 22 14 26 21 17 11 | 59 60 36 41 28 22 21 29
R19 | 879 51 51 18 11 20 36 19 10 | 59 62 38 39 30 25 25 31
R20 | 840 61 101 30 21 27 62 21 15 | 58 86 36 31 32 22 22 24
R21 | 676 39 21 31 12 30 27 12 11 | 52 50 34 40 36 22 27 29
R22 | 678 50 49 16 16 23 35 17 11 | 64 62 36 43 28 30 19 30
R23 | 628 23 22 21 17 8 29 13 8 | 23 25 35 43 30 25 25 28
R24 | 562 32 33 52 28 31 81 29 18 | 42 50 50 51 29 35 18 32
XR26 | ---- 60 156 --- --- --- --- 24 38 | 43 232 --- --- --- --- 48 36
------+----------------------------------------------+------------------------------------------
RMS | 1623 42 46 29 19 26 39 26 |T 87 127 86 82 66 71 61 78
WRMS | 1623 40 41 28 16 21 34 26 |NE 66 82 56 53 41 37 36 43
MEDI | 879 40 40 22 16 24 33 21 |MD 74 84 65 63 42 44 40 51
Table 3.1884.1 GPS week: 1884 Day: 1 MJD: 57433
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 | 1795 56 55 19 17 20 38 18 --- 11 | 70 73 57 48 46 35 38 --- 45
R02 | 709 24 26 21 11 19 19 21 --- 8 | 61 60 59 54 47 53 41 --- 50
R03 | 928 28 32 17 15 13 24 27 114 9 | 63 64 54 60 54 68 38 20 53
R04 | 730 31 43 20 13 12 24 22 --- 8 | 65 74 62 47 58 46 50 --- 52
R05 | 987 61 55 56 22 11 64 22 --- 17 | 58 55 77 55 53 44 36 --- 49
R06 | 1388 22 29 17 17 23 34 18 --- 9 | 54 61 46 50 36 47 30 --- 41
R07 | 2107 44 48 42 9 26 15 29 79 12 | 61 62 64 40 34 41 31 96 40
R08 | 674 38 41 33 19 14 34 25 --- 11 | 61 61 65 43 46 39 31 --- 43
XR09E | 1154 --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 23 --- 46
R10E | 2731 22 33 19 13 12 25 21 --- 8 | 51 53 42 43 45 37 43 --- 41
R11E | 4851 81 75 39 25 61 160 37 --- 28 | 143 110 142 128 136 197 114 --- 130
R13E | 4706 35 35 29 13 20 35 28 --- 11 | 72 74 87 68 70 81 65 --- 70
R14E | 1533 26 20 35 28 32 46 42 --- 15 | 104 111 101 112 120 93 103 --- 102
R15E | 8582 35 28 68 20 63 46 89 --- 26 | 193 183 217 182 201 182 116 --- 176
XR17E | 6360 --- --- --- --- 20 --- 15 --- 17 | --- --- --- --- 4 --- 1 --- 1
R18 | 1029 46 49 22 17 34 40 15 --- 12 | 42 43 29 26 25 19 15 --- 19
R19 | 822 48 48 19 13 22 36 15 --- 10 | 46 44 30 32 26 46 22 --- 26
R20 | 679 66 55 40 35 23 67 35 --- 18 | 48 63 44 58 55 21 16 --- 35
R21 | 605 36 56 19 15 28 27 16 210 10 | 31 51 19 22 23 13 16 100 16
R22 | 685 54 57 22 13 27 41 15 --- 12 | 40 44 23 25 23 19 16 --- 18
R23 | 810 24 22 16 27 17 51 14 --- 11 | 20 23 34 41 32 24 25 --- 26
R24 | 1006 21 40 37 31 35 60 36 --- 16 | 38 47 43 54 35 50 23 --- 35
XR26 | ---- 93 773 --- --- --- --- 49 --- 67 | 41 720 --- --- --- --- 65 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 2709 43 45 33 20 29 53 32 146 |T 64 98 64 59 55 57 41 72 50
WRMS | 2709 40 43 38 18 26 43 32 146 |NE 49 96 47 43 39 37 30 72 36
MEDI | 1006 36 43 22 17 22 36 22 114 |MD 58 61 54 48 46 44 31 96 41
Table 3.1884.2 GPS week: 1884 Day: 2 MJD: 57434
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 | 1623 77 91 21 28 19 40 16 --- 14 | 83 96 29 48 37 25 29 --- 32
R02 | 966 26 29 24 13 24 22 20 --- 9 | 61 65 60 51 34 38 44 --- 46
R03 | 1610 35 28 27 18 18 108 27 124 16 | 72 65 65 49 44 94 32 23 47
R04 | 1125 35 34 29 11 22 32 19 --- 10 | 70 68 68 46 40 46 37 --- 47
R05 | 758 41 60 29 18 32 25 25 --- 12 | 63 85 34 50 68 39 31 --- 41
R06 | 1208 30 33 17 18 26 25 20 --- 9 | 57 59 48 47 32 43 29 --- 38
R07 | 1229 53 52 19 18 32 25 21 122 12 | 72 70 44 45 34 25 27 47 35
R08 | 676 46 44 32 21 31 30 18 --- 12 | 69 68 62 53 26 26 33 --- 40
XR09E | 2052 71 78 32 --- --- --- --- --- 47 | 25 35 44 --- --- --- --- --- 119
R10E | 1973 30 35 23 19 12 35 20 --- 9 | 46 54 46 49 46 53 47 --- 44
R11E | 4643 56 42 34 34 28 56 21 --- 15 | 109 108 123 133 132 163 115 --- 124
R13E | 2568 38 46 20 17 23 35 25 --- 11 | 98 98 109 107 114 108 98 --- 104
R14E | 1709 27 27 21 24 30 41 35 --- 13 | 103 105 97 95 113 114 89 --- 95
R15E | 8358 24 16 32 21 37 28 19 --- 12 | 137 144 172 142 150 143 138 --- 146
XR17E | ---- --- --- --- --- --- --- --- --- 0 | 28 57 --- --- --- --- 1 --- 0
R18 | 745 36 35 14 25 19 41 14 --- 10 | 42 42 28 45 26 25 21 --- 27
R19 | 652 44 56 31 22 29 95 21 --- 16 | 47 56 45 44 28 77 21 --- 29
R20 | 893 40 21 28 16 19 53 15 --- 11 | 29 38 29 33 36 29 21 --- 24
R21 | 685 58 56 22 10 19 42 21 259 12 | 50 51 26 24 30 17 24 70 21
R22 | 607 52 56 16 20 27 41 18 --- 11 | 54 57 34 39 22 19 17 --- 24
R23 | 1059 18 20 18 25 15 39 19 --- 9 | 18 18 22 42 22 19 31 --- 24
R24 | 2140 24 42 49 44 42 117 20 --- 21 | 36 64 55 74 33 51 28 --- 40
XR26 | ---- 48 1465 --- --- --- --- 14 --- 27 | 38 9999 --- --- --- --- 56 --- 45
------+---------------------------------------------------+-----------------------------------------------
RMS | 2495 42 45 27 22 26 54 21 180 |T 61 68 59 60 53 57 44 46 54
WRMS | 2495 42 44 25 20 24 40 21 180 |NE 53 60 43 46 34 38 30 46 35
MEDI | 1208 38 42 24 19 24 39 20 124 |MD 57 64 46 48 34 39 31 47 40
Table 3.1884.3 GPS week: 1884 Day: 3 MJD: 57435
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 | 1025 79 102 36 22 33 36 16 --- 15 | 91 110 54 37 32 30 25 --- 31
R02 | 774 30 35 25 15 13 31 8 --- 8 | 63 68 56 41 35 20 38 --- 39
R03 | 1077 31 48 31 21 25 40 14 133 11 | 74 88 68 62 48 28 39 42 50
R04 | 594 29 32 21 18 16 35 12 --- 9 | 70 72 62 65 48 38 47 --- 53
R05 | 1086 42 54 22 23 19 31 20 --- 10 | 71 85 61 52 39 41 38 --- 44
R06 | 1548 27 39 14 18 16 19 14 --- 7 | 64 74 49 49 53 46 36 --- 45
R07 | 1067 50 56 18 12 20 34 16 184 10 | 86 95 54 57 43 32 49 118 49
R08 | 893 52 61 29 21 30 27 19 --- 12 | 83 87 61 50 37 33 37 --- 42
XR09E | 2470 229 232 264 --- --- --- 61 --- 119 | 19 22 58 --- --- --- 66 --- 122
R10E | 1493 29 31 23 18 15 28 17 --- 9 | 68 73 81 70 77 75 72 --- 72
R11E | 4187 55 51 36 16 33 38 20 --- 13 | 96 100 99 125 127 152 119 --- 117
R13E | 1019 35 27 21 14 21 39 15 --- 9 | 122 125 118 129 136 131 129 --- 127
R14E | 2762 24 36 38 28 43 35 37 --- 16 | 137 143 137 129 147 132 142 --- 134
R15E | 5430 21 29 20 18 33 26 16 --- 10 | 125 126 130 130 133 145 125 --- 129
XR17E | 1228 137 144 123 --- --- --- 109 --- 83 | 39 48 28 --- --- --- 1 --- 1
R18 | 801 32 35 18 17 15 49 16 --- 10 | 50 52 37 44 44 22 29 --- 34
R19 | 546 45 42 27 14 15 36 20 --- 10 | 59 56 47 36 27 29 20 --- 29
R20 | 820 41 52 27 25 21 51 28 --- 13 | 41 60 47 41 40 40 20 --- 29
R21 | 692 53 50 17 13 18 40 14 337 10 | 55 53 28 31 27 39 22 190 26
R22 | 560 54 51 17 18 14 49 14 --- 11 | 57 55 36 43 33 27 21 --- 30
R23 | 786 16 20 24 22 12 29 12 --- 8 | 20 21 27 41 25 18 27 --- 25
R24 | 2944 20 24 45 27 36 53 22 --- 15 | 53 46 78 60 42 30 29 --- 45
XR26 | ---- 133 1155 --- --- --- --- 37 --- 70 | 82 9999 --- --- --- --- 87 --- 68
------+---------------------------------------------------+-----------------------------------------------
RMS | 1978 41 47 27 19 24 37 19 235 |T 70 75 64 64 59 55 52 116 58
WRMS | 1978 39 42 28 19 18 33 19 235 |NE 63 68 51 47 38 31 35 116 39
MEDI | 1025 41 48 24 18 19 35 16 184 |MD 68 72 56 50 42 33 38 118 45
Table 3.1884.4 GPS week: 1884 Day: 4 MJD: 57436
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 | 1360 71 51 19 13 30 37 11 --- 12 | 81 64 42 42 31 34 35 --- 35
R02 | 815 35 36 21 13 24 33 10 --- 9 | 55 53 41 34 23 27 26 --- 28
R03 | 981 54 52 29 16 16 43 13 87 11 | 64 58 46 28 24 34 26 70 26
R04 | 1515 38 38 28 12 14 48 12 --- 10 | 67 65 58 40 36 44 37 --- 40
R05 | 1700 30 20 34 25 23 69 18 --- 14 | 54 46 41 62 39 52 42 --- 45
R06 | 1277 23 20 22 12 17 19 13 --- 7 | 56 53 46 42 45 52 31 --- 40
R07 | 1214 52 58 31 9 21 34 14 195 10 | 75 78 57 32 42 26 30 110 37
R08 | 1149 54 55 18 19 23 30 16 --- 10 | 71 74 43 47 27 26 32 --- 36
XR09E | 2111 170 178 196 --- --- --- 152 --- 120 | 22 27 36 --- --- --- 60 --- 66
R10E | 1713 27 38 17 17 27 37 11 --- 9 | 58 62 60 56 61 76 60 --- 57
R11E | 2022 62 77 47 15 38 36 26 --- 15 | 86 92 76 91 103 91 95 --- 87
R13 | 1422 50 33 37 24 31 37 49 --- 17 | 134 139 138 133 133 144 78 --- 117
R14E | 3712 29 23 26 21 26 37 24 --- 11 | 106 97 95 94 98 107 100 --- 96
R15E | 1671 29 32 24 16 38 25 24 --- 11 | 144 142 142 142 147 152 127 --- 138
XR17E | 1736 146 149 130 --- --- --- 107 --- 85 | 31 37 50 --- --- --- 1 --- 1
R18 | 692 30 33 31 12 12 54 12 --- 10 | 43 46 43 34 31 21 24 --- 28
R19 | 1081 38 46 40 21 16 50 20 --- 13 | 52 59 41 46 37 38 24 --- 31
R20 | 603 42 30 28 30 27 41 23 --- 13 | 46 45 27 47 35 28 23 --- 28
R21 | 703 49 49 20 13 31 21 10 83 9 | 50 53 29 30 24 31 24 102 24
R22 | 587 61 59 17 12 25 49 10 --- 11 | 49 50 23 19 22 26 16 --- 17
R23 | 709 17 17 13 18 24 18 15 --- 8 | 17 21 21 29 21 21 18 --- 18
R24 | 2341 37 40 48 17 42 38 36 --- 15 | 46 54 54 37 33 32 16 --- 26
XR26 | ---- 224 731 --- --- --- --- 58 --- 114 | 41 611 --- --- --- --- 244 --- 192
------+---------------------------------------------------+-----------------------------------------------
RMS | 1542 44 43 29 18 26 40 21 132 |T 62 88 54 54 50 53 50 94 52
WRMS | 1542 42 43 28 16 24 37 21 132 |NE 54 89 40 37 31 32 40 94 40
MEDI | 1277 42 40 28 16 24 37 16 87 |MD 55 58 43 42 35 34 31 102 36
Table 3.1884.5 GPS week: 1884 Day: 5 MJD: 57437
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 | 706 61 72 9 14 23 40 16 --- 11 | 55 68 28 41 34 30 23 --- 28
R02 | 708 34 38 15 15 26 29 11 --- 9 | 47 52 33 36 20 19 27 --- 26
R03 | 735 54 61 29 9 28 29 15 58 11 | 57 62 40 30 25 21 23 30 24
R04 | 2324 44 46 27 17 16 34 22 --- 11 | 56 61 42 37 39 28 22 --- 31
R05 | 1907 29 35 41 23 18 84 19 --- 15 | 42 52 37 43 39 23 30 --- 31
R06 | 1027 13 15 15 21 15 27 20 --- 8 | 39 39 38 50 37 39 26 --- 36
R07 | 1306 46 50 33 12 20 39 22 370 11 | 55 58 47 34 22 32 16 57 27
R08 | 954 47 50 13 17 21 43 18 --- 10 | 56 61 30 39 47 19 26 --- 30
XR09 | 1576 271 266 290 --- --- --- 80 --- 148 | 26 26 33 --- --- --- 75 --- 85
R10E | 993 27 28 26 18 15 35 26 --- 10 | 70 81 73 74 72 82 85 --- 74
R11 | 707 79 88 24 13 36 33 17 --- 14 | 94 95 104 94 108 120 93 --- 97
R13 | 1881 17 21 26 18 17 32 10 --- 8 | 103 97 97 92 99 94 92 --- 93
R14 | 3225 31 43 44 27 28 41 44 --- 16 | 129 125 139 121 113 135 115 --- 118
R15 | 3511 38 34 22 19 34 28 20 --- 11 | 90 92 85 88 99 96 88 --- 87
XR17E | 1549 126 127 129 --- --- --- 122 --- 88 | 29 33 29 --- --- --- 1 --- 1
R18 | 634 41 42 30 13 24 50 9 --- 11 | 36 37 27 25 25 22 21 --- 19
R19 | 961 40 44 20 20 14 40 18 --- 10 | 42 45 29 40 35 26 23 --- 29
R20 | 574 31 51 49 26 15 69 16 --- 15 | 48 63 39 46 40 19 29 --- 33
R21 | 602 47 47 26 26 19 28 21 73 11 | 52 53 33 43 30 26 17 49 27
R22 | 625 57 54 17 24 19 37 26 --- 12 | 52 50 31 41 22 20 14 --- 23
R23 | 1371 17 20 17 24 17 26 16 --- 8 | 25 26 26 29 24 29 12 --- 17
R24 | 1788 41 59 46 15 20 38 26 --- 13 | 39 57 34 30 33 28 17 --- 23
XR26 | ---- 37 222 --- --- --- --- 10 --- 20 | 38 279 --- --- --- --- 51 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 1573 43 48 29 19 22 41 21 220 |T 55 70 48 51 48 45 40 45 43
WRMS | 1573 42 45 26 19 17 40 21 220 |NE 46 66 34 37 31 25 23 45 27
MEDI | 993 41 47 26 18 19 35 19 73 |MD 52 58 34 41 35 28 26 49 30
Table 3.1884.6 GPS week: 1884 Day: 6 MJD: 57438
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 | 1047 68 64 26 12 15 30 14 --- 11 | 93 89 48 41 28 40 33 --- 36
R02 | 898 33 28 20 15 16 35 16 --- 9 | 74 71 57 50 37 31 35 --- 43
R03 | 885 41 47 15 23 35 37 15 62 11 | 83 88 60 56 41 34 37 40 45
R04 | 1529 47 50 20 9 25 27 9 --- 9 | 86 87 57 49 39 42 38 --- 45
R05 | 1559 49 56 40 22 18 87 19 --- 15 | 73 85 46 57 38 42 39 --- 43
R06 | 871 16 27 28 16 23 36 15 --- 9 | 65 73 61 61 43 49 39 --- 50
R07 | 1216 44 40 21 19 23 25 22 539 10 | 87 86 68 56 39 33 32 92 47
R08 | 925 41 44 24 17 20 35 16 --- 10 | 87 89 66 53 34 28 40 --- 47
XR09 | 2364 289 302 361 --- --- --- 77 --- 150 | 33 48 47 --- --- --- 110 --- 119
R10 | 1237 22 21 30 17 16 24 11 --- 8 | 59 56 71 56 57 71 57 --- 58
R11 | 1152 82 70 36 9 25 39 19 --- 14 | 94 86 96 99 111 101 103 --- 99
R13 | 1675 23 22 25 14 17 24 11 --- 8 | 75 68 66 69 66 67 69 --- 67
R14 | 3138 28 32 43 27 23 47 30 --- 14 | 139 146 130 139 154 135 139 --- 137
R15 | 3825 27 35 20 24 31 39 22 --- 11 | 124 115 132 124 130 141 126 --- 127
XR17E | 1004 144 143 134 --- --- --- 109 --- 86 | 27 23 30 --- --- --- 1 --- 1
R18 | 669 37 39 10 19 22 44 11 --- 9 | 60 62 49 45 28 22 28 --- 35
R19 | 987 43 38 16 9 24 43 8 --- 9 | 62 59 37 38 19 28 25 --- 29
R20 | 963 46 45 84 23 16 50 25 --- 18 | 59 63 42 45 33 26 21 --- 32
R21 | 872 41 43 19 23 15 56 21 84 12 | 60 60 41 46 26 26 24 33 32
R22 | 538 55 65 27 18 22 33 22 --- 12 | 64 71 45 37 19 17 16 --- 27
R23 | 1294 18 17 20 32 29 85 10 --- 14 | 24 28 23 49 25 27 24 --- 26
R24 | 755 33 21 47 26 27 61 16 --- 14 | 40 35 35 40 27 21 19 --- 24
XR26 | ---- 76 108 --- --- --- --- 21 --- 39 | 64 164 --- --- --- --- 36 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1522 43 43 32 20 23 46 18 317 |T 70 76 59 60 49 49 47 55 52
WRMS | 1522 43 42 37 20 25 40 18 317 |NE 67 75 49 48 31 31 30 55 36
MEDI | 1004 41 43 25 18 22 37 16 84 |MD 65 71 49 50 37 33 36 40 43
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