[IGSREPORT-22539] Wk 1779 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Sat Mar 1 12:47:30 PST 2014
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1779 (Feb 09, 2014 - Feb 15, 2014)
Contact: J. Griffiths (jake.griffiths at noaa.gov)
K. Choi (kevin.choi at noaa.gov)
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 2.1779.
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:
igl1779[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1779 in the SP3 format.
igl17797.sum Combination Report for GPS Week 1779.
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 | 182.7 ns
1 | 183.2 ns
2 | 179.8 ns
3 | 181.2 ns
4 | 179.2 ns
5 | 179.5 ns
6 | 180.6 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 1.1779, 1a.1779).
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 2.1779.0-6)
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 3.1779.0-6).
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 1779 summary. (Feb 09, 2014 - Feb 15, 2014)
Table 1.1779.a GPS week : 1779 MJD: 56697.0-56703.0
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 10 -2 7 27 .41 29 23 | --- --- --- ---
| 1 1 3 16 16 18 .04 | --- ---
cof n/a| 0 0 7 -18 19 22 .40 32 25 | --- --- --- ---
| 2 1 2 18 28 37 .04 | --- ---
emx n/a| 0 0 -4 -78 -54 -16 -.38 31 31 | 181198 -959 3790 6656
| 1 0 2 26 32 45 .05 | 1441 1175
esx n/a| -2 -1 0 10 -19 -30 .05 21 17 | 179001 -2020 3784 6748
| 1 2 1 20 16 32 .04 | 5708 2300
gfz n/a| -1 0 -2 28 10 25 .16 21 16 | 0 -2033 3791 6706
| 1 0 2 25 14 18 .04 | 0 1969
grg n/a| 0 1 0 -50 -6 50 -.40 35 30 | -876533 -2015 5360 73983
| 1 2 5 29 9 41 .10 | 60761 1699
iac n/a| 2 0 -3 39 37 -31 -.11 27 27 | 182476 -780 3795 7118
| 1 0 6 36 28 84 .06 | 1482 1264
mcc n/a| 6 2 79 46 114 684 -.65 187 187 | --- --- --- ---
| 8 16 17 190 150 252 .41 | --- ---
Table 1.1779.b GPS week : 1779 MJD: 56697.0-56703.0
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 | 16 13 10 10 13 11 12 |
R02 | 11 10 7 8 10 8 7 |
R03 | 10 10 12 11 10 8 10 |
R04 | 8 6 10 10 9 10 10 |
R05 | 10 6 9 9 11 9 10 |
R06 | 10 7 7 8 9 9 9 |
R07 | 9 9 7 8 7 8 9 |
R08 | 11 9 10 9 10 11 12 |
R09 | 19 18 18 16 18 21 21 |
R10 | 9 9 7 9 8 9 9 |
R11 | 18 18 18 18 18 17 18 |
R12 | 14 15 18 15 19 20 18 |
R13 | 13 14 14 11 11 13 13 |
R14 | 17 20 18 15 16 16 24 |
R15 | 10 10 9 9 9 9 12 |
R16 | 13 10 10 12 10 10 11 |
R17 | 10 10 10 7 8 8 9 |
R18 | 9 9 9 0 --- --- --- |
R19 | 10 10 9 8 8 10 10 |
R20 | 13 13 14 12 11 12 16 |
R21 | 16 16 17 14 13 14 17 |
R22 | 8 7 9 8 8 10 13 |
R23 | 6 9 7 9 7 7 9 |
R24 | 9 8 6 8 9 10 9 |
Table 1.1779.c GPS week : 1779 MJD: 56697.0-56703.0
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 1779 0 | 21 33 211 -138 -935 71 85.7 1593 1593 | 182740 0
brd 1779 1 | -17 -66 66 1108 570 1205 87.9 1785 1785 | 183157 0
brd 1779 2 | 4 -68 59 -1584 1123 466 85.4 1717 1717 | 179769 0
brd 1779 3 | 47 33 33 -1673 1633 -355 85.0 1527 1527 | 181246 0
brd 1779 4 | 7 45 -44 -560 1714 -3279 83.5 1571 1571 | 179249 0
brd 1779 5 | -58 -53 98 -157 -441 -6289 84.2 1649 1649 | 179541 0
brd 1779 6 | 15 -37 169 -25 637 -7284 83.7 1566 1566 | 180584 0
-------------+------------------------------------------------------------+----------------
brd 1779 mean| 2 -16 84 -432 614 -2209 85.0 1629 1629 | 180898 0
brd 1779 sdev| 33 51 85 964 1002 3439 1.5 92 92 | 1557 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 2.1779.0 GPS week: 1779 Day: 0 MJD: 56697
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 -1 7 6 30 4 .46 28 23 | --- --- --- ---
cof n/a| -2 0 5 -3 16 -25 .38 30 25 | --- --- --- ---
emx n/a| 0 0 -2 -97 -98 -31 -.36 33 32 | 183032 -166 3998 6940
esx n/a| -3 -1 0 23 -22 -81 .07 22 19 | 188720 -414 3984 6730
gfz n/a| 0 0 -5 -9 21 39 .14 20 14 | 0 -293 3979 6969
grg n/a| 0 -2 10 -16 -2 24 -.53 33 33 | -844808 -610 4013 40555
iac n/a| 4 1 -10 75 52 86 -.10 27 27 | 183924 -58 3979 7433
mcc n/a| -2 12 87 33 271 791 -.44 96 96 | --- --- --- ---
Table 2.1779.1 GPS week: 1779 Day: 1 MJD: 56698
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 15 -9 -14 16 .46 28 23 | --- --- --- ---
cof n/a| 0 1 7 -22 -25 32 .37 32 26 | --- --- --- ---
emx n/a| 2 0 -5 -74 -80 60 -.34 33 35 | 183070 -305 3560 6625
esx n/a| -3 -2 0 -33 -13 -25 .03 21 16 | 177656 -1292 3564 6969
gfz n/a| 0 -1 -2 18 24 51 .22 21 16 | 0 164 3560 6569
grg n/a| 0 0 0 -51 8 5 -.53 37 30 | -841443 82 3579 37128
iac n/a| 2 1 -6 65 29 -44 -.15 22 22 | 184930 345 3562 6837
mcc n/a| 4 -11 80 258 -17 1094 -.12 130 130 | --- --- --- ---
Table 2.1779.2 GPS week: 1779 Day: 2 MJD: 56699
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 3 -17 -5 57 .41 26 19 | --- --- --- ---
cof n/a| -1 -1 4 -12 46 26 .41 29 24 | --- --- --- ---
emx n/a| 3 0 -5 -34 -20 -37 -.46 36 40 | 181370 -3112 3443 6178
esx n/a| -1 -3 -1 25 -18 -26 -.02 21 17 | 181513 -7066 3426 6434
gfz n/a| -2 0 -2 26 18 26 .18 19 15 | 0 -5232 3436 6230
grg n/a| 3 4 -1 -63 0 65 -.40 36 31 | -999999 -4980 14197 302405
iac n/a| 2 0 3 -12 22 -53 -.17 26 26 | 182358 -2574 3436 6707
mcc n/a| -1 -4 88 101 -101 770 -.95 161 161 | --- --- --- ---
Table 2.1779.3 GPS week: 1779 Day: 3 MJD: 56700
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 10 -21 3 38 .39 23 20 | --- --- --- ---
cof n/a| -1 1 8 -35 43 65 .37 24 20 | --- --- --- ---
emx n/a| 0 1 0 -61 -39 29 -.40 28 29 | 181184 -404 3994 5930
esx n/a| -1 -4 0 19 7 -48 .05 18 15 | 177019 -1272 3984 5988
gfz n/a| -1 0 -3 41 -16 30 .15 21 16 | 0 -545 3984 6052
grg n/a| 1 2 -2 -81 -17 82 -.37 35 31 | -839103 -1450 4000 29154
iac n/a| 1 0 -5 6 39 -108 -.18 27 27 | 182014 -1109 3980 6607
mcc n/a| 13 -2 102 258 183 782 -.51 210 210 | --- --- --- ---
Table 2.1779.4 GPS week: 1779 Day: 4 MJD: 56701
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 14 -11 5 31 .45 29 23 | --- --- --- ---
cof n/a| 1 -2 7 -44 0 26 .43 38 25 | --- --- --- ---
emx n/a| 0 -1 -3 -114 -85 -16 -.40 24 23 | 179280 -643 4026 7329
esx n/a| -1 0 1 15 -30 -3 .08 20 17 | 171797 -1381 4020 7254
gfz n/a| -3 0 -2 63 5 25 .09 23 16 | 0 -3124 4083 7381
grg n/a| 0 3 -5 -70 -6 -5 -.28 35 29 | -830257 -2265 4026 32892
iac n/a| 4 0 -8 48 92 -44 -.02 26 26 | 182072 -1763 4078 7711
mcc n/a| 14 -13 85 22 307 504 -.96 228 228 | --- --- --- ---
Table 2.1779.5 GPS week: 1779 Day: 5 MJD: 56702
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 11 6 2 34 .36 35 27 | --- --- --- ---
cof n/a| 4 2 13 -19 47 59 .35 39 32 | --- --- --- ---
emx n/a| -2 0 -7 -72 -19 -48 -.33 30 27 | 180311 -2089 3944 7411
esx n/a| 0 -3 0 16 -16 18 .08 20 19 | 173929 -2180 3951 7677
gfz n/a| -1 0 2 48 16 14 .20 18 15 | 0 -3353 3960 7480
grg n/a| 1 0 0 -67 -17 78 -.38 34 29 | -909572 -3283 4100 43702
iac n/a| 0 1 -5 11 2 -132 -.09 27 27 | 180557 -1320 3959 7802
mcc n/a| 2 1 65 -62 41 521 -1.24 255 255 | --- --- --- ---
Table 2.1779.6 GPS week: 1779 Day: 6 MJD: 56703
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 10 26 29 8 .37 34 26 | --- --- --- ---
cof n/a| -1 1 7 10 6 -28 .45 33 27 | --- --- --- ---
emx n/a| 0 0 -6 -93 -35 -69 -.37 34 29 | 180144 0 3565 6185
esx n/a| -2 1 -3 8 -45 -49 .04 24 20 | 182373 -536 3560 6185
gfz n/a| 0 0 -4 7 4 -6 .16 23 18 | 0 -1854 3541 6264
grg n/a| 1 0 0 -2 -8 102 -.30 33 28 | -870549 -1604 3607 32045
iac n/a| 3 0 6 78 26 78 -.07 31 31 | 181481 1016 3572 6735
mcc n/a| 16 32 47 -287 116 326 -.30 232 232 | --- --- --- ---
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 3.1779.0 GPS week: 1779 Day: 0 MJD: 56697
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 | 1014 23 26 41 38 15 56 38 --- 15 | 97 110 116 126 101 70 81 --- 98
R02 | 769 23 26 24 25 15 36 29 --- 11 | 70 74 95 89 75 66 56 --- 73
R03 | 984 23 21 16 19 19 29 21 --- 9 | 69 69 84 83 84 64 73 --- 76
R04 | 724 18 14 23 10 17 21 14 --- 7 | 68 67 76 64 69 56 59 --- 64
R05 | 917 23 25 22 15 24 28 10 72 9 | 71 75 88 74 88 64 73 17 76
R06 | 1955 19 11 27 21 18 29 18 --- 9 | 63 70 96 69 81 63 77 --- 72
R07 | 2192 12 13 16 12 18 27 24 88 8 | 79 87 95 88 97 79 77 29 86
XR08 | 588 12 8 26 21 12 --- 31 --- 10 | 73 77 92 88 81 --- 69 --- 80
R09E | 1850 54 53 68 29 32 39 25 --- 18 | 44 42 65 73 70 55 61 --- 56
R10E | 3026 17 20 22 13 17 13 36 --- 9 | 58 55 58 46 49 51 37 --- 47
R11E | 1254 49 41 52 22 35 50 38 --- 18 | 121 121 123 124 141 135 111 --- 123
R12E | 1024 33 40 39 22 17 47 24 --- 13 | 39 39 44 56 52 75 47 --- 47
R13E | 1347 19 30 45 20 25 41 29 --- 13 | 29 39 28 39 48 46 32 --- 32
R14E | 1146 28 26 40 41 25 56 33 --- 16 | 105 110 88 120 111 100 109 --- 103
R15E | 3160 21 24 22 18 14 24 33 --- 9 | 25 32 22 28 30 37 20 --- 22
R16E | 2890 26 29 26 21 25 30 44 --- 13 | 24 25 44 31 33 33 25 --- 24
R17 | 1022 33 41 24 17 16 15 23 49 9 | 23 32 31 23 24 18 23 24 14
R18 | 1002 27 28 18 15 13 20 22 146 8 | 11 16 14 15 23 13 19 50 17
R19 | 874 27 32 27 22 18 14 23 --- 10 | 36 37 30 35 29 24 21 --- 24
R20 | 1729 23 27 40 21 27 34 34 --- 13 | 33 36 44 37 37 32 31 --- 24
R21 | 877 38 36 50 34 23 42 26 --- 15 | 27 42 39 63 59 50 44 --- 42
R22 | 1208 23 25 22 15 14 14 17 --- 8 | 24 27 31 23 22 22 24 --- 18
R23 | 805 13 28 14 9 6 20 11 --- 5 | 18 29 17 13 15 22 15 --- 10
R24 | 626 26 35 20 13 12 15 28 --- 8 | 20 32 29 23 28 24 22 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS | 1592 28 30 33 22 20 33 27 96 |T 51 55 60 59 60 52 50 30 51
WRMS | 1592 23 25 32 19 14 33 27 96 |NE 48 55 61 57 57 44 47 30 49
MEDI | 1022 23 26 24 20 17 29 25 72 |MD 39 42 44 56 52 51 44 24 47
Table 3.1779.1 GPS week: 1779 Day: 1 MJD: 56698
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 | 1449 29 25 42 16 18 60 16 --- 13 | 62 71 81 71 71 54 63 --- 64
R02 | 554 14 14 23 10 21 40 21 --- 9 | 52 53 64 53 69 38 45 --- 53
R03 | 1361 34 21 20 22 17 29 13 --- 10 | 46 58 72 84 77 56 73 --- 69
R04 | 883 12 13 12 9 16 16 14 --- 6 | 44 49 44 48 50 52 48 --- 45
R05 | 869 12 20 23 12 10 15 11 83 6 | 42 40 52 49 43 47 47 22 45
R06 | 1090 13 17 17 10 15 20 15 --- 6 | 40 39 53 48 51 63 50 --- 47
R07 | 3038 18 26 21 16 17 33 20 124 9 | 57 58 67 46 60 50 52 32 52
XR08 | 1056 21 17 19 19 14 --- 20 --- 9 | 51 59 64 56 56 --- 64 --- 56
R09E | 3306 46 32 47 28 41 62 24 --- 17 | 33 46 42 72 81 52 55 --- 51
R10E | 4472 20 20 23 12 17 27 19 --- 8 | 46 47 47 38 46 41 35 --- 38
R11E | 952 36 34 43 34 26 74 35 --- 18 | 108 109 93 138 126 131 111 --- 116
R12E | 907 35 36 38 22 35 38 30 --- 14 | 37 54 40 54 60 65 48 --- 44
R13E | 1623 29 30 33 20 30 43 32 --- 13 | 44 56 28 51 47 58 31 --- 37
R14E | 914 33 37 68 44 37 53 31 --- 19 | 166 173 126 171 161 152 170 --- 157
R15E | 1668 33 42 25 16 17 22 25 219 10 | 30 36 19 20 25 27 28 50 17
R16E | 2277 19 17 16 12 16 34 30 --- 9 | 22 27 24 30 28 41 21 --- 21
R17 | 808 30 53 23 21 18 28 21 72 10 | 19 36 23 37 31 44 23 20 22
R18 | 1351 29 40 18 22 12 18 22 97 9 | 14 30 23 18 24 30 20 51 21
R19 | 1002 23 20 30 17 14 19 26 --- 9 | 39 45 55 46 43 39 27 --- 37
R20 | 2263 27 27 54 21 17 29 26 --- 13 | 21 20 56 26 28 25 31 --- 22
R21 | 1310 53 69 47 33 25 42 17 --- 16 | 29 36 47 69 59 58 39 --- 47
R22 | 1059 18 26 19 12 13 19 17 --- 7 | 23 33 27 22 24 23 22 --- 18
R23 | 938 18 17 27 15 9 43 9 --- 9 | 20 25 25 23 15 42 13 --- 15
R24 | 789 28 24 22 12 10 16 18 --- 8 | 21 26 27 21 19 15 16 --- 15
------+---------------------------------------------------+-----------------------------------------------
RMS | 1785 28 32 33 21 21 37 22 130 |T 44 51 49 53 53 52 47 35 46
WRMS | 1785 23 26 35 16 16 30 22 130 |NE 36 42 48 44 45 42 39 31 39
MEDI | 1059 27 25 23 16 17 29 20 97 |MD 39 45 47 48 47 47 39 32 44
Table 3.1779.2 GPS week: 1779 Day: 2 MJD: 56699
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 | 2416 23 27 23 31 10 31 16 --- 10 | 71 78 63 62 69 79 73 --- 66
R02 | 637 11 16 33 11 12 13 18 --- 7 | 54 52 71 51 58 57 38 --- 52
R03 | 752 21 27 48 22 13 28 35 --- 12 | 54 52 88 62 48 41 30 --- 49
R04 | 1239 13 11 23 14 15 32 34 --- 9 | 58 52 65 61 52 38 32 --- 49
R05 | 994 10 10 26 19 15 26 22 81 8 | 56 55 67 43 60 41 55 31 52
R06 | 1237 9 12 20 15 12 22 19 --- 7 | 50 53 61 53 63 41 51 --- 53
R07 | 1104 9 18 21 9 10 26 20 194 6 | 65 68 69 65 53 75 50 96 59
XR08 | 1146 14 13 28 26 11 --- 20 --- 10 | 61 58 69 46 59 --- 52 --- 54
R09E | 3045 40 37 61 32 24 65 33 --- 18 | 40 45 56 61 59 60 56 --- 48
R10E | 4728 19 27 15 11 15 15 17 --- 7 | 33 32 32 35 31 36 29 --- 29
R11E | 806 33 27 59 25 32 69 33 --- 18 | 90 105 90 122 129 106 110 --- 107
R12E | 1234 42 27 57 19 34 64 30 --- 17 | 37 43 38 67 77 82 45 --- 51
R13E | 1098 23 23 35 18 35 53 26 --- 14 | 27 34 23 37 46 50 31 --- 27
R14E | 848 43 46 34 43 24 51 40 --- 17 | 154 107 113 112 135 155 104 --- 124
R15E | 1448 17 29 18 18 13 23 26 223 8 | 28 43 20 35 37 36 25 77 26
R16E | 1502 18 15 23 17 16 32 26 --- 9 | 25 21 23 20 30 33 29 --- 19
R17 | 799 25 28 27 21 12 25 30 102 10 | 19 35 34 32 24 37 24 19 18
XR18 | 9685 19 15 18 --- 13 18 24 144 9 | 17 18 20 --- 24 20 24 84 18
R19 | 742 17 27 19 20 15 15 26 --- 8 | 20 27 21 20 23 16 21 --- 12
R20 | 2300 31 44 61 21 16 36 23 --- 13 | 25 39 48 36 28 31 30 --- 23
R21 | 1963 59 59 48 30 28 27 32 --- 17 | 26 37 40 61 55 51 39 --- 39
R22 | 906 20 30 35 17 18 21 17 --- 9 | 23 27 22 17 30 24 20 --- 16
R23 | 906 10 19 25 15 13 15 10 --- 6 | 21 28 18 14 29 19 21 --- 17
R24 | 829 17 27 18 11 12 15 8 --- 6 | 24 30 17 15 22 16 21 --- 17
------+---------------------------------------------------+-----------------------------------------------
RMS | 1716 26 29 36 21 19 36 26 161 |T 44 47 48 49 51 49 42 61 42
WRMS | 1716 19 24 40 17 15 31 26 161 |NE 40 44 48 42 43 39 36 57 37
MEDI | 1104 19 27 26 19 15 26 24 144 |MD 33 43 40 46 48 41 31 77 39
Table 3.1779.3 GPS week: 1779 Day: 3 MJD: 56700
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 | 1509 31 23 18 25 19 21 13 --- 10 | 83 81 87 78 88 98 77 --- 81
R02 | 510 13 15 27 16 10 31 11 --- 8 | 55 63 74 57 63 48 53 --- 56
R03 | 802 22 23 35 20 18 28 17 --- 10 | 63 68 93 61 80 59 74 --- 69
R04 | 1020 12 14 23 14 15 47 19 --- 9 | 62 75 77 75 77 47 68 --- 67
R05 | 1080 18 16 26 14 12 23 24 78 8 | 62 56 84 75 73 60 51 52 67
R06 | 1042 10 8 32 9 14 20 15 --- 7 | 54 56 77 56 57 50 59 --- 57
R07 | 761 11 12 16 14 14 24 26 104 7 | 71 73 73 75 80 88 63 101 73
XR08 | 603 18 22 20 11 13 --- 22 --- 8 | 64 69 66 63 73 --- 53 --- 63
R09E | 3086 31 31 36 23 37 48 42 --- 15 | 48 50 54 68 67 64 63 --- 55
R10E | 4254 12 18 26 12 16 22 26 --- 8 | 30 33 25 34 35 31 29 --- 26
R11E | 753 34 31 36 31 25 72 53 417 18 | 112 117 124 139 138 142 92 157 121
R12E | 1142 26 31 39 21 32 57 32 --- 15 | 34 41 34 63 64 70 38 --- 43
R13E | 1359 14 19 34 20 20 42 24 --- 11 | 30 35 39 40 45 42 38 --- 31
R14E | 673 24 26 34 27 28 39 47 --- 14 | 215 237 206 227 229 198 222 --- 216
R15E | 1384 19 32 17 19 20 16 19 133 8 | 25 28 26 39 31 30 29 85 26
R16E | 953 23 30 30 14 23 35 36 --- 11 | 32 45 29 30 35 33 29 --- 23
R17 | 678 14 18 20 14 13 15 16 110 7 | 21 26 26 24 22 34 20 30 20
XR18 | ---- --- --- --- --- --- --- 8 60 0 | --- --- --- --- --- --- 30 124 32
R19 | 704 20 17 18 14 14 27 15 --- 8 | 28 28 30 32 32 26 19 --- 22
R20 | 1717 26 26 40 18 24 34 21 --- 12 | 26 29 20 36 43 40 26 --- 24
R21 | 2008 49 47 31 21 19 32 31 --- 14 | 25 34 41 55 48 44 49 --- 38
R22 | 707 17 15 21 14 16 17 15 --- 7 | 20 24 20 31 34 25 31 --- 23
R23 | 756 24 24 18 13 24 23 22 --- 9 | 28 28 21 22 32 29 22 --- 18
R24 | 774 20 21 21 8 17 20 16 --- 7 | 28 29 28 22 25 23 20 --- 18
------+---------------------------------------------------+-----------------------------------------------
RMS | 1527 23 24 28 18 21 35 27 210 |T 52 57 58 60 63 58 52 91 52
WRMS | 1527 20 20 29 15 16 31 27 210 |NE 46 49 54 50 55 47 44 76 45
MEDI | 953 20 22 26 14 18 27 21 104 |MD 34 45 41 56 57 44 38 85 38
Table 3.1779.4 GPS week: 1779 Day: 4 MJD: 56701
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 | 1016 34 47 27 34 16 26 24 --- 12 | 76 93 71 63 60 89 60 --- 65
R02 | 1451 19 19 13 15 17 23 35 --- 9 | 46 48 55 45 58 58 31 --- 45
R03 | 893 33 33 20 16 16 23 22 --- 9 | 41 53 75 71 71 70 72 --- 65
R04 | 886 18 15 24 9 19 32 17 --- 8 | 45 55 72 55 72 49 54 --- 58
R05 | 1226 23 29 28 19 17 39 26 111 11 | 55 65 70 59 60 45 48 27 54
R06 | 1595 18 18 22 9 15 26 26 --- 8 | 45 45 63 59 56 52 41 --- 51
R07 | 1247 10 12 12 9 14 29 19 98 7 | 57 65 66 55 67 48 72 41 60
XR08 | 544 10 15 22 19 19 --- 21 --- 9 | 47 57 68 44 55 --- 55 --- 51
R09E | 2448 54 53 21 26 37 63 41 --- 18 | 40 55 48 62 53 72 53 --- 46
R10E | 2557 20 18 22 11 15 27 19 --- 8 | 25 27 27 27 28 36 27 --- 22
R11E | 659 28 27 41 32 31 68 42 449 18 | 115 118 131 132 136 134 114 24 123
R12E | 1572 38 29 34 39 40 69 35 --- 18 | 41 44 49 61 74 61 33 --- 42
R13E | 936 17 19 24 18 26 38 24 --- 11 | 28 32 25 34 47 42 32 --- 30
R14E | 1115 38 40 44 32 24 35 33 --- 15 | 128 131 136 145 129 133 134 --- 132
R15E | 3909 23 25 20 8 24 25 15 163 8 | 26 28 24 21 33 31 24 41 20
R16E | 1309 22 40 17 19 26 28 20 --- 10 | 25 30 30 31 34 29 24 --- 22
R17 | 709 16 30 20 17 17 20 21 96 8 | 25 36 29 13 20 21 19 27 13
R19 | 737 25 26 14 17 18 20 16 --- 8 | 27 32 20 23 29 28 19 --- 16
R20 | 1375 33 26 20 18 26 23 29 --- 11 | 24 22 26 30 37 29 28 --- 19
R21 | 1288 53 116 25 17 26 31 21 --- 13 | 27 86 31 34 37 38 43 --- 25
R22 | 1722 15 20 20 10 19 23 15 --- 7 | 16 19 18 27 32 25 23 --- 19
R23 | 621 21 26 17 10 10 20 19 --- 7 | 19 23 21 18 21 20 19 --- 13
R24 | 1210 23 25 23 14 17 25 17 --- 8 | 33 36 36 25 33 36 24 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1571 29 38 24 20 23 35 26 228 |T 43 52 51 49 54 52 45 36 44
WRMS | 1571 23 25 23 17 16 29 26 228 |NE 38 49 48 41 47 43 40 38 38
MEDI | 1226 23 26 22 17 19 26 21 111 |MD 40 45 48 44 53 42 33 27 42
Table 3.1779.5 GPS week: 1779 Day: 5 MJD: 56702
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 | 1256 35 26 27 18 18 22 30 --- 11 | 59 54 56 54 51 47 34 --- 47
R02 | 1847 16 19 19 15 11 16 23 --- 7 | 36 31 34 31 36 33 36 --- 32
R03 | 2055 36 39 20 14 11 16 13 --- 8 | 29 29 48 50 49 50 43 --- 45
R04 | 1301 34 57 17 17 18 18 26 --- 9 | 36 32 59 66 66 55 41 --- 55
R05 | 970 31 26 24 10 16 15 17 120 8 | 43 44 62 46 45 48 49 27 47
R06 | 1015 21 29 16 13 12 24 28 --- 8 | 35 29 53 48 39 54 26 --- 41
R07 | 1025 14 30 20 16 11 22 24 158 8 | 49 32 61 54 52 74 43 34 53
XR08 | 1266 37 51 15 19 15 --- 20 --- 10 | 46 31 54 50 55 --- 43 --- 48
R09E | 1868 71 71 52 27 31 71 42 --- 21 | 39 47 57 39 53 44 48 --- 37
R10E | 820 26 25 16 11 12 32 28 --- 9 | 25 26 19 25 27 30 33 --- 21
R11E | 1000 42 39 42 32 27 51 37 473 16 | 85 92 98 113 93 116 80 19 95
R12E | 1350 36 38 43 35 27 83 43 --- 20 | 39 51 62 59 57 73 40 --- 45
R13E | 737 26 18 27 24 22 40 30 --- 12 | 28 28 26 40 39 43 34 --- 28
R14E | 1252 34 50 59 20 20 37 35 --- 15 | 113 123 101 118 125 123 117 --- 114
R15E | 4599 28 24 20 21 13 18 21 242 9 | 26 29 26 28 26 30 22 42 20
R16E | 1125 31 35 30 11 11 24 31 --- 10 | 26 28 27 25 24 25 19 --- 19
R17 | 616 20 23 16 14 14 21 20 66 7 | 15 23 16 19 17 20 22 21 11
R19 | 1167 30 60 26 23 13 17 20 --- 9 | 28 53 31 23 24 29 15 --- 17
R20 | 1435 35 45 29 27 20 24 22 --- 11 | 25 40 25 31 29 25 19 --- 13
R21 | 1651 70 66 23 19 24 24 23 --- 14 | 38 37 34 35 42 35 33 --- 27
R22 | 2119 13 21 34 18 15 22 25 --- 9 | 20 25 30 20 25 33 21 --- 16
R23 | 1060 20 11 14 18 13 16 15 --- 7 | 19 12 19 23 19 21 18 --- 13
R24 | 1484 29 37 25 13 18 20 28 --- 9 | 22 31 13 26 29 19 22 --- 17
------+---------------------------------------------------+-----------------------------------------------
RMS | 1648 35 39 30 20 18 34 27 255 |T 38 40 43 44 44 46 37 35 37
WRMS | 1648 27 32 27 19 15 29 27 255 |NE 33 33 39 38 38 38 31 38 32
MEDI | 1256 31 35 24 18 15 22 25 158 |MD 35 31 34 39 39 35 34 27 32
Table 3.1779.6 GPS week: 1779 Day: 6 MJD: 56703
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 | 1002 27 25 32 21 17 48 15 --- 12 | 94 97 96 89 92 80 92 --- 89
R02 | 986 15 19 16 8 14 22 22 --- 7 | 64 67 69 64 74 55 65 --- 65
R03 | 1035 32 38 25 7 16 22 30 --- 10 | 55 62 88 78 82 80 69 --- 75
R04 | 1377 13 18 25 22 16 26 29 --- 9 | 60 64 81 67 78 55 71 --- 68
R05 | 1018 16 15 22 32 12 21 25 102 10 | 68 68 92 70 78 73 71 33 72
R06 | 1024 14 12 17 12 15 27 32 --- 9 | 56 61 77 68 64 79 59 --- 65
R07 | 2088 10 14 22 22 10 23 33 254 9 | 80 88 93 98 90 80 67 41 85
XR08 | 1279 22 12 17 15 19 --- 40 --- 11 | 79 86 89 88 95 --- 70 --- 84
R09E | 1091 68 68 54 24 27 49 61 --- 21 | 54 56 43 63 57 73 52 --- 51
R10E | 1019 27 31 25 17 13 19 20 --- 9 | 32 38 28 32 32 34 34 --- 28
R11E | 1984 40 36 27 46 35 50 38 328 18 | 91 95 102 115 112 119 99 25 102
R12E | 562 43 28 35 33 41 51 34 --- 17 | 46 56 53 70 68 81 46 --- 52
R13E | 733 22 26 28 23 25 43 30 --- 12 | 27 35 25 43 40 49 36 --- 29
R14E | 858 55 39 80 39 37 46 59 --- 23 | 79 98 100 124 93 101 93 --- 94
R15E | 3890 28 36 28 14 23 40 23 290 11 | 25 27 28 32 37 39 30 54 25
R16E | 1223 30 30 31 14 11 35 22 --- 10 | 26 27 26 36 27 45 24 --- 25
R17 | 656 17 22 21 17 14 21 24 59 8 | 27 27 25 19 21 23 24 33 15
R19 | 1685 27 25 25 16 16 18 29 --- 9 | 33 36 32 27 27 27 20 --- 22
R20 | 1073 44 38 59 29 18 34 24 --- 16 | 30 26 32 41 30 39 35 --- 25
R21 | 2728 61 66 33 40 27 19 28 --- 16 | 41 55 33 55 45 36 34 --- 31
R22 | 1799 20 24 38 21 38 14 28 --- 13 | 24 30 31 30 41 18 24 --- 19
R23 | 1248 23 34 16 15 18 16 23 --- 8 | 33 42 21 16 23 22 15 --- 14
R24 | 1224 23 28 17 16 13 21 23 --- 8 | 33 39 21 27 23 25 20 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS | 1565 34 33 34 24 23 33 31 232 |T 50 55 55 58 57 56 50 42 50
WRMS | 1565 26 27 29 20 18 28 31 232 |NE 51 56 58 55 57 49 49 43 49
MEDI | 1091 27 28 25 21 17 23 28 254 |MD 46 56 43 63 57 49 46 33 51
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