[IGSREPORT-20049] Wk 1647 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 18 07:45:33 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1647 (Jul 31, 2011 - Aug 06, 2011)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths 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 2.1647.
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:
igl1647[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1647 in the SP3 format.
igl16477.sum Combination Report for GPS Week 1647.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
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).
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 | 167.4 ns
1 | 167.8 ns
2 | 164.8 ns
3 | 163.5 ns
4 | 166.9 ns
5 | 161.1 ns
6 | 161.4 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 | IAC | R04
1 | IAC | R04
2 | IAC | R04
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 1.1647, 1a.1647).
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 2.1647.0-6)
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 3.1647.0-6).
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 1647 summary. (Jul 31, 2011 - Aug 06, 2011)
Table 1.1647.a GPS week : 1647 MJD: 55773.0-55779.0
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 250| 0 0 0 48 1 0 -.12 30 30 | --- --- --- ---
| 1 1 4 32 37 32 .04 | --- ---
esx 137| 0 0 9 -24 -4 -16 .46 22 20 | 164218 -412 5035 5178
| 1 0 4 35 40 53 .04 | 3001 3435
gfz 196| 0 0 3 -2 -16 37 -.20 23 18 | 0 -754 5103 8343
| 1 0 4 52 56 22 .05 | 0 2496
grg 130| -1 1 -2 -8 18 157 .07 46 42 | --- --- --- ---
| 2 2 2 46 20 106 .06 | --- ---
iac n/a| 1 0 -11 -5 10 -81 -.24 23 23 | 165674 -868 5036 8414
| 1 1 6 19 19 70 .07 | 1960 1789
mcc n/a| -1 4 42 42 -3 174 .19 114 114 | --- --- --- ---
| 9 7 23 143 426 1077 .47 | --- ---
Table 1.1647.b GPS week : 1647 MJD: 55773.0-55779.0
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 | 15 9 11 10 15 14 13 |
R02 | 10 8 12 12 11 8 12 |
R03 | 17 12 10 12 12 12 11 |
R04 | 33 45 41 25 47 29 23 |
R05 | 19 17 14 15 11 13 12 |
R06 | 11 21 12 11 11 11 15 |
R07 | 11 15 17 13 12 12 16 |
R08 | 8 11 11 12 13 12 10 |
R09 | 14 10 12 13 16 15 14 |
R10 | 12 11 13 13 12 9 6 |
R11 | 24 17 14 14 15 19 22 |
R12 | 13 11 11 10 10 12 11 |
R13 | 13 18 14 12 12 13 10 |
R15 | 11 13 12 17 13 12 10 |
R16 | 12 11 14 14 16 14 14 |
R17 | 23 14 15 13 13 18 23 |
R18 | 11 13 13 14 12 11 11 |
R19 | 22 12 12 11 11 11 10 |
R20 | 32 23 18 14 13 18 15 |
R21 | 20 10 15 12 11 12 16 |
R22 | 14 12 12 12 14 13 14 |
R23 | 14 10 8 12 11 13 10 |
R24 | 9 10 10 11 12 13 13 |
Table 1.1647.c GPS week : 1647 MJD: 55773.0-55779.0
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 1647 0 | 46 -7 215 -2314 877 -17440 83.9 1983 1983 | 167395 0
brd 1647 1 | 0 -45 310 1180 -941 -11410 88.0 2053 2053 | 167751 0
brd 1647 2 | -174 -34 201 145 -1133 -11130 86.5 2253 2253 | 164817 0
brd 1647 3 | -28 5 160 1351 -2315 -15230 85.7 2049 2049 | 163489 0
brd 1647 4 | -66 -89 197 2712 -4078 -17450 85.8 2226 2226 | 166892 0
brd 1647 5 | -65 -87 318 -579 -2089 -17590 84.8 2448 2448 | 161141 0
brd 1647 6 | 28 -94 309 344 -3317 -11090 86.1 1855 1855 | 161388 0
-------------+------------------------------------------------------------+----------------
brd 1647 mean| -37 -50 244 405 -1856 -14477 85.8 2123 2123 | 164696 0
brd 1647 sdev| 74 40 65 1594 1641 3161 1.3 197 197 | 2783 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 2.1647.0 GPS week: 1647 Day: 0 MJD: 55773
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 250| -1 0 8 80 -49 19 -.11 35 30 | --- --- --- ---
esx 137| -1 0 2 22 -19 -55 .48 23 20 | 169939 -3568 4841 4998
gfz 196| 0 0 -4 -88 -1 75 -.20 26 19 | 0 -2402 4929 6698
grg 130| 0 2 -5 -11 15 47 .00 47 43 | --- --- --- ---
iac n/a| 0 0 -3 19 49 -72 -.35 37 37 | 169185 -3121 4831 7200
mcc n/a| 7 0 49 53 27 -582 .10 121 121 | --- --- --- ---
Table 2.1647.1 GPS week: 1647 Day: 1 MJD: 55774
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 250| 0 0 0 94 -32 -12 -.06 29 29 | --- --- --- ---
esx 137| 1 -1 10 -35 -10 -4 .43 24 20 | 166657 1765 4493 4573
gfz 196| -3 0 3 -55 55 30 -.26 24 18 | 0 1313 4571 8196
grg 130| -2 1 -1 74 5 37 .03 41 36 | --- --- --- ---
iac n/a| 4 0 -13 -1 -6 -30 -.21 23 23 | 166663 838 4513 8241
mcc n/a| 11 0 41 74 -29 -359 -.20 119 119 | --- --- --- ---
Table 2.1647.2 GPS week: 1647 Day: 2 MJD: 55775
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 250| 1 -2 -1 25 27 -63 -.05 28 30 | --- --- --- ---
esx 137| -1 0 10 -74 -32 -38 .49 21 20 | 162143 1953 4793 4912
gfz 196| 0 0 1 15 2 41 -.23 22 21 | 0 -781 4838 8391
grg 130| 0 2 1 -2 19 107 .09 40 40 | --- --- --- ---
iac n/a| 1 1 -9 21 1 -8 -.30 22 22 | 165953 -666 4788 8545
mcc n/a| -5 -3 41 34 -87 -507 -.13 92 92 | --- --- --- ---
Table 2.1647.3 GPS week: 1647 Day: 3 MJD: 55776
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 250| -1 0 -3 16 -24 -2 -.15 29 32 | --- --- --- ---
esx 137| 1 0 12 -18 -46 -104 .50 20 20 | 162214 -594 5198 5348
gfz 196| 0 0 2 37 17 54 -.15 20 16 | 0 -1735 5304 7880
grg 130| -1 -1 0 22 -11 143 .10 50 50 | --- --- --- ---
iac n/a| 2 0 -12 -25 16 -23 -.27 19 19 | 165114 -1843 5201 7830
mcc n/a| -3 0 20 -78 -19 -529 -.04 112 112 | --- --- --- ---
Table 2.1647.4 GPS week: 1647 Day: 4 MJD: 55777
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 250| -3 0 -7 19 27 5 -.14 29 31 | --- --- --- ---
esx 137| 0 -1 6 -58 -25 3 .43 20 20 | 163777 4908 5650 5809
gfz 196| 0 0 4 61 -7 3 -.21 21 17 | 0 3853 5648 8259
grg 130| -4 5 -5 -28 13 339 .06 47 42 | --- --- --- ---
iac n/a| 2 0 -4 -12 3 -104 -.14 19 19 | 165741 2104 5631 8881
mcc n/a| 0 7 9 -27 128 -280 .04 79 79 | --- --- --- ---
Table 2.1647.5 GPS week: 1647 Day: 5 MJD: 55778
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 250| -1 0 0 71 11 36 -.16 28 27 | --- --- --- ---
esx 137| 0 0 7 16 62 59 .47 20 17 | 162729 -4331 5520 5728
gfz 196| -1 0 10 11 -110 29 -.13 26 20 | 0 -3027 5602 9894
grg 130| -3 -2 -5 -64 36 217 .01 44 39 | --- --- --- ---
iac n/a| 0 -1 -10 -27 -6 -206 -.25 21 21 | 163841 -1812 5524 9137
mcc n/a| -7 14 84 -90 -751 1901 1.17 156 156 | --- --- --- ---
Table 2.1647.6 GPS week: 1647 Day: 6 MJD: 55779
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 250| 0 1 1 33 51 22 -.13 29 30 | --- --- --- ---
esx 137| 1 0 15 -24 39 20 .42 24 20 | 162067 -3022 4755 4883
gfz 196| 0 0 8 1 -74 30 -.23 21 17 | 0 -2501 4835 9088
grg 130| 1 0 -3 -48 53 208 .16 50 44 | --- --- --- ---
iac n/a| 0 -1 -23 -10 16 -125 -.16 22 22 | 163226 -1577 4766 9069
mcc n/a| -17 15 50 334 708 1576 .36 116 116 | --- --- --- ---
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 3.1647.0 GPS week: 1647 Day: 0 MJD: 55773
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 884 25 36 10 54 26 --- 15 | 64 95 69 51 49 --- 67
R02 | 1331 21 11 16 40 13 --- 10 | 50 41 43 41 38 --- 39
R03 | 3145 22 31 36 35 38 --- 16 | 27 48 29 31 20 --- 23
XR04E | 1840 38 28 --- --- 361 --- 33 | 31 67 --- --- 181 --- 47
R05 | 1075 45 34 23 69 14 170 18 | 71 50 35 53 29 7 35
R06 | 1188 33 13 13 40 14 --- 11 | 53 39 33 35 21 --- 29
R07 | 2891 24 16 19 34 19 --- 10 | 47 32 29 30 24 --- 28
R08 | 989 14 9 13 26 19 76 8 | 43 33 37 25 21 43 29
R09 | 885 26 18 22 57 19 --- 13 | 27 32 36 52 23 --- 22
R10 | 979 20 20 22 33 30 --- 12 | 30 47 41 51 36 --- 37
R11 | 2021 78 38 34 68 23 149 24 | 37 60 47 64 35 22 34
R12 | 1267 38 21 19 32 16 --- 12 | 29 43 32 40 27 --- 28
R13 | 1256 36 30 20 25 16 --- 13 | 34 54 33 36 25 --- 30
R15 | 1737 13 20 19 43 18 42 11 | 20 28 24 45 19 41 17
R16 | 1496 30 12 19 46 12 --- 11 | 43 44 42 66 49 --- 43
R17E | 4972 47 26 35 58 66 --- 23 | 80 72 66 63 49 --- 59
R18E | 2439 28 16 16 38 20 --- 11 | 69 90 88 98 76 --- 82
R19E | 1160 42 15 29 64 64 --- 21 | 101 111 113 116 76 --- 98
R20E | 2122 55 29 59 65 97 --- 31 | 138 162 170 172 96 --- 142
R21E | 2145 29 28 24 44 64 --- 19 | 80 83 74 68 85 --- 74
R22E | 1359 26 14 28 50 23 --- 13 | 47 65 60 65 50 --- 54
R23E | 1676 18 21 24 48 29 --- 13 | 42 62 54 65 41 --- 49
R24E | 1445 18 15 16 27 20 --- 9 | 54 71 60 64 61 --- 61
------+-----------------------------------------+-------------------------------------
RMS | 1982 35 23 26 47 37 121 |T 52 62 55 60 49 28 49
WRMS | 1982 30 20 19 43 37 121 |NE 41 46 37 44 29 28 32
MEDI | 1445 28 20 20 43 20 76 |MD 47 54 42 52 38 22 39
Table 3.1647.1 GPS week: 1647 Day: 1 MJD: 55774
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 856 15 11 14 38 13 --- 8 | 32 37 38 36 27 --- 30
R02 | 2560 15 14 19 18 10 --- 7 | 33 34 26 41 27 --- 28
R03 | 3239 27 21 17 33 20 --- 11 | 21 33 25 30 23 --- 20
XR04E | 3036 55 36 --- --- 282 --- 45 | 42 120 --- --- 124 --- 84
R05 | 863 47 16 26 65 20 172 16 | 48 51 47 43 31 6 37
R06 | 1263 38 54 26 73 22 --- 21 | 47 85 36 56 31 --- 41
R07 | 2220 34 18 32 38 25 --- 14 | 46 22 27 30 42 --- 25
R08 | 1794 22 15 16 44 12 52 10 | 36 26 43 48 39 31 33
R09 | 1127 24 16 13 32 15 --- 9 | 29 30 27 41 30 --- 25
R10 | 1385 14 17 20 30 27 --- 11 | 15 22 42 37 21 --- 19
R11 | 1436 60 28 25 29 23 144 17 | 33 40 39 33 29 23 21
R12 | 1592 29 24 17 29 16 --- 11 | 19 34 34 50 27 --- 26
R13 | 1609 28 18 50 57 28 --- 18 | 25 42 31 57 34 --- 28
R15 | 4780 31 25 25 31 21 57 13 | 19 46 36 32 19 25 25
R16 | 1564 27 17 25 25 18 --- 11 | 48 62 74 50 58 --- 57
R17E | 1756 35 20 18 41 27 --- 13 | 42 35 37 45 45 --- 30
R18E | 1959 19 30 16 39 28 --- 13 | 53 68 65 82 50 --- 59
R19E | 1058 24 15 22 45 18 --- 12 | 56 63 67 57 46 --- 54
R20E | 1023 27 43 49 60 45 --- 22 | 78 93 89 106 65 --- 75
R21E | 2238 16 20 14 24 21 --- 9 | 43 52 51 42 42 --- 43
R22E | 1326 18 21 12 50 15 --- 11 | 32 54 37 52 36 --- 38
R23E | 1597 24 13 16 25 22 --- 10 | 33 46 44 53 52 --- 43
R24E | 3224 17 14 19 31 21 --- 10 | 53 63 52 62 54 --- 53
------+-----------------------------------------+-------------------------------------
RMS | 2053 29 24 24 41 22 119 |T 38 50 43 49 41 21 38
WRMS | 2053 29 20 18 36 22 119 |NE 32 40 37 41 31 21 29
MEDI | 1597 27 18 19 33 21 57 |MD 36 46 38 45 36 23 33
Table 3.1647.2 GPS week: 1647 Day: 2 MJD: 55775
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1469 14 20 17 41 17 --- 10 | 55 58 40 44 34 --- 44
R02 | 1844 13 27 10 37 27 --- 12 | 37 45 38 47 24 --- 33
R03 | 1247 25 18 10 39 16 --- 10 | 22 43 28 33 27 --- 27
XR04E | 3925 48 34 --- --- 285 --- 40 | 31 90 --- --- 152 --- 62
R05 | 1103 39 20 16 36 31 --- 14 | 49 50 40 40 21 --- 35
R06 | 1183 12 21 19 45 19 --- 11 | 39 64 50 27 31 --- 41
R07 | 4143 37 29 37 51 16 --- 16 | 54 36 29 44 32 --- 26
R08 | 1460 27 18 14 43 14 45 11 | 40 22 28 31 29 37 24
R09 | 1067 29 14 25 45 12 --- 12 | 15 31 34 36 18 --- 19
R10 | 1156 35 16 29 25 21 --- 12 | 25 42 60 31 37 --- 38
R11 | 2518 46 19 19 48 14 141 14 | 31 27 33 43 16 57 16
R12 | 1436 27 13 21 27 21 --- 10 | 29 29 48 42 31 --- 31
R13 | 929 40 25 15 38 23 --- 13 | 18 40 35 39 22 --- 22
R15 | 6026 21 19 28 39 16 59 12 | 20 31 28 30 20 25 19
R16 | 1190 30 33 21 31 26 --- 14 | 37 50 50 52 52 --- 43
R17E | 1917 40 14 23 36 36 --- 15 | 50 53 52 34 44 --- 42
R18E | 1604 25 17 23 51 19 --- 12 | 56 69 76 79 56 --- 64
R19E | 1691 21 22 18 41 20 --- 11 | 65 77 64 68 52 --- 62
R20E | 922 36 29 37 36 37 --- 17 | 59 78 95 70 63 --- 69
R21E | 2245 24 24 24 49 29 --- 14 | 50 65 68 76 44 --- 54
R22E | 1757 21 17 21 39 22 --- 11 | 28 47 47 52 35 --- 38
R23E | 2435 9 13 16 26 18 --- 8 | 30 42 42 47 38 --- 37
R24E | 3025 15 18 15 37 16 --- 9 | 41 50 50 61 43 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 2253 28 21 22 40 22 92 |T 38 49 47 46 40 39 38
WRMS | 2253 30 20 21 40 22 92 |NE 33 40 38 38 28 39 29
MEDI | 1604 27 19 19 39 20 59 |MD 37 47 42 43 34 37 38
Table 3.1647.3 GPS week: 1647 Day: 3 MJD: 55776
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 961 12 19 10 53 17 --- 10 | 45 57 45 20 48 --- 43
R02 | 1250 31 17 16 46 16 --- 11 | 50 44 37 44 27 --- 34
R03 | 2527 24 23 17 46 23 --- 12 | 21 42 30 49 18 --- 22
XR04E |13883 35 41 --- --- 29 --- 25 | 28 56 --- --- 116 --- 31
R05 | 1576 55 27 21 31 17 --- 15 | 54 32 26 34 27 --- 22
R06 | 1415 23 17 10 51 18 --- 10 | 49 48 32 45 28 --- 32
R07 | 5329 29 22 26 42 15 --- 12 | 47 48 33 30 27 --- 30
R08 | 1697 21 11 24 59 18 61 12 | 54 49 66 58 39 47 48
R09 | 1008 41 23 16 47 15 --- 13 | 31 48 35 30 37 --- 33
R10 | 2419 22 16 16 78 13 --- 13 | 20 29 31 52 23 --- 21
R11 | 2450 47 20 23 39 17 170 14 | 25 52 50 57 31 73 35
R12 | 1174 19 20 18 31 12 --- 9 | 20 30 22 32 13 --- 15
R13 | 1024 36 11 15 48 18 --- 11 | 42 41 30 56 30 --- 31
R15 | 1394 29 22 27 90 19 73 17 | 23 45 47 51 28 64 27
R16 | 1059 47 19 15 45 16 --- 13 | 41 60 58 57 45 --- 48
R17E | 1494 19 18 22 40 33 --- 13 | 35 41 43 34 43 --- 33
R18E | 1853 21 20 23 69 16 --- 13 | 52 71 73 80 66 --- 64
R19E | 2091 14 16 24 45 20 --- 11 | 51 59 62 48 50 --- 52
R20E | 815 25 23 25 40 30 --- 14 | 66 74 90 62 62 --- 69
R21E | 1398 22 19 23 41 22 --- 12 | 56 63 64 72 61 --- 58
R22E | 1386 19 24 17 47 19 --- 11 | 42 60 56 58 44 --- 47
R23E | 2872 14 25 18 46 24 --- 12 | 21 46 37 53 31 --- 30
R24E | 2555 22 23 19 28 18 --- 10 | 50 80 55 74 61 --- 62
------+-----------------------------------------+-------------------------------------
RMS | 2049 29 20 20 50 19 112 |T 40 51 46 49 41 61 38
WRMS | 2049 32 20 16 50 19 112 |NE 37 44 38 43 30 61 31
MEDI | 1494 23 20 18 46 18 73 |MD 42 48 43 51 37 64 33
Table 3.1647.4 GPS week: 1647 Day: 4 MJD: 55777
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1077 27 37 15 64 12 --- 14 | 46 92 62 55 65 --- 65
R02 | 1047 25 18 12 53 11 --- 11 | 43 29 29 42 37 --- 32
R03 | 3294 25 17 18 49 18 --- 11 | 24 31 32 34 25 --- 23
XR04E |14035 53 81 --- --- 60 --- 47 | 36 137 --- --- 66 --- 65
R05 | 1999 33 16 16 40 16 --- 11 | 52 43 40 36 52 --- 43
R06 | 1283 36 11 18 30 14 --- 10 | 41 31 33 24 31 --- 27
R07 | 4939 26 21 15 43 20 --- 11 | 47 39 47 33 33 --- 34
R08 | 2642 22 24 13 42 26 51 12 | 39 48 39 21 20 58 29
R09 | 897 45 29 32 40 16 --- 15 | 23 48 40 53 24 --- 28
R10 | 2498 19 22 26 29 22 --- 11 | 24 35 42 28 24 --- 24
R11 | 1975 40 21 29 59 18 89 15 | 17 45 46 37 32 37 29
R12 | 947 24 13 23 32 12 --- 9 | 22 31 45 39 31 --- 28
R13 | 1603 24 14 16 42 24 --- 11 | 21 28 29 43 19 --- 18
R15 | 3237 29 9 23 58 14 89 12 | 22 23 27 58 20 97 18
R16 | 1298 46 25 14 71 18 --- 16 | 26 51 44 43 46 --- 37
R17E | 3349 27 22 21 39 23 --- 12 | 34 44 31 45 32 --- 28
R18E | 1299 18 18 22 55 16 --- 11 | 29 53 54 55 35 --- 41
R19E | 2834 16 23 24 36 15 --- 11 | 35 57 61 42 36 --- 43
R20E | 1327 37 16 23 30 23 --- 12 | 51 70 80 80 58 --- 64
R21E | 1804 19 16 20 39 18 --- 10 | 56 70 70 47 53 --- 58
R22E | 1133 19 17 24 67 22 --- 14 | 38 51 48 91 42 --- 43
R23E | 1978 21 19 19 36 21 --- 11 | 36 41 37 38 33 --- 32
R24E | 1083 22 20 23 42 21 --- 12 | 27 49 48 44 44 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 2226 29 20 21 47 19 79 |T 34 49 44 44 37 64 36
WRMS | 2226 31 20 17 42 19 79 |NE 31 41 39 39 32 64 31
MEDI | 1804 25 19 20 42 18 89 |MD 35 45 42 42 33 58 32
Table 3.1647.5 GPS week: 1647 Day: 5 MJD: 55778
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1358 19 19 24 66 21 --- 14 | 38 55 47 65 48 --- 43
R02 | 824 14 11 18 23 15 --- 8 | 45 52 44 50 48 --- 46
R03 | 2666 9 14 20 63 17 --- 12 | 12 29 21 54 17 --- 16
XR04E | 9562 42 29 --- --- 50 --- 29 | 31 43 --- --- 39 --- 24
R05 | 1633 31 19 20 42 26 --- 13 | 41 46 60 46 32 --- 41
R06 | 676 22 8 15 51 19 --- 11 | 34 35 43 46 23 --- 30
R07 | 4965 17 11 28 40 25 --- 11 | 33 36 60 32 20 --- 30
R08 | 2056 29 17 23 27 22 107 11 | 31 36 35 36 22 65 24
R09 | 1502 45 18 27 49 16 --- 15 | 26 55 63 63 46 --- 46
R10 | 2734 17 14 26 16 15 --- 9 | 22 26 36 21 20 --- 18
R11 | 1381 52 32 32 48 25 --- 18 | 15 47 54 29 31 --- 29
R12 | 949 20 11 31 41 16 --- 11 | 16 25 46 37 19 --- 21
R13 | 1958 33 11 23 54 15 --- 12 | 23 27 38 61 29 --- 25
R15 | 5425 27 14 20 45 17 194 11 | 29 27 28 47 25 196 17
R16 | 1084 45 20 18 35 19 --- 13 | 34 51 49 41 33 --- 36
R17E | 4936 32 35 38 43 33 --- 18 | 33 53 61 40 38 --- 31
R18E | 1050 21 22 24 31 16 --- 11 | 35 52 49 63 48 --- 44
R19E | 2076 24 19 26 30 16 --- 11 | 33 50 42 42 35 --- 35
R20E | 2982 36 24 36 69 25 --- 17 | 78 88 106 76 65 --- 78
R21E | 1196 21 15 28 41 20 --- 11 | 49 62 70 51 53 --- 55
R22E | 1346 23 24 30 39 22 --- 13 | 29 56 60 53 33 --- 41
R23E | 1004 25 17 25 38 26 --- 12 | 40 37 40 36 27 --- 29
R24E | 507 19 28 24 32 27 --- 13 | 37 56 47 49 39 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 2447 28 20 26 44 21 156 |T 33 45 49 47 34 130 34
WRMS | 2447 27 17 20 39 21 156 |NE 28 39 44 44 29 130 30
MEDI | 1502 24 18 24 41 20 107 |MD 33 47 47 46 33 65 31
Table 3.1647.6 GPS week: 1647 Day: 6 MJD: 55779
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2207 19 20 19 64 15 --- 12 | 50 80 72 33 64 --- 62
R02 | 755 17 15 15 65 15 --- 11 | 51 53 51 42 44 --- 45
R03 | 1703 13 19 18 40 27 --- 11 | 18 34 35 40 21 --- 24
XR04E | 4045 40 32 --- --- 26 --- 23 | 29 58 --- --- 84 --- 38
R05 | 1646 37 7 12 51 18 --- 12 | 74 53 49 28 50 --- 51
R06 | 786 12 32 15 70 25 --- 14 | 60 60 65 37 65 --- 57
R07 | 2311 20 28 25 77 20 --- 15 | 58 51 42 38 46 --- 43
R08 | 3040 20 16 16 36 21 148 10 | 46 36 42 22 38 55 35
R09 | 1131 48 15 26 32 14 --- 14 | 25 40 46 51 31 --- 30
R10 | 1048 7 12 9 14 17 --- 6 | 17 22 25 20 17 --- 15
R11 | 904 56 47 40 48 30 --- 22 | 25 80 65 35 37 --- 43
R12 | 1031 31 18 21 20 14 --- 10 | 9 34 40 34 18 --- 20
R13 | 1580 26 15 16 38 13 --- 10 | 15 36 34 30 33 --- 26
R15 | 3988 12 12 18 43 18 71 9 | 17 22 20 42 19 104 15
R16 | 1349 44 20 17 43 23 --- 14 | 28 47 47 40 42 --- 34
R17E | 2884 54 52 34 68 34 --- 23 | 45 79 68 38 47 --- 47
R18E | 844 22 18 16 40 17 --- 10 | 42 59 50 64 44 --- 48
R19E | 2280 14 19 17 40 20 --- 10 | 46 56 56 60 42 --- 48
R20E | 1166 25 32 22 35 33 --- 14 | 72 80 82 66 60 --- 68
R21E | 1629 24 23 21 78 26 --- 16 | 65 69 76 83 57 --- 64
R22E | 1634 23 21 21 60 20 --- 13 | 31 51 53 74 33 --- 40
R23E | 1490 21 14 18 26 20 --- 9 | 25 37 43 45 31 --- 33
R24E | 1353 20 18 23 38 30 --- 12 | 35 53 51 49 41 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1855 29 24 21 50 22 116 |T 38 51 50 44 41 79 40
WRMS | 1855 30 20 17 44 22 116 |NE 35 46 45 35 37 79 35
MEDI | 1580 22 19 18 40 20 71 |MD 35 53 49 40 42 55 41
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