[IGSREPORT-20801] Wk 1684 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu May 3 11:30:38 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1684 (Apr 15, 2012 - Apr 21, 2012)
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 2.1684.
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:
igl1684[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1684 in the SP3 format.
igl16847.sum Combination Report for GPS Week 1684.
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). 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 | 165.1 ns
1 | 166.0 ns
2 | 166.4 ns
3 | 160.6 ns
4 | 152.2 ns
5 | 154.8 ns
6 | 156.9 ns
5. The following orbit solutions were excluded from the combination because
they were biasing the weighted average. They were still used for statistics
computation.
Day | Centre | PRN list
----+--------+---------------
0 | EMX | ALL (high Transformation - See Table 1)
1 | EMX | ALL (high Transformation - See Table 1)
2 | EMX | ALL (high Transformation - See Table 1)
3 | EMX | ALL (high Transformation - See Table 1)
4 | EMX | ALL (high Transformation - See Table 1)
5 | EMX | ALL (high Transformation - See Table 1)
6 | EMX | ALL (high Transformation - See Table 1)
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 1.1684, 1a.1684).
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 2.1684.0-6)
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 3.1684.0-6).
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 1684 summary. (Apr 15, 2012 - Apr 21, 2012)
Table 1.1684.a GPS week : 1684 MJD: 56032.0-56038.0
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 259| -1 1 -8 21 15 -58 -.19 27 26 | --- --- --- ---
| 1 1 3 20 29 41 .05 | --- ---
emx 137| 2 0 -10 -122 -62 -125 -.07 39 39 | 161186 -2665 4539 7647
| 2 0 2 27 64 34 .04 | 3284 5538
esx 172| 0 0 1 -19 18 -25 .35 17 16 | 162223 -4163 4529 4757
| 1 0 3 23 27 17 .03 | 3161 7504
gfz 191| 0 -1 0 15 -34 12 -.28 19 18 | 0 -4208 4538 7540
| 1 1 1 54 43 19 .06 | 0 7597
grg 124| 0 1 5 1 -55 74 -.06 40 37 | 160933 -4259 4536 20929
| 1 1 3 36 33 55 .10 | 8524 7167
iac n/a| -1 1 1 -9 15 18 -.03 24 24 | 161648 -610 4545 7841
| 2 1 8 24 28 53 .06 | 5886 977
mcc n/a| -1 -3 -11 55 51 -131 -.14 264 264 | --- --- --- ---
| 12 7 13 236 191 774 .44 | --- ---
Table 1.1684.b GPS week : 1684 MJD: 56032.0-56038.0
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 | 12 15 14 10 10 10 11 |
R02 | 11 8 18 10 9 9 10 |
R03 | 10 9 11 21 15 14 11 |
R04 | 9 9 11 10 14 13 17 |
R05 | 9 11 9 12 13 19 13 |
R06 | 12 9 10 10 11 11 13 |
R07 | 12 12 12 12 10 12 12 |
R08 | 12 14 10 10 9 9 9 |
R09 | 12 9 12 11 12 12 10 |
R10 | 11 9 12 10 10 11 12 |
R11 | 19 21 17 19 22 18 16 |
R12 | 12 10 10 11 12 10 9 |
R13 | 12 9 9 12 14 11 11 |
R14 | 9 15 12 13 14 12 14 |
R15 | 13 17 10 13 11 11 18 |
R16 | 15 10 11 10 11 12 12 |
R17 | 12 7 10 14 11 12 13 |
R18 | 8 10 10 10 14 10 9 |
R19 | 11 7 11 9 10 15 12 |
R20 | 17 16 13 14 12 16 19 |
R21 | 14 12 13 15 15 13 11 |
R22 | 15 12 8 7 10 12 11 |
R23 | 8 13 13 11 11 9 11 |
R24 | 9 9 11 9 7 9 12 |
R26 | --- --- --- --- --- 0 0 |
Table 1.1684.c GPS week : 1684 MJD: 56032.0-56038.0
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 1684 0 | 5 -23 163 600 -1852 7335 86.7 1658 1658 | 165130 0
brd 1684 1 | 68 163 97 1749 175 3116 83.9 1586 1586 | 166008 0
brd 1684 2 | -160 1 72 231 -1099 4453 83.2 1930 1930 | 166379 0
brd 1684 3 | -88 -46 27 -670 -2624 1304 84.1 1749 1749 | 160620 0
brd 1684 4 | 121 -2 200 -1525 -1599 -3304 85.1 1928 1928 | 152249 0
brd 1684 5 | 40 110 152 -1067 432 2136 86.1 1681 1681 | 154787 0
brd 1684 6 | -56 -93 179 594 982 -618 84.6 1740 1740 | 156910 0
-------------+------------------------------------------------------------+----------------
brd 1684 mean| -9 15 127 -12 -797 2060 84.8 1753 1753 | 160297 0
brd 1684 sdev| 97 89 63 1135 1342 3444 1.3 131 131 | 5768 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 2.1684.0 GPS week: 1684 Day: 0 MJD: 56032
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 259| 0 0 -14 9 -11 -60 -.21 27 24 | --- --- --- ---
emx 137| 0 -1 -12 -125 -108 -148 -.12 34 32 | 164978 -585 3641 6555
esx 172| 1 0 1 -38 0 -17 .36 20 18 | 167584 -4387 3634 3882
gfz 191| -1 -2 1 11 -10 22 -.17 17 15 | 0 -2499 3636 6497
grg 124| -2 3 4 0 -126 52 .01 45 45 | 157660 -2120 3642 18231
iac n/a| 0 1 4 0 31 16 .02 21 21 | 166374 -495 3654 7201
mcc n/a| -18 -6 3 114 -72 586 .47 155 155 | --- --- --- ---
Table 2.1684.1 GPS week: 1684 Day: 1 MJD: 56033
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 259| 0 0 -7 0 27 -87 -.27 29 30 | --- --- --- ---
emx 137| 0 0 -8 -96 69 -61 -.09 40 36 | 164305 2548 4225 7333
esx 172| -1 0 0 -48 -3 -20 .30 17 15 | 163094 4578 4234 4369
gfz 191| 1 0 1 91 -40 42 -.24 18 19 | 0 2281 4235 7021
grg 124| 0 0 4 -56 -29 86 -.02 42 33 | 163396 1974 4217 21648
iac n/a| 0 0 -1 -17 21 -23 .01 20 20 | 166761 42 4233 7230
mcc n/a| 12 -2 -1 168 7 68 .31 255 255 | --- --- --- ---
Table 2.1684.2 GPS week: 1684 Day: 2 MJD: 56034
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 259| -1 0 -7 38 -6 -95 -.19 27 27 | --- --- --- ---
emx 137| 4 0 -9 -146 -41 -98 -.09 37 37 | 163958 4396 3906 6993
esx 172| 1 0 -1 -17 47 -21 .34 16 15 | 164939 3823 3877 4029
gfz 191| 0 0 2 57 -80 27 -.31 19 19 | 0 6001 3885 7137
grg 124| 0 2 10 -40 -24 152 .01 38 33 | 157456 4532 3885 19429
iac n/a| 0 2 0 -37 18 -23 .04 21 21 | 167943 132 3871 7713
mcc n/a| 11 3 -10 -28 188 326 .09 174 174 | --- --- --- ---
Table 2.1684.3 GPS week: 1684 Day: 3 MJD: 56035
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 259| -4 4 -8 0 29 -103 -.15 29 28 | --- --- --- ---
emx 137| 4 0 -9 -121 -83 -139 -.09 36 36 | 161316 -1838 3685 6362
esx 172| 0 -1 3 -18 34 -21 .34 16 14 | 159418 238 3605 3779
gfz 191| 0 0 0 52 -57 -4 -.30 19 20 | 0 -1538 3674 6146
grg 124| -1 1 8 21 -51 47 -.07 36 40 | 155411 -1679 3698 17883
iac n/a| 0 -1 -6 -24 44 101 -.05 27 27 | 163411 -479 3669 6141
mcc n/a| -1 -7 -31 -324 249 474 -.42 191 191 | --- --- --- ---
Table 2.1684.4 GPS week: 1684 Day: 4 MJD: 56036
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 259| -1 3 -4 12 45 -28 -.16 26 24 | --- --- --- ---
emx 137| 3 -1 -7 -103 -57 -141 -.03 39 41 | 157202 -10665 5731 10061
esx 172| 0 -2 2 -15 41 -10 .38 19 17 | 159111 -14896 5719 6105
gfz 191| 3 -2 0 -16 -68 -5 -.34 22 19 | 0 -16084 5710 9921
grg 124| -1 1 6 29 -54 91 -.07 36 31 | 150828 -16204 5712 19251
iac n/a| 1 1 -2 0 -8 -11 -.03 23 23 | 156023 -2329 5722 9930
mcc n/a| -18 -5 -15 88 26 -1281 -.22 418 418 | --- --- --- ---
Table 2.1684.5 GPS week: 1684 Day: 5 MJD: 56037
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 259| 0 2 -9 40 47 -42 -.18 26 26 | --- --- --- ---
emx 137| 0 0 -14 -95 -95 -160 -.01 42 43 | 158483 -8728 6268 8996
esx 172| 3 -1 -3 26 34 -18 .38 16 15 | 161405 -11636 6314 6661
gfz 191| 0 -1 -1 -64 -32 -7 -.29 20 18 | 0 -10613 6316 9006
grg 124| 0 3 0 15 -59 114 -.27 39 38 | 177064 -10129 6294 29661
iac n/a| -5 0 19 -23 -35 -13 -.11 28 28 | 153298 369 6342 9340
mcc n/a| 4 -12 -25 444 241 -1182 -.41 305 305 | --- --- --- ---
Table 2.1684.6 GPS week: 1684 Day: 6 MJD: 56038
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 259| 0 1 -5 49 -23 9 -.13 24 22 | --- --- --- ---
emx 137| 0 0 -7 -167 -120 -130 -.06 42 45 | 158062 -3789 4321 7234
esx 172| 1 -1 6 -28 -24 -64 .38 17 15 | 160013 -6864 4321 4478
gfz 191| 1 -2 -1 -22 48 14 -.33 19 17 | 0 -7009 4311 7056
grg 124| 0 0 2 39 -40 -21 -.01 42 38 | 164718 -6189 4309 20403
iac n/a| -1 4 0 38 37 86 -.09 30 30 | 157729 -1511 4324 7333
mcc n/a| -1 9 0 -73 -277 84 -.77 351 351 | --- --- --- ---
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 3.1684.0 GPS week: 1684 Day: 0 MJD: 56032
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1293 22 25 8 12 63 22 --- 12 | 50 63 57 56 70 63 --- 56
R02 | 1269 24 17 13 15 41 20 --- 10 | 61 43 40 40 55 55 --- 46
R03 | 2314 30 45 18 14 18 17 --- 9 | 60 64 48 43 45 55 --- 48
R04 | 1431 27 17 18 12 19 17 --- 9 | 72 63 60 51 50 50 --- 54
R05 | 922 32 20 13 9 23 16 152 9 | 65 50 48 45 50 43 87 46
R06 | 1306 34 22 23 13 28 18 --- 11 | 54 47 48 43 38 47 --- 43
R07 | 2498 24 24 22 14 47 16 --- 11 | 49 33 37 37 56 29 --- 32
R08 | 1288 19 25 15 15 65 13 112 12 | 55 42 36 45 67 41 73 41
R09E | 1695 28 34 16 24 30 27 --- 12 | 38 53 57 58 73 41 --- 49
R10E | 1617 30 23 18 17 30 23 --- 11 | 85 78 84 89 98 84 --- 85
R11E | 1089 47 47 26 27 68 33 --- 18 | 79 93 117 118 139 84 --- 103
R12E | 614 17 43 13 15 61 19 --- 11 | 44 57 53 56 67 40 --- 49
R13E | 802 22 44 23 17 46 22 --- 12 | 69 76 85 81 71 62 --- 73
R14E | 4126 22 41 20 12 21 16 --- 9 | 43 54 48 44 53 46 --- 43
R15E | 2010 25 40 27 14 50 23 174 13 | 54 60 59 59 58 49 96 52
R16E | 504 33 28 15 20 70 21 --- 15 | 40 40 45 54 71 39 --- 43
R17 | 1546 20 36 28 26 22 15 143 11 | 62 66 58 82 77 63 39 65
R18 | 2129 16 28 13 16 24 16 182 8 | 50 47 48 59 52 52 87 51
R19 | 844 22 28 15 12 51 21 --- 11 | 54 48 54 58 57 66 --- 56
R20 | 2174 39 56 27 23 71 19 --- 16 | 37 66 57 65 50 51 --- 49
R21 | 645 34 56 29 17 44 19 --- 13 | 86 47 81 78 57 61 --- 72
R22 | 505 23 24 30 13 39 40 --- 14 | 58 72 86 73 81 42 --- 65
R23 | 1381 14 25 9 13 26 20 --- 8 | 41 44 49 51 53 27 --- 42
R24 | 910 14 30 10 16 33 19 --- 9 | 52 49 55 52 67 45 --- 51
------+----------------------------------------------+------------------------------------------
RMS | 1657 27 34 20 17 45 21 154 |T 56 56 58 59 64 51 76 54
WRMS | 1657 24 32 18 15 45 21 154 |NE 56 52 56 55 58 49 80 51
MEDI | 1293 24 28 18 15 39 19 152 |MD 54 53 54 56 57 49 87 49
Table 3.1684.1 GPS week: 1684 Day: 1 MJD: 56033
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 983 23 28 16 23 64 30 --- 15 | 40 59 57 65 82 48 --- 51
R02 | 1210 24 24 11 14 22 11 --- 8 | 54 51 39 43 49 47 --- 43
R03 | 1597 27 32 16 13 26 16 --- 9 | 45 49 47 40 33 39 --- 39
R04 | 1155 32 31 13 14 13 16 --- 9 | 55 54 44 48 46 37 --- 43
R05 | 1097 31 21 14 17 37 18 176 11 | 57 48 45 42 57 39 69 42
R06 | 1317 18 17 19 15 27 14 --- 9 | 48 54 49 49 41 43 --- 44
R07 | 3019 45 20 13 16 31 18 --- 12 | 41 37 32 32 49 29 --- 29
R08 | 1131 32 15 12 18 66 14 49 13 | 46 37 39 37 85 31 71 38
R09E | 1106 17 34 19 15 22 19 --- 9 | 30 28 38 38 44 29 --- 32
R10E | 2298 24 33 12 16 19 19 --- 8 | 70 71 79 68 79 68 --- 72
R11E | 949 47 47 36 23 77 37 535 20 | 57 98 93 80 118 58 100 74
R12E | 815 20 26 14 14 36 16 --- 9 | 32 37 45 48 56 31 --- 37
R13E | 1227 11 26 11 12 42 13 --- 8 | 74 71 70 76 80 67 --- 71
R14E | 3475 24 73 22 22 58 31 --- 15 | 40 51 40 43 50 46 --- 36
R15E | 1904 32 53 16 18 92 15 165 17 | 54 57 61 64 77 56 76 55
R16E | 1624 26 37 14 16 32 14 --- 9 | 30 42 35 42 50 37 --- 34
R17 | 1290 12 28 9 16 13 13 134 6 | 43 48 50 48 56 46 27 46
R18 | 1285 27 24 17 12 27 20 164 10 | 37 42 36 35 18 45 70 32
R19 | 1065 18 18 10 13 24 12 --- 7 | 40 30 33 34 38 35 --- 33
R20 | 1795 46 110 23 35 22 28 --- 15 | 24 28 47 62 55 50 --- 45
R21 | 936 45 45 22 10 34 12 --- 12 | 56 34 27 39 24 31 --- 30
R22 | 1017 34 24 22 13 30 24 --- 12 | 32 34 41 35 22 19 --- 26
R23 | 1608 23 30 20 24 45 24 --- 12 | 25 38 23 38 35 25 --- 23
R24 | 779 18 29 9 22 24 19 --- 9 | 41 53 55 62 38 44 --- 48
------+----------------------------------------------+------------------------------------------
RMS | 1586 29 40 17 18 42 20 255 |T 44 47 46 48 53 41 68 42
WRMS | 1586 30 36 15 19 33 20 255 |NE 42 40 41 43 50 36 70 37
MEDI | 1210 24 28 14 16 30 16 164 |MD 41 48 44 43 49 39 70 39
Table 3.1684.2 GPS week: 1684 Day: 2 MJD: 56034
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1387 25 25 13 22 58 21 --- 13 | 40 58 55 58 72 46 --- 47
R02 | 832 24 18 15 19 88 23 --- 17 | 51 50 36 57 95 39 --- 45
R03 | 993 32 26 19 10 27 19 --- 10 | 50 52 34 42 44 42 --- 37
R04 | 1542 36 21 18 13 19 19 --- 10 | 53 51 45 40 39 35 --- 39
R05 | 650 26 10 10 13 31 11 184 9 | 51 46 41 37 38 40 88 38
R06 | 1975 27 18 7 16 31 16 --- 9 | 48 42 37 40 32 33 --- 34
R07 | 3009 22 18 13 15 55 17 --- 12 | 40 37 33 36 71 37 --- 35
R08 | 1328 35 24 11 18 20 17 91 10 | 37 36 25 27 30 28 59 24
R09E | 1021 28 35 18 19 29 26 --- 11 | 37 27 43 50 55 41 --- 39
R10E | 1583 23 34 12 23 24 33 --- 11 | 83 75 85 91 79 64 --- 78
R11E | 1500 40 53 22 29 62 27 265 17 | 67 79 99 96 116 75 83 86
R12E | 634 19 23 19 17 31 19 --- 10 | 35 40 52 54 62 35 --- 44
R13E | 1268 19 18 13 13 23 19 --- 8 | 76 80 88 87 92 83 --- 84
R14E | 2361 24 57 18 13 38 29 --- 12 | 43 49 47 45 46 51 --- 42
R15E | 4035 23 29 18 17 24 21 201 10 | 46 45 49 47 58 43 81 43
R16E | 1649 22 34 13 22 33 20 --- 10 | 34 29 50 53 51 34 --- 42
R17 | 1013 27 28 16 15 25 16 109 9 | 51 54 57 57 61 35 53 49
R18 | 3103 20 25 16 18 22 21 131 9 | 40 54 42 49 40 23 87 36
R19 | 1121 27 24 21 23 21 20 --- 11 | 40 36 23 34 43 37 --- 25
R20 | 4368 36 110 14 31 33 18 --- 13 | 30 46 26 25 23 33 --- 22
R21 | 855 39 27 17 13 43 16 --- 12 | 60 38 50 51 56 40 --- 48
R22 | 1303 15 44 12 16 18 19 --- 8 | 42 57 37 50 47 40 --- 40
R23 | 1206 15 20 16 26 51 21 --- 13 | 30 39 45 60 26 28 --- 35
R24 | 972 18 24 18 21 19 32 --- 11 | 42 56 68 71 58 37 --- 54
------+----------------------------------------------+------------------------------------------
RMS | 1929 27 37 16 19 38 21 174 |T 46 49 48 52 55 41 75 44
WRMS | 1929 27 37 15 19 33 21 174 |NE 43 44 36 39 45 37 73 34
MEDI | 1303 24 25 16 17 29 19 131 |MD 42 46 45 50 51 37 81 40
Table 3.1684.3 GPS week: 1684 Day: 3 MJD: 56035
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1360 27 27 16 15 20 26 --- 10 | 55 58 63 57 59 61 --- 58
R02 | 1031 23 22 12 18 33 18 --- 10 | 58 51 49 49 47 57 --- 48
R03 | 1172 37 12 14 20 95 38 --- 20 | 49 40 36 50 98 46 --- 43
R04 | 975 24 19 12 18 26 19 --- 9 | 58 55 50 54 57 54 --- 51
R05 | 601 37 35 14 17 35 21 207 12 | 63 62 44 41 33 56 199 43
R06 | 1496 20 22 12 18 28 19 --- 9 | 57 52 48 39 56 41 --- 45
R07 | 2302 31 25 9 18 42 22 --- 11 | 52 44 37 34 44 45 --- 35
R08 | 745 28 21 10 18 31 15 125 10 | 51 52 46 48 43 55 108 46
R09E | 930 23 57 11 18 30 29 --- 10 | 43 59 62 65 67 44 --- 55
R10E | 1117 27 23 14 10 28 22 --- 9 | 101 93 107 106 116 98 --- 104
R11E | 2451 58 76 29 27 57 29 253 19 | 77 102 125 128 135 90 153 111
R12E | 558 22 21 17 24 28 24 --- 11 | 42 54 62 65 69 38 --- 54
R13E | 1169 25 24 17 18 21 38 --- 12 | 126 123 138 137 136 118 --- 132
R14E | 2710 28 27 19 18 29 38 --- 13 | 58 73 81 91 77 61 --- 73
R15E | 3109 30 27 19 15 36 37 264 13 | 66 71 80 87 93 61 291 75
R16E | 1332 27 41 17 15 21 18 --- 9 | 52 60 59 65 60 48 --- 55
R17 | 1547 18 42 14 18 35 48 124 13 | 64 53 68 71 79 30 79 60
R18 | 3601 22 27 9 15 36 22 103 10 | 39 48 51 46 63 30 115 43
R19 | 1103 12 20 14 14 33 17 --- 9 | 56 60 69 61 48 44 --- 56
R20 | 3123 43 79 12 34 19 22 --- 13 | 31 51 35 51 40 45 --- 35
R21 | 814 43 29 27 17 20 37 --- 14 | 66 48 46 45 54 57 --- 46
R22 | 1228 14 34 12 13 21 12 --- 7 | 44 59 60 47 42 39 --- 47
R23 | 1125 16 26 20 19 35 15 --- 10 | 24 34 26 34 47 20 --- 22
R24 | 1166 19 27 10 17 30 20 --- 9 | 52 56 64 75 52 44 --- 58
------+----------------------------------------------+------------------------------------------
RMS | 1749 29 36 16 19 36 27 191 |T 57 60 62 64 67 53 157 58
WRMS | 1749 28 36 14 20 40 27 191 |NE 52 54 49 47 46 49 153 45
MEDI | 1169 25 27 14 18 30 22 125 |MD 55 55 59 54 57 46 115 51
Table 3.1684.4 GPS week: 1684 Day: 4 MJD: 56036
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1779 17 27 22 16 14 22 --- 9 | 55 64 55 58 59 68 --- 57
R02 | 951 19 25 11 17 28 20 --- 9 | 50 41 41 37 29 54 --- 40
R03 | 1721 29 30 18 19 60 25 --- 15 | 38 41 42 39 91 45 --- 42
R04 | 975 24 25 23 20 57 20 --- 14 | 69 58 64 73 72 62 --- 61
R05 | 1540 33 37 17 20 42 18 204 12 | 59 43 43 40 39 47 161 43
R06 | 2313 26 26 12 18 41 14 --- 11 | 56 55 49 45 49 56 --- 48
R07 | 1606 25 16 12 22 20 21 --- 10 | 46 40 43 39 53 45 --- 41
R08 | 1347 18 19 10 19 25 19 91 9 | 52 33 44 49 40 42 90 42
R09E | 921 14 40 16 17 48 20 --- 11 | 48 46 52 48 75 36 --- 46
R10E | 2936 24 49 13 17 25 21 --- 10 | 88 74 88 88 102 85 --- 88
R11E | 3507 53 75 37 37 70 28 684 22 | 90 102 132 135 128 96 177 112
R12E | 1857 21 18 13 21 29 32 --- 11 | 44 52 57 65 67 36 --- 51
R13E | 775 21 23 19 27 35 34 --- 13 | 130 132 142 140 144 106 --- 131
R14E | 4217 31 51 29 21 29 28 --- 14 | 70 66 72 60 64 61 --- 61
R15E | 2045 28 41 17 23 22 21 621 11 | 70 65 83 79 70 69 293 73
R16E | 695 17 32 20 18 37 18 --- 10 | 43 56 46 48 67 36 --- 43
R17 | 1866 15 49 20 18 26 29 245 11 | 48 48 79 72 61 40 165 60
R18 | 2462 15 35 13 26 34 41 294 13 | 38 45 62 68 78 33 124 52
R19 | 826 28 27 13 18 24 16 --- 10 | 43 60 55 63 66 50 --- 53
R20 | 2088 21 85 25 30 22 18 --- 12 | 31 42 33 43 39 31 --- 28
R21 | 977 44 41 24 32 33 17 --- 15 | 59 38 37 40 64 46 --- 40
R22 | 1749 29 33 11 19 20 13 --- 9 | 47 51 29 31 29 32 --- 29
R23 | 1012 19 15 15 23 28 28 --- 11 | 39 27 44 45 32 18 --- 32
R24 | 1105 15 30 10 13 23 13 --- 7 | 38 34 36 40 58 34 --- 38
------+----------------------------------------------+------------------------------------------
RMS | 1928 26 39 19 22 36 23 418 |T 56 54 59 60 65 51 168 54
WRMS | 1928 24 41 17 19 31 23 418 |NE 49 47 43 45 48 46 125 42
MEDI | 1606 21 30 16 19 28 20 245 |MD 48 48 49 48 64 45 161 46
Table 3.1684.5 GPS week: 1684 Day: 5 MJD: 56037
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1164 18 36 11 21 26 24 --- 9 | 54 68 57 51 68 62 --- 55
R02 | 866 12 47 12 17 30 21 --- 9 | 42 44 46 51 54 58 --- 47
R03 | 1840 26 20 20 29 28 37 --- 14 | 37 42 42 45 40 55 --- 37
R04 | 998 27 28 16 21 52 23 --- 13 | 57 49 51 46 54 52 --- 45
R05 | 1017 37 41 18 19 90 22 197 18 | 59 42 45 51 103 56 71 51
R06 | 1547 21 38 12 14 46 25 --- 11 | 39 40 33 36 44 38 --- 31
R07 | 1491 33 33 15 23 35 21 --- 12 | 37 35 39 39 48 28 --- 30
R08 | 2291 19 21 9 22 20 18 125 8 | 36 34 32 35 28 32 57 29
R09E | 734 12 30 19 14 49 25 --- 11 | 32 51 35 37 47 36 --- 30
R10E | 1288 18 49 12 12 47 26 --- 11 | 77 71 75 83 94 81 --- 78
R11E | 1008 55 82 24 29 38 36 546 18 | 66 97 100 109 94 99 95 91
R12E | 2338 23 36 13 19 24 19 --- 9 | 27 33 43 55 53 48 --- 41
R13E | 2170 20 21 16 15 25 32 --- 10 | 126 124 138 140 129 128 --- 132
R14E | 3455 16 47 17 15 44 27 --- 11 | 49 44 59 59 59 59 --- 54
R15E | 1682 19 22 19 17 35 29 349 11 | 55 43 44 43 57 58 114 46
R16E | 824 24 31 22 20 29 30 --- 12 | 44 47 49 54 48 53 --- 46
R17 | 2184 18 61 21 15 29 34 123 11 | 56 70 75 58 76 38 79 59
R18 | 2697 18 23 11 20 43 15 262 10 | 34 26 38 48 39 44 72 37
R19 | 920 21 24 18 30 52 39 --- 15 | 44 54 67 70 52 41 --- 54
R20 | 1555 36 89 24 16 40 49 --- 16 | 32 36 31 36 36 39 --- 27
R21 | 545 36 39 10 30 18 25 --- 12 | 57 32 53 57 60 57 --- 53
R22 | 1677 35 36 16 20 25 24 --- 12 | 37 40 25 25 27 42 --- 21
R23 | 1481 19 23 10 20 25 19 --- 9 | 23 24 30 30 28 30 --- 23
R24 | 958 25 32 13 14 27 14 --- 9 | 49 31 37 40 48 41 --- 39
XR26 | ---- --- --- --- --- --- 12 --- 0 | --- --- --- --- --- 62 --- 59
------+----------------------------------------------+------------------------------------------
RMS | 1680 26 42 16 20 39 28 305 |T 48 49 51 54 57 53 81 48
WRMS | 1680 26 43 15 18 38 28 305 |NE 43 42 42 44 51 45 64 41
MEDI | 1481 21 33 16 19 30 25 197 |MD 44 42 44 48 52 52 72 46
Table 3.1684.6 GPS week: 1684 Day: 6 MJD: 56038
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 935 20 38 13 20 27 35 --- 11 | 65 73 69 62 76 78 --- 67
R02M | 1140 21 36 16 21 23 21 --- 10 | 70 57 59 64 51 63 --- 60
R03M | 1943 17 35 18 16 33 25 --- 10 | 84 62 77 68 75 88 --- 76
R04M | 1483 28 59 33 22 51 39 --- 16 | 110 112 125 118 104 97 --- 112
R05 | 1022 30 21 11 22 49 23 379 12 | 86 69 68 60 94 86 50 72
R06 | 2469 23 30 7 22 62 16 --- 12 | 64 59 52 55 62 53 --- 54
R07 | 1546 29 21 19 16 44 18 --- 12 | 55 45 44 38 60 40 --- 41
R08 | 1490 23 25 8 16 30 20 239 9 | 53 39 41 34 56 42 68 40
R09E | 1149 22 23 10 14 39 21 --- 10 | 57 53 67 71 78 60 --- 63
R10E | 1144 18 40 15 20 47 27 --- 11 | 131 122 117 123 146 120 --- 123
R11E | 907 43 60 19 20 52 24 623 15 | 118 142 150 152 151 145 182 142
R12E | 1059 19 48 10 18 27 20 --- 9 | 57 68 77 82 79 72 --- 72
R13E | 2491 28 26 13 18 37 19 --- 11 | 127 138 136 141 142 127 --- 133
R14E | 2851 20 43 16 26 58 32 --- 14 | 78 76 90 90 81 81 --- 82
R15E | 3064 17 31 25 13 61 64 --- 18 | 88 80 88 82 85 90 --- 84
R16E | 1056 24 26 21 18 29 25 --- 11 | 63 65 68 70 78 65 --- 65
R17M | 1873 17 40 23 18 48 24 77 12 | 61 63 81 63 72 62 65 65
R18M | 2523 14 42 9 11 30 25 148 8 | 47 42 46 51 46 42 73 45
R19 | 1205 18 19 12 22 44 28 --- 11 | 61 69 66 66 52 53 --- 59
R20 | 2564 40 123 24 29 56 48 --- 18 | 50 57 54 62 43 45 --- 49
R21 | 518 23 24 16 18 31 26 --- 11 | 88 68 88 80 77 81 --- 82
R22 | 1668 21 19 14 24 26 30 --- 11 | 60 56 56 57 45 50 --- 51
R23M | 1254 28 31 19 10 28 25 --- 11 | 44 41 38 32 39 31 --- 31
R24M | 900 17 25 15 21 43 32 --- 12 | 48 42 50 51 56 59 --- 48
XR26 | ---- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- 82 --- 79
------+----------------------------------------------+------------------------------------------
RMS | 1740 24 42 17 19 42 30 351 |T 73 70 75 73 77 72 87 71
WRMS | 1740 22 45 15 17 38 30 351 |NE 64 59 59 57 62 61 59 59
MEDI | 1254 21 31 15 18 39 25 239 |MD 63 63 68 64 75 65 68 65
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