[IGSREPORT-21198] Wk 1705 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Sep 28 05:53:35 PDT 2012
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1705 (Sep 09, 2012 - Sep 15, 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 2.1705.
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:
igl1705[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1705 in the SP3 format.
igl17057.sum Combination Report for GPS Week 1705.
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 | 215.4 ns
1 | 212.6 ns
2 | 209.5 ns
3 | 207.5 ns
4 | 208.0 ns
5 | 200.6 ns
6 | 193.8 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 | R08
0 | GRG | R08
0 | IAC | R08
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 1.1705, 1a.1705).
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 2.1705.0-6)
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 3.1705.0-6).
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 1705 summary. (Sep 09, 2012 - Sep 15, 2012)
Table 1.1705.a GPS week : 1705 MJD: 56179.0-56185.0
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 0 -5 68 -30 25 -.17 29 29 | --- --- --- ---
| 1 1 2 28 17 27 .06 | --- ---
emx n/a| 1 0 -2 -29 -36 -30 -.14 29 29 | 205346 979 3980 6756
| 2 1 3 19 31 32 .06 | 6251 2375
esx n/a| 0 -2 1 -18 43 -66 .37 19 16 | 204519 3548 3991 4180
| 1 0 1 18 29 30 .06 | 6234 3552
gfz n/a| 0 0 -1 10 16 -10 -.25 18 17 | 0 2410 3991 6588
| 1 1 1 17 43 31 .04 | 0 3389
grg n/a| -1 1 6 -9 -71 -16 .10 37 36 | 164560 1935 4117 32803
| 1 2 3 34 35 41 .14 | 18219 2976
iac n/a| 1 0 5 -23 5 101 .02 24 24 | 207803 -967 3981 6632
| 0 1 9 28 19 46 .05 | 7617 893
mcc n/a| -6 1 28 32 -67 196 .22 211 211 | --- --- --- ---
| 14 9 13 124 126 556 .41 | --- ---
Table 1.1705.b GPS week : 1705 MJD: 56179.0-56185.0
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 | 11 10 10 11 13 12 17 |
R02 | 11 10 8 10 10 12 12 |
R03 | 15 13 9 9 11 10 10 |
R04 | 12 8 8 7 6 8 9 |
R05 | 8 9 9 9 9 9 9 |
R06 | 7 9 10 10 9 9 8 |
R07 | 9 12 11 9 9 10 13 |
R08 | 19 94 0 --- --- --- --- |
R09 | 10 12 9 9 10 11 10 |
R10 | 9 10 8 8 8 10 9 |
R11 | 19 16 15 17 17 20 19 |
R12 | 10 9 9 20 11 11 7 |
R13 | 11 9 9 8 9 11 8 |
R14 | 14 11 11 11 16 16 13 |
R15 | 10 9 11 9 11 12 11 |
R16 | 12 12 8 10 10 9 9 |
R17 | 7 10 11 10 10 12 11 |
R18 | 7 10 12 8 8 9 10 |
R19 | 10 10 9 13 11 9 9 |
R20 | 18 14 17 16 13 14 18 |
R21 | 14 16 16 13 20 15 14 |
R22 | 11 12 11 9 8 11 13 |
R23 | 7 9 11 10 8 9 10 |
R24 | 12 9 7 8 7 8 8 |
Table 1.1705.c GPS week : 1705 MJD: 56179.0-56185.0
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 1705 0 | 107 55 68 -716 -1199 -7464 87.1 1382 1382 | 215356 0
brd 1705 1 | -20 16 45 404 -508 -7497 84.8 1339 1339 | 212616 0
brd 1705 2 | 93 45 91 203 -2261 -13540 83.3 1222 1222 | 209450 0
brd 1705 3 | -39 35 169 -1214 -1535 -13130 84.6 1376 1376 | 207536 0
brd 1705 4 | -72 3 180 -385 -3091 -9510 85.8 1607 1607 | 208040 0
brd 1705 5 | -103 9 166 -589 -1728 -1439 84.4 1524 1524 | 200551 0
brd 1705 6 | -89 -8 182 665 -1825 -6470 84.8 1652 1652 | 193790 0
-------------+------------------------------------------------------------+----------------
brd 1705 mean| -17 22 129 -233 -1735 -8435 85.0 1443 1443 | 206762 0
brd 1705 sdev| 85 23 58 677 811 4161 1.2 155 155 | 7353 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 2.1705.0 GPS week: 1705 Day: 0 MJD: 56179
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 -8 92 -34 12 -.22 28 28 | --- --- --- ---
emx n/a| 0 1 -2 -26 -31 -22 -.12 31 32 | 213115 3341 3433 6686
esx n/a| 1 -2 0 -6 51 -53 .43 18 17 | 212399 5622 3441 3663
gfz n/a| 0 2 -3 0 20 -8 -.25 18 17 | 0 5317 3447 6445
grg n/a| 0 -3 0 -44 -32 -32 -.04 43 43 | 181067 4903 3442 30625
iac n/a| 1 0 11 -43 5 67 -.02 24 24 | 216384 -2065 3449 6650
mcc n/a| -31 11 31 77 -185 19 .45 268 268 | --- --- --- ---
Table 2.1705.1 GPS week: 1705 Day: 1 MJD: 56180
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 -8 41 -30 4 -.09 27 26 | --- --- --- ---
emx n/a| 0 0 -3 -32 -21 -4 -.04 28 28 | 210620 1853 3959 6268
esx n/a| 0 -1 -1 -19 1 -90 .35 17 17 | 210738 3430 3959 4204
gfz n/a| 3 0 -3 11 57 -49 -.29 19 14 | 0 4668 3954 6144
grg n/a| -3 0 8 -49 -96 40 -.08 37 35 | 167129 3548 3970 18636
iac n/a| 2 0 17 -2 7 173 -.06 26 26 | 214634 -1638 3934 6238
mcc n/a| 3 -4 29 87 -3 -577 -.31 148 148 | --- --- --- ---
Table 2.1705.2 GPS week: 1705 Day: 2 MJD: 56181
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 0 -3 37 -35 11 -.12 28 29 | --- --- --- ---
emx n/a| 4 0 3 -39 -20 2 -.08 28 29 | 207108 1566 4164 6553
esx n/a| 0 -3 3 -48 79 -97 .38 17 16 | 206003 4898 4151 4323
gfz n/a| -1 1 0 46 -6 -8 -.27 19 17 | 0 3468 4154 6384
grg n/a| -1 2 5 -31 -89 -18 .06 33 32 | 185699 3670 4157 100437
iac n/a| 2 0 -4 31 -31 131 .02 22 22 | 210731 -1779 4148 6467
mcc n/a| -9 -4 26 -123 -60 -145 -.38 173 173 | --- --- --- ---
Table 2.1705.3 GPS week: 1705 Day: 3 MJD: 56182
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 -3 56 -16 67 -.17 27 28 | --- --- --- ---
emx n/a| 2 1 -2 4 -75 -74 -.15 29 28 | 204757 3211 3836 6384
esx n/a| 1 -3 2 7 34 -102 .38 25 18 | 202851 8440 3856 4040
gfz n/a| -1 -1 0 -10 36 -23 -.16 17 17 | 0 5214 3812 6192
grg n/a| -4 5 5 -2 -83 30 .08 32 31 | 158352 3740 4575 23156
iac n/a| 1 0 0 -47 0 65 .06 19 19 | 207436 160 3816 6246
mcc n/a| -7 -4 34 -70 -90 115 .53 261 261 | --- --- --- ---
Table 2.1705.4 GPS week: 1705 Day: 4 MJD: 56183
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 -2 112 -52 48 -.17 29 26 | --- --- --- ---
emx n/a| 3 -1 1 -18 -87 -71 -.17 28 27 | 206582 1536 3894 6296
esx n/a| -1 -2 3 -33 17 -25 .37 18 16 | 205243 4746 3930 4124
gfz n/a| 0 0 0 8 69 32 -.22 16 17 | 0 2931 3971 6147
grg n/a| 0 -1 8 3 -107 -56 .11 38 33 | 162080 2220 3989 21481
iac n/a| 1 0 -4 -36 29 66 .07 25 25 | 209348 77 3956 6097
mcc n/a| 6 -9 50 41 71 747 .65 330 330 | --- --- --- ---
Table 2.1705.5 GPS week: 1705 Day: 5 MJD: 56184
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 -7 52 -45 40 -.12 31 31 | --- --- --- ---
emx n/a| -1 1 -6 -58 -10 1 -.20 29 29 | 200944 -2227 4181 7279
esx n/a| 0 -1 0 -8 40 -58 .41 18 15 | 200352 -1335 4199 4370
gfz n/a| 0 0 -3 8 -4 -41 -.27 17 14 | 0 -1847 4192 7206
grg n/a| -2 1 3 40 -77 -9 .24 38 34 | 167827 -2048 4294 21215
iac n/a| 1 -2 14 -34 24 142 .06 27 27 | 201678 -884 4172 7208
mcc n/a| -16 6 17 251 -269 127 .26 157 157 | --- --- --- ---
Table 2.1705.6 GPS week: 1705 Day: 6 MJD: 56185
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 -6 85 0 -8 -.26 33 35 | --- --- --- ---
emx n/a| 0 0 -5 -33 -9 -41 -.19 31 27 | 194301 -2427 4397 7827
esx n/a| 0 -1 0 -22 80 -36 .25 17 14 | 194051 -965 4401 4540
gfz n/a| 0 0 0 10 -56 28 -.26 19 20 | 0 -2881 4407 7601
grg n/a| 0 3 10 20 -11 -71 .33 41 43 | 129768 -2483 4394 14076
iac n/a| 1 0 1 -31 2 61 .03 24 24 | 194414 -643 4396 7522
mcc n/a| 9 15 7 -38 65 1088 .36 143 143 | --- --- --- ---
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 3.1705.0 GPS week: 1705 Day: 0 MJD: 56179
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 | 1128 28 35 17 18 32 15 --- 10 | 80 61 64 75 78 73 --- 69
R02 | 1577 42 17 15 19 26 21 --- 10 | 75 44 51 51 51 55 --- 50
R03 | 848 15 34 32 23 72 27 --- 14 | 73 67 81 49 68 49 --- 60
R04 | 766 30 23 24 9 40 34 --- 11 | 64 53 57 48 37 37 --- 47
R05 | 2630 24 16 9 10 38 13 245 7 | 56 39 50 51 32 45 38 46
R06 | 1502 13 15 6 11 38 18 --- 7 | 43 42 47 48 42 37 --- 42
R07 | 1347 15 16 16 18 27 24 --- 8 | 72 62 70 78 58 56 --- 65
XR08 | 5191 320 29 --- 10 2704 408 482 18 | 79 1 --- 4 4 8 34 322
R09E | 810 19 19 17 19 46 21 --- 10 | 32 35 38 41 57 31 --- 32
R10E | 1270 18 21 11 13 36 21 --- 8 | 72 78 74 79 73 78 --- 75
R11E | 2040 39 54 27 26 88 35 309 18 | 89 104 117 116 107 94 97 103
R12E | 1036 22 20 18 18 33 23 --- 9 | 20 27 34 40 47 23 --- 28
R13E | 1399 30 15 19 18 25 36 --- 11 | 27 31 33 38 29 33 --- 27
R14E | 1583 24 53 19 26 48 16 --- 13 | 24 53 46 55 42 34 --- 40
R15E | 2022 13 23 16 15 40 29 436 9 | 25 22 22 22 21 23 195 18
R16E | 997 22 24 16 21 61 23 --- 11 | 31 53 43 58 55 30 --- 40
R17 | 1242 19 20 13 7 17 19 62 7 | 31 30 30 22 32 35 45 26
R18 | 1521 27 13 14 8 14 14 96 6 | 43 27 23 22 21 30 44 24
R19 | 861 34 15 18 13 31 18 --- 9 | 47 28 35 27 32 30 --- 28
R20 | 886 38 76 21 18 34 42 --- 17 | 42 44 48 39 45 45 --- 37
R21 | 844 48 36 22 18 55 15 --- 13 | 54 49 48 46 53 42 --- 41
R22 | 949 29 30 15 18 43 16 --- 10 | 45 30 28 20 48 27 --- 23
R23 | 770 20 15 10 12 32 16 --- 7 | 43 29 30 21 27 28 --- 25
R24 | 1785 29 41 16 25 29 24 --- 12 | 42 43 35 41 32 36 --- 33
------+----------------------------------------------+------------------------------------------
RMS | 1381 28 31 18 18 43 24 268 |T 50 43 48 45 45 40 75 54
WRMS | 1381 28 32 17 17 43 24 268 |NE 55 40 46 40 41 39 40 58
MEDI | 1242 24 21 16 18 36 21 245 |MD 43 42 46 41 42 35 44 40
Table 3.1705.1 GPS week: 1705 Day: 1 MJD: 56180
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 | 982 14 26 22 16 30 26 --- 10 | 52 61 69 53 61 54 --- 57
R02 | 959 23 30 10 17 35 20 --- 9 | 47 33 50 47 55 54 --- 45
R03 | 952 29 53 15 19 38 23 --- 13 | 47 36 51 41 67 39 --- 42
R04 | 879 20 11 15 12 24 19 --- 7 | 44 35 30 34 61 34 --- 34
R05 | 1529 20 13 12 16 47 18 232 9 | 45 34 39 48 24 39 34 37
R06 | 1488 12 26 16 15 34 15 --- 8 | 28 28 38 42 17 34 --- 31
R07 | 1261 29 21 16 21 60 23 --- 12 | 50 52 45 47 45 29 --- 39
XR08 | ---- 60 --- --- --- --- 117 167 93 | 111 --- --- --- --- 7 42 132
R09E | 1121 21 20 19 22 54 31 --- 12 | 19 28 39 36 55 31 --- 26
R10E | 2125 22 23 14 21 31 28 --- 10 | 92 109 100 101 95 102 --- 98
R11E | 827 35 34 22 30 45 46 111 15 | 77 73 86 86 97 83 153 78
R12E | 1337 14 29 11 15 28 25 --- 9 | 20 40 27 34 42 22 --- 25
R13E | 1234 20 26 13 16 23 26 --- 9 | 22 38 39 30 41 33 --- 30
R14E | 1910 30 36 16 22 22 20 --- 10 | 29 42 44 48 48 41 --- 38
R15E | 2662 16 24 22 14 17 23 148 9 | 26 35 33 34 36 40 96 30
R16E | 1039 23 13 17 34 47 24 --- 12 | 30 29 37 36 48 35 --- 28
R17 | 1528 24 37 14 16 16 22 117 9 | 27 35 32 24 25 24 71 21
R18 | 1409 27 18 19 15 38 20 92 10 | 31 26 31 21 33 26 31 23
R19 | 845 27 19 23 18 22 22 --- 9 | 32 20 32 19 27 29 --- 22
R20 | 921 31 31 20 25 51 36 --- 14 | 38 33 43 51 58 39 --- 35
R21 | 1190 57 40 25 19 48 25 --- 15 | 41 60 57 53 52 32 --- 44
R22 | 850 42 26 13 13 44 18 --- 11 | 32 30 27 22 44 32 --- 23
R23 | 795 18 24 16 15 25 27 --- 9 | 31 32 26 25 25 37 --- 24
R24 | 1120 17 23 12 15 16 33 --- 9 | 30 25 24 20 23 32 --- 21
------+----------------------------------------------+------------------------------------------
RMS | 1338 27 28 17 19 37 26 148 |T 41 40 43 41 46 38 71 40
WRMS | 1338 26 28 17 14 35 26 148 |NE 42 36 39 36 41 33 44 39
MEDI | 1121 23 26 16 16 34 23 117 |MD 32 35 39 36 45 34 42 31
Table 3.1705.2 GPS week: 1705 Day: 2 MJD: 56181
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 | 1715 24 24 19 22 26 21 --- 10 | 57 66 67 74 60 70 --- 64
R02 | 982 21 21 7 19 29 16 --- 8 | 60 52 63 71 53 53 --- 58
R03 | 607 26 29 17 17 19 19 --- 9 | 59 57 52 60 61 44 --- 52
R04 | 607 16 20 14 17 22 18 --- 7 | 42 37 34 36 55 32 --- 35
R05 | 829 20 15 14 9 40 17 275 8 | 46 38 55 45 34 29 21 40
R06 | 1849 17 20 20 10 23 33 --- 9 | 35 34 42 35 50 25 --- 30
R07 | 919 36 29 15 12 48 11 --- 11 | 54 56 40 39 29 32 --- 36
XR08 | ---- 4 --- --- --- --- --- 99 0 | 71 --- --- --- --- --- 24 92
R09E | 1225 22 24 9 13 29 19 --- 8 | 25 40 33 36 48 30 --- 30
R10E | 1726 16 26 16 15 18 19 --- 8 | 68 63 61 74 63 61 --- 62
R11E | 1081 38 31 32 33 38 32 234 15 | 64 66 78 71 69 59 110 62
R12E | 1303 21 13 14 16 32 19 --- 8 | 25 24 44 36 37 24 --- 25
R13E | 1154 19 23 13 14 34 16 --- 8 | 22 31 32 33 36 30 --- 25
R14E | 1789 23 36 19 20 29 23 --- 11 | 27 43 45 46 51 44 --- 37
R15E | 1905 26 23 28 19 24 24 79 11 | 24 25 37 32 26 32 53 22
R16E | 1158 18 18 12 17 31 17 --- 8 | 21 36 34 37 41 25 --- 27
R17 | 1073 14 25 17 22 30 29 71 10 | 37 44 51 39 40 39 30 37
R18 | 774 30 24 14 18 48 30 86 12 | 32 29 24 29 26 38 26 22
R19 | 1114 29 13 15 18 23 20 --- 8 | 41 31 30 32 35 36 --- 27
R20 | 1008 40 72 22 25 29 23 --- 16 | 47 47 43 36 35 40 --- 34
R21 | 1175 56 35 23 26 49 27 --- 15 | 46 52 54 55 33 38 --- 39
R22 | 1201 36 24 15 18 35 18 --- 10 | 36 33 32 29 30 22 --- 23
R23 | 778 38 28 9 22 42 15 --- 11 | 51 24 32 25 34 33 --- 25
R24 | 671 10 23 10 18 21 16 --- 7 | 37 38 42 39 27 40 --- 35
------+----------------------------------------------+------------------------------------------
RMS | 1222 28 28 17 19 33 22 173 |T 42 42 44 43 42 38 44 39
WRMS | 1222 29 29 16 17 32 22 173 |NE 46 42 44 42 40 38 25 40
MEDI | 1114 22 24 15 18 29 19 86 |MD 41 38 42 37 37 36 26 35
Table 3.1705.3 GPS week: 1705 Day: 3 MJD: 56182
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 | 1821 29 31 22 12 24 23 --- 10 | 70 69 76 73 62 58 --- 66
R02 | 1375 14 30 10 20 33 18 --- 9 | 56 44 62 75 48 70 --- 61
R03 | 1147 26 26 16 14 25 17 --- 9 | 59 40 56 50 59 37 --- 47
R04 | 949 11 12 9 12 29 13 --- 6 | 49 36 42 49 34 41 --- 41
R05 | 896 26 24 13 13 18 20 272 8 | 50 38 40 33 42 26 43 34
R06 | 1797 24 16 13 13 50 12 --- 9 | 40 46 47 48 51 28 --- 38
R07 | 1156 24 18 20 11 37 12 --- 9 | 65 54 66 55 58 46 --- 54
R09E | 1100 21 21 10 19 28 17 --- 8 | 21 42 32 33 40 25 --- 25
R10E | 2329 12 16 13 14 30 18 --- 7 | 105 104 117 119 120 113 --- 113
R11E | 1960 39 45 29 27 61 32 500 16 | 100 104 111 113 127 96 146 103
R12E | 936 21 40 85 26 31 21 --- 19 | 40 47 64 52 51 39 --- 33
R13E | 1043 18 20 20 15 23 15 --- 8 | 35 48 52 44 34 46 --- 41
R14E | 2111 25 24 23 15 31 25 --- 10 | 26 36 41 35 39 34 --- 29
R15E | 1095 24 23 18 17 22 20 67 9 | 34 41 34 33 39 46 37 34
R16E | 1098 15 22 19 15 41 20 --- 9 | 31 44 42 41 58 27 --- 34
R17 | 800 24 33 13 17 30 18 43 10 | 60 56 46 50 37 44 65 46
R18 | 1014 30 11 18 13 20 18 103 8 | 40 26 29 22 28 31 30 24
R19 | 1922 42 31 18 22 33 25 --- 12 | 50 47 47 43 27 49 --- 39
R20 | 1662 43 66 24 22 30 22 --- 15 | 61 46 59 56 57 39 --- 47
R21 | 1000 47 25 27 18 38 18 --- 12 | 53 61 61 45 90 45 --- 49
R22 | 740 31 20 21 16 21 15 --- 9 | 40 16 27 23 30 31 --- 20
R23 | 1039 28 22 11 24 21 18 --- 9 | 36 32 25 32 24 32 --- 23
R24 | 817 18 22 12 12 29 12 --- 7 | 30 24 37 30 27 27 --- 27
------+----------------------------------------------+------------------------------------------
RMS | 1375 27 29 25 17 32 19 261 |T 50 47 52 50 51 44 57 44
WRMS | 1375 28 28 18 17 31 19 261 |NE 50 42 48 45 44 40 40 41
MEDI | 1098 24 23 18 15 30 18 103 |MD 49 44 47 45 42 39 37 39
Table 3.1705.4 GPS week: 1705 Day: 4 MJD: 56183
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 | 1505 43 24 25 23 45 26 --- 13 | 66 48 62 62 37 34 --- 47
R02 | 1421 28 32 10 16 33 16 --- 9 | 60 48 49 55 45 43 --- 46
R03 | 1459 33 33 14 13 29 24 --- 10 | 46 44 41 47 46 23 --- 38
R04 | 1024 14 14 11 13 18 14 --- 6 | 39 40 30 32 33 37 --- 31
R05 | 739 29 13 11 14 29 29 279 9 | 46 33 38 41 37 22 57 33
R06 | 2526 21 22 13 15 40 16 --- 9 | 38 46 31 31 50 29 --- 31
R07 | 1665 23 14 15 20 19 21 --- 8 | 46 39 43 40 40 26 --- 36
R09E | 911 15 27 15 16 36 24 --- 9 | 22 36 37 39 55 37 --- 30
R10E | 3321 17 28 18 12 24 15 --- 8 | 47 61 40 39 52 46 --- 43
R11E | 1852 42 35 23 31 71 38 675 17 | 106 90 100 112 137 76 374 97
R12E | 1808 25 23 27 16 35 19 --- 10 | 39 38 37 38 52 29 --- 27
R13E | 1319 23 21 18 15 25 21 --- 8 | 30 37 31 34 36 40 --- 29
R14E | 1761 30 58 32 19 32 40 --- 16 | 26 26 51 40 49 38 --- 30
R15E | 1384 25 41 14 16 31 29 56 11 | 28 28 44 41 48 32 38 32
R16E | 1134 26 23 14 17 42 23 --- 10 | 19 33 45 40 58 24 --- 31
R17 | 692 21 37 17 12 29 17 36 9 | 46 29 41 33 43 34 44 34
R18 | 812 18 20 15 13 28 13 80 7 | 34 21 34 35 28 26 44 27
R19 | 1960 30 37 11 16 27 29 --- 11 | 38 25 25 26 38 38 --- 26
R20 | 2220 43 34 23 21 35 28 --- 13 | 46 60 46 38 44 55 --- 40
R21 | 1335 58 29 28 17 95 42 --- 19 | 47 52 64 55 70 38 --- 46
R22 | 864 25 19 14 9 17 21 --- 7 | 38 47 33 28 37 27 --- 29
R23 | 1403 28 10 13 9 24 22 --- 7 | 27 27 26 21 26 37 --- 21
R24 | 1091 18 10 14 10 27 20 --- 7 | 34 35 38 30 33 39 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1606 29 28 18 16 38 25 330 |T 42 41 42 41 47 36 100 36
WRMS | 1606 26 27 16 17 33 25 330 |NE 43 39 40 38 40 33 47 34
MEDI | 1403 25 24 15 16 29 22 80 |MD 39 38 40 39 44 37 44 32
Table 3.1705.5 GPS week: 1705 Day: 5 MJD: 56184
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 | 688 43 30 16 22 28 19 --- 11 | 54 33 51 57 51 36 --- 44
R02 | 1338 39 21 20 15 47 19 --- 11 | 46 31 35 29 48 37 --- 30
R03 | 1551 44 17 15 14 29 17 --- 10 | 51 38 37 39 37 26 --- 35
R04 | 969 12 24 15 10 30 19 --- 8 | 32 39 38 37 22 39 --- 34
R05 | 962 23 15 11 11 36 22 213 8 | 39 24 36 31 30 23 42 28
R06 | 1141 20 17 11 10 37 29 --- 8 | 37 20 36 35 37 28 --- 29
R07 | 2802 24 24 17 19 28 22 --- 9 | 44 34 43 27 52 33 --- 33
R09E | 1299 25 26 11 22 33 29 --- 10 | 17 38 39 47 40 33 --- 33
R10E | 3566 26 20 20 14 32 22 --- 9 | 79 79 90 92 95 85 --- 86
R11E | 1999 45 50 35 29 65 54 147 19 | 89 119 120 111 98 87 269 100
R12E | 2198 21 34 14 17 40 26 --- 10 | 24 33 37 38 37 26 --- 27
R13E | 1109 16 31 9 16 41 32 --- 10 | 34 50 40 45 47 43 --- 38
R14E | 1320 25 46 31 27 51 41 --- 16 | 32 38 63 59 52 36 --- 41
R15E | 1378 27 33 16 19 42 26 177 11 | 40 33 51 50 51 40 39 40
R16E | 1123 15 16 16 16 38 24 --- 9 | 26 29 39 29 47 34 --- 29
R17 | 845 26 26 25 25 44 24 83 12 | 50 46 39 47 46 52 96 41
R18 | 834 25 17 16 15 32 19 134 8 | 36 21 33 36 35 33 41 30
R19 | 1536 30 21 11 10 42 18 --- 9 | 40 42 41 36 35 23 --- 32
R20 | 740 29 48 24 16 42 26 --- 13 | 45 51 54 45 57 52 --- 45
R21 | 1141 60 40 18 15 45 30 --- 15 | 52 49 59 49 44 59 --- 47
R22 | 1119 42 29 14 13 27 27 --- 11 | 39 31 38 37 32 24 --- 28
R23 | 907 28 25 15 12 19 20 --- 8 | 32 23 30 26 21 26 --- 23
R24 | 820 19 8 15 11 27 25 --- 8 | 31 26 27 22 30 35 --- 24
------+----------------------------------------------+------------------------------------------
RMS | 1524 31 29 18 17 38 27 157 |T 42 40 46 44 45 39 87 39
WRMS | 1524 31 29 15 14 34 27 157 |NE 41 33 39 36 38 35 54 33
MEDI | 1141 26 25 16 15 37 24 147 |MD 39 34 39 38 44 35 41 33
Table 3.1705.6 GPS week: 1705 Day: 6 MJD: 56185
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 | 730 50 22 23 22 91 22 --- 16 | 77 50 70 67 89 54 --- 59
R02 | 1003 46 32 23 19 33 15 --- 12 | 74 53 63 56 62 56 --- 56
R03 | 1098 29 33 13 12 34 25 --- 10 | 58 55 53 51 39 46 --- 49
R04 | 1057 20 19 14 23 32 15 --- 9 | 60 50 52 58 43 49 --- 51
R05 | 873 16 18 15 26 27 22 190 9 | 59 48 52 70 51 47 51 53
R06 | 1012 13 12 12 16 37 16 --- 7 | 48 39 46 52 30 38 --- 42
R07 | 3369 35 18 16 26 64 19 --- 12 | 66 49 48 55 49 46 --- 47
R09E | 749 24 28 15 22 27 20 --- 9 | 21 29 38 35 49 29 --- 28
R10E | 3340 22 24 9 16 23 25 --- 8 | 66 77 74 72 76 69 --- 71
R11E | 2148 45 56 30 39 51 46 143 19 | 63 71 88 100 102 75 164 78
R12E | 3007 22 17 9 12 22 15 --- 6 | 33 29 36 41 46 33 --- 32
R13E | 760 15 17 13 11 31 22 --- 8 | 26 27 36 32 41 37 --- 30
R14E | 1620 31 37 22 20 44 28 --- 13 | 25 28 55 47 52 31 --- 35
R15E | 1458 24 29 18 17 39 25 167 10 | 36 37 32 33 46 36 29 31
R16E | 2256 23 27 15 15 35 18 --- 9 | 33 47 45 41 57 36 --- 39
R17 | 816 31 27 23 17 23 25 52 10 | 46 37 34 32 36 41 52 32
R18 | 803 41 20 19 18 30 12 122 10 | 57 27 33 36 32 37 36 32
R19 | 909 35 19 8 13 29 16 --- 8 | 51 26 33 29 26 31 --- 29
R20 | 710 32 79 18 15 54 35 --- 17 | 61 53 58 50 57 53 --- 50
R21 | 2165 56 28 10 18 28 41 --- 13 | 64 49 59 51 59 50 --- 49
R22 | 994 49 31 12 21 48 25 --- 13 | 57 30 32 28 45 32 --- 28
R23 | 956 38 14 10 17 36 23 --- 9 | 44 25 30 30 33 28 --- 26
R24 | 847 25 8 14 10 34 15 --- 7 | 39 32 36 35 34 33 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1651 33 31 17 19 41 24 143 |T 50 42 47 47 50 42 58 42
WRMS | 1651 35 27 14 19 43 24 143 |NE 57 41 46 46 45 42 38 42
MEDI | 1003 31 24 15 17 34 22 143 |MD 57 39 46 47 46 38 36 39
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