[IGSREPORT-24624] Wk 1905 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Jul 28 20:28:55 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1905 (Jul 10, 2016 - Jul 16, 2016)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1905.
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:
igl1905[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1905 in the SP3 format.
igl19057.sum Combination Report for GPS Week 1905.
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 | 5.4 ns
1 | 6.4 ns
2 | -2.3 ns
3 | -1.1 ns
4 | 6.6 ns
5 | 3.7 ns
6 | -0.8 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 1.1905, 1a.1905).
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 2.1905.0-6)
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 3.1905.0-6).
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 1905 summary. (Jul 10, 2016 - Jul 16, 2016)
Table 1.1905.a GPS week : 1905 MJD: 57579.0-57585.0
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| -1 0 -1 27 -49 22 .45 33 32 | --- --- --- ---
| 1 1 1 14 26 52 .07 | --- ---
cof n/a| 0 0 -1 24 -17 19 .35 35 34 | --- --- --- ---
| 0 1 2 20 27 70 .08 | --- ---
emx n/a| 0 0 9 -39 -48 -14 .28 24 22 | 0 -1733 3741 6984
| 1 1 2 16 11 53 .06 | 0 1520
esx n/a| 0 -1 -1 12 19 14 -.23 20 17 | 4154 -4547 3744 7973
| 0 1 2 14 21 25 .08 | 8780 3199
gfz n/a| 1 1 6 51 89 68 -.20 25 19 | -54016 -3323 3403 6582
| 1 1 1 31 21 46 .07 | 7984 1900
grg n/a| 0 0 -6 1 57 -71 -.23 32 31 | 4322 -3264 3756 7028
| 1 1 6 25 20 70 .06 | 4217 2428
iac n/a| 0 0 -4 -33 -44 -10 .06 20 20 | 2575 -397 3752 7078
| 1 0 1 21 35 86 .05 | 3906 1567
mcc n/a| 7 -5 -4 -3 -116 -121 .06 196 196 | --- --- --- ---
| 10 9 22 101 133 859 .62 | --- ---
Table 1.1905.b GPS week : 1905 MJD: 57579.0-57585.0
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 12 11 12 11 9 9 |
R02 | 10 9 8 7 7 9 6 |
R03 | 7 7 7 7 5 10 8 |
R04 | 5 6 8 7 8 6 6 |
R05 | 15 13 14 16 12 12 14 |
R06 | 11 8 10 10 12 10 11 |
R07 | 7 5 6 7 7 7 5 |
R08 | 8 7 7 9 10 8 7 |
R09 | 7 7 7 8 8 8 7 |
R10 | 8 10 9 9 9 13 8 |
R11 | 7 7 7 9 9 8 7 |
R13 | 8 9 11 9 8 9 7 |
R14 | 20 23 26 21 18 19 20 |
R15 | 10 12 11 9 11 10 10 |
R16 | 14 13 16 17 14 14 16 |
R17 | 11 10 10 12 12 10 10 |
R18 | 7 7 8 9 8 9 8 |
R19 | 14 13 13 15 13 14 15 |
R20 | 16 17 16 16 15 13 14 |
R21 | 10 11 10 9 9 8 11 |
R22 | 10 12 11 11 9 9 11 |
R23 | 10 9 10 11 9 10 9 |
R24 | 15 15 18 15 12 17 16 |
R26 | 27 56 52 67 33 38 34 |
Table 1.1905.c GPS week : 1905 MJD: 57579.0-57585.0
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 1905 0 | 40 -10 240 1337 -966 1975 85.5 1833 1833 | 5444 0
brd 1905 1 | 29 -35 244 267 -1721 2420 85.4 1780 1780 | 6377 0
brd 1905 2 | 0 55 199 73 -184 2063 84.8 1435 1435 | -2267 0
brd 1905 3 | 20 -27 195 470 565 4773 83.1 1385 1385 | -1077 0
brd 1905 4 | 4 -27 98 -179 217 2997 82.0 1426 1426 | 6592 0
brd 1905 5 | 74 13 133 451 911 880 83.2 1507 1507 | 3659 0
brd 1905 6 | -1 -9 171 1195 -277 3892 84.5 1412 1412 | -794 0
-------------+------------------------------------------------------------+----------------
brd 1905 mean| 24 -6 183 516 -207 2714 84.1 1539 1539 | 2562 0
brd 1905 sdev| 27 31 53 560 903 1298 1.3 186 186 | 3832 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 2.1905.0 GPS week: 1905 Day: 0 MJD: 57579
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 0 39 -90 29 .45 31 28 | --- --- --- ---
cof n/a| 0 0 -1 34 -27 52 .24 32 30 | --- --- --- ---
emx n/a| -1 0 9 -40 -40 7 .28 22 21 | 0 -1777 3852 6873
esx n/a| 1 0 -2 10 27 12 -.32 20 15 | 18956 -5790 3852 7456
gfz n/a| 0 1 6 93 112 26 -.20 26 19 | -42434 -3899 3632 6688
grg n/a| 2 0 -12 10 77 -174 -.29 36 33 | 8152 -4906 3872 6967
iac n/a| 0 0 -4 -53 -55 21 .12 20 20 | 5276 -141 3864 7234
mcc n/a| 13 -2 -16 -90 -278 1062 -.29 143 143 | --- --- --- ---
Table 2.1905.1 GPS week: 1905 Day: 1 MJD: 57580
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 -28 101 .50 31 30 | --- --- --- ---
cof n/a| 0 0 -4 4 -17 113 .32 33 32 | --- --- --- ---
emx n/a| -2 0 12 -31 -68 74 .34 25 22 | 0 -2044 3674 5976
esx n/a| 0 -1 0 3 3 48 -.23 20 17 | 3173 -5675 3663 6940
gfz n/a| 0 0 5 57 65 113 -.33 26 20 | -45030 -4176 3369 5763
grg n/a| 1 1 -1 -11 68 -126 -.21 33 30 | 8608 -4077 3666 5736
iac n/a| 1 0 -5 -8 -11 -131 .08 19 19 | 6318 -735 3661 5895
mcc n/a| 7 2 -23 -82 117 -1016 .84 167 167 | --- --- --- ---
Table 2.1905.2 GPS week: 1905 Day: 2 MJD: 57581
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 3 -4 11 -36 64 .52 33 33 | --- --- --- ---
cof n/a| 0 0 -2 21 19 37 .49 34 33 | --- --- --- ---
emx n/a| -1 0 8 -21 -38 -1 .25 24 21 | 0 -2764 3494 6569
esx n/a| 1 -3 -5 8 57 5 -.16 23 19 | -6553 -5133 3507 8080
gfz n/a| 0 0 2 30 107 38 -.19 26 19 | -56337 -4215 3411 6091
grg n/a| -1 -1 1 -10 62 -85 -.35 36 37 | 194 -4788 3526 6484
iac n/a| 3 0 -2 -28 -98 23 .12 20 20 | -1971 -706 3517 6304
mcc n/a| 11 5 -9 -3 -213 -944 .13 157 157 | --- --- --- ---
Table 2.1905.3 GPS week: 1905 Day: 3 MJD: 57582
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| -3 1 0 25 -57 -14 .47 30 29 | --- --- --- ---
cof n/a| 0 0 -1 11 6 -79 .39 34 31 | --- --- --- ---
emx n/a| 0 1 10 -71 -55 -102 .32 26 24 | 0 -3553 3731 7500
esx n/a| 1 -1 0 38 33 -15 -.18 22 21 | -587 -7941 3732 8552
gfz n/a| 1 2 5 79 105 5 -.20 25 17 | -59555 -5992 3400 7324
grg n/a| -1 0 -15 -22 82 -76 -.21 32 32 | 1487 -4930 3764 7457
iac n/a| 0 0 -3 -48 -85 144 .02 22 22 | -787 -2075 3753 7500
mcc n/a| 8 -2 -14 134 -152 -420 -.00 216 216 | --- --- --- ---
Table 2.1905.4 GPS week: 1905 Day: 4 MJD: 57583
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| -5 0 -2 41 -71 -44 .50 33 34 | --- --- --- ---
cof n/a| -2 0 0 8 -51 17 .40 35 35 | --- --- --- ---
emx n/a| 1 -1 10 -38 -42 -6 .35 24 23 | 0 -1105 3802 7928
esx n/a| 0 -1 1 20 7 49 -.35 21 17 | 10788 -3527 3800 8734
gfz n/a| 0 1 7 70 56 131 -.22 24 20 | -55233 -1732 3486 7708
grg n/a| 0 0 -7 -6 31 -72 -.17 25 22 | 7695 -1962 3812 8118
iac n/a| 0 0 -5 -63 -8 -33 .03 18 18 | 6668 -578 3806 8112
mcc n/a| -10 -23 -20 116 -41 -720 .40 270 270 | --- --- --- ---
Table 2.1905.5 GPS week: 1905 Day: 5 MJD: 57584
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 0 10 -9 -23 .41 34 35 | --- --- --- ---
cof n/a| 0 -3 -3 22 -4 -69 .32 38 38 | --- --- --- ---
emx n/a| -2 0 8 -26 -53 -20 .25 26 25 | 0 -2133 3404 6838
esx n/a| 1 -1 0 9 -1 2 -.26 17 16 | 6600 -5849 3395 8181
gfz n/a| 4 0 8 16 90 79 -.15 24 18 | -54105 -3107 3221 6890
grg n/a| 0 0 -2 -3 43 16 -.19 32 28 | 5735 -3903 3419 7046
iac n/a| -2 0 -4 -21 -29 -60 .04 20 20 | 4270 -1407 3412 6829
mcc n/a| 21 -9 13 -121 -193 398 .45 173 173 | --- --- --- ---
Table 2.1905.6 GPS week: 1905 Day: 6 MJD: 57585
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 -1 44 -50 42 .32 36 35 | --- --- --- ---
cof n/a| 0 0 1 65 -49 62 .28 35 36 | --- --- --- ---
emx n/a| 0 0 5 -47 -38 -48 .18 21 20 | 0 1242 4236 7204
esx n/a| 0 0 0 -6 6 -4 -.14 18 15 | -3293 2086 4263 7869
gfz n/a| 2 2 8 13 85 82 -.10 27 20 | -65422 -143 3303 5616
grg n/a| -2 1 -7 55 36 17 -.21 32 38 | -1612 1718 4234 7392
iac n/a| 0 0 -5 -10 -24 -39 -.01 19 19 | -1743 2859 4256 7674
mcc n/a| 1 -5 38 27 -52 793 -1.09 250 250 | --- --- --- ---
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 3.1905.0 GPS week: 1905 Day: 0 MJD: 57579
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 | 941 32 35 17 23 35 35 17 --- 11 | 62 70 72 82 90 79 73 --- 72
R02 | 751 15 22 21 13 30 35 19 --- 9 | 53 48 82 53 58 84 62 --- 62
R03 | 2040 16 23 16 14 26 16 7 196 7 | 68 65 83 76 81 65 72 62 73
R04 | 896 10 12 11 9 11 19 10 --- 5 | 59 60 69 62 65 55 54 --- 60
R05 | 822 20 25 24 28 22 75 21 --- 14 | 51 58 73 67 67 57 63 --- 59
R06 | 1385 31 31 18 12 26 35 30 --- 11 | 62 64 67 51 51 51 60 --- 55
R07 | 1178 13 10 13 13 13 34 9 --- 7 | 75 77 82 75 81 90 74 --- 77
R08 | 733 13 14 14 16 8 38 16 --- 8 | 71 67 71 73 76 83 63 --- 69
R09E | 6003 13 15 16 8 19 13 19 --- 6 | 21 22 17 25 33 26 29 --- 21
R10E | 1011 19 19 15 17 24 24 10 --- 8 | 49 51 58 57 63 63 51 --- 54
R11E | 2222 18 25 14 12 19 19 14 --- 7 | 42 44 35 31 41 31 33 --- 32
R13E | 1670 23 24 15 10 24 30 12 --- 8 | 41 41 25 30 32 26 27 --- 26
R14E | 1275 33 26 48 43 40 67 39 --- 20 | 49 55 38 71 73 45 52 --- 47
XR15E | 7724 13 16 20 18 --- 32 17 --- 10 | 29 32 24 37 --- 22 26 --- 24
R16E | 1160 33 33 33 25 33 41 27 --- 14 | 39 42 30 29 40 38 42 --- 25
R17 | 894 35 42 18 23 21 31 14 --- 10 | 56 60 30 32 24 27 24 --- 25
R18 | 918 20 17 12 12 21 20 9 --- 6 | 42 43 26 39 37 36 29 --- 31
R19 | 1209 64 70 24 19 30 27 17 --- 14 | 71 78 24 31 39 28 24 --- 25
R20 | 859 56 51 22 24 46 49 27 --- 16 | 64 65 31 49 57 38 35 --- 32
R21 | 1041 42 47 17 16 26 21 14 51 10 | 62 65 30 37 35 26 28 76 30
R22 | 661 48 44 17 9 23 13 17 --- 10 | 61 61 32 26 24 26 27 --- 26
R23 | 2806 24 23 21 27 13 34 16 --- 10 | 30 32 36 62 47 41 50 --- 42
R24 | 1410 18 31 37 34 25 44 37 --- 15 | 41 63 55 60 55 41 50 --- 44
XR26 | ---- 39 155 --- --- --- --- 16 --- 27 | 69 248 --- --- --- --- 33 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1833 31 32 22 20 26 36 20 143 |T 52 62 47 50 53 46 45 69 43
WRMS | 1833 28 30 21 15 19 33 20 143 |NE 58 72 53 54 55 51 48 69 48
MEDI | 1160 20 25 17 16 24 32 16 51 |MD 53 60 36 51 51 41 42 62 41
Table 3.1905.1 GPS week: 1905 Day: 1 MJD: 57580
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 | 949 15 36 15 37 30 34 22 --- 12 | 45 62 39 41 54 44 42 --- 37
R02 | 749 16 16 15 19 21 34 12 --- 8 | 39 44 50 39 37 52 39 --- 39
R03 | 1550 24 22 10 11 25 13 8 115 7 | 48 44 54 54 49 60 51 36 49
R04 | 1014 10 16 15 12 18 11 9 --- 5 | 47 49 54 55 48 43 39 --- 46
R05 | 634 36 38 18 32 31 47 14 --- 13 | 41 46 60 64 51 54 54 --- 53
R06 | 772 27 35 18 9 8 18 20 --- 8 | 43 43 45 46 41 37 33 --- 38
R07 | 1282 12 15 13 9 9 14 12 255 5 | 51 49 54 44 54 49 42 181 46
R08 | 1322 20 18 12 16 11 21 10 --- 6 | 45 49 44 46 50 63 41 --- 44
R09E | 5830 19 15 21 9 16 13 14 --- 7 | 21 23 21 28 32 26 26 --- 23
R10E | 1066 22 22 22 20 21 28 17 --- 9 | 38 39 46 44 54 53 30 --- 40
R11E | 1426 18 24 15 16 21 19 10 --- 7 | 35 41 34 29 35 24 28 --- 27
R13E | 1841 22 24 19 13 18 32 11 --- 8 | 41 41 29 28 29 35 32 --- 27
R14E | 1965 35 28 64 26 60 82 38 --- 23 | 60 63 66 74 100 79 71 --- 66
XR15E |14016 16 22 24 27 --- 22 22 --- 11 | 32 42 32 37 --- 27 25 --- 26
R16E | 1543 23 40 34 17 25 38 28 --- 12 | 36 54 30 34 43 35 41 --- 28
R17 | 1391 42 42 15 14 19 30 11 --- 10 | 52 52 25 29 30 24 18 --- 24
R18 | 767 16 20 17 15 16 17 9 --- 6 | 33 40 29 31 27 29 23 --- 26
R19 | 876 56 59 27 15 31 17 17 --- 12 | 55 60 24 36 35 34 25 --- 26
R20 | 770 54 50 32 38 40 46 25 --- 17 | 47 56 32 56 60 32 38 --- 34
R21 | 871 46 41 19 12 26 17 16 72 10 | 53 50 26 29 27 27 24 65 24
R22 | 778 49 56 23 11 30 25 13 --- 11 | 55 60 30 20 27 34 21 --- 23
R23 | 2081 27 32 16 25 11 21 15 --- 9 | 26 25 28 45 31 25 33 --- 29
R24 | 2000 24 30 41 23 25 46 35 --- 15 | 40 46 61 42 47 36 37 --- 35
XR26 | ---- 78 288 --- --- --- --- 40 --- 56 | 124 350 --- --- --- --- 27 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1779 31 33 25 20 26 33 18 167 |T 46 59 39 41 43 40 35 94 35
WRMS | 1779 30 32 22 17 20 30 18 167 |NE 49 66 40 42 41 40 34 94 36
MEDI | 1282 23 28 18 16 21 22 14 115 |MD 43 46 34 41 41 35 33 65 34
Table 3.1905.2 GPS week: 1905 Day: 2 MJD: 57581
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 | 1320 23 26 20 28 24 35 19 --- 11 | 56 71 63 55 67 73 58 --- 58
R02 | 657 16 18 17 21 18 23 13 --- 8 | 48 44 62 50 48 62 58 --- 53
R03 | 860 11 12 15 13 21 21 16 108 7 | 49 55 65 56 59 50 59 17 55
R04 | 785 13 16 17 12 21 34 11 --- 8 | 48 45 59 47 42 78 46 --- 49
R05 | 949 46 24 28 25 26 54 14 --- 14 | 56 79 89 83 69 78 79 --- 74
R06 | 819 31 30 11 21 19 33 16 --- 9 | 47 52 46 43 60 65 34 --- 45
R07 | 1044 12 24 8 16 12 16 14 247 6 | 48 56 62 57 66 54 60 41 57
R08 | 802 10 9 12 21 10 16 15 --- 6 | 54 50 51 52 50 55 53 --- 50
R09E | 3785 20 20 18 13 11 14 14 --- 6 | 21 25 16 24 28 25 24 --- 18
R10E | 1145 28 26 19 15 11 22 22 --- 9 | 52 56 63 59 62 67 51 --- 56
R11E | 988 14 18 17 17 18 13 16 --- 7 | 31 33 34 31 38 26 29 --- 27
R13E | 2669 24 25 30 15 18 36 22 --- 11 | 38 37 35 28 30 22 33 --- 25
R14E | 2226 39 38 66 52 68 73 43 --- 25 | 35 56 39 73 87 36 49 --- 36
XR15E |14394 23 24 14 24 --- 31 19 --- 11 | 40 42 25 36 --- 38 29 --- 26
R16E | 740 44 51 26 30 41 40 30 --- 15 | 46 45 35 42 63 34 42 --- 33
R17 | 1105 42 46 16 15 19 25 19 --- 10 | 56 59 27 35 28 37 21 --- 27
R18 | 786 24 24 14 16 19 19 12 --- 7 | 38 39 26 28 19 24 28 --- 23
R19 | 1430 63 56 26 11 27 14 17 --- 13 | 57 58 24 33 41 36 34 --- 28
R20 | 684 50 65 25 32 35 51 27 --- 16 | 65 73 35 38 48 38 40 --- 33
R21 | 793 43 46 15 15 24 19 13 40 10 | 53 58 31 38 33 33 33 45 31
R22 | 1306 48 47 15 9 28 23 16 --- 10 | 59 58 31 32 33 33 28 --- 28
R23 | 1060 24 15 14 26 10 28 22 --- 9 | 27 31 29 49 36 22 39 --- 31
R24 | 1193 31 30 33 32 25 81 26 --- 17 | 45 50 39 48 35 47 36 --- 30
XR26 | ---- 70 365 --- --- --- --- 39 --- 52 | 112 346 --- --- --- --- 37 --- 57
------+---------------------------------------------------+-----------------------------------------------
RMS | 1435 33 34 24 23 26 36 20 157 |T 49 63 42 45 47 44 41 34 39
WRMS | 1435 33 33 21 19 19 37 20 157 |NE 54 72 46 46 45 49 43 34 42
MEDI | 1044 24 25 17 17 19 25 16 108 |MD 48 52 35 43 42 38 37 41 33
Table 3.1905.3 GPS week: 1905 Day: 3 MJD: 57582
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 | 2403 21 21 30 27 30 28 25 --- 12 | 52 46 71 53 60 42 66 --- 53
R02 | 529 14 14 14 18 17 19 13 --- 7 | 49 53 64 52 78 64 60 --- 60
R03 | 659 7 11 17 15 9 24 14 99 6 | 59 55 63 50 58 60 55 19 55
R04 | 809 10 12 13 13 11 25 15 --- 6 | 43 47 56 50 50 34 43 --- 45
R05 | 1245 38 44 34 41 21 50 20 --- 15 | 48 56 82 83 52 35 56 --- 58
R06 | 884 29 35 11 20 14 28 26 --- 9 | 46 47 45 59 45 43 33 --- 43
R07 | 1477 11 11 13 13 9 27 17 357 7 | 60 59 74 69 68 41 65 84 63
R08 | 780 17 20 14 14 16 47 8 --- 9 | 57 59 57 55 58 24 50 --- 48
R09E | 1743 17 22 24 11 14 19 18 --- 8 | 30 39 29 30 36 32 29 --- 25
R10E | 1394 19 24 15 21 13 23 26 --- 9 | 39 40 41 54 52 50 44 --- 44
R11E | 812 19 20 17 15 28 23 16 --- 9 | 33 34 31 30 36 35 28 --- 27
R13E | 2629 23 33 21 13 20 22 14 --- 8 | 34 38 28 26 32 36 29 --- 24
R14E | 1018 36 20 65 36 44 46 41 --- 20 | 72 82 67 96 104 78 85 --- 79
XR15E | 8612 17 24 15 14 --- 26 16 --- 9 | 37 42 31 33 --- 29 25 --- 26
R16E | 925 32 54 34 23 49 54 32 --- 17 | 49 54 46 31 51 27 43 --- 26
R17 | 880 47 51 29 13 28 21 15 --- 12 | 63 67 31 36 29 32 24 --- 29
R18 | 793 27 33 16 16 17 23 14 --- 8 | 42 45 32 38 32 31 27 --- 28
R19 | 1750 62 69 20 23 30 31 21 --- 14 | 61 70 32 37 31 36 34 --- 26
R20 | 1597 41 48 24 34 40 44 34 --- 16 | 60 71 29 41 54 51 37 --- 33
R21 | 822 37 34 16 13 21 16 14 47 9 | 54 53 28 30 32 32 28 33 27
R22 | 1362 47 50 18 8 23 21 19 --- 11 | 62 66 33 31 26 35 27 --- 27
R23 | 1169 22 26 33 25 15 29 16 --- 10 | 27 33 28 52 47 36 45 --- 35
R24 | 2127 23 23 37 33 23 42 33 --- 14 | 45 50 53 49 47 29 38 --- 33
XR26 | ---- 83 112 --- --- --- --- 52 --- 66 | 121 148 --- --- --- --- 23 --- 53
------+---------------------------------------------------+-----------------------------------------------
RMS | 1384 30 34 26 22 25 32 22 216 |T 51 56 45 47 49 39 41 45 40
WRMS | 1384 29 31 24 21 17 32 22 216 |NE 55 60 48 49 47 39 41 45 42
MEDI | 1169 23 24 18 16 20 26 17 99 |MD 49 53 41 49 47 35 37 33 33
Table 3.1905.4 GPS week: 1905 Day: 4 MJD: 57583
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 | 1566 17 18 30 27 21 32 17 --- 11 | 49 46 61 47 53 32 57 --- 44
R02 | 696 15 16 18 15 19 19 12 --- 7 | 47 45 60 54 62 50 47 --- 51
R03 | 872 9 9 10 9 14 11 11 120 5 | 52 58 58 54 68 64 49 45 55
R04 | 2070 13 13 23 11 27 11 12 --- 7 | 41 40 48 34 40 36 26 --- 34
R05 | 1252 28 47 29 30 13 38 17 --- 12 | 34 30 68 59 46 28 44 --- 45
R06 | 1374 34 27 33 27 30 21 10 --- 11 | 35 37 55 37 37 45 32 --- 36
R07 | 1021 22 21 15 15 16 17 11 449 7 | 57 59 64 73 67 67 57 138 63
R08 | 1134 20 16 14 22 15 36 11 --- 9 | 46 53 56 71 66 34 63 --- 55
R09E | 1022 23 23 20 16 17 20 17 --- 8 | 29 33 32 31 30 31 28 --- 26
R10E | 1406 25 33 21 12 15 24 23 --- 9 | 33 41 37 33 30 33 28 --- 27
R11E | 1192 29 33 16 13 19 24 14 --- 8 | 37 44 27 35 30 25 29 --- 27
R13E | 2678 21 25 22 13 23 21 10 --- 8 | 33 40 23 27 31 27 26 --- 23
R14E | 935 42 39 54 32 43 32 36 --- 17 | 46 56 39 75 72 48 55 --- 49
XR15E | 9109 17 22 27 22 --- 23 15 --- 10 | 39 37 31 38 --- 36 33 --- 31
R16E | 914 37 48 24 24 38 27 33 --- 13 | 39 48 29 36 47 33 46 --- 27
R17 | 736 52 59 28 11 28 23 14 --- 11 | 55 60 32 21 26 30 19 --- 20
R18 | 949 31 30 13 16 20 22 10 --- 8 | 38 40 21 30 19 17 25 --- 20
R19 | 1453 65 63 22 18 26 28 16 --- 13 | 54 52 25 29 34 38 26 --- 22
R20 | 2020 43 35 29 33 32 35 31 --- 15 | 48 54 43 44 53 39 39 --- 34
R21 | 792 38 36 18 16 22 16 10 51 9 | 45 45 23 29 34 25 25 36 23
R22 | 1185 48 51 18 9 19 13 9 --- 9 | 55 58 29 25 27 29 22 --- 25
R23 | 2155 24 32 23 23 11 18 13 --- 8 | 29 29 32 47 33 34 37 --- 33
R24 | 1816 27 27 22 28 37 29 21 --- 12 | 42 47 36 45 45 39 33 --- 29
XR26 | ---- 51 102 --- --- --- --- 21 --- 33 | 76 198 --- --- --- --- 42 --- 46
------+---------------------------------------------------+-----------------------------------------------
RMS | 1425 33 35 24 21 24 25 18 270 |T 44 52 40 42 43 36 37 73 35
WRMS | 1425 34 35 23 17 20 22 18 270 |NE 47 55 44 43 44 37 37 73 37
MEDI | 1192 27 30 22 16 20 23 14 120 |MD 42 45 36 37 37 34 33 45 31
Table 3.1905.5 GPS week: 1905 Day: 5 MJD: 57584
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 | 1038 23 26 22 19 19 20 17 --- 8 | 41 40 49 53 65 47 60 --- 51
R02 | 509 12 18 21 15 15 38 10 --- 8 | 35 28 44 29 43 21 31 --- 29
R03 | 736 16 18 24 9 12 48 9 157 9 | 43 43 49 40 38 20 34 66 34
R04 | 2686 18 19 16 7 11 10 13 --- 5 | 34 34 40 32 39 29 24 --- 30
R05 | 1933 22 16 31 20 22 44 21 --- 11 | 33 35 51 38 48 60 29 --- 36
R06 | 1467 38 46 32 15 17 21 12 --- 9 | 31 32 48 24 32 42 29 --- 30
R07 | 774 18 19 14 14 15 17 11 227 6 | 46 46 58 53 46 53 52 116 50
R08 | 1363 25 38 14 17 13 28 10 --- 7 | 38 37 50 64 50 34 48 --- 48
R09E | 1318 17 23 20 12 20 23 12 --- 7 | 22 21 22 22 28 15 25 --- 18
R10E | 2791 21 28 17 18 29 47 35 --- 13 | 46 47 44 57 65 53 33 --- 45
R11E | 1293 27 36 20 12 15 22 16 --- 8 | 39 50 33 27 31 28 32 --- 27
R13E | 2542 25 25 23 9 19 31 11 --- 8 | 38 38 24 27 30 26 28 --- 24
R14E | 1405 46 34 45 29 38 50 46 --- 18 | 66 71 67 85 83 71 76 --- 68
XR15E | 6657 13 26 16 24 --- 27 15 --- 10 | 31 35 26 35 --- 38 30 --- 29
R16E | 674 36 40 33 23 31 29 37 --- 14 | 37 37 24 37 44 36 44 --- 30
R17 | 960 47 52 22 12 23 29 11 --- 10 | 50 54 30 31 27 22 22 --- 24
R18 | 820 35 41 13 17 25 17 13 --- 8 | 40 46 24 31 24 29 25 --- 23
R19 | 674 70 69 32 9 32 24 14 --- 13 | 58 60 33 23 31 25 26 --- 23
R20 | 1828 41 76 34 19 25 39 22 --- 12 | 41 73 44 37 31 38 29 --- 26
R21 | 817 40 42 15 9 20 11 11 115 8 | 46 48 22 27 23 24 27 35 24
R22 | 871 46 45 21 11 21 14 14 --- 9 | 49 47 25 24 25 29 24 --- 23
R23 | 1596 34 31 20 21 20 31 10 --- 10 | 28 31 39 49 44 28 36 --- 38
R24 | 1751 31 33 43 31 45 53 23 --- 16 | 48 52 45 43 43 28 36 --- 33
XR26 | ---- 58 791 --- --- --- --- 25 --- 38 | 86 538 --- --- --- --- 30 --- 40
------+---------------------------------------------------+-----------------------------------------------
RMS | 1507 34 38 26 17 24 32 20 173 |T 42 64 38 38 40 34 34 72 33
WRMS | 1507 35 38 25 16 18 28 20 173 |NE 43 73 40 37 38 33 33 72 33
MEDI | 1318 27 33 21 15 20 28 13 157 |MD 40 43 40 35 38 29 30 66 30
Table 3.1905.6 GPS week: 1905 Day: 6 MJD: 57585
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 | 939 36 26 14 16 33 21 12 --- 9 | 60 65 78 73 104 86 83 --- 78
R02 | 586 23 21 9 10 19 18 9 --- 6 | 62 63 76 72 84 60 65 --- 68
R03 | 943 14 18 18 11 13 32 9 207 7 | 71 71 75 64 68 47 63 59 64
R04 | 1624 11 13 17 9 10 15 9 --- 5 | 56 57 62 52 53 48 46 --- 51
R05 | 2353 25 25 30 20 30 57 27 --- 14 | 46 52 69 59 62 68 50 --- 54
R06 | 1289 25 21 32 14 27 23 23 --- 10 | 55 55 68 47 52 60 42 --- 51
R07 | 1332 7 11 10 11 11 13 13 331 5 | 78 80 87 86 79 81 76 104 81
R08 | 944 15 10 20 14 12 22 9 --- 7 | 63 65 74 67 68 54 66 --- 65
R09E | 1485 17 19 17 11 15 22 12 --- 7 | 33 36 25 33 35 29 35 --- 29
R10E | 2506 24 26 18 13 13 21 16 --- 7 | 48 49 59 58 60 58 45 --- 52
R11E | 1706 24 26 17 10 16 16 10 --- 6 | 38 38 30 32 25 28 31 --- 28
R13E | 2269 25 29 17 11 16 22 9 --- 7 | 38 42 25 31 27 39 30 --- 28
R14E | 971 47 38 32 37 55 67 36 --- 19 | 71 67 51 67 75 73 65 --- 55
XR15E | 5331 15 16 15 23 --- 29 14 --- 10 | 34 40 30 49 --- 40 35 --- 36
R16E | 989 68 64 33 25 40 30 33 --- 16 | 51 59 32 42 56 35 47 --- 37
R17 | 1065 42 41 19 13 25 25 16 --- 9 | 60 59 36 28 24 22 20 --- 25
R18 | 823 35 35 14 14 24 15 12 --- 8 | 48 47 28 37 28 34 25 --- 28
R19 | 931 74 77 26 14 37 38 22 --- 15 | 66 70 26 25 40 35 24 --- 22
R20 | 852 47 23 23 32 28 33 26 --- 13 | 50 42 30 29 35 28 35 --- 22
R21 | 865 47 55 17 15 28 23 18 187 10 | 54 60 18 23 28 25 28 39 20
R22 | 1159 45 47 22 15 28 21 16 --- 10 | 55 57 34 31 25 26 26 --- 25
R23 | 877 20 31 16 22 11 31 11 --- 8 | 32 30 31 58 43 30 48 --- 41
R24 | 2120 32 34 23 24 37 66 33 --- 15 | 57 58 37 49 45 44 43 --- 38
XR26 | ---- 55 1413 --- --- --- --- 19 --- 33 | 68 839 --- --- --- --- 33 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1412 36 35 21 18 27 32 19 250 |T 53 87 47 48 50 45 44 67 43
WRMS | 1412 35 36 20 15 20 38 19 250 |NE 57 104 51 50 52 46 45 67 45
MEDI | 1065 25 26 18 14 24 23 14 207 |MD 55 57 36 49 45 40 42 59 37
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