[IGSREPORT-24693] Wk 1909 IGLOS Final Orbits
IGS ACC
acc at igs.org
Mon Aug 29 04:31:05 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1909 (Aug 07, 2016 - Aug 13, 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 2.1909.
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:
igl1909[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1909 in the SP3 format.
igl19097.sum Combination Report for GPS Week 1909.
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 | 59.0 ns
1 | 54.4 ns
2 | 50.3 ns
3 | 50.8 ns
4 | 44.4 ns
5 | 42.8 ns
6 | 45.0 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 1.1909, 1a.1909).
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 2.1909.0-6)
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 3.1909.0-6).
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 1909 summary. (Aug 07, 2016 - Aug 13, 2016)
Table 1.1909.a GPS week : 1909 MJD: 57607.0-57613.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 6 46 -39 21 .23 33 34 | --- --- --- ---
| 2 2 3 25 40 16 .04 | --- ---
cof n/a| 0 1 6 55 -18 38 .25 37 36 | --- --- --- ---
| 1 0 3 14 21 17 .05 | --- ---
emx n/a| -1 0 9 -61 -47 8 .20 25 25 | 45365 -677 4159 7437
| 1 1 2 31 37 51 .05 | 11575 1572
esx n/a| 0 0 -2 -13 21 -19 -.18 18 15 | 47090 -2543 4174 7992
| 1 1 1 23 24 40 .03 | 4213 3277
gfz n/a| 0 0 -1 27 75 66 .08 25 21 | 0 -494 3843 7244
| 1 1 1 39 39 64 .05 | 0 3266
grg n/a| 0 0 -4 40 0 14 -.23 31 29 | 49543 -231 4170 7321
| 2 1 5 36 25 71 .05 | 5045 2852
iac n/a| 1 0 -2 0 -6 -51 .09 21 21 | 50444 -220 4179 7533
| 1 1 2 30 47 54 .04 | 5230 1049
mcc n/a| 0 3 5 25 -103 423 -.48 90 90 | --- --- --- ---
| 5 7 18 89 108 442 .20 | --- ---
Table 1.1909.b GPS week : 1909 MJD: 57607.0-57613.0
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 13 9 13 14 16 13 |
R02 | 8 9 9 7 8 10 12 |
R03 | 8 8 11 8 8 10 12 |
R04 | 8 8 7 10 7 7 9 |
R05 | 14 12 12 12 12 14 16 |
R06 | 9 10 12 11 9 12 12 |
R07 | 10 9 9 10 10 9 11 |
R08 | 10 8 9 9 11 9 10 |
R09 | 9 7 9 9 7 7 8 |
R10 | 8 8 7 9 9 10 11 |
R11 | 6 7 8 8 8 7 8 |
R13 | 10 8 9 8 8 7 9 |
R14 | 15 14 18 19 14 15 16 |
R15 | 11 10 13 11 12 10 11 |
R16 | 12 12 13 13 11 12 14 |
R17 | 11 13 10 9 11 11 12 |
R18 | 9 10 10 9 10 9 9 |
R19 | 15 13 15 14 12 13 14 |
R20 | 15 15 17 13 16 14 14 |
R21 | 10 11 11 10 13 12 9 |
R22 | 9 9 13 12 11 11 11 |
R23 | 9 9 9 9 8 8 8 |
R24 | 15 18 18 17 16 15 14 |
Table 1.1909.c GPS week : 1909 MJD: 57607.0-57613.0
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 1909 0 | 13 -10 149 1000 -136 1401 84.0 1768 1768 | 58994 0
brd 1909 1 | 24 -43 159 -898 -274 -2611 84.4 1565 1565 | 54415 0
brd 1909 2 | -50 34 102 -295 545 -2268 86.3 1692 1692 | 50275 0
brd 1909 3 | -4 -3 217 -115 -803 -609 85.6 1973 1973 | 50779 0
brd 1909 4 | 38 -14 148 268 290 983 82.6 2412 2412 | 44413 0
brd 1909 5 | 22 -36 182 1444 682 -971 84.6 2397 2397 | 42826 0
brd 1909 6 | -12 19 239 1460 277 3796 85.0 1804 1804 | 44957 0
-------------+------------------------------------------------------------+----------------
brd 1909 mean| 4 -7 171 409 83 -39 84.7 1944 1944 | 49522 0
brd 1909 sdev| 29 27 46 915 518 2258 1.2 337 337 | 5881 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 2.1909.0 GPS week: 1909 Day: 0 MJD: 57607
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 2 2 77 -22 25 .23 34 36 | --- --- --- ---
cof n/a| -1 1 4 50 -2 21 .29 36 38 | --- --- --- ---
emx n/a| -2 0 12 -117 -48 45 .15 25 25 | 55155 1022 4213 8180
esx n/a| 2 0 -3 4 2 12 -.21 17 14 | 48577 -235 4219 8572
gfz n/a| 0 0 0 29 89 76 .07 24 21 | 0 1743 3879 8107
grg n/a| 0 0 -9 4 24 23 -.26 31 30 | 57624 2440 4196 7964
iac n/a| 2 0 -1 20 -24 -120 .16 21 21 | 57749 448 4215 8317
mcc n/a| 12 2 -3 90 -24 96 -.66 115 115 | --- --- --- ---
Table 2.1909.1 GPS week: 1909 Day: 1 MJD: 57608
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 0 6 26 -41 28 .18 32 34 | --- --- --- ---
cof n/a| -1 0 2 56 -13 30 .21 36 35 | --- --- --- ---
emx n/a| 1 -2 9 -37 -49 -11 .13 22 20 | 61557 1634 4585 7218
esx n/a| 0 0 -3 9 48 -20 -.16 17 15 | 51936 1395 4560 7634
gfz n/a| -1 1 0 31 0 199 .11 30 30 | 0 3333 4167 6839
grg n/a| 1 1 -2 55 21 38 -.29 29 27 | 52812 3016 4583 7198
iac n/a| 0 0 -4 -16 1 -104 .07 21 21 | 56210 639 4581 7191
mcc n/a| -4 18 6 48 -27 -233 -.35 86 86 | --- --- --- ---
Table 2.1909.2 GPS week: 1909 Day: 2 MJD: 57609
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 4 78 -101 52 .23 33 32 | --- --- --- ---
cof n/a| 0 0 3 59 -47 57 .29 36 33 | --- --- --- ---
emx n/a| -1 1 10 -53 -11 -64 .21 27 27 | 37461 -2058 3819 5792
esx n/a| 1 -1 0 -44 43 -107 -.19 19 17 | 46211 -3987 3816 6911
gfz n/a| -1 0 0 39 73 48 .08 24 21 | 0 -2167 3597 5724
grg n/a| 0 0 -3 21 -35 131 -.20 35 31 | 51167 -2011 3826 5939
iac n/a| 2 0 -6 21 -10 25 .06 21 21 | 51559 -988 3825 5912
mcc n/a| -3 0 20 174 -70 215 -.42 65 65 | --- --- --- ---
Table 2.1909.3 GPS week: 1909 Day: 3 MJD: 57610
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 2 32 -84 11 .25 34 33 | --- --- --- ---
cof n/a| 0 2 4 69 -49 44 .27 38 35 | --- --- --- ---
emx n/a| 0 0 10 -28 -64 63 .23 27 28 | 52472 -1140 3614 6193
esx n/a| 0 0 -4 -46 39 -9 -.19 18 15 | 53089 -7047 3596 7495
gfz n/a| -1 1 0 90 99 68 .06 24 17 | 0 1174 3298 5982
grg n/a| 0 0 2 83 21 -57 -.24 30 27 | 50830 -184 3584 6114
iac n/a| 0 -1 -3 -43 -9 -36 .11 21 21 | 51191 -885 3599 6059
mcc n/a| -3 0 -2 -43 -81 538 -.42 79 79 | --- --- --- ---
Table 2.1909.4 GPS week: 1909 Day: 4 MJD: 57611
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 1 7 51 -1 10 .23 35 34 | --- --- --- ---
cof n/a| 0 2 10 58 -18 33 .20 39 36 | --- --- --- ---
emx n/a| -2 -1 9 -83 -110 69 .26 28 28 | 34113 -30 4362 7586
esx n/a| 0 1 -2 7 -13 -12 -.23 16 15 | 43094 966 4348 8280
gfz n/a| -1 0 -1 28 53 46 .14 22 14 | 0 1663 3955 7378
grg n/a| 1 0 -3 8 -16 -50 -.23 27 25 | 43396 2208 4335 7596
iac n/a| 0 -1 -1 -33 83 -91 .09 21 21 | 45436 1416 4354 7607
mcc n/a| 4 0 -25 -82 -4 776 -.82 108 108 | --- --- --- ---
Table 2.1909.5 GPS week: 1909 Day: 5 MJD: 57612
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 3 7 9 6 20 .18 33 35 | --- --- --- ---
cof n/a| 1 1 9 27 -9 61 .20 40 38 | --- --- --- ---
emx n/a| -3 0 8 -74 -58 -11 .18 21 21 | 31009 -2307 3694 9031
esx n/a| 0 -1 -1 -18 1 8 -.14 18 16 | 42946 -3523 3834 8978
gfz n/a| 1 -1 -2 15 115 32 -.01 27 22 | 0 -4170 3632 9292
grg n/a| 0 2 -13 91 4 -51 -.14 33 31 | 44556 -3711 3828 8704
iac n/a| 2 0 0 31 -7 -33 .07 20 20 | 44646 -1417 3838 9605
mcc n/a| 1 9 13 -41 -240 476 -.50 92 92 | --- --- --- ---
Table 2.1909.6 GPS week: 1909 Day: 6 MJD: 57613
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 5 12 47 -30 2 .28 32 35 | --- --- --- ---
cof n/a| 0 1 10 70 7 18 .32 33 35 | --- --- --- ---
emx n/a| -2 -2 5 -36 6 -28 .22 24 25 | 45790 -1866 4830 8065
esx n/a| 0 1 -1 -6 28 -5 -.18 19 15 | 43781 -5370 4849 8080
gfz n/a| 0 1 -3 -42 101 -4 .10 27 22 | 0 -5034 4378 7387
grg n/a| -4 -2 -1 18 -27 65 -.25 35 36 | 46416 -3377 4838 7732
iac n/a| 0 2 -1 19 -79 -2 .07 24 24 | 46319 -756 4844 8042
mcc n/a| 0 -2 30 34 -273 1095 -.23 87 87 | --- --- --- ---
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 3.1909.0 GPS week: 1909 Day: 0 MJD: 57607
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 | 861 41 42 43 18 26 30 37 --- 14 | 83 81 82 47 40 61 35 --- 51
R02 | 1256 33 29 21 10 18 19 14 --- 8 | 72 71 67 47 45 46 40 --- 49
R03 | 703 26 33 23 7 16 24 16 134 8 | 83 85 86 61 55 57 52 93 63
R04 | 664 23 32 21 12 22 15 8 --- 7 | 69 74 77 48 41 51 54 --- 54
R05 | 619 35 38 31 18 21 50 33 --- 14 | 65 67 70 42 48 58 32 --- 46
R06 | 3463 20 19 26 13 15 33 18 --- 9 | 48 50 59 33 33 33 36 --- 38
R07 | 1703 23 28 29 13 12 31 18 112 9 | 75 78 80 52 56 45 49 42 56
R08 | 544 24 25 23 18 11 34 25 --- 10 | 72 71 70 64 59 48 42 --- 56
R09E | 2834 18 14 16 14 23 26 17 --- 8 | 16 18 17 29 34 23 24 --- 20
R10E | 995 9 15 18 18 18 22 19 --- 8 | 45 44 43 51 51 47 47 --- 45
R11E | 1022 12 13 13 10 20 17 10 --- 6 | 27 29 24 25 34 28 25 --- 23
R13E | 2356 18 16 28 13 35 23 18 --- 10 | 41 41 45 42 47 37 32 --- 38
R14E | 3213 31 36 42 38 25 31 25 --- 15 | 68 78 77 57 65 60 56 --- 56
XR15E | 6983 23 25 21 21 --- 24 15 --- 10 | 101 101 92 100 --- 95 99 --- 97
R16E | 1193 38 40 33 27 15 24 24 --- 12 | 42 44 41 41 37 35 40 --- 33
R17 | 666 52 58 15 9 22 21 21 --- 10 | 75 78 46 35 23 40 22 --- 34
R18 | 958 28 27 16 15 25 17 20 --- 9 | 53 54 47 34 28 42 25 --- 34
R19 | 688 66 69 19 17 36 35 28 --- 15 | 82 83 41 32 30 44 23 --- 34
R20 | 885 54 63 21 14 31 59 30 --- 15 | 66 75 23 29 29 47 24 --- 26
R21 | 845 42 47 12 11 25 24 13 97 9 | 68 70 48 34 32 46 36 40 39
R22 | 1255 36 32 20 10 21 25 17 --- 9 | 62 61 48 33 25 40 26 --- 33
R23 | 4146 20 16 21 14 11 34 12 --- 8 | 28 32 41 41 36 27 31 --- 32
R24 | 701 30 23 30 21 43 51 20 --- 14 | 45 54 40 51 32 40 32 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 1768 34 36 25 17 24 31 21 115 |T 60 62 54 44 40 45 38 58 43
WRMS | 1768 36 38 25 14 21 30 21 115 |NE 65 67 57 42 38 45 34 58 42
MEDI | 995 28 29 21 14 21 25 18 112 |MD 66 70 48 42 36 45 35 42 38
Table 3.1909.1 GPS week: 1909 Day: 1 MJD: 57608
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 | 1134 31 24 22 22 43 32 26 --- 12 | 62 57 58 65 46 43 37 --- 49
R02 | 1747 27 32 21 14 26 23 15 --- 9 | 45 50 48 43 22 26 29 --- 35
R03 | 646 28 24 19 13 14 20 19 112 8 | 52 48 53 53 59 50 38 68 48
R04 | 617 20 18 20 15 16 14 15 --- 7 | 47 42 50 38 40 47 40 --- 40
R05 | 920 35 42 25 18 35 29 29 --- 12 | 42 53 44 30 51 37 31 --- 33
R06 | 1884 32 30 24 16 21 19 18 --- 9 | 36 32 42 28 29 28 26 --- 28
R07 | 1517 28 15 25 12 23 17 20 86 9 | 54 42 58 36 50 36 32 40 41
R08 | 517 22 27 12 15 21 21 17 --- 8 | 51 55 46 59 47 34 38 --- 46
R09E | 3758 12 12 16 11 23 18 12 --- 6 | 20 22 17 25 42 23 23 --- 19
R10E | 883 15 33 19 17 24 24 10 --- 8 | 41 54 47 52 52 50 46 --- 46
R11E | 804 15 15 12 12 18 24 9 --- 6 | 30 29 22 23 30 24 21 --- 20
R13E | 856 20 18 15 13 22 25 12 --- 7 | 35 33 33 34 42 37 27 --- 31
R14E | 3636 26 27 29 31 38 16 33 --- 13 | 57 62 44 75 63 70 48 --- 55
XR15E | 4843 17 19 18 18 --- 31 15 --- 10 | 126 126 126 122 --- 133 128 --- 126
R16E | 1224 31 48 22 21 25 35 29 --- 12 | 37 52 28 38 29 43 30 --- 26
R17 | 1255 49 51 21 16 37 34 22 --- 12 | 49 51 32 29 26 45 18 --- 25
R18 | 640 27 27 16 11 38 25 21 --- 9 | 36 37 29 30 23 38 18 --- 24
R19 | 562 62 56 17 15 36 25 23 --- 13 | 54 52 29 30 39 31 18 --- 26
R20 | 968 46 42 31 30 29 33 32 --- 14 | 46 40 29 36 27 34 25 --- 21
R21 | 927 42 48 20 11 43 18 18 47 11 | 43 49 32 26 29 30 27 30 25
R22 | 1418 33 39 18 10 31 16 19 --- 9 | 41 48 33 24 25 31 23 --- 26
R23 | 1948 23 32 20 21 18 20 15 --- 8 | 21 21 24 39 42 24 36 --- 30
R24 | 908 29 64 39 18 46 78 19 --- 18 | 43 77 57 34 28 26 31 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1564 32 36 22 17 30 29 21 86 |T 46 49 42 42 38 40 34 46 37
WRMS | 1564 34 35 20 15 30 27 21 86 |NE 45 47 41 37 36 35 29 46 33
MEDI | 968 28 30 20 15 25 24 19 86 |MD 43 49 42 36 39 36 30 40 31
Table 3.1909.2 GPS week: 1909 Day: 2 MJD: 57609
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 | 1457 28 32 19 11 23 27 16 --- 9 | 66 72 53 70 62 53 57 --- 58
R02 | 1623 14 16 14 20 11 25 22 --- 8 | 57 56 62 74 55 47 40 --- 55
R03 | 675 23 24 27 17 13 33 27 88 10 | 56 58 67 60 44 22 23 43 44
R04 | 623 23 26 18 6 16 13 20 --- 7 | 45 47 48 39 41 38 25 --- 36
R05 | 2025 29 30 30 25 23 17 28 --- 11 | 57 51 51 56 55 36 26 --- 41
R06 | 1309 30 34 33 14 19 43 20 --- 11 | 37 43 51 27 27 30 26 --- 26
R07 | 1152 27 33 23 10 19 16 22 61 8 | 50 55 52 46 32 44 26 29 37
R08 | 908 26 23 15 20 23 18 20 --- 9 | 54 52 43 60 41 53 33 --- 44
R09E | 4325 20 18 26 15 25 22 15 --- 9 | 20 19 17 27 39 25 26 --- 20
R10E | 922 12 15 15 13 15 27 11 --- 7 | 41 40 27 33 41 32 36 --- 31
R11E | 1129 19 15 24 13 16 24 14 --- 8 | 28 26 32 28 28 26 23 --- 21
R13E | 1169 22 23 20 11 28 15 20 --- 8 | 36 40 38 39 43 33 28 --- 32
R14E | 2245 41 35 37 48 26 46 33 --- 17 | 44 46 50 88 67 50 46 --- 53
XR15E | 4248 21 22 22 24 --- 29 31 --- 13 | 89 91 93 107 --- 81 70 --- 87
R16E | 1114 24 35 36 31 26 36 24 --- 13 | 29 47 34 42 42 33 34 --- 28
R17 | 1354 42 44 17 13 24 26 14 --- 10 | 59 59 41 31 28 47 24 --- 32
R18 | 775 27 27 18 13 31 25 16 --- 9 | 43 42 37 37 28 41 23 --- 29
R19 | 637 65 71 21 14 31 41 28 --- 15 | 69 76 40 33 25 56 21 --- 33
R20 | 1018 51 69 45 23 23 61 29 --- 17 | 50 62 50 51 48 41 24 --- 33
R21 | 875 45 41 21 12 30 20 17 37 10 | 56 52 40 34 25 31 24 21 30
R22 | 1051 40 39 28 13 39 34 17 --- 12 | 51 50 44 36 36 38 24 --- 30
R23 | 3130 23 16 23 16 16 17 18 --- 8 | 28 37 39 51 52 40 39 --- 41
R24 | 2321 37 54 46 17 24 87 20 --- 18 | 62 54 41 54 37 41 44 --- 43
------+---------------------------------------------------+-----------------------------------------------
RMS | 1692 33 36 27 19 24 35 21 65 |T 49 51 45 48 40 40 32 31 38
WRMS | 1692 32 33 27 17 21 31 21 65 |NE 52 54 47 47 39 41 29 31 38
MEDI | 1152 27 30 23 14 23 26 20 61 |MD 50 51 43 42 41 40 26 29 33
Table 3.1909.3 GPS week: 1909 Day: 3 MJD: 57610
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 | 1117 54 44 23 25 25 24 14 --- 12 | 77 75 49 43 50 65 43 --- 46
R02 | 919 16 18 22 7 11 20 19 --- 7 | 64 65 72 58 63 71 47 --- 60
R03 | 656 22 28 22 9 13 22 18 81 7 | 69 76 68 56 49 44 42 31 52
R04 | 605 23 25 25 10 25 32 23 --- 10 | 56 57 58 42 32 40 32 --- 39
R05 | 1417 34 42 31 14 31 30 22 --- 11 | 49 69 57 38 46 33 26 --- 35
R06 | 913 25 32 24 15 22 31 26 --- 10 | 49 55 55 49 51 38 31 --- 43
R07 | 950 36 44 24 7 12 27 30 97 10 | 69 78 54 48 55 61 28 55 47
R08 | 592 34 42 23 13 20 16 21 --- 9 | 64 72 62 46 45 52 33 --- 45
R09E | 5527 19 22 17 12 16 29 22 --- 8 | 27 27 18 26 38 24 30 --- 21
R10E | 952 14 13 20 18 19 29 14 --- 8 | 61 62 57 66 72 64 57 --- 61
R11E | 1096 17 28 13 14 20 25 6 --- 7 | 27 32 24 27 38 33 26 --- 25
R13E | 924 21 24 25 10 18 18 11 --- 7 | 39 40 37 33 42 35 33 --- 33
R14E | 1086 33 28 47 39 53 52 31 --- 19 | 45 51 39 64 69 48 43 --- 39
XR15E | 5618 22 23 25 16 --- 23 27 --- 11 | 131 134 130 127 --- 146 137 --- 133
R16E | 1534 33 37 28 30 26 23 26 --- 12 | 41 49 29 48 59 42 44 --- 38
R17 | 1246 41 43 21 10 18 18 17 --- 9 | 63 63 44 37 38 38 26 --- 36
R18 | 543 25 24 21 12 22 18 22 --- 8 | 51 53 45 43 39 34 23 --- 36
R19 | 1015 67 71 27 12 27 27 28 --- 14 | 84 89 50 39 26 50 21 --- 39
R20 | 697 40 40 33 21 20 37 22 --- 12 | 42 48 51 28 29 26 20 --- 24
R21 | 717 43 43 24 17 22 17 15 52 10 | 60 60 41 23 24 39 32 21 30
R22 | 1638 41 41 30 11 26 26 26 --- 11 | 57 58 46 30 25 36 22 --- 28
R23 | 5221 16 16 23 18 30 11 12 --- 8 | 29 35 27 37 27 29 24 --- 25
R24 | 2794 26 65 48 26 27 67 19 --- 16 | 58 94 28 61 45 50 44 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1973 34 38 27 18 24 30 21 79 |T 57 62 49 46 43 47 37 35 42
WRMS | 1973 33 35 28 15 17 27 21 79 |NE 58 65 50 42 40 44 30 35 39
MEDI | 1015 26 32 24 14 22 25 22 81 |MD 57 60 49 43 42 40 32 31 39
Table 3.1909.4 GPS week: 1909 Day: 4 MJD: 57611
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 | 1015 59 71 24 21 31 25 24 --- 13 | 64 77 45 42 47 43 29 --- 36
R02 | 597 25 31 19 10 13 17 23 --- 8 | 54 64 51 43 45 43 29 --- 41
R03 | 486 16 17 25 6 15 18 19 79 7 | 65 66 71 57 48 58 45 41 55
R04 | 795 14 19 19 13 11 22 17 --- 7 | 55 61 57 55 42 46 37 --- 47
R05 | 798 44 37 37 19 16 21 28 --- 12 | 58 58 48 41 42 38 25 --- 35
R06 | 1478 34 29 21 8 9 31 20 --- 9 | 46 42 44 31 37 24 23 --- 30
R07 | 852 35 31 22 13 15 25 22 146 9 | 61 56 45 38 39 54 29 91 39
R08 | 623 33 34 29 12 21 22 28 --- 10 | 58 60 55 37 40 52 25 --- 39
R09E | 7415 20 17 17 10 15 18 17 --- 7 | 22 25 22 24 27 33 28 --- 21
R10E | 845 12 10 25 14 20 28 13 --- 8 | 53 53 66 52 49 65 54 --- 54
R11E | 851 15 15 16 11 21 20 16 --- 7 | 36 36 44 35 42 32 27 --- 32
R13E | 973 17 23 23 19 16 16 12 --- 8 | 41 41 38 45 47 46 39 --- 41
R14E | 2040 34 55 42 24 33 33 21 --- 13 | 46 73 39 48 64 41 46 --- 38
XR15E | 8575 13 18 15 12 --- 35 30 --- 11 | 75 78 71 68 --- 76 77 --- 71
R16E | 1157 28 42 23 19 29 22 30 --- 11 | 48 66 34 43 52 38 42 --- 37
R17 | 618 50 47 27 14 21 21 16 --- 11 | 55 54 42 34 36 27 25 --- 30
R18 | 1015 30 30 23 20 18 32 15 --- 10 | 45 48 39 32 41 38 22 --- 31
R19 | 1174 60 61 24 19 18 18 23 --- 12 | 78 80 39 43 44 39 31 --- 40
R20 | 567 40 42 45 25 33 46 23 --- 15 | 45 51 45 52 42 53 19 --- 33
R21 | 709 44 55 25 20 27 36 21 88 12 | 55 63 41 28 22 49 24 24 29
R22 | 1328 40 46 19 10 28 32 22 --- 11 | 56 61 40 31 27 56 24 --- 32
R23 | 6645 6 13 16 20 22 15 13 --- 7 | 26 24 36 35 31 20 19 --- 24
R24 | 3054 38 50 54 17 29 50 17 --- 15 | 63 69 57 47 39 34 35 --- 38
------+---------------------------------------------------+-----------------------------------------------
RMS | 2411 35 39 28 16 22 27 21 108 |T 52 56 46 41 41 43 32 52 37
WRMS | 2411 34 36 28 15 14 25 21 108 |NE 55 58 47 40 38 42 27 52 36
MEDI | 973 33 31 23 14 20 22 21 88 |MD 55 60 44 42 42 43 29 41 37
Table 3.1909.5 GPS week: 1909 Day: 5 MJD: 57612
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
------+---------------------------------------------------+-----------------------------------------------
XR01 | 1249 54 45 19 31 --- 34 23 --- 15 | 44 37 28 34 --- 33 26 --- 20
R02 | 746 33 35 24 9 20 22 21 --- 9 | 43 47 41 22 24 33 19 --- 24
R03 | 532 26 24 21 15 22 27 20 36 9 | 50 50 47 27 31 54 29 79 36
R04 | 820 18 22 16 9 13 23 16 --- 7 | 46 48 40 40 33 26 29 --- 35
R05 | 799 37 73 33 23 17 44 29 --- 13 | 48 82 35 40 31 22 26 --- 29
R06 | 1384 28 41 24 19 21 39 29 --- 11 | 41 52 34 41 33 27 21 --- 29
R07 | 2180 29 42 16 13 13 30 18 115 8 | 43 53 33 31 32 37 26 72 29
R08 | 569 23 33 14 19 20 31 14 --- 8 | 39 49 31 38 33 51 29 --- 32
R09E | 7527 12 12 13 11 15 18 17 --- 6 | 17 17 13 21 26 23 23 --- 15
R10E | 1303 17 11 17 17 19 44 13 --- 9 | 71 79 75 81 85 74 65 --- 74
R11E | 1014 15 12 20 12 17 18 12 --- 7 | 27 29 28 23 29 30 22 --- 21
R13E | 1367 21 27 14 11 17 20 8 --- 6 | 39 39 35 38 41 36 34 --- 33
R14E | 1997 35 39 25 32 43 47 29 --- 15 | 52 63 46 64 68 37 47 --- 43
XR15E |11097 20 21 18 15 --- 26 18 --- 9 | 111 109 102 104 --- 110 111 --- 105
R16E | 1007 26 34 16 22 39 28 29 --- 11 | 38 34 34 45 51 26 41 --- 32
R17 | 497 44 58 24 11 37 16 20 --- 11 | 47 57 39 31 28 35 21 --- 28
R18 | 905 28 27 18 16 29 22 10 --- 8 | 41 37 30 27 26 31 25 --- 26
R19 | 1385 66 65 21 20 29 22 16 --- 13 | 63 65 37 33 44 27 27 --- 31
R20 | 636 46 58 27 20 40 40 19 --- 13 | 48 57 45 25 29 35 24 --- 25
R21 | 670 43 42 21 11 38 28 24 103 11 | 49 47 35 26 25 45 25 21 26
R22 | 673 44 47 21 13 28 25 22 --- 11 | 50 51 37 27 24 37 21 --- 26
R23 | 5906 8 11 13 19 24 20 11 --- 7 | 19 24 20 25 25 23 16 --- 17
R24 | 2450 26 41 24 26 29 75 20 --- 15 | 36 45 38 38 26 35 19 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 2396 33 40 21 18 27 33 20 92 |T 46 50 39 38 35 38 31 57 33
WRMS | 2396 35 38 21 16 22 31 20 92 |NE 44 50 35 31 29 34 23 57 27
MEDI | 1014 28 35 20 16 22 27 19 103 |MD 44 49 35 33 31 35 26 72 29
Table 3.1909.6 GPS week: 1909 Day: 6 MJD: 57613
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 | 859 44 45 27 26 25 34 14 --- 12 | 75 78 54 53 48 54 38 --- 46
R02 | 709 29 32 31 17 27 20 31 --- 11 | 68 70 67 45 42 47 32 --- 46
R03 | 635 35 34 27 17 35 26 22 70 12 | 79 83 76 56 53 64 45 77 57
R04 | 1020 24 22 19 9 28 16 24 --- 9 | 72 72 67 51 48 50 44 --- 53
R05 | 736 33 30 36 18 22 72 23 --- 15 | 75 76 59 57 55 53 37 --- 51
R06 | 1497 19 17 19 20 20 45 32 --- 12 | 58 56 58 62 54 44 42 --- 52
R07 | 2114 28 26 28 13 26 27 24 78 10 | 76 74 71 51 50 44 40 92 52
R08 | 673 32 21 17 24 19 26 15 --- 10 | 74 70 62 57 46 65 41 --- 53
R09E | 6361 14 15 16 14 17 23 18 --- 7 | 27 32 22 36 38 25 28 --- 26
R10E | 1476 17 25 17 17 25 22 39 --- 10 | 75 74 68 64 71 63 83 --- 67
R11E | 801 16 18 15 11 25 24 12 --- 7 | 36 37 34 39 50 40 31 --- 36
R13E | 1252 19 14 15 12 22 38 13 --- 9 | 51 49 50 54 61 47 52 --- 51
R14E | 1576 32 26 39 44 24 32 32 --- 16 | 43 57 45 88 68 59 43 --- 54
XR15E | 5846 23 23 22 10 --- 34 18 --- 10 | 106 106 102 103 --- 109 99 --- 102
R16E | 1407 26 54 36 20 39 42 29 --- 14 | 66 83 48 50 76 46 49 --- 48
R17 | 506 42 39 22 12 31 31 23 --- 11 | 67 67 46 42 40 35 26 --- 38
R18 | 842 28 35 18 11 20 30 18 --- 9 | 56 62 46 45 39 43 29 --- 38
R19 | 1184 62 61 30 18 29 16 25 --- 14 | 87 86 50 32 32 43 22 --- 37
R20 | 756 49 54 26 21 26 39 26 --- 13 | 78 82 47 50 48 53 32 --- 45
R21 | 606 34 34 14 7 18 19 21 108 8 | 64 66 45 35 37 50 29 23 39
R22 | 703 39 37 23 9 34 26 20 --- 11 | 69 68 49 37 27 52 25 --- 38
R23 | 2610 16 20 22 18 17 20 16 --- 8 | 23 27 31 43 34 29 28 --- 30
R24 | 1106 14 18 17 14 38 67 22 --- 13 | 51 54 46 42 32 44 27 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1803 32 33 24 19 27 35 24 87 |T 64 66 54 51 47 50 40 64 47
WRMS | 1803 35 35 25 15 22 36 24 87 |NE 67 68 54 47 42 48 33 64 44
MEDI | 1020 28 26 22 17 25 27 22 78 |MD 68 70 50 50 48 47 37 77 46
More information about the IGSREPORT
mailing list