[IGSREPORT-25249] Wk 1945 IGLOS Final Orbits
acc
acc at igs.org
Sun May 7 17:10:57 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1945 (Apr 16, 2017 - Apr 22, 2017)
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 2.1945.
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:
igl1945[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1945 in the SP3 format.
igl19457.sum Combination Report for GPS Week 1945.
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
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.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 | 0.7 ns
1 | -12.2 ns
2 | -1.1 ns
3 | 0.2 ns
4 | 0.5 ns
5 | -0.0 ns
6 | -1.9 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
----+--------+---------------
1 | IAC | R01
2 | COD | R01
2 | GRG | R01
2 | IAC | R01
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 1.1945, 1a.1945).
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 2.1945.0-6)
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 3.1945.0-6).
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 1945 summary. (Apr 16, 2017 - Apr 22, 2017)
Table 1.1945.a GPS week : 1945 MJD: 57859.0-57865.0
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 18 -37 3 -19 .13 37 36 | 306 -733 3171 11914
| 2 0 2 12 22 32 .03 | 3963 1943
cof n/a| -1 1 21 -35 16 -30 .15 40 37 | 311 -743 3169 11912
| 3 2 2 33 29 54 .05 | 3957 1944
emx n/a| 0 0 0 -22 -38 2 .11 25 25 | 9488 341 3163 11053
| 0 1 1 21 15 25 .05 | 12456 754
esx n/a| 0 0 0 18 11 -13 .13 16 14 | -6085 -511 3170 13925
| 1 1 1 19 12 25 .03 | 10517 1809
gfz n/a| -2 0 -11 -14 48 -10 .04 26 25 | 0 -888 3165 11735
| 1 1 1 26 15 28 .07 | 0 1858
grg n/a| 1 0 6 -40 9 48 -.32 29 26 | -1512 -800 3201 11554
| 1 1 3 26 40 36 .04 | 4311 2037
iac n/a| 2 0 -5 59 -13 -14 -.12 26 26 | -1243 -202 3169 11011
| 0 1 2 71 60 31 .03 | 4367 997
mcc n/a| 0 1 23 31 -38 1029 -.29 139 139 | --- --- --- ---
| 4 1 18 115 111 390 .16 | --- ---
Table 1.1945.b GPS week : 1945 MJD: 57859.0-57865.0
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 13 71 17 13 12 13 |
R02 | 8 8 8 7 7 7 8 |
R03 | 8 10 9 9 8 8 9 |
R04 | 8 8 9 8 9 7 9 |
R05 | 13 13 15 12 15 12 14 |
R06 | 8 9 7 7 7 9 10 |
R07 | 8 8 10 10 9 8 9 |
R08 | 8 9 8 9 8 9 8 |
R09 | 6 9 9 9 8 6 7 |
R10 | 9 9 8 8 9 9 10 |
R11 | 10 6 8 7 7 8 9 |
R13 | 10 8 7 8 8 8 8 |
R14 | 10 16 12 13 16 14 14 |
R15 | 12 11 9 11 10 9 8 |
R16 | 16 12 16 17 14 15 13 |
R17 | 10 9 12 11 10 8 8 |
R18 | 10 9 8 9 9 8 8 |
R19 | 13 19 15 12 16 17 16 |
R20 | 14 13 13 14 18 11 12 |
R21 | 11 10 9 11 11 10 10 |
R22 | 13 13 11 9 12 10 10 |
R23 | 8 9 11 11 12 9 8 |
R24 | 17 13 15 13 20 13 14 |
R26 | 31 25 19 19 24 40 21 |
Table 1.1945.c GPS week : 1945 MJD: 57859.0-57865.0
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 1945 0 | 18 -17 134 -1084 852 3507 83.6 1328 1328 | 706 0
brd 1945 1 | 42 -36 123 -737 544 954 85.4 1516 1516 | -12209 0
brd 1945 2 | 61 30 174 -590 -269 -166 84.4 1306 1306 | -1077 0
brd 1945 3 | 61 79 161 -851 -273 -4029 85.4 2052 2052 | 159 0
brd 1945 4 | 10 32 249 -12 -332 -4920 86.6 1897 1897 | 521 0
brd 1945 5 | 38 46 254 -845 -767 -727 84.2 1283 1283 | -30 0
brd 1945 6 | -28 52 200 -2951 -1423 1894 83.0 >>>>> >>>>> | -1892 0
-------------+------------------------------------------------------------+----------------
brd 1945 mean| 29 26 185 -1010 -238 -498 84.7 24668 24668 | -1974 0
brd 1945 sdev| 31 40 51 919 763 3056 1.2 61131 61131 | 4606 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 2.1945.0 GPS week: 1945 Day: 0 MJD: 57859
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 19 -21 4 -48 .11 36 37 | 2847 916 3120 11952
cof n/a| 0 0 24 19 30 -93 .09 39 36 | 2854 902 3114 11950
emx n/a| -1 -1 0 -19 -50 24 .14 26 26 | 14258 1108 3109 11130
esx n/a| 0 1 -1 24 1 -62 .09 15 14 | -10742 324 3115 13849
gfz n/a| -3 0 -11 25 29 -36 .15 27 25 | 0 981 3101 11826
grg n/a| 2 -2 3 8 -14 15 -.33 30 26 | 147 1356 3114 11855
iac n/a| 1 -2 -2 -22 31 31 -.10 22 22 | 727 1274 3114 11145
mcc n/a| 3 0 10 -168 157 1826 -.36 246 246 | --- --- --- ---
Table 2.1945.1 GPS week: 1945 Day: 1 MJD: 57860
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 15 -47 4 -62 .12 35 34 | -8428 -1060 2971 11829
cof n/a| 0 0 20 -48 28 -90 .23 36 35 | -8410 -1088 2974 11828
emx n/a| 0 0 1 -42 -40 14 .04 26 26 | -10507 107 2942 11042
esx n/a| 0 1 0 35 0 -29 .14 17 15 | -21761 788 2961 13879
gfz n/a| -5 0 -11 3 35 12 .06 25 26 | 0 -1515 2955 11542
grg n/a| 0 0 6 -56 -7 31 -.29 29 26 | -11281 -1623 3046 11800
iac n/a| 1 0 -8 37 -11 -14 -.14 59 59 | -10958 -842 2973 10978
mcc n/a| -5 1 54 60 -61 995 -.18 124 124 | --- --- --- ---
Table 2.1945.2 GPS week: 1945 Day: 2 MJD: 57861
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 14 -24 35 -10 .13 33 33 | 1313 -2069 3090 12030
cof n/a| -4 0 16 -23 56 -38 .10 37 35 | 1302 -2061 3089 12031
emx n/a| 0 0 0 15 -29 10 .11 25 25 | 7809 192 3135 11198
esx n/a| -2 0 -1 25 18 7 .17 17 17 | -8407 -1699 3094 14450
gfz n/a| -1 0 -9 -24 47 -31 -.02 25 21 | 0 -2201 3093 11898
grg n/a| 1 0 11 -61 55 -9 -.32 30 26 | 157 -2075 3112 11920
iac n/a| 3 1 -7 37 -80 1 -.13 19 19 | -809 294 3120 11134
mcc n/a| 2 3 29 97 -140 791 -.41 108 108 | --- --- --- ---
Table 2.1945.3 GPS week: 1945 Day: 3 MJD: 57862
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 17 -33 -16 6 .17 38 35 | 435 66 3236 12226
cof n/a| -4 3 19 -8 -3 36 .15 38 36 | 460 17 3233 12223
emx n/a| -1 0 0 -7 -42 -33 .13 25 25 | 5422 456 3218 11298
esx n/a| 0 0 -1 39 28 4 .16 17 16 | 6228 -583 3242 13868
gfz n/a| 0 0 -11 -4 73 40 .02 26 23 | 0 328 3218 11997
grg n/a| -1 1 11 -24 -26 61 -.25 25 25 | -59 405 3264 11552
iac n/a| 2 1 -8 0 2 -2 -.08 22 22 | 1084 -476 3226 11245
mcc n/a| -3 0 19 -67 -2 855 -.37 105 105 | --- --- --- ---
Table 2.1945.4 GPS week: 1945 Day: 4 MJD: 57863
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 19 -30 -18 -5 .14 40 36 | 2217 1675 3516 11108
cof n/a| 4 2 20 -71 -35 -39 .17 43 38 | 2200 1704 3518 11105
emx n/a| 0 0 -1 -39 -48 31 .19 27 27 | 2397 1284 3506 10354
esx n/a| 0 -1 -1 0 -5 -11 .16 17 14 | 7693 2184 3509 12828
gfz n/a| -3 -1 -13 -49 37 -32 .05 27 26 | 0 641 3540 11156
grg n/a| 1 1 6 -45 -34 65 -.36 26 22 | -168 1382 3636 10809
iac n/a| 2 0 -5 108 79 -71 -.10 22 22 | 1283 -256 3511 10207
mcc n/a| -5 -1 -5 163 39 987 -.00 111 111 | --- --- --- ---
Table 2.1945.5 GPS week: 1945 Day: 5 MJD: 57864
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 19 -47 -13 25 .07 39 37 | 2848 -525 2936 12066
cof n/a| -3 5 22 -74 13 44 .17 42 39 | 2859 -543 2929 12064
emx n/a| 0 2 0 -21 -51 -29 .05 24 24 | 28265 255 2917 11050
esx n/a| -1 0 2 -16 17 10 .11 12 11 | -3138 -1252 2935 14308
gfz n/a| -2 2 -10 -44 56 -20 .07 25 28 | 0 -264 2920 11880
grg n/a| 0 -2 2 -68 19 81 -.37 30 28 | 307 -820 2956 11389
iac n/a| 3 -1 -5 188 -24 -25 -.17 22 22 | 764 423 2917 11279
mcc n/a| 3 1 23 119 -110 607 -.25 106 106 | --- --- --- ---
Table 2.1945.6 GPS week: 1945 Day: 6 MJD: 57865
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 21 -54 31 -40 .16 40 40 | 916 -4134 3330 12189
cof n/a| -4 0 24 -39 29 -32 .12 42 41 | 915 -4138 3330 12189
emx n/a| 0 2 -1 -43 -9 -2 .12 19 19 | 18774 -1014 3315 11303
esx n/a| -1 -1 -1 21 18 -14 .11 17 15 | -12471 -3344 3334 14296
gfz n/a| -4 0 -9 -4 59 -4 -.08 25 25 | 0 -4191 3329 11846
grg n/a| 2 0 6 -36 70 91 -.31 34 29 | 311 -4228 3284 11556
iac n/a| 1 0 -2 69 -93 -23 -.15 19 19 | -796 -1835 3323 11092
mcc n/a| 1 3 31 15 -152 1143 -.46 173 173 | --- --- --- ---
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 3.1945.0 GPS week: 1945 Day: 0 MJD: 57859
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 | 935 52 35 27 16 36 21 26 --- 12 | 7 8 377 13 12 4 11 --- 9
R02 | 1917 28 30 13 11 20 20 16 151 7 | 2 3 2 3 3 1 2 6 2
R03 | 1132 35 36 13 8 26 13 15 253 7 | 2 2 3 3 3 3 2 13 2
R04 | 577 31 32 19 11 22 15 9 --- 7 | 2 4 2 4 3 2 2 --- 2
R05 | 821 25 36 40 19 33 37 26 --- 13 | 2 8 3 5 9 3 4 --- 3
R06 | 1054 26 31 22 15 24 16 10 --- 8 | 3 5 2 3 4 3 3 --- 3
R07 | 788 34 34 18 11 22 18 16 157 8 | 2 4 2 3 2 3 2 11 2
R08 | 632 28 32 18 10 21 21 12 --- 7 | 3 3 2 3 2 3 2 --- 2
XR09 | 1730 21 25 9 7 15 --- 12 --- 6 | 1 2 1 2 2 --- 2 --- 1
R10 | 1670 31 28 19 16 17 19 19 --- 8 | 3 3 2 3 4 2 1 --- 1
R11 | 640 32 31 27 9 32 19 18 199 9 | 2 2 2 4 6 5 1 10 3
R13 | 3267 22 26 16 13 20 26 31 --- 9 | 1 4 2 5 4 2 3 --- 3
R14 | 1495 47 44 20 12 18 31 10 --- 10 | 2 5 5 8 6 6 5 --- 5
R15 | 836 40 38 27 19 26 22 29 --- 11 | 2 3 2 5 4 2 3 --- 2
R16 | 965 35 53 42 27 15 60 24 --- 16 | 2 7 4 4 3 3 2 --- 2
R17 | 606 28 22 23 9 32 29 23 --- 10 | 2 3 2 3 4 2 2 --- 1
R18 | 749 29 23 24 10 35 20 17 --- 9 | 2 3 2 3 4 4 3 --- 2
R19 | 1813 52 56 35 14 26 27 31 --- 13 | 2 4 4 8 7 2 2 --- 3
R20 | 1699 50 76 27 16 29 36 34 --- 13 | 3 6 3 5 7 5 2 --- 3
R21 | 894 46 52 30 8 34 13 25 390 11 | 2 3 2 4 7 3 2 23 3
R22 | 638 46 46 30 11 40 30 26 --- 12 | 2 3 3 5 3 2 3 --- 3
R23 | 900 35 30 14 17 17 16 15 --- 8 | 2 4 2 3 5 3 1 --- 2
R24 | 1720 16 33 30 26 28 71 35 --- 17 | 4 6 2 7 9 4 3 --- 2
XR26 | ---- 46 56 --- --- --- --- 20 --- 30 | 7 9 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1328 36 39 26 15 27 30 22 246 |T 2 4 18 4 4 3 2 12 2
WRMS | 1328 37 36 26 14 25 26 22 246 |NE 2 4 18 4 4 3 2 12 2
MEDI | 935 32 33 23 12 26 21 19 199 |MD 2 4 2 4 4 3 2 11 2
Table 3.1945.1 GPS week: 1945 Day: 1 MJD: 57860
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 | 1395 36 48 27 18 31 23 259 --- 12 | 69 70 351 62 99 30 27 --- 74
R02 | 1935 28 31 13 12 21 16 18 125 7 | 2 5 3 6 4 3 2 9 2
R03 | 885 42 38 20 12 24 16 20 106 9 | 2 3 3 6 7 5 3 21 4
R04 | 562 36 38 21 9 22 15 8 --- 8 | 2 4 2 4 4 3 3 --- 2
R05 | 1518 36 32 33 19 29 31 31 --- 13 | 2 8 4 5 8 4 4 --- 3
R06 | 1884 22 22 14 17 27 20 13 --- 8 | 3 4 3 5 4 3 3 --- 2
R07 | 567 32 31 16 8 21 16 15 54 7 | 3 6 3 3 4 4 2 18 2
R08 | 611 34 34 22 12 17 24 15 --- 9 | 3 4 2 4 3 4 2 --- 2
XR09 | 2253 18 21 10 14 18 --- 27 --- 9 | 1 2 2 5 3 --- 2 --- 2
R10 | 1025 18 24 25 22 12 20 14 --- 8 | 2 5 3 4 5 3 2 --- 2
R11 | 560 22 28 10 8 19 8 16 159 6 | 2 3 4 7 9 5 2 15 4
R13 | 1726 19 20 19 8 28 15 20 --- 8 | 1 6 3 5 4 3 2 --- 3
R14 | 2894 39 31 50 20 18 55 22 --- 15 | 2 13 8 11 8 5 6 --- 7
R15 | 1005 23 22 22 23 20 42 17 --- 11 | 2 3 3 5 5 3 4 --- 3
R16 | 764 46 41 29 19 19 35 17 --- 12 | 2 7 3 4 3 4 4 --- 2
R17 | 620 27 35 11 13 21 26 24 --- 9 | 2 4 3 6 6 2 2 --- 3
R18 | 747 19 23 23 14 22 20 21 --- 8 | 2 4 2 3 4 4 2 --- 2
R19 | 2615 64 62 51 29 45 39 33 --- 18 | 2 5 4 7 8 5 3 --- 3
R20 | 1062 51 44 17 16 20 42 32 --- 13 | 4 6 5 8 10 4 3 --- 4
R21 | 570 34 36 26 6 32 23 20 149 10 | 2 3 2 6 8 4 3 39 4
R22 | 1223 48 49 31 14 42 26 24 --- 13 | 2 3 3 7 7 2 2 --- 3
R23 | 1225 32 43 20 22 14 16 15 --- 9 | 2 6 3 4 5 4 2 --- 2
R24 | 3259 18 22 31 22 20 50 26 --- 13 | 4 6 4 7 9 6 4 --- 3
XR26 | ---- 36 73 --- --- --- --- 16 --- 24 | 5 12 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1515 35 36 26 17 25 29 59 124 |T 5 8 18 8 9 5 3 20 5
WRMS | 1515 34 35 26 15 26 26 59 124 |NE 5 8 18 8 9 5 3 20 5
MEDI | 1062 32 32 22 14 21 23 20 125 |MD 2 5 3 5 5 4 3 18 3
Table 3.1945.2 GPS week: 1945 Day: 2 MJD: 57861
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 | 4222 154 155 --- 51 98 382 693 --- 71 | 67 68 --- 85 93 47 45 --- 88
R02 | 1379 22 19 17 14 23 17 11 124 7 | 2 4 3 5 4 2 2 2 2
R03 | 630 40 45 16 11 29 12 19 111 9 | 2 6 2 6 8 7 4 2 3
R04 | 939 37 40 16 13 23 18 13 --- 8 | 3 5 2 4 5 3 4 --- 3
R05 | 1088 35 43 31 21 22 57 27 --- 14 | 3 8 4 4 9 4 4 --- 3
R06 | 1601 18 25 14 12 16 28 10 --- 7 | 3 4 3 5 5 2 3 --- 2
R07 | 699 37 41 23 18 28 21 8 46 9 | 3 5 3 9 7 3 2 3 4
R08 | 445 34 47 18 16 17 9 17 --- 8 | 3 5 3 4 3 4 3 --- 2
XR09 | 1494 24 17 19 13 22 --- 12 --- 8 | 2 4 3 5 4 --- 3 --- 2
R10 | 1019 19 16 18 16 26 15 11 --- 7 | 2 4 4 4 5 3 3 --- 3
R11 | 655 31 34 12 12 26 17 17 147 8 | 2 5 4 6 7 4 2 1 4
R13 | 1977 20 24 17 12 25 17 9 --- 7 | 2 5 2 5 3 5 3 --- 3
R14 | 2097 34 43 35 18 31 30 12 --- 11 | 2 12 8 8 7 3 4 --- 5
R15 | 963 18 23 18 18 22 28 12 --- 8 | 2 3 2 3 6 5 2 --- 3
R16 | 1040 40 51 48 22 17 54 26 --- 15 | 3 8 2 8 5 3 4 --- 3
R17 | 593 38 35 22 17 32 38 18 --- 11 | 2 6 3 9 6 3 2 --- 4
R18 | 814 21 21 23 12 19 12 16 --- 7 | 2 4 2 7 5 4 3 --- 3
R19 | 1841 49 43 32 13 36 32 43 --- 15 | 3 5 3 7 7 5 3 --- 3
R20 | 669 38 53 21 23 23 43 24 --- 12 | 4 7 5 9 9 5 3 --- 4
R21 | 999 36 29 21 9 19 17 15 85 8 | 2 3 3 6 7 3 4 5 4
R22 | 645 46 44 22 10 35 20 19 --- 11 | 2 4 2 6 9 3 3 --- 3
R23 | 1105 33 36 27 29 10 29 14 --- 11 | 2 5 2 4 5 5 2 --- 2
R24 | 2982 22 20 39 19 28 53 29 --- 14 | 4 9 5 4 10 4 4 --- 3
XR26 | ---- 28 84 --- --- --- --- 13 --- 19 | 3 17 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1305 33 37 25 17 25 30 19 108 |T 5 8 3 9 9 5 4 2 6
WRMS | 1305 33 35 25 17 21 26 19 108 |NE 5 8 3 9 9 5 4 2 6
MEDI | 1019 34 36 21 16 23 21 15 111 |MD 2 5 3 6 6 4 3 2 3
Table 3.1945.3 GPS week: 1945 Day: 3 MJD: 57862
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 | 7916 69 60 30 22 31 27 49 --- 16 | 21 21 9999 51 26 30 48 --- 46
R02 | 772 21 16 16 14 15 18 11 110 7 | 3 4 3 3 3 3 3 3 2
R03 | 1032 40 42 15 10 24 24 14 126 9 | 3 6 3 4 5 6 3 2 3
R04 | 1290 38 33 13 14 26 10 12 --- 8 | 3 6 3 4 4 4 3 --- 3
R05 | 1475 29 41 28 17 19 27 35 --- 11 | 3 9 5 6 8 4 4 --- 3
R06 | 1422 19 21 16 13 19 18 14 --- 7 | 3 6 3 7 5 3 3 --- 3
R07 | 597 40 46 23 16 25 17 16 83 9 | 3 5 3 8 7 4 3 3 4
R08 | 568 32 35 17 10 22 22 17 --- 8 | 3 5 3 4 3 4 3 --- 2
XR09 | 1299 21 26 13 16 18 --- 19 --- 8 | 2 4 3 3 3 --- 3 --- 2
R10 | 750 21 23 22 19 20 13 8 --- 7 | 2 5 4 5 7 6 4 --- 4
R11 | 1006 31 36 9 11 22 13 10 135 6 | 2 4 3 4 4 4 2 2 3
R13 | 944 20 22 17 19 19 21 14 --- 8 | 2 3 2 5 3 6 3 --- 3
R14 | 1132 50 55 23 20 31 32 23 --- 12 | 3 7 6 11 7 4 3 --- 6
R15 | 1652 37 41 33 15 36 16 18 --- 11 | 2 3 2 3 5 4 3 --- 2
R16 | 1499 44 47 66 12 21 42 20 --- 17 | 3 6 4 7 4 4 3 --- 4
R17 | 672 39 30 24 18 32 20 19 --- 10 | 2 5 3 9 5 3 2 --- 4
R18 | 701 25 21 16 19 29 21 15 --- 9 | 2 4 3 7 5 4 2 --- 3
R19 | 2709 56 48 26 11 28 19 27 --- 11 | 2 4 3 6 6 4 3 --- 3
R20 | 732 28 22 20 26 21 50 33 --- 14 | 4 9 6 6 8 5 4 --- 4
R21 | 1260 43 55 28 15 35 17 17 48 11 | 2 4 3 5 5 5 3 5 3
R22 | 780 38 43 12 14 20 21 23 --- 9 | 2 5 4 5 8 4 3 --- 3
R23 | 663 29 30 26 24 27 18 17 --- 10 | 2 3 2 5 5 4 2 --- 2
R24 | 1250 39 30 19 27 30 41 23 --- 13 | 4 8 5 5 9 3 3 --- 3
XR26 | ---- 31 114 --- --- --- --- 12 --- 19 | 5 17 --- --- --- --- 5 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 2051 38 38 25 17 26 25 22 105 |T 3 6 3 7 6 5 4 3 4
WRMS | 2051 35 36 25 16 23 25 22 105 |NE 3 6 3 7 6 5 4 3 4
MEDI | 1032 32 35 20 16 24 20 17 110 |MD 3 5 3 5 5 4 3 3 3
Table 3.1945.4 GPS week: 1945 Day: 4 MJD: 57863
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 | 6687 67 83 26 17 35 23 20 --- 13 | 8 10 9999 13 17 4 5 --- 11
R02 | 512 22 31 16 12 25 10 10 93 6 | 3 5 3 4 4 2 3 4 3
R03 | 1006 39 43 20 10 17 14 14 139 8 | 3 4 2 4 3 3 3 10 2
R04 | 1074 39 43 20 9 23 22 22 --- 9 | 2 4 3 5 4 4 2 --- 3
R05 | 1624 38 40 38 21 25 37 39 --- 14 | 2 11 9 6 8 6 4 --- 3
R06 | 2371 24 24 19 16 17 13 11 --- 7 | 3 5 3 7 5 3 3 --- 3
R07 | 854 42 36 21 13 22 11 21 135 9 | 2 5 2 4 5 3 2 11 2
R08 | 586 33 33 16 8 22 19 15 --- 7 | 2 4 3 5 4 3 3 --- 2
XR09 | 1555 24 25 21 9 21 --- 8 --- 8 | 2 3 2 5 5 --- 2 --- 3
R10 | 761 23 32 23 13 20 24 12 --- 8 | 2 4 4 4 6 6 3 --- 4
R11 | 640 27 29 9 6 29 15 9 120 6 | 2 3 2 3 5 4 2 5 2
R13 | 1417 24 22 13 8 18 24 19 --- 7 | 2 4 2 4 4 5 2 --- 3
R14 | 1157 49 59 28 35 31 44 24 --- 15 | 3 5 4 11 9 5 2 --- 6
R15 | 1482 33 35 22 9 28 14 28 --- 9 | 2 4 2 3 2 2 2 --- 2
R16 | 1852 24 34 55 9 38 26 21 --- 13 | 2 5 6 5 3 3 2 --- 3
R17 | 787 35 37 29 11 33 12 20 --- 9 | 2 3 2 6 7 3 2 --- 3
R18 | 769 28 23 18 12 31 19 22 --- 9 | 2 3 3 5 5 2 2 --- 3
R19 | 2106 79 80 34 28 35 25 26 --- 15 | 2 8 3 4 6 4 2 --- 2
R20 | 888 24 33 36 28 25 70 31 --- 18 | 3 8 5 6 6 5 3 --- 3
R21 | 1160 46 34 30 10 29 18 26 34 11 | 2 4 3 3 4 4 3 4 2
R22 | 664 53 51 28 7 32 20 25 --- 11 | 2 4 3 3 6 3 3 --- 3
R23 | 956 39 39 30 29 15 17 21 --- 11 | 2 3 2 5 6 4 2 --- 3
XR24 | 1075 30 68 37 22 --- 61 34 --- 19 | 4 12 5 6 --- 3 3 --- 3
XR26 | ---- 37 105 --- --- --- --- 15 --- 24 | 5 71 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1897 40 43 27 17 27 26 22 111 |T 2 8 3 5 5 3 2 6 3
WRMS | 1897 36 38 27 14 26 22 22 111 |NE 2 8 3 5 5 3 2 6 3
MEDI | 1074 33 35 23 12 25 19 21 120 |MD 2 4 3 5 5 3 2 5 3
Table 3.1945.5 GPS week: 1945 Day: 5 MJD: 57864
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 | 2582 72 62 23 12 32 21 17 --- 12 | 8 7 9999 10 15 4 5 --- 9
R02 | 835 24 37 14 11 21 11 16 58 6 | 2 5 3 4 5 2 2 5 2
R03 | 626 36 41 16 7 26 16 17 97 8 | 2 3 3 4 5 3 3 17 2
R04 | 876 34 36 17 9 18 12 16 --- 7 | 2 2 3 5 4 3 2 --- 3
R05 | 1057 24 32 31 15 25 38 34 --- 12 | 3 8 7 5 10 5 4 --- 3
R06 | 2352 22 27 20 10 21 26 20 --- 8 | 3 6 4 7 5 4 2 --- 3
R07 | 1069 39 43 15 9 25 16 17 86 8 | 2 4 3 5 6 4 2 18 3
R08 | 957 26 25 20 12 27 18 23 --- 8 | 2 4 3 4 5 3 2 --- 2
XR09 | 1410 23 31 13 6 17 --- 12 --- 6 | 1 2 2 5 5 --- 2 --- 3
R10 | 721 25 21 20 13 20 26 21 --- 8 | 2 5 3 5 5 4 3 --- 3
R11 | 745 29 28 11 11 17 25 13 152 7 | 2 4 2 3 4 2 2 8 2
R13 | 1789 22 27 15 11 32 23 13 --- 8 | 2 5 2 4 3 3 2 --- 2
R14 | 1842 44 43 31 19 20 53 29 --- 14 | 2 6 3 8 7 5 2 --- 4
R15 | 1152 32 34 20 17 20 18 19 --- 9 | 2 5 2 4 3 2 2 --- 2
R16 | 1317 35 31 53 10 28 46 23 --- 14 | 2 9 4 6 3 5 2 --- 3
R17 | 745 32 30 17 8 21 16 25 --- 8 | 2 2 3 4 6 3 3 --- 2
R18 | 753 27 29 19 7 33 15 12 --- 8 | 2 3 2 5 7 3 3 --- 3
R19 | 781 83 98 29 17 43 47 28 --- 16 | 3 8 2 4 5 5 2 --- 3
R20 | 910 23 40 29 14 20 40 24 --- 11 | 3 11 6 6 8 5 3 --- 3
R21 | 1697 45 52 23 6 23 21 25 115 9 | 2 5 2 2 5 3 2 4 2
R22 | 852 51 43 18 7 31 21 26 --- 10 | 2 3 2 2 5 2 3 --- 2
R23 | 1321 29 34 13 15 16 28 17 --- 8 | 2 5 2 4 7 3 2 --- 3
R24 | 588 35 50 29 11 17 55 25 --- 12 | 5 10 7 7 9999 3 3 --- 4
XR26 | ---- 61 259 --- --- --- --- 26 --- 40 | 7 69 --- --- --- --- 5 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1283 39 42 24 12 25 30 22 106 |T 2 7 3 4 5 3 2 10 3
WRMS | 1283 37 39 24 11 28 28 22 106 |NE 2 7 3 4 5 3 2 10 3
MEDI | 957 32 34 20 11 21 21 20 97 |MD 2 5 3 5 5 3 2 8 3
Table 3.1945.6 GPS week: 1945 Day: 6 MJD: 57865
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 | 2839 61 60 18 11 33 42 21 --- 12 | 6 6 9999 7 10 5 4 --- 7
R02 | 728 25 22 18 11 23 22 11 75 7 | 2 3 3 3 4 3 2 3 2
R03 | 730 45 41 17 11 28 19 15 70 9 | 2 2 2 3 4 3 2 2 2
R04 | 811 40 38 19 10 22 13 20 --- 8 | 2 2 2 3 3 1 3 --- 2
R05 | 1021 35 27 27 23 22 59 25 --- 14 | 3 4 3 3 7 3 3 --- 3
R06 | 2679 30 36 22 25 17 32 12 --- 10 | 4 6 3 4 4 4 2 --- 2
R07 | 482 50 47 13 9 29 15 14 288 9 | 2 3 2 4 5 3 2 3 3
R08 | 1233 32 31 14 13 20 20 8 --- 7 | 2 3 2 2 3 2 2 --- 2
XR09 | 1419 21 22 14 9 18 --- 11 --- 6 | 1 2 2 4 3 --- 2 --- 2
R10 | 1357 33 51 19 14 29 12 24 --- 9 | 2 5 2 4 4 2 2 --- 2
R11 | 727 36 39 16 10 26 32 9 202 8 | 1 3 2 2 2 3 1 2 2
R13 | 1630 23 18 9 15 27 23 11 --- 7 | 2 3 2 2 2 2 2 --- 1
R14 | 1992 38 43 12 25 28 57 27 --- 13 | 2 5 2 4 3 3 2 --- 2
R15 | 943 30 33 15 13 23 24 6 --- 7 | 1 3 2 3 3 1 1 --- 2
R16 | 1356 29 52 24 24 28 58 16 --- 13 | 1 7 2 4 2 3 2 --- 2
R17 | 584 28 39 18 8 17 23 22 --- 8 | 2 3 2 2 4 3 2 --- 1
R18 | 852 26 26 16 12 20 16 17 --- 7 | 2 2 2 4 6 3 3 --- 3
R19 | 1231 83 74 33 17 40 32 25 --- 15 | 3 3 3 3 4 4 2 --- 2
R20 | 749 37 33 24 16 29 39 27 --- 12 | 3 7 5 4 7 3 3 --- 3
R21 | 1693 43 43 19 18 24 23 14 128 9 | 2 4 2 3 3 2 3 5 2
R22 | 1371 43 54 20 10 26 16 21 --- 9 | 2 3 2 2 4 2 4 --- 2
R23 |>>>>> 29 20 13 20 15 24 13 --- 8 | 2 5 2 3 5 2 2 --- 2
R24 | 1029 30 38 24 25 19 60 27 --- 14 | 4 7 4 5 9999 2 2 --- 3
XR26 | ---- 35 57 --- --- --- --- 13 --- 20 | 4 24 --- --- --- --- 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 40 42 19 17 25 34 19 173 |T 2 4 2 3 4 2 2 3 2
WRMS |>>>>> 40 41 19 15 25 29 19 173 |NE 2 4 2 3 4 2 2 3 2
MEDI | 1231 33 38 18 13 24 23 15 128 |MD 2 3 2 3 4 3 2 3 2
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