[IGSREPORT-25323] Wk 1950 IGLOS Final Orbits
acc
acc at igs.org
Tue Jun 13 03:15:48 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1950 (May 21, 2017 - May 27, 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 2.1950.
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:
igl1950[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1950 in the SP3 format.
igl19507.sum Combination Report for GPS Week 1950.
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 | -20.4 ns
1 | -17.1 ns
2 | -18.7 ns
3 | -20.8 ns
4 | -20.1 ns
5 | -19.7 ns
6 | -16.0 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 1.1950, 1a.1950).
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 2.1950.0-6)
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 3.1950.0-6).
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 1950 summary. (May 21, 2017 - May 27, 2017)
Table 1.1950.a GPS week : 1950 MJD: 57894.0-57900.0
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 0 10 5 -18 9 .11 28 25 | -15249 -1648 3465 12056
| 1 0 2 24 21 27 .05 | 3594 2669
cof n/a| 1 1 10 -13 -15 -5 .15 30 26 | -15256 -1638 3464 12058
| 1 1 4 22 32 38 .06 | 3599 2672
emx n/a| 0 0 2 -24 -18 11 .11 25 23 | -19613 -682 3447 11330
| 1 1 2 13 23 38 .04 | 13842 1605
esx n/a| 0 0 -2 7 8 -32 .18 18 16 | -22240 -1593 3461 14325
| 1 0 2 21 23 30 .03 | 7081 2427
gfz n/a| -1 0 -4 -4 39 22 .01 22 20 | 0 -1890 3474 11747
| 1 1 2 24 24 35 .05 | 0 2550
grg n/a| 0 0 -3 -93 11 -30 -.36 30 29 | -18071 -1850 3516 11756
| 2 1 2 29 16 100 .10 | 2230 2816
iac n/a| 1 0 0 83 -18 27 -.13 21 21 | -18090 -117 3470 11137
| 1 1 1 42 29 34 .04 | 2028 1568
mcc n/a| 0 -4 11 145 -95 -573 -.16 164 164 | --- --- --- ---
| 7 6 8 132 79 371 .32 | --- ---
Table 1.1950.b GPS week : 1950 MJD: 57894.0-57900.0
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 10 12 10 9 11 12 |
R02 | 7 9 6 7 7 7 8 |
R03 | 8 8 10 10 9 8 8 |
R04 | 10 8 7 10 8 8 7 |
R05 | 13 13 17 12 14 14 15 |
R06 | 6 9 10 10 9 8 9 |
R07 | 11 8 7 8 8 7 8 |
R08 | 8 8 7 7 9 8 7 |
R09 | 8 9 8 9 8 9 9 |
R10 | 7 8 8 11 11 8 10 |
R11 | 9 8 9 8 8 9 10 |
R13 | 10 10 9 8 7 7 7 |
R14 | 16 18 17 16 15 19 18 |
R15 | 10 10 8 8 8 11 10 |
R16 | 14 16 16 17 16 19 14 |
R17 | 15 11 10 8 7 8 7 |
R18 | 10 9 7 8 8 6 8 |
R19 | 11 14 10 10 9 10 13 |
R20 | 14 15 14 13 13 12 12 |
R21 | 14 9 7 10 8 8 8 |
R22 | 12 10 10 10 9 8 8 |
R23 | 11 9 8 10 9 8 10 |
R24 | 14 15 12 14 14 12 14 |
R26 | 17 16 27 17 16 14 17 |
Table 1.1950.c GPS week : 1950 MJD: 57894.0-57900.0
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 1950 0 | -44 78 262 294 -2180 4099 84.7 1417 1417 | -20438 0
brd 1950 1 | -10 -39 253 -873 -686 6750 86.3 1487 1487 | -17096 0
brd 1950 2 | -39 -33 136 211 819 6892 86.0 1263 1263 | -18720 0
brd 1950 3 | 14 43 94 -421 609 3334 83.9 1276 1276 | -20799 0
brd 1950 4 | -9 -25 88 -289 1270 1521 86.4 1330 1330 | -20078 0
brd 1950 5 | 18 -11 141 123 937 -1473 84.3 1208 1208 | -19661 0
brd 1950 6 | 22 -4 153 -263 -1227 186 84.8 1264 1264 | -15979 0
-------------+------------------------------------------------------------+----------------
brd 1950 mean| -6 0 161 -173 -65 3044 85.2 1320 1320 | -18967 0
brd 1950 sdev| 27 43 69 413 1306 3178 1.0 98 98 | 1813 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 2.1950.0 GPS week: 1950 Day: 0 MJD: 57894
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 11 41 -51 -48 .10 32 29 | -10457 -4946 3909 11134
cof n/a| 1 4 21 -7 -31 -34 .24 35 32 | -10454 -4943 3915 11133
emx n/a| 0 0 1 -27 -6 18 .12 21 21 | -20202 -2569 3919 10729
esx n/a| -1 0 1 -5 -2 -31 .14 17 13 | -13344 -4598 3904 13280
gfz n/a| -2 0 -5 -51 55 41 .05 24 24 | 0 -5056 3920 10797
grg n/a| -3 -1 -6 -136 29 91 -.58 33 30 | -17680 -5643 4010 10884
iac n/a| 3 1 0 149 -14 -3 -.17 28 28 | -18503 -1930 3937 10293
mcc n/a| 3 -4 3 274 -220 -860 .11 238 238 | --- --- --- ---
Table 2.1950.1 GPS week: 1950 Day: 1 MJD: 57895
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 12 -31 7 23 .13 29 25 | -11464 1726 4098 11851
cof n/a| 0 2 9 -57 14 -63 .23 35 29 | -11468 1743 4097 11847
emx n/a| -1 0 1 -13 3 -26 .15 23 21 | -10400 1747 3961 10900
esx n/a| 0 0 0 10 33 -70 .20 21 16 | -29777 1859 4079 14212
gfz n/a| -1 1 -7 -4 81 -34 .04 23 21 | 0 1365 4148 11740
grg n/a| 1 -2 -5 -86 7 113 -.32 27 25 | -18215 1794 4097 11460
iac n/a| 1 1 0 94 -53 48 -.17 22 22 | -16276 641 4099 10990
mcc n/a| 6 -5 14 91 -115 -1030 -.37 214 214 | --- --- --- ---
Table 2.1950.2 GPS week: 1950 Day: 2 MJD: 57896
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 11 -12 -27 1 .10 29 24 | -12578 -3994 3422 13315
cof n/a| 0 1 7 -2 -7 26 .13 29 22 | -12579 -4007 3425 13318
emx n/a| 0 1 5 -3 -32 -15 .13 24 21 | -19793 -1875 3411 11965
esx n/a| 0 1 -3 7 32 0 .18 18 16 | -18155 -4487 3420 15141
gfz n/a| -3 0 -4 -3 37 28 -.06 21 19 | 0 -4111 3411 13130
grg n/a| 4 -2 -2 -78 -4 -26 -.33 30 26 | -16691 -4392 3465 12844
iac n/a| 0 0 -1 76 -33 14 -.11 21 21 | -17266 -1748 3421 12599
mcc n/a| -11 -13 19 -15 -118 -260 .23 188 188 | --- --- --- ---
Table 2.1950.3 GPS week: 1950 Day: 3 MJD: 57897
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 10 2 -16 29 .05 27 24 | -18390 1165 3473 12184
cof n/a| 0 0 10 11 -57 -9 .09 30 26 | -18400 1188 3473 12191
emx n/a| 0 2 4 -40 -27 -39 .07 25 24 | -29947 707 3484 11630
esx n/a| 0 0 -4 10 20 -38 .15 16 14 | -20610 -153 3471 14358
gfz n/a| -2 0 -8 23 39 41 .01 25 20 | 0 -3 3483 11761
grg n/a| 0 0 -3 -61 -13 -61 -.38 31 31 | -21130 860 3599 11855
iac n/a| 1 -1 1 75 -11 73 -.17 20 20 | -21205 2248 3473 11260
mcc n/a| 0 -7 5 159 -91 -197 -.13 154 154 | --- --- --- ---
Table 2.1950.4 GPS week: 1950 Day: 4 MJD: 57898
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 10 -6 10 5 .06 24 21 | -17892 49 2850 12102
cof n/a| 0 1 11 -29 0 45 .08 29 23 | -17893 44 2835 12106
emx n/a| 1 0 2 -25 -6 55 .16 22 20 | -31929 -76 2862 11630
esx n/a| 0 0 -4 -28 -4 -24 .17 19 16 | -21472 -766 2850 14370
gfz n/a| -3 0 -1 19 0 75 -.01 22 19 | 0 271 2853 11764
grg n/a| 0 0 -4 -122 19 -132 -.34 31 29 | -19747 -257 2872 11710
iac n/a| 0 -1 -2 111 -6 -27 -.09 19 19 | -19566 1299 2851 11096
mcc n/a| 9 -9 1 271 -106 -511 .03 135 135 | --- --- --- ---
Table 2.1950.5 GPS week: 1950 Day: 5 MJD: 57899
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 10 17 -20 30 .12 27 27 | -18792 -1856 3197 11551
cof n/a| 4 0 9 -8 24 20 .11 27 26 | -18799 -1848 3199 11554
emx n/a| 0 1 1 -20 3 39 .05 26 24 | -31287 -527 3210 11158
esx n/a| 1 0 -6 15 10 -69 .21 19 16 | -33721 -225 3213 14616
gfz n/a| 0 0 -3 -4 37 0 .08 20 19 | 0 -1549 3215 11210
grg n/a| -1 1 0 -107 21 -53 -.30 30 34 | -18840 -1589 3233 11373
iac n/a| 1 0 0 66 -45 43 -.11 19 19 | -18625 -554 3214 10546
mcc n/a| 0 -2 21 266 -67 -959 -.72 119 119 | --- --- --- ---
Table 2.1950.6 GPS week: 1950 Day: 6 MJD: 57900
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 6 25 -28 21 .20 25 24 | -17174 -3686 3310 12259
cof n/a| 0 -1 6 -1 -54 -24 .15 28 26 | -17200 -3646 3306 12262
emx n/a| -1 0 -2 -39 -60 47 .10 33 28 | 6265 -2183 3285 11300
esx n/a| -1 2 0 43 -31 5 .21 19 17 | -18602 -2781 3293 14302
gfz n/a| 0 1 -3 -13 24 6 -.05 20 15 | 0 -4152 3292 11830
grg n/a| 0 0 -2 -59 23 -144 -.29 27 25 | -14197 -3729 3337 12170
iac n/a| 3 0 1 13 35 41 -.07 20 20 | -15195 -781 3300 11175
mcc n/a| -6 7 18 -26 48 -191 -.30 100 100 | --- --- --- ---
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 3.1950.0 GPS week: 1950 Day: 0 MJD: 57894
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 | 534 52 46 28 11 23 30 10 --- 11 | 2 5 3 4 6 2 3 --- 3
R02 | 654 14 21 14 6 22 18 20 138 7 | 1 3 2 2 2 2 2 2 1
R03 | 1320 22 27 16 9 13 33 17 168 8 | 2 2 2 4 3 7 2 1 2
R04 | 941 31 39 28 13 28 19 10 --- 9 | 1 3 1 2 3 5 2 --- 1
R05 | 1688 38 34 20 17 20 59 24 --- 13 | 2 6 2 5 7 4 6 --- 3
R06 | 1974 14 21 17 7 11 16 12 --- 5 | 2 3 1 2 5 5 2 --- 2
R07 | 1441 28 24 25 13 12 24 36 101 10 | 1 3 2 3 3 3 3 1 1
R08 | 1515 21 27 14 9 10 17 32 --- 8 | 1 5 2 3 4 3 3 --- 2
XR09 | 2091 18 20 22 6 16 --- 11 --- 7 | 1 6 1 2 5 --- 2 --- 2
R10 | 1034 11 21 18 12 16 18 8 --- 6 | 2 3 2 5 3 5 3 --- 2
R11 | 1057 29 33 10 10 31 25 15 141 8 | 2 4 2 3 2 3 2 2 2
R13 | 2025 24 29 17 19 27 30 11 --- 9 | 2 5 2 4 4 2 3 --- 2
R14 | 1607 49 50 15 36 37 45 32 --- 16 | 2 7 4 14 12 3 4 --- 6
R15 | 1614 37 42 18 13 28 20 21 --- 10 | 3 4 3 4 3 4 2 --- 2
R16 | 1920 42 50 25 14 27 62 14 --- 13 | 2 6 4 5 4 6 2 --- 2
R17 | 944 28 26 22 21 30 23 64 --- 15 | 3 7 4 5 4 7 7 --- 3
R18E | 541 21 29 15 10 23 36 27 --- 9 | 2 5 5 3 5 5 5 --- 2
R19 | 2598 43 46 26 11 27 25 24 --- 11 | 2 6 3 6 3 4 5 --- 2
R20 | 1533 28 29 23 20 24 65 28 --- 14 | 3 5 5 4 6 5 4 --- 3
R21E | 928 39 29 23 17 27 27 54 454 14 | 3 4 7 6 5 6 3 3 3
R22E | 1313 30 31 17 15 28 26 40 --- 11 | 2 4 3 7 7 6 3 --- 3
R23E | 973 35 49 32 20 15 19 22 --- 11 | 4 7 3 5 5 7 3 --- 3
R24E | 846 34 28 32 29 30 28 29 --- 13 | 5 9 4 6 9999 7 2 --- 3
XR26E | ---- 20 104 --- --- --- --- 14 --- 17 | 3 37 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1417 32 35 21 17 24 33 28 238 |T 2 6 2 4 4 4 3 1 2
WRMS | 1417 29 32 21 13 24 30 28 238 |NE 1 4 2 4 4 3 2 1 2
MEDI | 1320 28 29 20 13 24 25 21 141 |MD 2 5 3 4 4 5 3 2 2
Table 3.1950.1 GPS week: 1950 Day: 1 MJD: 57895
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 | 576 33 51 24 14 24 27 15 --- 10 | 2 7 4 7 7 2 3 --- 3
R02 | 556 20 20 27 8 20 21 20 150 8 | 1 3 2 5 6 4 3 11 3
R03 | 1463 21 20 15 11 16 9 24 186 7 | 1 2 2 4 5 6 2 8 3
R04 | 974 27 21 22 18 20 14 6 --- 8 | 1 4 2 4 3 4 1 --- 2
R05 | 2131 29 32 25 27 20 42 22 --- 12 | 2 7 6 10 10 4 6 --- 5
R06 | 1923 12 19 22 23 23 12 17 --- 8 | 2 4 2 4 5 4 3 --- 3
R07 | 1420 22 26 17 9 11 11 29 137 8 | 1 3 2 4 5 3 2 4 3
R08 | 909 15 15 8 22 10 13 25 --- 7 | 1 6 2 5 4 3 3 --- 2
XR09 | 1751 17 23 22 14 17 --- 12 --- 8 | 1 6 2 4 5 --- 3 --- 3
R10 | 1224 14 20 19 22 20 14 12 --- 8 | 2 5 3 8 7 4 3 --- 3
R11 | 1083 25 30 12 10 33 12 9 123 8 | 2 4 3 3 2 3 3 23 2
R13 | 2092 22 30 16 21 32 24 16 --- 10 | 2 6 2 4 5 5 3 --- 2
R14 | 1302 48 57 27 49 38 48 18 --- 17 | 2 9 4 19 14 3 3 --- 6
R15 | 2190 34 37 25 14 26 23 11 --- 10 | 3 6 4 3 5 5 2 --- 2
R16 | 944 38 43 47 24 23 46 23 --- 15 | 3 7 8 6 7 6 3 --- 4
R17E | 1705 26 34 17 15 27 17 39 --- 11 | 3 6 4 6 5 7 8 --- 5
R18E | 905 20 20 21 16 14 32 16 --- 9 | 2 4 5 5 5 4 5 --- 3
R19E | 2314 52 65 23 17 26 42 27 --- 14 | 3 7 6 7 5 6 3 --- 3
R20E | 2046 25 63 30 23 33 45 42 --- 15 | 5 16 5 11 13 6 4 --- 4
R21E | 588 32 24 18 12 17 18 17 371 8 | 3 4 6 8 5 4 4 23 3
R22E | 727 30 19 20 15 22 21 21 --- 9 | 3 4 6 10 11 4 4 --- 4
R23E | 1737 20 17 27 21 11 17 20 --- 9 | 3 6 3 5 5 6 4 --- 4
XR24E | 896 33 26 20 34 --- 40 18 --- 15 | 8 13 6 13 --- 6 5 --- 5
XR26E | ---- 19 163 --- --- --- --- 12 --- 15 | 3 36 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1486 29 35 23 20 23 27 22 214 |T 2 7 3 6 6 4 3 13 3
WRMS | 1486 25 29 21 16 21 25 22 214 |NE 1 5 3 6 6 4 2 11 3
MEDI | 1302 25 26 22 17 20 21 18 150 |MD 2 6 4 5 5 4 3 11 3
Table 3.1950.2 GPS week: 1950 Day: 2 MJD: 57896
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 | 669 23 18 21 23 13 46 20 --- 11 | 2 7 3 6 5 3 2 --- 2
R02 | 598 15 15 17 10 15 9 16 157 6 | 2 3 3 7 7 3 3 19 3
R03 | 1335 32 35 28 13 18 17 24 107 9 | 2 3 3 5 5 3 3 14 3
R04 | 556 20 21 13 6 11 14 21 --- 6 | 2 4 3 4 4 3 2 --- 2
R05 | 2281 32 26 35 28 23 73 26 --- 17 | 3 7 5 8 8 5 4 --- 4
R06 | 1525 20 15 29 23 14 25 16 --- 9 | 2 5 3 7 5 5 2 --- 3
R07 | 665 18 20 18 8 15 12 13 107 6 | 2 3 2 7 6 4 3 5 4
R08 | 866 18 18 11 10 16 16 17 --- 6 | 2 4 2 4 4 3 1 --- 2
XR09 | 1901 15 14 18 11 14 --- 20 --- 8 | 2 4 3 4 3 --- 2 --- 3
R10 | 1069 23 20 16 14 19 18 20 --- 8 | 2 6 3 7 8 4 2 --- 3
R11 | 1349 23 16 11 12 31 22 11 317 8 | 3 5 3 3 3 5 2 37 2
R13 | 1321 12 13 18 18 24 32 16 --- 9 | 3 4 4 4 4 6 2 --- 2
R14 | 1007 53 63 54 29 21 38 26 --- 16 | 3 7 7 14 11 2 3 --- 4
R15 | 2179 26 27 15 14 19 19 11 --- 7 | 3 5 3 3 5 4 2 --- 2
R16 | 541 38 37 31 31 33 57 29 --- 16 | 3 8 7 16 16 4 3 --- 6
R17E | 2113 23 26 17 20 20 19 30 --- 10 | 3 5 4 8 5 7 3 --- 4
R18E | 1099 17 17 20 13 17 13 15 --- 7 | 3 4 4 6 6 5 5 --- 4
R19E | 1316 44 48 19 9 19 21 16 --- 9 | 4 5 6 7 7 4 5 --- 4
R20E | 1132 44 28 28 16 29 40 28 --- 13 | 5 13 9 11 13 5 5 --- 5
R21E | 730 28 33 18 12 13 12 13 170 7 | 3 7 3 7 5 4 4 36 3
R22E | 883 29 27 20 14 22 18 25 --- 9 | 3 6 5 8 9 4 5 --- 4
R23E | 1421 21 26 24 16 12 14 21 --- 8 | 3 6 4 6 5 5 6 --- 4
R24E | 809 35 36 18 22 31 31 24 --- 12 | 6 12 6 17 1 4 5 --- 7
XR26E | ---- 33 71 --- --- --- --- 21 --- 27 | 3 21 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1262 29 29 24 18 21 30 21 188 |T 2 6 4 7 6 4 3 22 3
WRMS | 1262 24 22 21 16 19 26 21 188 |NE 2 5 3 6 6 3 2 18 3
MEDI | 1099 23 26 18 14 19 19 20 157 |MD 3 5 3 7 5 4 3 19 3
Table 3.1950.3 GPS week: 1950 Day: 3 MJD: 57897
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 | 551 22 23 27 14 12 44 14 --- 10 | 4 8 4 8 5 5 4 --- 3
R02 | 1222 19 25 24 11 17 10 12 84 7 | 4 4 4 6 6 2 2 2 2
R03 | 809 29 31 27 9 24 23 19 73 9 | 4 5 5 6 8 4 3 1 2
R04 | 1038 27 31 22 7 30 25 22 --- 9 | 4 4 4 5 7 3 2 --- 3
R05 | 1648 29 32 22 16 17 56 21 --- 12 | 4 7 5 6 6 6 4 --- 3
R06 | 1134 20 25 24 21 16 37 11 --- 9 | 4 5 4 7 6 5 2 --- 3
R07 | 590 20 19 22 18 20 14 14 150 8 | 4 4 4 7 5 4 3 1 3
R08 | 665 16 22 11 11 15 17 17 --- 6 | 4 5 4 4 6 4 2 --- 1
XR09 | 2283 22 26 20 9 18 --- 23 --- 9 | 4 5 5 7 6 --- 2 --- 3
R10 | 839 24 29 29 19 23 20 25 --- 10 | 4 6 5 6 7 7 3 --- 3
R11 | 1720 20 17 15 13 23 24 12 230 7 | 4 5 4 4 4 6 2 3 2
R13 | 751 14 15 17 18 21 24 16 --- 8 | 4 5 5 7 5 5 2 --- 3
R14 | 1051 42 31 54 24 37 31 22 --- 15 | 4 14 13 12 10 6 3 --- 7
R15 | 3279 21 18 11 12 29 19 8 --- 7 | 4 4 5 7 6 4 3 --- 4
R16 | 721 44 73 41 17 43 63 24 --- 16 | 5 10 6 13 13 5 3 --- 5
R17E | 2218 22 22 20 10 25 17 14 --- 8 | 4 7 5 8 7 7 4 --- 4
R18E | 1042 17 19 20 12 19 15 17 --- 7 | 4 6 6 6 6 6 5 --- 5
R19E | 977 41 38 19 12 26 21 14 --- 10 | 4 5 5 6 6 4 5 --- 4
R20E | 668 27 29 24 24 39 41 23 --- 13 | 5 9 7 9 11 4 5 --- 5
R21E | 1072 30 30 18 17 27 32 19 177 10 | 4 7 4 8 8 6 4 5 4
R22E | 725 28 32 19 11 19 17 34 --- 10 | 4 6 5 8 7 5 7 --- 4
R23E | 778 20 27 20 18 16 24 25 --- 9 | 4 6 5 7 6 4 6 --- 4
R24E | 1084 35 30 30 25 24 42 35 --- 14 | 6 13 6 16 1 8 5 --- 8
XR26E | ---- 21 49 --- --- --- --- 13 --- 17 | 4 20 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1275 27 30 25 16 25 31 20 154 |T 4 7 5 7 6 5 3 2 3
WRMS | 1275 24 26 24 14 20 31 20 154 |NE 4 6 5 7 6 4 2 1 3
MEDI | 1038 22 27 22 14 23 24 17 150 |MD 4 6 5 7 6 5 3 2 3
Table 3.1950.4 GPS week: 1950 Day: 4 MJD: 57898
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 | 734 19 21 17 23 13 26 15 --- 8 | 5 13 6 15 8 6 4 --- 5
R02 | 968 18 19 18 14 17 21 11 61 7 | 5 5 6 7 7 4 2 2 3
R03 | 874 17 23 19 18 25 16 20 78 8 | 5 6 6 6 8 3 3 1 2
R04 | 703 16 16 18 10 13 10 30 --- 8 | 5 6 6 6 7 3 3 --- 2
R05 | 853 23 27 27 19 19 59 34 --- 14 | 5 8 6 8 8 5 4 --- 3
R06 | 1080 16 21 23 10 23 25 24 --- 9 | 5 7 6 7 8 5 2 --- 2
R07 | 495 24 19 20 12 16 17 17 187 8 | 5 6 6 6 6 3 2 1 2
R08 | 1074 24 23 16 14 11 36 13 --- 8 | 5 6 5 6 8 9 3 --- 3
XR09 | 2228 17 18 20 10 12 --- 13 --- 7 | 5 8 6 7 6 --- 3 --- 2
R10 | 827 22 20 28 18 26 38 11 --- 10 | 5 6 6 7 7 7 2 --- 3
R11 | 1505 19 24 14 12 28 19 13 159 8 | 5 6 5 5 6 6 2 3 2
R13 | 1468 14 14 11 20 14 22 14 --- 7 | 5 5 6 7 5 6 2 --- 2
R14 | 3314 43 44 30 41 26 36 18 --- 15 | 5 16 11 18 12 5 4 --- 7
R15 | 1759 22 28 14 12 21 22 13 --- 7 | 5 8 6 10 7 4 4 --- 3
R16 | 768 41 60 39 21 28 67 18 --- 16 | 6 12 7 9 9 4 3 --- 3
R17E | 1984 19 22 15 10 18 13 10 --- 6 | 5 7 7 10 9 6 5 --- 5
R18E | 843 14 14 20 17 16 28 15 --- 8 | 6 7 7 8 7 6 5 --- 4
R19E | 691 30 44 18 14 28 14 15 --- 9 | 6 8 6 8 7 5 4 --- 3
R20E | 1215 25 33 21 28 25 48 22 --- 12 | 6 8 6 12 12 4 4 --- 5
R21E | 824 27 30 19 12 22 18 13 144 8 | 5 7 6 8 9 6 5 5 4
R22E | 1359 29 28 17 12 25 22 14 --- 9 | 5 6 6 9 9 7 5 --- 4
R23E | 1665 23 19 24 22 14 23 11 --- 9 | 5 8 6 8 8 4 6 --- 4
R24E | 1091 24 34 29 30 42 32 31 --- 14 | 6 14 6 11 1 7 4 --- 6
XR26E | ---- 17 40 --- --- --- --- 14 --- 15 | 6 18 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1330 24 29 22 19 22 31 19 135 |T 5 8 6 8 7 5 3 2 3
WRMS | 1330 21 23 20 16 19 29 19 135 |NE 5 7 6 8 7 5 2 1 2
MEDI | 1074 22 23 19 14 21 22 14 144 |MD 5 7 6 8 8 5 4 2 3
Table 3.1950.5 GPS week: 1950 Day: 5 MJD: 57899
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 24 25 19 30 14 21 27 --- 10 | 6 13 12 16 13 5 4 --- 5
R02 | 670 19 22 20 17 12 16 14 89 7 | 6 9 6 9 7 4 3 11 3
R03 | 841 19 20 21 16 16 16 12 100 7 | 6 6 6 6 6 3 3 4 2
R04 | 697 20 25 25 20 11 17 12 --- 8 | 6 7 7 6 7 3 6 --- 5
R05 | 463 33 24 35 19 25 58 20 --- 14 | 6 9 7 11 9 4 5 --- 5
R06 | 1062 17 20 20 13 12 20 19 --- 7 | 6 8 6 8 8 5 4 --- 3
R07 | 700 18 21 21 9 11 18 14 192 6 | 6 6 6 7 7 5 2 8 2
R08 | 1241 21 21 18 14 16 25 15 --- 8 | 6 6 6 7 7 8 6 --- 5
XR09 | 2468 15 21 20 17 15 --- 17 --- 8 | 6 8 7 7 7 --- 6 --- 5
R10 | 819 18 31 17 13 23 16 11 --- 7 | 6 8 6 7 7 5 4 --- 3
R11 | 1213 25 25 17 12 27 20 15 105 8 | 6 7 6 7 7 5 5 10 4
R13 | 1908 14 25 11 14 15 27 12 --- 7 | 6 7 6 7 7 5 4 --- 4
R14 | 2521 60 47 61 28 27 44 32 --- 18 | 6 15 8 21 17 6 3 --- 6
R15 | 804 31 22 27 22 25 20 13 --- 10 | 6 8 6 10 8 3 3 --- 2
R16 | 777 38 34 51 28 35 69 27 --- 18 | 7 12 10 12 10 3 5 --- 3
R17E | 1687 23 19 14 14 15 17 15 --- 7 | 6 6 7 9 8 3 7 --- 6
R18E | 755 11 10 14 12 13 20 14 --- 6 | 6 7 7 7 8 5 6 --- 6
R19E | 661 31 32 20 20 21 19 25 --- 10 | 7 8 9 11 12 6 6 --- 6
R20E | 1497 26 29 21 26 20 43 25 --- 12 | 7 12 8 15 13 6 6 --- 7
R21E | 636 22 23 19 11 21 15 12 68 7 | 6 8 6 8 7 5 7 7 6
R22E | 1778 22 32 23 8 22 17 11 --- 7 | 6 7 7 9 9 6 7 --- 6
R23E | 1660 23 30 16 21 20 16 11 --- 8 | 6 8 8 7 7 5 5 --- 4
R24E | 715 29 34 24 23 24 33 28 --- 12 | 8 16 9 9 1 6 7 --- 7
XR26E | ---- 17 38 --- --- --- --- 10 --- 13 | 7 10 --- --- --- --- 5 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1207 27 27 26 19 20 29 19 119 |T 6 8 7 9 8 4 4 8 4
WRMS | 1207 27 26 24 16 19 34 19 119 |NE 6 8 7 9 8 4 4 8 3
MEDI | 841 22 25 20 17 20 20 14 100 |MD 6 8 7 8 7 5 5 8 5
Table 3.1950.6 GPS week: 1950 Day: 6 MJD: 57900
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 | 619 23 20 55 17 19 19 21 --- 11 | 6 9 10 10 11 2 4 --- 3
R02 | 756 22 19 30 15 8 21 12 112 8 | 6 8 6 8 7 2 3 17 2
R03 | 610 22 25 23 10 19 21 11 70 8 | 6 6 6 6 6 2 3 3 2
R04 | 922 20 24 23 12 15 16 11 --- 7 | 6 6 6 6 6 2 4 --- 4
R05 | 710 34 23 56 30 18 48 21 --- 15 | 6 8 7 9 7 3 4 --- 3
R06 | 1610 15 19 26 14 29 11 21 --- 9 | 6 7 6 7 7 3 3 --- 2
R07 | 697 16 20 20 12 12 20 21 107 7 | 6 6 6 6 6 4 2 10 2
R08 | 973 18 17 18 17 10 11 13 --- 6 | 6 6 6 6 6 4 5 --- 4
XR09 | 2417 21 26 16 14 21 --- 17 --- 9 | 6 6 6 7 7 --- 5 --- 4
R10 | 955 31 29 26 14 23 23 18 --- 10 | 6 7 6 6 6 4 4 --- 3
R11 | 1485 29 37 19 12 30 16 18 105 9 | 6 7 6 7 7 4 4 19 3
R13 | 1276 13 18 16 18 20 16 12 --- 7 | 6 7 6 7 7 3 5 --- 4
R14 | 1798 47 51 70 33 28 47 20 --- 18 | 6 11 7 15 15 5 4 --- 5
R15 | 1621 28 37 25 25 15 26 17 --- 10 | 6 7 6 8 7 4 3 --- 2
R16 | 1454 23 44 57 18 22 30 30 --- 13 | 7 9 9 9 8 2 5 --- 2
R17E | 1417 23 23 22 8 18 17 9 --- 7 | 6 6 6 7 7 4 6 --- 5
R18E | 703 18 16 20 13 15 24 16 --- 7 | 6 6 6 7 8 4 5 --- 5
R19E | 948 38 40 20 23 26 28 29 --- 12 | 6 7 8 9 10 5 6 --- 5
R20E | 1835 30 29 25 21 21 35 26 --- 11 | 7 12 7 11 10 5 6 --- 5
R21E | 818 18 21 19 12 22 22 13 99 7 | 6 7 7 8 7 5 7 9 6
R22E | 1991 20 19 18 13 21 20 16 --- 8 | 6 6 7 7 7 4 6 --- 5
R23E | 1970 25 27 24 23 10 27 23 --- 10 | 6 8 7 7 7 5 5 --- 4
R24E | 650 18 17 40 28 22 45 34 --- 14 | 7 12 8 8 1 5 6 --- 6
XR26E | ---- 19 35 --- --- --- --- 14 --- 17 | 6 9 --- --- --- --- 6 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1264 25 28 33 19 20 27 20 100 |T 6 7 6 7 7 3 4 11 3
WRMS | 1264 24 26 28 17 15 25 20 100 |NE 6 7 6 7 7 3 3 12 3
MEDI | 973 22 23 23 15 20 21 17 105 |MD 6 7 6 7 7 4 5 10 4
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