[IGSREPORT-25277] Wk 1947 IGLOS Final Orbits
acc
acc at igs.org
Mon May 22 04:38:55 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1947 (Apr 30, 2017 - May 06, 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 2.1947.
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:
igl1947[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1947 in the SP3 format.
igl19477.sum Combination Report for GPS Week 1947.
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 | 0.2 ns
1 | -0.5 ns
2 | 0.4 ns
3 | 0.7 ns
4 | 0.9 ns
5 | 0.1 ns
6 | 0.0 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 1.1947, 1a.1947).
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 2.1947.0-6)
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 3.1947.0-6).
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 1947 summary. (Apr 30, 2017 - May 06, 2017)
Table 1.1947.a GPS week : 1947 MJD: 57873.0-57879.0
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 20 -9 17 20 .16 38 36 | 7756 363 3303 11888
| 1 1 2 31 20 33 .05 | 1026 1401
cof n/a| 0 0 24 -13 9 26 .15 40 38 | 7753 361 3303 11889
| 2 2 1 29 32 54 .08 | 1017 1399
emx n/a| 0 0 1 -28 -32 -15 .13 21 20 | 2492 864 3296 11303
| 1 1 3 26 19 25 .02 | 16380 975
esx n/a| 0 0 1 28 17 5 .12 16 14 | -4116 -562 3293 14163
| 0 0 2 13 13 26 .02 | 8278 1230
gfz n/a| -1 0 -11 -8 52 33 .02 26 25 | 0 82 3291 11764
| 0 1 1 25 23 35 .05 | 0 759
grg n/a| 1 0 1 -64 11 6 -.34 27 25 | 1874 -3088 3324 11494
| 1 0 4 30 18 46 .03 | 4350 7955
iac n/a| 0 -1 -7 53 -22 -18 -.12 20 20 | 1267 29 3292 11026
| 1 1 1 44 48 71 .03 | 449 519
mcc n/a| 4 0 21 50 -51 140 -.29 143 143 | --- --- --- ---
| 8 3 13 93 68 495 .18 | --- ---
Table 1.1947.b GPS week : 1947 MJD: 57873.0-57879.0
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 | 13 11 13 10 12 14 15 |
R02 | 7 8 8 9 7 6 9 |
R03 | 9 10 10 11 10 8 8 |
R04 | 7 8 8 8 10 10 8 |
R05 | 14 13 12 13 13 12 14 |
R06 | 8 6 8 8 9 7 8 |
R07 | 9 8 7 9 10 10 10 |
R08 | 7 7 8 7 8 8 8 |
R09 | 12 8 6 7 7 8 6 |
R10 | 8 9 10 8 10 10 7 |
R11 | 7 7 8 9 10 7 7 |
R13 | 9 6 8 8 9 10 8 |
R14 | 12 12 16 13 15 15 16 |
R15 | 10 10 11 11 8 9 9 |
R16 | 14 15 14 10 16 12 11 |
R17 | 10 9 9 8 9 9 9 |
R18 | 6 7 6 7 7 7 7 |
R19 | 16 13 13 13 12 12 15 |
R20 | 12 12 13 11 11 13 15 |
R21 | 10 11 10 8 8 8 9 |
R22 | 10 9 12 11 10 9 10 |
R23 | 9 11 10 11 11 12 12 |
R24 | 13 14 21 16 13 13 11 |
R26 | 15 16 14 16 18 21 30 |
Table 1.1947.c GPS week : 1947 MJD: 57873.0-57879.0
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 1947 0 | -31 24 199 -688 -221 3519 84.9 >>>>> >>>>> | 163 0
brd 1947 1 | -19 -5 224 -1045 -75 3841 83.5 90510 90510 | -509 0
brd 1947 2 | -7 26 233 -177 -184 5356 84.7 44280 44280 | 354 0
brd 1947 3 | -17 43 244 -1183 510 2661 84.4 1173 1173 | 659 0
brd 1947 4 | -5 -79 289 1413 -830 3712 84.3 1111 1111 | 852 0
brd 1947 5 | -20 -23 196 -1033 -1041 3720 82.8 1124 1124 | 75 0
brd 1947 6 | -16 36 219 -727 -1155 2032 84.8 1379 1379 | 43 0
-------------+------------------------------------------------------------+----------------
brd 1947 mean| -16 3 229 -491 -428 3548 84.2 41368 41368 | 233 0
brd 1947 sdev| 8 43 31 903 601 1040 .8 58707 58707 | 446 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 2.1947.0 GPS week: 1947 Day: 0 MJD: 57873
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 17 -40 3 43 .12 36 35 | 7845 1148 3162 11847
cof n/a| -1 1 24 -27 -38 12 .04 40 37 | 7837 1144 3166 11849
emx n/a| 0 0 0 -45 -9 0 .10 17 17 | 15389 1068 3148 11228
esx n/a| 0 0 0 40 12 -6 .14 17 15 | 4753 -1250 3151 14183
gfz n/a| -1 0 -10 31 61 -13 -.05 27 26 | 0 -67 3153 11713
grg n/a| 0 0 3 -23 -12 -78 -.36 28 26 | -293 613 3161 11488
iac n/a| 0 0 -5 53 -30 39 -.15 22 22 | 1265 241 3143 10933
mcc n/a| 2 2 29 75 -56 -421 -.31 120 120 | --- --- --- ---
Table 2.1947.1 GPS week: 1947 Day: 1 MJD: 57874
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 23 -50 12 -26 .11 37 35 | 8070 -2038 3235 11642
cof n/a| -2 1 23 -20 8 -38 .19 41 38 | 8070 -2045 3233 11641
emx n/a| 0 1 1 -5 -34 -40 .12 22 21 | 23189 -154 3227 11120
esx n/a| 0 0 -3 24 29 -14 .13 14 12 | -5010 -929 3222 13594
gfz n/a| -1 0 -12 9 60 -12 .04 27 25 | 0 -937 3212 11466
grg n/a| 0 -1 7 -65 11 21 -.33 25 23 | 465 -1708 3204 11377
iac n/a| 0 -2 -8 34 -45 63 -.13 21 21 | 537 -209 3224 10690
mcc n/a| -3 0 37 -23 -101 -310 -.10 114 114 | --- --- --- ---
Table 2.1947.2 GPS week: 1947 Day: 2 MJD: 57875
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 -2 23 -17 54 15 .12 37 34 | 5946 1262 3408 11600
cof n/a| 0 0 26 -26 62 99 .18 37 35 | 5967 1224 3404 11602
emx n/a| 2 0 5 -5 -28 9 .13 23 22 | -2218 1745 3423 11092
esx n/a| 0 1 1 36 36 37 .11 16 15 | -15856 1328 3411 13847
gfz n/a| -2 2 -13 7 85 74 .07 29 27 | 0 404 3430 11762
grg n/a| 0 1 2 -58 32 -14 -.36 26 23 | 116 787 3462 11368
iac n/a| 0 -3 -7 -20 -112 -103 -.08 19 19 | 1115 349 3409 10809
mcc n/a| 5 -7 36 -60 -52 -338 -.01 109 109 | --- --- --- ---
Table 2.1947.3 GPS week: 1947 Day: 3 MJD: 57876
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 3 21 -20 19 69 .25 38 37 | 7148 590 3335 12188
cof n/a| -3 3 23 -5 -19 86 .24 38 37 | 7154 568 3332 12186
emx n/a| 0 -1 -1 -64 -58 20 .16 20 20 | 19193 649 3302 11407
esx n/a| 0 1 3 41 26 19 .14 17 16 | -1138 -659 3292 14513
gfz n/a| -1 1 -9 -15 24 68 -.01 26 25 | 0 817 3285 12154
grg n/a| 2 0 0 -74 -10 23 -.32 26 24 | 395 700 3352 11657
iac n/a| 0 -1 -7 84 -1 -118 -.15 18 18 | 1709 -584 3299 11406
mcc n/a| -8 -3 14 -7 -103 640 -.32 154 154 | --- --- --- ---
Table 2.1947.4 GPS week: 1947 Day: 4 MJD: 57877
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 20 22 33 -12 .17 40 39 | 7627 2179 3471 12328
cof n/a| -1 -2 26 -4 10 -27 .08 42 41 | 7604 2202 3474 12330
emx n/a| 0 2 -2 -44 -26 -30 .14 24 21 | -16157 2482 3458 11632
esx n/a| 0 0 3 24 6 40 .11 18 15 | 6213 297 3471 14717
gfz n/a| -1 0 -9 -37 22 46 -.02 22 24 | 0 1199 3456 11962
grg n/a| 2 0 3 -122 8 21 -.29 26 22 | 11722 -21014 3507 11746
iac n/a| 2 -1 -5 111 -16 -16 -.07 20 20 | 1478 878 3461 11440
mcc n/a| 8 0 17 184 -66 703 -.48 135 135 | --- --- --- ---
Table 2.1947.5 GPS week: 1947 Day: 5 MJD: 57878
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 20 37 -7 38 .20 41 39 | 9182 132 3444 12629
cof n/a| 2 1 26 41 32 54 .08 43 41 | 9174 135 3447 12628
emx n/a| 1 0 1 5 -15 -45 .10 22 21 | -12303 -115 3449 12200
esx n/a| -1 0 3 27 0 -23 .09 15 12 | -4840 -2560 3442 14845
gfz n/a| -1 -2 -12 -27 45 41 .08 26 24 | 0 -475 3440 12425
grg n/a| 1 0 -2 -62 20 73 -.40 27 26 | 485 -643 3491 12218
iac n/a| 1 0 -6 24 10 35 -.12 18 18 | 1824 -536 3445 11710
mcc n/a| 4 -1 2 24 -76 535 -.47 161 161 | --- --- --- ---
Table 2.1947.6 GPS week: 1947 Day: 6 MJD: 57879
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 2 20 0 6 16 .15 38 35 | 8479 -728 3070 10988
cof n/a| 1 1 21 -54 11 1 .23 42 37 | 8468 -698 3069 10990
emx n/a| -1 1 5 -37 -57 -20 .13 17 17 | -9649 377 3065 10442
esx n/a| -1 0 0 1 12 -12 .09 18 14 | -12939 -162 3066 13444
gfz n/a| -1 -1 -11 -29 69 31 .02 27 22 | 0 -363 3061 10869
grg n/a| 3 0 -4 -41 31 0 -.33 28 28 | 229 -354 3093 10607
iac n/a| 3 0 -8 84 38 -32 -.12 23 23 | 943 68 3063 10199
mcc n/a| 19 2 10 162 96 178 -.32 211 211 | --- --- --- ---
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 3.1947.0 GPS week: 1947 Day: 0 MJD: 57873
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 | 733 55 35 18 19 25 40 20 --- 12 | 2 4 2 3 3 3 2 --- 2
R02 | 514 15 24 17 12 26 15 11 130 7 | 3 3 2 3 2 2 2 2 2
R03 | 916 37 36 14 10 31 22 19 41 9 | 2 3 4 5 5 3 3 2 2
R04 | 823 31 38 12 10 19 13 15 --- 7 | 2 3 2 4 4 2 2 --- 2
R05 | 577 24 25 19 24 27 56 36 --- 14 | 2 10 4 5 12 2 3 --- 3
R06 | 1193 26 27 12 16 18 22 19 --- 8 | 3 3 2 5 2 2 3 --- 2
R07 | 975 37 42 17 12 32 19 18 172 9 | 2 4 3 5 4 3 3 1 3
R08 | 804 28 30 12 12 21 17 15 --- 7 | 2 2 3 3 3 2 2 --- 2
XR09 | 1797 15 19 16 30 15 --- 27 --- 11 | 2 2 1 6 5 --- 3 --- 2
R10 | 714 36 39 14 13 28 11 14 --- 8 | 3 3 2 3 99 1 3 --- 2
R11 | 712 24 33 14 12 23 13 17 90 7 | 2 3 2 2 3 2 2 5 1
R13 | 927 21 31 11 24 26 20 16 --- 8 | 2 5 2 3 3 4 2 --- 1
R14 | 1857 31 39 16 20 30 36 31 --- 11 | 3 7 4 4 5 1 1 --- 2
R15 | 926 38 43 16 15 34 21 17 --- 9 | 2 3 3 4 3 3 2 --- 3
R16 | 704 38 70 23 28 24 49 19 --- 13 | 3 5 3 5 6 2 3 --- 2
R17 | 630 41 37 17 13 26 29 18 --- 10 | 2 5 4 5 3 4 2 --- 3
R18 |>>>>> 24 26 11 11 20 10 11 --- 6 | 2 4 2 2 2 5 2 --- 2
R19 | 986 67 79 33 16 47 28 35 --- 15 | 2 5 3 4 7 4 3 --- 3
R20 | 661 40 34 19 23 33 30 29 --- 12 | 2 10 6 7 10 3 3 --- 4
R21 | 1309 43 50 21 16 32 19 17 126 10 | 3 4 3 5 7 2 3 3 3
R22 | 1546 44 44 17 11 26 17 24 --- 9 | 3 3 2 3 2 2 3 --- 2
R23 | 800 24 24 17 26 10 24 15 --- 9 | 2 3 3 2 2 5 3 --- 2
R24 | 1201 27 33 16 21 23 40 38 --- 12 | 2 8 4 4 38 7 3 --- 3
XR26 | ---- 23 71 --- --- --- --- 9 --- 14 | 4 25 --- --- --- --- 2 --- 2
------+---------------------------------------------------+-----------------------------------------------
RMS |>>>>> 36 40 17 17 27 28 22 120 |T 2 5 2 4 10 2 2 2 2
WRMS |>>>>> 35 37 17 15 26 26 22 120 |NE 2 5 2 4 10 2 2 2 2
MEDI | 916 31 35 16 16 26 21 18 126 |MD 2 4 3 4 4 2 3 2 2
Table 3.1947.1 GPS week: 1947 Day: 1 MJD: 57874
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 | 813 46 65 23 11 34 21 23 --- 10 | 3 10 3 11 7 8 4 --- 6
R02 | 1255 22 17 22 8 22 16 20 116 7 | 3 5 3 5 4 5 4 3 3
R03 | 783 37 42 28 13 29 22 16 59 10 | 2 4 3 5 8 3 3 2 3
R04 | 546 32 36 18 7 26 18 13 --- 7 | 2 4 3 4 6 2 3 --- 3
R05 | 538 16 29 24 19 30 40 36 --- 12 | 4 13 5 12 14 3 4 --- 6
R06 | 1659 26 30 14 7 15 15 13 --- 6 | 3 5 4 6 3 3 4 --- 3
R07 | 1154 39 31 18 12 22 13 15 140 8 | 2 5 3 6 5 3 2 2 3
R08 | 918 24 29 15 11 28 14 14 --- 7 | 2 4 4 7 4 6 2 --- 3
XR09 | 1593 23 22 18 10 16 --- 15 --- 7 | 1 3 1 7 5 --- 3 --- 3
R10 | 708 42 40 21 8 21 16 17 --- 8 | 2 5 4 5 103 4 2 --- 3
R11 | 678 29 26 14 8 17 23 15 91 7 | 3 5 3 3 4 5 2 6 3
R13 | 1043 24 32 8 10 19 19 13 --- 6 | 2 3 2 5 5 6 3 --- 3
R14 | 4088 52 62 23 21 32 19 21 --- 11 | 4 7 6 9 6 8 4 --- 6
R15 | 1826 44 43 27 11 26 17 16 --- 9 | 3 6 6 6 7 5 3 --- 5
R16 | 896 32 39 46 21 19 46 23 --- 14 | 3 5 5 5 5 3 2 --- 3
R17 | 670 37 43 20 7 38 14 14 --- 8 | 3 6 5 7 5 6 2 --- 4
R18 |>>>>> 27 27 12 8 23 16 13 --- 6 | 4 7 6 7 5 5 3 --- 5
R19 | 1976 63 63 29 8 41 21 31 --- 13 | 3 8 4 6 10 3 4 --- 4
R20 | 572 35 39 23 16 42 30 30 --- 12 | 4 11 5 10 12 6 4 --- 6
R21 | 791 42 44 19 14 35 29 22 140 10 | 3 5 5 7 10 6 4 3 5
R22 | 1723 47 46 18 9 32 14 19 --- 9 | 3 7 4 9 8 5 3 --- 6
R23 | 851 39 46 27 25 15 23 11 --- 10 | 3 6 3 6 5 6 3 --- 4
R24 | 1855 24 30 14 22 15 53 37 --- 13 | 4 10 6 6 37 8 4 --- 5
XR26 | ---- 24 43 --- --- --- --- 10 --- 15 | 4 22 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS |90514 37 41 22 14 27 25 21 113 |T 2 6 4 6 12 4 3 3 4
WRMS |90514 35 38 21 12 25 23 21 113 |NE 2 6 4 6 12 4 3 3 4
MEDI | 918 32 39 20 11 26 19 16 116 |MD 3 5 4 6 6 5 3 3 3
Table 3.1947.2 GPS week: 1947 Day: 2 MJD: 57875
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 | 995 51 31 31 19 39 25 24 --- 13 | 3 9 5 10 10 6 4 --- 6
R02 | 1064 25 33 16 11 26 16 18 105 7 | 3 5 4 8 5 6 3 4 4
R03 | 1467 40 38 21 8 28 22 19 102 9 | 2 4 2 3 6 3 2 11 2
R04 | 1320 30 35 16 11 28 18 15 --- 8 | 2 4 3 4 5 2 3 --- 3
R05 |>>>>> 25 33 19 14 35 44 26 --- 12 | 3 10 5 11 11 4 4 --- 6
R06 | 1367 27 32 22 12 21 15 12 --- 7 | 3 5 4 5 4 3 3 --- 3
R07 | 1736 33 36 13 7 16 14 13 110 6 | 3 6 3 4 6 2 2 5 3
R08 | 1083 32 24 17 15 17 19 14 --- 8 | 2 4 3 6 4 5 2 --- 2
XR09 | 1361 23 28 9 9 16 --- 9 --- 6 | 1 3 2 5 4 --- 3 --- 2
R10 | 814 23 37 19 18 32 17 21 --- 9 | 2 6 3 6 108 5 2 --- 3
R11 | 1286 27 37 14 10 27 21 11 91 7 | 3 4 2 4 6 4 2 33 3
R13 | 824 25 40 16 14 22 27 10 --- 8 | 2 5 3 7 6 5 3 --- 3
R14 | 3838 63 56 45 25 21 42 17 --- 15 | 3 13 5 12 8 7 4 --- 7
R15 | 1584 35 36 20 17 34 26 17 --- 10 | 2 6 5 4 7 5 3 --- 4
R16 | 906 29 24 35 23 33 42 22 --- 13 | 3 7 7 6 4 3 3 --- 4
R17 | 689 29 24 17 16 22 22 21 --- 9 | 3 4 4 6 5 5 3 --- 4
R18 | 803 19 24 13 11 21 11 12 --- 6 | 3 6 6 6 5 3 3 --- 4
R19 | 1680 55 48 21 12 33 34 28 --- 12 | 4 8 4 8 8 5 3 --- 5
R20 | 649 37 34 23 21 35 36 25 --- 12 | 4 8 5 11 13 5 4 --- 6
R21 | 570 39 34 24 10 36 18 18 134 10 | 3 4 5 8 11 6 5 4 6
R22 | 1365 46 45 25 20 34 24 19 --- 11 | 3 7 3 10 10 4 4 --- 6
R23 | 936 43 46 28 16 18 12 21 --- 10 | 3 12 3 6 5 5 4 --- 4
XR24 | 2061 20 35 32 31 --- 70 37 --- 20 | 4 9 7 8 --- 4 4 --- 4
XR26 | ---- 20 46 --- --- --- --- 10 --- 13 | 4 13 --- --- --- --- 4 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS |44281 37 37 23 16 29 26 19 109 |T 2 6 4 6 11 4 3 11 4
WRMS |44281 34 35 22 15 27 23 19 109 |NE 2 6 4 6 11 4 3 11 4
MEDI | 1286 29 35 20 14 27 22 18 105 |MD 3 6 4 6 6 5 3 5 4
Table 3.1947.3 GPS week: 1947 Day: 3 MJD: 57876
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 | 905 49 57 15 19 20 23 12 --- 9 | 3 4 5 9 10 3 3 --- 4
R02 | 611 32 29 20 18 26 11 11 59 8 | 2 4 3 6 4 6 2 8 3
R03 | 1999 49 49 21 15 31 20 19 68 10 | 2 3 3 4 2 4 2 17 2
R04 | 961 34 30 17 9 17 19 17 --- 8 | 2 3 4 3 3 2 2 --- 2
R05 | 725 42 39 23 25 25 35 28 --- 12 | 3 6 4 6 8 4 3 --- 4
R06 | 667 24 25 17 11 20 26 14 --- 8 | 2 3 2 5 4 4 2 --- 2
R07 | 958 41 43 14 10 27 23 16 69 9 | 2 4 2 6 7 2 2 7 3
R08 | 768 28 33 12 12 14 20 11 --- 7 | 3 5 2 5 4 3 3 --- 3
XR09 | 967 23 24 10 11 18 --- 14 --- 7 | 1 4 2 4 3 --- 3 --- 2
R10 | 989 21 15 13 18 22 8 20 --- 7 | 2 5 3 4 114 3 2 --- 1
R11 | 1481 33 28 10 17 27 22 20 268 9 | 2 3 2 6 7 3 2 53 2
R13 | 656 25 24 15 9 32 23 10 --- 8 | 2 4 3 5 4 3 3 --- 2
R14 | 2884 67 61 25 23 29 28 16 --- 13 | 2 12 3 13 9 5 3 --- 6
R15 | 1143 33 31 20 23 35 34 10 --- 11 | 2 5 3 3 4 5 3 --- 2
R16 | 666 28 32 16 20 28 30 9 --- 9 | 3 7 7 6 6 3 2 --- 4
R17 | 684 32 32 18 14 18 17 15 --- 8 | 3 3 3 7 4 4 3 --- 3
R18 | 924 21 12 17 11 21 16 13 --- 7 | 2 4 3 3 4 2 4 --- 2
R19 | 788 60 59 24 15 36 29 19 --- 12 | 3 6 3 7 8 4 3 --- 4
R20 | 593 27 35 21 19 19 35 22 --- 10 | 3 6 3 10 11 2 3 --- 4
R21 | 645 33 37 19 10 21 11 17 184 8 | 2 3 4 6 7 3 4 5 4
R22 | 1068 47 49 29 14 33 15 20 --- 11 | 2 5 3 7 8 3 3 --- 4
R23 | 1302 39 50 33 24 13 12 19 --- 11 | 2 9 4 6 4 3 2 --- 3
R24 | 1569 21 26 24 23 43 58 34 --- 16 | 3 7 7 7 9999 4 3 --- 3
XR26 | ---- 24 64 --- --- --- --- 11 --- 15 | 3 15 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1173 38 38 20 17 26 26 18 154 |T 2 5 3 6 10 3 2 18 3
WRMS | 1173 37 37 20 16 25 24 18 154 |NE 2 5 3 6 10 3 2 18 3
MEDI | 924 32 32 18 15 25 22 16 69 |MD 2 4 3 6 4 3 3 8 3
Table 3.1947.4 GPS week: 1947 Day: 4 MJD: 57877
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 | 952 60 51 31 16 17 24 20 --- 11 | 3 4 4 9 10 2 4 --- 4
R02 | 877 26 30 14 8 20 13 10 61 6 | 2 3 2 3 5 4 3 2 2
R03 | 1664 48 57 19 9 24 26 19 79 10 | 2 4 2 5 2 6 2 2 2
R04 | 778 42 45 16 10 29 19 22 --- 9 | 2 2 3 4 4 3 2 --- 2
R05 | 959 36 39 28 20 21 43 28 --- 13 | 3 5 8 6 9 5 3 --- 3
R06 | 585 23 28 16 17 15 28 24 --- 9 | 2 3 2 4 4 5 2 --- 2
R07 | 843 49 45 13 10 30 20 15 66 9 | 2 3 4 6 7 2 2 2 3
R08 | 814 36 33 16 12 19 10 20 --- 8 | 2 5 3 5 3 3 3 --- 3
XR09 | 1003 24 28 13 10 19 --- 10 --- 7 | 2 4 2 6 4 --- 3 --- 3
XR10 | 1444 21 28 15 23 --- 24 10 --- 9 | 3 4 3 5 --- 4 2 --- 2
R11 | 1067 30 45 17 22 24 25 19 177 10 | 2 5 2 5 5 5 3 6 2
R13 | 1549 27 32 16 20 26 22 13 --- 9 | 2 4 2 3 4 4 4 --- 2
R14 | 890 60 65 22 32 32 28 29 --- 14 | 3 8 6 10 7 4 2 --- 5
R15 | 2066 29 38 24 16 17 10 16 --- 8 | 2 3 3 3 4 3 3 --- 2
R16 | 936 34 50 53 21 17 49 20 --- 15 | 2 8 6 4 6 4 3 --- 2
R17 | 704 43 42 18 17 27 12 15 --- 9 | 2 4 3 7 6 3 2 --- 3
R18 | 1281 22 26 17 10 18 14 11 --- 6 | 2 6 3 4 3 2 3 --- 3
R19 | 966 69 59 27 11 22 25 21 --- 12 | 2 4 3 6 6 5 4 --- 3
R20 | 1259 21 15 18 25 22 34 26 --- 11 | 3 8 3 6 8 2 3 --- 3
R21 | 677 37 38 20 8 20 18 14 214 8 | 2 2 4 3 3 4 4 3 2
R22 | 1187 44 44 26 11 24 10 19 --- 9 | 2 3 4 5 5 3 3 --- 3
R23 | 1226 37 43 31 25 15 23 15 --- 10 | 2 3 4 7 3 3 2 --- 3
R24 | 846 14 19 22 26 22 44 33 --- 13 | 3 4 7 6 9999 5 3 --- 4
XR26 | ---- 28 56 --- --- --- --- 12 --- 18 | 3 13 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1111 40 42 24 18 22 26 20 135 |T 2 4 3 5 5 3 2 3 2
WRMS | 1111 39 41 21 15 23 22 20 135 |NE 2 4 3 5 5 3 2 3 2
MEDI | 959 34 39 18 16 21 23 19 79 |MD 2 4 3 5 5 4 3 2 3
Table 3.1947.5 GPS week: 1947 Day: 5 MJD: 57878
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 | 915 70 78 20 15 36 40 21 --- 13 | 3 7 4 10 10 4 3 --- 5
R02 | 623 22 24 10 6 21 15 10 82 5 | 3 5 5 3 6 4 4 3 4
R03 | 1079 37 34 14 11 19 21 16 100 8 | 2 4 4 5 6 5 3 3 3
R04 | 578 42 46 22 13 34 25 15 --- 10 | 2 2 2 4 4 5 2 --- 2
R05 | 897 33 34 24 15 24 39 32 --- 12 | 4 7 8 8 9 4 4 --- 4
R06 | 921 24 21 15 10 19 15 11 --- 6 | 3 3 3 4 4 4 3 --- 3
R07 | 1028 44 50 19 11 29 21 17 86 9 | 3 4 4 4 6 3 4 2 3
R08 | 1642 35 43 15 9 21 21 22 --- 8 | 2 5 4 5 4 5 3 --- 3
XR09 | 936 24 28 15 8 19 --- 17 --- 7 | 2 4 3 5 3 --- 3 --- 3
R10 | 1051 27 26 22 17 34 20 13 --- 9 | 3 8 4 7 9999 8 5 --- 5
R11 | 1365 29 25 15 7 29 17 11 129 7 | 3 4 4 3 4 6 4 6 4
R13 | 1922 27 26 26 19 27 23 9 --- 9 | 2 4 2 7 7 5 2 --- 4
R14 | 1499 64 64 28 27 36 38 19 --- 14 | 3 7 8 12 12 4 4 --- 8
R15 | 1436 31 36 19 13 21 22 20 --- 8 | 2 4 3 3 3 5 3 --- 2
R16 | 643 53 59 35 7 17 39 13 --- 11 | 3 9 6 8 6 7 3 --- 5
R17 | 537 44 40 18 11 25 12 19 --- 8 | 2 5 4 7 7 5 3 --- 5
R18 | 1097 27 26 14 7 26 13 13 --- 6 | 3 6 3 8 6 4 3 --- 5
R19 | 1114 75 75 25 11 22 16 20 --- 11 | 3 6 4 4 3 6 4 --- 3
R20 | 1202 19 25 20 24 18 47 27 --- 12 | 4 9 5 7 9 4 4 --- 4
R21 | 545 43 43 15 7 24 19 15 297 8 | 3 3 3 2 3 7 3 3 3
R22 | 589 45 49 17 8 30 19 12 --- 8 | 3 4 4 4 4 4 3 --- 3
R23 | 841 37 39 34 23 19 25 18 --- 11 | 3 5 5 5 3 7 3 --- 4
R24 | 1651 17 15 31 22 22 41 26 --- 12 | 4 8 5 6 9999 6 3 --- 4
XR26 | ---- 39 61 --- --- --- --- 11 --- 21 | 5 13 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1123 41 43 22 15 26 27 18 161 |T 2 5 4 5 5 5 3 3 3
WRMS | 1123 39 41 21 12 24 26 18 161 |NE 2 5 4 5 5 5 3 3 3
MEDI | 1028 35 36 19 11 24 21 16 100 |MD 3 5 4 5 6 5 3 3 4
Table 3.1947.6 GPS week: 1947 Day: 6 MJD: 57879
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 | 648 66 85 21 23 45 37 25 --- 15 | 2 6 3 7 7 4 3 --- 4
R02 | 724 15 20 14 18 29 19 19 124 8 | 3 4 4 3 4 3 3 2 3
R03 | 1366 26 28 13 7 17 18 22 107 7 | 3 3 4 3 6 3 2 3 3
R04 | 823 32 31 13 6 25 16 16 --- 7 | 2 3 3 2 2 4 2 --- 2
R05 | 785 28 26 19 29 23 44 37 --- 13 | 4 7 5 6 6 3 4 --- 3
R06 | 1791 23 18 18 9 26 22 15 --- 8 | 2 3 2 3 3 2 3 --- 2
R07 | 1288 43 38 15 6 21 22 36 115 10 | 2 3 2 3 4 3 3 2 2
R08 | 2255 33 35 13 11 17 10 23 --- 7 | 2 3 3 4 3 4 2 --- 2
XR09 | 1675 18 19 12 8 14 --- 13 --- 6 | 1 2 2 2 2 --- 2 --- 1
R10 | 836 22 31 17 14 18 14 9 --- 7 | 2 6 3 4 9999 6 5 --- 4
R11 | 1337 25 35 7 13 27 16 12 143 7 | 2 2 3 3 4 4 4 5 3
R13 | 2361 25 31 10 16 14 26 21 --- 8 | 2 2 2 6 6 3 1 --- 3
R14 | 1521 59 65 23 31 45 42 26 --- 15 | 3 5 5 9 10 4 3 --- 6
R15 | 2746 33 39 16 14 29 14 19 --- 8 | 2 3 3 2 2 4 2 --- 2
R16 | 647 32 42 16 25 20 24 31 --- 10 | 2 6 5 7 5 6 3 --- 4
R17 | 591 35 37 16 14 25 21 14 --- 8 | 2 4 3 6 6 5 3 --- 4
R18 | 1171 25 21 14 19 14 12 12 --- 7 | 2 5 3 6 5 4 3 --- 4
R19 | 696 84 86 21 20 35 34 25 --- 15 | 4 5 4 3 3 3 3 --- 2
R20 | 929 23 33 25 20 31 63 28 --- 15 | 4 5 4 6 6 3 3 --- 4
R21 | 879 36 31 14 11 24 22 19 402 8 | 2 3 2 2 3 5 3 3 2
R22 | 840 49 46 15 12 33 17 13 --- 9 | 3 4 3 3 3 3 3 --- 2
R23 | 1029 29 29 30 26 17 23 31 --- 12 | 3 5 4 3 3 6 3 --- 3
R24 | 1956 28 24 17 19 21 42 23 --- 11 | 4 8 3 4 9999 4 3 --- 3
XR26 | ---- 44 108 --- --- --- --- 20 --- 30 | 5 12 --- --- --- --- 3 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1379 38 42 17 18 27 28 23 211 |T 2 4 3 4 4 3 2 3 3
WRMS | 1379 35 37 17 14 22 28 23 211 |NE 2 4 3 4 4 3 2 3 3
MEDI | 1029 29 31 16 14 24 22 20 124 |MD 2 4 3 3 4 4 3 3 3
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