[IGSREPORT-25310] Wk 1949 IGLOS Final Orbits
acc
acc at igs.org
Wed Jun 7 04:04:41 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1949 (May 14, 2017 - May 20, 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 2.1949.
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:
igl1949[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1949 in the SP3 format.
igl19497.sum Combination Report for GPS Week 1949.
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 | 0.1 ns
1 | 0.3 ns
2 | 0.5 ns
3 | -1.4 ns
4 | 0.4 ns
5 | -15.9 ns
6 | -7.2 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 1.1949, 1a.1949).
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 2.1949.0-6)
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 3.1949.0-6).
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 1949 summary. (May 14, 2017 - May 20, 2017)
Table 1.1949.a GPS week : 1949 MJD: 57887.0-57893.0
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 14 -6 3 5 .16 33 31 | 5665 163 3253 12008
| 0 1 2 14 23 29 .03 | 7666 2098
cof n/a| 0 1 18 -20 -2 11 .17 35 32 | 5662 164 3253 12008
| 1 2 2 22 34 42 .03 | 7673 2105
emx n/a| 0 0 3 1 -6 -6 .12 22 21 | -8049 419 3259 11346
| 1 1 2 22 26 26 .03 | 8085 1389
esx n/a| 0 0 0 17 3 -39 .14 17 15 | -12162 -566 3257 14432
| 0 0 1 17 15 23 .02 | 9337 2088
gfz n/a| 0 0 -7 4 48 12 .04 24 21 | 0 -101 3266 11916
| 1 1 2 10 20 27 .07 | 0 2245
grg n/a| 0 1 1 -106 15 28 -.38 28 27 | -3326 -33 3275 11575
| 1 1 5 24 18 66 .06 | 7010 2110
iac n/a| 1 -1 -5 48 -28 39 -.10 19 19 | -2369 168 3256 11161
| 0 0 1 43 29 27 .03 | 6354 345
mcc n/a| 3 0 26 58 -42 -307 -.38 145 145 | --- --- --- ---
| 4 7 10 82 82 486 .13 | --- ---
Table 1.1949.b GPS week : 1949 MJD: 57887.0-57893.0
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 11 10 11 11 12 |
R02 | 8 9 8 9 8 9 8 |
R03 | 8 10 11 11 9 9 9 |
R04 | 10 7 7 10 7 8 9 |
R05 | 15 14 13 12 12 15 13 |
R06 | 8 6 8 8 10 8 8 |
R07 | 9 10 10 9 6 9 9 |
R08 | 7 6 9 9 9 8 9 |
R09 | 8 9 8 7 8 8 9 |
R10 | 8 7 7 9 8 10 8 |
R11 | 9 7 7 9 8 9 8 |
R13 | 9 11 7 7 7 9 9 |
R14 | 17 15 12 13 16 14 14 |
R15 | 11 12 7 9 9 11 9 |
R16 | 15 14 15 16 16 14 16 |
R17 | 8 7 7 8 8 8 9 |
R18 | 7 6 7 8 7 7 8 |
R19 | 12 12 12 11 13 11 12 |
R20 | 14 13 12 12 11 11 12 |
R21 | 8 7 9 7 8 8 10 |
R22 | 9 9 9 9 8 10 8 |
R23 | 12 9 9 10 9 10 12 |
R24 | 15 13 14 14 14 15 14 |
R26 | 27 25 28 24 28 24 27 |
Table 1.1949.c GPS week : 1949 MJD: 57887.0-57893.0
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 1949 0 | -16 10 201 98 -1069 5135 88.3 1045 1045 | 100 0
brd 1949 1 | 40 -7 217 624 -42 4170 86.1 1250 1250 | 300 0
brd 1949 2 | -38 -22 230 736 -1043 3291 85.7 1288 1288 | 488 0
brd 1949 3 | -49 9 195 -409 -608 -1189 85.2 99680 99680 | -1425 0
brd 1949 4 | -36 -24 268 -35 195 -2959 85.7 1165 1165 | 408 0
brd 1949 5 | 24 25 268 -567 220 -542 86.6 1207 1207 | -15900 0
brd 1949 6 | 53 117 273 -1748 57 757 85.9 1220 1220 | -7208 0
-------------+------------------------------------------------------------+----------------
brd 1949 mean| -3 15 236 -185 -327 1237 86.2 15265 15265 | -3319 0
brd 1949 sdev| 41 48 33 841 569 3024 1.0 37223 37223 | 6193 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 2.1949.0 GPS week: 1949 Day: 0 MJD: 57887
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 17 -18 -11 34 .18 34 31 | 11054 -93 3430 12030
cof n/a| 0 4 21 -17 -5 63 .16 35 32 | 11072 -125 3422 12024
emx n/a| 1 1 6 45 14 -41 .09 19 19 | -576 262 3434 11358
esx n/a| -1 -1 0 0 1 -48 .15 20 18 | -3689 -468 3460 14697
gfz n/a| -2 -2 -7 -12 64 20 .07 26 21 | 0 -577 3497 12243
grg n/a| 0 1 -1 -75 15 0 -.39 29 29 | 132 -358 3366 11036
iac n/a| 1 -2 -7 4 -51 36 -.11 19 19 | 1341 -77 3433 11186
mcc n/a| 1 0 44 3 -54 236 -.22 139 139 | --- --- --- ---
Table 2.1949.1 GPS week: 1949 Day: 1 MJD: 57888
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 18 -4 -12 51 .19 33 31 | 10366 -222 3181 12401
cof n/a| 0 -2 19 -26 30 53 .14 34 33 | 10369 -241 3188 12400
emx n/a| -1 0 4 -1 -42 -36 .11 20 20 | -4163 -83 3198 11126
esx n/a| -1 0 1 8 0 -32 .14 15 13 | -10701 -551 3178 14766
gfz n/a| 0 0 -9 14 72 6 -.07 24 18 | 0 -573 3179 12334
grg n/a| 1 0 -6 -103 -19 33 -.36 30 26 | 495 -566 3184 12071
iac n/a| 2 0 -5 51 -7 46 -.05 19 19 | 851 -150 3175 11586
mcc n/a| 1 -7 26 108 -19 178 -.53 160 160 | --- --- --- ---
Table 2.1949.2 GPS week: 1949 Day: 2 MJD: 57889
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 11 -21 19 -11 .11 34 30 | 10932 498 3144 12047
cof n/a| -3 1 15 -27 -10 -20 .17 37 32 | 10927 505 3138 12047
emx n/a| 1 1 4 12 -8 -1 .11 21 21 | -797 723 3145 11405
esx n/a| -1 0 0 32 14 -45 .13 16 14 | -1714 -1113 3137 14285
gfz n/a| -1 1 -7 13 40 38 .09 23 21 | 0 277 3140 11843
grg n/a| 0 0 -1 -106 35 5 -.37 27 23 | 125 571 3152 11375
iac n/a| 2 -1 -4 40 -44 59 -.09 19 19 | 1616 787 3138 11204
mcc n/a| 5 -8 15 153 -89 -49 -.42 119 119 | --- --- --- ---
Table 2.1949.3 GPS week: 1949 Day: 3 MJD: 57890
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 14 -18 31 4 .17 31 30 | 8676 -3653 3133 12021
cof n/a| 2 2 16 0 43 -4 .14 36 33 | 8673 -3650 3129 12023
emx n/a| -1 2 2 -1 1 -12 .09 21 21 | -9438 -2003 3138 11611
esx n/a| 0 1 -1 24 7 -1 .17 15 13 | -12557 -3876 3143 14262
gfz n/a| 1 0 -11 0 59 24 .06 25 21 | 0 -3954 3165 11884
grg n/a| 0 0 2 -139 8 -71 -.40 23 20 | 543 -3641 3196 11805
iac n/a| 1 -2 -3 47 -28 72 -.14 18 18 | -128 -171 3148 11091
mcc n/a| 2 -2 19 72 -82 -273 -.23 92 92 | --- --- --- ---
Table 2.1949.4 GPS week: 1949 Day: 4 MJD: 57891
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 13 -5 32 -28 .16 33 31 | 5647 130 3272 12051
cof n/a| 0 2 18 -27 12 4 .17 32 31 | 5647 119 3280 12056
emx n/a| 0 0 1 -8 21 17 .12 24 21 | -6035 162 3294 11393
esx n/a| 0 1 1 -7 8 -35 .13 15 13 | -14879 -1165 3290 14138
gfz n/a| 0 0 -7 15 56 3 .11 25 23 | 0 49 3296 11896
grg n/a| -1 -1 0 -130 14 9 -.33 24 25 | 686 -285 3361 11966
iac n/a| 0 -1 -7 135 -51 39 -.14 20 20 | 550 232 3285 11208
mcc n/a| 11 3 32 144 57 -397 -.42 95 95 | --- --- --- ---
Table 2.1949.5 GPS week: 1949 Day: 5 MJD: 57892
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 1 15 7 -20 -19 .16 33 32 | -10452 3442 3332 12281
cof n/a| -1 4 17 -56 -47 40 .17 35 33 | -10462 3455 3331 12281
emx n/a| 0 -1 0 -6 8 -4 .17 24 22 | -11434 2515 3316 11750
esx n/a| 0 0 -1 42 21 -32 .16 18 16 | -30373 3205 3311 15279
gfz n/a| -1 0 -8 2 31 33 -.04 22 21 | 0 3720 3317 12131
grg n/a| 0 1 5 -78 32 133 -.33 30 33 | -17737 3514 3364 11893
iac n/a| 2 0 -5 5 -45 -16 -.09 18 18 | -15860 164 3326 11505
mcc n/a| 1 0 30 -21 -170 -768 -.53 200 200 | --- --- --- ---
Table 2.1949.6 GPS week: 1949 Day: 6 MJD: 57893
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 11 16 -16 4 .15 32 31 | 3433 1045 3285 11231
cof n/a| -1 -1 16 15 -43 -52 .22 33 32 | 3411 1085 3285 11229
emx n/a| 0 0 1 -25 -42 31 .12 23 20 | -23902 1363 3288 10779
esx n/a| 0 0 -1 18 -26 -78 .11 18 15 | -11225 4 3283 13603
gfz n/a| -1 0 -4 -1 16 -42 .05 22 20 | 0 345 3273 11082
grg n/a| -1 4 9 -112 18 88 -.49 32 30 | -7527 529 3302 10883
iac n/a| 1 0 -6 52 28 39 -.08 17 17 | -4957 396 3290 10349
mcc n/a| 0 13 13 -51 59 -1081 -.32 212 212 | --- --- --- ---
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 3.1949.0 GPS week: 1949 Day: 0 MJD: 57887
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 | 676 52 50 22 24 35 27 18 --- 12 | 2 3 2 8 6 3 3 --- 3
R02 | 655 18 20 10 12 26 23 21 111 8 | 2 4 4 5 5 4 3 5 3
R03 | 784 21 23 19 11 15 17 18 92 7 | 2 2 2 3 5 3 3 4 2
R04 | 717 33 30 24 9 27 12 19 --- 9 | 2 3 1 3 4 2 2 --- 2
R05 | 988 39 32 21 26 23 54 35 --- 15 | 2 10 2 9 10 4 4 --- 4
R06 | 1819 12 15 14 16 20 19 20 --- 7 | 3 5 3 4 3 2 2 --- 2
R07 | 733 33 25 21 11 20 19 23 140 9 | 2 2 1 4 6 4 3 8 3
XR08 | 1270 15 16 15 11 15 --- 16 --- 7 | 2 3 2 3 1 --- 3 --- 2
XR09 | 2649 22 25 16 12 25 --- 10 --- 8 | 2 4 3 3 4 --- 3 --- 3
R10 | 728 21 28 16 16 18 21 10 --- 7 | 3 3 3 5 3 4 2 --- 1
R11 | 968 30 29 10 10 30 24 15 119 8 | 2 4 3 2 1 2 1 25 1
R13 | 1472 17 23 14 25 17 25 14 --- 8 | 2 3 3 3 5 2 2 --- 2
R14 | 745 58 62 21 47 31 52 18 --- 17 | 2 5 2 10 6 5 2 --- 3
R15 | 1465 38 38 16 18 36 27 10 --- 10 | 2 2 2 2 4 4 2 --- 1
R16 | 931 35 29 26 29 36 46 26 --- 14 | 3 4 68 428 6 3 3 --- 3
R17 | 951 30 37 18 15 24 17 12 --- 8 | 3 4 4 4 5 3 4 --- 4
R18 | 913 23 21 16 14 17 16 11 --- 7 | 3 4 3 4 6 5 3 --- 4
R19 | 1300 62 66 18 15 33 22 14 --- 12 | 3 6 2 2 4 218 3 --- 2
R20 | 622 19 37 21 20 31 56 30 --- 14 | 5 11 6 4 18 2 4 --- 4
R21 | 1404 30 29 13 15 16 16 14 205 7 | 3 4 4 3 3 2 3 15 2
R22 | 1048 42 44 15 12 30 16 15 --- 9 | 3 4 2 3 3 3 3 --- 2
R23 | 945 21 20 35 22 21 18 25 --- 11 | 3 6 5 4 2 3 3 --- 3
XR24 | 970 32 30 23 23 --- 51 24 --- 15 | 4 10 5 8 --- 4 5 --- 5
XR26 | ---- 40 88 --- --- --- --- 16 --- 26 | 4 40 --- --- --- --- 4 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1044 34 35 19 20 26 29 19 139 |T 2 6 5 22 5 13 2 11 2
WRMS | 1044 31 32 19 18 21 29 19 139 |NE 2 6 5 22 5 13 2 11 2
MEDI | 951 30 29 18 15 24 22 16 119 |MD 2 4 3 4 4 3 3 8 3
Table 3.1949.1 GPS week: 1949 Day: 1 MJD: 57888
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 | 643 33 26 15 16 22 41 16 --- 10 | 2 4 2 8 6 3 4 --- 4
R02 | 556 19 23 13 8 24 35 21 105 8 | 2 4 3 7 7 5 3 10 4
R03 | 1303 30 32 23 13 24 23 26 78 10 | 3 2 3 5 7 4 4 4 4
R04 | 772 25 30 16 6 14 13 18 --- 6 | 3 4 3 3 5 2 3 --- 2
R05 | 1120 25 28 25 23 24 62 25 --- 14 | 2 9 5 10 11 4 3 --- 5
R06 | 2580 14 17 15 10 15 16 9 --- 5 | 2 5 3 4 4 3 2 --- 2
R07 | 982 31 34 26 8 29 9 23 111 9 | 3 4 2 6 5 6 4 11 4
R08 | 1089 18 20 17 6 15 15 9 --- 5 | 3 5 4 5 5 9999 2 --- 3
XR09 | 1208 23 28 17 17 14 --- 13 --- 8 | 2 4 4 4 4 --- 3 --- 3
R10 | 685 23 27 15 11 17 16 11 --- 6 | 2 5 3 7 4 4 3 --- 3
R11 | 1012 27 28 9 9 19 12 16 282 6 | 2 4 3 5 4 3 2 41 2
R13 | 2964 15 17 22 21 33 35 14 --- 10 | 3 5 5 6 6 4 2 --- 4
R14 | 843 63 64 32 25 17 41 23 --- 14 | 2 6 7 11 7 6 2 --- 5
R15 | 722 35 36 19 13 29 46 19 --- 11 | 2 5 3 3 3 4 2 --- 2
R16 | 632 50 49 23 20 41 38 20 --- 13 | 3 11 69 423 8 5 3 --- 4
R17 | 720 32 31 15 9 18 15 12 --- 7 | 3 6 6 6 6 4 5 --- 5
R18 | 499 20 22 13 11 19 14 10 --- 6 | 3 3 4 5 7 5 4 --- 4
R19 | 1188 63 61 21 7 24 22 19 --- 11 | 4 6 4 3 5 227 4 --- 3
R20 | 548 27 25 19 20 42 36 32 --- 12 | 4 13 7 6 17 4 4 --- 5
R21 | 2062 27 34 17 8 17 14 16 137 7 | 3 5 4 6 4 5 4 24 4
R22 | 1062 41 40 16 11 22 11 18 --- 8 | 3 4 4 4 4 5 5 --- 3
R23 | 832 22 25 24 20 14 20 21 --- 9 | 3 5 5 4 4 4 2 --- 3
R24 | 903 31 32 26 19 23 50 26 --- 12 | 3 12 5 9 9999 4 3 --- 4
XR26 | ---- 37 138 --- --- --- --- 15 --- 24 | 6 42 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1250 33 34 20 15 24 30 19 160 |T 2 7 6 23 6 14 3 18 3
WRMS | 1250 31 33 20 13 18 26 19 160 |NE 2 7 6 23 6 14 3 18 3
MEDI | 903 27 28 17 11 22 20 18 111 |MD 3 5 4 6 5 4 3 11 4
Table 3.1949.2 GPS week: 1949 Day: 2 MJD: 57889
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 | 1079 43 39 17 13 17 42 20 --- 11 | 2 5 2 5 5 3 3 --- 3
R02 | 708 21 23 16 15 14 21 18 73 7 | 1 4 2 5 5 4 2 1 3
R03 | 1106 34 37 28 13 17 22 27 74 10 | 2 3 3 8 6 4 3 2 4
R04 | 768 26 23 14 8 25 14 15 --- 7 | 3 4 4 3 5 3 3 --- 2
R05 | 858 22 25 20 17 17 59 24 --- 13 | 2 4 5 10 7 5 3 --- 5
R06 | 3554 22 23 18 10 20 24 12 --- 7 | 2 6 3 4 5 3 2 --- 2
R07 | 798 36 32 31 14 27 17 15 89 10 | 2 4 4 4 4 6 3 2 3
R08 | 1009 28 29 20 12 24 26 15 --- 9 | 2 5 4 5 7 9999 2 --- 3
XR09 | 1089 21 25 16 13 21 --- 13 --- 8 | 2 4 3 5 3 --- 3 --- 2
R10 | 681 17 23 18 16 22 14 8 --- 7 | 2 6 3 6 4 5 3 --- 3
R11 | 844 21 16 9 15 16 24 8 193 7 | 2 4 2 5 4 3 2 3 2
R13 | 1049 12 20 15 14 25 16 12 --- 7 | 2 5 4 5 5 4 2 --- 3
R14 | 2222 48 49 17 25 26 23 27 --- 12 | 3 8 7 10 6 6 3 --- 5
R15 | 852 28 25 16 14 20 12 12 --- 7 | 2 5 3 4 3 2 2 --- 2
R16 | 452 60 81 37 16 32 39 17 --- 14 | 4 12 69 420 8 4 3 --- 3
R17 | 691 31 27 13 10 22 13 10 --- 7 | 3 6 5 5 5 3 3 --- 4
R18 | 507 22 24 14 13 20 24 10 --- 7 | 3 4 4 4 6 4 4 --- 4
R19 | 2021 61 72 24 16 26 17 18 --- 11 | 3 5 4 4 5 222 4 --- 3
R20 | 904 36 35 17 21 37 29 29 --- 12 | 3 9 5 7 9 4 4 --- 4
R21 | 1468 31 23 20 14 29 21 12 123 9 | 3 5 4 6 5 4 4 3 3
R22 | 958 41 41 18 9 20 24 15 --- 9 | 3 6 4 6 6 4 3 --- 4
R23 | 730 27 38 22 20 12 23 9 --- 8 | 2 5 3 4 4 3 3 --- 3
R24 | 760 27 36 34 25 20 33 38 --- 13 | 3 11 4 10 1 3 4 --- 4
XR26 | ---- 44 48 --- --- --- --- 18 --- 28 | 7 20 --- --- --- --- 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS | 1287 34 37 21 16 23 27 19 119 |T 2 6 6 23 5 14 2 2 3
WRMS | 1287 30 32 21 14 21 23 19 119 |NE 2 6 6 23 5 14 2 2 3
MEDI | 858 28 27 18 14 21 23 15 89 |MD 2 5 4 5 5 4 3 2 3
Table 3.1949.3 GPS week: 1949 Day: 3 MJD: 57890
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 | 902 44 67 17 15 24 20 21 --- 10 | 2 11 5 14 8 3 3 --- 6
R02 | 537 24 21 27 10 22 17 17 73 8 | 1 4 2 3 3 4 2 1 2
R03 | 888 35 34 33 17 15 20 26 77 11 | 2 3 2 6 6 3 2 2 3
R04 | 1108 33 35 26 11 30 13 18 --- 9 | 2 3 3 5 7 3 3 --- 3
R05 | 1293 30 39 19 16 24 45 26 --- 12 | 2 5 5 9 10 4 3 --- 5
R06 | 3459 22 29 19 5 22 19 24 --- 8 | 2 5 3 5 8 3 3 --- 2
R07 | 875 26 29 20 14 21 25 13 83 8 | 1 2 3 3 3 4 2 2 2
R08 | 571 22 28 22 12 21 31 13 --- 9 | 2 4 2 4 7 9999 3 --- 3
XR09 | 1314 20 21 16 12 15 --- 13 --- 7 | 2 3 3 4 4 --- 4 --- 2
R10 | 882 15 33 16 19 32 26 13 --- 9 | 2 7 3 5 6 4 2 --- 2
R11 | 757 31 43 15 10 32 23 7 117 8 | 2 5 4 3 4 2 2 3 2
R13 | 1007 17 22 15 11 22 18 7 --- 6 | 2 4 3 4 3 4 2 --- 2
R14 | 2139 50 49 31 27 25 27 22 --- 13 | 3 10 4 12 7 8 4 --- 6
R15 | 1086 27 32 17 16 37 17 11 --- 9 | 2 5 3 4 3 3 2 --- 2
XR16 | 6213 43 91 --- --- 20 27 19 --- 15 | 3 13 --- --- 6 4 4 --- 3
R17 | 643 33 29 16 11 25 14 14 --- 8 | 2 4 4 4 4 3 3 --- 2
R18 | 682 21 19 16 11 23 9 23 --- 7 | 2 4 3 4 3 4 2 --- 2
XR19 | 1599 50 47 19 9 18 --- 17 --- 11 | 3 4 3 4 5 --- 3 --- 3
R20 | 755 28 40 20 21 35 39 24 --- 12 | 4 11 3 10 6 4 3 --- 4
R21 |>>>>> 25 25 16 11 21 14 15 105 7 | 2 4 3 3 6 4 3 3 3
R22 | 680 41 42 18 7 23 20 13 --- 8 | 2 5 3 4 4 2 2 --- 3
R23 | 664 39 34 22 24 10 18 13 --- 9 | 3 6 4 5 5 3 2 --- 3
XR24 | 1606 29 34 31 30 --- 20 28 --- 14 | 3 7 4 8 --- 2 4 --- 3
XR26 | ---- 63 119 --- --- --- 22 18 --- 23 | 6 16 --- --- --- 9999 3 --- 3
------+---------------------------------------------------+-----------------------------------------------
RMS |99679 31 36 21 15 25 23 18 92 |T 2 6 3 5 5 3 2 2 2
WRMS |99679 30 33 21 13 21 20 18 92 |NE 2 6 3 5 5 3 2 2 2
MEDI | 902 29 34 19 12 22 20 17 83 |MD 2 5 3 4 5 3 3 2 3
Table 3.1949.4 GPS week: 1949 Day: 4 MJD: 57891
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 | 514 41 24 15 24 26 20 18 --- 10 | 2 9 8 13 9 4 3 --- 7
R02 | 835 25 30 28 7 21 17 13 98 8 | 2 8 4 6 5 7 3 3 5
R03 | 1021 30 32 28 9 21 11 26 100 9 | 2 3 3 5 6 4 2 2 3
R04 | 1834 22 26 17 10 15 12 18 --- 6 | 2 3 2 4 6 3 3 --- 3
R05 | 911 23 22 20 19 28 42 24 --- 12 | 2 9 5 12 11 3 4 --- 6
R06 | 2123 22 24 22 18 31 26 17 --- 10 | 3 5 3 5 7 3 3 --- 3
R07 | 716 25 24 14 8 19 12 10 98 6 | 3 3 2 6 5 4 2 7 3
R08 | 729 30 25 27 10 19 24 15 --- 9 | 2 3 2 3 4 9999 4 --- 2
XR09 | 1480 22 26 18 14 20 --- 11 --- 8 | 2 3 2 2 4 --- 2 --- 2
R10 | 732 14 17 19 16 27 15 14 --- 8 | 2 5 4 5 6 4 3 --- 2
R11 | 667 33 34 14 9 30 23 8 61 8 | 2 5 3 2 5 2 2 11 2
R13 | 1057 24 33 12 11 28 19 9 --- 7 | 2 4 4 4 4 5 3 --- 2
R14 | 1812 58 47 39 24 27 22 44 --- 15 | 2 12 5 15 12 6 6 --- 7
R15 | 902 28 29 18 13 22 26 18 --- 9 | 2 4 2 4 4 4 3 --- 2
R16 | 1008 45 31 56 21 33 43 23 --- 16 | 4 9 9999 9999 4 3 5 --- 4
R17 | 797 34 36 16 10 17 18 17 --- 8 | 2 4 3 4 5 6 3 --- 3
R18 | 803 25 25 12 10 17 15 19 --- 7 | 3 4 3 4 5 4 3 --- 3
XR19 | 2003 57 55 23 15 29 --- 15 --- 12 | 3 4 3 4 5 --- 2 --- 3
R20 | 989 46 47 18 19 31 24 22 --- 11 | 5 11 4 9 11 5 3 --- 4
R21 | 706 29 31 19 11 24 14 13 111 7 | 3 3 3 4 6 3 4 7 3
R22 | 681 37 36 16 10 23 16 12 --- 8 | 3 4 3 5 6 5 3 --- 3
R23 | 899 38 38 24 14 15 17 16 --- 9 | 3 6 4 5 4 3 2 --- 3
R24 | 2348 32 37 23 21 40 45 34 --- 14 | 3 15 7 6 9999 3 4 --- 5
XR26 | ---- 41 64 --- --- --- --- 19 --- 27 | 11 15 --- --- --- --- 2 --- 5
------+---------------------------------------------------+-----------------------------------------------
RMS | 1165 33 32 24 15 25 24 20 95 |T 2 6 3 5 6 4 3 6 3
WRMS | 1165 31 31 21 13 23 25 20 95 |NE 2 6 3 5 6 4 3 6 3
MEDI | 902 30 31 19 13 24 19 17 98 |MD 2 4 3 5 5 4 3 7 3
Table 3.1949.5 GPS week: 1949 Day: 5 MJD: 57892
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 | 712 31 39 25 15 15 34 22 --- 10 | 2 4 7 7 8 4 3 --- 4
R02 | 1126 25 22 26 10 25 20 18 86 9 | 2 7 4 6 4 6 4 6 4
R03 | 1027 38 38 28 11 25 10 12 135 9 | 2 4 3 6 4 4 2 3 3
R04 | 1141 30 31 19 8 14 11 17 --- 7 | 2 3 2 3 5 3 2 --- 2
R05 | 688 35 24 35 27 26 57 18 --- 14 | 2 9 5 10 10 4 4 --- 5
R06 | 1080 19 21 20 13 20 19 13 --- 7 | 2 4 3 4 4 4 3 --- 2
R07 | 875 27 29 15 9 23 25 23 116 9 | 3 3 3 6 8 4 3 11 3
R08 | 740 25 24 20 10 11 25 13 --- 7 | 2 6 3 6 4 9999 3 --- 3
XR09 | 1676 20 21 16 8 22 --- 14 --- 8 | 2 3 3 4 5 --- 2 --- 2
R10 | 983 19 24 21 26 20 28 13 --- 9 | 3 6 3 4 4 4 3 --- 2
R11 | 730 27 26 19 12 22 34 15 168 9 | 2 3 4 3 4 2 2 16 1
R13 | 674 23 24 16 18 24 25 8 --- 8 | 2 4 4 4 5 6 3 --- 2
R14 | 1494 47 55 23 35 29 27 25 --- 13 | 2 10 4 18 13 5 4 --- 8
R15 | 1300 37 40 26 25 27 30 10 --- 11 | 3 4 2 3 4 4 2 --- 2
R16 | 919 37 51 48 15 23 46 20 --- 14 | 4 6 9999 9999 5 2 4 --- 4
R17 | 813 29 23 16 10 18 20 15 --- 7 | 3 4 3 4 4 6 3 --- 3
R18 | 706 26 24 16 15 15 16 9 --- 7 | 3 4 2 3 4 6 3 --- 3
R19 | 2212 58 59 14 9 33 17 15 --- 11 | 3 4 5 6 5 9999 3 --- 3
R20 | 1092 33 37 17 18 26 32 22 --- 10 | 3 11 3 9 11 4 3 --- 4
R21 | 792 32 34 18 11 19 21 15 366 8 | 3 4 3 4 5 3 4 12 3
R22 | 1170 42 35 22 16 20 16 17 --- 9 | 2 6 4 6 8 5 3 --- 4
R23 | 902 33 39 25 18 14 19 18 --- 9 | 3 5 4 5 4 3 3 --- 3
R24 | 2860 24 34 22 27 32 60 31 --- 15 | 3 13 6 5 9999 4 3 --- 4
XR26 | ---- 39 68 --- --- --- --- 14 --- 24 | 9 12 --- --- --- --- 2 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1207 33 35 24 18 22 30 18 200 |T 2 5 3 5 5 4 2 9 3
WRMS | 1207 32 33 22 16 21 33 18 200 |NE 2 5 3 5 5 4 2 9 3
MEDI | 983 30 31 20 15 22 25 15 135 |MD 2 4 3 5 5 4 3 11 3
Table 3.1949.6 GPS week: 1949 Day: 6 MJD: 57893
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 | 493 45 48 31 19 12 41 16 --- 12 | 2 3 3 4 5 3 3 --- 2
R02 | 823 18 13 12 14 21 20 16 111 7 | 2 3 3 3 2 2 2 2 2
R03 | 764 28 30 22 19 15 19 16 163 8 | 2 3 3 4 3 3 2 1 2
R04 | 1116 35 32 22 11 23 13 13 --- 8 | 1 2 2 2 4 2 2 --- 2
R05 | 641 35 40 20 7 18 57 26 --- 12 | 1 5 3 4 6 3 4 --- 2
R06 | 1047 18 20 17 18 23 26 10 --- 8 | 2 3 2 3 4 3 4 --- 2
R07 | 937 31 34 16 16 24 30 15 104 9 | 2 2 2 3 6 3 2 2 2
R08 | 992 23 21 22 14 19 15 18 --- 8 | 2 5 2 5 3 9999 3 --- 3
XR09 | 2094 17 22 21 10 18 --- 18 --- 8 | 2 2 3 3 3 --- 2 --- 2
R10 | 1370 15 18 13 16 20 27 9 --- 7 | 2 4 2 3 2 2 2 --- 2
R11 | 792 32 37 13 12 21 19 17 191 8 | 2 3 3 2 3 2 2 3 1
R13 | 1023 21 24 15 24 22 28 14 --- 9 | 2 3 3 3 3 5 4 --- 2
R14 | 2088 47 45 16 40 27 32 24 --- 14 | 2 4 2 12 9 4 4 --- 5
R15 | 1018 30 36 22 16 20 25 10 --- 8 | 3 4 2 2 2 2 2 --- 2
R16 | 1837 34 47 50 18 29 57 14 --- 15 | 2 4 9999 9999 4 2 3 --- 2
R17 | 792 27 25 17 11 26 31 13 --- 9 | 3 4 3 3 4 4 3 --- 2
R18 | 680 22 23 15 11 15 26 16 --- 7 | 3 3 2 2 2 5 3 --- 2
R19 | 2281 51 36 29 17 28 23 15 --- 12 | 3 6 3 4 4 9999 4 --- 2
R20 | 768 26 27 20 22 23 33 29 --- 11 | 3 9 3 7 6 4 3 --- 3
R21 | 826 33 27 16 14 22 35 12 373 9 | 3 3 2 3 3 3 3 4 2
R22 | 1997 32 49 13 10 17 20 12 --- 7 | 2 6 3 5 6 3 3 --- 3
R23 | 516 35 31 30 27 13 29 23 --- 11 | 3 3 3 4 3 2 3 --- 2
R24 | 1567 36 34 26 23 36 51 26 --- 14 | 3 6 3 4 1 4 3 --- 2
XR26 | ---- 40 97 --- --- --- --- 18 --- 27 | 10 8 --- --- --- --- 3 --- 4
------+---------------------------------------------------+-----------------------------------------------
RMS | 1219 32 33 23 18 22 32 17 212 |T 2 4 2 3 3 3 2 2 2
WRMS | 1219 31 32 20 15 20 30 17 212 |NE 2 4 2 3 3 3 2 2 2
MEDI | 992 31 31 20 16 21 27 16 163 |MD 2 3 3 3 3 3 3 2 2
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