[IGSREPORT-24392] Wk 1891 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Apr 21 18:25:14 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1891 (Apr 03, 2016 - Apr 09, 2016)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1891.
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:
igl1891[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1891 in the SP3 format.
igl18917.sum Combination Report for GPS Week 1891.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -5.0 ns
1 | -8.0 ns
2 | -7.0 ns
3 | -10.6 ns
4 | -7.6 ns
5 | -5.5 ns
6 | -8.6 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
----+--------+---------------
4 | GFZ | R01
4 | GRG | 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 1.1891, 1a.1891).
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 2.1891.0-6)
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 3.1891.0-6).
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 1891 summary. (Apr 03, 2016 - Apr 09, 2016)
Table 1.1891.a GPS week : 1891 MJD: 57481.0-57487.0
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 8 12 -22 5 .19 26 27 | --- --- --- ---
| 1 2 2 17 28 37 .04 | --- ---
cof n/a| -1 0 8 10 -15 -23 .18 31 30 | --- --- --- ---
| 2 1 2 26 41 44 .03 | --- ---
emx n/a| 0 -1 5 -50 -67 -80 .07 27 27 | -8058 435 3741 7535
| 1 2 3 30 35 45 .06 | 7590 1442
esx n/a| 0 0 0 18 1 -4 -.14 17 16 | -36172 25 3982 13539
| 0 0 1 16 20 30 .03 | 71828 3453
gfz n/a| 0 0 -2 40 67 30 -.04 20 19 | 0 483 3715 7390
| 1 0 3 18 25 44 .06 | 0 3163
grg n/a| 0 0 0 -40 18 54 -.21 35 33 | -427252 627 8602 613887
| 1 2 2 21 24 52 .10 | 14682 2866
iac n/a| 0 0 -5 -14 -13 -24 .14 19 19 | -5478 153 3946 11685
| 1 1 2 39 60 64 .06 | 2878 2161
mcc n/a| 0 -1 -1 68 32 560 .26 190 190 | --- --- --- ---
| 5 4 24 219 99 837 .23 | --- ---
Table 1.1891.b GPS week : 1891 MJD: 57481.0-57487.0
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 13 12 12 108 22 13 |
R02 | 8 6 8 7 8 9 10 |
R03 | 7 7 7 8 8 9 10 |
R04 | 10 7 8 8 8 8 9 |
R05 | 14 11 14 12 14 10 11 |
R06 | 11 10 9 9 11 8 8 |
R07 | 9 8 8 9 8 9 8 |
R08 | 10 8 8 8 8 9 8 |
R09 | 9 7 8 9 8 9 8 |
R10 | 10 9 9 9 8 8 9 |
R13 | 11 9 8 10 10 11 10 |
R14 | 14 11 10 11 10 16 19 |
R15 | 11 11 13 18 14 14 13 |
R16 | 18 12 14 12 14 21 17 |
R17 | 10 11 12 12 10 9 11 |
R18 | 8 7 7 9 11 8 8 |
R19 | 10 11 10 9 13 10 8 |
R20 | 15 12 13 12 17 12 13 |
R21 | 9 7 9 10 11 8 10 |
R22 | 9 9 8 11 11 10 9 |
R23 | 7 10 12 11 7 9 8 |
R24 | 19 13 17 12 12 13 14 |
R26 | 22 48 45 74 56 85 42 |
Table 1.1891.c GPS week : 1891 MJD: 57481.0-57487.0
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 1891 0 | -43 12 152 -588 -1692 2763 84.1 1586 1586 | -4949 0
brd 1891 1 | 37 -5 98 -894 -1823 3477 86.5 1366 1366 | -7990 0
brd 1891 2 | -35 55 108 -1856 -678 3903 86.0 1439 1439 | -7042 0
brd 1891 3 | 13 -3 33 559 -950 5278 86.1 1745 1745 | -10550 0
brd 1891 4 | -20 83 106 -1180 87 2326 86.3 1964 1964 | -7578 0
brd 1891 5 | 22 8 154 -660 849 1899 85.3 1705 1705 | -5480 0
brd 1891 6 | 66 -25 64 -115 -99 284 84.8 1580 1580 | -8571 0
-------------+------------------------------------------------------------+----------------
brd 1891 mean| 5 17 102 -676 -615 2847 85.6 1626 1626 | -7451 0
brd 1891 sdev| 40 38 43 768 969 1589 .9 200 200 | 1891 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 2.1891.0 GPS week: 1891 Day: 0 MJD: 57481
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 8 -21 -61 44 .19 24 24 | --- --- --- ---
cof n/a| -1 0 11 -40 -59 -16 .15 31 27 | --- --- --- ---
emx n/a| -2 0 4 -106 -86 -95 .06 29 31 | -8258 1302 4330 7281
esx n/a| 0 0 -1 -9 -20 28 -.09 19 18 | -9582 2046 4442 8335
gfz n/a| 0 0 -4 50 75 -23 -.02 23 19 | 0 3442 4284 6899
grg n/a| -2 0 3 -47 19 -4 -.33 39 35 | -427986 3531 7067 618023
iac n/a| 0 0 -2 62 11 -18 .08 20 20 | -4727 2329 4434 7184
mcc n/a| 3 0 -28 287 119 794 .13 85 85 | --- --- --- ---
Table 2.1891.1 GPS week: 1891 Day: 1 MJD: 57482
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 6 28 -56 24 .20 25 27 | --- --- --- ---
cof n/a| -3 0 5 30 -44 34 .16 27 30 | --- --- --- ---
emx n/a| 1 -1 0 -53 -90 -93 .07 24 25 | -8676 -289 3412 6676
esx n/a| 0 0 0 13 -18 15 -.15 16 15 | -10821 -232 3414 7490
gfz n/a| -2 1 2 66 53 -1 -.04 19 20 | 0 -633 3460 6512
grg n/a| 0 1 0 -30 49 106 -.23 34 32 | -412748 459 15448 608083
iac n/a| 0 0 -4 -39 40 -11 .19 18 18 | -5740 -1551 3462 6574
mcc n/a| -1 2 -30 -41 87 519 .07 129 129 | --- --- --- ---
Table 2.1891.2 GPS week: 1891 Day: 2 MJD: 57483
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 8 13 -4 48 .14 25 26 | --- --- --- ---
cof n/a| -1 0 6 15 -32 -16 .14 31 27 | --- --- --- ---
emx n/a| 0 0 2 -52 -61 -90 .08 24 23 | -16207 194 3755 8128
esx n/a| 1 0 1 11 23 -34 -.12 18 16 | -197648 755 4895 42717
gfz n/a| 0 -1 -1 54 60 21 -.09 20 21 | 0 740 3624 7772
grg n/a| -2 -1 3 -83 4 127 -.26 38 35 | -407398 594 13724 597627
iac n/a| 2 1 -9 -22 -32 -18 .17 19 19 | 540 1347 4710 36717
mcc n/a| -5 -5 11 -341 86 214 .11 177 177 | --- --- --- ---
Table 2.1891.3 GPS week: 1891 Day: 3 MJD: 57484
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 6 9 12 -17 .13 24 27 | --- --- --- ---
cof n/a| 0 3 7 -6 66 30 .19 32 29 | --- --- --- ---
emx n/a| 0 -2 6 -48 1 -2 -.01 27 26 | -12424 -1249 4223 8282
esx n/a| 0 0 0 16 33 34 -.14 16 15 | -13099 -4733 4250 9917
gfz n/a| 0 0 1 39 87 119 -.09 23 18 | 0 -3507 4076 8041
grg n/a| 0 0 -2 -22 -23 48 -.14 35 37 | -429454 -3513 4227 616704
iac n/a| 1 0 -8 -7 -124 -156 .16 20 20 | -8226 -2257 4262 8379
mcc n/a| -4 -1 27 -22 -154 -670 .23 134 134 | --- --- --- ---
Table 2.1891.4 GPS week: 1891 Day: 4 MJD: 57485
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 6 17 -3 11 .20 26 30 | --- --- --- ---
cof n/a| 1 -1 5 36 -26 -74 .19 31 32 | --- --- --- ---
emx n/a| 0 -3 11 -62 -110 -34 -.01 26 27 | 7946 386 3263 8123
esx n/a| 1 0 -2 35 3 -36 -.18 18 17 | -15846 -2455 3560 10291
gfz n/a| -2 0 -3 26 21 23 .09 20 21 | 0 -130 3403 8746
grg n/a| 1 2 -3 -38 44 80 -.30 36 32 | -452780 -237 9515 622171
iac n/a| 0 0 -5 -16 60 -30 .04 21 21 | -7328 -279 3503 8965
mcc n/a| -2 -10 29 204 38 -51 .71 154 154 | --- --- --- ---
Table 2.1891.5 GPS week: 1891 Day: 5 MJD: 57486
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 10 33 -13 -17 .25 28 29 | --- --- --- ---
cof n/a| -6 2 10 25 -3 -54 .22 32 31 | --- --- --- ---
emx n/a| 1 -6 8 -19 -66 -136 .14 28 29 | -9617 3172 3795 7883
esx n/a| 0 1 0 40 -13 -24 -.17 17 16 | -17247 6060 3879 8462
gfz n/a| 0 0 -3 14 72 32 -.09 19 15 | 0 5644 3724 7677
grg n/a| -1 -2 -1 -43 9 32 -.16 32 28 | -432888 4964 6827 617968
iac n/a| 2 2 -4 -64 -10 47 .20 18 18 | -6273 3220 3849 7817
mcc n/a| 0 3 -17 191 -49 1289 .40 284 284 | --- --- --- ---
Table 2.1891.6 GPS week: 1891 Day: 6 MJD: 57487
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 4 12 6 -29 -55 .24 32 30 | --- --- --- ---
cof n/a| 0 2 11 9 -7 -68 .19 33 31 | --- --- --- ---
emx n/a| 0 1 4 -12 -61 -109 .14 31 29 | -9172 -468 3414 6374
esx n/a| 0 0 -1 19 0 -13 -.13 16 16 | 11034 -1265 3437 7564
gfz n/a| 0 0 -5 29 102 43 -.02 20 16 | 0 -2172 3434 6084
grg n/a| 1 -4 2 -18 26 -10 -.06 34 31 | -427515 -1406 3411 616639
iac n/a| 0 1 -2 -14 -39 17 .12 17 17 | -6597 -1734 3405 6161
mcc n/a| 10 0 0 200 96 1830 .17 368 368 | --- --- --- ---
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 3.1891.0 GPS week: 1891 Day: 0 MJD: 57481
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 2646 35 34 31 18 28 37 29 --- 13 | 91 9999 60 50 275 336 57 --- 68
R02E | 1423 18 24 11 14 19 22 18 --- 7 | 36 40 43 42 44 39 44 --- 39
R03E | 729 18 19 21 13 14 19 13 108 7 | 35 38 48 40 35 37 38 46 35
R04E | 1063 23 31 27 11 17 33 23 --- 9 | 48 57 54 46 46 53 35 --- 42
R05E | 1061 25 33 41 23 32 44 24 --- 13 | 42 48 45 45 60 57 43 --- 41
R06E | 708 26 39 29 14 27 34 16 --- 10 | 39 59 44 45 43 39 37 --- 38
R07E | 690 20 27 18 12 24 28 16 79 8 | 31 35 34 27 28 36 24 68 25
R08E | 2130 21 27 25 13 20 39 17 --- 9 | 36 36 30 32 36 42 34 --- 30
R09 | 1878 27 37 18 16 20 26 15 --- 9 | 33 42 29 38 42 37 28 --- 31
R10 | 1841 21 19 24 17 24 31 20 --- 9 | 37 43 44 39 29 26 33 --- 29
R13 | 543 24 24 42 15 17 34 18 --- 11 | 38 41 38 33 29 35 29 --- 27
R14 | 1129 35 52 34 31 23 42 21 --- 13 | 32 40 45 55 45 36 41 --- 38
R15 | 4153 31 29 25 18 24 38 17 --- 11 | 48 49 41 38 38 32 26 --- 31
XR16 | 940 13 28 34 --- 27 82 22 --- 17 | 39 44 39 --- 39 33 37 --- 32
XR17 | 710 23 24 18 --- 13 26 16 --- 9 | 59 60 49 --- 37 34 29 --- 39
R18 | 800 22 22 14 14 14 21 17 --- 7 | 47 47 39 39 34 21 25 --- 31
R19 | 1081 35 23 16 11 17 30 19 --- 9 | 64 52 45 36 34 31 26 --- 35
R20 | 780 17 28 48 18 16 91 15 --- 15 | 47 52 59 46 44 32 32 --- 39
R21 | 613 20 18 23 16 14 40 11 62 8 | 60 60 65 49 36 31 41 32 45
R22 | 805 22 26 18 16 23 34 13 --- 9 | 63 65 63 55 39 34 39 --- 47
R23 | 1665 10 19 20 11 10 24 13 --- 6 | 26 37 31 33 28 27 22 --- 25
R24 | 1013 24 55 52 41 45 51 41 --- 19 | 77 100 98 86 47 49 40 --- 62
XR26 | ---- 26 372 --- --- --- --- 18 --- 22 | 56 320 --- --- --- --- 49 --- 46
------+---------------------------------------------------+-----------------------------------------------
RMS | 1586 24 31 29 19 23 39 20 85 |T 47 62 47 43 49 49 35 48 38
WRMS | 1586 24 27 31 18 19 35 20 85 |NE 48 53 50 48 37 34 32 --- 37
MEDI | 1013 23 27 24 15 20 34 17 79 |MD 42 47 44 40 38 35 35 46 38
Table 3.1891.1 GPS week: 1891 Day: 1 MJD: 57482
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1152 35 26 40 18 27 32 24 --- 12 | 72 9999 35 67 241 314 56 --- 67
R02E | 940 12 15 12 12 15 18 8 --- 5 | 28 27 24 23 35 34 27 --- 24
R03E | 1407 14 17 14 10 14 33 12 149 7 | 22 25 27 25 30 28 24 49 21
R04E | 759 22 16 18 11 14 23 15 --- 7 | 28 34 31 27 29 35 18 --- 23
R05E | 962 26 30 24 23 23 32 20 --- 10 | 24 30 34 43 48 42 42 --- 35
R06E | 1629 25 26 34 22 13 22 17 --- 10 | 33 38 37 40 28 36 30 --- 28
R07E | 663 23 34 26 11 18 22 9 136 8 | 34 43 32 26 29 29 24 37 25
R08E | 1513 18 19 17 17 15 28 19 --- 8 | 24 25 19 29 27 35 26 --- 22
R09 | 1966 21 27 15 14 14 27 8 --- 7 | 23 22 25 34 30 16 22 --- 24
R10 | 1393 17 24 26 14 19 40 14 --- 9 | 33 36 36 28 28 29 27 --- 25
R13 | 595 30 23 20 11 25 19 12 --- 8 | 22 26 23 32 36 26 18 --- 22
R14 | 867 32 32 30 24 21 35 17 --- 11 | 33 47 48 34 38 23 25 --- 28
R15 | 3194 33 47 20 17 19 44 19 --- 10 | 37 44 20 25 31 26 16 --- 18
XR16 | 778 32 44 27 --- 12 37 18 --- 12 | 33 46 34 --- 28 38 26 --- 22
XR17 | 609 30 36 24 --- 21 17 17 --- 11 | 41 44 32 --- 31 29 23 --- 25
R18 | 709 19 23 11 12 9 32 14 --- 7 | 29 31 19 24 22 17 15 --- 18
R19 | 1298 28 31 24 17 18 25 30 --- 10 | 38 40 38 38 29 31 14 --- 26
R20 | 650 19 19 31 16 19 63 22 --- 12 | 28 30 30 36 42 28 20 --- 25
R21 | 972 12 16 17 11 10 38 7 96 6 | 42 44 48 37 44 30 41 27 39
R22 | 711 23 30 20 15 18 37 15 --- 9 | 41 44 39 31 33 15 40 --- 31
R23 | 2086 22 24 16 19 29 32 13 --- 9 | 15 22 29 23 40 25 22 --- 18
R24 | 832 42 43 33 11 19 41 33 --- 13 | 67 66 55 38 36 34 31 --- 39
XR26 | ---- 64 508 --- --- --- --- 34 --- 47 | 69 490 --- --- --- --- 41 --- 37
------+---------------------------------------------------+-----------------------------------------------
RMS | 1365 25 27 24 16 19 34 18 129 |T 35 57 32 33 42 41 27 37 27
WRMS | 1365 27 30 25 15 20 32 18 129 |NE 35 41 35 31 33 27 24 --- 25
MEDI | 940 23 26 20 14 18 32 17 136 |MD 33 36 32 31 31 29 25 37 25
Table 3.1891.2 GPS week: 1891 Day: 2 MJD: 57483
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 2067 23 35 22 18 22 46 34 --- 12 | 68 9999 64 71 467 257 53 --- 65
R02E | 1463 12 15 15 14 13 33 16 --- 7 | 34 34 38 33 30 41 29 --- 29
R03E | 916 12 19 15 12 16 24 17 176 7 | 36 38 40 38 41 43 33 76 35
R04E | 1548 16 29 22 11 15 33 13 --- 7 | 34 39 35 38 37 47 28 --- 32
R05E | 1198 20 34 28 31 30 49 29 --- 13 | 52 58 49 58 55 64 42 --- 45
R06E | 3312 25 43 24 17 15 33 15 --- 9 | 40 56 40 33 26 30 33 --- 28
R07E | 721 22 27 25 11 15 30 10 213 8 | 37 39 35 30 28 42 29 90 28
R08E | 812 21 45 20 19 14 23 14 --- 8 | 33 49 28 33 32 35 29 --- 28
R09 | 1583 17 21 21 16 12 21 14 --- 7 | 27 31 23 32 31 22 29 --- 25
R10 | 818 13 23 33 17 20 24 14 --- 9 | 30 39 33 32 21 28 30 --- 25
R13 | 852 29 32 25 9 12 25 11 --- 8 | 32 36 30 22 28 20 24 --- 21
R14 | 649 24 30 22 25 13 40 19 --- 10 | 36 40 40 32 34 38 30 --- 28
R15 | 2959 41 35 13 17 35 31 29 --- 13 | 48 44 27 24 52 27 21 --- 23
XR16 | 859 16 29 34 --- 16 62 14 --- 13 | 36 33 31 --- 41 29 31 --- 29
XR17 | 813 30 22 22 --- 14 19 26 --- 11 | 49 42 41 --- 28 40 18 --- 29
R18 | 591 15 13 7 11 15 36 12 --- 7 | 34 31 25 31 31 25 21 --- 25
R19 | 683 23 24 21 17 19 42 15 --- 9 | 44 42 40 31 26 34 20 --- 26
R20 | 680 30 45 31 23 20 60 24 --- 13 | 45 62 41 46 38 35 27 --- 32
R21 | 676 18 17 28 14 19 36 11 131 9 | 48 46 55 46 42 27 39 36 41
R22 | 706 22 25 25 10 12 30 14 --- 8 | 51 49 53 39 39 20 28 --- 37
XR23 | 1913 19 41 --- 11 --- 41 15 --- 11 | 26 44 --- 27 --- 34 20 --- 20
R24 | 878 49 48 33 22 38 70 22 --- 16 | 63 63 57 58 49 34 35 --- 44
XR26 | ---- 55 359 --- --- --- --- 36 --- 44 | 44 376 --- --- --- --- 68 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1438 25 31 24 18 20 38 19 177 |T 41 58 39 37 56 44 31 67 31
WRMS | 1438 26 27 23 16 21 35 19 177 |NE 42 43 39 33 38 29 26 --- 28
MEDI | 852 22 29 22 16 15 33 15 176 |MD 37 42 40 33 34 34 29 76 29
Table 3.1891.3 GPS week: 1891 Day: 3 MJD: 57484
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 2188 24 55 11 19 24 45 31 --- 11 | 73 9999 66 63 693 545 41 --- 54
R02E | 1491 14 54 19 11 18 23 10 --- 6 | 46 66 45 41 45 46 38 --- 40
R03E | 1184 14 15 28 12 16 18 12 112 7 | 44 48 44 37 41 46 38 55 38
R04E | 930 11 13 22 13 17 27 18 --- 7 | 65 66 70 65 74 61 52 --- 62
R05E | 1287 31 55 30 19 32 39 17 --- 12 | 72 86 65 67 69 68 59 --- 62
R06E | 2376 19 19 30 13 16 28 19 --- 9 | 45 61 55 57 56 52 42 --- 49
R07E | 976 18 16 32 14 18 26 16 78 9 | 44 48 66 56 58 61 39 100 50
R08E | 1344 25 22 14 13 16 19 13 --- 7 | 44 47 43 44 46 45 39 --- 40
R09 | 1280 22 25 19 18 11 29 15 --- 8 | 42 53 52 52 50 47 37 --- 43
R10 | 844 10 22 26 16 19 31 13 --- 8 | 43 48 51 53 47 40 44 --- 45
R13 | 826 34 39 21 15 18 31 12 --- 9 | 46 51 42 44 44 36 28 --- 36
R14 | 789 29 30 16 23 16 44 21 --- 11 | 40 48 46 46 48 42 31 --- 38
R15 | 5370 43 46 41 12 62 60 23 --- 18 | 51 55 53 44 98 44 31 --- 44
XR16 | 951 19 20 24 --- 11 46 17 --- 11 | 54 66 59 --- 51 52 41 --- 49
XR17 | 797 26 32 25 --- 11 37 24 --- 12 | 59 67 62 --- 52 49 36 --- 47
R18 | 736 18 25 26 13 13 41 15 --- 9 | 47 52 54 45 52 36 35 --- 41
R19 | 1262 20 18 19 10 19 35 18 --- 8 | 53 53 53 47 53 41 29 --- 43
R20 | 948 22 16 24 17 22 51 26 --- 11 | 69 62 65 72 60 70 39 --- 60
R21 | 1902 23 22 22 20 20 32 23 187 10 | 61 57 64 65 54 47 40 39 53
R22 | 636 30 31 30 14 19 24 28 --- 10 | 59 59 70 53 48 36 30 --- 45
R23 | 981 25 21 45 20 19 18 17 --- 11 | 34 38 60 52 49 51 31 --- 42
R24 | 1025 20 30 36 18 16 38 29 --- 11 | 56 70 71 57 61 53 39 --- 52
XR26 | ---- 87 165 --- --- --- --- 62 --- 73 | 119 132 --- --- --- --- 59 --- 54
------+---------------------------------------------------+-----------------------------------------------
RMS | 1745 24 32 27 16 23 35 20 134 |T 55 60 57 53 84 71 39 64 47
WRMS | 1745 27 29 26 15 18 37 20 134 |NE 49 55 56 49 56 44 32 --- 43
MEDI | 981 22 25 24 14 18 31 18 112 |MD 51 55 55 52 52 47 39 55 45
Table 3.1891.4 GPS week: 1891 Day: 4 MJD: 57485
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
------+---------------------------------------------------+-----------------------------------------------
XR01E |16512 130 >>>> --- --- 3804 2549 89 --- 108 | 175 9999 --- --- 9999 9999 32 --- 76
R02E | 1490 20 46 20 13 16 25 20 --- 8 | 45 63 39 41 45 45 38 --- 39
R03E | 924 19 18 17 13 17 33 17 104 8 | 35 34 31 30 36 48 25 24 28
R04E | 2062 12 8 24 14 15 20 18 --- 7 | 42 41 47 41 43 42 36 --- 39
R05E | 1296 22 29 35 19 33 36 37 --- 13 | 53 60 64 67 87 60 35 --- 58
R06E | 1416 27 37 41 18 16 19 15 --- 10 | 40 43 46 41 48 42 43 --- 39
R07E | 606 20 13 25 14 14 23 14 138 8 | 70 62 50 52 52 53 47 45 51
R08E | 1640 23 19 15 12 15 19 16 --- 7 | 36 35 24 30 26 37 30 --- 26
R09M | 1185 23 26 15 17 8 33 9 --- 7 | 23 27 30 35 27 36 25 --- 25
R10M | 673 19 24 18 18 20 21 12 --- 8 | 29 38 37 38 34 28 30 --- 30
R13 | 847 38 35 13 14 25 30 12 --- 10 | 44 43 26 28 26 35 20 --- 23
R14 | 735 21 25 25 20 12 36 21 --- 9 | 29 38 42 44 41 24 26 --- 32
R15 | 6999 41 43 27 20 33 36 27 --- 13 | 44 47 32 39 41 28 25 --- 28
XR16 | 704 22 41 34 --- 16 44 21 --- 13 | 39 47 51 --- 33 33 31 --- 29
XR17M | 653 21 33 19 --- 14 28 21 --- 10 | 50 60 50 --- 49 29 28 --- 39
R18M | 518 17 18 26 14 21 55 11 --- 10 | 39 34 47 35 25 43 32 --- 31
R19 | 789 42 37 33 22 22 36 14 --- 12 | 43 40 42 41 38 19 21 --- 27
R20M | 1130 28 54 40 33 24 65 43 --- 17 | 44 69 55 39 31 33 40 --- 33
R21M | 1656 37 45 26 16 18 31 26 203 11 | 61 71 63 55 47 49 55 35 50
R22 | 754 33 36 23 17 15 31 26 --- 10 | 47 47 42 34 22 27 22 --- 27
R23 | 925 13 15 11 21 10 23 11 --- 6 | 19 20 34 32 28 16 21 --- 22
R24 | 869 19 21 31 13 20 59 23 --- 12 | 48 48 62 51 59 21 36 --- 44
XR26M | ---- 66 539 --- --- --- --- 47 --- 55 | 99 531 --- --- --- --- 31 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1963 26 31 26 18 20 36 21 154 |T 50 68 43 40 39 35 31 34 36
WRMS | 1963 30 32 27 17 21 32 21 154 |NE 39 41 41 38 36 25 25 --- 29
MEDI | 924 22 33 25 17 16 31 20 138 |MD 44 43 42 39 38 35 31 35 32
Table 3.1891.5 GPS week: 1891 Day: 5 MJD: 57486
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
------+---------------------------------------------------+-----------------------------------------------
XR01E |10598 38 49 --- --- 37 46 33 --- 21 | 51 9999 --- --- 798 597 79 --- 61
R02E | 1565 26 29 16 14 20 20 20 --- 8 | 43 47 35 47 42 38 40 --- 39
R03E | 808 25 20 23 12 18 28 18 108 9 | 40 37 35 32 36 52 28 25 30
R04E | 1022 19 19 24 9 16 19 18 --- 7 | 33 34 38 36 41 47 26 --- 32
R05E | 1602 16 33 37 16 23 32 17 --- 10 | 50 62 53 47 47 54 37 --- 42
R06E | 1701 13 16 24 11 20 31 15 --- 8 | 37 35 43 41 46 45 41 --- 38
R07E | 824 37 45 22 10 14 20 15 387 8 | 83 80 68 63 59 56 52 51 60
R08E | 2021 24 28 36 10 18 14 10 --- 8 | 36 36 40 26 29 29 26 --- 25
R09 | 918 31 29 23 17 18 24 13 --- 9 | 24 26 31 32 29 28 26 --- 25
R10 | 833 23 28 22 15 13 20 12 --- 7 | 31 37 39 32 30 22 24 --- 26
R13 | 838 31 54 22 19 22 44 13 --- 10 | 42 62 35 43 30 26 24 --- 28
R14 | 1137 45 46 45 31 26 48 30 --- 16 | 41 71 38 50 37 39 28 --- 31
R15 | 5481 42 42 26 30 30 41 23 --- 14 | 45 43 28 23 45 30 24 --- 26
XR16 | 591 44 58 58 --- 17 75 25 --- 21 | 59 66 56 --- 35 42 29 --- 32
XR17 | 760 24 24 16 --- 13 22 13 --- 8 | 45 47 40 --- 39 28 24 --- 32
R18 | 525 12 16 17 14 9 39 16 --- 8 | 36 39 34 43 36 47 24 --- 33
R19 | 1713 25 31 19 21 12 36 19 --- 9 | 38 44 34 44 29 17 23 --- 29
R20 | 932 28 23 33 11 17 57 22 --- 12 | 45 52 49 29 36 23 21 --- 28
R21 | 588 26 30 23 12 13 21 13 283 7 | 49 51 47 46 40 36 43 32 41
R22 | 588 38 39 24 16 11 19 21 --- 9 | 41 42 32 35 34 25 16 --- 25
R23 | 1333 19 17 27 23 15 18 19 --- 9 | 21 30 39 39 26 28 15 --- 25
R24 | 834 25 32 50 19 23 36 17 --- 12 | 36 47 54 39 32 26 26 --- 28
XR26 | ---- 117 134 --- --- --- --- 60 --- 84 | 158 90 --- --- --- --- 33 --- 60
------+---------------------------------------------------+-----------------------------------------------
RMS | 1704 28 32 28 17 19 32 18 284 |T 47 49 41 39 71 60 30 36 34
WRMS | 1704 29 31 29 16 15 28 18 284 |NE 40 50 39 39 33 29 23 --- 28
MEDI | 918 26 30 24 15 17 28 18 283 |MD 41 44 39 39 36 30 26 32 31
Table 3.1891.6 GPS week: 1891 Day: 6 MJD: 57487
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
------+---------------------------------------------------+-----------------------------------------------
R01E | 1671 41 41 28 19 28 27 32 --- 13 | 77 9999 50 62 677 358 57 --- 64
R02E | 1376 24 33 44 15 17 27 12 --- 10 | 63 67 57 62 65 69 60 --- 59
R03E | 1274 28 22 26 14 21 37 14 116 9 | 58 56 47 54 49 69 50 35 50
R04E | 899 20 19 22 11 20 36 16 --- 9 | 61 63 50 56 54 67 54 --- 54
R05E | 918 28 26 35 16 19 35 18 --- 10 | 41 44 53 47 53 45 46 --- 43
R06E | 1053 17 15 19 16 15 21 13 --- 7 | 46 49 45 54 59 57 49 --- 50
R07E | 896 20 21 21 15 21 27 13 538 8 | 65 71 64 59 62 79 63 83 61
R08E | 2343 21 30 24 12 15 24 9 --- 7 | 44 49 34 40 46 56 45 --- 40
R09 | 765 21 23 24 11 16 38 10 --- 8 | 28 33 28 39 44 37 29 --- 32
R10 | 841 24 18 27 18 14 27 9 --- 8 | 39 36 33 39 34 25 30 --- 30
R13 | 473 32 23 19 12 24 33 14 --- 9 | 43 38 29 29 29 27 26 --- 25
R14 | 858 65 67 64 27 31 59 24 --- 19 | 50 65 41 47 34 31 27 --- 30
R15 | 4929 48 51 20 18 34 36 21 --- 13 | 53 55 34 32 48 27 29 --- 29
XR16 | 619 21 20 59 --- 21 38 24 --- 16 | 33 37 39 --- 34 29 34 --- 29
XR17 | 718 29 29 26 --- 23 19 14 --- 11 | 59 57 55 --- 38 35 29 --- 37
R18 | 585 17 21 20 9 14 35 10 --- 7 | 50 51 49 38 35 25 32 --- 35
R19 | 2034 24 22 25 11 9 21 16 --- 7 | 57 56 52 38 40 39 27 --- 37
R20 | 621 45 49 26 27 20 40 22 --- 12 | 64 61 67 66 51 41 39 --- 51
R21 | 563 32 34 30 19 20 22 12 323 9 | 67 72 69 61 54 52 52 36 55
R22 | 492 30 35 27 9 13 22 18 --- 8 | 62 66 53 42 38 29 36 --- 40
R23 | 1404 20 22 15 18 12 19 18 --- 7 | 24 23 26 36 27 32 19 --- 24
R24 | 758 31 41 50 14 14 56 27 --- 13 | 58 62 60 48 45 31 38 --- 42
XR26 | ---- 64 213 --- --- --- --- 27 --- 42 | 62 191 --- --- --- --- 28 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1579 32 33 31 16 20 34 17 368 |T 52 59 47 47 73 57 39 51 40
WRMS | 1579 30 31 29 16 16 31 17 368 |NE 47 50 41 38 36 30 29 --- 32
MEDI | 858 28 26 26 15 19 27 16 323 |MD 57 56 49 47 45 37 36 36 40
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