[IGSREPORT-24362] Wk 1889 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Apr 7 17:31:22 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1889 (Mar 20, 2016 - Mar 26, 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 2.1889.
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:
igl1889[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1889 in the SP3 format.
igl18897.sum Combination Report for GPS Week 1889.
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 | -4.6 ns
1 | -2.0 ns
2 | 1.4 ns
3 | -2.3 ns
4 | 14.6 ns
5 | -4.9 ns
6 | -5.0 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 1.1889, 1a.1889).
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 2.1889.0-6)
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 3.1889.0-6).
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 1889 summary. (Mar 20, 2016 - Mar 26, 2016)
Table 1.1889.a GPS week : 1889 MJD: 57467.0-57473.0
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| -1 0 -2 16 -19 31 .28 31 29 | --- --- --- ---
| 0 1 4 10 27 45 .03 | --- ---
cof n/a| 0 0 -4 28 1 11 .25 33 31 | --- --- --- ---
| 1 1 7 21 37 55 .04 | --- ---
emx n/a| 0 -2 9 0 -34 -80 .26 26 26 | -1250 480 3601 7167
| 2 1 3 12 18 45 .04 | 8386 966
esx n/a| 0 0 0 -6 11 19 -.07 19 17 | 1082 141 3673 8444
| 1 0 1 11 19 18 .03 | 11961 1567
gfz n/a| 1 -1 2 50 72 30 .07 23 20 | 0 339 3578 6978
| 1 1 1 9 31 24 .08 | 0 1725
grg n/a| -1 0 5 -29 -15 62 -.42 36 32 | -422447 352 4843 618123
| 1 2 4 41 24 33 .11 | 6867 1790
iac n/a| 0 1 -8 -27 -26 -17 -.15 20 20 | 487 3 3661 6962
| 1 1 3 27 38 47 .02 | 7459 1419
mcc n/a| -2 1 -38 71 -108 504 -.51 134 134 | --- --- --- ---
| 12 6 30 193 57 546 .43 | --- ---
Table 1.1889.b GPS week : 1889 MJD: 57467.0-57473.0
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 | 15 11 16 14 14 14 14 |
R02 | 8 8 10 11 8 7 10 |
R03 | 9 9 9 10 10 8 8 |
R04 | 8 9 9 9 9 9 10 |
R05 | 14 16 16 13 12 12 15 |
R06 | 9 10 12 9 9 8 10 |
R07 | 10 10 12 10 9 10 13 |
R08 | 10 10 12 12 8 10 10 |
R09 | 8 6 6 8 11 13 8 |
R10 | 10 10 8 10 8 8 7 |
R13 | 10 8 10 12 10 12 12 |
R14 | 11 9 12 15 17 13 15 |
R15 | 12 12 15 13 13 12 15 |
R16 | 17 18 15 14 12 13 13 |
R17 | 10 10 9 9 9 8 11 |
R18 | 9 7 7 7 8 8 8 |
R19 | 8 9 15 8 6 7 8 |
R20 | 17 12 18 13 19 12 15 |
R21 | 9 8 11 8 10 10 10 |
R22 | 9 9 10 8 8 10 10 |
R23 | 9 8 9 9 9 7 6 |
R24 | 14 15 14 15 17 17 19 |
R26 | 24 237 24 54 41 26 42 |
Table 1.1889.c GPS week : 1889 MJD: 57467.0-57473.0
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 1889 0 | 64 55 35 241 229 3653 83.9 1490 1490 | -4632 0
brd 1889 1 | 40 -19 -1 871 1370 4299 81.9 1647 1647 | -2019 0
brd 1889 2 | 16 1 15 -1219 2171 6098 82.5 1746 1746 | 1406 0
brd 1889 3 | 19 63 -16 -950 265 6994 84.3 1697 1697 | -2282 0
brd 1889 4 | 20 -73 -5 700 685 6470 86.2 1330 1330 | 14633 0
brd 1889 5 | -21 -98 -23 475 -1249 4377 86.7 1476 1476 | -4929 0
brd 1889 6 | 8 -122 -16 -667 -1447 6649 85.3 1404 1404 | -4982 0
-------------+------------------------------------------------------------+----------------
brd 1889 mean| 21 -27 -1 -78 289 5505 84.4 1541 1541 | -400 0
brd 1889 sdev| 26 73 20 849 1307 1351 1.8 156 156 | 7009 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 2.1889.0 GPS week: 1889 Day: 0 MJD: 57467
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 -10 4 -52 70 .31 34 33 | --- --- --- ---
cof n/a| 0 0 -15 19 -26 -9 .25 38 34 | --- --- --- ---
emx n/a| 0 -2 5 10 -13 -111 .24 22 23 | -8355 -330 3720 7625
esx n/a| 0 0 0 0 29 7 -.00 19 18 | -7514 -1061 3742 8099
gfz n/a| 0 -2 5 50 123 11 .07 25 22 | 0 -475 3655 7408
grg n/a| -3 2 0 -29 -6 51 -.52 33 28 | -426038 -640 3732 617459
iac n/a| 0 0 -3 -34 -71 30 -.13 18 18 | -3492 -147 3718 7363
mcc n/a| -4 2 23 73 -134 681 -.64 151 151 | --- --- --- ---
Table 2.1889.1 GPS week: 1889 Day: 1 MJD: 57468
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 -5 15 13 42 .32 32 30 | --- --- --- ---
cof n/a| 0 1 -8 3 54 81 .21 34 33 | --- --- --- ---
emx n/a| 0 -2 9 5 -17 -7 .24 21 20 | 1408 303 3407 7904
esx n/a| 0 0 1 -17 14 -1 -.09 16 15 | 809 177 3289 8769
gfz n/a| 3 -1 0 48 90 51 .14 21 18 | 0 647 3423 7908
grg n/a| -1 2 1 -43 -58 45 -.46 34 32 | -423956 -448 3392 617862
iac n/a| 0 0 -4 0 -65 -52 -.14 19 19 | -1144 -47 3419 7756
mcc n/a| -4 4 -31 68 -35 886 -.06 102 102 | --- --- --- ---
Table 2.1889.2 GPS week: 1889 Day: 2 MJD: 57469
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 0 4 18 -9 .24 29 28 | --- --- --- ---
cof n/a| -3 0 -8 40 50 -15 .21 32 31 | --- --- --- ---
emx n/a| 1 0 10 18 -38 -86 .20 31 34 | -8091 909 3268 8002
esx n/a| 2 0 -2 -7 31 22 -.05 16 15 | -7809 -455 3280 9566
gfz n/a| 0 -1 1 53 68 27 .11 23 21 | 0 546 3269 7875
grg n/a| -2 2 4 -17 -30 132 -.49 38 32 | -421236 923 3280 616354
iac n/a| -2 2 -5 -64 -37 -78 -.17 28 28 | 2304 251 3252 7831
mcc n/a| -12 5 -46 -46 -106 702 -.43 92 92 | --- --- --- ---
Table 2.1889.3 GPS week: 1889 Day: 3 MJD: 57470
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 0 34 -21 -38 .27 29 28 | --- --- --- ---
cof n/a| 0 0 -7 22 -8 -84 .25 31 28 | --- --- --- ---
emx n/a| -1 -1 7 -10 -63 -97 .26 26 25 | 2182 697 3812 6636
esx n/a| -1 1 1 -12 -16 15 -.08 18 17 | -772 153 3833 7316
gfz n/a| 0 0 1 30 20 21 .04 21 17 | 0 851 3778 6507
grg n/a| 0 -3 6 -28 3 73 -.43 34 30 | -425648 803 5961 616902
iac n/a| 0 1 -13 -9 31 53 -.14 24 24 | -1546 -253 3816 6487
mcc n/a| -16 -1 -61 -67 -63 1056 -.00 141 141 | --- --- --- ---
Table 2.1889.4 GPS week: 1889 Day: 4 MJD: 57471
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 -3 16 -22 55 .29 32 29 | --- --- --- ---
cof n/a| 0 0 0 41 -22 63 .33 36 35 | --- --- --- ---
emx n/a| 0 -3 8 -12 -37 -28 .32 24 21 | 14398 414 3813 8055
esx n/a| 0 0 1 -19 -13 36 -.11 24 19 | 25098 178 4291 10159
gfz n/a| 2 -2 0 54 64 64 -.07 22 24 | 0 -1000 3880 7944
grg n/a| 0 -3 12 -41 -1 35 -.49 43 32 | -407603 1230 10326 624106
iac n/a| 0 2 -10 0 10 -48 -.13 17 17 | 16435 -862 4201 7672
mcc n/a| 19 -7 -71 151 -205 749 -1.00 183 183 | --- --- --- ---
Table 2.1889.5 GPS week: 1889 Day: 5 MJD: 57472
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 2 22 -50 88 .30 31 30 | --- --- --- ---
cof n/a| -1 0 3 63 -42 37 .26 30 28 | --- --- --- ---
emx n/a| -3 -2 16 3 -51 -104 .30 30 27 | -9062 -833 3768 5942
esx n/a| 2 0 -1 -1 6 8 -.09 19 17 | 6487 -1398 3791 6919
gfz n/a| 0 0 3 53 62 -8 .05 21 20 | 0 -1778 3666 5616
grg n/a| 0 -1 7 -91 12 53 -.26 36 32 | -424647 -2558 3756 617025
iac n/a| 0 0 -11 -19 -13 3 -.15 16 16 | -3467 -1764 3770 5764
mcc n/a| -4 -2 -33 451 -140 -353 -.36 159 159 | --- --- --- ---
Table 2.1889.6 GPS week: 1889 Day: 6 MJD: 57473
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 0 14 -20 13 .23 27 24 | --- --- --- ---
cof n/a| 0 1 4 6 3 11 .21 31 29 | --- --- --- ---
emx n/a| 2 -3 9 -12 -21 -129 .30 30 29 | -1230 2200 3421 6011
esx n/a| 0 0 0 11 25 50 -.07 21 20 | -8720 3393 3487 8283
gfz n/a| 1 0 2 61 76 43 .16 25 21 | 0 3583 3377 5589
grg n/a| -5 0 4 49 -24 44 -.27 37 36 | -428006 3154 3460 617154
iac n/a| 0 0 -7 -62 -39 -25 -.18 19 19 | -5678 2844 3455 5864
mcc n/a| 5 12 -45 -128 -74 -187 -1.09 107 107 | --- --- --- ---
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 3.1889.0 GPS week: 1889 Day: 0 MJD: 57467
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 | 2514 74 80 30 17 36 41 14 --- 15 | 99 103 82 89 100 95 85 --- 87
R02 | 2009 23 25 18 15 19 24 12 --- 8 | 60 64 58 62 60 51 54 --- 56
R03 | 1777 38 37 12 14 20 25 13 90 8 | 55 58 52 48 53 54 49 45 48
R04 | 1121 36 41 12 14 20 23 12 --- 8 | 47 51 45 45 47 45 44 --- 42
R05 | 1450 33 52 32 27 36 42 25 --- 14 | 48 59 52 49 64 44 52 --- 45
R06 | 725 20 22 22 26 13 22 15 --- 9 | 57 57 51 58 55 55 56 --- 53
R07 | 1912 43 37 13 10 27 33 14 164 9 | 61 61 58 54 62 73 56 100 55
R08 | 899 38 37 13 19 23 28 15 --- 9 | 63 64 57 61 56 62 52 --- 55
R09 | 1850 22 27 13 17 14 32 13 --- 8 | 25 32 19 27 24 23 19 --- 17
R10 | 1382 23 23 12 26 15 34 20 --- 9 | 48 47 32 61 38 36 39 --- 40
R13 | 677 40 37 14 12 28 25 13 --- 9 | 49 51 32 30 37 24 23 --- 26
R14 | 1219 24 28 22 22 27 33 23 --- 11 | 49 53 35 53 44 33 48 --- 41
R15 | 2730 47 40 24 17 37 22 17 --- 12 | 63 62 39 43 56 23 24 --- 34
XR16 | 2307 23 22 50 --- 13 47 20 --- 17 | 54 57 38 --- 45 42 49 --- 38
XR17 | 842 24 28 17 --- 11 36 9 --- 9 | 75 74 72 --- 61 56 57 --- 62
R18 | 609 18 17 21 9 28 30 14 --- 8 | 57 56 61 49 52 36 39 --- 46
R19 | 1293 25 28 17 15 14 19 17 --- 8 | 63 63 61 56 51 31 35 --- 48
R20 | 1251 19 37 45 30 30 68 31 --- 17 | 51 68 71 68 63 44 39 --- 49
R21 | 833 27 32 18 13 21 26 19 182 8 | 69 72 62 55 57 42 34 100 49
R22 | 1439 26 35 18 12 17 27 21 --- 8 | 70 73 67 56 53 47 42 --- 53
R23 | 701 17 33 17 24 15 20 15 --- 8 | 24 29 29 45 38 22 16 --- 27
R24 | 961 35 38 36 24 41 43 20 --- 14 | 63 65 72 62 40 45 30 --- 48
XR26 | ---- 30 >>>> --- --- --- --- 21 --- 24 | 233 9999 --- --- --- --- 206 --- 244
------+---------------------------------------------------+-----------------------------------------------
RMS | 1490 34 38 22 19 25 33 18 151 |T 64 59 52 53 52 44 49 81 54
WRMS | 1490 33 34 23 18 22 28 18 151 |NE 66 57 49 50 47 36 46 100 54
MEDI | 1251 26 35 18 17 20 28 15 164 |MD 57 59 52 54 53 44 44 100 48
Table 3.1889.1 GPS week: 1889 Day: 1 MJD: 57468
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 | 1031 51 49 23 13 26 32 14 --- 11 | 93 92 87 94 96 95 85 --- 89
R02 | 1139 28 38 17 10 21 23 13 --- 8 | 50 55 54 51 62 47 50 --- 51
R03 | 709 35 46 28 10 23 18 11 43 9 | 41 46 43 37 44 36 38 46 36
R04 | 1440 32 30 16 11 19 37 11 --- 9 | 44 42 41 37 46 54 36 --- 39
R05 | 2511 31 31 24 25 36 77 30 --- 16 | 47 58 48 56 68 57 53 --- 48
R06 | 1153 19 14 18 26 16 23 25 --- 10 | 87 87 84 85 88 79 76 --- 80
R07 | 2450 43 47 20 15 19 23 19 153 10 | 56 59 51 54 63 51 54 71 51
R08 | 1393 44 43 18 15 23 19 11 --- 9 | 53 52 40 48 50 50 48 --- 45
R09 | 2211 18 23 16 14 12 11 12 --- 6 | 18 26 13 27 24 19 14 --- 17
R10 | 3276 13 18 27 20 20 25 19 --- 9 | 33 32 29 37 31 31 28 --- 27
R13 | 867 31 38 16 12 17 25 11 --- 8 | 36 41 25 23 29 18 16 --- 20
R14 | 1095 20 20 19 18 11 36 19 --- 9 | 31 32 28 31 28 31 31 --- 23
R15 | 2833 46 59 19 15 24 45 22 --- 12 | 47 62 31 23 47 22 20 --- 23
XR16 | 2852 21 52 45 --- 35 47 19 --- 17 | 31 60 34 --- 49 27 31 --- 24
XR17 | 949 25 29 22 --- 20 24 13 --- 10 | 57 58 60 --- 45 44 44 --- 48
R18 | 630 20 24 19 8 20 17 9 --- 6 | 39 39 43 21 25 35 25 --- 27
R19 | 683 25 24 20 11 16 30 16 --- 8 | 34 31 38 28 25 15 14 --- 24
R20 | 1179 24 26 19 18 22 48 26 --- 11 | 47 55 60 44 43 36 23 --- 37
R21 | 670 25 24 16 14 17 17 20 76 8 | 43 40 42 42 32 32 20 102 33
R22 | 1874 26 19 21 9 16 17 27 --- 8 | 42 38 45 37 29 48 17 --- 32
R23 | 815 19 19 14 22 12 13 17 --- 7 | 18 20 18 32 28 16 10 --- 18
R24 | 1107 45 41 39 19 27 65 21 --- 15 | 33 28 49 34 28 17 13 --- 23
XR26 | ---- 355 >>>> --- --- --- --- 157 --- 237 | 238 9999 --- --- --- --- 262 --- 214
------+---------------------------------------------------+-----------------------------------------------
RMS | 1646 32 34 21 16 21 34 19 102 |T 52 47 43 42 44 39 43 73 44
WRMS | 1646 30 33 20 15 18 32 19 102 |NE 49 40 36 31 33 27 37 102 39
MEDI | 1139 26 30 19 14 20 24 19 76 |MD 43 42 42 37 43 35 31 71 33
Table 3.1889.2 GPS week: 1889 Day: 2 MJD: 57469
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 | 1099 38 30 28 18 21 46 57 --- 15 | 127 127 117 115 118 130 84 --- 110
R02 | 793 30 26 30 11 19 31 23 --- 10 | 86 91 80 83 86 87 75 --- 79
R03 | 1050 35 32 14 9 22 26 16 48 9 | 61 67 50 54 54 53 57 51 52
R04 | 1371 27 28 17 13 20 28 15 --- 8 | 46 50 44 43 45 44 39 --- 40
R05E | 2900 26 28 45 17 31 54 44 --- 15 | 57 60 70 53 59 60 61 --- 51
R06 | 1458 23 27 27 25 19 22 35 --- 11 | 64 65 56 64 63 62 75 --- 60
R07 | 962 34 43 18 15 27 34 39 118 12 | 77 78 66 70 74 65 56 61 64
R08 | 1152 43 50 20 19 21 29 35 --- 12 | 73 84 66 72 69 78 55 --- 64
R09 | 2418 17 16 16 12 8 20 12 --- 6 | 17 20 26 27 25 21 16 --- 19
R10 | 2340 11 22 28 16 16 16 14 --- 7 | 35 53 32 42 32 35 33 --- 32
R13 | 740 34 26 23 11 22 23 17 --- 9 | 44 40 31 28 29 24 21 --- 26
R14 | 1149 27 23 38 15 16 33 35 --- 12 | 42 45 61 46 51 35 34 --- 40
R15 | 4497 44 40 31 14 45 41 22 --- 14 | 60 54 37 39 46 23 28 --- 33
XR16 | 1592 21 37 24 --- 28 52 20 --- 14 | 33 45 43 --- 39 40 39 --- 31
XR17 | 789 19 21 15 --- 10 25 21 --- 9 | 62 62 61 --- 53 52 37 --- 50
R18 | 683 18 28 11 8 16 25 14 --- 6 | 46 51 45 42 33 33 37 --- 38
R19 | 967 40 46 36 9 12 82 14 --- 14 | 44 50 48 33 35 65 21 --- 28
R20 | 1494 20 26 66 29 43 49 20 --- 17 | 54 60 61 54 55 51 51 --- 46
R21 | 674 27 33 33 16 23 30 25 96 11 | 55 58 59 53 45 54 26 49 44
R22 | 1787 27 32 23 12 19 22 27 --- 9 | 55 60 54 49 38 41 24 --- 41
R23 | 831 17 13 14 25 13 20 27 --- 9 | 23 25 31 38 27 35 12 --- 24
R24 | 1381 23 44 48 15 13 57 28 --- 13 | 40 62 50 37 39 27 18 --- 32
XR26 | ---- 26 216 --- --- --- --- 21 --- 23 | 42 9999 --- --- --- --- 98 --- 67
------+---------------------------------------------------+-----------------------------------------------
RMS | 1745 29 32 31 16 23 38 28 92 |T 54 59 54 52 50 50 43 53 46
WRMS | 1745 28 31 34 15 21 32 28 92 |NE 43 48 45 40 39 38 33 49 36
MEDI | 1149 27 28 24 15 19 29 22 96 |MD 54 58 50 46 45 44 37 51 41
Table 3.1889.3 GPS week: 1889 Day: 3 MJD: 57470
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 | 963 38 46 32 22 26 40 34 --- 13 | 149 157 155 142 150 143 142 --- 144
R02E | 1014 26 30 27 18 19 43 16 --- 10 | 78 95 82 89 88 87 80 --- 82
R03E | 1471 34 47 27 12 19 33 18 104 10 | 68 77 79 71 82 79 78 64 74
R04E | 972 28 35 18 11 19 27 21 --- 9 | 41 44 44 41 52 48 41 --- 42
R05E | 1848 27 23 32 25 26 38 28 --- 12 | 61 54 59 48 56 53 57 --- 50
R06E | 2071 17 19 15 22 15 30 15 --- 8 | 55 56 56 59 59 55 52 --- 54
R07E | 803 29 35 15 14 26 18 24 196 9 | 38 41 34 35 41 36 38 89 31
R08E | 1144 35 40 23 16 19 33 35 --- 11 | 67 75 67 66 62 78 50 --- 60
R09 | 2151 23 17 14 15 14 25 15 --- 7 | 18 18 24 24 24 21 22 --- 17
R10 | 1848 29 27 18 18 9 33 26 --- 9 | 37 31 34 36 27 37 28 --- 26
R13 | 1108 42 44 15 10 34 23 27 --- 11 | 49 54 31 30 33 27 27 --- 24
R14 | 616 34 32 42 29 25 38 32 --- 14 | 49 62 51 59 49 44 42 --- 42
R15 | 4637 47 48 20 14 34 38 17 --- 12 | 62 65 34 27 35 35 26 --- 27
XR16 | 829 41 40 35 --- 15 30 20 --- 14 | 38 42 46 --- 39 37 43 --- 33
XR17 | 874 18 34 13 --- 14 23 17 --- 8 | 69 77 61 --- 69 58 53 --- 61
R18 | 1152 17 18 16 9 9 27 15 --- 6 | 55 55 55 45 40 34 36 --- 43
R19 | 1969 25 20 13 11 15 32 20 --- 8 | 56 49 48 44 32 26 33 --- 38
R20 | 1286 16 25 40 18 24 47 32 --- 13 | 61 68 66 41 51 51 63 --- 50
R21 | 490 25 25 16 7 16 27 19 101 8 | 55 57 54 47 43 39 37 65 43
R22 | 728 20 23 21 17 11 16 15 --- 7 | 66 69 57 62 59 50 46 --- 55
R23 | 1387 13 11 23 24 14 11 27 --- 9 | 24 28 31 47 33 29 22 --- 29
R24 | 1457 29 20 47 24 18 60 29 --- 15 | 63 45 52 56 40 34 23 --- 39
XR26 | ---- 67 107 --- --- --- --- 43 --- 54 | 47 9999 --- --- --- --- 91 --- 76
------+---------------------------------------------------+-----------------------------------------------
RMS | 1696 29 31 26 18 21 34 24 141 |T 56 59 55 53 52 50 49 72 49
WRMS | 1696 28 28 25 17 17 30 24 141 |NE 49 51 46 43 41 37 39 65 40
MEDI | 1144 28 30 20 16 18 30 21 104 |MD 55 55 52 47 43 39 42 65 43
Table 3.1889.4 GPS week: 1889 Day: 4 MJD: 57471
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 | 1300 49 50 35 21 31 38 21 --- 14 | 81 88 94 93 90 89 73 --- 82
R02E | 1007 25 22 19 15 18 22 10 --- 7 | 69 72 68 67 69 74 69 --- 66
R03E | 1060 34 37 17 15 23 38 15 139 10 | 63 67 63 63 69 70 64 64 62
R04E | 874 25 30 21 16 17 39 12 --- 9 | 46 51 49 45 41 57 44 --- 43
R05E | 859 30 46 23 22 18 36 27 --- 11 | 50 55 54 55 56 61 51 --- 49
R06E | 1131 14 23 23 20 10 38 14 --- 8 | 62 71 68 59 65 66 61 --- 62
R07E | 663 32 35 17 13 25 19 9 247 8 | 50 54 50 45 57 48 47 167 47
R08E | 1863 33 37 14 16 19 18 12 --- 8 | 61 66 66 58 63 67 64 --- 61
XR09 | 1817 21 34 --- 21 29 30 11 --- 11 | 18 26 --- 33 37 35 16 --- 20
R10 | 1194 18 24 21 23 22 19 9 --- 8 | 29 36 22 36 25 21 20 --- 21
R13 | 1539 42 57 14 24 19 23 18 --- 10 | 47 61 27 37 29 17 17 --- 22
R14 | 620 39 40 30 51 28 42 33 --- 16 | 38 61 38 74 50 30 35 --- 38
R15 | 2425 45 59 17 9 42 46 18 --- 13 | 49 61 34 25 40 25 25 --- 25
XR16 | 778 29 43 30 --- 16 26 17 --- 11 | 34 44 33 --- 37 27 41 --- 32
XR17 | 699 23 17 16 --- 21 23 13 --- 9 | 57 51 57 --- 55 43 44 --- 48
R18 | 975 12 22 10 26 15 21 12 --- 7 | 43 46 48 68 54 43 39 --- 48
R19 | 2819 15 17 14 12 12 26 9 --- 6 | 51 56 57 46 54 42 44 --- 48
R20 | 748 21 26 30 31 24 127 15 --- 19 | 50 47 51 62 36 65 36 --- 41
R21 | 774 31 30 21 22 9 49 13 143 10 | 48 48 45 26 28 23 32 122 30
R22 | 495 26 26 13 11 20 28 13 --- 7 | 61 61 52 50 57 35 37 --- 46
R23 | 934 18 15 13 33 20 20 16 --- 9 | 23 30 29 55 37 34 22 --- 30
R24 | 1355 51 50 55 27 23 39 27 --- 16 | 70 77 83 40 34 29 27 --- 39
XR26 | ---- 65 53 --- --- --- --- 25 --- 41 | 80 9999 --- --- --- --- 38 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1330 32 36 24 24 22 43 17 183 |T 51 55 51 51 49 45 41 117 43
WRMS | 1330 29 35 21 19 24 32 17 183 |NE 46 50 44 46 40 33 31 122 34
MEDI | 975 29 34 19 21 20 28 14 143 |MD 50 55 51 50 50 42 39 122 43
Table 3.1889.5 GPS week: 1889 Day: 5 MJD: 57472
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 | 2035 53 47 33 26 32 34 23 --- 14 | 100 95 95 85 96 91 76 --- 84
R02E | 1903 17 23 14 18 18 23 8 --- 7 | 48 50 52 54 51 51 50 --- 49
R03E | 816 25 28 17 16 16 26 12 79 7 | 37 40 37 35 40 46 32 72 33
R04E | 717 28 29 18 12 23 25 14 --- 8 | 36 36 33 36 40 51 35 --- 34
R05E | 955 33 48 29 24 28 44 20 --- 12 | 43 54 39 36 62 54 43 --- 39
R06E | 1051 22 16 18 20 12 21 15 --- 8 | 68 59 62 53 60 58 58 --- 57
R07E | 885 37 30 24 13 22 32 15 249 10 | 41 37 42 43 44 47 33 261 36
R08E | 2202 33 33 32 19 25 27 11 --- 10 | 41 40 34 49 46 53 39 --- 40
R09 | 2254 27 26 57 26 16 24 14 --- 12 | 19 25 61 30 31 24 18 --- 21
R10 | 974 19 10 24 18 13 23 8 --- 7 | 32 25 21 31 27 27 24 --- 22
R13 | 1351 51 46 17 19 24 35 15 --- 11 | 46 42 22 27 28 32 16 --- 20
R14 | 683 30 25 30 30 24 32 26 --- 12 | 41 46 50 68 53 35 38 --- 43
R15 | 2406 45 28 15 16 33 37 18 --- 12 | 45 35 24 35 40 18 24 --- 24
XR16 | 1358 31 25 29 --- 20 28 23 --- 12 | 28 29 36 --- 30 14 32 --- 25
XR17 | 725 18 24 18 --- 16 15 10 --- 7 | 55 59 60 --- 54 50 42 --- 49
R18 | 1158 18 14 19 11 20 34 8 --- 7 | 40 38 46 34 36 11 26 --- 30
R19 | 1817 17 16 15 13 14 27 12 --- 7 | 49 49 51 46 43 32 39 --- 41
R20 | 661 20 22 34 17 14 58 21 --- 11 | 42 44 51 43 37 43 22 --- 33
R21 | 933 31 33 27 15 11 45 13 86 10 | 45 45 43 29 25 18 23 98 26
R22 | 704 39 36 36 18 13 24 9 --- 10 | 46 44 45 19 23 21 20 --- 21
R23 | 1279 13 20 18 13 17 17 15 --- 7 | 17 16 27 18 29 17 17 --- 15
R24 | 2187 30 37 67 17 29 75 19 --- 17 | 66 74 88 50 40 41 41 --- 48
XR26 | ---- 44 213 --- --- --- --- 15 --- 26 | 34 9999 --- --- --- --- 31 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1476 31 30 30 19 21 36 16 159 |T 44 44 46 41 42 37 33 143 35
WRMS | 1476 30 28 27 17 20 32 16 159 |NE 40 40 44 35 35 27 27 98 30
MEDI | 1051 30 28 24 17 18 27 15 86 |MD 42 42 43 36 40 35 32 98 34
Table 3.1889.6 GPS week: 1889 Day: 6 MJD: 57473
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 | 2065 47 51 30 22 32 48 20 --- 14 | 80 90 73 94 99 84 83 --- 83
R02E | 1448 18 21 15 20 19 28 24 --- 9 | 81 87 85 77 86 86 86 --- 81
R03E | 1073 25 29 13 16 16 18 11 92 7 | 56 56 55 59 61 57 54 48 55
R04E | 738 27 29 24 15 18 29 19 --- 9 | 46 47 48 41 48 50 38 --- 41
R05E | 1467 42 34 37 21 41 35 21 --- 14 | 57 51 49 51 59 56 52 --- 46
R06E | 1137 17 16 30 24 10 28 22 --- 10 | 137 141 122 147 139 155 141 --- 140
R07E | 1178 28 35 29 15 25 34 35 143 12 | 59 58 54 62 74 68 73 82 62
R08E | 1923 35 34 19 16 24 29 15 --- 10 | 61 62 59 62 65 71 64 --- 61
R09 | 2225 18 26 27 15 11 29 11 --- 8 | 25 30 27 31 24 22 15 --- 18
R10 | 1410 16 26 17 17 14 18 15 --- 7 | 40 50 27 46 32 28 29 --- 32
R13 | 1161 42 52 24 18 12 39 17 --- 11 | 49 54 26 27 21 31 18 --- 20
R14 | 962 31 33 52 34 31 36 17 --- 15 | 36 42 29 56 47 31 43 --- 36
R15 | 2040 29 33 29 27 50 40 19 --- 14 | 56 58 26 52 44 34 27 --- 34
XR16 | 1827 22 34 28 --- 25 31 24 --- 13 | 48 45 42 --- 39 31 48 --- 38
XR17 | 1217 26 26 13 --- 31 24 8 --- 10 | 68 68 65 --- 46 52 48 --- 52
R18 | 1388 11 12 9 20 18 30 10 --- 7 | 57 59 61 63 47 34 41 --- 50
R19 | 1079 18 21 20 14 16 23 14 --- 7 | 64 65 61 56 56 47 42 --- 52
R20 | 799 18 17 60 13 23 65 12 --- 14 | 48 59 59 57 63 47 41 --- 49
R21 | 906 20 27 20 22 16 24 24 75 9 | 70 75 66 67 48 43 33 76 52
R22 | 977 28 27 28 11 20 28 16 --- 9 | 73 73 77 56 46 43 35 --- 52
R23 | 1244 12 16 18 11 17 13 11 --- 6 | 21 24 28 33 22 19 12 --- 18
R24 | 1540 26 45 44 38 45 82 25 --- 19 | 84 91 80 75 54 38 43 --- 60
XR26 | ---- 54 516 --- --- --- --- 32 --- 42 | 43 9999 --- --- --- --- 68 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1403 27 31 30 21 25 37 19 107 |T 59 62 55 60 55 51 49 68 50
WRMS | 1403 24 29 29 20 21 36 19 107 |NE 52 56 48 51 42 35 36 76 39
MEDI | 1217 26 29 24 17 19 29 17 92 |MD 57 58 55 56 48 43 43 76 50
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