[IGSREPORT-24347] Wk 1888 IGLOS Final Orbits
IGS ACC
acc at igs.org
Sat Apr 2 04:24:18 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1888 (Mar 13, 2016 - Mar 19, 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 2.1888.
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:
igl1888[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1888 in the SP3 format.
igl18887.sum Combination Report for GPS Week 1888.
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 | -8.7 ns
1 | -8.6 ns
2 | -6.7 ns
3 | -7.1 ns
4 | -5.4 ns
5 | -3.7 ns
6 | -3.1 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 1.1888, 1a.1888).
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 2.1888.0-6)
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 3.1888.0-6).
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 1888 summary. (Mar 13, 2016 - Mar 19, 2016)
Table 1.1888.a GPS week : 1888 MJD: 57460.0-57466.0
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 -7 29 -43 82 .26 37 34 | --- --- --- ---
| 1 1 2 16 24 94 .03 | --- ---
cof n/a| -1 0 -11 40 -30 43 .23 41 37 | --- --- --- ---
| 2 1 2 14 31 97 .05 | --- ---
emx n/a| 0 -1 3 -16 -56 -68 .25 27 28 | -103 504 3487 7482
| 2 1 2 28 25 63 .04 | 7428 568
esx n/a| 0 0 0 -18 -9 65 -.04 19 18 | -8870 -804 3540 8454
| 1 0 1 24 32 36 .04 | 4751 1441
gfz n/a| 0 -1 3 41 75 77 .13 21 20 | 0 35 3375 7212
| 0 1 1 16 27 40 .04 | 0 1066
grg n/a| -1 1 8 -30 54 -1 -.46 45 39 | -429090 -134 5034 618691
| 2 1 2 46 41 59 .06 | 5057 1232
iac n/a| 0 1 -4 -4 -28 -92 -.14 19 19 | -4072 -159 3591 12071
| 1 0 1 22 56 95 .03 | 2865 632
mcc n/a| -4 0 -28 4 9 -441 -.20 137 137 | --- --- --- ---
| 16 9 19 142 100 746 .37 | --- ---
Table 1.1888.b GPS week : 1888 MJD: 57460.0-57466.0
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 | 14 12 12 14 15 14 15 |
R02 | 9 8 10 9 9 8 8 |
R03 | 11 11 11 9 10 9 8 |
R04 | 10 10 11 10 10 8 8 |
R05 | 15 15 17 13 14 14 14 |
R06 | 10 10 9 10 11 10 8 |
R07 | 11 11 10 10 11 11 9 |
R08 | 12 12 11 10 11 11 9 |
R09 | 8 8 8 11 10 10 9 |
R10 | 10 9 7 8 9 9 9 |
R13 | 10 11 17 12 10 9 10 |
R14 | 12 13 17 19 14 11 12 |
R15 | 15 13 13 15 20 14 11 |
R16 | 31 35 19 16 14 13 15 |
R17 | 12 10 9 13 11 9 10 |
R18 | 14 9 7 7 10 10 10 |
R19 | 9 12 8 7 9 16 9 |
R20 | 13 12 10 15 15 13 16 |
R21 | 10 9 9 13 9 10 7 |
R22 | 12 12 9 9 6 9 8 |
R23 | 9 9 6 10 10 8 9 |
R24 | 17 17 15 16 16 21 16 |
R26 | 121 36 45 45 21 23 47 |
Table 1.1888.c GPS week : 1888 MJD: 57460.0-57466.0
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 1888 0 | -18 53 -48 1273 -279 75 85.7 1382 1382 | -8715 0
brd 1888 1 | -92 4 -59 -648 -718 605 83.8 1443 1443 | -8563 0
brd 1888 2 | -75 0 -4 -1027 -1131 413 84.0 1572 1572 | -6684 0
brd 1888 3 | 8 -32 -142 -392 -1318 2274 82.8 1462 1462 | -7109 0
brd 1888 4 | -40 -14 -51 -1295 -2831 -323 82.6 1311 1311 | -5411 0
brd 1888 5 | 61 -7 26 -232 -2642 -440 82.4 1531 1531 | -3666 0
brd 1888 6 | 7 0 52 92 -880 440 82.7 1500 1500 | -3096 0
-------------+------------------------------------------------------------+----------------
brd 1888 mean| -21 0 -32 -318 -1399 434 83.4 1457 1457 | -6177 0
brd 1888 sdev| 53 26 64 844 971 902 1.2 89 89 | 2222 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 2.1888.0 GPS week: 1888 Day: 0 MJD: 57460
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 46 -39 23 .26 36 36 | --- --- --- ---
cof n/a| -1 -1 -14 57 -41 -56 .19 37 37 | --- --- --- ---
emx n/a| 0 -2 6 23 -63 -91 .21 26 27 | 10664 911 3633 8474
esx n/a| 0 0 1 -1 -10 32 -.06 20 20 | -9412 542 3691 9439
gfz n/a| 0 0 1 46 66 40 .19 22 18 | 0 419 3481 7955
grg n/a| -3 0 5 -83 43 -67 -.47 43 37 | -421474 -1684 4253 623576
iac n/a| 0 1 -5 -5 -4 -31 -.17 20 20 | 781 -288 4325 41629
mcc n/a| -25 13 -45 -148 8 -1318 -.43 243 243 | --- --- --- ---
Table 2.1888.1 GPS week: 1888 Day: 1 MJD: 57461
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -10 16 -10 -24 .23 35 34 | --- --- --- ---
cof n/a| -2 1 -10 22 11 -53 .31 40 38 | --- --- --- ---
emx n/a| 0 -1 4 -7 -35 -179 .21 28 29 | 7604 1067 3370 8079
esx n/a| 0 0 -1 -46 7 59 -.03 19 17 | -14502 -641 3434 9508
gfz n/a| 0 -1 3 28 76 63 .18 22 19 | 0 758 3345 8032
grg n/a| 0 2 8 0 39 55 -.48 37 37 | -437907 367 7723 619384
iac n/a| 0 2 -4 26 -64 4 -.15 21 21 | -8519 354 3387 8199
mcc n/a| -23 -5 -35 47 67 -1458 -.04 193 193 | --- --- --- ---
Table 2.1888.2 GPS week: 1888 Day: 2 MJD: 57462
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 -1 1 -73 52 .30 38 34 | --- --- --- ---
cof n/a| 2 3 -9 46 -28 10 .25 41 37 | --- --- --- ---
emx n/a| -1 -2 0 -58 -49 -102 .27 27 28 | -7042 498 3437 8177
esx n/a| -1 0 -1 -20 -31 105 -.05 19 17 | -8271 -1910 3569 8773
gfz n/a| 1 0 4 26 30 77 .12 22 19 | 0 94 3051 7977
grg n/a| -1 2 11 30 104 47 -.46 46 37 | -432227 968 9366 616815
iac n/a| 0 2 -1 14 28 -112 -.10 17 17 | -4644 -316 3445 7985
mcc n/a| 15 -12 -12 290 107 -834 .48 93 93 | --- --- --- ---
Table 2.1888.3 GPS week: 1888 Day: 3 MJD: 57463
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 46 -77 275 .29 39 35 | --- --- --- ---
cof n/a| -4 0 -12 24 -91 216 .25 44 38 | --- --- --- ---
emx n/a| -1 -2 0 -49 -77 -28 .28 25 24 | 1408 275 3209 8035
esx n/a| -1 1 0 -55 -63 114 -.10 23 20 | -6376 -2844 3238 8338
gfz n/a| 1 -2 3 24 76 155 .12 20 19 | 0 -966 3163 7839
grg n/a| 2 3 7 16 103 43 -.58 57 49 | -428643 -838 3161 618604
iac n/a| 2 1 -3 7 43 -269 -.16 18 18 | -5597 209 3203 7748
mcc n/a| 15 -2 -39 -91 113 -11 -.11 109 109 | --- --- --- ---
Table 2.1888.4 GPS week: 1888 Day: 4 MJD: 57464
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 1 -6 33 -34 102 .25 38 34 | --- --- --- ---
cof n/a| -2 2 -9 55 -11 99 .16 42 38 | --- --- --- ---
emx n/a| -3 -1 6 3 -92 -67 .29 32 31 | -4743 -518 3298 6401
esx n/a| 4 0 -1 -11 -14 77 -.04 20 18 | -7405 -1585 3262 7101
gfz n/a| 0 -2 5 53 60 62 .10 21 19 | 0 -1331 3203 6333
grg n/a| -1 1 5 -35 69 -97 -.39 44 44 | -429117 -1114 3242 618395
iac n/a| 1 0 -6 -22 -14 -52 -.11 20 20 | -4724 -1008 3267 6112
mcc n/a| -2 -2 -44 29 10 326 -.49 87 87 | --- --- --- ---
Table 2.1888.5 GPS week: 1888 Day: 5 MJD: 57465
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 20 -21 62 .24 35 31 | --- --- --- ---
cof n/a| -1 -1 -9 40 -32 -1 .22 37 33 | --- --- --- ---
emx n/a| 0 -2 3 -11 -59 -20 .29 30 30 | -9230 251 3874 6421
esx n/a| 0 1 -2 6 38 15 -.05 18 14 | -14899 -523 3952 8243
gfz n/a| 0 -1 3 70 98 43 .11 22 23 | 0 -496 3803 6222
grg n/a| -3 0 10 -58 -12 13 -.46 49 38 | -427098 -430 3903 617008
iac n/a| -1 0 -3 -37 -98 -32 -.10 20 20 | -2643 -811 3916 6234
mcc n/a| -6 0 -32 -56 -82 -3 -.20 99 99 | --- --- --- ---
Table 2.1888.6 GPS week: 1888 Day: 6 MJD: 57466
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 -8 39 -47 81 .23 36 32 | --- --- --- ---
cof n/a| -2 1 -16 32 -19 87 .22 42 37 | --- --- --- ---
emx n/a| 3 0 0 -12 -16 8 .23 25 27 | 613 1045 3594 6792
esx n/a| -1 0 2 0 4 51 .03 16 16 | -1231 1330 3637 7780
gfz n/a| -1 -1 4 38 117 102 .11 22 20 | 0 1768 3583 6132
grg n/a| -3 2 10 -80 32 -3 -.40 37 31 | -427168 1789 3590 617059
iac n/a| 1 0 -6 -11 -89 -156 -.16 18 18 | -3163 744 3594 6594
mcc n/a| -5 10 6 -36 -159 207 -.64 136 136 | --- --- --- ---
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 3.1888.0 GPS week: 1888 Day: 0 MJD: 57460
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 | 510 57 56 35 19 20 45 17 --- 13 | 72 74 29 34 23 19 20 --- 21
R02 | 1754 36 28 15 16 19 23 14 --- 8 | 98 99 85 89 84 68 88 --- 85
R03 | 854 51 50 15 22 24 29 14 251 11 | 99 104 74 69 60 64 77 44 70
R04 | 680 43 43 16 16 18 36 14 --- 10 | 97 101 63 66 60 74 77 --- 68
R05 | 807 37 40 32 22 29 69 22 --- 14 | 92 93 77 90 79 73 91 --- 82
R06 | 714 26 33 22 25 14 25 22 --- 10 | 80 81 92 106 89 73 91 --- 90
R07 | 883 50 47 16 12 27 31 13 329 10 | 102 102 79 76 66 68 74 75 73
R08 | 628 50 44 18 23 23 27 19 --- 11 | 101 101 69 68 58 58 70 --- 66
R09 | 2601 18 22 17 18 14 26 14 --- 7 | 19 23 22 31 27 22 17 --- 18
R10 | 1175 19 23 23 23 16 31 19 --- 9 | 44 48 30 53 36 26 37 --- 35
R13 | 535 25 31 18 18 30 20 20 --- 9 | 44 49 32 32 31 33 23 --- 24
R14 | 1222 30 31 24 24 21 41 26 --- 11 | 50 63 50 70 60 32 50 --- 51
R15 | 3812 53 57 15 20 48 33 31 --- 15 | 68 74 29 35 46 26 30 --- 29
XR16 |13002 67 114 --- --- --- 51 23 --- 30 | 246 265 --- --- --- 255 269 --- 266
XR17 | 1395 35 37 21 --- 24 31 17 --- 12 | 64 65 59 --- 49 36 38 --- 45
R18 | 1013 25 26 17 10 21 92 17 --- 13 | 56 54 51 43 39 46 44 --- 39
R19 | 1019 23 21 21 9 16 46 9 --- 8 | 60 59 57 46 38 26 36 --- 41
R20 | 659 27 37 35 28 19 53 22 --- 13 | 53 67 61 77 57 37 39 --- 53
R21 | 993 32 38 28 17 19 24 19 78 10 | 67 72 67 63 48 41 39 25 51
R22 | 1256 34 32 27 22 15 19 31 --- 11 | 71 70 66 67 51 42 36 --- 52
R23 | 669 13 15 19 30 11 15 21 --- 9 | 24 29 27 46 30 23 18 --- 25
R24 | 1170 18 34 63 19 14 81 27 --- 17 | 45 49 59 55 42 31 29 --- 42
XR26 | ---- 190 >>>> --- --- --- --- 76 --- 121 | 49 9999 --- --- --- --- 40 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1382 36 37 26 20 22 43 20 243 |T 73 79 56 60 51 53 57 48 59
WRMS | 1382 36 37 27 20 18 37 20 243 |NE 73 79 56 60 51 53 57 48 59
MEDI | 993 34 37 21 19 19 31 19 251 |MD 67 70 59 63 49 37 39 44 51
Table 3.1888.1 GPS week: 1888 Day: 1 MJD: 57461
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 | 916 54 42 20 19 25 30 23 --- 12 | 45 34 30 43 33 33 27 --- 26
R02 | 1690 32 40 17 16 19 24 8 --- 8 | 99 103 100 97 95 96 102 --- 97
R03 | 1073 48 46 21 15 24 38 9 225 11 | 96 98 83 86 82 80 84 29 83
R04 | 583 43 44 16 14 20 36 17 --- 10 | 89 91 67 81 69 87 73 --- 75
R05 | 644 33 44 24 19 27 78 27 --- 15 | 91 98 91 90 81 88 92 --- 87
R06 | 737 19 23 24 22 15 31 21 --- 9 | 75 73 81 85 78 84 86 --- 81
R07 | 783 43 55 31 9 28 33 11 233 11 | 85 92 78 72 65 63 71 34 70
R08 | 728 49 61 19 19 27 25 28 --- 12 | 92 100 70 76 70 73 84 --- 74
R09 | 3279 20 20 18 14 11 33 14 --- 7 | 16 20 31 35 37 42 12 --- 24
R10 | 1748 22 22 18 24 19 17 13 --- 8 | 34 34 22 36 23 25 20 --- 22
R13 | 677 35 35 27 14 22 30 22 --- 10 | 37 37 34 25 27 60 24 --- 21
R14 | 1430 27 27 36 26 23 30 33 --- 13 | 46 53 51 46 48 43 43 --- 39
R15 | 2766 46 52 13 21 36 46 17 --- 12 | 56 61 22 32 64 20 27 --- 29
XR16 | 8591 70 58 --- --- 72 57 46 --- 35 | 175 197 --- --- 144 192 168 --- 188
XR17 | 1475 26 30 19 --- 18 27 12 --- 9 | 46 47 47 --- 34 25 36 --- 36
R18 | 1138 29 37 18 11 12 36 17 --- 8 | 43 52 40 36 32 39 29 --- 32
R19 | 1571 38 42 43 15 18 39 17 --- 12 | 39 44 54 19 18 18 16 --- 19
R20 | 701 30 47 24 27 28 43 19 --- 12 | 56 76 48 61 46 42 40 --- 45
R21 | 1401 27 25 15 20 14 34 18 80 9 | 42 41 36 47 32 28 26 12 33
R22 | 1053 41 42 25 15 28 42 17 --- 11 | 52 54 42 35 34 27 20 --- 28
R23 | 636 12 25 17 27 11 11 23 --- 8 | 18 24 16 32 25 20 12 --- 16
R24 | 1633 18 39 69 15 12 46 37 --- 16 | 25 37 30 26 29 24 25 --- 18
XR26 | ---- 57 118 --- --- --- --- 21 --- 35 | 66 9999 --- --- --- --- 37 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1443 35 40 28 19 22 37 21 193 |T 61 66 51 53 53 54 50 25 51
WRMS | 1443 34 38 29 17 19 37 21 193 |NE 61 66 51 53 53 54 50 25 51
MEDI | 1073 33 42 20 16 20 33 18 225 |MD 52 53 47 43 37 42 36 29 33
Table 3.1888.2 GPS week: 1888 Day: 2 MJD: 57462
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 | 938 64 80 23 18 25 36 14 --- 12 | 57 77 24 32 25 21 21 --- 19
R02 | 997 38 45 15 20 21 24 19 --- 9 | 76 81 77 85 68 76 60 --- 70
R03 | 742 52 53 22 18 20 42 10 93 10 | 81 83 52 58 41 49 41 39 48
R04 | 949 50 46 19 14 24 50 13 --- 11 | 75 75 54 51 30 51 41 --- 43
R05 | 624 42 37 55 26 29 71 24 --- 16 | 81 89 92 77 70 80 72 --- 73
R06 | 1050 14 22 28 18 17 24 13 --- 8 | 73 83 88 81 70 74 72 --- 75
R07 | 1451 47 41 24 13 21 32 12 93 9 | 86 83 65 70 63 53 52 56 61
R08 | 924 55 58 17 16 31 21 14 --- 11 | 91 89 61 73 68 54 61 --- 64
R09 | 2108 28 22 16 18 11 18 14 --- 7 | 15 21 29 30 26 35 13 --- 19
R10 | 1753 19 20 20 13 12 17 13 --- 6 | 34 35 34 32 29 23 22 --- 25
R13 | 595 41 56 19 25 32 120 15 --- 17 | 45 54 31 36 29 75 21 --- 25
R14 | 2073 36 24 47 35 28 51 33 --- 16 | 52 60 62 64 57 33 49 --- 45
R15 | 3663 56 50 24 14 33 45 18 --- 12 | 64 60 25 28 33 32 22 --- 23
XR16 | 1573 41 37 58 --- 15 59 24 --- 18 | 200 222 49 --- 74 188 207 --- 201
XR17 | 865 22 25 16 --- 15 15 16 --- 8 | 52 52 49 --- 51 49 36 --- 42
R18 | 845 19 15 20 13 13 26 14 --- 7 | 47 43 44 48 44 46 37 --- 42
R19 | 1734 22 35 21 13 12 33 14 --- 8 | 48 59 52 45 36 20 30 --- 37
R20 | 807 28 31 27 17 23 31 16 --- 9 | 59 59 66 43 37 40 44 --- 43
R21 | 1072 22 26 16 16 18 42 14 92 8 | 52 55 44 48 56 33 37 14 42
R22 | 738 36 50 22 18 20 27 13 --- 9 | 66 76 35 54 53 39 45 --- 46
R23 | 2318 16 25 13 12 12 17 12 --- 6 | 21 39 26 27 23 32 23 --- 22
R24 | 2141 27 27 43 27 17 70 22 --- 14 | 36 42 47 51 34 41 17 --- 31
XR26 | ---- 87 103 --- --- --- --- 22 --- 45 | 38 9999 --- --- --- --- 70 --- 58
------+---------------------------------------------------+-----------------------------------------------
RMS | 1571 38 41 27 19 22 46 17 93 |T 63 69 50 51 46 52 47 36 50
WRMS | 1571 34 37 28 17 19 37 17 93 |NE 63 69 50 51 46 52 47 36 50
MEDI | 997 36 37 21 17 20 32 14 93 |MD 57 60 49 48 41 41 41 39 43
Table 3.1888.3 GPS week: 1888 Day: 3 MJD: 57463
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 | 768 74 68 27 15 26 37 16 --- 13 | 73 66 30 33 32 24 25 --- 23
R02 | 1000 33 30 12 17 21 46 12 --- 9 | 116 113 118 106 110 82 116 --- 109
R03 | 595 47 55 12 14 21 25 10 109 9 | 114 117 99 93 89 84 103 52 95
R04 | 644 45 53 19 12 21 38 10 --- 9 | 108 115 87 100 86 110 101 --- 95
R05 | 884 41 41 24 24 15 66 26 --- 12 | 95 101 59 100 88 86 104 --- 89
R06 | 1364 14 37 20 16 12 66 15 --- 9 | 73 66 90 86 74 77 87 --- 81
R07 | 763 51 54 16 11 20 27 14 104 9 | 99 100 82 80 77 81 79 99 79
R08 | 1043 57 57 18 16 14 26 16 --- 10 | 104 108 76 82 72 83 87 --- 79
R09 | 1527 29 36 25 23 22 57 16 --- 11 | 19 28 19 34 35 49 20 --- 17
R10 | 1045 26 23 23 20 15 19 12 --- 8 | 43 45 31 41 26 26 33 --- 29
R13 | 529 40 32 13 21 21 83 13 --- 12 | 51 48 34 39 31 26 35 --- 30
R14 | 2085 31 41 40 57 26 83 35 --- 19 | 50 76 75 84 56 40 60 --- 54
R15 | 3374 52 72 21 17 29 91 25 --- 15 | 66 87 31 43 49 33 31 --- 35
XR16 | 1722 43 47 38 --- 20 53 23 --- 15 | 126 131 25 --- 63 105 127 --- 120
XR17 | 691 34 32 29 --- 16 21 24 --- 12 | 51 50 53 --- 45 33 31 --- 36
R18 | 749 19 23 14 9 10 25 18 --- 6 | 48 50 50 43 45 44 29 --- 40
R19 | 1682 29 22 15 12 13 23 10 --- 7 | 59 52 44 44 46 27 43 --- 43
R20 | 1043 35 51 39 31 22 77 16 --- 14 | 61 72 62 70 41 26 43 --- 48
R21 | 1060 34 43 27 21 19 93 10 113 13 | 56 61 47 40 36 79 37 22 37
R22 | 1667 22 25 13 27 15 46 14 --- 9 | 61 65 55 72 61 31 48 --- 54
R23 | 2752 20 21 14 32 17 28 16 --- 9 | 27 28 32 58 34 19 36 --- 33
R24 | 820 28 41 53 20 27 66 27 --- 15 | 36 45 57 40 43 26 27 --- 31
XR26 | ---- 79 139 --- --- --- --- 24 --- 44 | 76 9999 --- --- --- --- 38 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1462 39 44 25 23 20 57 18 109 |T 70 73 57 64 56 54 58 57 55
WRMS | 1462 35 38 24 20 19 49 18 109 |NE 70 73 57 64 56 54 58 57 55
MEDI | 1043 34 41 20 17 20 46 16 109 |MD 61 66 53 58 46 40 43 52 43
Table 3.1888.4 GPS week: 1888 Day: 4 MJD: 57464
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 | 1176 70 88 31 20 23 47 21 --- 14 | 72 91 34 40 27 23 23 --- 24
R02 | 933 22 32 27 18 21 24 10 --- 8 | 62 75 66 67 49 64 57 --- 57
R03 | 926 39 47 14 13 22 37 10 89 9 | 70 80 43 58 42 48 44 54 47
R04 | 780 43 54 26 14 24 22 14 --- 10 | 69 78 42 41 33 36 40 --- 38
R05 | 1726 47 59 33 22 27 47 23 --- 13 | 76 88 49 69 65 51 59 --- 58
R06 | 1484 24 24 28 22 16 43 23 --- 11 | 49 56 49 62 53 38 57 --- 51
R07 | 1016 55 58 27 12 21 34 11 67 11 | 63 64 34 31 31 42 33 57 29
R08 | 618 44 51 11 24 20 39 18 --- 11 | 60 63 31 35 30 53 36 --- 31
R09 | 1000 26 25 46 12 12 27 12 --- 9 | 25 26 28 28 26 26 19 --- 19
R10 | 780 16 19 26 19 16 24 22 --- 9 | 38 43 36 44 34 35 33 --- 33
R13 | 537 38 50 26 21 23 25 11 --- 10 | 43 52 33 29 28 47 22 --- 23
R14 | 1130 33 34 46 33 19 37 23 --- 13 | 45 57 52 73 55 33 47 --- 49
R15 | 2826 51 33 25 23 33 109 34 --- 19 | 59 46 25 44 53 56 26 --- 28
XR16 | 3238 31 37 32 --- 20 52 19 --- 14 | 113 131 39 --- 52 110 118 --- 114
XR17 | 982 27 26 23 --- 20 20 19 --- 10 | 50 47 50 --- 38 31 26 --- 34
R18 | 648 32 25 24 14 17 33 24 --- 10 | 44 39 42 29 34 20 14 --- 23
R19 | 2210 31 37 21 16 18 39 13 --- 9 | 44 48 30 33 39 64 28 --- 30
R20 | 883 27 33 56 19 20 73 23 --- 15 | 40 44 56 39 36 19 19 --- 29
R21 | 793 27 23 24 17 20 32 16 102 9 | 50 46 53 43 35 33 24 37 34
R22 | 1441 21 20 16 7 13 19 12 --- 6 | 56 52 58 45 59 46 41 --- 48
R23 | 1731 22 20 23 23 21 20 19 --- 9 | 29 32 41 48 37 32 23 --- 31
R24 | 1045 37 44 58 24 18 58 30 --- 16 | 61 64 78 56 39 33 23 --- 41
XR26 | ---- 32 204 --- --- --- --- 14 --- 20 | 38 9999 --- --- --- --- 42 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1310 38 42 32 20 21 44 20 87 |T 54 60 44 45 40 42 37 49 39
WRMS | 1310 34 38 31 18 19 44 20 87 |NE 54 60 44 45 40 42 37 49 39
MEDI | 1000 32 34 26 19 20 34 19 89 |MD 50 52 42 43 37 36 33 54 34
Table 3.1888.5 GPS week: 1888 Day: 5 MJD: 57465
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 | 1513 73 66 31 13 31 43 15 --- 14 | 68 65 20 40 50 23 27 --- 32
R02 | 1047 19 16 25 12 18 25 13 --- 7 | 85 83 103 93 97 84 90 --- 93
R03 | 1549 40 34 19 10 19 27 10 99 8 | 80 74 78 71 67 78 79 54 73
R04 | 869 38 34 19 10 18 24 11 --- 8 | 79 81 67 68 60 73 67 --- 66
R05 | 1643 50 54 38 15 24 55 25 --- 13 | 75 79 57 73 70 88 79 --- 69
R06 | 1119 16 16 29 16 15 19 28 --- 9 | 51 55 62 69 60 71 65 --- 63
R07 | 1669 49 49 20 13 21 35 15 47 10 | 80 79 70 60 62 62 60 38 61
R08 | 1209 34 31 39 18 23 27 9 --- 10 | 66 67 51 73 70 71 65 --- 64
R09 | 823 25 21 28 15 10 52 15 --- 9 | 20 19 14 35 35 37 14 --- 20
R10 | 701 20 24 33 10 9 35 17 --- 8 | 41 32 36 33 32 33 29 --- 31
R13 | 501 40 45 23 12 15 26 12 --- 8 | 44 46 29 29 23 28 24 --- 23
R14 | 1080 25 27 38 20 19 21 21 --- 10 | 36 38 29 39 36 40 46 --- 33
R15 | 3642 41 51 20 17 41 50 23 --- 13 | 46 54 26 35 33 43 25 --- 23
XR16 | 3139 15 40 38 --- 17 39 22 --- 12 | 138 135 42 --- 48 115 131 --- 129
XR17 | 982 23 31 23 --- 11 17 18 --- 9 | 42 47 45 --- 42 42 25 --- 35
R18 | 763 26 34 27 17 17 29 24 --- 10 | 39 47 42 37 27 21 13 --- 26
R19 | 2859 36 40 17 17 16 117 22 --- 16 | 43 45 20 30 32 80 11 --- 23
R20 | 1044 20 32 47 18 17 61 21 --- 12 | 30 54 28 27 34 29 17 --- 19
R21 | 1214 25 29 21 16 12 57 19 131 10 | 37 36 34 42 41 63 29 32 33
R22 | 1039 32 37 20 11 25 25 13 --- 9 | 43 43 34 39 30 27 33 --- 31
R23 | 1757 15 20 25 17 10 20 19 --- 8 | 28 32 44 31 31 27 16 --- 25
R24 | 892 29 41 45 43 38 99 37 --- 20 | 71 82 81 83 56 57 44 --- 60
XR26 | ---- 35 485 --- --- --- --- 15 --- 22 | 32 9999 --- --- --- --- 41 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1531 35 37 30 18 22 49 20 99 |T 55 58 46 50 47 54 44 41 46
WRMS | 1531 31 33 30 14 23 38 20 99 |NE 55 58 46 50 47 54 44 41 46
MEDI | 1080 29 34 25 15 17 29 18 99 |MD 44 54 42 39 41 43 33 38 33
Table 3.1888.6 GPS week: 1888 Day: 6 MJD: 57466
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 | 2109 77 88 34 12 37 34 18 --- 15 | 79 89 18 29 37 28 20 --- 21
R02 | 1900 18 22 14 13 18 30 14 --- 7 | 78 81 79 85 80 70 77 --- 78
R03 | 1623 35 43 14 14 14 26 14 131 8 | 79 82 65 68 56 62 61 57 62
R04 | 914 39 40 12 13 18 15 12 --- 7 | 73 76 49 57 38 53 52 --- 50
R05 | 697 55 49 26 17 31 35 31 --- 13 | 75 78 61 67 66 76 68 --- 63
R06 | 828 18 26 22 18 11 18 20 --- 8 | 56 55 61 82 64 66 74 --- 69
R07 | 771 44 48 17 10 19 24 14 108 8 | 77 82 53 61 46 67 53 54 54
R08 | 1521 38 43 16 12 25 34 10 --- 9 | 74 79 51 63 50 72 55 --- 56
R09 | 1059 30 24 18 12 15 36 15 --- 8 | 21 20 19 29 32 46 14 --- 20
R10 | 989 17 32 21 19 20 31 18 --- 9 | 50 64 33 51 40 31 38 --- 39
R13 | 782 40 43 22 15 25 21 11 --- 9 | 46 54 29 33 36 24 25 --- 27
R14 | 1507 27 36 29 29 14 33 30 --- 12 | 43 49 33 59 44 45 56 --- 46
R15 | 3134 38 43 25 18 24 41 16 --- 11 | 65 70 42 42 45 31 30 --- 35
XR16 | 1776 20 30 40 --- 15 48 24 --- 15 | 131 141 32 --- 59 114 125 --- 119
XR17 | 767 23 24 16 --- 18 37 12 --- 10 | 65 64 57 --- 46 48 38 --- 47
R18 | 810 25 30 20 19 22 32 17 --- 9 | 57 58 54 54 37 30 26 --- 41
R19 | 2604 25 33 13 18 19 26 22 --- 9 | 60 63 48 55 48 46 27 --- 43
R20 | 1874 18 46 55 15 26 80 19 --- 16 | 41 60 48 44 48 23 23 --- 35
R21 | 1342 19 22 11 11 20 16 15 163 6 | 63 64 52 56 54 48 46 35 50
R22 | 806 33 39 12 13 12 32 11 --- 7 | 69 68 54 57 50 44 42 --- 50
R23 | 713 20 22 20 14 16 39 11 --- 8 | 25 27 34 34 28 31 17 --- 23
R24 | 810 36 49 49 20 26 67 27 --- 16 | 64 72 82 51 45 26 32 --- 46
XR26 | ---- 79 213 --- --- --- --- 29 --- 47 | 51 9999 --- --- --- --- 31 --- 29
------+---------------------------------------------------+-----------------------------------------------
RMS | 1500 36 42 25 16 22 37 18 136 |T 62 68 47 53 47 49 44 48 47
WRMS | 1500 32 37 27 16 20 31 18 136 |NE 62 68 47 53 47 49 44 48 47
MEDI | 989 30 39 20 14 19 32 16 131 |MD 64 64 49 55 46 46 38 54 46
More information about the IGSREPORT
mailing list