[IGSREPORT-24492] Wk 1897 IGLOS Final Orbits
IGS ACC
acc at igs.org
Fri Jun 3 06:37:24 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1897 (May 15, 2016 - May 21, 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 2.1897.
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:
igl1897[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1897 in the SP3 format.
igl18977.sum Combination Report for GPS Week 1897.
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 | -0.5 ns
1 | 4.6 ns
2 | 5.3 ns
3 | 7.0 ns
4 | 6.8 ns
5 | 7.3 ns
6 | 8.3 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
----+--------+---------------
5 | GRG | R17
5 | IAC | R17
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 1.1897, 1a.1897).
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 2.1897.0-6)
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 3.1897.0-6).
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 1897 summary. (May 15, 2016 - May 21, 2016)
Table 1.1897.a GPS week : 1897 MJD: 57523.0-57529.0
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| -2 1 25 25 -4 -43 .26 38 36 | --- --- --- ---
| 1 1 3 25 24 33 .04 | --- ---
cof n/a| -1 2 28 15 1 -51 .24 40 37 | --- --- --- ---
| 1 1 4 29 19 60 .08 | --- ---
emx n/a| 0 1 5 12 -57 -23 .24 26 25 | 5077 279 3741 7603
| 1 1 2 46 19 44 .04 | 6019 1277
esx n/a| -1 -1 1 -1 -8 -23 -.18 16 14 | 5072 -492 3743 8797
| 0 0 1 19 5 23 .04 | 4710 2552
gfz n/a| -2 0 -14 18 88 34 .01 28 26 | 0 329 3711 6992
| 1 1 2 21 11 27 .09 | 0 1766
grg n/a| 1 0 1 -12 45 12 -.21 37 26 | 5453 248 3747 7630
| 1 1 4 19 23 51 .04 | 2773 1915
iac n/a| 1 0 -7 -10 -21 47 .06 32 32 | 6351 113 3734 7369
| 1 1 2 27 13 24 .03 | 3281 1148
mcc n/a| -2 0 14 56 -37 762 -.37 84 84 | --- --- --- ---
| 4 6 9 52 64 585 .33 | --- ---
Table 1.1897.b GPS week : 1897 MJD: 57523.0-57529.0
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 13 11 12 14 14 12 |
R02 | 8 8 9 8 7 10 9 |
R03 | 7 8 9 10 9 8 9 |
R04 | 8 7 8 9 9 9 8 |
R05 | 14 13 12 12 12 16 14 |
R06 | 9 10 9 10 8 11 9 |
R07 | 8 9 8 10 8 9 10 |
R08 | 10 9 8 9 10 8 8 |
R09 | 8 9 8 9 9 9 11 |
R10 | 8 9 8 8 10 7 7 |
R12 | --- --- --- 0 67 68 79 |
R13 | 10 10 10 11 12 10 11 |
R14 | 14 18 17 16 16 18 19 |
R15 | 8 9 10 10 10 10 10 |
R16 | 16 15 14 21 14 16 11 |
R17 | 8 8 8 9 9 29 27 |
R18 | 8 9 7 7 8 9 9 |
R19 | 7 8 9 8 9 9 10 |
R20 | 13 14 11 13 17 15 15 |
R21 | 9 9 9 9 9 8 8 |
R22 | 10 8 8 9 10 11 14 |
R23 | 11 10 10 10 10 11 12 |
R24 | 12 16 11 13 13 16 14 |
R26 | 51 32 41 36 46 58 69 |
Table 1.1897.c GPS week : 1897 MJD: 57523.0-57529.0
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 1897 0 | -66 -6 195 495 1296 2601 84.6 1485 1485 | -547 0
brd 1897 1 | -36 -6 269 502 -941 681 84.4 1638 1638 | 4609 0
brd 1897 2 | 26 17 243 316 -424 1851 85.1 2028 2028 | 5338 0
brd 1897 3 | 50 26 285 -1057 1389 2721 83.9 1988 1988 | 7031 0
brd 1897 4 | 25 19 290 -674 1500 3588 86.3 2372 2372 | 6838 0
brd 1897 5 | 2 -1 248 -185 1528 3309 86.3 2008 2008 | 7278 0
brd 1897 6 | -3 -74 203 -13 1800 3600 86.4 2252 2252 | 8273 0
-------------+------------------------------------------------------------+----------------
brd 1897 mean| 0 -3 248 -88 878 2621 85.3 1967 1967 | 5545 0
brd 1897 sdev| 40 33 37 598 1088 1059 1.0 314 314 | 2954 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 2.1897.0 GPS week: 1897 Day: 0 MJD: 57523
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 28 -4 15 -57 .30 40 38 | --- --- --- ---
cof n/a| -1 2 32 -10 -2 -71 .29 40 38 | --- --- --- ---
emx n/a| 0 2 1 78 -59 -47 .19 26 27 | 7748 -449 3519 8035
esx n/a| 0 0 0 -17 -12 -62 -.16 15 13 | 103 -5837 3513 9279
gfz n/a| -2 -2 -14 22 94 1 .14 28 28 | 0 -980 3444 7880
grg n/a| 1 -1 7 -29 45 93 -.24 28 28 | 273 -1410 3518 8060
iac n/a| 2 -1 -8 -35 -9 90 .02 17 17 | 218 88 3506 8068
mcc n/a| -3 9 -4 -22 37 762 -.39 87 87 | --- --- --- ---
Table 2.1897.1 GPS week: 1897 Day: 1 MJD: 57524
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 27 -5 -30 -94 .26 39 39 | --- --- --- ---
cof n/a| 0 1 34 -29 3 -110 .32 44 41 | --- --- --- ---
emx n/a| 1 0 7 -11 -53 -94 .24 28 27 | 9754 1438 4212 8089
esx n/a| 0 0 2 -11 -7 -10 -.19 16 14 | 5559 645 4211 9657
gfz n/a| -2 -2 -11 51 78 34 -.05 27 26 | 0 796 4101 7228
grg n/a| 1 0 4 -4 76 -51 -.21 32 26 | 3817 997 4198 8184
iac n/a| 0 0 -10 1 -40 65 .05 16 16 | 4515 1031 4193 7485
mcc n/a| 0 2 13 136 11 176 -.64 100 100 | --- --- --- ---
Table 2.1897.2 GPS week: 1897 Day: 2 MJD: 57525
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 3 26 60 -18 -49 .27 37 35 | --- --- --- ---
cof n/a| 0 3 29 36 -14 54 .16 39 36 | --- --- --- ---
emx n/a| -1 1 4 66 -40 44 .30 24 22 | 5758 -439 4128 6650
esx n/a| -1 0 1 6 -8 -6 -.15 15 13 | 3061 -249 4132 8082
gfz n/a| 0 0 -14 17 85 81 .04 27 25 | 0 -1779 4104 6261
grg n/a| 0 0 0 -36 60 -43 -.22 27 24 | 6054 -1031 4144 6704
iac n/a| 3 0 -8 -34 -17 37 .03 17 17 | 5568 716 4147 6462
mcc n/a| -10 1 17 52 -118 295 -.77 86 86 | --- --- --- ---
Table 2.1897.3 GPS week: 1897 Day: 3 MJD: 57526
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 25 25 21 -29 .25 36 35 | --- --- --- ---
cof n/a| 0 2 27 31 -16 -103 .25 38 37 | --- --- --- ---
emx n/a| 0 -2 5 17 -58 -33 .23 24 24 | 3203 1350 3552 8029
esx n/a| -2 -1 3 -2 0 -11 -.21 14 12 | 14321 2451 3544 9020
gfz n/a| -1 0 -13 8 85 26 -.09 27 26 | 0 625 3316 7005
grg n/a| 3 3 -7 -9 0 32 -.19 30 29 | 6500 1249 3567 8033
iac n/a| 1 1 -8 -10 -1 51 .11 18 18 | 7600 998 3539 8079
mcc n/a| 0 1 19 82 -106 419 -.41 81 81 | --- --- --- ---
Table 2.1897.4 GPS week: 1897 Day: 4 MJD: 57527
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 3 28 36 18 -40 .28 37 35 | --- --- --- ---
cof n/a| -5 3 27 28 40 -55 .28 38 37 | --- --- --- ---
emx n/a| 2 2 8 -54 -99 13 .25 27 27 | 5341 -378 3920 6690
esx n/a| -1 -1 0 8 -13 -11 -.19 18 15 | 6875 146 3914 7676
gfz n/a| -6 -1 -18 14 110 39 .03 27 25 | 0 782 3917 5998
grg n/a| 1 1 4 12 36 3 -.15 25 23 | 6848 154 3921 6723
iac n/a| 2 0 -5 6 -25 15 .08 18 18 | 8632 -687 3898 6373
mcc n/a| 4 -2 16 31 21 543 -.06 88 88 | --- --- --- ---
Table 2.1897.5 GPS week: 1897 Day: 5 MJD: 57528
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 18 51 1 17 .18 37 33 | --- --- --- ---
cof n/a| 0 2 26 -1 3 4 .11 41 36 | --- --- --- ---
emx n/a| -1 1 5 -1 -48 -36 .28 28 28 | -7179 1924 3304 7139
esx n/a| -2 -2 0 -27 -6 -49 -.24 18 15 | 1217 -424 3307 8197
gfz n/a| 0 -1 -11 -16 74 6 .08 34 24 | 0 3625 3292 6598
grg n/a| 2 0 0 9 49 49 -.21 83 25 | 5592 3652 3325 7229
iac n/a| 1 0 -4 34 -31 48 .05 109 109 | 7828 744 3315 7038
mcc n/a| 0 -12 10 17 -31 1681 .18 79 79 | --- --- --- ---
Table 2.1897.6 GPS week: 1897 Day: 6 MJD: 57529
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 20 15 -35 -47 .31 38 34 | --- --- --- ---
cof n/a| 0 0 21 54 -5 -81 .27 40 37 | --- --- --- ---
emx n/a| 4 2 5 -10 -46 -8 .21 28 23 | 10919 -1487 3558 8590
esx n/a| -2 -1 0 31 -15 -9 -.14 16 13 | 4368 -176 3583 9673
gfz n/a| -2 1 -16 34 86 53 -.11 27 24 | 0 -762 3808 7974
grg n/a| 1 -1 1 -31 50 6 -.27 35 28 | 9091 -1869 3559 8477
iac n/a| 0 2 -4 -40 -25 27 .10 32 32 | 10102 -2098 3544 8084
mcc n/a| -6 -1 27 94 -80 1460 -.51 67 67 | --- --- --- ---
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 3.1897.0 GPS week: 1897 Day: 0 MJD: 57523
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 | 1468 73 81 43 19 35 29 24 --- 15 | 59 66 18 40 48 22 31 --- 22
R02 | 528 28 28 27 6 23 14 18 --- 8 | 42 44 23 19 20 30 15 --- 17
R03 | 1379 36 40 17 6 23 11 11 100 7 | 57 61 33 24 18 27 16 77 21
R04 | 1525 42 40 12 9 32 13 12 --- 8 | 59 61 32 28 32 30 18 --- 25
R05 | 913 35 44 26 20 30 52 28 --- 14 | 48 54 41 47 37 41 41 --- 38
R06 | 1084 37 35 26 16 19 26 12 --- 9 | 59 60 32 34 24 50 25 --- 31
R07 | 1239 38 37 20 10 19 17 18 84 8 | 63 64 35 35 20 33 17 100 28
R08 | 1475 43 44 18 17 25 18 19 --- 9 | 58 62 30 33 23 25 15 --- 23
XR09 | 1682 25 24 15 6 --- 27 9 --- 7 | 32 30 33 26 --- 36 32 --- 29
R10 | 2146 28 36 13 12 30 15 14 --- 7 | 40 42 33 42 32 35 31 --- 33
R13 | 1133 28 28 25 14 29 31 16 --- 10 | 60 57 49 56 37 56 38 --- 47
R14 | 810 51 48 40 15 28 46 14 --- 13 | 44 41 47 45 31 31 36 --- 36
R15 | 3728 30 28 18 12 35 9 11 --- 8 | 48 46 40 40 38 36 33 --- 36
R16 | 921 36 37 53 26 28 53 17 --- 16 | 55 46 39 62 37 32 41 --- 44
R17 | 1540 38 43 19 13 24 17 12 --- 8 | 653 656 648 645 650 651 655 --- 648
R18 | 679 28 27 18 12 25 19 13 --- 7 | 82 83 59 58 46 71 59 --- 59
R19 | 1658 34 33 14 9 23 16 13 --- 7 | 87 86 66 56 44 68 52 --- 58
R20 | 557 40 36 31 16 45 32 26 --- 13 | 87 91 61 61 43 66 58 --- 56
R21 | 730 39 32 20 12 25 20 14 76 8 | 76 76 57 50 42 54 37 63 47
R22 | 488 47 45 18 12 31 26 10 --- 9 | 86 87 56 46 36 57 39 --- 47
R23 | 2344 46 36 30 24 19 24 16 --- 11 | 61 65 73 96 76 78 91 --- 82
R24 | 678 27 26 21 22 19 41 23 --- 11 | 98 94 80 88 79 79 84 --- 81
XR26 | ---- 96 131 --- --- --- --- 27 --- 50 | 89 141 --- --- --- --- 49 --- 47
------+---------------------------------------------------+-----------------------------------------------
RMS | 1485 40 40 26 15 28 28 17 87 |T 88 91 72 74 67 73 65 80 67
WRMS | 1485 38 38 27 13 28 28 17 87 |NE 88 91 72 74 67 73 65 80 67
MEDI | 1133 37 36 20 12 25 20 14 84 |MD 59 62 40 45 37 36 37 77 38
Table 3.1897.1 GPS week: 1897 Day: 1 MJD: 57524
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 | 600 67 71 30 18 43 10 20 --- 13 | 43 53 27 38 55 24 23 --- 25
R02 | 500 32 37 23 8 26 19 13 --- 8 | 33 39 15 18 23 22 12 --- 13
R03 | 645 41 33 19 6 20 19 11 92 8 | 47 42 26 18 15 28 13 78 17
R04 | 1227 36 38 15 6 18 15 12 --- 7 | 41 43 24 20 26 21 12 --- 17
R05 | 783 30 29 38 20 28 37 22 --- 12 | 42 49 36 48 28 27 40 --- 34
R06 | 926 41 41 23 8 28 33 10 --- 9 | 48 49 26 25 27 38 25 --- 24
R07 | 1173 35 34 25 14 18 15 15 127 8 | 46 45 25 34 26 29 17 82 24
R08 | 1059 34 33 14 17 19 18 17 --- 8 | 44 42 22 39 19 22 13 --- 22
XR09 | 1685 24 29 17 13 --- 31 11 --- 9 | 21 19 28 23 --- 33 27 --- 24
R10 | 2345 23 28 19 24 18 18 14 --- 8 | 26 24 24 30 21 24 22 --- 21
R13 | 1289 34 38 29 9 19 25 19 --- 9 | 41 44 38 29 34 38 26 --- 29
R14 | 1807 58 49 65 24 26 52 25 --- 18 | 52 70 49 44 33 31 26 --- 32
R15 | 4939 23 26 20 19 33 18 16 --- 9 | 29 30 28 36 28 30 21 --- 26
R16 | 724 39 68 43 18 36 58 13 --- 14 | 43 71 30 34 20 22 29 --- 24
R17 | 1921 34 25 17 9 27 24 12 --- 8 | 725 726 714 718 716 716 720 --- 716
R18 | 546 32 39 16 12 28 36 10 --- 9 | 62 72 46 52 43 47 42 --- 45
R19 | 2489 38 48 13 10 26 16 7 --- 7 | 62 69 44 42 32 41 41 --- 40
R20 | 525 40 66 37 24 32 35 23 --- 13 | 66 97 45 54 42 55 41 --- 42
R21 | 715 37 38 21 11 28 22 16 72 9 | 53 54 40 31 32 43 28 59 31
R22 | 513 43 41 14 11 23 15 12 --- 8 | 55 59 40 37 32 39 27 --- 33
R23 | 1587 48 51 19 19 16 21 16 --- 9 | 51 51 63 74 64 57 70 --- 66
R24 | 846 27 46 22 24 35 72 22 --- 15 | 63 76 50 54 63 69 61 --- 54
XR26 | ---- 61 126 --- --- --- --- 15 --- 31 | 73 116 --- --- --- --- 35 --- 36
------+---------------------------------------------------+-----------------------------------------------
RMS | 1637 39 44 28 16 27 32 16 100 |T 76 84 65 68 65 66 59 73 60
WRMS | 1637 39 41 27 14 26 26 16 100 |NE 76 84 65 68 65 66 59 73 60
MEDI | 926 36 38 20 13 26 21 15 92 |MD 47 51 30 36 32 31 27 78 29
Table 3.1897.2 GPS week: 1897 Day: 2 MJD: 57525
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 | 637 54 46 28 17 28 18 19 --- 11 | 48 45 23 43 46 26 24 --- 28
R02 | 529 27 32 25 15 28 18 14 --- 9 | 36 44 19 28 21 25 12 --- 18
R03 | 1180 38 46 25 7 34 18 13 61 9 | 47 56 35 20 22 29 12 45 18
R04 | 676 26 30 15 6 19 27 16 --- 7 | 47 53 27 23 20 46 12 --- 24
R05 | 1103 28 34 27 19 18 43 24 --- 12 | 56 73 44 47 37 40 47 --- 40
R06 | 1044 38 45 14 8 36 24 11 --- 9 | 54 60 37 30 27 30 23 --- 25
R07 | 925 37 40 14 6 22 19 19 94 8 | 50 55 25 24 16 33 14 60 22
R08 | 1051 29 29 13 13 19 27 16 --- 8 | 50 53 34 35 33 36 23 --- 30
XR09 | 1830 17 26 14 12 --- 27 12 --- 8 | 21 28 23 22 --- 34 28 --- 23
R10 | 1964 17 19 12 19 22 19 19 --- 8 | 30 32 29 33 25 34 23 --- 26
R13 | 1126 37 38 21 10 36 19 18 --- 9 | 47 49 46 39 29 32 28 --- 34
R14 | 2273 54 82 48 25 28 60 15 --- 17 | 47 83 39 36 51 22 25 --- 26
R15 | 7236 24 31 27 13 39 15 15 --- 9 | 38 41 32 35 52 25 25 --- 30
R16 | 666 45 36 33 23 32 45 23 --- 14 | 49 56 61 39 38 29 28 --- 32
R17 | 1770 28 31 17 10 19 21 16 --- 7 | 380 385 388 388 389 369 377 --- 381
R18 | 853 31 24 16 6 22 10 11 --- 6 | 66 56 50 45 35 44 40 --- 43
R19 | 2879 44 41 20 12 26 14 9 --- 8 | 70 69 47 40 34 45 36 --- 40
R20 | 638 48 26 29 11 18 21 26 --- 10 | 86 65 56 50 44 61 52 --- 51
R21 | 723 32 40 16 12 27 21 17 99 8 | 61 69 45 42 34 52 34 37 39
R22 | 974 38 29 17 10 29 11 14 --- 8 | 67 60 48 41 36 43 32 --- 38
R23 | 861 42 47 25 22 15 18 17 --- 10 | 41 39 47 73 50 53 65 --- 58
R24 | 1289 27 31 22 23 29 33 21 --- 11 | 67 71 48 61 45 39 57 --- 49
XR26 | ---- 71 202 --- --- --- --- 23 --- 40 | 68 198 --- --- --- --- 47 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 2027 37 39 24 15 27 27 17 86 |T 66 75 54 54 51 52 46 47 48
WRMS | 2027 35 36 22 13 25 24 17 86 |NE 66 75 54 54 51 52 46 47 48
MEDI | 1044 37 34 20 12 27 19 16 94 |MD 50 56 39 39 35 34 28 45 32
Table 3.1897.3 GPS week: 1897 Day: 3 MJD: 57526
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 | 1035 49 50 29 18 20 36 17 --- 11 | 50 56 27 30 22 26 18 --- 18
R02 | 884 23 19 12 11 22 24 17 --- 7 | 39 30 27 26 15 36 9 --- 19
R03 | 945 45 46 20 14 29 23 15 41 9 | 52 52 35 26 20 32 16 27 21
R04 | 644 38 40 16 9 28 19 15 --- 8 | 50 52 28 29 25 27 16 --- 21
R05 | 1079 31 37 22 10 30 48 25 --- 12 | 52 53 43 42 29 43 46 --- 40
R06 | 1159 27 29 22 8 25 40 21 --- 10 | 63 62 50 42 38 50 22 --- 39
R07 | 858 46 42 22 11 31 27 15 76 10 | 60 56 35 25 25 31 15 58 23
R08 | 2471 31 33 14 11 30 24 18 --- 8 | 51 51 25 28 15 33 20 --- 23
XR09 | 2036 24 25 20 17 --- 17 15 --- 9 | 21 15 21 26 --- 34 34 --- 24
R10 | 1220 22 18 17 11 28 20 10 --- 7 | 32 29 25 33 24 36 29 --- 27
XR12 | ---- 15 >>>> --- --- --- --- --- --- 0 | 106 9999 --- --- --- --- --- --- 116
R13 | 568 42 45 28 15 36 22 19 --- 11 | 52 53 38 44 33 42 30 --- 35
R14 | 934 56 59 46 23 30 45 23 --- 15 | 57 63 38 52 42 45 32 --- 37
R15 | 7261 30 26 30 11 33 28 14 --- 10 | 36 33 35 30 35 35 24 --- 27
XR16 | 650 44 72 61 25 --- 48 36 --- 20 | 52 77 56 42 --- 31 29 --- 30
R17 | 921 35 39 18 15 30 26 9 --- 9 | 838 843 839 836 846 843 859 --- 836
R18 | 717 23 27 19 7 17 19 13 --- 6 | 72 82 61 64 58 60 57 --- 60
R19 | 2037 37 33 15 7 24 19 9 --- 7 | 76 70 53 57 38 48 51 --- 52
R20 | 698 32 56 24 22 27 39 31 --- 12 | 68 97 58 46 40 40 58 --- 47
R21 | 703 37 33 15 12 21 28 10 112 8 | 59 63 42 37 32 33 33 41 34
R22 | 765 36 42 17 10 28 26 15 --- 9 | 69 78 47 46 43 55 33 --- 43
R23 | 848 29 34 28 24 20 21 16 --- 10 | 62 58 68 86 73 52 70 --- 70
R24 | 1813 35 25 39 19 29 36 24 --- 13 | 89 76 67 72 49 50 64 --- 61
XR26 | ---- 63 174 --- --- --- --- 19 --- 35 | 48 135 --- --- --- --- 81 --- 68
------+---------------------------------------------------+-----------------------------------------------
RMS | 1987 36 38 24 14 27 30 18 81 |T 89 94 78 78 75 76 71 42 73
WRMS | 1987 35 37 24 12 26 29 18 81 |NE 89 94 78 78 75 76 71 42 73
MEDI | 921 35 37 20 11 28 26 16 76 |MD 52 58 38 42 33 36 32 41 35
Table 3.1897.4 GPS week: 1897 Day: 4 MJD: 57527
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 | 830 65 61 33 21 35 27 16 --- 13 | 51 47 28 31 40 34 19 --- 21
R02 | 1400 24 24 19 7 16 15 15 --- 7 | 33 34 22 22 26 24 16 --- 18
R03 | 801 30 29 19 8 24 24 21 54 9 | 52 50 40 32 17 42 15 47 27
R04 | 674 37 40 17 18 32 13 14 --- 9 | 44 46 25 38 26 32 23 --- 25
R05 | 832 35 36 27 13 26 32 26 --- 11 | 49 48 36 43 37 42 39 --- 36
R06 | 1236 33 33 20 14 15 16 18 --- 8 | 56 56 46 31 28 39 21 --- 30
R07 | 738 29 32 18 9 14 21 17 106 7 | 59 62 41 43 31 47 27 96 37
R08 | 1899 35 32 34 10 26 22 16 --- 10 | 54 50 43 32 23 28 22 --- 27
XR09 | 2283 24 26 21 18 --- 16 13 --- 8 | 19 24 15 30 --- 19 25 --- 20
R10 | 939 25 29 26 24 24 18 13 --- 9 | 28 33 26 35 26 18 27 --- 23
XR12 | ---- 77 74 --- --- 57 --- --- --- 66 | 57 9999 --- --- 42 --- --- --- 47
R13 | 567 34 41 22 23 30 31 21 --- 11 | 43 50 37 46 32 42 23 --- 31
R14 | 800 60 56 43 30 45 32 17 --- 16 | 50 64 35 64 63 41 32 --- 42
R15 | 9507 28 40 21 18 40 13 11 --- 9 | 34 43 33 35 49 27 26 --- 28
XR16 | 1621 38 54 24 20 --- 43 14 --- 13 | 33 52 35 32 --- 29 25 --- 24
R17 | 952 39 35 13 10 30 20 11 --- 8 | 749 747 744 746 752 750 772 --- 744
R18 | 550 26 28 16 13 26 23 7 --- 8 | 72 73 61 50 53 74 55 --- 56
R19 | 2291 34 42 23 15 23 15 12 --- 8 | 66 73 55 52 49 56 56 --- 52
R20 | 548 30 29 43 29 25 52 32 --- 16 | 66 53 67 39 44 59 60 --- 47
R21 | 706 30 39 24 14 26 19 10 97 8 | 45 54 35 24 27 28 29 61 25
R22 | 607 43 40 27 12 25 18 15 --- 9 | 63 63 38 34 25 41 25 --- 31
R23 | 726 29 21 33 23 18 21 13 --- 10 | 61 66 49 75 62 75 63 --- 64
R24 | 1429 42 53 36 26 28 27 23 --- 13 | 96 102 44 68 49 67 60 --- 57
XR26 | ---- 81 110 --- --- --- --- 24 --- 46 | 56 102 --- --- --- --- 79 --- 71
------+---------------------------------------------------+-----------------------------------------------
RMS | 2372 37 38 27 18 27 25 18 88 |T 80 86 70 72 71 73 66 68 65
WRMS | 2372 35 37 27 15 25 23 18 88 |NE 80 86 70 72 71 73 66 68 65
MEDI | 830 34 36 23 15 26 21 15 97 |MD 52 53 37 35 37 41 27 61 31
Table 3.1897.5 GPS week: 1897 Day: 5 MJD: 57528
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 | 710 63 71 17 17 41 31 23 --- 13 | 48 55 21 33 51 35 18 --- 25
R02 | 1048 23 26 28 9 35 23 20 --- 10 | 27 30 32 21 28 23 13 --- 17
R03 | 836 31 33 17 15 17 17 15 52 8 | 42 43 29 16 31 32 21 43 22
R04 | 1019 27 30 21 11 25 27 14 --- 9 | 42 45 22 28 25 43 21 --- 26
R05 | 1064 47 47 42 24 35 44 27 --- 15 | 44 59 49 54 36 40 40 --- 38
R06 | 1153 41 46 21 10 29 20 33 --- 11 | 47 51 37 29 17 19 29 --- 24
R07 | 666 34 31 26 9 20 14 24 73 9 | 51 48 48 27 29 36 17 84 30
R08 | 990 27 34 22 11 21 8 13 --- 7 | 42 50 36 31 29 29 30 --- 29
XR09 | 1494 25 25 18 16 --- 18 18 --- 9 | 24 28 22 23 --- 25 25 --- 19
R10 | 1566 19 24 10 18 18 22 10 --- 7 | 27 28 26 32 24 23 22 --- 23
XR12 | ---- 75 97 --- --- 60 --- --- --- 68 | 45 9999 --- --- 26 --- --- --- 37
R13 | 844 26 31 20 20 30 20 23 --- 10 | 39 40 39 47 29 36 23 --- 33
R14 | 1249 44 45 48 32 39 50 29 --- 17 | 35 64 40 65 60 31 29 --- 39
R15 | 7581 19 28 13 14 54 20 11 --- 10 | 33 42 34 32 46 43 27 --- 29
R16 | 1449 34 40 40 23 29 59 24 --- 15 | 38 43 25 39 33 32 25 --- 25
R17 | 1535 55 53 42 30 80 352 491 --- 28 | 9999 9999 9999 9999 9999 9999 9999 --- 9999
R18 | 928 29 29 20 10 23 19 19 --- 8 | 85 91 71 74 71 64 65 --- 69
R19 | 1865 36 29 17 12 24 18 17 --- 8 | 75 68 67 62 57 57 63 --- 61
R20 | 806 21 53 23 21 32 68 27 --- 15 | 52 78 56 41 52 56 51 --- 46
R21 | 784 30 25 15 11 23 14 19 102 8 | 52 47 41 34 31 38 31 81 33
R22 | 574 50 44 20 9 31 26 16 --- 11 | 59 57 29 27 32 42 26 --- 28
R23 | 1292 31 29 31 20 19 24 21 --- 10 | 66 73 68 75 68 71 74 --- 69
R24 | 1781 48 68 47 25 23 41 25 --- 15 | 99 125 71 84 67 62 61 --- 70
XR26 | ---- 85 233 --- --- --- --- 38 --- 57 | 65 215 --- --- --- --- 56 --- 46
------+---------------------------------------------------+-----------------------------------------------
RMS | 2008 37 41 28 18 34 83 109 79 |T 49 62 41 41 40 39 34 69 36
WRMS | 2008 33 36 28 15 24 25 109 79 |NE 49 62 41 41 40 39 34 69 36
MEDI | 1048 31 33 21 15 29 22 21 73 |MD 45 50 37 33 32 36 27 81 30
Table 3.1897.6 GPS week: 1897 Day: 6 MJD: 57529
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 | 1262 59 70 24 15 29 31 16 --- 12 | 68 74 19 25 29 34 11 --- 18
R02 | 1620 25 25 17 7 33 25 11 --- 8 | 48 49 33 25 16 34 17 --- 23
R03 | 1175 37 42 17 11 26 25 10 60 8 | 64 67 35 22 13 46 23 39 27
R04 | 1144 27 27 18 7 14 27 16 --- 7 | 59 61 41 34 36 44 24 --- 34
R05 | 1208 47 46 25 25 18 47 22 --- 13 | 61 60 40 54 35 45 41 --- 43
R06 | 1417 32 38 23 7 28 14 16 --- 8 | 66 72 53 40 24 38 30 --- 38
R07 | 601 36 41 22 7 31 22 26 75 10 | 74 77 60 38 26 52 23 64 40
R08 | 622 25 30 21 10 19 19 13 --- 7 | 66 68 54 39 30 48 34 --- 41
XR09 | 1211 17 25 18 16 --- 28 24 --- 10 | 28 31 23 40 --- 41 37 --- 32
R10 | 1394 21 19 17 15 20 12 8 --- 7 | 38 37 34 40 31 29 33 --- 33
XR12 | ---- 95 81 --- --- 65 --- --- --- 78 | 52 9999 --- --- 35 --- --- --- 54
R13 | 987 37 41 23 8 36 33 24 --- 11 | 50 51 36 39 36 50 27 --- 35
R14 | 1328 44 47 68 26 27 57 30 --- 19 | 57 60 55 59 38 38 32 --- 42
R15 | 3815 25 25 17 10 42 24 17 --- 9 | 37 40 35 35 30 37 29 --- 30
R16 | 847 33 30 31 13 25 34 17 --- 10 | 37 40 29 39 27 34 31 --- 28
R17 | 7920 55 51 45 29 39 51 115 --- 27 | 9999 9999 9999 9999 9999 9999 932 --- 9999
R18 | 1719 26 19 20 14 20 21 24 --- 9 | 100 102 94 102 95 86 72 --- 91
R19 | 1510 37 40 20 12 23 27 19 --- 9 | 87 90 72 71 67 78 54 --- 68
R20 | 669 49 40 22 12 36 59 29 --- 14 | 83 85 58 63 51 57 58 --- 55
R21 | 690 28 39 13 10 18 19 23 67 8 | 58 65 40 30 30 40 42 73 33
R22 | 660 49 53 28 33 21 29 17 --- 13 | 72 73 35 41 30 38 34 --- 35
R23 | 1615 35 41 36 21 19 32 24 --- 12 | 82 78 86 98 81 103 91 --- 90
R24 | 1857 46 40 27 17 24 57 24 --- 14 | 119 110 80 81 71 98 90 --- 83
XR26 | ---- 98 114 --- --- --- --- 47 --- 69 | 96 110 --- --- --- --- 51 --- 50
------+---------------------------------------------------+-----------------------------------------------
RMS | 2251 38 40 28 16 27 35 32 67 |T 65 68 48 48 39 50 78 58 44
WRMS | 2251 34 37 23 13 24 28 32 67 |NE 65 68 48 48 39 50 78 58 44
MEDI | 1211 36 40 22 12 25 27 22 67 |MD 64 67 40 40 31 44 34 64 38
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