[IGSREPORT-23540] Wk 1839 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Fri Apr 24 10:13:27 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1839 (Apr 05, 2015 - Apr 11, 2015)
Contact: igs.acc at noaa.gov
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 2.1839.
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:
igl1839[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1839 in the SP3 format.
igl18397.sum Combination Report for GPS Week 1839.
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 | -15.5 ns
1 | 292.1 ns
2 | -15.3 ns
3 | -14.9 ns
4 | -15.1 ns
5 | -6.8 ns
6 | -7.1 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
----+--------+---------------
0 | COD | R11
2 | COD | R11 R12
2 | GRG | R13 R16
3 | COD | R11
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 1.1839, 1a.1839).
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 2.1839.0-6)
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 3.1839.0-6).
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 1839 summary. (Apr 05, 2015 - Apr 11, 2015)
Table 1.1839.a GPS week : 1839 MJD: 57117.0-57123.0
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 0 7 33 -18 75 .41 49 47 | --- --- --- ---
| 1 1 2 35 31 27 .04 | --- ---
cof n/a| -4 1 4 39 -14 73 .44 53 49 | --- --- --- ---
| 1 1 3 32 35 47 .06 | --- ---
emx n/a| 0 0 4 -47 -78 -65 .25 25 25 | 28790 -600 3750 6953
| 1 1 1 44 7 26 .02 | 117830 926
esx n/a| 0 0 0 11 48 19 -.12 20 19 | 32120 83 3772 7714
| 1 1 1 13 18 24 .06 | 113134 1661
gfz n/a| 0 -1 1 49 58 53 .02 21 17 | 0 -873 19994 148793
| 1 1 2 9 19 27 .03 | 0 857
grg n/a| 0 0 11 -24 22 41 -.30 36 31 | 130606 -567 3743 21111
| 1 1 4 24 22 34 .06 | 112186 920
iac n/a| 1 0 -12 -21 -37 -70 -.08 19 19 | -11180 -470 20048 148858
| 1 1 1 33 23 59 .03 | 3586 848
mcc n/a| -2 0 -29 7 -42 793 -.14 179 179 | --- --- --- ---
| 7 2 7 104 103 395 .24 | --- ---
Table 1.1839.b GPS week : 1839 MJD: 57117.0-57123.0
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 13 13 13 13 14 13 |
R02 | 9 9 10 11 10 8 8 |
R03 | 9 9 9 9 9 10 12 |
R04 | 9 9 10 9 11 10 12 |
R05 | 14 12 13 12 14 14 15 |
R06 | 9 9 9 9 8 8 8 |
R07 | 11 9 9 10 10 9 8 |
R08 | 9 8 10 10 9 10 9 |
R09 | 13 11 11 11 12 11 13 |
R10 | 9 9 8 10 8 8 9 |
R11 | 18 21 14 18 22 19 19 |
R12 | 23 24 17 23 20 21 21 |
R13 | 10 8 11 9 9 10 10 |
R14 | 10 14 13 13 10 13 19 |
R15 | 13 12 11 9 11 10 10 |
R16 | 11 13 11 8 8 9 11 |
R17 | 9 7 8 9 9 7 10 |
R18 | 8 9 7 7 7 8 8 |
R19 | 9 6 6 7 7 9 9 |
R20 | 12 17 14 16 11 11 12 |
R21 | 11 11 9 8 8 8 7 |
R22 | 8 10 9 7 6 9 9 |
R23 | 8 10 8 9 7 9 12 |
R24 | 9 8 8 12 11 10 10 |
R25 | 0 0 0 0 0 0 0 |
R26 | 0 0 0 0 0 0 0 |
Table 1.1839.c GPS week : 1839 MJD: 57117.0-57123.0
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 1839 0 | 9 0 71 1316 1868 8191 85.7 1955 1955 | -15510 0
brd 1839 1 | 6 2 58 -63 1395 7052 86.4 1535 1535 | 292100 0
brd 1839 2 | -2 68 60 218 603 7703 87.9 2333 2333 | -15305 0
brd 1839 3 | -59 23 56 429 -629 5142 86.5 1761 1761 | -14890 0
brd 1839 4 | -54 -29 18 328 72 3723 86.5 1934 1934 | -15134 0
brd 1839 5 | -68 -31 0 -104 2187 1584 86.8 1924 1924 | -6767 0
brd 1839 6 | -20 -43 -28 724 1487 217 87.0 1899 1899 | -7138 0
-------------+------------------------------------------------------------+----------------
brd 1839 mean| -27 -1 34 406 997 4801 86.7 1905 1905 | 31050 0
brd 1839 sdev| 32 38 37 492 1018 3098 .7 239 239 | 115177 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 2.1839.0 GPS week: 1839 Day: 0 MJD: 57117
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 3 57 -23 42 .33 50 39 | --- --- --- ---
cof n/a| -3 0 0 44 4 32 .47 54 41 | --- --- --- ---
emx n/a| -1 0 7 -49 -65 -12 .28 23 24 | -15267 -1790 3483 7715
esx n/a| 0 2 1 11 49 9 -.05 18 18 | -8084 325 3505 8417
gfz n/a| 2 0 -1 60 57 59 .03 22 18 | 0 -2094 3452 7541
grg n/a| 0 0 5 -46 0 40 -.41 31 28 | 79921 -1463 3412 9000
iac n/a| 2 -1 -11 -23 -43 -137 -.11 25 25 | -13174 -1008 3477 7565
mcc n/a| -4 -1 -26 -41 -53 452 .12 161 161 | --- --- --- ---
Table 2.1839.1 GPS week: 1839 Day: 1 MJD: 57118
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 2 5 27 -15 40 .41 50 51 | --- --- --- ---
cof n/a| -6 3 0 -8 -31 22 .52 52 52 | --- --- --- ---
emx n/a| 0 0 5 -16 -75 -100 .21 25 26 | 295423 -766 3881 6436
esx n/a| 1 0 1 8 20 -15 -.10 20 19 | 287560 -224 3932 7210
gfz n/a| 0 -1 2 40 37 28 .07 22 17 | 0 -1738 117917 999999
grg n/a| 0 1 6 -13 33 88 -.26 36 32 | 384556 -421 3893 6184
iac n/a| 0 0 -12 -46 -12 10 -.13 19 19 | -11687 -1742 117911 999999
mcc n/a| 1 -2 -27 43 22 1384 -.42 189 189 | --- --- --- ---
Table 2.1839.2 GPS week: 1839 Day: 2 MJD: 57119
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 9 32 -37 87 .40 51 53 | --- --- --- ---
cof n/a| -6 -1 9 50 -62 38 .35 56 57 | --- --- --- ---
emx n/a| 0 -3 5 10 -88 -71 .24 27 28 | 81 -1341 4009 7629
esx n/a| -1 1 2 -4 67 63 -.23 22 19 | -21880 -2543 4047 8660
gfz n/a| 0 -1 -2 51 75 79 .03 19 17 | 0 -849 4028 7593
grg n/a| -1 0 13 -24 12 -7 -.28 59 38 | 96146 -1710 4043 42649
iac n/a| 2 2 -12 -19 -40 -115 -.09 16 16 | -13223 -601 4036 7709
mcc n/a| 0 1 -21 4 84 683 -.49 221 221 | --- --- --- ---
Table 2.1839.3 GPS week: 1839 Day: 3 MJD: 57120
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 15 33 85 .44 50 51 | --- --- --- ---
cof n/a| -3 1 4 37 40 115 .46 52 51 | --- --- --- ---
emx n/a| -1 -1 1 -77 -78 -67 .25 26 28 | -24318 339 4032 6704
esx n/a| 0 0 -1 15 54 21 -.11 22 21 | 6324 -1123 4022 6920
gfz n/a| 1 -2 0 45 63 91 -.03 20 16 | 0 -99 4019 6547
grg n/a| 0 2 15 -5 12 53 -.32 25 24 | 96165 -1062 4002 41336
iac n/a| 1 1 -15 -26 -67 -117 -.09 21 21 | -14062 408 4002 6779
mcc n/a| -8 2 -32 -100 -204 919 .09 147 147 | --- --- --- ---
Table 2.1839.4 GPS week: 1839 Day: 4 MJD: 57121
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 0 8 -8 4 69 .45 48 47 | --- --- --- ---
cof n/a| -3 2 8 1 -50 79 .47 52 49 | --- --- --- ---
emx n/a| -2 -1 4 -126 -84 -68 .24 24 25 | -19750 600 3751 6788
esx n/a| 4 0 -1 1 69 7 -.14 21 20 | -25519 1248 3761 7822
gfz n/a| 2 -2 2 61 83 15 .04 20 16 | 0 -1212 3459 6687
grg n/a| -3 0 12 -22 54 0 -.23 31 29 | 92268 834 3722 32750
iac n/a| 0 1 -10 48 -62 1 -.08 16 16 | -13968 -712 3743 6767
mcc n/a| -1 -3 -28 206 -148 1178 -.06 179 179 | --- --- --- ---
Table 2.1839.5 GPS week: 1839 Day: 5 MJD: 57122
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 7 8 -26 118 .37 49 38 | --- --- --- ---
cof n/a| -3 0 6 78 6 74 .38 50 39 | --- --- --- ---
emx n/a| 0 0 5 -43 -77 -71 .27 25 25 | -14325 -1269 3722 6818
esx n/a| 0 1 -2 37 30 29 -.09 19 18 | -7503 2668 3748 7770
gfz n/a| 0 0 4 34 29 66 .01 21 17 | 0 205 3707 6628
grg n/a| -1 0 13 7 0 57 -.27 32 30 | 83652 -433 3744 7179
iac n/a| 0 0 -11 -55 -3 -83 -.04 17 17 | -5553 782 3782 6559
mcc n/a| 10 4 -45 -92 -37 673 -.14 173 173 | --- --- --- ---
Table 2.1839.6 GPS week: 1839 Day: 6 MJD: 57123
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 11 99 -64 81 .45 48 47 | --- --- --- ---
cof n/a| -1 2 4 72 -11 150 .46 54 50 | --- --- --- ---
emx n/a| 0 2 2 -29 -79 -66 .26 23 23 | -20310 27 3377 6583
esx n/a| 0 -2 1 12 48 24 -.10 20 16 | -6054 232 3394 7200
gfz n/a| -1 0 2 50 62 36 -.01 22 16 | 0 -329 3382 6556
grg n/a| 2 1 16 -63 46 58 -.31 40 36 | 81540 285 3385 8680
iac n/a| 2 0 -14 -28 -30 -50 -.08 21 21 | -6593 -421 3391 6628
mcc n/a| -11 1 -27 30 41 260 -.05 180 180 | --- --- --- ---
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 3.1839.0 GPS week: 1839 Day: 0 MJD: 57117
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 | 1837 47 49 28 19 26 32 33 --- 13 | 129 130 141 144 148 162 --- --- 0
R02 | 2360 30 35 17 13 14 34 20 269 9 | 187 183 194 196 197 205 --- 135 0
R03 | 1755 21 23 21 17 17 20 29 --- 9 | 27 32 31 29 34 35 --- --- 0
R04 | 1546 30 39 17 16 20 21 16 --- 8 | 45 46 47 47 58 52 --- --- 0
R05 | 865 32 38 20 24 45 34 28 --- 14 | 40 54 29 28 69 32 --- --- 0
R06 | 1955 26 39 13 19 18 22 29 --- 9 | 86 92 78 80 80 79 --- --- 0
R07 | 2109 25 43 18 16 17 37 34 115 11 | 38 47 27 28 38 38 --- 49 0
R08 | 1870 35 47 14 20 20 18 16 --- 9 | 43 51 34 41 42 42 --- --- 0
R09 | 1411 39 51 34 29 14 40 20 --- 13 | 30 39 26 59 42 33 --- --- 0
R10 | 2077 30 34 17 22 12 21 18 --- 9 | 44 54 28 48 31 27 --- --- 0
R11 | 2556 156 158 49 18 29 56 22 --- 18 | 103 106 22 45 66 71 --- --- 0
R12 | 1317 124 128 39 17 40 54 30 119 23 | 95 99 29 47 62 63 --- 39 0
R13 | 1632 35 30 25 23 18 16 20 --- 10 | 35 34 26 31 27 40 --- --- 0
R14 | 1947 41 47 15 21 13 23 21 --- 9 | 30 37 38 40 36 27 --- --- 0
R15 | 5153 54 49 14 17 33 34 19 --- 12 | 48 48 30 36 41 41 --- --- 0
XR16 | 756 26 40 13 21 21 --- 26 --- 10 | 40 42 29 34 40 --- --- --- 0
R17 | 791 20 22 20 11 17 31 17 131 8 | 65 66 63 50 45 47 --- 27 0
R18 | 1840 12 17 18 12 16 22 28 117 8 | 61 61 61 50 45 38 --- 17 0
R19 | 1454 23 22 23 10 24 14 16 --- 8 | 66 67 64 45 48 55 --- --- 0
R20 | 1196 29 44 24 21 22 34 28 --- 11 | 81 95 75 79 63 67 --- --- 0
R21 | 1739 10 17 15 18 12 18 49 --- 10 | 69 76 72 77 69 77 --- --- 0
R22 | 1184 12 9 12 19 11 16 29 --- 8 | 70 69 77 81 71 69 --- --- 0
R23 | 1002 12 15 14 11 18 28 17 --- 7 | 20 22 30 40 33 22 --- --- 0
R24 | 586 12 18 26 18 14 30 9 --- 9 | 52 52 54 45 41 34 --- --- 0
XR25 |20671 --- --- --- --- --- --- 10 --- 0 | --- --- --- --- --- --- --- --- 0
XR26 |15362 --- --- --- --- --- --- 11 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1954 50 54 23 18 22 31 25 161 |T 62 66 54 58 59 58 --- 53 ---
WRMS | 1954 39 41 24 18 18 28 25 161 |NE 62 66 54 58 59 58 --- 53 ---
MEDI | 1739 29 38 18 18 18 28 20 119 |MD 48 54 34 45 45 42 --- 39 ---
Table 3.1839.1 GPS week: 1839 Day: 1 MJD: 57118
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 | 1827 40 50 31 17 27 48 20 --- 12 | 112 110 116 119 116 115 --- --- 0
R02 | 1706 25 41 17 16 21 34 11 336 8 | 141 140 147 148 144 165 --- 142 0
R03 | 1763 24 34 19 19 13 24 25 --- 9 | 29 35 28 36 30 39 --- --- 0
R04 | 1029 32 40 13 17 24 29 14 --- 9 | 38 43 37 42 52 51 --- --- 0
R05 | 676 42 49 25 16 28 37 24 --- 12 | 48 57 40 41 55 53 --- --- 0
R06 | 1618 33 38 15 19 20 21 10 --- 8 | 67 73 61 67 71 63 --- --- 0
R07 | 1310 31 44 14 11 18 36 13 123 8 | 37 44 27 26 36 40 --- 31 0
R08 | 2461 33 45 15 17 15 22 16 --- 8 | 43 51 36 36 39 31 --- --- 0
R09 | 1499 36 29 35 32 10 14 13 --- 11 | 29 30 27 37 28 18 --- --- 0
R10 | 1345 30 29 23 22 14 25 13 --- 9 | 34 36 26 30 26 25 --- --- 0
R11 | 2486 138 139 26 15 31 46 29 --- 20 | 82 84 32 35 49 49 --- --- 0
R12 | 948 141 133 40 17 40 71 27 113 23 | 83 78 34 43 59 62 --- 30 0
R13 | 2002 28 41 10 12 15 30 13 --- 7 | 40 51 27 38 31 90 --- --- 0
R14 | 1470 37 35 36 25 25 28 33 --- 13 | 27 39 46 32 38 41 --- --- 0
R15 | 1411 37 53 16 23 30 54 17 --- 12 | 34 52 29 35 32 50 --- --- 0
XR16 | 626 19 48 22 27 21 --- 28 --- 12 | 35 55 40 45 35 --- --- --- 0
R17 | 859 11 12 19 12 16 19 13 156 6 | 48 50 42 47 60 46 --- 23 0
R18 | 2143 26 21 21 13 15 40 13 118 9 | 43 41 43 43 47 26 --- 15 0
R19 | 975 20 22 19 8 10 20 11 --- 6 | 43 43 39 31 29 19 --- --- 0
R20 | 893 34 30 59 38 30 18 22 --- 16 | 61 54 56 52 46 49 --- --- 0
R21 | 1662 19 23 23 23 20 37 23 --- 10 | 43 46 53 49 33 36 --- --- 0
R22 | 1452 21 16 23 16 16 46 13 --- 9 | 46 43 55 51 44 30 --- --- 0
R23 | 921 22 28 11 23 15 48 13 --- 9 | 17 25 24 31 30 33 --- --- 0
R24 | 902 20 22 17 16 12 18 25 --- 8 | 25 48 46 35 48 44 --- --- 0
XR25 |18786 --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- --- --- 0
XR26 |16915 --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1535 50 52 25 20 22 36 19 189 |T 50 55 46 47 49 51 --- 48 ---
WRMS | 1535 51 52 26 19 17 32 19 189 |NE 50 55 46 47 49 51 --- 48 ---
MEDI | 1452 30 35 19 17 18 30 13 123 |MD 43 48 39 38 39 44 --- 30 ---
Table 3.1839.2 GPS week: 1839 Day: 2 MJD: 57119
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 | 2440 41 34 23 28 20 43 21 --- 12 | 107 114 115 127 123 117 --- --- 0
R02 | 2315 31 26 20 16 15 38 16 395 10 | 179 185 189 187 198 184 --- 158 0
R03 | 904 28 34 19 16 14 29 15 --- 8 | 31 36 25 25 26 36 --- --- 0
R04 | 899 26 28 18 15 18 37 18 --- 9 | 44 42 47 49 56 77 --- --- 0
R05 | 4637 45 48 23 26 24 31 24 --- 12 | 52 44 45 41 52 48 --- --- 0
R06 | 1765 28 35 28 17 17 26 11 --- 9 | 77 77 79 63 69 73 --- --- 0
R07 | 1183 30 46 22 15 22 27 11 144 9 | 38 48 20 24 37 36 --- 72 0
R08 | 3305 36 45 16 15 21 29 18 --- 10 | 43 47 19 28 32 40 --- --- 0
R09 | 1309 34 39 32 39 11 13 12 --- 11 | 29 31 33 58 44 27 --- --- 0
R10 | 677 18 22 21 23 11 24 12 --- 8 | 33 31 21 31 28 30 --- --- 0
R11 | 4023 156 162 33 25 31 24 23 --- 13 | 89 93 36 44 62 38 --- --- 0
R12 | 1069 141 165 51 29 28 38 21 149 16 | 76 96 29 30 58 47 --- 71 0
R13 | 1565 39 42 14 14 23 191 15 --- 10 | 42 45 21 22 24 128 --- --- 0
R14 | 1386 28 35 27 38 17 27 27 --- 12 | 23 38 33 41 25 22 --- --- 0
R15 | 5511 36 31 24 24 22 32 16 --- 11 | 33 29 28 28 31 41 --- --- 0
R16 | 782 20 29 34 20 22 171 11 --- 11 | 34 42 48 26 30 77 --- --- 0
R17 | 1218 20 26 22 18 16 19 9 163 7 | 53 62 53 36 39 49 --- 51 0
R18 | 2299 13 23 18 13 9 23 17 136 7 | 50 62 46 50 50 44 --- 26 0
R19 | 617 13 15 15 12 12 16 15 --- 6 | 50 52 54 47 40 47 --- --- 0
R20 | 2960 30 36 52 16 26 38 15 --- 13 | 58 72 55 44 40 71 --- --- 0
R21 | 2509 18 18 29 17 18 25 18 --- 9 | 52 50 50 50 44 51 --- --- 0
R22 | 1167 16 22 32 13 14 30 10 --- 8 | 54 59 65 47 44 42 --- --- 0
R23 | 1052 20 20 16 25 16 21 12 --- 8 | 18 22 21 38 23 25 --- --- 0
R24 | 1089 19 27 23 14 18 20 10 --- 7 | 43 41 38 33 31 32 --- --- 0
XR25 |18667 --- --- --- --- --- --- 10 --- 0 | --- --- --- --- --- --- --- --- 0
XR26 |22022 --- --- --- --- --- --- 10 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 2333 51 56 27 22 19 59 16 221 |T 54 59 48 48 50 57 --- 75 ---
WRMS | 2333 53 57 28 19 17 38 16 221 |NE 54 59 48 48 50 57 --- 75 ---
MEDI | 1386 28 31 23 17 18 27 15 149 |MD 44 47 38 41 40 44 --- 71 ---
Table 3.1839.3 GPS week: 1839 Day: 3 MJD: 57120
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 | 1522 42 49 23 13 20 34 36 --- 12 | 105 103 100 101 110 119 --- --- 0
R02 | 1327 31 43 22 20 19 18 30 226 10 | 163 165 167 174 175 166 --- 178 0
R03 | 971 35 40 15 19 16 24 14 --- 9 | 37 44 23 30 29 31 --- --- 0
R04 | 776 29 41 20 15 16 22 13 --- 8 | 46 55 39 46 48 59 --- --- 0
R05 | 1240 44 60 19 20 15 38 24 --- 12 | 46 66 30 44 41 62 --- --- 0
R06 | 2290 29 21 22 17 17 17 19 --- 8 | 69 63 62 65 63 69 --- --- 0
R07 | 1769 26 37 28 20 19 21 18 167 9 | 38 45 25 37 44 43 --- 61 0
R08 | 3710 40 59 16 18 22 28 13 --- 10 | 50 66 37 43 48 49 --- --- 0
R09 | 1601 36 31 19 30 12 28 14 --- 10 | 27 28 34 55 45 25 --- --- 0
R10 | 574 34 28 18 23 17 23 15 --- 9 | 43 41 27 41 39 34 --- --- 0
R11 | 1953 156 155 42 30 27 50 24 --- 17 | 92 94 27 53 62 71 --- --- 0
R12 | 917 125 109 44 16 36 40 36 84 22 | 92 78 40 44 60 43 --- 61 0
R13 | 1464 39 44 12 20 19 17 16 --- 9 | 43 51 22 33 35 34 --- --- 0
R14 | 1307 29 25 26 42 15 25 28 --- 13 | 26 31 44 49 34 38 --- --- 0
R15 | 4535 28 30 12 14 21 21 24 --- 9 | 32 41 24 27 32 20 --- --- 0
R16 | 1573 11 9 22 21 18 15 13 --- 8 | 32 33 36 43 31 36 --- --- 0
R17 | 846 21 23 26 12 16 24 19 93 9 | 55 54 59 43 45 45 --- 57 0
R18 | 1501 14 12 13 19 14 13 12 114 6 | 57 58 58 52 64 67 --- 25 0
R19 | 564 12 13 14 19 10 18 14 --- 6 | 59 59 59 56 56 64 --- --- 0
R20 | 729 51 59 63 30 20 24 20 --- 16 | 69 74 73 97 74 88 --- --- 0
R21 | 2128 21 24 23 18 14 14 18 --- 8 | 64 65 62 53 54 63 --- --- 0
R22 | 804 17 18 7 16 17 13 13 --- 6 | 61 61 48 58 48 49 --- --- 0
R23 | 1068 17 15 18 26 15 22 13 --- 8 | 27 33 34 45 34 22 --- --- 0
R24 | 717 31 38 33 25 36 12 21 --- 12 | 52 62 54 40 45 50 --- --- 0
XR25 |16346 --- --- --- --- --- --- 11 --- 0 | --- --- --- --- --- --- --- --- 0
XR26 |20075 --- --- --- --- --- --- 11 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1760 50 52 26 22 20 25 21 147 |T 57 61 49 55 54 56 --- 76 ---
WRMS | 1760 51 51 28 21 16 24 21 147 |NE 57 61 49 55 54 56 --- 76 ---
MEDI | 1327 29 31 20 19 17 22 16 114 |MD 50 58 39 45 45 49 --- 61 ---
Table 3.1839.4 GPS week: 1839 Day: 4 MJD: 57121
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 | 1010 47 65 27 30 29 34 18 --- 12 | 144 159 151 164 156 154 --- --- 0
R02 | 3070 36 36 27 16 15 31 13 312 9 | 159 159 165 150 158 162 --- 136 0
R03 | 961 35 38 19 17 16 28 13 --- 8 | 40 43 22 22 29 30 --- --- 0
R04 | 918 40 38 19 24 20 20 25 --- 10 | 93 94 84 97 102 109 --- --- 0
R05 | 877 50 42 33 23 36 38 20 --- 14 | 66 62 36 43 68 41 --- --- 0
R06 | 5843 25 33 19 13 19 28 12 --- 8 | 77 83 85 73 71 85 --- --- 0
R07 | 1962 33 29 22 17 17 31 15 182 9 | 38 33 27 31 36 42 --- 43 0
R08 | 2947 37 43 15 25 20 24 11 --- 9 | 40 43 39 52 38 33 --- --- 0
R09 | 1027 36 41 30 36 13 25 16 --- 11 | 32 38 38 53 37 35 --- --- 0
R10 | 1166 18 25 13 20 13 30 8 --- 7 | 40 47 42 42 36 36 --- --- 0
R11 | 1939 135 135 42 19 34 60 28 --- 22 | 74 76 36 44 57 70 --- --- 0
R12 | 867 125 140 34 22 28 53 23 99 20 | 77 87 27 41 58 62 --- 24 0
R13 | 1052 38 34 19 19 23 20 10 --- 9 | 32 31 25 20 26 29 --- --- 0
R14 | 975 21 31 20 25 19 16 21 --- 9 | 23 34 38 44 29 28 --- --- 0
XR15 | 4776 31 34 20 18 --- 27 18 --- 10 | 34 35 32 36 --- 27 --- --- 0
R16 | 1839 17 19 19 25 12 24 15 --- 8 | 30 34 30 46 40 32 --- --- 0
R17 | 1289 14 15 20 14 14 36 15 101 8 | 38 44 45 42 43 30 --- 38 0
R18 | 1313 15 14 23 12 14 21 11 99 7 | 50 49 55 36 42 41 --- 16 0
R19 | 856 13 19 15 16 14 26 9 --- 7 | 52 60 46 39 47 62 --- --- 0
R20 | 962 35 32 33 28 15 31 12 --- 11 | 46 53 84 55 54 83 --- --- 0
R21 | 1503 14 18 18 13 14 41 10 --- 8 | 52 60 56 57 56 29 --- --- 0
R22 | 733 17 16 13 15 11 19 9 --- 6 | 58 56 57 60 54 51 --- --- 0
R23 | 2330 9 15 17 14 17 23 11 --- 7 | 24 21 27 28 31 39 --- --- 0
R24 | 835 44 53 28 18 25 13 20 --- 11 | 59 66 48 43 35 38 --- --- 0
XR25 |19394 --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- --- --- 0
XR26 | ---- --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1934 48 52 24 21 20 31 16 179 |T 57 61 53 54 56 56 --- 51 ---
WRMS | 1934 47 49 25 20 16 29 16 179 |NE 57 61 53 54 56 56 --- 51 ---
MEDI | 1166 33 33 20 18 17 27 13 101 |MD 46 49 39 43 43 39 --- 38 ---
Table 3.1839.5 GPS week: 1839 Day: 5 MJD: 57122
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 | 1144 52 78 31 29 30 36 17 --- 13 | 94 103 100 118 111 104 --- --- 0
R02 | 5145 33 56 15 13 17 29 11 290 8 | 124 129 122 121 121 128 --- 102 0
R03 | 898 43 42 20 16 19 33 12 --- 9 | 50 46 28 35 35 37 --- --- 0
R04 | 837 41 47 21 14 18 35 13 --- 9 | 67 70 56 50 57 69 --- --- 0
R05 | 886 52 51 27 29 31 30 30 --- 14 | 69 72 44 62 56 43 --- --- 0
R06 | 1267 35 32 21 13 16 21 15 --- 8 | 90 90 76 81 75 69 --- --- 0
R07 | 677 32 39 18 11 20 35 17 188 9 | 39 46 21 28 31 37 --- 33 0
R08 | 2230 36 31 23 19 21 24 16 --- 9 | 44 42 19 38 44 40 --- --- 0
R09 | 1256 36 38 32 25 16 19 20 --- 11 | 29 33 30 42 24 25 --- --- 0
R10 | 644 31 22 13 21 16 27 10 --- 8 | 44 39 30 38 20 23 --- --- 0
R11 | 1514 121 116 37 18 32 40 20 --- 18 | 65 64 32 39 47 45 --- --- 0
R12 | 1025 132 106 38 23 36 63 24 91 21 | 74 56 25 45 55 62 --- 14 0
R13 | 3913 36 36 27 16 9 38 17 --- 10 | 30 32 29 28 22 31 --- --- 0
R14 | 868 42 44 41 33 19 28 16 --- 13 | 29 33 37 32 38 44 --- --- 0
R15 | 4181 40 56 19 17 18 31 16 --- 9 | 36 47 22 28 29 27 --- --- 0
R16 | 803 30 34 18 19 20 19 18 --- 8 | 40 41 28 35 22 29 --- --- 0
R17 | 1424 13 14 18 13 16 18 16 110 7 | 39 41 37 38 34 33 --- 17 0
R18 | 1369 12 13 16 13 15 29 14 99 7 | 41 45 42 44 39 37 --- 12 0
R19 | 992 20 20 17 13 19 25 21 --- 8 | 43 48 44 37 45 54 --- --- 0
R20 | 1519 28 31 37 20 17 27 18 --- 11 | 35 42 56 29 52 50 --- --- 0
R21 | 1400 17 24 15 15 12 30 13 --- 7 | 44 48 44 33 40 37 --- --- 0
R22 | 1008 10 14 18 17 15 35 16 --- 8 | 45 53 55 49 55 31 --- --- 0
R23 | 1067 24 20 22 14 14 35 19 --- 9 | 19 33 24 32 37 18 --- --- 0
R24 | 921 43 56 18 12 32 24 14 --- 10 | 56 75 35 27 31 29 --- --- 0
XR25 |17765 --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- --- --- 0
XR26 |13029 --- --- --- --- --- --- 8 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1923 49 50 25 19 21 32 17 173 |T 51 55 43 46 46 45 --- 35 ---
WRMS | 1923 38 39 25 18 17 30 17 173 |NE 51 55 43 46 46 45 --- 35 ---
MEDI | 1144 35 36 20 16 18 29 16 110 |MD 44 46 35 38 39 37 --- 17 ---
Table 3.1839.6 GPS week: 1839 Day: 6 MJD: 57123
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 | 2335 50 59 26 19 35 36 24 --- 13 | 112 111 124 124 133 128 --- --- 0
R02 | 5139 26 30 16 15 18 24 17 232 8 | 175 177 182 181 186 188 --- 127 0
R03 | 810 44 64 16 19 18 48 29 --- 12 | 87 100 81 86 81 98 --- --- 0
R04 | 1774 45 55 16 17 19 29 34 --- 11 | 61 67 50 57 62 71 --- --- 0
R05 | 903 50 66 34 24 33 46 27 --- 14 | 83 95 73 73 79 57 --- --- 0
R06 | 2427 34 42 17 12 15 22 15 --- 8 | 90 92 71 76 74 77 --- --- 0
R07 | 841 35 45 14 13 14 22 15 244 7 | 50 54 38 46 55 53 --- 37 0
R08 | 1108 31 49 18 14 18 27 15 --- 8 | 41 52 30 35 43 41 --- --- 0
R09 | 797 37 39 27 38 12 40 20 --- 13 | 28 33 39 67 40 41 --- --- 0
R10 | 1033 34 50 18 22 13 31 16 --- 9 | 53 62 29 46 28 25 --- --- 0
R11 | 1753 112 113 27 9 30 62 32 --- 19 | 90 92 23 29 45 50 --- --- 0
R12 | 795 128 137 37 12 36 56 23 142 20 | 90 98 22 39 64 62 --- 23 0
R13 | 919 38 51 20 17 19 25 20 --- 9 | 42 56 26 33 29 24 --- --- 0
R14 | 1134 40 42 43 31 33 92 23 --- 19 | 24 28 35 43 34 73 --- --- 0
R15 | 3281 48 51 22 15 19 25 12 --- 9 | 50 54 25 34 28 23 --- --- 0
R16 | 768 40 47 20 24 27 23 14 --- 10 | 50 55 29 46 32 26 --- --- 0
R17 | 1105 23 26 19 11 32 27 15 139 9 | 56 60 57 44 43 57 --- 39 0
R18 | 1318 12 23 20 12 15 21 18 101 7 | 55 61 53 51 43 50 --- 18 0
R19 | 844 23 16 18 8 21 25 21 --- 8 | 66 65 55 51 50 69 --- --- 0
R20 | 3369 27 21 32 31 20 22 15 --- 11 | 62 60 74 57 55 71 --- --- 0
R21 | 1591 20 20 15 11 8 21 21 --- 7 | 71 74 73 60 64 68 --- --- 0
R22 | 2079 19 23 21 13 10 38 16 --- 8 | 76 74 81 75 63 46 --- --- 0
R23 | 977 23 29 9 35 13 61 15 --- 12 | 31 29 35 61 41 22 --- --- 0
R24 | 712 32 21 23 14 19 43 16 --- 10 | 70 64 57 48 37 32 --- --- 0
XR25 |17825 --- --- --- --- --- --- 9 --- 0 | --- --- --- --- --- --- --- --- 0
XR26 |13173 --- --- --- --- --- --- 9 --- 0 | --- --- --- --- --- --- --- --- 0
------+---------------------------------------------------+-----------------------------------------------
RMS | 1899 48 54 23 20 22 40 21 180 |T 67 71 56 60 58 60 --- 48 ---
WRMS | 1899 47 50 23 16 16 36 21 180 |NE 67 71 56 60 58 60 --- 48 ---
MEDI | 1108 34 42 20 15 19 27 16 142 |MD 61 62 50 51 45 53 --- 37 ---
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