[IGSREPORT-25424] Wk 1958 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 4 05:12:07 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1958 (Jul 16, 2017 - Jul 22, 2017)
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 2.1958.
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:
igl1958[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1958 in the SP3 format.
igl19587.sum Combination Report for GPS Week 1958.
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
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
ftp://igs.org/pub/station/general/igs14.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 | 8.0 ns
1 | 7.9 ns
2 | 8.3 ns
3 | 0.3 ns
4 | -0.8 ns
5 | -13.5 ns
6 | -19.2 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 | R16
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 1.1958, 1a.1958).
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 2.1958.0-6)
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 3.1958.0-6).
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 1958 summary. (Jul 16, 2017 - Jul 22, 2017)
Table 1.1958.a GPS week : 1958 MJD: 57950.0-57956.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 1 -28 3 50 .07 30 31 | 3840 27 3361 10959
| 1 0 3 21 14 20 .03 | 8537 1944
cof n/a| 0 1 0 -24 18 43 .10 33 33 | 3840 17 3358 10958
| 0 1 2 21 20 22 .06 | 8530 1938
emx n/a| -1 0 9 0 -45 73 .03 21 21 | -4861 -446 3367 10170
| 1 1 3 19 28 33 .03 | 15800 936
esx n/a| 0 0 0 14 20 -27 .15 17 15 | -2267 -1258 3361 12728
| 0 0 2 19 12 20 .03 | 9841 2442
gfz n/a| 0 0 2 -17 36 28 .09 23 20 | 0 -152 3369 10640
| 1 1 2 22 14 43 .04 | 0 1280
grg n/a| 0 0 -6 -73 22 -119 -.39 539 28 | 9059 -124 6308 59986
| 1 1 8 12 26 42 .06 | 23757 1689
iac n/a| 1 0 -2 45 -21 -8 -.09 17 17 | 204 -1094 3475 10048
| 0 0 2 37 32 46 .03 | 10962 616
mcc n/a| 1 0 -6 91 -26 545 .14 125 125 | --- --- --- ---
| 7 5 12 102 112 380 .26 | --- ---
Table 1.1958.b GPS week : 1958 MJD: 57950.0-57956.0
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 | 9 7 9 13 7 11 9 |
R02 | 6 7 8 9 6 6 8 |
R03 | 6 7 4 7 10 9 6 |
R04 | 6 6 7 5 7 9 7 |
R05 | 12 11 13 13 11 16 12 |
R06 | 12 9 8 7 9 10 10 |
R07 | 6 5 6 7 6 8 7 |
R08 | 8 6 7 7 8 6 8 |
R09 | 12 10 7 7 8 10 8 |
R10 | 8 8 7 8 8 9 10 |
R11 | 6 8 7 7 6 7 7 |
R13 | 6 7 8 8 8 7 7 |
R15 | 10 11 9 10 8 11 8 |
R16 | 11 10 9 10 9 15 11 |
R17 | 12 12 10 9 10 10 10 |
R18 | 9 10 9 9 9 11 8 |
R19 | 15 14 15 15 14 15 15 |
R20 | 15 12 15 13 16 15 16 |
R21 | 11 11 9 11 12 13 11 |
R22 | 12 11 11 10 12 14 12 |
R23 | 10 8 8 9 8 7 8 |
R24 | 15 15 17 17 21 14 16 |
R26 | 20 43 31 17 14 28 24 |
Table 1.1958.c GPS week : 1958 MJD: 57950.0-57956.0
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 1958 0 | -48 -47 131 2129 1078 1429 84.5 1302 1302 | 8024 0
brd 1958 1 | 55 -17 126 1883 1555 2345 84.0 1201 1201 | 7893 0
brd 1958 2 | 33 16 174 -322 -392 3603 84.2 1237 1237 | 8347 0
brd 1958 3 | 27 -21 52 40 -432 6404 82.2 1556 1556 | 339 0
brd 1958 4 | 2 -12 41 66 424 4121 81.5 1802 1802 | -816 0
brd 1958 5 | 72 -2 5 1600 890 1884 82.0 1528 1528 | -13473 0
brd 1958 6 | -79 22 88 495 -204 884 82.1 1388 1388 | -19228 0
-------------+------------------------------------------------------------+----------------
brd 1958 mean| 8 -8 88 841 416 2952 82.9 1430 1430 | -1273 0
brd 1958 sdev| 55 24 59 1002 787 1906 1.2 212 212 | 11083 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 2.1958.0 GPS week: 1958 Day: 0 MJD: 57950
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 -3 22 53 .11 30 32 | 8871 957 3741 10732
cof n/a| 1 0 -2 -28 1 18 .20 33 35 | 8870 962 3741 10733
emx n/a| -1 -1 6 -16 -16 63 .04 20 20 | 9831 420 3735 9907
esx n/a| 1 0 -2 -8 6 -16 .18 21 18 | 3045 953 3739 12144
gfz n/a| -1 0 -1 -39 7 68 .11 24 19 | 0 776 3733 10484
grg n/a| 2 2 8 -56 13 -137 -.31 25 22 | 7447 1141 3741 10060
iac n/a| 0 0 -4 83 -8 5 -.08 18 18 | 10062 -1415 3740 9858
mcc n/a| -8 3 -9 247 -96 486 -.12 105 105 | --- --- --- ---
Table 2.1958.1 GPS week: 1958 Day: 1 MJD: 57951
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 2 -2 -25 3 49 .12 31 29 | 10985 -583 3298 10571
cof n/a| 0 3 -3 -8 27 54 .05 34 32 | 10982 -601 3295 10571
emx n/a| 0 0 4 -22 -18 32 .01 16 16 | -2770 -1038 3320 9770
esx n/a| 0 0 -1 4 20 -29 .16 17 16 | 8105 -2316 3305 13085
gfz n/a| 0 0 2 -39 31 67 .04 23 19 | 0 -262 3303 10387
grg n/a| 0 1 1 -76 18 -44 -.46 30 28 | 8151 -744 3309 9874
iac n/a| 0 0 -4 90 -18 -41 -.11 17 17 | 9129 -1283 3311 9537
mcc n/a| -2 -7 -13 129 -186 651 .01 105 105 | --- --- --- ---
Table 2.1958.2 GPS week: 1958 Day: 2 MJD: 57952
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 2 -37 10 67 .05 31 29 | 10776 3004 3000 11504
cof n/a| 0 1 0 -24 25 62 .10 32 28 | 10775 2992 2994 11503
emx n/a| -2 -1 10 31 -43 102 .01 21 21 | 2972 1043 3016 10616
esx n/a| 0 0 0 5 21 -11 .16 15 14 | -5819 3113 3017 13195
gfz n/a| 0 0 6 17 55 57 .10 23 18 | 0 1724 3036 11266
grg n/a| -1 0 -14 -62 -6 -137 -.32 27 24 | 6895 2753 3012 10520
iac n/a| 0 1 -1 18 -18 -52 -.11 16 16 | 9200 103 3029 10447
mcc n/a| 0 -5 -16 145 -17 369 .00 122 122 | --- --- --- ---
Table 2.1958.3 GPS week: 1958 Day: 3 MJD: 57953
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 1 -3 -1 64 .02 28 28 | 6630 -262 3168 11669
cof n/a| 0 3 2 -14 27 37 .15 32 32 | 6621 -252 3165 11668
emx n/a| 0 -2 9 -13 -38 86 .03 25 25 | -14022 -762 3179 10869
esx n/a| 0 1 1 11 21 -18 .15 14 12 | -5828 -1932 3151 13146
gfz n/a| 0 -2 6 -23 37 53 .12 22 22 | 0 71 3163 11319
grg n/a| -1 -1 -7 -72 18 -174 -.43 33 30 | 264 28 3159 10602
iac n/a| 1 0 -4 36 -30 -38 -.14 17 17 | 1833 -1152 3935 10911
mcc n/a| 0 -2 -14 122 104 438 -.02 126 126 | --- --- --- ---
Table 2.1958.4 GPS week: 1958 Day: 4 MJD: 57954
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 -19 12 24 .08 29 31 | 6097 -1883 3621 10902
cof n/a| 0 2 1 -4 45 10 .03 32 34 | 6084 -1875 3621 10902
emx n/a| -2 0 10 5 -31 27 -.00 17 17 | 10982 -1160 3622 10237
esx n/a| 1 1 2 42 36 -30 .13 17 14 | 10983 -3256 3621 12780
gfz n/a| -3 1 0 7 32 -33 .15 22 22 | 0 -1732 3627 10917
grg n/a| 0 0 -14 -78 75 -144 -.45 28 30 | 15 -1860 3696 10165
iac n/a| 0 0 -4 -2 -79 64 -.07 16 16 | 556 -1919 3612 9961
mcc n/a| 12 -2 -13 -37 -111 721 .64 132 132 | --- --- --- ---
Table 2.1958.5 GPS week: 1958 Day: 5 MJD: 57955
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 1 -46 4 21 .06 31 34 | -6210 1513 3453 10399
cof n/a| 0 0 2 -20 20 72 .12 33 35 | -6191 1465 3446 10395
emx n/a| -2 0 11 5 -84 92 .08 24 23 | -6522 -85 3471 9711
esx n/a| 1 0 -2 41 33 -72 .08 18 16 | -11398 -1647 3467 12073
gfz n/a| -1 -3 3 -15 47 -14 .08 24 18 | 0 180 3473 9564
grg n/a| 0 0 -4 -73 34 -104 -.42 3604 36 | 58827 -107 24017 358910
iac n/a| 2 0 -3 14 -24 41 -.05 17 17 | -11693 -1039 3469 9633
mcc n/a| 10 5 7 -38 2 1201 .33 143 143 | --- --- --- ---
Table 2.1958.6 GPS week: 1958 Day: 6 MJD: 57956
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 7 -61 -24 69 .07 30 30 | -10266 -2551 3250 10942
cof n/a| 0 0 3 -69 -15 49 .06 34 31 | -10261 -2566 3245 10940
emx n/a| -2 -1 13 13 -85 111 .06 25 25 | -34502 -1546 3229 10080
esx n/a| 0 0 -3 4 3 -15 .16 15 14 | -14958 -3722 3230 12675
gfz n/a| 1 0 1 -26 41 -1 .03 23 19 | 0 -1822 3254 10543
grg n/a| -1 0 -13 -97 4 -94 -.36 29 26 | -18186 -2082 3223 9773
iac n/a| 2 0 1 76 29 -36 -.08 17 17 | -17657 -959 3232 9994
mcc n/a| -4 4 16 71 117 -47 .12 142 142 | --- --- --- ---
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 3.1958.0 GPS week: 1958 Day: 0 MJD: 57950
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 | 1075 22 22 16 14 14 30 17 --- 8 | 50 54 66 55 52 73 50 --- 56
R02 | 1280 14 14 14 15 11 17 8 147 6 | 59 56 57 48 45 43 47 64 48
R03 | 1041 11 10 13 7 11 21 10 114 5 | 60 60 60 60 59 61 59 39 58
R04 | 1712 9 14 10 7 22 11 9 --- 5 | 59 58 59 56 49 59 52 --- 54
R05 | 796 30 41 21 29 17 36 27 --- 12 | 45 53 54 51 59 51 41 --- 47
R06 | 1461 23 19 31 29 32 31 12 --- 12 | 28 31 36 39 36 28 24 --- 24
R07 | 1136 11 13 11 15 10 7 16 111 5 | 62 63 65 68 60 65 51 74 61
R08 | 717 12 18 9 19 10 20 25 --- 8 | 53 53 53 58 57 52 44 --- 51
R09E | 2925 18 18 23 21 15 47 15 --- 11 | 53 52 61 54 64 58 59 --- 56
R10E | 1287 24 23 11 18 13 22 21 --- 8 | 46 47 41 48 48 44 51 --- 45
R11E | 951 12 14 14 10 17 17 9 75 6 | 33 36 27 37 31 34 32 61 31
R13E | 1506 10 12 13 14 14 11 12 --- 5 | 38 40 35 44 32 33 40 --- 36
R15E | 2185 19 14 22 27 21 25 17 --- 10 | 51 52 44 54 43 40 50 --- 45
R16E | 1248 14 26 24 32 18 32 22 --- 11 | 53 64 59 68 64 9999 53 --- 55
R17 | 553 52 57 24 21 30 15 17 --- 12 | 81 86 51 50 35 46 37 --- 46
R18 | 691 34 39 19 18 21 14 14 --- 9 | 72 75 47 51 35 49 42 --- 45
R19 | 922 60 62 23 23 37 27 23 --- 14 | 96 98 51 49 36 62 41 --- 49
R20 | 1384 62 69 27 26 36 28 23 --- 15 | 78 89 41 48 39 48 42 --- 42
R21 | 934 48 48 18 13 24 10 20 51 10 | 82 87 55 56 44 57 44 63 53
R22 | 674 44 49 20 10 31 21 24 --- 11 | 95 98 64 66 55 71 58 --- 64
R23 | 704 18 18 20 32 26 19 11 --- 9 | 46 46 48 70 40 50 56 --- 51
R24 | 908 23 25 33 34 44 35 29 --- 15 | 68 85 76 91 59 75 76 --- 74
XR26 | ---- 25 51 --- --- --- --- 16 --- 20 | 65 78 --- --- --- --- 44 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1302 30 33 20 21 24 25 18 105 |T 59 63 52 55 47 52 47 60 49
WRMS | 1302 32 35 20 18 19 22 18 105 |NE 64 68 55 57 47 55 47 60 51
MEDI | 1041 22 22 19 18 18 21 17 111 |MD 59 58 53 54 45 51 47 63 49
Table 3.1958.1 GPS week: 1958 Day: 1 MJD: 57951
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 | 825 18 21 11 10 18 13 21 --- 7 | 34 34 48 46 47 42 33 --- 40
R02 | 1227 13 18 10 15 11 29 12 166 6 | 40 43 39 42 40 49 31 100 38
R03 | 1406 11 14 10 19 13 29 11 112 7 | 43 42 38 50 41 32 43 56 40
R04 | 789 10 12 9 13 17 26 9 --- 6 | 40 43 41 38 40 63 45 --- 42
R05 | 794 26 22 12 16 35 42 17 --- 10 | 31 34 30 31 41 56 29 --- 29
R06 | 1130 25 30 12 20 19 27 19 --- 8 | 20 26 23 34 32 23 24 --- 22
R07 | 925 5 10 8 11 11 15 9 92 4 | 43 43 45 41 46 45 44 56 43
R08 | 1071 10 11 7 15 13 19 9 --- 5 | 37 35 41 46 45 33 44 --- 40
R09E | 3348 16 13 19 12 15 53 16 --- 10 | 38 41 50 45 50 53 43 --- 44
R10E | 923 15 27 12 16 24 19 17 --- 7 | 42 42 40 42 45 34 37 --- 38
R11E | 951 14 14 16 14 25 21 11 50 7 | 28 29 33 32 33 30 26 55 27
R13E | 901 14 14 12 15 17 27 14 --- 7 | 35 35 31 36 36 27 35 --- 31
R15E | 1555 22 17 27 19 32 32 19 --- 11 | 34 33 39 40 39 36 38 --- 34
R16E | 1419 18 29 23 20 17 32 20 --- 9 | 41 46 52 46 45 9999 44 --- 41
R17 | 594 44 54 21 16 34 18 22 --- 11 | 52 62 42 44 30 39 28 --- 35
R18 | 551 36 39 16 11 23 35 10 --- 9 | 45 46 32 33 25 35 30 --- 29
R19 | 747 70 67 17 15 35 36 20 --- 14 | 62 59 37 30 32 36 29 --- 31
R20 | 1209 53 74 20 19 21 24 26 --- 12 | 49 70 35 40 33 26 36 --- 31
R21 | 790 45 47 17 17 29 17 17 60 10 | 47 46 31 33 20 24 28 47 27
R22 | 734 49 49 13 12 28 24 15 --- 10 | 59 60 42 44 44 49 45 --- 43
R23 | 679 10 11 19 19 11 26 8 --- 7 | 33 37 33 39 34 34 35 --- 33
R24 | 712 42 38 23 35 35 51 27 --- 15 | 31 44 51 58 39 44 45 --- 42
XR26 | ---- 58 202 --- --- --- --- 31 --- 42 | 78 204 --- --- --- --- 38 --- 44
------+---------------------------------------------------+-----------------------------------------------
RMS | 1200 31 34 16 17 23 30 17 104 |T 41 50 38 40 38 38 36 62 35
WRMS | 1200 29 32 16 16 19 28 17 104 |NE 43 54 38 40 36 39 35 64 35
MEDI | 901 18 22 13 15 19 26 17 92 |MD 40 43 39 40 39 36 36 56 38
Table 3.1958.2 GPS week: 1958 Day: 2 MJD: 57952
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 | 672 19 19 32 11 18 17 12 --- 8 | 47 42 39 46 44 41 38 --- 38
R02 | 1254 14 12 15 11 14 32 11 180 7 | 49 46 49 44 49 30 36 123 40
R03 | 816 9 13 5 9 7 10 12 145 4 | 46 51 45 46 48 46 42 39 44
R04 | 560 18 15 19 12 13 28 7 --- 7 | 47 46 41 43 48 29 36 --- 37
R05 | 491 34 31 22 18 40 39 19 --- 12 | 40 43 53 42 67 42 39 --- 43
R06 | 855 18 25 17 10 15 25 16 --- 7 | 25 27 29 34 30 34 27 --- 26
R07 | 656 11 13 13 11 13 17 13 76 5 | 49 47 53 57 46 34 41 49 46
R08 | 862 16 15 18 18 11 14 16 --- 7 | 43 41 47 37 37 37 34 --- 35
R09E | 3255 12 19 18 10 16 21 12 --- 6 | 27 31 26 36 42 39 35 --- 32
R10E | 1329 16 15 18 16 17 20 11 --- 7 | 36 44 33 38 38 40 40 --- 35
R11E | 777 13 15 15 9 19 25 13 99 7 | 27 28 24 23 26 36 22 43 22
R13E | 1284 16 17 14 11 22 22 16 --- 7 | 45 46 37 43 38 39 43 --- 39
R15E | 1478 18 25 17 21 23 27 15 --- 9 | 57 61 50 59 53 45 58 --- 52
R16E | 2220 20 35 15 20 16 28 17 --- 8 | 22 40 25 36 29 734 21 --- 23
R17 | 969 39 29 20 11 26 16 16 --- 9 | 60 55 43 46 35 54 35 --- 42
R18 | 565 32 32 20 13 25 10 13 --- 8 | 53 54 40 44 26 36 34 --- 37
R19 | 970 71 84 31 12 37 20 23 --- 14 | 78 87 50 42 25 47 23 --- 38
R20 | 1073 56 41 33 24 34 43 24 --- 15 | 57 54 49 41 28 42 28 --- 29
R21 | 761 41 41 17 8 30 14 13 70 9 | 51 52 32 33 25 41 28 52 31
R22 | 871 45 46 20 15 33 19 14 --- 10 | 72 72 64 67 53 51 57 --- 58
R23 | 756 15 16 18 20 9 27 12 --- 8 | 36 43 38 47 36 30 44 --- 38
R24 | 1218 47 39 32 27 28 64 25 --- 16 | 99 106 98 105 90 93 106 --- 99
XR26 | ---- 43 66 --- --- --- --- 21 --- 30 | 58 68 --- --- --- --- 46 --- 48
------+---------------------------------------------------+-----------------------------------------------
RMS | 1236 31 32 21 15 23 27 16 122 |T 48 51 43 45 41 73 39 61 40
WRMS | 1236 29 28 21 14 18 24 16 122 |NE 53 54 48 48 42 42 40 65 42
MEDI | 862 18 25 18 12 18 21 14 99 |MD 47 46 41 43 38 40 36 49 38
Table 3.1958.3 GPS week: 1958 Day: 3 MJD: 57953
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 | 699 20 33 57 9 23 34 19 --- 12 | 55 70 43 43 62 61 47 --- 43
R02 | 938 18 17 20 13 11 49 9 154 9 | 57 58 64 60 61 35 50 70 53
R03 | 1067 8 9 9 9 15 31 12 138 6 | 54 56 53 55 60 42 46 33 51
R04 | 2061 7 10 12 7 12 14 13 --- 5 | 46 47 46 48 47 46 37 --- 43
R05 | 700 34 35 34 18 20 56 22 --- 13 | 46 54 61 62 49 37 46 --- 49
R06 | 803 11 17 11 18 10 24 14 --- 7 | 26 32 25 43 38 28 27 --- 29
R07 | 648 18 21 19 8 11 22 15 97 6 | 55 58 53 42 51 46 34 40 43
R08 | 784 20 21 14 12 16 16 17 --- 7 | 47 51 46 60 62 49 50 --- 52
R09E | 4805 14 20 19 11 12 30 15 --- 7 | 29 28 30 32 36 47 35 --- 32
R10E | 1567 12 13 26 13 17 25 11 --- 7 | 38 42 33 51 51 32 44 --- 41
R11E | 2160 11 12 17 9 19 20 11 152 6 | 26 29 24 29 34 29 26 43 25
R13E | 967 15 13 17 15 22 28 16 --- 8 | 67 64 56 67 64 57 67 --- 62
R15E | 1587 21 20 14 11 20 39 26 --- 9 | 42 46 41 43 41 46 47 --- 41
R16E | 1745 21 30 29 20 21 30 15 --- 10 | 38 53 35 45 42 956 38 --- 35
R17 | 829 38 44 18 9 23 10 17 --- 9 | 61 66 43 43 31 42 31 --- 39
R18 | 1039 29 29 15 9 26 21 16 --- 8 | 63 63 44 46 41 54 43 --- 46
R19 | 735 66 59 25 16 39 22 25 --- 15 | 92 87 56 49 34 58 41 --- 49
R20 | 1659 41 54 38 15 31 29 28 --- 13 | 57 71 35 44 37 58 40 --- 36
R21 | 595 49 59 16 10 35 13 13 68 11 | 70 76 42 41 27 43 37 36 40
R22 | 710 41 41 18 7 28 15 16 --- 9 | 80 77 50 55 46 57 54 --- 55
R23 | 695 18 27 23 25 18 25 10 --- 9 | 31 28 36 56 42 31 44 --- 41
R24 | 1089 28 34 45 24 27 78 23 --- 16 | 65 65 58 58 47 52 66 --- 54
XR26 | 6307 22 47 --- --- --- --- 12 --- 16 | 41 78 --- --- --- --- 35 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1555 28 32 25 14 22 33 17 126 |T 51 56 44 48 45 86 42 44 43
WRMS | 1555 28 32 25 12 22 30 17 126 |NE 55 61 47 50 45 46 42 44 44
MEDI | 967 20 27 18 11 20 25 15 138 |MD 54 58 43 46 42 46 43 40 43
Table 3.1958.4 GPS week: 1958 Day: 4 MJD: 57954
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 | 596 21 31 13 12 14 17 15 --- 6 | 54 64 47 50 47 48 42 --- 46
R02 | 538 12 18 14 10 14 19 10 127 6 | 54 54 57 49 51 40 49 33 50
R03 | 997 8 12 9 25 24 41 21 121 10 | 50 53 55 68 68 34 43 34 52
R04 | 2713 10 11 14 14 8 25 17 --- 7 | 47 48 46 45 44 36 41 --- 42
R05 | 707 22 25 22 29 16 39 16 --- 11 | 46 64 64 54 69 33 49 --- 50
R06 | 1437 10 10 20 17 26 30 19 --- 9 | 34 34 31 43 50 33 29 --- 32
R07 | 1301 17 22 11 12 11 15 13 133 6 | 56 59 49 47 49 51 41 87 47
R08 | 898 9 11 13 10 22 33 15 --- 7 | 50 50 51 52 45 67 46 --- 49
R09E | 5876 17 16 17 11 15 32 14 --- 8 | 40 39 41 52 51 56 54 --- 47
R10E | 2556 20 21 23 11 19 19 12 --- 7 | 43 44 37 44 42 34 49 --- 40
R11E | 1701 11 13 10 8 14 18 13 178 5 | 35 36 35 37 37 35 40 43 35
R13E | 1481 17 21 24 13 15 20 12 --- 7 | 34 34 28 32 31 30 31 --- 28
R15E | 1263 14 16 14 15 15 29 22 --- 8 | 46 46 45 46 44 48 43 --- 43
R16E | 1007 14 21 18 16 26 30 18 --- 9 | 44 46 46 47 48 9999 52 --- 45
R17 | 715 47 48 15 10 24 16 17 --- 10 | 59 59 34 35 36 34 34 --- 34
R18 | 763 34 40 14 6 22 30 13 --- 8 | 56 60 37 37 34 46 40 --- 38
R19 | 813 61 68 19 28 31 21 22 --- 14 | 75 80 45 53 40 42 43 --- 45
R20 | 1468 46 45 25 27 43 58 18 --- 15 | 54 62 40 58 52 54 48 --- 43
R21 | 725 50 52 21 14 30 22 17 88 11 | 68 69 45 40 28 56 45 42 43
R22 | 761 52 53 18 15 32 18 19 --- 11 | 102 103 83 90 85 84 83 --- 86
R23 | 571 14 13 14 27 10 22 15 --- 8 | 35 45 37 45 34 31 43 --- 36
XR24 | 1231 35 53 57 25 --- 51 33 --- 21 | 91 108 68 89 --- 67 91 --- 79
XR26 | ---- 19 38 --- --- --- --- 9 --- 13 | 67 84 --- --- --- --- 55 --- 56
------+---------------------------------------------------+-----------------------------------------------
RMS | 1801 29 32 17 17 22 28 16 132 |T 53 58 46 50 46 45 47 47 46
WRMS | 1801 31 34 17 14 22 30 16 132 |NE 58 64 49 53 48 47 48 49 48
MEDI | 997 17 21 15 14 19 22 16 127 |MD 50 54 45 47 45 42 43 42 45
Table 3.1958.5 GPS week: 1958 Day: 5 MJD: 57955
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 | 878 24 34 24 25 28 29 14 --- 10 | 32 27 45 36 45 46 23 --- 29
R02 | 1038 14 22 12 12 12 13 12 114 5 | 49 54 49 41 48 54 37 48 43
R03 | 1207 13 18 25 17 12 17 24 96 8 | 49 48 59 39 42 42 26 47 38
R04 | 1820 18 21 17 13 15 39 16 --- 8 | 46 48 46 42 44 28 31 --- 36
R05 | 548 20 20 33 32 23 89 16 --- 16 | 34 37 55 35 37 50 29 --- 32
R06 | 1198 23 23 24 24 14 33 16 --- 10 | 25 28 26 44 34 20 25 --- 28
R07 | 1605 14 15 19 12 13 39 13 187 8 | 46 44 39 38 42 70 32 148 39
R08 | 1049 12 18 15 16 11 19 8 --- 6 | 42 45 36 34 38 42 31 --- 34
R09E | 4597 17 21 27 11 13 49 15 --- 9 | 31 36 37 38 43 66 39 --- 37
R10E | 1876 26 23 19 15 24 32 11 --- 9 | 34 35 36 39 44 33 34 --- 33
R11E | 1091 10 13 15 14 16 25 9 178 6 | 24 28 25 29 26 35 23 35 23
R13E | 1675 13 17 15 11 20 22 11 --- 6 | 48 50 40 39 42 54 41 --- 41
R15E | 1037 20 16 22 21 34 28 21 --- 11 | 32 33 35 38 38 37 31 --- 29
R16E | 1564 22 24 28 27 40 >>>> 27 --- 14 | 51 53 51 71 79 9999 53 --- 57
R17 | 810 43 51 17 11 22 20 11 --- 9 | 46 51 29 33 28 24 32 --- 29
R18 | 558 32 31 18 9 22 53 13 --- 10 | 49 49 28 34 37 58 36 --- 34
R19 | 1114 71 67 27 20 29 17 23 --- 15 | 64 61 32 41 33 32 37 --- 34
R20 | 826 39 55 35 19 37 64 18 --- 15 | 39 57 37 40 27 48 36 --- 31
R21 | 1055 49 48 20 11 33 29 25 113 12 | 55 54 35 36 26 46 24 64 31
R22 | 658 55 55 21 11 33 31 27 --- 13 | 66 67 49 52 47 63 36 --- 46
R23 | 684 11 18 16 20 11 24 13 --- 7 | 33 28 32 43 27 27 36 --- 32
R24 | 1498 30 24 48 19 27 49 21 --- 14 | 74 69 73 68 91 42 58 --- 62
XR26 | ---- 39 84 --- --- --- --- 19 --- 28 | 27 58 --- --- --- --- 44 --- 34
------+---------------------------------------------------+-----------------------------------------------
RMS | 1528 31 33 24 18 24 3603 17 143 |T 43 46 40 41 41 43 34 68 36
WRMS | 1528 34 35 23 16 18 36 17 143 |NE 45 48 41 41 40 43 33 76 36
MEDI | 1055 22 23 20 15 22 29 16 114 |MD 46 48 37 39 38 42 34 48 34
Table 3.1958.6 GPS week: 1958 Day: 6 MJD: 57956
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 | 609 18 23 20 23 21 25 12 --- 9 | 59 59 56 53 53 59 43 --- 49
R02 | 1343 20 21 18 12 29 22 13 122 8 | 61 62 63 55 55 39 53 33 52
R03 | 1110 15 21 10 12 14 18 12 88 6 | 68 70 67 67 65 59 55 74 63
R04 | 1087 16 17 18 17 12 22 11 --- 7 | 67 65 67 55 58 50 52 --- 56
R05 | 1133 24 19 27 24 18 43 21 --- 11 | 52 46 60 44 53 48 50 --- 48
R06 | 1432 20 19 17 14 24 37 17 --- 9 | 38 40 37 44 47 36 36 --- 36
R07 | 1500 9 17 14 10 9 29 14 181 6 | 71 71 66 64 68 80 53 156 64
R08 | 808 12 12 14 12 17 31 12 --- 7 | 63 63 59 58 61 65 51 --- 57
R09E | 3533 14 15 19 17 16 28 13 --- 8 | 29 30 31 40 45 40 39 --- 35
R10E | 2123 15 17 16 14 26 25 27 --- 9 | 38 40 30 44 46 38 40 --- 36
R11E | 1042 12 15 16 12 20 27 11 136 7 | 33 34 28 34 36 37 34 82 31
R13E | 1050 13 12 16 15 17 16 19 --- 7 | 46 47 48 54 52 46 34 --- 45
R15E | 1323 18 25 28 9 19 27 10 --- 8 | 59 60 54 56 51 57 51 --- 52
R16E | 891 18 42 32 18 30 21 21 --- 10 | 44 64 47 50 56 9999 48 --- 45
R17 | 654 46 47 20 9 24 17 19 --- 10 | 73 76 45 43 32 33 34 --- 39
R18 | 633 31 37 21 10 20 16 12 --- 8 | 68 72 43 49 36 47 43 --- 45
R19 | 1866 73 79 32 20 37 19 17 --- 15 | 100 105 52 48 41 47 40 --- 47
R20 | 1164 48 31 50 15 26 46 24 --- 15 | 84 79 52 59 49 55 50 --- 52
R21 | 925 45 45 21 11 25 20 22 163 10 | 81 83 53 55 39 51 40 102 49
R22 | 1140 50 52 16 12 35 23 18 --- 11 | 94 94 67 64 50 70 55 --- 62
R23 | 1061 16 12 17 16 13 24 18 --- 7 | 38 40 44 58 38 33 52 --- 45
R24 | 915 24 59 50 14 36 62 25 --- 15 | 82 106 81 85 69 64 74 --- 74
XR26 | ---- 32 114 --- --- --- --- 17 --- 23 | 46 101 --- --- --- --- 67 --- 56
------+---------------------------------------------------+-----------------------------------------------
RMS | 1387 30 34 25 15 23 29 17 142 |T 60 65 52 53 50 50 47 89 49
WRMS | 1387 30 31 25 14 19 26 17 142 |NE 67 72 57 56 50 52 49 91 52
MEDI | 1087 18 21 18 14 20 24 17 136 |MD 61 64 52 54 50 48 50 82 49
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