[IGSREPORT-26104] Wk 2014 IGLOS Final Orbits
acc
acc at igs.org
Mon Sep 3 04:24:07 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2014 (Aug 12, 2018 - Aug 18, 2018)
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 2.2014.
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:
igl2014[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2014 in the SP3 format.
igl20147.sum Combination Report for GPS Week 2014.
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 | 2.3 ns
1 | 3.3 ns
2 | 1.8 ns
3 | -0.3 ns
4 | 3.3 ns
5 | 4.0 ns
6 | 2.4 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2014, 1a.2014).
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 2.2014.0-6)
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 3.2014.0-6).
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 2014 summary. (Aug 12, 2018 - Aug 18, 2018)
Table 1.2014.a GPS week : 2014 MJD: 58342.0-58348.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 11 7 -2 -32 -.01 39 37 | 5125 -773 3596 10131
| 1 1 2 10 19 37 .03 | 1027 2199
cof n/a| -1 0 15 5 3 -24 .03 42 38 | 5126 -782 3596 10131
| 1 1 2 28 23 23 .05 | 1024 2201
emx n/a| 0 1 0 5 -32 64 .03 25 25 | -2237 -1241 3569 9511
| 1 2 2 19 16 36 .04 | 9728 1223
esx n/a| 0 0 0 7 18 7 .11 13 11 | 9539 -1108 3560 11877
| 0 0 1 13 9 20 .01 | 6997 1842
gfz n/a| -1 1 -8 14 37 40 .12 27 24 | 0 -919 3553 9808
| 0 2 4 24 19 32 .03 | 0 2361
grg n/a| 2 -1 2 -57 0 -163 -.31 46 41 | 2697 -588 3612 9377
| 1 1 3 18 19 89 .06 | 1397 2526
iac n/a| 1 0 -2 -1 -15 -6 -.20 20 20 | 3969 -306 4263 10950
| 1 1 2 23 23 41 .05 | 951 1229
mcc n/a| 1 -6 40 14 -17 -146 -.66 149 149 | --- --- --- ---
| 6 8 7 125 150 579 .56 | --- ---
Table 1.2014.b GPS week : 2014 MJD: 58342.0-58348.0
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 | 18 18 21 17 19 16 15 |
R02 | 9 9 11 9 9 8 7 |
R03 | 10 9 11 12 11 11 10 |
R04 | 8 8 8 9 9 8 9 |
R07 | 12 14 11 9 9 9 10 |
R08 | 9 9 10 10 9 8 8 |
R09 | 5 7 8 6 6 8 7 |
R10 | 8 7 7 7 10 10 9 |
R11 | 7 7 7 7 7 9 11 |
R13 | 10 7 10 9 8 8 10 |
R14 | 9 9 8 7 7 9 8 |
R15 | 12 14 13 12 10 11 11 |
R16 | 13 11 16 14 14 13 12 |
R17 | 10 8 8 12 10 8 10 |
R18 | 7 8 7 9 8 7 7 |
R19 | 19 20 18 19 16 16 15 |
R20 | 15 17 12 14 16 13 12 |
R21 | 11 9 11 11 12 10 9 |
R22 | 9 10 8 8 10 9 8 |
R23 | 11 8 9 10 8 9 10 |
R24 | 19 18 16 12 14 17 18 |
R26 | 25 21 16 15 22 29 14 |
Table 1.2014.c GPS week : 2014 MJD: 58342.0-58348.0
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 2014 0 | -2 -139 178 1947 -1449 -2902 82.7 1500 1500 | 2312 0
brd 2014 1 | 10 -43 125 -623 194 -858 83.8 1682 1682 | 3292 0
brd 2014 2 | -5 -38 212 936 -6 420 82.5 1856 1856 | 1816 0
brd 2014 3 | 50 11 160 278 2566 3483 82.2 1642 1642 | -267 0
brd 2014 4 | 52 11 117 303 1192 3798 85.0 1709 1709 | 3257 0
brd 2014 5 | -54 104 215 129 -440 5183 85.4 1650 1650 | 4013 0
brd 2014 6 | -11 -51 119 607 762 5566 83.9 1432 1432 | 2422 0
-------------+------------------------------------------------------------+----------------
brd 2014 mean| 5 -20 161 511 402 2098 83.7 1638 1638 | 2406 0
brd 2014 sdev| 37 74 42 793 1276 3238 1.3 139 139 | 1390 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 2.2014.0 GPS week: 2014 Day: 0 MJD: 58342
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 11 12 -28 -28 -.02 40 40 | 4283 -647 3463 10303
cof n/a| 0 0 14 54 16 -69 .09 41 41 | 4302 -686 3466 10301
emx n/a| -1 0 2 36 0 22 -.03 24 24 | 8053 -1881 3341 9813
esx n/a| 0 0 0 -2 21 0 .10 14 10 | 12772 416 3324 12515
gfz n/a| -1 5 -13 19 69 -4 .10 27 22 | 0 -1040 3345 9934
grg n/a| 0 0 6 -70 34 -41 -.28 52 48 | 2706 -691 3543 9587
iac n/a| 0 1 -4 -16 -29 29 -.17 20 20 | 3257 971 4696 10002
mcc n/a| 5 -8 36 -34 -199 -302 -.74 110 110 | --- --- --- ---
Table 2.2014.1 GPS week: 2014 Day: 1 MJD: 58343
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 9 12 -12 -8 .03 41 36 | 4428 925 3692 10970
cof n/a| 0 0 15 9 3 3 .07 42 36 | 4429 917 3693 10972
emx n/a| 0 3 0 14 -38 58 .00 32 32 | -6749 -587 3650 10077
esx n/a| 0 -1 0 26 25 -28 .10 10 9 | 11384 -247 3640 12421
gfz n/a| -1 2 -13 -27 24 34 .12 29 23 | 0 1061 3632 10437
grg n/a| 3 1 6 -91 -1 -91 -.30 52 48 | 2695 929 3616 10056
iac n/a| 0 0 -3 -1 -52 17 -.27 20 20 | 5573 245 4304 13253
mcc n/a| 9 -3 52 104 -117 -134 -.62 135 135 | --- --- --- ---
Table 2.2014.2 GPS week: 2014 Day: 2 MJD: 58344
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 -1 9 -2 22 39 -.03 42 38 | 4923 1087 4225 10643
cof n/a| -3 -1 13 -26 -24 -7 -.04 47 41 | 4897 1133 4232 10647
emx n/a| 0 -1 0 18 -37 53 .06 22 22 | 4705 -576 4252 10132
esx n/a| -1 1 2 0 17 15 .09 14 11 | 1385 311 4243 12460
gfz n/a| -1 1 -7 5 36 13 .15 27 22 | 0 205 4183 10438
grg n/a| 2 -1 1 -41 -9 -186 -.30 46 42 | 1278 926 4190 9738
iac n/a| 3 -1 -3 9 -2 -14 -.26 21 21 | 2745 -804 4960 12407
mcc n/a| -7 -12 33 198 25 -870 -1.05 136 136 | --- --- --- ---
Table 2.2014.3 GPS week: 2014 Day: 3 MJD: 58345
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 -3 10 20 -6 -51 .03 39 37 | 5697 -2937 3483 9596
cof n/a| -1 -3 13 25 -30 -12 .08 39 38 | 5701 -2951 3483 9596
emx n/a| -1 2 -3 -18 -36 66 .03 21 21 | -18113 -2993 3406 9143
esx n/a| 0 0 1 3 12 38 .11 14 13 | -1964 -3858 3394 11302
gfz n/a| 0 0 -6 21 6 43 .11 28 23 | 0 -3319 3397 9379
grg n/a| 1 -1 -2 -52 0 -241 -.25 45 35 | 1318 -3089 3410 8964
iac n/a| 2 0 1 3 16 -87 -.18 19 19 | 3716 -1838 4277 9918
mcc n/a| 1 -16 46 6 216 -836 -.46 159 159 | --- --- --- ---
Table 2.2014.4 GPS week: 2014 Day: 4 MJD: 58346
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 15 9 18 -59 -.05 39 38 | 7193 -4623 3770 9505
cof n/a| -1 0 18 3 18 -23 -.04 42 40 | 7193 -4623 3766 9504
emx n/a| -2 0 0 4 -27 38 .07 25 25 | -9998 -2561 3753 8774
esx n/a| 1 0 -1 7 34 5 .13 13 11 | 13899 -3350 3766 10739
gfz n/a| 0 0 -8 22 47 55 .14 27 26 | 0 -4816 3762 9013
grg n/a| 3 -3 6 -40 -31 -168 -.42 49 47 | 5490 -4638 3901 8702
iac n/a| 1 0 -2 -14 -30 4 -.19 19 19 | 3841 -1901 4074 11109
mcc n/a| 4 -7 47 -178 -161 49 .26 161 161 | --- --- --- ---
Table 2.2014.5 GPS week: 2014 Day: 5 MJD: 58347
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 12 -11 -22 -62 -.03 38 35 | 4464 872 3253 10448
cof n/a| 0 1 16 0 6 -33 .01 41 37 | 4478 826 3252 10450
emx n/a| 0 0 -5 -9 -51 137 .07 28 28 | 6504 62 3274 9793
esx n/a| 0 0 1 25 16 -1 .12 14 10 | 12424 484 3259 12521
gfz n/a| -2 0 -3 53 29 42 .14 27 24 | 0 1694 3256 10221
grg n/a| 2 -3 0 -47 1 -299 -.38 39 35 | 2748 2720 3346 9898
iac n/a| 0 0 -3 -32 3 29 -.18 18 18 | 4837 1030 3705 10051
mcc n/a| 1 -4 37 -79 14 423 -.45 174 174 | --- --- --- ---
Table 2.2014.6 GPS week: 2014 Day: 6 MJD: 58348
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 12 9 9 -54 -.01 37 35 | 4890 -91 3292 9452
cof n/a| -3 0 17 -26 35 -29 .05 38 35 | 4883 -94 3286 9452
emx n/a| -1 4 0 -11 -35 76 -.01 22 22 | -67 -151 3313 8848
esx n/a| 0 0 1 -7 5 20 .13 13 13 | 16873 -1517 3300 11185
gfz n/a| 0 -1 -3 5 45 98 .05 25 25 | 0 -222 3297 9236
grg n/a| 3 -2 0 -58 1 -113 -.26 40 31 | 2648 -275 3278 8699
iac n/a| 1 -3 -4 41 -13 -25 -.15 20 20 | 3819 150 3831 9912
mcc n/a| -4 9 31 83 100 646 -1.54 170 170 | --- --- --- ---
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 3.2014.0 GPS week: 2014 Day: 0 MJD: 58342
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 | 981 85 81 37 12 34 68 31 --- 18 | 89 86 26 30 48 61 41 --- 29
R02 | 1005 34 33 18 7 29 21 15 119 8 | 88 90 60 69 47 82 55 128 63
R03 | 1024 45 46 20 8 33 28 12 107 10 | 111 111 84 76 66 102 72 118 79
R04 | 1667 32 34 15 6 23 21 16 --- 8 | 92 94 69 70 65 87 62 --- 70
R07 | 601 50 47 23 14 25 50 22 86 12 | 97 99 74 70 62 100 59 111 69
R08 | 1797 35 41 17 7 22 35 19 --- 9 | 106 111 88 86 77 104 79 --- 86
R09 | 3047 13 14 9 5 15 26 10 --- 5 | 67 66 64 64 69 67 69 --- 65
R10 | 2157 11 13 22 13 24 29 8 --- 7 | 63 64 44 63 45 81 55 --- 56
R11 | 1535 24 25 19 9 24 17 8 129 7 | 64 63 45 55 44 63 49 109 51
R13 | 2159 17 12 22 13 17 53 17 --- 9 | 69 69 58 77 66 93 61 --- 69
R14 | 852 26 28 16 10 27 46 15 --- 9 | 86 89 75 84 79 84 78 --- 80
R15 | 2838 58 58 22 11 32 25 24 --- 12 | 88 89 56 56 50 65 48 --- 54
R16 | 746 29 41 27 11 23 71 25 --- 12 | 97 106 71 87 72 106 83 --- 82
R17 | 677 29 32 18 10 23 25 33 --- 10 | 23 24 24 26 23 29 20 --- 20
R18 | 815 13 20 18 9 13 30 15 --- 6 | 21 25 24 19 25 27 18 --- 19
R19 | 962 80 82 28 27 34 75 35 --- 19 | 57 61 40 28 26 55 25 --- 29
R20 | 789 21 20 34 21 28 95 19 --- 15 | 39 47 43 30 24 38 24 --- 26
R21 | 1110 37 38 26 13 36 35 19 106 11 | 44 44 40 44 45 47 34 20 40
XR22 | 1105 29 41 17 13 23 --- 9 --- 8 | 24 27 21 24 23 --- 21 --- 20
R23 | 702 22 26 30 26 16 37 11 --- 11 | 13 18 17 28 27 24 14 --- 17
R24 | 949 34 46 44 15 38 118 21 --- 18 | 50 64 53 36 38 68 26 --- 37
XR26 | 1980 34 73 --- --- --- --- 18 --- 24 | 28 73 --- --- --- --- 26 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1500 40 41 24 14 27 52 20 110 |T 64 69 51 53 48 69 46 97 49
WRMS | 1500 40 41 24 10 22 48 20 110 |NE 64 69 51 53 48 69 46 97 49
MEDI | 1005 29 34 22 11 24 35 17 107 |MD 64 66 53 56 47 67 48 111 51
Table 3.2014.1 GPS week: 2014 Day: 1 MJD: 58343
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 | 896 89 80 38 11 37 68 31 --- 17 | 65 60 30 21 43 40 36 --- 22
R02 | 1084 37 46 19 7 25 30 21 117 8 | 75 82 50 59 49 67 54 148 56
R03 | 739 42 41 21 5 23 30 19 88 9 | 97 97 90 86 80 93 80 121 86
R04 | 2257 33 28 18 6 31 25 12 --- 8 | 72 69 51 53 51 69 53 --- 54
R07 | 1356 49 47 26 13 32 76 23 52 13 | 88 87 73 67 63 104 61 139 67
R08 | 1678 38 30 15 9 20 36 17 --- 8 | 87 89 77 86 75 89 75 --- 81
R09 | 2645 11 14 12 7 17 46 16 --- 7 | 54 54 51 47 63 74 57 --- 52
R10 | 993 13 13 21 12 19 25 13 --- 7 | 46 49 37 46 35 45 35 --- 40
R11 | 1796 22 22 15 9 20 17 15 250 6 | 45 45 39 44 39 39 36 161 39
R13 | 1941 12 17 19 7 18 46 11 --- 7 | 45 50 49 53 50 59 41 --- 48
R14 | 916 23 24 14 7 26 56 18 --- 9 | 57 58 55 59 61 71 56 --- 57
R15 | 4025 64 70 17 8 48 61 27 --- 14 | 58 64 40 38 50 67 36 --- 38
R16 | 765 31 38 33 13 26 53 21 --- 11 | 59 65 59 55 44 81 58 --- 53
R17 | 593 36 36 13 6 24 17 15 --- 7 | 13 15 18 20 20 32 11 --- 16
R18 | 866 20 16 18 9 30 36 13 --- 8 | 16 26 24 24 29 38 17 --- 23
R19 | 769 89 97 55 21 47 48 41 --- 20 | 33 44 46 33 24 30 24 --- 24
R20 | 1029 23 22 76 14 25 87 21 --- 17 | 43 68 77 37 23 40 24 --- 35
R21 | 1340 35 40 18 7 28 18 25 67 9 | 26 30 19 23 20 34 29 21 21
R22 | 1861 33 22 22 7 40 47 13 --- 10 | 18 28 16 22 29 34 17 --- 18
R23 | 669 17 18 25 11 14 35 10 --- 7 | 19 26 21 20 26 37 15 --- 19
R24 | 2460 31 33 68 12 25 115 21 --- 18 | 59 67 63 41 47 21 30 --- 38
XR26 | 1909 28 55 --- --- --- --- 15 --- 20 | 30 43 --- --- --- --- 25 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1681 41 42 32 10 29 52 20 135 |T 50 55 46 44 43 55 39 118 41
WRMS | 1681 36 36 32 9 23 48 20 135 |NE 50 55 46 44 43 55 39 118 41
MEDI | 1084 31 30 19 9 25 46 17 88 |MD 46 54 49 44 44 45 36 139 38
Table 3.2014.2 GPS week: 2014 Day: 2 MJD: 58344
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 | 835 91 107 37 30 46 69 33 --- 20 | 73 93 44 49 54 53 29 --- 28
R02 | 842 39 38 15 7 28 46 23 184 10 | 80 78 59 60 51 80 41 71 56
R03 | 761 41 39 17 8 24 41 28 123 10 | 92 89 70 73 60 85 55 70 69
R04 | 1970 29 35 14 11 25 22 13 --- 7 | 126 132 109 107 95 126 101 --- 107
R07 | 1798 46 54 19 11 33 32 18 160 10 | 95 97 70 67 61 77 67 73 68
R08 | 895 34 38 18 12 29 44 18 --- 10 | 84 89 73 76 65 89 59 --- 71
R09 | 2878 10 12 12 14 10 29 25 --- 7 | 49 49 48 50 49 21 55 --- 46
R10 | 735 8 11 18 11 12 36 9 --- 7 | 50 48 36 46 35 56 41 --- 42
R11 | 997 24 29 11 11 21 19 19 104 7 | 41 45 29 35 25 37 17 81 28
R13 | 1440 16 20 23 15 18 47 14 --- 9 | 46 48 37 59 47 73 39 --- 48
R14 | 1152 23 20 17 13 25 18 17 --- 8 | 72 74 72 78 71 48 68 --- 72
R15 | 5904 66 66 18 6 35 23 30 --- 12 | 67 68 37 32 33 38 31 --- 32
R16 | 1042 32 56 42 10 22 85 25 --- 15 | 73 85 41 55 46 91 56 --- 52
R17 | 871 27 30 12 7 18 44 17 --- 8 | 17 20 21 17 33 31 14 --- 17
R18 | 1151 13 21 16 9 19 33 15 --- 7 | 14 18 17 22 20 23 15 --- 18
R19 | 1034 89 90 37 23 47 34 28 --- 18 | 40 43 35 31 28 32 18 --- 24
R20 | 1590 32 31 18 17 16 67 22 --- 12 | 30 39 41 29 20 33 22 --- 21
R21 | 1276 38 38 20 14 26 34 23 81 10 | 60 59 59 58 67 64 54 38 58
R22 | 1812 29 35 15 8 28 16 14 --- 7 | 21 23 18 19 20 24 20 --- 17
R23 | 794 17 15 23 17 22 21 20 --- 9 | 15 16 22 33 32 16 12 --- 19
R24 | 1428 48 66 29 14 34 92 20 --- 16 | 49 70 46 32 21 32 23 --- 28
XR26 | 1545 21 60 --- --- --- --- 12 --- 16 | 21 50 --- --- --- --- 20 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1856 42 47 22 14 27 46 21 136 |T 55 60 46 48 44 53 38 66 42
WRMS | 1856 38 41 22 11 22 42 21 136 |NE 55 60 46 48 44 53 38 66 42
MEDI | 1151 29 35 18 11 25 34 19 123 |MD 49 50 41 49 46 48 31 71 32
Table 3.2014.3 GPS week: 2014 Day: 3 MJD: 58345
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 | 769 70 57 26 20 44 73 27 --- 17 | 59 58 20 44 53 50 32 --- 28
R02 | 941 35 39 14 8 25 39 16 199 9 | 92 99 71 73 63 94 69 52 73
R03 | 894 43 47 18 12 30 55 20 189 11 | 130 136 121 114 112 143 106 66 116
R04 | 1902 31 30 13 11 26 21 22 --- 8 | 99 97 85 94 99 88 74 --- 88
R07 | 2027 49 48 16 7 26 15 13 141 9 | 125 130 112 108 110 107 103 55 109
R08 | 1082 33 39 21 7 34 38 20 --- 10 | 126 132 110 116 98 116 109 --- 112
R09 | 3476 11 15 14 13 13 21 11 --- 6 | 20 18 18 25 27 31 25 --- 20
R10 | 1077 10 16 14 7 20 45 6 --- 7 | 47 51 39 42 25 63 42 --- 40
R11 | 1121 26 24 12 10 19 26 16 145 7 | 46 48 28 32 25 26 22 99 26
R13 | 1470 18 19 20 10 13 47 12 --- 8 | 42 42 29 50 45 72 39 --- 42
R14 | 978 24 25 12 10 31 13 9 --- 7 | 51 50 31 36 22 58 35 --- 32
R15 | 3277 60 64 20 8 35 35 22 --- 12 | 71 75 39 30 34 25 30 --- 31
R16 | 1014 43 33 34 12 31 67 21 --- 14 | 75 62 38 57 38 85 50 --- 50
R17 | 1559 30 34 19 16 33 68 18 --- 12 | 25 28 22 32 26 59 14 --- 23
R18 | 821 17 24 21 18 17 27 15 --- 8 | 17 24 18 24 25 17 15 --- 16
R19 | 664 84 76 21 27 38 68 38 --- 18 | 40 42 43 53 38 38 20 --- 35
R20 | 1752 35 43 39 16 29 57 17 --- 13 | 29 35 46 25 25 25 26 --- 20
R21 | 2087 36 39 17 11 33 43 23 98 10 | 35 38 38 42 47 28 26 18 35
R22 | 1232 34 28 13 10 20 18 20 --- 8 | 20 21 21 27 27 26 18 --- 20
R23 | 1119 14 16 28 16 23 20 20 --- 9 | 16 20 28 26 25 22 13 --- 19
R24 | 1514 27 42 28 20 29 55 18 --- 12 | 34 38 63 28 21 29 19 --- 27
XR26 | 1863 19 25 --- --- --- --- 11 --- 14 | 29 39 --- --- --- --- 20 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1642 39 39 21 14 28 45 19 159 |T 55 58 48 51 46 57 41 58 44
WRMS | 1642 37 38 21 13 23 35 19 159 |NE 55 58 48 51 46 57 41 58 44
MEDI | 1121 31 33 19 11 29 39 18 145 |MD 42 42 38 42 34 50 26 55 31
Table 3.2014.4 GPS week: 2014 Day: 4 MJD: 58346
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 | 980 57 64 40 32 43 72 33 --- 18 | 49 57 36 59 64 36 33 --- 37
R02 | 1557 34 35 15 8 29 30 17 143 8 | 72 73 54 59 59 68 47 41 55
R03 | 884 43 34 16 10 27 47 20 122 10 | 88 83 71 64 64 85 54 69 65
R04 | 2459 34 34 12 6 25 43 12 --- 8 | 115 116 97 93 96 115 95 --- 97
R07 | 2789 45 48 18 7 32 17 14 211 9 | 94 96 80 73 77 76 70 32 74
R08 | 1677 33 39 19 8 22 42 13 --- 8 | 83 88 75 65 53 73 60 --- 65
R09 | 3587 14 14 16 8 17 16 9 --- 5 | 52 51 58 54 53 58 57 --- 54
R10 | 1162 16 17 26 17 24 46 16 --- 10 | 47 46 40 54 37 78 47 --- 48
R11 | 1887 24 29 10 7 24 32 10 208 6 | 44 47 29 35 30 51 27 136 31
XR13 | 2945 19 26 16 11 28 --- 12 --- 8 | 44 47 38 45 43 --- 37 --- 39
XR14 | 805 23 23 11 10 24 --- 12 --- 7 | 63 63 53 61 60 --- 60 --- 58
R15 | 2039 51 41 18 6 32 27 18 --- 10 | 56 50 38 34 41 39 28 --- 33
R16 | 1059 35 63 34 15 29 70 28 --- 13 | 79 104 45 63 63 92 53 --- 58
R17 | 850 32 27 21 10 29 41 16 --- 9 | 19 23 20 24 25 20 12 --- 17
R18 | 859 18 23 15 11 20 47 13 --- 8 | 17 21 22 21 18 26 12 --- 16
R19 | 771 70 73 25 22 21 57 34 --- 15 | 23 29 32 45 40 19 19 --- 28
R20 | 1409 52 58 47 10 28 85 15 --- 15 | 39 48 44 30 28 29 25 --- 25
R21 | 2031 40 39 23 11 36 52 21 83 11 | 65 65 64 64 70 55 54 25 61
R22 | 689 41 42 20 8 29 24 23 --- 10 | 15 17 21 23 27 14 20 --- 18
R23 | 1122 17 17 23 12 14 18 17 --- 7 | 20 22 21 22 24 23 16 --- 17
R24 | 1295 27 39 39 13 21 85 14 --- 13 | 47 60 25 30 24 64 20 --- 25
XR26 | 2121 30 68 --- --- --- --- 16 --- 22 | 20 54 --- --- --- --- 22 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS | 1708 39 42 25 13 27 49 19 161 |T 52 57 45 48 47 53 39 60 42
WRMS | 1708 38 40 25 11 26 47 19 161 |NE 52 57 45 48 47 53 39 60 42
MEDI | 1295 33 35 19 10 27 43 16 143 |MD 47 51 40 54 43 55 33 41 37
Table 3.2014.5 GPS week: 2014 Day: 5 MJD: 58347
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 | 1130 63 62 35 31 26 45 24 --- 15 | 55 61 31 67 46 40 30 --- 39
R02 | 1344 28 31 18 11 23 28 13 99 8 | 80 82 68 72 62 79 66 28 69
R03 | 1454 41 45 19 7 35 46 16 157 10 | 107 108 97 98 91 110 91 71 96
R04 | 1242 31 37 17 6 22 30 16 --- 8 | 119 120 111 114 108 124 103 --- 111
R07 | 2381 48 45 19 8 21 24 17 169 9 | 120 118 101 101 98 111 103 46 103
R08 | 1789 33 30 15 11 27 19 13 --- 8 | 118 116 107 120 110 124 104 --- 113
R09 | 2943 14 14 21 4 13 42 12 --- 7 | 51 52 52 56 60 61 54 --- 53
R10 | 1104 19 21 23 14 15 49 19 --- 9 | 50 47 42 47 42 70 37 --- 44
R11 | 1651 23 24 20 12 30 41 12 275 9 | 48 49 40 39 42 59 41 169 40
XR13 | 3557 14 14 14 12 19 --- 18 --- 7 | 52 52 50 56 54 --- 49 --- 51
XR14 | 863 27 24 11 11 31 --- 14 --- 8 | 61 63 62 65 61 --- 64 --- 63
R15 | 3133 45 41 19 9 46 30 15 --- 11 | 54 59 44 48 66 63 44 --- 48
R16 | 1144 40 30 37 19 20 43 30 --- 13 | 87 85 70 72 66 75 59 --- 67
R17 | 895 33 39 15 8 24 27 14 --- 8 | 24 30 22 26 31 52 19 --- 25
R18 | 612 15 21 6 7 30 28 10 --- 6 | 17 25 19 33 38 18 15 --- 23
R19 | 1370 66 69 18 21 37 71 24 --- 16 | 25 33 29 33 25 40 23 --- 24
R20 | 857 43 56 45 7 19 57 16 --- 13 | 38 53 41 27 41 16 25 --- 27
R21 | 1727 41 43 24 9 30 28 19 108 10 | 36 40 38 45 38 54 37 55 40
R22 | 837 42 44 22 8 27 17 17 --- 9 | 21 23 24 29 27 28 22 --- 24
R23 | 1937 17 20 28 19 14 19 18 --- 9 | 20 24 20 26 18 23 17 --- 17
R24 | 1059 32 50 68 21 24 52 21 --- 16 | 53 79 52 41 32 44 18 --- 31
XR26 |15424 47 83 --- --- --- --- 18 --- 29 | 37 74 --- --- --- --- 24 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1649 38 41 28 14 27 39 18 174 |T 57 63 53 57 55 62 47 73 51
WRMS | 1649 35 37 28 10 24 35 18 174 |NE 57 63 53 57 55 62 47 73 51
MEDI | 1344 33 37 19 11 24 30 16 157 |MD 51 53 44 48 46 59 37 55 40
Table 3.2014.6 GPS week: 2014 Day: 6 MJD: 58348
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 | 1004 66 71 34 22 36 40 25 --- 15 | 64 73 41 43 42 37 30 --- 29
R02 | 1397 25 35 17 6 20 20 13 240 6 | 82 86 57 65 53 73 55 157 61
R03 | 1587 38 43 15 5 30 36 19 106 9 | 105 107 75 78 69 102 66 62 77
R04 | 1127 29 30 18 8 32 32 12 --- 8 | 126 130 109 110 100 125 99 --- 108
R07 | 1733 47 46 13 6 29 24 19 164 9 | 119 120 96 92 87 103 88 110 93
R08 | 1597 31 30 14 7 17 21 21 --- 7 | 110 109 91 93 87 108 88 --- 93
R09 | 2078 14 16 19 10 13 15 22 --- 7 | 53 51 50 49 51 52 54 --- 50
R10 | 1988 11 10 20 11 14 43 16 --- 8 | 64 63 49 69 51 83 54 --- 61
R11 | 988 26 15 25 13 30 39 21 176 10 | 67 59 50 53 36 67 40 275 48
R13 | 2587 15 16 15 12 25 52 13 --- 9 | 59 60 48 61 57 83 51 --- 56
R14 | 1293 31 38 13 10 25 23 7 --- 7 | 77 80 68 74 73 78 73 --- 72
R15 | 2072 49 35 23 14 18 31 17 --- 10 | 72 68 42 38 36 39 33 --- 36
R16 | 1102 29 40 30 17 19 50 22 --- 11 | 93 102 64 85 64 90 67 --- 74
R17 | 648 33 30 16 10 23 38 31 --- 10 | 27 28 21 27 26 36 16 --- 21
R18 | 1149 23 23 11 10 20 24 18 --- 7 | 18 23 23 27 24 33 16 --- 21
R19 | 1468 71 70 25 11 43 39 28 --- 14 | 45 46 30 25 21 34 21 --- 23
R20 | 720 44 45 20 13 30 50 26 --- 12 | 29 36 36 29 26 31 21 --- 22
R21 | 810 32 37 26 8 12 29 22 133 9 | 44 47 44 44 46 56 43 87 42
R22 | 995 36 36 17 5 23 18 18 --- 8 | 24 24 25 28 27 27 25 --- 25
R23 | 1009 24 30 28 24 8 18 10 --- 9 | 16 23 17 28 23 20 18 --- 18
R24 | 742 32 35 39 22 21 100 28 --- 17 | 33 45 47 47 37 39 18 --- 30
XR26 |15766 19 82 --- --- --- --- 10 --- 14 | 24 74 --- --- --- --- 28 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1432 37 38 22 13 25 40 20 170 |T 61 66 51 55 49 62 45 138 49
WRMS | 1432 35 35 22 13 25 31 20 170 |NE 61 66 51 55 49 62 45 138 49
MEDI | 1149 31 35 19 10 23 32 19 164 |MD 59 60 48 49 46 56 40 110 42
More information about the IGSREPORT
mailing list