[IGSREPORT-26115] Wk 2015 IGLOS Final Orbits
acc
acc at igs.org
Sun Sep 9 17:55:34 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2015 (Aug 19, 2018 - Aug 25, 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 2.2015.
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:
igl2015[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2015 in the SP3 format.
igl20157.sum Combination Report for GPS Week 2015.
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 | 5.0 ns
1 | 4.5 ns
2 | 3.9 ns
3 | 2.3 ns
4 | 4.4 ns
5 | 3.4 ns
6 | 2.0 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 1.2015, 1a.2015).
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 2.2015.0-6)
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 3.2015.0-6).
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 2015 summary. (Aug 19, 2018 - Aug 25, 2018)
Table 1.2015.a GPS week : 2015 MJD: 58349.0-58355.0
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 10 -13 -9 -34 .03 36 34 | 3595 -819 3412 9878
| 1 1 0 22 29 40 .04 | 1331 2434
cof n/a| -1 0 13 3 -7 -30 .04 38 36 | 3593 -822 3414 9879
| 1 2 1 26 16 51 .05 | 1333 2438
emx n/a| -1 0 0 21 -23 -6 .01 22 22 | -4636 -865 3426 9458
| 1 1 0 23 31 26 .03 | 7132 1691
esx n/a| 0 0 0 1 14 0 .12 14 12 | 2834 -1492 3419 11721
| 1 0 0 11 12 21 .02 | 10496 3103
gfz n/a| -1 0 -8 15 32 26 .09 27 25 | 0 -744 3412 9597
| 1 1 3 13 29 34 .06 | 0 2394
grg n/a| 2 0 2 -73 4 -79 -.34 44 37 | 3989 -732 3476 9290
| 1 1 5 24 20 45 .08 | 1382 2558
iac n/a| 1 0 -1 -1 1 39 -.13 20 20 | 4693 -205 4369 11284
| 0 0 0 31 31 49 .03 | 1275 1867
mcc n/a| 6 -4 40 6 -59 -4 -.58 117 117 | --- --- --- ---
| 6 9 22 67 84 190 .19 | --- ---
Table 1.2015.b GPS week : 2015 MJD: 58349.0-58355.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 15 15 16 17 18 19 16 |
R02 | 7 7 7 8 9 8 7 |
R03 | 9 8 8 9 9 9 9 |
R04 | 8 8 7 8 8 9 8 |
R05 | --- --- --- 0 0 0 0 |
R07 | 10 9 10 10 10 10 9 |
R08 | 9 10 8 9 8 8 9 |
R09 | 6 5 5 8 11 8 6 |
R10 | 8 7 7 6 7 8 7 |
R11 | 8 8 7 7 9 7 11 |
R13 | 11 9 9 9 10 9 9 |
R14 | 9 9 8 8 8 8 8 |
R15 | 16 14 12 12 13 13 11 |
R16 | 16 14 14 14 15 14 13 |
R17 | 10 9 9 8 10 10 9 |
R18 | 7 7 7 7 7 8 7 |
R19 | 17 18 20 18 17 14 15 |
R20 | 13 12 16 13 14 11 13 |
R21 | 12 12 11 9 11 11 9 |
R22 | 9 11 11 9 10 12 10 |
R23 | 10 9 7 6 7 8 9 |
R24 | 21 18 17 14 16 15 17 |
R26 | 19 12 21 24 13 14 15 |
Table 1.2015.c GPS week : 2015 MJD: 58349.0-58355.0
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 2015 0 | 61 -23 157 504 -605 684 82.4 1314 1314 | 5022 0
brd 2015 1 | -30 18 255 -2254 -38 4182 84.5 1256 1256 | 4453 0
brd 2015 2 | 59 -6 156 -364 -1191 3648 83.0 1257 1257 | 3886 0
brd 2015 3 | -28 13 203 -39 -1779 5595 81.7 1371 1371 | 2335 0
brd 2015 4 | 0 -12 187 1964 -312 1919 81.2 1322 1322 | 4354 0
brd 2015 5 | 39 13 263 1146 -180 -1277 83.1 1185 1185 | 3420 0
brd 2015 6 | -6 65 200 -588 -28 -180 83.5 1405 1405 | 2008 0
-------------+------------------------------------------------------------+----------------
brd 2015 mean| 13 9 203 52 -590 2081 82.8 1301 1301 | 3639 0
brd 2015 sdev| 39 29 42 1351 663 2502 1.1 74 74 | 1122 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 2.2015.0 GPS week: 2015 Day: 0 MJD: 58349
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 10 -2 12 -54 -.03 35 35 | 5983 -4025 2995 10659
cof n/a| -1 -5 12 14 20 -62 .03 41 39 | 5991 -4049 2994 10660
emx n/a| -1 2 0 2 -53 0 -.01 23 23 | -10413 -3201 3023 10227
esx n/a| 1 0 0 -15 20 -12 .09 14 14 | 14729 -4058 3006 12583
gfz n/a| -2 3 -6 15 22 36 .11 29 25 | 0 -3855 3000 10355
grg n/a| 3 -1 0 -101 -3 -49 -.48 44 38 | 7014 -3647 3002 10218
iac n/a| 0 0 -3 49 11 47 -.13 23 23 | 4233 398 3941 11449
mcc n/a| 0 -20 46 -50 -155 -125 -.61 132 132 | --- --- --- ---
Table 2.2015.1 GPS week: 2015 Day: 1 MJD: 58350
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 9 -52 -25 -6 .01 38 35 | 2112 1458 3619 9868
cof n/a| -2 0 13 -36 -20 32 .04 40 37 | 2129 1419 3627 9869
emx n/a| -1 0 -1 63 -54 48 .02 26 26 | -3896 631 3630 9559
esx n/a| 0 0 0 -8 13 -24 .11 11 11 | 6925 2624 3634 11854
gfz n/a| -2 0 -10 12 18 49 .12 27 24 | 0 1143 3627 9667
grg n/a| 3 0 1 -66 41 -133 -.33 46 36 | 3619 1683 3620 9107
iac n/a| 1 0 0 -3 38 31 -.13 20 20 | 6385 188 4516 10784
mcc n/a| 16 -1 50 13 -108 103 -.60 122 122 | --- --- --- ---
Table 2.2015.2 GPS week: 2015 Day: 2 MJD: 58351
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 0 -19 -50 .05 38 35 | 3045 687 3375 10620
cof n/a| 0 3 17 24 5 -78 .04 37 36 | 3024 720 3378 10625
emx n/a| 0 0 -1 32 -4 -21 -.02 26 26 | -8901 -229 3414 10246
esx n/a| -1 0 0 7 14 4 .10 11 9 | -9337 -344 3416 12409
gfz n/a| 0 0 -14 37 27 -4 .05 29 25 | 0 882 3411 10431
grg n/a| 2 0 10 -80 -1 -127 -.33 48 37 | 3132 1107 3392 9730
iac n/a| 2 0 -3 -20 -27 80 -.19 19 19 | 4998 -35 4107 10722
mcc n/a| 12 3 55 69 39 155 -.74 125 125 | --- --- --- ---
Table 2.2015.3 GPS week: 2015 Day: 3 MJD: 58352
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 10 14 26 -93 .03 38 36 | 2390 -1290 3462 9099
cof n/a| 0 0 11 -2 -13 -96 -.01 41 38 | 2380 -1281 3464 9099
emx n/a| -2 0 1 33 -15 -34 -.02 18 18 | -10964 -1348 3480 8852
esx n/a| 0 -1 0 0 25 -26 .14 14 12 | -1219 -2958 3465 11035
gfz n/a| -2 0 -9 23 85 -32 .12 29 31 | 0 -2199 3452 8841
grg n/a| 1 0 1 -98 -8 -48 -.23 41 37 | 3715 -2887 3732 8136
iac n/a| 2 0 -2 -35 -33 122 -.10 19 19 | 5873 -1739 4130 9106
mcc n/a| 0 -6 64 -62 -64 113 -.31 131 131 | --- --- --- ---
Table 2.2015.4 GPS week: 2015 Day: 4 MJD: 58353
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 -24 21 -56 .10 38 36 | 3692 182 3182 9795
cof n/a| -5 0 15 41 -5 -37 .11 41 38 | 3697 177 3181 9791
emx n/a| -2 0 0 7 33 -9 .06 22 22 | 8783 -258 3212 9541
esx n/a| -1 -1 0 19 0 25 .11 17 14 | 17648 150 3192 12012
gfz n/a| 0 0 -9 19 58 20 .13 26 22 | 0 1164 3194 9582
grg n/a| 3 -2 6 -32 15 -118 -.37 44 39 | 3798 979 3186 9065
iac n/a| 2 0 -1 -18 -31 18 -.09 16 16 | 3848 -1272 4088 14506
mcc n/a| -1 -12 50 116 39 -128 -.80 114 114 | --- --- --- ---
Table 2.2015.5 GPS week: 2015 Day: 5 MJD: 58354
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 10 -3 -48 0 -.01 34 32 | 4557 1454 3746 9913
cof n/a| 0 0 13 -16 -28 6 -.02 36 33 | 4552 1460 3750 9917
emx n/a| -1 1 -1 -3 -43 -15 .05 19 19 | 376 1230 3739 9335
esx n/a| 1 0 -2 -2 -2 19 .16 16 14 | -6962 532 3747 11201
gfz n/a| 0 -2 -5 3 19 57 .12 27 24 | 0 1317 3732 9705
grg n/a| 0 -1 4 -81 7 -62 -.28 44 39 | 2847 1426 3721 9468
iac n/a| 2 0 -1 35 29 -20 -.12 19 19 | 4928 3327 5635 10572
mcc n/a| 9 1 12 12 -14 -327 -.67 101 101 | --- --- --- ---
Table 2.2015.6 GPS week: 2015 Day: 6 MJD: 58355
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 10 -25 -34 22 .06 31 28 | 3389 -4201 3510 9194
cof n/a| -2 0 13 -2 -11 23 .07 32 29 | 3382 -4206 3510 9195
emx n/a| -2 0 -1 15 -25 -10 .01 22 22 | -7439 -2884 3487 8447
esx n/a| 1 0 0 9 32 17 .13 13 12 | -1945 -6391 3473 10959
gfz n/a| 0 1 -3 -4 -2 60 -.03 24 26 | 0 -3660 3469 8604
grg n/a| 1 0 -6 -53 -22 -18 -.34 39 33 | 3801 -3787 3682 9306
iac n/a| 1 0 -1 -16 20 -5 -.12 22 22 | 2587 -2306 4169 11850
mcc n/a| 5 3 6 -49 -154 175 -.31 95 95 | --- --- --- ---
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 3.2015.0 GPS week: 2015 Day: 0 MJD: 58349
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 | 1518 63 74 29 12 30 48 27 --- 14 | 77 86 58 53 54 47 51 --- 48
R02 | 1090 26 23 15 5 25 15 9 113 6 | 90 92 76 77 77 82 73 123 77
R03 | 556 38 36 16 10 30 21 18 91 9 | 113 109 88 89 77 99 84 134 88
R04 | 845 27 27 17 10 23 22 15 --- 8 | 106 106 88 89 82 95 87 --- 89
R07 | 1037 47 48 18 12 25 21 20 203 10 | 99 99 84 72 68 91 75 73 77
R08 | 905 32 35 15 11 19 31 17 --- 8 | 102 107 89 95 88 103 87 --- 92
R09 | 1901 11 16 8 9 16 13 19 --- 5 | 117 119 118 113 118 106 119 --- 115
R10 | 2689 13 15 17 14 23 26 20 --- 8 | 59 64 48 66 49 69 53 --- 56
R11 | 968 22 28 19 6 30 22 20 70 8 | 64 68 54 50 47 60 38 79 49
R13 | 1887 14 11 23 16 31 50 12 --- 10 | 59 57 50 59 51 89 51 --- 55
R14 | 1684 31 27 14 11 33 23 13 --- 8 | 67 67 59 63 58 69 50 --- 58
R15 | 1809 56 55 36 20 52 39 27 --- 16 | 81 80 52 43 48 45 32 --- 42
R16 | 819 41 59 43 18 20 62 30 --- 15 | 71 81 57 67 51 100 56 --- 62
R17 | 573 29 32 20 11 24 39 22 --- 10 | 26 29 28 29 26 35 18 --- 25
R18 | 1254 24 25 11 12 15 17 16 --- 6 | 26 28 25 33 26 30 29 --- 27
R19 | 1662 69 79 19 21 38 61 37 --- 16 | 40 44 36 46 45 29 22 --- 35
R20 | 740 16 23 19 23 38 54 30 --- 13 | 35 39 35 33 41 32 33 --- 30
R21 | 953 34 35 20 16 29 47 29 143 12 | 28 34 29 38 34 32 27 62 30
R22 | 700 31 35 17 9 22 19 24 --- 8 | 29 29 27 28 37 35 29 --- 27
R23 | 640 22 17 26 22 8 17 23 --- 9 | 31 29 28 37 36 30 25 --- 30
R24 | 817 24 59 46 16 41 126 28 --- 21 | 37 59 51 27 28 72 22 --- 28
XR26 | 2053 23 64 --- --- --- --- 15 --- 18 | 52 64 --- --- --- --- 38 --- 42
------+---------------------------------------------------+-----------------------------------------------
RMS | 1313 35 41 23 14 29 44 23 132 |T 64 67 56 57 54 64 49 94 53
WRMS | 1313 35 39 23 14 25 38 23 132 |NE 64 67 56 57 54 64 49 94 53
MEDI | 968 27 32 19 12 25 26 20 113 |MD 59 64 52 53 49 69 38 79 48
Table 3.2015.1 GPS week: 2015 Day: 1 MJD: 58350
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 | 1034 60 72 32 10 28 64 29 --- 14 | 64 75 57 55 61 49 59 --- 52
R02 | 1217 27 26 14 5 17 20 16 96 6 | 77 78 66 63 61 72 61 107 64
R03 | 1237 39 36 16 5 27 14 14 136 8 | 94 94 75 76 62 78 69 125 74
R04 | 983 29 31 18 7 22 25 13 --- 7 | 84 85 75 73 66 72 66 --- 71
R07 | 1224 42 42 17 6 21 30 14 138 8 | 72 72 53 55 55 65 53 47 55
R08 | 1134 39 38 16 12 31 38 21 --- 10 | 84 87 72 79 81 78 63 --- 73
R09 | 1672 10 13 12 5 11 17 13 --- 4 | 103 103 104 100 102 96 107 --- 102
R10 | 2440 10 13 22 12 18 22 10 --- 6 | 50 50 53 56 43 42 52 --- 51
R11 | 1068 22 22 19 8 33 30 13 107 8 | 49 46 47 47 54 42 39 70 44
R13 | 1890 15 21 25 9 16 39 19 --- 8 | 46 48 32 41 39 54 33 --- 37
R14 | 1184 23 21 18 9 30 42 21 --- 9 | 49 49 46 46 46 63 47 --- 45
R15 | 1527 56 55 33 12 40 25 33 --- 13 | 54 51 39 43 42 45 37 --- 38
R16 | 943 41 43 43 18 20 69 18 --- 14 | 42 45 35 50 36 63 46 --- 44
R17 | 692 32 34 18 9 25 26 20 --- 8 | 14 16 19 20 17 17 12 --- 14
R18 | 1159 16 17 18 11 20 30 12 --- 7 | 15 17 20 25 21 26 18 --- 17
R19 | 1141 81 71 33 20 37 76 30 --- 18 | 27 33 31 33 25 36 19 --- 24
R20 | 736 19 36 15 16 21 72 21 --- 11 | 34 54 24 28 22 18 25 --- 23
R21 | 1007 40 40 29 10 42 33 22 128 11 | 18 21 23 24 29 15 24 30 20
R22 | 1102 31 29 19 11 27 57 24 --- 11 | 17 23 20 20 19 27 18 --- 15
R23 | 802 23 25 30 15 15 21 17 --- 9 | 24 27 23 25 35 31 25 --- 24
R24 | 806 49 74 54 16 31 100 20 --- 18 | 48 66 55 39 43 24 35 --- 36
XR26 |16209 15 62 --- --- --- --- 8 --- 11 | 16 61 --- --- --- --- 27 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1256 38 40 26 11 27 46 20 122 |T 49 54 46 47 45 48 42 75 42
WRMS | 1256 35 37 26 11 24 36 20 122 |NE 49 54 46 47 45 48 42 75 42
MEDI | 1134 29 34 19 10 25 30 18 128 |MD 48 50 46 46 43 45 37 70 38
Table 3.2015.2 GPS week: 2015 Day: 2 MJD: 58351
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 | 828 76 52 32 11 40 55 31 --- 15 | 65 51 49 51 61 49 60 --- 46
R02 | 1451 29 21 13 8 20 28 16 115 7 | 60 56 51 46 41 64 43 105 47
R03 | 2491 39 36 14 7 22 23 15 142 8 | 75 72 50 57 47 65 47 127 53
R04 | 1911 29 34 15 5 27 19 9 --- 7 | 65 69 50 54 41 59 47 --- 51
R07 | 1103 43 38 22 7 29 27 17 79 9 | 68 65 49 47 42 58 35 54 45
R08 | 1351 35 41 18 5 22 25 12 --- 7 | 63 68 45 45 41 55 40 --- 44
R09 | 937 14 18 14 5 13 23 11 --- 5 | 120 118 121 122 125 117 125 --- 122
R10 | 1655 14 16 18 12 20 13 13 --- 6 | 46 46 48 53 42 56 52 --- 49
R11 | 723 17 14 11 7 19 37 8 135 6 | 54 60 44 45 46 75 46 106 47
R13 | 982 12 20 17 9 20 57 18 --- 9 | 56 61 48 56 45 88 46 --- 53
R14 | 1266 23 26 16 13 17 19 21 --- 7 | 57 59 53 44 44 55 48 --- 47
R15 | 1335 56 57 19 6 28 44 24 --- 11 | 69 70 48 42 37 68 32 --- 42
R16 | 1366 44 49 26 16 40 74 22 --- 14 | 59 66 60 61 43 83 51 --- 55
R17 | 721 34 36 12 9 29 22 24 --- 9 | 21 23 29 28 29 27 15 --- 23
R18 | 1209 15 19 20 9 30 18 13 --- 7 | 21 26 26 27 22 20 21 --- 21
R19 | 1051 70 82 41 24 50 96 33 --- 20 | 29 41 30 36 36 42 17 --- 24
R20 | 714 29 25 63 16 22 68 18 --- 15 | 39 35 52 38 25 28 19 --- 28
R21 | 743 38 40 22 12 32 36 26 143 10 | 23 23 21 32 32 39 24 83 26
R22 | 1370 36 36 29 6 39 22 22 --- 10 | 26 32 21 27 37 38 27 --- 26
R23 | 767 20 23 12 12 24 26 11 --- 7 | 26 31 28 25 29 29 20 --- 23
R24 | 689 39 32 43 12 28 115 18 --- 17 | 37 48 44 34 30 26 31 --- 30
XR26 |12841 30 42 --- --- --- --- 15 --- 21 | 21 27 --- --- --- --- 29 --- 22
------+---------------------------------------------------+-----------------------------------------------
RMS | 1256 38 37 26 11 29 48 19 125 |T 50 52 46 46 42 54 39 95 42
WRMS | 1256 35 36 26 9 25 37 19 125 |NE 50 52 46 46 42 54 39 95 42
MEDI | 1103 30 34 18 9 27 27 17 135 |MD 54 51 48 45 41 55 35 105 44
Table 3.2015.3 GPS week: 2015 Day: 3 MJD: 58352
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 | 732 87 90 25 22 34 52 30 --- 17 | 71 74 36 52 60 30 50 --- 39
R02 | 1561 31 45 13 10 27 30 11 81 8 | 74 85 49 51 51 72 44 74 51
R03 | 2934 39 43 17 13 24 25 18 109 9 | 81 86 58 62 51 63 46 101 56
R04 | 1943 30 26 16 10 22 25 11 --- 7 | 70 64 46 59 47 59 45 --- 51
XR05 | ---- 8 8209 --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07 | 704 41 53 20 10 24 25 26 109 10 | 74 86 59 57 48 62 39 44 53
R08 | 905 31 30 19 7 23 31 19 --- 8 | 73 72 55 54 49 65 38 --- 52
R09 | 917 23 20 20 16 18 12 15 --- 8 | 81 78 73 74 76 76 64 --- 70
R10 | 1268 10 15 10 11 25 26 8 --- 6 | 49 46 45 53 36 62 45 --- 47
R11 | 536 22 18 11 7 24 26 13 186 6 | 51 49 47 47 38 49 40 92 43
R13 | 786 16 15 13 14 21 49 12 --- 8 | 54 54 54 52 52 78 54 --- 53
R14 | 1630 27 20 13 12 29 19 14 --- 7 | 54 51 45 47 41 45 41 --- 42
R15 | 2184 60 57 26 16 33 23 17 --- 12 | 77 73 57 45 47 48 38 --- 46
R16 | 1448 25 52 25 17 21 74 25 --- 13 | 64 57 52 54 58 80 53 --- 53
R17 | 734 27 28 13 9 22 26 19 --- 7 | 33 36 40 32 40 44 28 --- 33
R18 | 872 17 20 18 15 20 16 13 --- 7 | 34 36 38 31 34 38 28 --- 31
R19 | 1578 69 70 30 32 52 68 23 --- 18 | 41 40 35 47 42 37 31 --- 35
R20 | 803 35 35 20 15 30 71 23 --- 13 | 48 61 52 47 51 44 36 --- 40
R21 | 633 32 30 16 8 27 21 20 141 8 | 33 33 36 34 33 38 31 46 31
R22 | 1358 30 33 11 8 43 24 21 --- 9 | 35 36 39 38 40 35 28 --- 34
R23 | 1161 17 21 8 12 19 19 12 --- 6 | 43 45 35 45 45 36 37 --- 38
R24 | 1366 40 43 15 11 41 78 27 --- 14 | 60 66 54 51 53 43 40 --- 44
XR26 | 2250 38 53 --- --- --- --- 13 --- 23 | 51 74 --- --- --- --- 36 --- 39
------+---------------------------------------------------+-----------------------------------------------
RMS | 1370 38 41 18 14 29 41 19 130 |T 56 59 47 49 47 52 40 71 44
WRMS | 1370 36 38 18 12 31 37 19 130 |NE 56 59 47 49 47 52 40 71 44
MEDI | 1161 30 33 16 12 24 26 17 109 |MD 54 57 47 51 47 48 39 74 43
Table 3.2015.4 GPS week: 2015 Day: 4 MJD: 58353
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 | 598 82 90 31 26 44 55 24 --- 18 | 62 74 30 48 57 24 36 --- 30
R02 | 1000 38 36 14 9 23 28 12 67 8 | 66 64 36 44 34 57 33 85 40
R03 | 2043 40 43 13 11 21 36 14 86 9 | 77 84 53 48 44 76 54 89 53
R04 | 1598 28 33 14 11 23 22 12 --- 7 | 65 73 48 53 37 54 43 --- 47
XR05 | ---- 7 13 --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07 | 879 44 42 19 11 26 19 17 123 9 | 62 64 43 38 32 49 34 37 38
R08 | 682 31 40 19 10 21 25 12 --- 8 | 55 68 43 45 41 56 38 --- 42
R09 | 1216 32 43 28 25 25 23 14 --- 10 | 140 143 136 131 138 129 142 --- 135
R10 | 2196 14 13 16 11 14 28 11 --- 6 | 36 38 38 42 31 55 41 --- 38
R11 | 668 24 19 16 9 25 34 17 147 8 | 49 48 45 33 37 51 28 59 35
R13 | 1050 16 24 17 22 20 45 14 --- 9 | 35 38 36 49 38 57 32 --- 37
R14 | 1259 25 24 17 11 30 25 8 --- 8 | 41 43 41 42 40 31 40 --- 37
R15 | 1858 56 60 32 13 33 31 15 --- 12 | 54 59 36 26 21 27 24 --- 24
R16 | 973 33 37 37 15 19 79 14 --- 14 | 61 61 41 50 37 81 49 --- 46
R17 | 790 28 30 17 11 30 42 14 --- 9 | 16 15 16 16 19 34 14 --- 12
R18 | 680 21 25 16 16 16 19 8 --- 7 | 15 22 19 20 31 21 14 --- 15
R19 | 1474 70 62 28 27 34 40 34 --- 16 | 20 28 35 45 33 31 22 --- 27
R20 | 1316 23 52 27 17 30 80 10 --- 13 | 29 49 37 26 22 35 28 --- 20
R21 | 710 36 40 25 18 29 26 17 127 10 | 19 22 15 31 25 19 24 22 21
R22 | 1079 36 34 11 19 28 38 13 --- 10 | 15 18 19 29 25 16 19 --- 18
R23 | 1670 16 18 15 23 10 13 10 --- 7 | 16 19 18 25 23 25 21 --- 19
R24 | 2011 19 15 25 21 32 94 26 --- 16 | 29 28 56 26 29 31 29 --- 29
XR26 | 1778 22 79 --- --- --- --- 7 --- 13 | 22 93 --- --- --- --- 23 --- 20
------+---------------------------------------------------+-----------------------------------------------
RMS | 1321 38 41 22 17 26 44 16 114 |T 44 52 40 41 37 45 35 58 35
WRMS | 1321 36 38 22 14 22 39 16 114 |NE 44 52 40 41 37 45 35 58 35
MEDI | 1079 28 36 17 15 25 31 14 123 |MD 36 48 37 42 33 35 29 59 30
Table 3.2015.5 GPS week: 2015 Day: 5 MJD: 58354
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 | 589 74 75 34 37 39 43 27 --- 18 | 85 93 68 97 90 63 79 --- 76
R02 | 582 33 40 13 11 20 22 15 62 8 | 71 76 60 64 58 69 54 82 60
R03 | 2089 37 34 16 10 28 32 12 59 9 | 80 78 66 69 59 78 63 47 66
R04 | 1475 29 28 14 13 25 34 10 --- 8 | 85 87 64 75 65 77 68 --- 70
XR05 | ---- 7 22 --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07 | 904 40 39 19 11 32 17 13 135 9 | 76 75 68 60 58 64 59 62 62
R08 | 963 33 33 17 12 25 21 11 --- 8 | 74 77 61 63 57 68 57 --- 60
R09 | 781 22 20 21 17 12 10 16 --- 8 | 80 84 75 89 83 79 81 --- 80
R10 | 1411 14 17 21 20 11 27 12 --- 8 | 61 61 56 71 62 73 58 --- 62
R11 | 909 19 24 10 11 27 18 13 97 6 | 62 68 63 56 50 57 57 58 56
R13 | 1322 10 11 19 15 17 49 11 --- 8 | 66 68 61 70 70 87 66 --- 67
R14 | 1122 24 26 11 10 27 34 15 --- 8 | 59 57 51 54 55 73 51 --- 53
R15 | 1580 55 48 25 22 30 28 18 --- 12 | 66 68 55 56 59 66 54 --- 56
R16 | 818 32 49 23 14 24 85 26 --- 14 | 77 91 62 73 76 94 67 --- 70
R17 | 814 30 30 21 7 39 20 26 --- 10 | 22 19 27 21 26 28 22 --- 21
R18 | 630 19 26 11 16 26 34 15 --- 8 | 25 27 29 30 29 32 24 --- 26
R19 | 822 50 55 28 13 27 21 38 --- 13 | 35 42 30 32 34 42 20 --- 23
R20 | 1539 31 36 14 15 29 62 14 --- 11 | 48 40 24 41 44 35 32 --- 33
R21 | 707 26 28 16 11 32 52 21 127 10 | 24 23 26 27 27 38 24 30 24
R22 | 877 29 30 13 15 34 58 21 --- 11 | 32 32 28 37 33 47 26 --- 30
R23 | 1357 18 19 17 20 9 29 15 --- 8 | 31 37 31 35 33 36 24 --- 29
R24 | 1918 21 24 22 17 21 96 24 --- 14 | 51 58 42 35 35 54 34 --- 36
XR26 | 1679 19 57 --- --- --- --- 9 --- 13 | 33 61 --- --- --- --- 26 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1185 34 36 19 16 27 44 19 101 |T 56 60 49 55 52 60 47 55 49
WRMS | 1185 32 33 19 14 24 39 19 101 |NE 56 60 49 55 52 60 47 55 49
MEDI | 909 29 30 17 14 27 32 15 97 |MD 61 61 56 56 57 64 54 58 56
Table 3.2015.6 GPS week: 2015 Day: 6 MJD: 58355
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 | 646 67 61 34 28 24 38 30 --- 16 | 103 111 88 98 96 80 86 --- 87
R02 | 910 26 30 14 13 17 19 12 60 7 | 90 93 70 76 73 81 77 110 75
R03 | 1900 36 39 17 10 26 16 16 85 8 | 101 103 78 82 71 94 81 79 81
R04 | 1143 30 36 17 9 24 21 13 --- 8 | 102 103 88 89 76 96 80 --- 86
XR05 | ---- 7 27 --- --- --- --- --- --- 0 | --- --- --- --- --- --- --- --- 0
R07 | 865 39 41 14 6 28 19 16 147 8 | 101 102 77 80 72 85 68 74 77
R08 | 1204 30 30 17 8 30 29 11 --- 8 | 93 92 72 74 68 91 69 --- 74
R09 | 786 12 14 14 11 10 13 14 --- 5 | 98 97 96 91 95 100 102 --- 95
R10 | 951 15 19 10 13 12 29 16 --- 6 | 83 81 82 89 75 94 75 --- 82
R11 | 733 19 20 18 13 26 47 26 53 10 | 81 83 72 76 64 91 61 53 71
R13 | 2535 7 12 13 9 22 50 15 --- 8 | 80 78 75 86 79 106 73 --- 80
R14 | 1081 30 28 15 9 26 11 20 --- 8 | 78 80 70 72 69 72 63 --- 68
R15 | 3582 39 38 23 8 20 21 40 --- 11 | 89 88 71 74 82 79 59 --- 71
R16 | 615 25 35 30 11 24 64 24 --- 12 | 99 103 79 92 77 115 81 --- 87
R17 | 839 28 30 10 9 28 21 30 --- 9 | 21 23 21 25 28 23 19 --- 19
R18 | 1306 16 19 13 11 22 21 16 --- 7 | 23 22 23 22 21 24 18 --- 19
R19 | 1398 50 53 30 16 39 53 29 --- 14 | 30 34 26 33 27 36 23 --- 25
R20 | 668 13 21 26 16 12 71 28 --- 12 | 35 40 30 39 46 24 23 --- 30
R21 | 835 28 28 19 5 28 17 23 99 8 | 19 18 15 25 23 22 25 42 20
R22 | 719 29 33 21 10 34 36 15 --- 10 | 26 28 26 25 26 30 23 --- 23
R23 | 826 24 26 22 20 12 16 11 --- 8 | 29 32 23 23 24 28 21 --- 21
R24 | 1875 25 21 46 23 15 87 24 --- 16 | 41 54 60 49 41 43 24 --- 40
XR26 | 1982 17 41 --- --- --- --- 12 --- 14 | 34 45 --- --- --- --- 25 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1405 31 32 22 13 24 39 22 95 |T 66 68 59 62 58 67 53 71 57
WRMS | 1405 28 29 22 12 26 33 22 95 |NE 66 68 59 62 58 67 53 71 57
MEDI | 910 26 30 17 11 24 21 16 85 |MD 80 80 71 74 69 80 61 74 71
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