[IGSREPORT-25349] Wk 1952 IGLOS Final Orbits
acc
acc at igs.org
Sun Jun 25 20:11:57 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1952 (Jun 04, 2017 - Jun 10, 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 2.1952.
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:
igl1952[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1952 in the SP3 format.
igl19527.sum Combination Report for GPS Week 1952.
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 | -6.5 ns
1 | -7.5 ns
2 | -3.1 ns
3 | -7.5 ns
4 | -8.1 ns
5 | -3.4 ns
6 | -1.4 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 1.1952, 1a.1952).
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 2.1952.0-6)
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 3.1952.0-6).
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 1952 summary. (Jun 04, 2017 - Jun 10, 2017)
Table 1.1952.a GPS week : 1952 MJD: 57908.0-57914.0
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 0 4 -10 -4 33 .13 22 19 | -15198 -593 3500 11887
| 0 1 1 22 14 26 .03 | 1989 1233
cof n/a| 0 0 3 -17 3 16 .13 25 21 | -15200 -592 3500 11888
| 1 0 2 12 21 36 .05 | 1996 1247
emx n/a| -1 0 4 -17 -17 -17 .00 22 21 | -5024 -374 3500 11014
| 1 1 1 14 27 37 .05 | 12087 790
esx n/a| 0 0 -3 0 14 7 .21 20 17 | -16498 -271 3500 13788
| 1 1 2 13 9 22 .04 | 8042 1752
gfz n/a| 0 1 0 -10 38 5 -.02 21 18 | 0 -760 3511 11484
| 0 1 1 17 16 25 .06 | 0 1296
grg n/a| 0 0 -4 -71 3 -74 -.37 29 25 | -5093 -613 3526 11220
| 1 1 6 24 24 52 .06 | 3056 1383
iac n/a| 0 0 -1 69 -31 17 -.07 19 18 | -4283 -368 3504 10891
| 1 0 1 15 30 45 .03 | 2435 521
mcc n/a| -1 1 0 137 -100 -307 .07 189 189 | --- --- --- ---
| 9 5 14 79 52 143 .42 | --- ---
Table 1.1952.b GPS week : 1952 MJD: 57908.0-57914.0
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 6 7 13 14 |
R02 | 9 6 7 7 8 6 6 |
R03 | 6 7 6 8 8 6 7 |
R04 | 8 7 6 7 6 6 7 |
R05 | 16 14 17 16 14 17 18 |
R06 | 12 11 9 10 13 10 10 |
R07 | 7 5 6 5 6 9 10 |
R08 | 10 11 9 7 9 7 7 |
R09 | 8 7 8 8 7 8 9 |
R10 | 8 8 6 8 10 8 8 |
R11 | 10 9 9 10 8 7 7 |
R13 | 8 8 9 9 10 7 8 |
R14 | 17 16 16 16 16 16 18 |
R15 | 11 9 8 9 8 9 7 |
R16 | 11 10 13 12 15 18 15 |
R17 | 7 7 9 7 8 10 8 |
R18 | 6 8 6 8 6 7 7 |
R19 | 11 10 13 11 12 9 10 |
R20 | 11 13 12 12 11 10 11 |
R21 | 8 7 7 7 8 7 8 |
R22 | 7 7 8 6 7 9 8 |
R23 | 8 10 9 9 10 11 9 |
R24 | 14 15 12 12 10 13 14 |
R26 | 15 14 21 19 21 22 23 |
Table 1.1952.c GPS week : 1952 MJD: 57908.0-57914.0
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 1952 0 | -87 -38 78 -1091 -350 1016 87.8 1439 1439 | -6457 0
brd 1952 1 | -13 -26 225 672 -1006 1125 87.0 1232 1232 | -7466 0
brd 1952 2 | -47 6 140 1318 1100 -1263 86.4 1278 1278 | -3087 0
brd 1952 3 | -13 -65 187 267 -393 -2043 86.4 1415 1415 | -7518 0
brd 1952 4 | 68 -38 237 156 -1352 1149 84.0 1179 1179 | -8139 0
brd 1952 5 | 0 -96 204 588 -570 3373 83.8 1316 1316 | -3434 0
brd 1952 6 | 55 35 152 872 497 3273 85.3 1087 1087 | -1387 0
-------------+------------------------------------------------------------+----------------
brd 1952 mean| -5 -31 175 397 -296 947 85.8 1278 1278 | -5355 0
brd 1952 sdev| 54 43 55 761 845 2049 1.5 125 125 | 2667 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 2.1952.0 GPS week: 1952 Day: 0 MJD: 57908
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 5 21 5 27 .16 23 22 | -17202 329 3556 12144
cof n/a| 0 -1 7 -6 -3 -4 .16 23 22 | -17226 362 3555 12145
emx n/a| -1 0 4 -6 -37 -50 .09 25 25 | 1137 414 3537 11431
esx n/a| -2 -3 -3 -2 11 -18 .19 22 18 | -23867 1292 3562 14180
gfz n/a| 0 0 0 -34 44 14 -.01 25 16 | 0 119 3563 11653
grg n/a| 1 0 -2 -92 8 -108 -.43 30 25 | -6673 167 3622 11418
iac n/a| 1 0 -2 53 -12 63 -.03 15 13 | -5666 -576 3562 11093
mcc n/a| 9 8 -12 94 -17 -40 -.44 158 158 | --- --- --- ---
Table 2.1952.1 GPS week: 1952 Day: 1 MJD: 57909
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 4 9 11 23 .16 22 20 | -16915 -108 3648 11638
cof n/a| -1 1 5 -19 1 15 .14 23 22 | -16928 -83 3648 11643
emx n/a| 0 0 2 -18 -15 11 .03 19 19 | -6179 -112 3659 10864
esx n/a| 0 0 -1 -11 7 8 .22 21 18 | -23058 1201 3657 12174
gfz n/a| 0 2 0 -24 47 18 .11 19 17 | 0 -45 3671 11348
grg n/a| 0 0 -2 -101 33 -141 -.44 27 23 | -7616 -281 3693 10823
iac n/a| 1 0 0 91 -64 22 -.10 17 17 | -6086 -651 3665 10628
mcc n/a| 1 7 -18 155 -116 -445 .10 160 160 | --- --- --- ---
Table 2.1952.2 GPS week: 1952 Day: 2 MJD: 57910
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 -14 -11 23 .10 21 18 | -12072 -557 3961 11796
cof n/a| 0 0 2 -31 -4 -21 .22 26 22 | -12064 -563 3964 11797
emx n/a| 0 1 2 -31 -28 5 .01 16 16 | 14102 -500 3953 11183
esx n/a| 0 0 -3 3 15 -9 .24 21 16 | -24990 1308 3948 12307
gfz n/a| 0 0 -1 -25 46 -1 -.03 23 21 | 0 -974 3955 11466
grg n/a| 1 -2 3 -45 4 -26 -.42 29 26 | -3155 -167 3958 11290
iac n/a| 0 0 -2 81 11 51 -.07 20 20 | -2104 -662 3959 10917
mcc n/a| -15 -2 3 162 -58 -424 .85 185 185 | --- --- --- ---
Table 2.1952.3 GPS week: 1952 Day: 3 MJD: 57911
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 5 -3 -3 66 .11 19 19 | -16371 485 3548 13999
cof n/a| -1 0 4 -4 -32 54 .11 24 22 | -16374 490 3545 13995
emx n/a| -3 -1 4 -37 -49 -13 .00 23 23 | 3812 -57 3570 12339
esx n/a| 1 1 -5 0 1 -1 .25 20 16 | -10245 541 3558 16525
gfz n/a| 1 0 -3 -2 57 -38 -.08 21 18 | 0 486 3598 13761
grg n/a| 0 0 0 -93 22 -78 -.31 26 24 | -7793 639 3598 13588
iac n/a| 2 1 -2 77 -23 15 -.07 18 18 | -5706 -855 3555 13070
mcc n/a| -10 3 26 24 -97 -376 .30 222 222 | --- --- --- ---
Table 2.1952.4 GPS week: 1952 Day: 4 MJD: 57912
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 3 -28 -14 65 .07 22 16 | -16196 -544 3201 9975
cof n/a| 0 -1 0 -21 32 76 .13 25 18 | -16175 -570 3204 9978
emx n/a| -3 0 4 -19 -28 35 -.06 20 20 | -16944 -131 3205 9187
esx n/a| 0 0 -2 10 30 50 .24 19 17 | -9445 -2143 3191 12384
gfz n/a| 1 1 0 -3 36 28 -.02 21 18 | 0 -1419 3198 9460
grg n/a| 0 -1 -6 -67 9 -125 -.32 28 23 | -7801 -712 3223 9266
iac n/a| 0 0 0 72 -76 -76 -.06 21 22 | -7151 711 3201 8928
mcc n/a| -1 -3 1 63 -164 -383 .04 230 230 | --- --- --- ---
Table 2.1952.5 GPS week: 1952 Day: 5 MJD: 57913
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 3 -17 10 33 .14 24 21 | -13174 -3215 3397 11628
cof n/a| 0 0 2 -35 7 13 .10 29 23 | -13166 -3238 3399 11630
emx n/a| -1 0 6 7 14 -49 -.06 23 23 | -19410 -2060 3388 10838
esx n/a| 2 0 0 -24 22 3 .13 18 16 | -18585 -2696 3395 13976
gfz n/a| 1 3 2 15 24 -13 -.03 23 16 | 0 -3300 3412 11123
grg n/a| 0 0 -15 -59 -42 -22 -.34 33 26 | -1570 -3600 3387 10773
iac n/a| -1 0 0 62 -24 20 -.04 20 20 | -2477 -313 3402 10616
mcc n/a| -3 -3 -2 239 -159 -229 -.16 209 209 | --- --- --- ---
Table 2.1952.6 GPS week: 1952 Day: 6 MJD: 57914
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 6 -43 -28 -8 .13 23 18 | -14456 -545 3190 12030
cof n/a| -2 0 2 -7 23 -17 .08 26 20 | -14469 -543 3191 12030
emx n/a| -1 1 6 -15 23 -63 .01 25 25 | -11688 -176 3188 11260
esx n/a| 3 2 -6 17 11 19 .21 21 18 | -5297 -1403 3193 14973
gfz n/a| 1 0 0 0 10 33 -.06 19 16 | 0 -191 3184 11582
grg n/a| -3 -2 -6 -42 -9 -18 -.33 32 31 | -1045 -339 3205 11388
iac n/a| 0 0 -2 49 -27 22 -.10 19 19 | -794 -230 3184 10985
mcc n/a| 9 -1 0 221 -92 -249 -.17 162 162 | --- --- --- ---
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 3.1952.0 GPS week: 1952 Day: 0 MJD: 57908
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 | 725 17 14 37 8 24 20 14 --- 9 | 23 22 26 20 21 26 21 --- 20
R02 | 1085 18 18 22 19 22 23 13 188 8 | 26 27 26 24 22 27 19 81 21
R03 | 826 15 15 12 16 6 16 10 111 5 | 25 23 22 19 18 16 16 15 18
R04 | 1799 23 17 25 9 20 22 10 --- 8 | 12 12 12 11 23 18 11 --- 10
R05 | 578 34 15 28 43 27 66 16 --- 16 | 14 26 27 33 27 26 19 --- 18
R06 | 1495 31 29 33 36 33 17 12 --- 12 | 16 26 22 38 44 24 26 --- 25
R07 | 1505 11 15 18 9 12 22 16 172 6 | 20 23 22 23 25 27 24 33 21
R08 | 880 18 18 22 21 18 39 13 --- 9 | 11 12 16 24 19 11 10 --- 13
XR09 |>>>>> 13 16 19 16 13 --- 16 --- 8 | 9 13 8 16 22 --- 20 --- 13
R10 | 669 17 17 15 20 25 25 7 --- 8 | 21 20 19 25 19 14 17 --- 18
R11 | 1162 27 36 19 14 32 17 16 211 9 | 27 32 21 25 22 21 19 24 21
R13 | 1838 16 21 20 15 20 23 9 --- 7 | 18 19 16 21 19 21 17 --- 17
R14 | 1684 40 40 37 40 41 40 28 --- 16 | 20 22 20 30 41 18 23 --- 19
R15 | 1182 25 26 23 24 34 25 15 --- 10 | 29 30 23 30 21 15 26 --- 24
R16 | 1316 12 20 37 23 25 36 16 --- 11 | 37 42 30 37 40 30 43 --- 35
R17E | 2109 20 14 20 14 19 14 11 --- 7 | 14 15 22 17 22 18 16 --- 16
R18E | 1026 11 15 19 15 13 12 11 --- 6 | 12 13 13 12 13 12 14 --- 11
R19E | 3202 25 19 26 21 29 30 15 --- 10 | 21 23 20 27 26 25 26 --- 21
R20E | 1567 31 36 27 20 32 29 16 --- 11 | 23 27 27 30 43 30 26 --- 25
R21E | 1454 16 22 19 12 21 23 13 53 7 | 11 22 18 14 21 14 16 17 13
R22E | 628 18 22 20 11 18 20 11 --- 7 | 11 15 12 13 16 14 14 --- 11
R23E | 1166 24 23 25 18 11 17 11 --- 8 | 17 24 17 23 20 24 20 --- 19
R24E | 1028 25 20 26 23 24 59 23 --- 13 | 18 25 20 17 9999 35 17 --- 14
XR26E | ---- 19 179 --- --- --- --- 11 --- 14 | 13 65 --- --- --- --- 10 --- 9
------+---------------------------------------------------+-----------------------------------------------
RMS | 1438 23 23 25 22 25 30 15 158 |T 18 24 19 23 24 21 19 34 18
WRMS | 1438 22 22 25 18 16 25 13 158 |NE 20 23 20 25 25 21 20 38 19
MEDI | 1182 18 19 22 18 22 23 13 172 |MD 18 23 20 23 22 21 19 24 18
Table 3.1952.1 GPS week: 1952 Day: 1 MJD: 57909
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 | 843 16 23 20 14 17 16 12 --- 7 | 19 21 14 23 23 24 16 --- 17
R02 | 1024 11 9 10 16 17 15 11 228 6 | 22 21 21 22 20 21 16 70 18
R03 | 613 14 14 13 18 13 17 11 119 6 | 22 20 22 27 22 17 19 8 21
R04 | 1530 10 15 16 11 11 17 25 --- 7 | 10 16 12 14 14 16 9 --- 9
R05 | 985 37 50 13 27 23 51 28 --- 13 | 13 15 20 30 18 20 20 --- 17
R06 | 1496 29 33 27 34 17 21 18 --- 11 | 16 18 18 34 30 30 26 --- 23
R07 | 1146 9 13 11 7 6 20 13 155 5 | 20 22 20 21 21 25 19 39 19
R08 | 756 22 24 17 22 15 53 11 --- 11 | 9 15 13 18 17 28 9 --- 11
XR09 | 2224 14 14 17 16 13 --- 13 --- 7 | 8 12 10 18 26 --- 18 --- 13
R10 | 1060 12 19 15 22 19 21 9 --- 7 | 17 23 18 21 18 13 18 --- 16
R11 | 1485 30 30 12 10 26 17 8 178 8 | 24 25 19 22 17 15 15 15 17
R13 | 1186 11 15 21 17 23 19 11 --- 8 | 16 16 16 21 20 18 16 --- 15
R14 | 1085 42 28 23 51 33 31 26 --- 15 | 16 30 19 48 43 28 24 --- 23
R15 | 1806 24 24 14 14 16 31 22 --- 9 | 27 32 23 27 23 18 23 --- 21
R16 | 1126 18 33 22 25 18 27 21 --- 9 | 33 38 26 29 44 22 36 --- 29
R17E | 1846 17 17 18 13 15 14 11 --- 6 | 13 14 19 16 19 16 17 --- 14
R18E | 693 13 10 20 15 17 18 19 --- 7 | 10 13 12 13 17 16 15 --- 11
R19E | 2201 26 12 25 16 23 32 15 --- 10 | 19 25 21 26 28 25 24 --- 21
R20E | 1021 28 25 23 29 25 41 23 --- 12 | 22 30 23 31 39 25 24 --- 23
R21E | 886 16 13 15 12 18 16 14 79 7 | 10 14 17 16 22 12 16 11 13
R22E | 925 20 22 16 9 20 19 12 --- 7 | 11 21 16 16 23 14 14 --- 13
R23E | 637 19 17 33 17 13 29 20 --- 10 | 18 23 18 23 20 24 21 --- 19
XR24E | 1011 23 33 28 32 --- 48 17 --- 14 | 12 19 15 18 --- 31 18 --- 13
XR26E | ---- 16 72 --- --- --- --- 10 --- 13 | 14 41 --- --- --- --- 11 --- 9
------+---------------------------------------------------+-----------------------------------------------
RMS | 1231 22 23 19 21 19 27 17 160 |T 16 21 17 23 23 20 18 28 16
WRMS | 1231 20 22 19 18 17 23 17 160 |NE 18 21 18 25 23 21 18 33 17
MEDI | 1060 17 19 17 16 17 20 13 155 |MD 16 21 18 22 21 20 18 15 17
Table 3.1952.2 GPS week: 1952 Day: 2 MJD: 57910
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 | 779 20 28 12 27 14 28 19 --- 9 | 17 17 37 21 17 33 12 --- 14
R02 | 1143 12 22 12 10 23 22 10 300 6 | 15 24 15 20 16 26 10 56 14
R03 | 1343 11 15 6 14 11 21 9 123 5 | 13 19 13 20 16 23 15 6 12
R04 | 796 7 11 16 9 9 17 11 --- 5 | 13 18 16 13 13 16 11 --- 12
R05 | 1647 44 39 18 41 18 66 32 --- 16 | 11 22 22 46 20 13 15 --- 18
R06 | 1273 19 26 12 11 25 20 26 --- 8 | 13 19 15 19 23 18 19 --- 11
R07 | 841 12 10 12 15 15 14 11 169 6 | 14 18 13 32 30 29 22 44 21
R08 | 723 17 20 9 21 18 32 26 --- 9 | 11 18 11 23 25 14 14 --- 12
XR09 | 3348 11 17 18 10 17 --- 14 --- 7 | 7 13 9 17 24 --- 13 --- 11
R10 | 906 10 16 11 17 18 17 10 --- 6 | 16 20 17 17 19 12 17 --- 15
R11 | 1367 25 33 12 13 33 16 9 157 8 | 19 23 18 22 20 19 15 29 16
R13 | 1405 9 13 17 17 24 23 23 --- 8 | 16 22 16 19 22 16 16 --- 16
R14 | 2249 29 39 20 44 39 57 16 --- 15 | 17 31 16 36 35 21 22 --- 18
R15 | 716 24 30 13 15 20 12 20 --- 8 | 23 31 19 20 15 13 17 --- 17
R16 | 1105 24 26 25 26 37 38 24 --- 12 | 26 39 20 27 43 21 29 --- 21
R17E | 2418 18 19 17 14 15 28 20 --- 8 | 13 13 16 18 21 21 17 --- 14
R18E | 902 11 15 13 10 14 20 13 --- 6 | 10 14 13 12 15 14 15 --- 10
R19E | 1179 34 19 30 17 25 31 27 --- 12 | 17 29 27 30 36 27 23 --- 23
R20E | 1064 31 44 20 25 30 26 24 --- 11 | 21 39 25 33 37 21 24 --- 24
R21E | 785 16 11 13 12 14 24 13 109 6 | 10 11 14 14 21 13 15 8 13
R22E | 1410 20 16 18 9 19 20 13 --- 7 | 11 15 16 15 22 14 15 --- 13
R23E | 698 12 37 22 18 17 21 22 --- 8 | 19 40 19 24 24 25 22 --- 19
R24E | 1512 24 39 17 35 30 29 24 --- 12 | 18 30 16 33 9999 18 15 --- 17
XR26E | ---- 22 58 --- --- --- --- 20 --- 21 | 23 79 --- --- --- --- 10 --- 12
------+---------------------------------------------------+-----------------------------------------------
RMS | 1278 21 26 16 21 23 29 20 184 |T 15 25 17 23 23 19 16 28 15
WRMS | 1278 18 22 16 16 21 26 20 184 |NE 15 22 17 23 22 19 16 33 15
MEDI | 1143 18 20 16 15 18 22 19 157 |MD 15 20 16 20 21 18 15 29 14
Table 3.1952.3 GPS week: 1952 Day: 3 MJD: 57911
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 | 627 16 40 22 9 10 16 8 --- 6 | 16 36 33 24 21 19 13 --- 17
R02 | 670 16 14 16 15 11 16 20 392 7 | 21 20 18 19 19 19 15 220 16
R03 | 1498 10 9 16 11 20 29 11 121 7 | 19 19 22 25 19 16 14 11 18
R04 | 1047 8 8 15 17 19 18 13 --- 6 | 16 18 18 22 20 21 18 --- 14
R05 | 1187 39 41 34 37 20 50 29 --- 15 | 13 26 23 20 25 19 23 --- 17
R06 | 1203 20 25 31 22 21 16 22 --- 10 | 16 22 18 24 19 15 20 --- 16
R07 | 660 7 11 15 6 12 20 11 187 5 | 16 20 19 18 21 26 21 54 18
R08 | 917 10 10 12 16 11 22 14 --- 6 | 12 13 13 17 13 25 9 --- 11
XR09 | 3861 14 15 19 8 14 --- 19 --- 7 | 11 11 10 18 23 --- 14 --- 12
R10 | 1164 13 35 21 22 11 20 14 --- 7 | 16 37 16 21 25 17 18 --- 15
R11 | 1159 22 24 15 13 22 34 19 173 9 | 22 22 19 24 21 17 15 63 18
R13 | 1585 14 25 27 22 17 24 18 --- 9 | 19 21 18 23 21 18 17 --- 17
R14 | 3646 31 24 38 37 47 42 21 --- 16 | 19 39 20 31 47 21 25 --- 22
R15 | 904 21 20 20 15 23 24 15 --- 9 | 19 21 20 22 16 15 18 --- 17
R16 | 1142 19 25 36 21 31 27 22 --- 11 | 31 37 32 32 41 30 32 --- 28
R17E | 2869 11 22 14 18 14 18 17 --- 7 | 16 21 18 20 22 20 17 --- 17
R18E | 778 10 28 19 25 14 21 16 --- 8 | 13 21 14 17 20 15 18 --- 14
R19E | 837 31 21 35 13 27 24 15 --- 11 | 18 28 29 32 35 31 24 --- 26
R20E | 787 26 31 23 27 27 23 29 --- 11 | 23 31 22 26 27 22 21 --- 19
R21E | 1190 13 12 20 13 17 19 14 115 7 | 11 15 19 11 19 20 18 20 13
R22E | 718 13 12 14 9 14 18 15 --- 6 | 14 16 17 15 24 14 16 --- 14
R23E | 993 13 18 18 15 15 29 22 --- 8 | 24 23 20 25 22 22 21 --- 20
XR24E | 1476 26 25 20 28 --- 21 19 --- 11 | 27 22 17 30 --- 13 20 --- 18
XR26E | ---- 17 279 --- --- --- --- 20 --- 19 | 22 183 --- --- --- --- 13 --- 14
------+---------------------------------------------------+-----------------------------------------------
RMS | 1415 19 24 23 20 21 26 18 222 |T 18 30 19 22 23 19 18 73 17
WRMS | 1415 19 22 23 16 18 24 18 222 |NE 17 24 19 22 23 19 18 87 17
MEDI | 1142 14 22 20 16 17 21 17 173 |MD 16 21 19 22 21 19 18 54 17
Table 3.1952.4 GPS week: 1952 Day: 4 MJD: 57912
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 | 721 19 18 14 16 13 16 18 --- 7 | 13 16 17 23 26 19 14 --- 16
R02 | 836 12 13 16 16 18 24 11 182 7 | 16 16 17 15 22 18 15 186 14
R03 | 677 5 6 10 14 25 11 28 150 7 | 15 17 16 19 25 15 17 26 15
R04 | 1025 11 13 9 8 17 20 17 --- 6 | 15 22 20 21 23 15 15 --- 16
R05 | 764 38 28 30 22 27 49 20 --- 14 | 15 29 24 23 23 17 19 --- 14
R06 | 1211 30 34 26 30 30 25 21 --- 12 | 10 30 13 28 27 20 19 --- 16
R07 | 745 8 13 11 8 9 26 16 117 6 | 11 12 15 20 20 22 15 47 14
R08 | 1229 15 17 20 13 21 29 17 --- 8 | 11 14 12 27 29 22 11 --- 14
XR09 | 3265 12 15 14 13 17 --- 11 --- 7 | 13 14 10 23 25 --- 16 --- 15
R10 | 1346 18 23 19 23 17 27 21 --- 9 | 19 22 17 19 14 18 17 --- 14
R11 | 1242 17 15 16 16 19 15 18 433 7 | 20 19 18 22 20 12 17 63 16
R13 | 1004 17 19 25 21 20 19 26 --- 9 | 19 21 16 22 19 17 19 --- 16
R14 | 2690 39 45 38 32 26 50 29 --- 16 | 18 32 23 28 28 34 28 --- 18
R15 | 1627 17 22 18 19 17 19 17 --- 8 | 18 23 20 22 19 14 17 --- 16
R16 | 809 35 32 17 25 34 54 25 --- 14 | 31 41 26 30 33 31 32 --- 26
R17E | 1767 21 19 20 11 15 16 20 --- 8 | 15 32 20 18 25 19 15 --- 17
R18E | 1024 12 15 15 13 13 15 13 --- 6 | 16 16 21 17 18 14 16 --- 15
R19E | 784 30 50 24 21 19 43 22 --- 12 | 22 37 31 34 30 27 25 --- 25
R20E | 763 21 16 21 23 27 30 30 --- 11 | 20 23 24 25 29 25 21 --- 20
R21E | 933 20 11 14 9 20 18 22 80 7 | 11 19 19 12 21 17 16 25 13
R22E | 752 17 14 14 11 17 19 14 --- 7 | 16 24 18 14 20 14 16 --- 14
R23E | 1122 21 22 19 15 15 25 29 --- 9 | 19 23 20 25 22 24 23 --- 20
R24E | 853 28 50 23 21 24 18 22 --- 10 | 14 43 15 23 9999 18 22 --- 15
XR26E | ---- 19 47 --- --- --- --- 21 --- 20 | 18 76 --- --- --- --- 14 --- 12
------+---------------------------------------------------+-----------------------------------------------
RMS | 1178 22 25 20 19 21 28 21 230 |T 16 25 18 22 23 19 18 69 16
WRMS | 1178 16 18 20 17 18 23 22 230 |NE 16 21 17 22 23 19 18 80 16
MEDI | 1004 18 18 18 16 19 20 20 150 |MD 16 22 18 22 23 18 17 47 15
Table 3.1952.5 GPS week: 1952 Day: 5 MJD: 57913
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 | 677 18 23 50 26 13 24 25 --- 12 | 12 19 24 28 14 13 16 --- 9
R02 | 696 14 18 13 15 11 19 12 128 6 | 23 24 26 32 31 16 17 53 22
R03 | 592 9 14 13 11 10 14 20 144 6 | 26 26 26 26 26 24 20 17 23
R04 | 1195 10 11 11 7 9 27 16 --- 6 | 14 18 16 19 17 16 13 --- 13
R05 | 836 42 40 45 14 22 70 37 --- 17 | 9 19 21 20 23 30 14 --- 11
R06 | 681 26 28 13 23 21 29 13 --- 9 | 15 16 18 23 21 20 19 --- 16
R07 | 717 17 18 22 12 15 37 19 119 9 | 21 19 20 19 21 44 20 33 19
R08 | 1110 14 16 15 10 20 28 13 --- 7 | 10 13 9 14 17 8 10 --- 9
XR09 | 2806 15 19 15 11 15 --- 17 --- 7 | 11 16 10 21 24 --- 16 --- 14
R10 | 754 13 21 13 18 25 21 15 --- 8 | 18 23 16 18 19 16 17 --- 15
R11 | 1775 19 26 12 15 21 11 14 399 7 | 26 28 21 24 17 13 20 55 19
R13 | 1238 15 17 17 18 17 19 13 --- 7 | 20 24 21 24 23 17 21 --- 20
R14 | 2743 40 42 42 30 28 46 26 --- 15 | 16 32 22 31 36 18 28 --- 19
R15 | 2067 11 15 17 18 25 31 13 --- 8 | 21 24 19 20 23 19 18 --- 18
R16 | 807 47 76 29 20 51 68 23 --- 17 | 49 76 33 40 46 32 42 --- 35
R17E | 1944 20 12 13 28 19 28 22 --- 10 | 14 19 19 26 29 17 15 --- 18
R18E | 920 12 17 12 15 22 20 14 --- 7 | 11 16 15 16 19 15 14 --- 12
R19E | 1085 24 21 18 16 19 20 15 --- 8 | 19 23 33 33 32 27 24 --- 26
R20E | 806 24 26 18 17 31 22 20 --- 10 | 25 29 21 29 27 24 20 --- 21
R21E | 1798 16 12 14 7 19 16 12 85 6 | 11 12 12 12 17 13 16 12 11
R22E | 1691 14 17 19 16 23 17 25 --- 8 | 9 22 19 17 21 11 14 --- 13
R23E | 1303 22 16 17 20 24 32 31 --- 11 | 20 21 19 23 28 24 22 --- 19
R24E | 722 36 56 14 25 22 45 22 --- 12 | 16 36 15 32 1 21 25 --- 19
XR26E | ---- 23 69 --- --- --- --- 21 --- 22 | 16 39 --- --- --- --- 11 --- 10
------+---------------------------------------------------+-----------------------------------------------
RMS | 1316 24 29 23 18 23 33 20 209 |T 18 24 19 23 23 19 18 34 17
WRMS | 1316 21 23 23 16 16 26 20 209 |NE 19 25 20 23 23 20 19 39 17
MEDI | 1085 17 18 15 16 21 24 17 128 |MD 16 22 19 23 23 17 17 33 18
Table 3.1952.6 GPS week: 1952 Day: 6 MJD: 57914
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 | 631 16 34 58 19 19 20 30 --- 13 | 14 25 31 14 12 12 23 --- 9
R02 | 538 11 17 20 12 14 15 11 68 6 | 26 28 26 23 20 20 20 52 21
R03 | 722 16 16 14 17 11 17 11 159 6 | 34 32 31 33 26 28 28 11 29
R04 | 984 11 13 14 17 8 25 14 --- 6 | 18 21 20 22 22 14 17 --- 17
R05 | 1266 48 57 33 28 20 70 33 --- 17 | 9 18 18 44 18 14 12 --- 14
R06 | 1041 23 27 15 25 22 33 17 --- 10 | 16 20 20 27 22 29 25 --- 19
R07 | 621 8 11 14 30 17 42 14 192 9 | 26 28 24 34 25 52 28 39 26
R08 | 1039 10 12 13 9 17 29 12 --- 6 | 13 13 15 18 22 13 14 --- 14
XR09 | 2428 16 13 15 19 17 --- 20 --- 8 | 11 18 12 21 27 --- 18 --- 16
R10 | 918 15 19 20 19 16 26 8 --- 7 | 19 25 18 20 19 18 17 --- 17
R11 | 1298 19 19 12 14 19 16 9 247 7 | 28 29 22 26 18 16 19 70 21
R13 | 2365 16 16 21 19 16 27 14 --- 8 | 19 20 17 28 23 13 20 --- 18
R14 | 1331 41 37 55 40 27 37 32 --- 17 | 17 24 14 22 33 16 25 --- 17
R15 | 967 10 8 12 17 16 18 12 --- 6 | 21 20 16 19 20 19 21 --- 18
R16 | 633 38 36 34 27 27 45 29 --- 14 | 50 45 33 46 37 36 45 --- 39
R17E | 1107 18 22 19 14 15 24 15 --- 7 | 17 15 17 22 18 16 19 --- 16
R18E | 744 11 15 13 12 16 19 16 --- 6 | 11 13 15 13 16 14 13 --- 12
R19E | 982 29 29 14 20 24 28 11 --- 9 | 19 22 23 23 26 22 20 --- 21
R20E | 894 30 28 18 18 23 42 17 --- 11 | 34 32 29 33 30 28 26 --- 27
R21E | 860 15 13 18 15 21 14 15 63 7 | 11 14 11 14 14 11 13 13 10
R22E | 1450 21 15 20 10 18 20 15 --- 8 | 10 14 15 17 18 15 15 --- 13
R23E | 918 18 16 19 18 13 31 17 --- 8 | 19 20 19 23 20 23 19 --- 18
R24E | 1096 18 43 33 35 25 42 29 --- 13 | 17 31 17 31 1 17 27 --- 20
XR26E | ---- 24 65 --- --- --- --- 21 --- 23 | 22 38 --- --- --- --- 14 --- 14
------+---------------------------------------------------+-----------------------------------------------
RMS | 1087 23 26 25 21 19 32 19 162 |T 20 23 20 24 21 20 20 37 18
WRMS | 1087 18 20 25 18 16 31 19 162 |NE 21 24 21 26 22 21 22 43 19
MEDI | 982 16 17 18 18 17 26 15 159 |MD 18 21 18 23 20 16 19 39 17
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