[IGSREPORT-25334] Wk 1951 IGLOS Final Orbits
acc
acc at igs.org
Sat Jun 17 06:38:05 PDT 2017
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1951 (May 28, 2017 - Jun 03, 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 2.1951.
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:
igl1951[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1951 in the SP3 format.
igl19517.sum Combination Report for GPS Week 1951.
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 | -14.2 ns
1 | -13.5 ns
2 | -8.2 ns
3 | -8.9 ns
4 | -6.1 ns
5 | -5.4 ns
6 | -7.1 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 1.1951, 1a.1951).
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 2.1951.0-6)
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 3.1951.0-6).
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 1951 summary. (May 28, 2017 - Jun 03, 2017)
Table 1.1951.a GPS week : 1951 MJD: 57901.0-57907.0
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 7 1 2 3 .14 24 21 | -17555 -1073 3394 12293
| 1 1 2 23 11 24 .03 | 1085 1323
cof n/a| 0 0 8 -11 6 4 .15 27 23 | -17557 -1068 3395 12296
| 1 1 4 27 17 34 .05 | 1088 1321
emx n/a| -1 0 2 -24 -15 -12 .04 23 22 | -7374 -401 3405 11376
| 1 1 2 24 19 41 .04 | 14514 815
esx n/a| 0 0 -2 -4 0 -38 .23 20 17 | -19725 -1662 3395 14633
| 0 0 1 12 19 49 .05 | 7554 2427
gfz n/a| 0 0 0 -20 42 -12 -.05 21 17 | 0 -1548 3406 11802
| 1 0 1 14 8 50 .06 | 0 1618
grg n/a| 0 0 -5 -65 34 -4 -.34 27 24 | -33725 47572 3407 11680
| 2 1 4 28 17 80 .07 | 41755 84809
iac n/a| 2 0 0 73 -30 45 -.08 18 18 | -8126 -238 3392 11307
| 1 1 2 28 20 38 .03 | 3340 477
mcc n/a| 2 -1 10 136 -133 -531 -.49 133 133 | --- --- --- ---
| 8 2 14 87 87 270 .36 | --- ---
Table 1.1951.b GPS week : 1951 MJD: 57901.0-57907.0
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 10 10 11 9 9 10 |
R02 | 7 7 7 8 7 7 7 |
R03 | 9 7 7 8 7 8 6 |
R04 | 9 6 6 8 6 5 8 |
R05 | 14 15 15 15 14 14 15 |
R06 | 11 9 12 9 9 10 9 |
R07 | 9 8 7 7 9 6 6 |
R08 | 8 8 7 9 9 5 8 |
R09 | 8 7 10 9 7 8 9 |
R10 | 10 8 8 8 9 9 9 |
R11 | 11 9 8 9 7 7 10 |
R13 | 8 9 9 10 7 6 7 |
R14 | 13 14 16 17 15 16 15 |
R15 | 10 10 8 8 7 8 8 |
R16 | 13 10 12 16 17 17 14 |
R17 | 11 7 8 10 9 7 7 |
R18 | 9 9 8 7 9 8 6 |
R19 | 10 11 13 11 10 11 11 |
R20 | 12 12 14 13 14 12 10 |
R21 | 8 8 8 9 9 9 8 |
R22 | 7 9 9 8 8 9 8 |
R23 | 10 12 9 7 9 10 11 |
R24 | 13 11 10 12 12 14 13 |
R26 | 0 0 33 25 22 22 23 |
Table 1.1951.c GPS week : 1951 MJD: 57901.0-57907.0
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 1951 0 | 24 38 107 350 -1217 3577 84.9 1367 1367 | -14185 0
brd 1951 1 | -24 72 202 -69 -1823 4045 83.2 1394 1394 | -13517 0
brd 1951 2 | -119 11 180 -1165 -1534 3373 83.0 1343 1343 | -8236 0
brd 1951 3 | -41 -77 100 518 429 2862 86.7 1765 1765 | -8888 0
brd 1951 4 | 94 11 194 1063 -1341 1006 88.3 1655 1655 | -6062 0
brd 1951 5 | -63 -45 172 170 -260 -287 87.5 1627 1627 | -5411 0
brd 1951 6 | 29 3 83 -311 -104 2361 85.9 1702 1702 | -7103 0
-------------+------------------------------------------------------------+----------------
brd 1951 mean| -14 2 148 79 -835 2419 85.6 1550 1550 | -9057 0
brd 1951 sdev| 70 50 49 703 849 1549 2.0 176 176 | 3487 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 2.1951.0 GPS week: 1951 Day: 0 MJD: 57901
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 8 34 -16 53 .19 25 25 | -18550 -2037 3593 13107
cof n/a| 0 0 10 16 -16 41 .18 26 25 | -18553 -2031 3596 13113
emx n/a| 0 0 1 -67 10 10 .07 29 29 | -29621 -1143 3592 12230
esx n/a| 0 0 0 -6 -13 -55 .26 18 16 | -32084 -3316 3588 15124
gfz n/a| 0 0 -1 -14 51 -4 -.04 20 18 | 0 -2611 3578 12693
grg n/a| 2 1 -3 -36 20 1 -.39 27 29 | -13013 -2307 3628 12569
iac n/a| 1 0 -1 79 -12 21 -.06 20 20 | -13472 -165 3581 12181
mcc n/a| 4 2 35 271 15 -769 -.59 87 87 | --- --- --- ---
Table 2.1951.1 GPS week: 1951 Day: 1 MJD: 57902
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 12 10 7 -4 .12 24 23 | -18815 -1656 3333 12869
cof n/a| 2 0 18 -6 17 8 .13 28 28 | -18822 -1640 3333 12870
emx n/a| -1 2 1 -45 0 -1 .03 22 22 | 18731 -544 3345 12010
esx n/a| 0 0 -2 13 2 -90 .28 20 18 | -12820 -5165 3330 14876
gfz n/a| 0 0 -1 -51 32 -79 .03 19 19 | 0 -2528 3337 12451
grg n/a| 0 0 -1 -83 43 114 -.43 28 24 | -12622 -1922 3324 12153
iac n/a| 1 0 -5 105 -66 68 -.05 17 17 | -12158 -586 3337 11881
mcc n/a| -6 -4 16 132 -111 -877 -.67 92 92 | --- --- --- ---
Table 2.1951.2 GPS week: 1951 Day: 2 MJD: 57903
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 7 -1 14 -24 .11 23 20 | -15672 -1164 3543 11662
cof n/a| 1 0 8 15 27 6 .21 28 24 | -15665 -1174 3540 11660
emx n/a| -3 1 3 -5 -22 59 .04 22 20 | -11087 56 3545 10673
esx n/a| 0 0 -2 -8 16 -82 .30 22 20 | -23816 198 3558 14139
gfz n/a| 0 0 -1 -21 41 -26 -.08 23 17 | 0 -1445 3559 11214
grg n/a| 0 0 -4 -33 63 62 -.28 25 21 | -7420 -1623 3558 11303
iac n/a| 1 0 -1 39 -38 -21 -.06 17 16 | -7324 -299 3537 10640
mcc n/a| -6 2 2 58 -189 -676 -.25 124 124 | --- --- --- ---
Table 2.1951.3 GPS week: 1951 Day: 3 MJD: 57904
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 -20 4 -4 .11 25 21 | -16987 -2926 3467 11215
cof n/a| 0 -1 7 -20 14 -61 .12 27 23 | -16994 -2909 3472 11221
emx n/a| -1 -1 -2 -15 -7 -7 .08 24 21 | -9335 -1727 3454 10437
esx n/a| -1 0 -4 -26 -7 -69 .22 19 17 | -16300 -3674 3460 13477
gfz n/a| -2 1 -2 -15 38 -64 -.11 22 18 | 0 -3282 3455 10797
grg n/a| 1 0 0 -47 19 33 -.34 29 22 | -7154 -3306 3461 10441
iac n/a| 3 0 0 85 -15 100 -.10 19 19 | -7239 -362 3454 10281
mcc n/a| 15 -2 8 172 -264 -347 -.30 164 164 | --- --- --- ---
Table 2.1951.4 GPS week: 1951 Day: 4 MJD: 57905
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 7 -32 7 -6 .13 25 21 | -18231 -194 3254 12415
cof n/a| 0 1 7 -51 11 5 .15 30 23 | -18233 -199 3250 12414
emx n/a| -1 0 5 -25 -20 -62 .04 22 22 | -7316 0 3259 11435
esx n/a| 0 0 0 5 28 -19 .19 18 17 | -9493 -786 3247 14209
gfz n/a| 1 1 0 -13 38 66 .02 23 17 | 0 -865 3263 11892
grg n/a| 0 -3 -11 -66 36 -69 -.36 28 22 | -91124 164144 3305 11643
iac n/a| 0 0 0 68 -41 53 -.10 17 16 | -6176 -110 3258 11412
mcc n/a| -2 -2 -10 145 -167 -155 .01 152 152 | --- --- --- ---
Table 2.1951.5 GPS week: 1951 Day: 5 MJD: 57906
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 7 -2 -9 0 .14 24 19 | -17474 1133 3359 12327
cof n/a| 0 -2 5 -40 6 -10 .20 29 20 | -17479 1148 3357 12332
emx n/a| 0 1 3 -11 -25 -47 .03 20 18 | -12343 708 3371 11892
esx n/a| 0 0 -4 -4 1 10 .22 21 17 | -21370 1617 3369 15048
gfz n/a| 0 1 0 -9 36 29 -.05 21 18 | 0 1630 3376 11997
grg n/a| -4 0 -10 -112 16 -77 -.38 28 27 | -98193 178974 3344 11592
iac n/a| 3 -1 -1 101 -10 41 -.13 19 18 | -4806 685 3371 11330
mcc n/a| 7 -3 5 175 -120 -283 -.51 150 150 | --- --- --- ---
Table 2.1951.6 GPS week: 1951 Day: 6 MJD: 57907
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 4 22 12 8 .15 23 19 | -17157 -669 3212 12458
cof n/a| 2 0 3 7 -18 41 .08 23 21 | -17155 -674 3217 12466
emx n/a| -1 2 3 1 -46 -36 -.04 23 22 | -647 -162 3269 10957
esx n/a| -2 0 -3 -2 -29 39 .16 19 17 | -22194 -512 3216 15564
gfz n/a| -1 0 -1 -15 55 -8 -.11 19 15 | 0 -1737 3279 11573
grg n/a| 0 -1 -5 -75 42 -99 -.24 27 26 | -6555 -951 3232 12063
iac n/a| 2 -2 2 32 -30 53 -.03 18 17 | -5708 -833 3207 11424
mcc n/a| 7 0 13 -1 -95 -608 -1.11 164 164 | --- --- --- ---
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 3.1951.0 GPS week: 1951 Day: 0 MJD: 57901
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 | 499 36 41 22 15 12 17 11 --- 8 | 2 5 3 8 7 3 3 --- 4
R02 | 640 21 23 16 13 14 15 16 107 7 | 1 2 2 4 4 1 2 2 2
R03 | 726 27 27 25 13 12 24 17 100 8 | 2 1 2 5 5 3 3 1 2
R04 | 1356 29 24 29 18 11 19 15 --- 9 | 1 2 2 3 2 2 2 --- 1
R05 | 745 28 22 26 17 20 57 33 --- 14 | 2 6 5 6 6 2 4 --- 3
R06 | 729 22 22 26 23 30 29 20 --- 11 | 1 3 2 4 4 2 3 --- 2
R07 | 708 20 18 21 8 10 21 33 80 9 | 2 2 3 5 4 2 3 2 2
R08 | 580 16 24 23 15 16 10 17 --- 7 | 2 4 3 2 3 2 2 --- 1
XR09 | 2218 18 23 22 11 15 --- 14 --- 8 | 2 3 3 4 3 --- 2 --- 2
R10 | 1174 17 25 21 24 22 26 13 --- 9 | 2 3 3 4 4 3 2 --- 2
R11 | 1904 40 35 24 18 21 27 18 77 11 | 3 6 3 4 3 2 2 2 2
R13 | 2408 16 16 16 11 22 20 12 --- 7 | 2 4 3 5 5 2 3 --- 2
R14 | 919 31 31 31 28 29 28 26 --- 12 | 3 15 5 8 6 5 5 --- 4
R15 | 1721 26 16 32 24 18 18 14 --- 10 | 3 8 4 5 4 4 2 --- 3
R16 | 1899 24 37 51 19 19 36 23 --- 12 | 5 12 4 5 8 2 3 --- 3
R17E | 1278 22 23 23 14 26 39 12 --- 10 | 2 4 2 6 7 4 4 --- 4
R18E | 831 17 21 33 10 17 26 12 --- 8 | 2 5 5 4 4 4 4 --- 3
R19E | 1718 34 36 24 15 20 26 16 --- 10 | 3 3 5 9 6 4 7 --- 4
R20E | 1170 31 30 24 22 22 31 29 --- 12 | 3 6 4 8 11 4 6 --- 5
R21E | 833 21 20 18 17 21 20 11 60 8 | 2 4 4 5 6 3 4 4 3
R22E | 1224 19 20 24 8 20 13 11 --- 7 | 3 3 3 6 5 4 5 --- 4
R23E | 2456 19 26 41 17 13 18 20 --- 9 | 3 4 3 5 4 3 4 --- 3
R24E | 1752 17 25 50 23 23 27 29 --- 12 | 4 9 4 6 5 6 5 --- 4
XR26E | ---- --- --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- 9999 --- 7
------+---------------------------------------------------+-----------------------------------------------
RMS | 1367 25 26 29 18 20 27 20 87 |T 2 4 3 5 5 3 3 2 3
WRMS | 1367 25 25 29 16 18 29 20 87 |NE 2 5 3 4 4 2 2 1 2
MEDI | 1174 22 24 24 17 20 24 16 80 |MD 2 4 3 5 5 3 3 2 3
Table 3.1951.1 GPS week: 1951 Day: 1 MJD: 57902
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 | 511 35 43 18 23 17 23 17 --- 10 | 3 8 4 9 8 3 3 --- 4
R02 | 830 14 15 16 15 10 14 15 87 6 | 2 4 4 8 4 2 1 2 2
R03 | 1130 21 18 12 14 18 14 14 120 7 | 2 3 3 6 6 2 2 1 2
R04 | 762 18 20 14 14 9 16 11 --- 6 | 2 2 2 4 4 3 3 --- 2
R05 | 980 23 31 20 22 28 72 23 --- 15 | 2 10 5 7 9 4 5 --- 4
R06 | 707 18 22 25 12 17 19 25 --- 9 | 2 5 2 6 7 3 2 --- 2
R07 | 710 20 23 17 20 11 18 18 52 7 | 2 2 3 5 4 2 3 2 1
R08 | 659 14 18 17 14 11 19 23 --- 7 | 2 5 4 4 3 2 3 --- 1
XR09 | 2486 17 16 15 12 9 --- 11 --- 6 | 2 3 3 5 4 --- 2 --- 2
R10 | 1351 13 16 24 20 13 16 14 --- 7 | 3 5 3 8 6 4 3 --- 3
R11 | 1583 28 42 14 15 27 12 14 105 8 | 3 5 3 4 4 2 3 2 2
R13 | 2571 18 25 26 14 22 21 14 --- 8 | 2 6 3 4 4 5 2 --- 2
R14 | 955 42 41 27 31 33 36 14 --- 13 | 3 15 8 19 15 5 5 --- 7
R15 | 891 28 38 17 17 15 34 16 --- 9 | 3 8 3 4 4 5 3 --- 3
R16 | 1936 22 28 20 26 19 30 19 --- 10 | 5 10 5 8 10 4 3 --- 4
R17E | 1556 21 20 19 15 15 12 10 --- 7 | 2 4 3 7 6 4 5 --- 4
R18E | 785 18 26 22 10 23 26 17 --- 8 | 3 6 5 4 6 5 4 --- 3
R19E | 2917 36 28 31 20 21 28 13 --- 11 | 3 4 9 11 7 3 6 --- 5
R20E | 1977 23 23 25 34 23 35 24 --- 12 | 4 9 5 11 19 7 7 --- 7
R21E | 676 20 22 20 13 18 14 14 84 7 | 2 4 4 8 6 4 6 4 4
R22E | 805 21 24 23 13 24 19 11 --- 8 | 3 4 5 7 8 4 4 --- 4
R23E | 2007 20 22 38 20 8 44 22 --- 11 | 3 5 3 6 5 7 4 --- 4
R24E | 725 24 36 19 31 22 28 20 --- 10 | 5 8 3 9 9 6 6 --- 5
XR26E | ---- 7 5232 --- --- --- --- --- --- 0 | 1 9999 --- --- --- --- --- --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1393 24 28 22 20 19 28 17 92 |T 2 5 4 7 6 3 3 2 3
WRMS | 1393 23 28 22 18 19 24 17 92 |NE 2 6 3 6 6 3 2 1 2
MEDI | 955 20 23 20 15 18 19 15 87 |MD 2 5 3 7 6 4 3 2 3
Table 3.1951.2 GPS week: 1951 Day: 2 MJD: 57903
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 | 652 34 45 22 31 10 11 13 --- 10 | 3 7 4 8 6 1 3 --- 2
R02 | 1028 10 12 15 21 10 19 17 59 7 | 2 5 4 8 5 3 2 13 2
R03 | 1461 20 25 10 14 11 16 13 121 6 | 2 3 3 5 4 2 2 3 2
R04 | 1192 17 21 17 14 13 12 10 --- 6 | 2 4 4 6 4 5 2 --- 3
R05 | 1404 24 30 17 35 38 56 21 --- 14 | 3 8 4 4 7 5 4 --- 3
R06 | 834 15 19 29 37 26 26 18 --- 11 | 3 8 2 7 7 3 2 --- 2
R07 | 584 14 10 20 15 12 15 14 100 7 | 2 4 2 6 3 3 3 9 2
R08 | 1053 13 13 13 18 14 19 15 --- 7 | 2 4 4 5 4 2 3 --- 2
XR09 | 2306 18 20 25 10 19 --- 21 --- 9 | 1 3 2 3 6 --- 2 --- 2
R10 | 940 14 16 17 23 19 23 10 --- 8 | 3 4 4 9 7 3 2 --- 3
R11 | 1352 20 21 16 11 22 16 12 198 7 | 2 4 3 3 3 2 2 4 2
R13 | 1593 17 27 23 18 29 15 8 --- 8 | 2 6 3 4 4 4 2 --- 2
R14 | 1614 50 61 29 34 41 43 18 --- 16 | 2 8 6 15 14 2 3 --- 6
R15 | 1291 27 36 12 18 22 16 12 --- 8 | 3 6 2 3 4 2 4 --- 2
R16 | 1256 25 29 37 28 18 29 25 --- 12 | 4 7 5 12 10 3 3 --- 5
R17E | 811 16 22 18 16 20 13 16 --- 7 | 3 4 3 6 5 4 5 --- 4
R18E | 899 17 18 25 10 19 21 10 --- 7 | 3 3 5 5 8 5 5 --- 4
R19E | 2104 37 34 37 23 24 30 18 --- 12 | 4 5 9 12 9 4 6 --- 6
R20E | 3153 26 18 23 27 44 36 29 --- 14 | 5 9 8 13 15 10 6 --- 7
R21E | 593 17 19 22 12 15 15 15 98 7 | 2 5 4 6 6 4 6 5 4
R22E | 645 22 24 16 11 22 21 21 --- 8 | 3 3 4 8 8 6 6 --- 5
R23E | 1263 15 20 17 21 15 27 15 --- 8 | 3 5 3 7 5 6 4 --- 3
R24E | 1086 24 41 23 23 22 27 17 --- 10 | 4 11 5 12 14 6 6 --- 6
XR26E | ---- 41 57 --- --- --- --- 26 --- 33 | 1 9999 --- --- --- --- 1 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1342 23 28 22 22 23 25 16 124 |T 2 5 4 7 6 3 3 6 3
WRMS | 1342 20 24 20 20 17 21 16 124 |NE 2 5 3 6 5 2 2 7 2
MEDI | 1192 18 21 20 18 19 19 15 100 |MD 3 5 4 6 6 3 3 5 3
Table 3.1951.3 GPS week: 1951 Day: 3 MJD: 57904
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 | 692 29 29 16 33 12 22 24 --- 11 | 4 6 5 7 6 3 4 --- 3
R02 | 1259 19 21 28 20 13 15 10 94 8 | 2 6 4 8 5 3 3 21 3
R03 | 1548 20 18 20 14 23 15 10 100 7 | 2 2 2 8 7 3 2 3 3
R04 | 1611 13 15 13 14 13 26 23 --- 8 | 2 3 4 5 3 4 2 --- 3
R05 | 2133 23 24 19 21 27 70 20 --- 14 | 3 5 4 8 7 9 5 --- 5
R06 | 1545 19 21 29 22 19 13 14 --- 9 | 4 8 3 7 7 4 3 --- 4
R07 | 1353 17 24 21 12 9 10 17 218 6 | 2 7 2 7 6 2 3 14 3
R08 | 892 20 19 19 15 20 20 20 --- 8 | 2 5 3 5 5 4 2 --- 2
XR09 | 2129 14 17 16 22 18 --- 13 --- 8 | 2 4 2 8 6 --- 2 --- 3
R10 | 920 13 12 16 15 23 18 14 --- 7 | 3 5 5 9 6 4 3 --- 4
R11 | 1278 22 24 15 14 26 25 11 244 8 | 3 3 5 6 7 4 3 7 4
R13 | 2984 12 19 19 15 26 33 25 --- 10 | 2 5 4 5 4 3 3 --- 2
R14 | 1597 50 57 45 32 27 42 26 --- 16 | 3 11 8 14 13 4 5 --- 7
R15 | 1408 28 30 14 13 18 17 13 --- 8 | 4 7 3 4 4 3 3 --- 3
R16 | 867 41 44 35 25 37 52 22 --- 15 | 4 8 5 16 14 3 3 --- 6
R17E | 746 18 15 19 16 23 18 32 --- 10 | 3 5 4 5 5 5 5 --- 4
R18E | 1071 14 13 18 13 18 15 10 --- 6 | 3 6 4 5 7 4 5 --- 4
R19E | 2090 38 45 26 16 26 21 13 --- 10 | 4 5 5 10 9 4 6 --- 5
R20E | 4707 26 23 34 18 33 33 25 --- 12 | 4 8 7 10 12 8 4 --- 5
R21E | 1086 22 16 15 10 21 24 20 96 8 | 3 5 4 6 6 4 5 7 4
R22E | 1323 15 17 25 14 17 15 18 --- 8 | 3 3 3 6 6 5 6 --- 4
R23E | 886 14 13 11 18 7 20 12 --- 6 | 2 5 3 10 5 4 6 --- 5
R24E | 1801 25 36 29 25 23 28 27 --- 11 | 3 10 4 14 13 5 5 --- 6
XR26E | ---- 29 111 --- --- --- --- 21 --- 25 | 1 9999 --- --- --- --- 1 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1764 25 27 24 19 22 29 19 164 |T 2 5 4 7 7 4 3 10 4
WRMS | 1764 21 23 21 17 18 22 19 164 |NE 2 5 3 7 6 3 3 11 3
MEDI | 1353 20 21 19 16 21 20 18 100 |MD 3 5 4 7 6 4 3 7 4
Table 3.1951.4 GPS week: 1951 Day: 4 MJD: 57905
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 | 640 23 31 30 15 12 26 14 --- 9 | 3 8 4 7 5 4 4 --- 4
R02 | 1571 14 15 14 19 9 11 13 94 6 | 2 5 4 6 6 4 3 3 4
R03 | 620 15 17 17 17 10 14 16 89 7 | 2 4 4 7 6 4 3 2 3
R04 | 1673 11 15 11 12 13 14 13 --- 5 | 1 3 3 3 3 2 2 --- 1
R05 | 1960 34 31 38 15 23 52 16 --- 13 | 3 4 7 10 8 8 5 --- 5
R06 | 1204 29 34 21 15 20 16 17 --- 8 | 3 6 4 5 7 3 3 --- 3
R07 | 1047 21 23 20 20 16 16 18 153 8 | 2 7 4 6 8 4 3 2 4
R08 | 1151 17 18 11 14 27 29 14 --- 8 | 2 5 2 4 3 5 2 --- 2
XR09 | 1744 14 22 9 20 13 --- 11 --- 7 | 3 4 5 9 6 --- 2 --- 4
R10 | 834 20 27 13 22 24 23 12 --- 8 | 3 7 4 6 6 3 2 --- 4
R11 | 972 17 17 13 17 21 11 14 265 7 | 3 4 5 5 6 4 3 3 4
R13 | 3473 15 17 14 18 23 16 11 --- 7 | 2 4 3 6 4 4 3 --- 3
R14 | 1143 39 37 39 28 31 44 15 --- 14 | 3 14 11 15 12 5 5 --- 8
R15 | 990 11 9 14 18 18 15 12 --- 6 | 3 5 5 7 4 3 3 --- 4
R16 | 1004 59 87 29 20 42 63 15 --- 17 | 7 11 5 12 12 4 3 --- 5
R17E | 1441 17 19 17 13 20 23 21 --- 8 | 3 5 4 5 8 4 5 --- 4
R18E | 934 12 17 19 10 20 34 17 --- 8 | 4 5 4 5 7 5 5 --- 4
R19E | 2862 34 29 22 19 27 15 12 --- 9 | 3 6 3 6 5 4 5 --- 4
R20E | 2832 21 20 28 26 34 38 33 --- 13 | 3 7 4 7 9 5 5 --- 4
R21E | 2364 21 27 25 15 20 19 14 73 8 | 3 5 5 7 8 4 5 4 5
R22E | 1140 22 16 19 11 17 19 16 --- 7 | 3 4 5 6 5 4 6 --- 4
R23E | 911 20 24 22 21 19 21 11 --- 8 | 3 4 3 12 7 4 7 --- 5
R24E | 1614 32 38 18 25 26 30 26 --- 11 | 4 12 3 13 20 7 5 --- 6
XR26E | ---- 29 122 --- --- --- --- 16 --- 22 | 1 9999 --- --- --- --- 1 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1655 25 30 22 18 23 28 17 152 |T 2 6 4 7 7 4 3 2 4
WRMS | 1655 21 23 22 17 17 22 16 152 |NE 2 6 4 7 6 4 3 2 3
MEDI | 1151 20 22 19 18 20 19 14 94 |MD 3 5 4 6 6 4 3 3 4
Table 3.1951.5 GPS week: 1951 Day: 5 MJD: 57906
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 | 660 20 19 14 23 12 19 22 --- 8 | 2 10 5 14 7 4 4 --- 5
R02 | 866 15 17 18 11 19 19 12 150 7 | 2 4 3 7 5 4 3 3 3
R03 | 566 22 17 13 21 15 14 14 94 7 | 2 4 4 4 5 3 3 2 2
R04 | 1327 11 11 14 11 9 14 9 --- 5 | 1 3 2 2 2 2 2 --- 1
R05 | 1032 25 28 19 24 16 59 32 --- 13 | 2 5 4 9 8 4 4 --- 3
R06 | 1833 26 28 23 27 15 20 23 --- 10 | 2 5 4 7 6 3 2 --- 3
R07 | 747 10 12 13 9 11 19 7 96 5 | 2 4 3 4 6 4 3 2 3
R08 | 1570 9 10 7 13 11 14 9 --- 4 | 2 5 5 6 7 7 3 --- 4
XR09 | 1559 15 15 17 11 17 --- 14 --- 7 | 2 3 4 5 5 --- 3 --- 3
R10 | 683 23 20 17 17 22 27 8 --- 8 | 3 6 3 5 6 4 2 --- 2
R11 | 982 19 26 15 11 23 13 12 253 7 | 2 3 3 2 4 3 3 2 2
R13 | 3272 13 13 11 13 16 15 14 --- 6 | 2 4 2 6 3 3 3 --- 2
R14 | 1076 45 57 38 41 19 34 34 --- 16 | 2 16 11 18 10 3 6 --- 8
R15 | 915 14 11 11 15 25 18 16 --- 7 | 3 3 4 5 4 3 3 --- 3
R16 | 811 47 74 39 28 23 60 24 --- 17 | 5 13 5 8 10 3 4 --- 3
R17E | 2009 13 20 13 13 19 15 16 --- 6 | 3 5 4 6 7 5 6 --- 4
R18E | 1047 10 11 18 17 16 17 18 --- 7 | 3 5 4 5 7 5 5 --- 4
R19E | 4065 24 24 22 20 31 25 17 --- 10 | 3 7 5 7 8 4 5 --- 5
R20E | 2181 34 45 23 22 26 31 22 --- 11 | 5 9 4 7 10 5 5 --- 4
R21E | 1712 17 17 20 14 19 18 23 89 8 | 3 3 4 8 8 5 5 4 5
R22E | 715 23 26 17 16 19 27 17 --- 9 | 3 4 6 8 7 4 5 --- 5
R23E | 811 21 25 13 29 17 24 18 --- 9 | 3 6 3 11 6 4 6 --- 5
R24E | 1475 31 28 23 26 42 40 26 --- 14 | 5 11 3 10 17 7 6 --- 6
XR26E | ---- 25 62 --- --- --- --- 19 --- 22 | 9999 9999 --- --- --- --- 1 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1626 24 29 20 21 21 28 19 150 |T 2 6 4 7 6 4 3 2 3
WRMS | 1626 19 20 18 17 18 27 18 150 |NE 2 5 4 6 5 3 3 2 3
MEDI | 1047 20 20 17 17 19 19 17 96 |MD 2 5 4 7 7 4 3 2 3
Table 3.1951.6 GPS week: 1951 Day: 6 MJD: 57907
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 | 656 15 19 22 23 24 15 24 --- 9 | 2 8 4 11 5 3 3 --- 4
R02 | 1328 15 20 16 19 15 18 11 186 7 | 1 3 2 5 3 3 2 2 2
R03 | 934 15 17 13 6 10 17 14 110 5 | 1 2 2 2 3 2 2 1 1
XR04 | 2670 12 26 --- 11 --- 19 15 --- 8 | 1 3 --- 2 --- 2 1 --- 1
R05 | 577 38 30 25 38 21 54 20 --- 15 | 2 3 2 6 4 3 2 --- 2
R06 | 1970 19 26 23 12 12 22 29 --- 9 | 2 4 3 6 4 3 1 --- 2
R07 | 780 12 9 14 9 7 21 14 87 5 | 2 2 2 1 2 2 1 1 1
R08 | 1498 17 12 16 16 16 27 13 --- 7 | 2 3 4 5 6 5 2 --- 3
XR09 | 1888 19 18 18 16 14 --- 16 --- 8 | 2 2 2 2 2 --- 2 --- 2
R10 | 764 18 24 24 24 19 19 15 --- 9 | 2 3 2 4 3 3 2 --- 2
R11 | 1082 27 27 20 17 29 21 15 256 9 | 2 2 3 2 3 2 2 2 2
R13 | 3127 11 11 15 18 17 20 12 --- 7 | 2 3 2 4 3 2 2 --- 2
R14 | 1706 33 35 38 33 28 40 33 --- 15 | 2 12 7 13 6 2 4 --- 5
R15 | 1013 14 17 13 18 18 31 13 --- 8 | 2 3 2 2 3 2 2 --- 2
R16 | 742 27 33 42 23 25 47 22 --- 13 | 3 8 3 6 6 3 4 --- 3
R17E | 1432 12 11 19 12 15 15 13 --- 6 | 3 4 3 5 4 5 5 --- 4
R18E | 1012 11 15 17 10 16 16 10 --- 6 | 3 3 4 4 6 4 5 --- 4
R19E | 4651 31 27 32 20 24 21 15 --- 10 | 4 5 4 6 7 4 5 --- 5
R20E | 2201 34 33 21 14 23 21 16 --- 10 | 5 7 3 5 8 4 4 --- 4
R21E | 794 19 18 23 10 21 18 11 119 7 | 3 3 3 6 6 4 5 4 4
R22E | 1001 19 19 19 8 17 26 13 --- 7 | 3 3 5 6 6 5 6 --- 5
R23E | 739 33 36 27 24 14 26 20 --- 11 | 2 5 3 7 4 3 5 --- 3
XR24E | 2355 30 27 21 23 --- 35 23 --- 13 | 5 8 3 6 --- 5 5 --- 4
XR26E | ---- 26 61 --- --- --- --- 21 --- 23 | 9999 9999 --- --- --- --- 1 --- 9999
------+---------------------------------------------------+-----------------------------------------------
RMS | 1701 23 23 23 19 19 27 18 164 |T 2 4 3 5 4 3 3 2 2
WRMS | 1701 19 21 22 17 15 26 17 164 |NE 1 4 2 4 3 2 2 1 2
MEDI | 1082 19 20 20 17 17 21 15 119 |MD 2 3 3 5 4 3 2 2 3
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