[IGSREPORT-24309] Wk 1886 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu Mar 17 16:09:48 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1886 (Feb 28, 2016 - Mar 05, 2016)
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 2.1886.
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:
igl1886[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1886 in the SP3 format.
igl18867.sum Combination Report for GPS Week 1886.
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
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 | 0.3 ns
1 | 2.4 ns
2 | 1.7 ns
3 | 1.9 ns
4 | 3.9 ns
5 | -3.6 ns
6 | -4.5 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
4 | COD | R11
5 | GRG | R06 R07 R09
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 1.1886, 1a.1886).
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 2.1886.0-6)
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 3.1886.0-6).
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 1886 summary. (Feb 28, 2016 - Mar 05, 2016)
Table 1.1886.a GPS week : 1886 MJD: 57446.0-57452.0
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 -7 41 -29 13 .19 44 39 | --- --- --- ---
| 1 1 2 44 25 33 .08 | --- ---
cof n/a| -2 1 -11 45 -21 -12 .16 47 41 | --- --- --- ---
| 2 3 3 55 33 53 .06 | --- ---
emx n/a| 0 -2 1 -22 -52 -85 .25 27 27 | 692 50 3257 6456
| 2 1 2 17 22 33 .05 | 7105 1398
esx n/a| 0 0 -1 -44 -24 21 -.07 20 20 | 288 -168 3315 7588
| 0 2 1 15 20 49 .02 | 5561 2660
gfz n/a| 0 0 7 55 47 58 .10 25 21 | 0 -195 3155 6184
| 1 0 3 5 19 42 .05 | 0 1884
grg n/a| -3 0 5 -28 73 66 -.40 54 39 | -521547 -731 9015 538525
| 2 1 1 26 37 57 .06 | 211003 2385
iac n/a| 1 0 -3 -1 -16 -97 -.12 32 32 | 1015 -673 3229 6097
| 2 0 3 31 71 210 .06 | 2717 1538
mcc n/a| 4 -3 -4 -19 -103 616 .06 159 159 | --- --- --- ---
| 7 8 19 130 113 807 .51 | --- ---
Table 1.1886.b GPS week : 1886 MJD: 57446.0-57452.0
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 14 19 23 17 14 |
R02 | 10 7 9 13 17 10 14 |
R03 | 15 10 10 11 11 14 11 |
R04 | 15 10 9 10 11 10 9 |
R05 | 15 15 13 14 13 14 15 |
R06 | 10 8 9 18 13 8 9 |
R07 | 12 10 12 15 13 12 10 |
R08 | 13 11 12 15 17 11 11 |
R09 | 8 7 8 9 8 8 8 |
R10 | 8 9 9 8 9 11 9 |
R11 | 20 19 18 20 49 --- --- |
R13 | 11 9 10 8 9 10 10 |
R14 | 19 17 18 13 14 13 12 |
R15 | 15 11 12 16 12 11 13 |
R17 | 16 13 12 17 16 9 14 |
R18 | 11 10 11 10 10 9 8 |
R19 | 12 10 9 10 15 11 10 |
R20 | 18 15 13 23 14 14 13 |
R21 | 9 11 14 16 15 11 10 |
R22 | 19 13 12 13 13 9 10 |
R23 | 12 16 10 12 21 8 9 |
R24 | 20 17 17 24 25 14 14 |
R26 | 80 32 31 31 29 17 16 |
Table 1.1886.c GPS week : 1886 MJD: 57446.0-57452.0
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 1886 0 | 28 6 -1 -644 1754 -2596 83.7 1867 1867 | 303 0
brd 1886 1 | -19 -40 -2 -310 449 -2774 83.7 1498 1498 | 2435 0
brd 1886 2 | -169 408 187 -2088 1107 3071 73.3 8975 8975 | 1667 0
brd 1886 3 | -179 -28 41 -14 -2362 645 86.0 5161 5161 | 1866 0
brd 1886 4 | 45 -29 23 599 -2124 -1572 83.0 1439 1439 | 3857 0
brd 1886 5 | 28 46 31 -817 -332 1380 84.6 1357 1357 | -3616 0
brd 1886 6 | 70 -11 -91 -286 436 -399 84.9 1666 1666 | -4450 0
-------------+------------------------------------------------------------+----------------
brd 1886 mean| -27 50 26 -508 -153 -320 82.7 3137 3137 | 294 0
brd 1886 sdev| 103 160 83 833 1566 2164 4.3 2906 2906 | 3147 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 2.1886.0 GPS week: 1886 Day: 0 MJD: 57446
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 -9 25 -44 -34 .14 42 43 | --- --- --- ---
cof n/a| 0 0 -12 60 7 -91 .18 48 45 | --- --- --- ---
emx n/a| 0 0 -3 -1 -60 -119 .23 31 33 | 5529 724 3974 9451
esx n/a| 1 0 0 -49 -18 27 -.07 20 19 | 3946 -414 3981 10492
gfz n/a| -3 0 10 55 31 89 .16 25 22 | 0 -1109 3605 9148
grg n/a| -4 0 7 -7 51 90 -.50 44 39 | -440013 -2703 3914 611596
iac n/a| 5 1 -8 -38 24 -1 -.13 38 38 | 1931 657 3751 8844
mcc n/a| 0 1 -16 -102 -133 607 -.55 137 137 | --- --- --- ---
Table 2.1886.1 GPS week: 1886 Day: 1 MJD: 57447
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 88 -49 15 .22 46 43 | --- --- --- ---
cof n/a| -4 -1 -8 126 -63 7 .18 48 45 | --- --- --- ---
emx n/a| 1 -2 2 -28 -63 -127 .29 28 28 | 4848 45 3802 6896
esx n/a| 0 -2 0 -35 -31 -36 -.04 22 21 | -3709 775 3988 8038
gfz n/a| -1 0 8 56 40 82 .09 27 28 | 0 591 3606 6444
grg n/a| -4 0 6 -53 74 43 -.38 43 36 | -445305 -1066 10338 608820
iac n/a| 0 1 -3 -14 36 26 -.12 17 17 | 2229 -515 3805 6205
mcc n/a| 0 -3 -5 -62 -122 459 -.17 204 204 | --- --- --- ---
Table 2.1886.2 GPS week: 1886 Day: 2 MJD: 57448
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 3 -6 21 -51 33 .19 48 41 | --- --- --- ---
cof n/a| -3 3 -9 35 -57 47 .12 49 43 | --- --- --- ---
emx n/a| 5 -2 2 -41 -57 -63 .30 30 30 | 4129 -1151 1466 2553
esx n/a| 0 -1 0 -33 -60 27 -.09 20 19 | 5404 845 1471 2582
gfz n/a| 0 0 7 42 39 43 .06 23 20 | 0 253 1448 2544
grg n/a| -5 -1 7 -19 129 48 -.31 42 39 | -999999 537 19456 68605
iac n/a| 0 0 -3 17 43 -40 -.04 18 18 | 2293 -2400 1467 2631
mcc n/a| -8 -13 31 -27 -90 1881 -.31 259 259 | --- --- --- ---
Table 2.1886.3 GPS week: 1886 Day: 3 MJD: 57449
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 -10 112 15 59 .14 48 39 | --- --- --- ---
cof n/a| 2 6 -12 101 20 6 .03 53 42 | --- --- --- ---
emx n/a| -2 -1 0 -43 -52 -31 .18 29 28 | -639 -1498 3605 6326
esx n/a| 0 0 -1 -28 8 69 -.08 18 18 | 7177 -3204 3658 7817
gfz n/a| 1 -1 10 56 47 63 .07 26 22 | 0 -2697 3576 6038
grg n/a| -2 0 4 -38 46 139 -.40 51 43 | -436735 -3235 19208 611845
iac n/a| 2 1 -7 39 -70 -520 -.20 53 53 | 3140 -2330 3614 6055
mcc n/a| 7 -6 -1 -62 -248 735 .87 188 188 | --- --- --- ---
Table 2.1886.4 GPS week: 1886 Day: 4 MJD: 57450
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 2 -10 4 -40 37 .07 44 38 | --- --- --- ---
cof n/a| -1 3 -16 -34 5 47 .17 45 40 | --- --- --- ---
emx n/a| 0 -2 1 -12 -3 -76 .17 21 22 | 7721 2508 3547 6221
esx n/a| 1 3 -4 -71 -14 92 -.07 23 23 | -678 4069 3594 7856
gfz n/a| -1 0 7 60 68 110 .12 26 21 | 0 3243 3492 5901
grg n/a| -1 2 5 12 18 39 -.43 40 35 | -439178 3820 3718 619505
iac n/a| 0 0 0 -42 -154 -232 -.19 64 64 | 3308 1856 3571 5738
mcc n/a| 8 9 -4 -142 -205 639 .37 128 128 | --- --- --- ---
Table 2.1886.5 GPS week: 1886 Day: 5 MJD: 57451
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 -4 49 -6 -16 .29 41 34 | --- --- --- ---
cof n/a| -5 -1 -3 21 -44 -61 .21 47 39 | --- --- --- ---
emx n/a| 2 -3 0 -24 -70 -104 .30 24 24 | -4182 680 2995 7044
esx n/a| 1 2 -1 -35 -31 4 -.09 21 20 | -8556 502 3051 8067
gfz n/a| 0 0 5 55 77 -20 .04 23 20 | 0 -198 2927 6725
grg n/a| -5 2 5 -23 98 -26 -.41 114 41 | -444816 -515 3067 625049
iac n/a| -1 0 -1 -3 -3 75 -.09 16 16 | -2868 -793 2993 6781
mcc n/a| 13 3 -33 7 -6 867 .47 92 92 | --- --- --- ---
Table 2.1886.6 GPS week: 1886 Day: 6 MJD: 57452
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 2 -5 -10 -29 -1 .26 40 35 | --- --- --- ---
cof n/a| -3 0 -13 5 -15 -42 .21 41 36 | --- --- --- ---
emx n/a| -2 -1 4 -3 -56 -76 .25 24 24 | -12556 -955 3416 6703
esx n/a| 1 0 -1 -54 -22 -36 -.08 18 18 | -1566 -3755 3465 8265
gfz n/a| 0 0 0 59 23 41 .17 23 17 | 0 -1449 3436 6489
grg n/a| 0 1 3 -65 93 127 -.36 45 37 | -444783 -1957 3407 624256
iac n/a| 2 0 -2 28 10 11 -.10 17 17 | -2922 -1190 3406 6429
mcc n/a| 11 -15 1 255 84 -870 -.26 102 102 | --- --- --- ---
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 3.1886.0 GPS week: 1886 Day: 0 MJD: 57446
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 57 88 21 16 18 44 49 --- 14 | 77 98 57 57 47 61 46 --- 48
R02 | 916 37 40 17 12 18 34 26 --- 10 | 72 72 50 60 43 46 47 --- 51
R03 | 1148 52 61 26 16 28 26 53 39 14 | 88 94 53 60 41 42 48 75 50
R04 | 1023 54 60 38 12 37 30 38 --- 15 | 87 91 59 62 48 53 53 --- 53
R05 | 753 40 61 36 22 18 59 32 --- 14 | 68 75 46 55 44 44 41 --- 44
R06 | 1678 12 16 21 18 22 34 27 --- 10 | 45 55 47 64 44 63 64 --- 52
R07 | 1059 44 53 21 15 22 37 31 187 11 | 76 82 60 51 46 37 38 138 47
R08 | 871 46 53 19 17 25 40 32 --- 12 | 80 84 56 60 39 34 39 --- 47
R09 | 1588 19 21 21 14 10 28 20 --- 8 | 37 39 34 39 38 32 25 --- 32
R10 | 697 20 28 18 16 13 18 21 --- 7 | 68 72 48 64 52 40 57 --- 55
R11 | 1313 105 111 30 10 32 37 49 --- 19 | 70 174 27 39 87 76 48 --- 81
R13 | 580 29 29 22 19 19 33 34 --- 11 | 63 67 47 57 47 42 43 --- 47
R14 | 1710 32 27 55 32 30 56 57 --- 19 | 73 76 82 80 85 48 74 --- 70
R15 | 6930 37 25 18 25 39 42 34 --- 14 | 67 63 45 59 42 44 45 --- 46
XR17 | 3222 39 54 --- --- 15 34 30 --- 16 | 73 85 --- --- 57 45 43 --- 52
R18 | 505 25 30 16 23 18 35 34 --- 11 | 85 90 80 84 69 57 61 --- 72
R19 | 2258 29 32 25 13 27 48 16 --- 11 | 65 68 59 58 48 36 49 --- 50
R20 | 588 24 20 57 26 19 81 15 --- 17 | 62 67 64 64 48 31 43 --- 51
R21 | 692 30 25 14 15 14 23 24 143 8 | 73 74 64 68 56 49 44 84 58
R22 | 733 47 48 31 34 29 60 68 --- 19 | 81 82 68 73 48 29 60 --- 53
R23 | 602 21 22 18 33 21 25 29 --- 11 | 35 42 35 61 43 33 33 --- 38
R24 | 966 37 27 58 18 40 74 48 --- 20 | 58 62 69 57 32 38 36 --- 44
XR26 | ---- 91 75 --- --- --- --- 69 --- 79 | 73 132 --- --- --- --- 111 --- 61
------+---------------------------------------------------+-----------------------------------------------
RMS | 1867 42 48 31 20 25 44 38 137 |T 68 80 54 60 50 44 49 99 52
WRMS | 1867 43 45 33 19 22 39 38 137 |NE 68 80 54 60 50 44 49 99 52
MEDI | 916 37 32 21 17 21 35 32 143 |MD 72 75 56 60 47 42 46 84 51
Table 3.1886.1 GPS week: 1886 Day: 1 MJD: 57447
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 | 1247 82 85 29 18 34 34 18 --- 14 | 74 74 45 47 44 42 25 --- 35
R02 | 545 35 47 12 13 14 29 7 --- 7 | 56 61 49 43 34 50 39 --- 42
R03 | 1706 50 52 18 14 23 25 16 45 10 | 62 61 51 44 39 34 19 83 35
R04 | 930 50 46 23 19 27 25 8 --- 10 | 61 59 41 49 37 39 33 --- 38
R05 | 815 46 58 30 26 33 65 21 --- 15 | 49 51 35 42 40 24 39 --- 33
R06 | 2079 19 23 19 22 12 23 12 --- 8 | 42 40 36 56 39 41 54 --- 43
R07 | 688 44 42 24 9 18 34 15 249 9 | 64 58 53 41 41 47 35 145 39
R08 | 1008 47 47 26 19 28 23 20 --- 11 | 63 61 52 48 36 36 28 --- 37
R09 | 1124 17 21 19 16 18 18 13 --- 7 | 25 30 22 33 32 43 25 --- 24
R10 | 1953 23 17 27 19 27 23 9 --- 9 | 45 35 38 48 36 30 34 --- 36
R11 | 1057 113 110 43 26 29 30 22 --- 18 | 63 155 32 45 87 60 37 --- 70
R13 | 581 29 31 24 17 22 24 12 --- 9 | 47 50 37 37 34 28 32 --- 32
R14 | 2847 30 31 34 36 51 49 29 --- 16 | 66 68 56 69 56 53 58 --- 52
R15 | 3766 32 40 22 22 33 37 16 --- 11 | 51 61 43 45 52 43 43 --- 41
XR17 | 3522 45 48 27 --- 17 41 15 --- 13 | 50 49 51 --- 31 55 35 --- 37
R18 | 543 28 34 21 14 12 35 24 --- 9 | 51 54 48 44 51 39 37 --- 40
R19 | 1214 30 31 18 22 23 35 13 --- 9 | 49 53 47 46 32 25 31 --- 36
R20 | 639 40 36 44 30 28 53 14 --- 14 | 64 59 44 52 32 31 34 --- 36
R21 | 673 38 40 17 22 28 45 15 246 11 | 59 61 53 52 39 39 35 126 42
R22 | 1267 46 42 27 21 18 57 17 --- 12 | 56 51 44 41 31 24 30 --- 31
R23 | 530 12 16 34 32 18 90 17 --- 15 | 26 30 38 38 24 69 23 --- 26
R24 | 1290 37 57 47 25 44 64 20 --- 16 | 39 48 52 31 31 20 36 --- 26
XR26 | ---- 65 148 --- --- --- --- 16 --- 32 | 84 184 --- --- --- --- 50 --- 52
------+---------------------------------------------------+-----------------------------------------------
RMS | 1498 46 48 28 22 27 43 17 204 |T 54 63 43 45 39 39 35 118 38
WRMS | 1498 43 45 28 21 28 36 17 204 |NE 54 63 43 45 39 39 35 118 38
MEDI | 1057 38 42 24 21 23 34 16 246 |MD 56 58 44 45 36 39 35 126 37
Table 3.1886.2 GPS week: 1886 Day: 2 MJD: 57448
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 | 9533 71 58 30 23 27 37 21 --- 14 | 65 53 39 45 40 38 48 --- 29
R02 | 8589 32 29 16 18 29 17 9 --- 8 | 53 46 38 45 23 33 42 --- 32
R03 | 7731 45 49 29 12 17 24 13 114 9 | 63 65 47 36 35 36 29 113 33
R04 | 6691 51 60 15 9 17 37 8 --- 9 | 65 72 37 37 31 26 35 --- 33
R05 | 6941 58 41 22 19 26 54 19 --- 13 | 56 60 32 44 35 31 39 --- 35
R06 | 5388 14 18 17 19 18 26 20 --- 8 | 36 40 36 50 29 31 55 --- 39
R07 |10298 60 52 33 16 25 34 11 356 12 | 63 55 40 31 28 37 20 179 23
R08 | 8485 56 51 22 16 21 45 15 --- 11 | 61 57 39 33 29 32 33 --- 25
R09 | 9034 18 19 26 19 13 23 11 --- 8 | 32 38 30 41 38 30 32 --- 33
R10 | 8739 20 27 28 15 14 34 18 --- 9 | 60 72 50 59 47 51 60 --- 53
R11 | 6842 110 106 31 26 30 37 28 --- 18 | 69 203 35 47 101 84 40 --- 89
R13 | 8047 33 32 24 23 17 25 14 --- 9 | 53 52 40 42 38 39 30 --- 35
R14 |10740 37 45 42 33 41 61 34 --- 17 | 59 94 63 87 83 60 74 --- 67
R15 | 7829 28 33 33 25 20 41 15 --- 11 | 59 59 54 52 46 32 47 --- 42
XR17 | 6771 48 46 22 --- 24 28 10 --- 11 | 50 46 25 --- 29 37 37 --- 28
R18 | 5117 33 30 32 18 19 41 19 --- 11 | 58 55 58 49 39 32 38 --- 42
R19 | 5110 40 46 17 15 22 26 15 --- 9 | 52 54 41 38 39 28 31 --- 33
R20 | 7713 43 77 37 18 23 52 20 --- 13 | 60 88 62 44 31 39 29 --- 35
R21 | 6683 49 53 36 13 29 67 14 247 14 | 61 67 62 47 44 34 57 147 40
R22 | 7184 53 59 34 12 19 42 17 --- 11 | 70 75 58 42 42 28 44 --- 40
R23 |17584 16 18 21 25 10 42 15 --- 9 | 33 39 44 54 46 40 46 --- 39
R24 |14265 44 40 48 27 32 72 23 --- 16 | 56 47 79 40 37 36 65 --- 39
XR26 | ---- 63 297 --- --- --- --- 14 --- 30 | 44 309 --- --- --- --- 55 --- 46
------+---------------------------------------------------+-----------------------------------------------
RMS | 8974 48 49 30 20 23 42 18 259 |T 55 75 45 45 41 37 42 146 39
WRMS | 8974 41 43 30 19 20 39 18 259 |NE 55 75 45 45 41 37 42 146 39
MEDI | 7731 44 46 28 18 21 37 15 247 |MD 59 57 40 44 38 34 40 147 35
Table 3.1886.3 GPS week: 1886 Day: 3 MJD: 57449
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 | 3830 67 69 36 16 24 37 101 --- 19 | 78 90 49 59 62 62 63 --- 50
R02 | 5486 30 35 23 13 23 36 59 --- 12 | 64 65 62 57 46 56 28 --- 50
R03 | 4333 49 52 20 9 31 24 21 84 11 | 78 80 57 48 37 40 40 57 44
R04 | 4788 50 52 14 10 19 28 33 --- 10 | 78 82 45 55 46 47 42 --- 48
R05 | 2046 61 83 28 18 19 47 45 --- 14 | 67 88 42 49 42 48 44 --- 40
R06 | 3441 23 25 38 26 23 34 98 --- 18 | 52 49 49 69 48 46 120 --- 58
R07 | 3434 67 78 31 15 39 35 24 248 14 | 73 82 45 34 43 58 29 95 31
R08 | 3223 59 64 22 14 28 43 58 --- 14 | 72 79 46 42 48 51 45 --- 41
R09 | 5296 18 18 22 17 12 27 23 --- 8 | 42 48 43 53 39 36 34 --- 42
R10 | 5022 26 30 19 16 16 29 13 --- 8 | 76 75 62 65 48 45 54 --- 56
R11 | 2033 112 116 37 17 39 48 42 --- 20 | 63 186 30 40 105 50 41 --- 86
R13 | 2197 33 39 16 12 15 23 17 --- 7 | 58 64 49 47 42 47 40 --- 44
R14 | 2420 29 36 30 25 28 29 29 --- 12 | 71 72 68 82 65 63 79 --- 69
R15 | 6285 34 31 36 15 37 55 53 --- 15 | 72 67 67 69 80 54 44 --- 62
XR17 | 3155 39 44 28 --- 19 26 65 --- 17 | 65 69 46 --- 56 53 49 --- 49
R18 | 3345 27 32 22 9 29 34 15 --- 9 | 66 68 65 57 44 50 51 --- 53
R19 | 4691 35 29 14 18 15 32 27 --- 9 | 66 65 51 58 50 44 30 --- 49
R20 |14882 41 57 58 13 19 135 28 --- 22 | 56 68 61 48 43 82 39 --- 43
R21 | 3680 50 47 32 17 21 49 74 195 16 | 67 64 57 57 45 43 59 85 47
R22 | 3839 47 49 24 10 29 54 29 --- 13 | 70 71 57 52 43 30 48 --- 46
R23 | 6235 16 16 15 18 14 33 63 --- 11 | 45 45 41 53 48 65 47 --- 45
R24 | 2252 30 41 38 38 35 94 103 --- 23 | 78 85 90 85 68 48 75 --- 70
XR26 | ---- 33 290 --- --- --- --- 28 --- 31 | 61 258 --- --- --- --- 45 --- 54
------+---------------------------------------------------+-----------------------------------------------
RMS | 5160 48 53 29 18 26 51 53 188 |T 66 83 53 56 52 50 49 79 51
WRMS | 5160 39 42 28 18 22 43 53 188 |NE 66 83 53 56 52 50 49 79 51
MEDI | 3680 35 44 24 16 23 34 33 195 |MD 67 71 49 55 46 48 45 85 49
Table 3.1886.4 GPS week: 1886 Day: 4 MJD: 57450
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 | 801 87 75 21 21 37 37 128 --- 22 | 79 76 37 49 56 33 67 --- 34
R02 | 715 34 34 21 15 25 44 97 --- 16 | 57 62 48 55 50 31 40 --- 42
R03 | 2134 38 42 14 12 27 34 26 84 10 | 64 68 44 50 44 39 39 43 42
R04 | 630 48 47 13 14 25 24 29 --- 10 | 68 68 42 43 33 35 38 --- 38
R05 | 711 67 59 21 23 22 21 23 --- 13 | 69 70 27 47 50 27 54 --- 39
R06 | 1526 21 28 18 19 11 35 72 --- 12 | 55 60 39 66 55 43 100 --- 52
R07 | 1039 62 61 19 13 30 30 18 165 12 | 78 78 46 47 40 115 34 89 40
R08 | 974 59 64 25 17 35 29 78 --- 16 | 70 76 41 43 36 28 51 --- 33
R09 | 1766 17 19 16 18 12 22 25 --- 8 | 31 29 28 35 31 96 27 --- 25
R10 | 1001 28 31 15 22 11 29 17 --- 9 | 63 74 43 60 45 42 47 --- 47
XR11 | 1415 531 859 --- --- 58 99 26 --- 49 | 80 567 --- --- 301 204 61 --- 260
R13 | 702 34 24 13 16 20 23 19 --- 8 | 52 46 43 41 40 39 36 --- 37
R14 | 1120 26 31 29 30 40 32 27 --- 14 | 53 70 65 77 57 57 60 --- 60
R15 | 3985 34 45 18 27 25 29 38 --- 12 | 58 72 43 62 58 48 44 --- 47
XR17 | 991 35 34 19 --- 21 40 60 --- 16 | 58 57 45 --- 50 48 37 --- 44
R18 | 742 27 29 15 20 28 26 15 --- 10 | 59 62 48 58 45 43 43 --- 48
R19 | 892 46 56 25 20 31 54 27 --- 14 | 60 70 49 38 33 58 26 --- 38
R20 | 1250 33 45 25 27 19 48 39 --- 13 | 24 58 56 61 57 36 23 --- 44
R21 | 595 33 32 12 21 20 41 85 123 14 | 47 45 41 50 52 39 67 45 41
R22 | 1041 37 32 12 19 23 37 67 --- 13 | 57 52 49 56 45 36 66 --- 44
R23 | 1096 36 41 25 23 19 88 98 --- 20 | 34 40 30 31 31 70 73 --- 23
R24 | 1773 39 50 40 53 26 60 125 --- 24 | 66 78 44 71 46 47 68 --- 47
XR26 | ---- 27 847 --- --- --- --- 29 --- 28 | 46 734 --- --- --- --- 32 --- 35
------+---------------------------------------------------+-----------------------------------------------
RMS | 1439 44 45 21 23 25 40 64 128 |T 57 113 43 52 57 55 49 59 50
WRMS | 1439 38 40 22 23 21 35 64 128 |NE 57 113 43 52 57 55 49 59 50
MEDI | 1001 35 42 19 20 25 34 29 123 |MD 58 68 43 50 45 42 44 45 42
Table 3.1886.5 GPS week: 1886 Day: 5 MJD: 57451
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 | 1099 94 116 33 21 39 39 14 --- 17 | 69 87 20 36 39 40 55 --- 21
R02 | 817 37 44 16 17 16 39 15 --- 9 | 46 49 30 38 32 51 33 --- 29
R03 | 1769 44 43 30 13 29 64 18 83 13 | 48 45 37 33 35 47 25 52 24
R04 | 689 45 52 12 18 20 27 15 --- 9 | 43 46 21 31 28 24 22 --- 23
R05 | 773 59 58 21 30 27 31 23 --- 13 | 38 53 27 43 29 30 33 --- 27
R06 | 853 8 17 23 14 16 201 15 --- 8 | 38 46 31 41 33 157 48 --- 36
R07 | 920 56 59 18 12 25 341 13 93 11 | 58 59 28 31 26 229 19 97 24
R08 | 1082 54 54 23 17 21 22 14 --- 10 | 57 56 32 38 29 32 38 --- 27
R09 | 3128 16 22 16 15 15 276 13 --- 7 | 29 33 27 36 33 163 23 --- 26
R10 | 1249 27 31 26 26 13 36 18 --- 10 | 59 60 42 63 48 34 43 --- 45
R13 | 747 30 48 19 20 19 43 13 --- 9 | 42 57 34 40 34 37 26 --- 30
R14 | 596 21 33 33 29 28 32 23 --- 12 | 45 51 47 55 49 34 52 --- 44
R15 | 3237 47 54 11 17 37 19 13 --- 10 | 61 66 45 43 51 28 35 --- 36
XR17 | 803 30 37 18 --- 12 28 11 --- 9 | 45 48 36 --- 42 41 40 --- 38
R18 | 705 21 22 13 24 18 32 13 --- 8 | 50 52 39 57 44 33 42 --- 42
R19 | 871 28 32 25 23 16 44 20 --- 11 | 51 57 51 50 41 20 27 --- 37
R20 | 957 19 30 45 19 17 61 17 --- 13 | 34 50 66 33 36 30 29 --- 34
R21 | 778 32 28 24 20 15 51 21 99 11 | 50 48 55 55 50 40 53 24 43
R22 | 584 24 23 21 15 26 18 10 --- 8 | 49 51 50 45 66 57 50 --- 48
R23 | 1105 8 13 19 20 12 31 11 --- 7 | 22 27 27 27 31 28 47 --- 19
R24 | 945 42 43 27 32 33 52 20 --- 14 | 52 56 40 48 35 25 76 --- 31
XR26 | ---- 30 188 --- --- --- --- 9 --- 16 | 38 288 --- --- --- --- 23 --- 25
------+---------------------------------------------------+-----------------------------------------------
RMS | 1356 41 47 24 21 23 114 16 92 |T 46 62 37 42 38 56 38 57 32
WRMS | 1356 34 39 24 20 20 41 16 92 |NE 46 62 37 42 38 56 38 57 32
MEDI | 871 30 37 21 19 19 39 14 93 |MD 46 51 36 40 35 34 35 52 30
Table 3.1886.6 GPS week: 1886 Day: 6 MJD: 57452
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 | 1112 81 82 27 13 31 33 12 --- 13 | 85 86 36 30 43 32 28 --- 29
R02 | 797 39 40 21 15 29 96 14 --- 14 | 62 65 45 44 36 29 25 --- 36
R03 | 1413 52 56 18 11 31 36 14 128 10 | 76 79 51 41 30 36 36 90 37
R04 | 797 40 32 15 13 20 24 12 --- 8 | 78 76 42 51 35 36 38 --- 42
R05 | 641 46 54 27 23 32 76 24 --- 15 | 64 78 31 55 40 36 44 --- 40
R06 | 1206 13 11 19 26 17 39 10 --- 9 | 56 61 51 81 51 68 74 --- 60
R07 | 1011 51 50 23 11 20 26 19 67 10 | 84 85 47 44 29 96 32 144 37
R08 | 731 52 52 21 19 27 31 18 --- 11 | 79 83 52 54 42 34 40 --- 43
R09 | 3250 20 20 17 16 18 22 17 --- 8 | 32 34 27 41 37 85 32 --- 32
R10 | 1895 26 26 26 18 15 31 10 --- 8 | 71 73 43 69 54 49 59 --- 57
R13 | 805 31 32 26 16 16 41 12 --- 9 | 61 61 48 45 41 36 42 --- 42
R14 | 669 27 21 31 24 22 39 20 --- 11 | 70 80 75 84 66 54 77 --- 72
R15 | 4571 41 38 20 14 37 61 16 --- 12 | 71 73 48 55 51 49 43 --- 46
XR17 | 1325 43 43 28 --- 23 57 7 --- 14 | 70 70 49 --- 40 54 37 --- 47
R18 | 728 26 32 18 13 19 40 6 --- 8 | 66 69 57 58 43 40 49 --- 50
R19 | 529 18 15 26 19 18 33 19 --- 9 | 67 67 66 62 44 42 41 --- 51
R20 | 1422 40 57 21 27 26 44 23 --- 12 | 67 76 54 52 41 43 37 --- 44
R21 | 1900 34 38 24 12 17 45 20 101 10 | 74 76 73 64 49 33 37 88 53
R22 | 746 40 42 24 14 15 31 22 --- 10 | 74 71 67 56 48 34 41 --- 50
R23 | 1038 14 19 20 22 19 29 16 --- 8 | 36 37 29 47 43 28 27 --- 32
R24 | 1831 39 35 42 16 19 57 30 --- 14 | 67 64 59 58 34 30 50 --- 43
XR26 | ---- 31 878 --- --- --- --- 6 --- 15 | 47 800 --- --- --- --- 37 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1666 40 41 24 18 23 45 17 102 |T 66 102 50 54 42 44 42 107 44
WRMS | 1666 35 36 24 18 17 37 17 102 |NE 66 102 50 54 42 44 42 107 44
MEDI | 1038 39 38 23 16 20 39 16 101 |MD 67 73 49 54 42 36 38 90 43
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