[IGSREPORT-26005] Wk 2006 IGLOS Final Orbits
acc
acc at igs.org
Sun Jul 8 17:08:24 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2006 (Jun 17, 2018 - Jun 23, 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 2.2006.
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:
igl2006[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2006 in the SP3 format.
igl20067.sum Combination Report for GPS Week 2006.
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 | 1.1 ns
1 | 2.6 ns
2 | 2.2 ns
3 | 5.4 ns
4 | 3.6 ns
5 | 4.4 ns
6 | 1.8 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
----+--------+---------------
2 | GRG | R05
3 | GRG | R05
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 1.2006, 1a.2006).
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 2.2006.0-6)
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 3.2006.0-6).
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 2006 summary. (Jun 17, 2018 - Jun 23, 2018)
Table 1.2006.a GPS week : 2006 MJD: 58286.0-58292.0
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 -3 12 -44 -5 .17 26 28 | 8811 -944 3605 10511
| 1 1 1 17 23 17 .07 | 1434 2133
cof n/a| 0 0 -4 12 -26 -7 .14 29 30 | 8802 -945 3608 10515
| 1 1 1 8 24 27 .09 | 1424 2131
emx n/a| -1 0 6 13 -8 -7 .03 27 27 | -5506 -520 3493 9844
| 1 1 1 21 27 39 .02 | 10393 1028
esx n/a| 0 0 0 12 30 7 .09 17 15 | 6435 -1332 3527 12572
| 1 0 1 25 15 14 .07 | 9768 2313
gfz n/a| 0 1 3 0 24 37 -.06 26 20 | 0 -904 3514 10235
| 1 1 1 25 18 27 .06 | 0 2049
grg n/a| 0 -1 -2 -38 -14 -86 -.31 33 25 | 289240 -143488 3516 9578
| 1 0 4 22 16 75 .09 | 756541 377690
iac n/a| 1 0 0 -4 -18 26 -.08 24 22 | 4409 -821 4414 10714
| 0 1 3 32 33 61 .03 | 1655 1412
mcc n/a| 0 -4 -22 7 -26 1192 -.36 176 176 | --- --- --- ---
| 4 8 12 109 131 332 .36 | --- ---
Table 1.2006.b GPS week : 2006 MJD: 58286.0-58292.0
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 | 20 16 16 16 15 21 20 |
R02 | 9 6 6 7 6 5 5 |
R03 | 8 7 5 5 6 6 5 |
R04 | 7 7 8 8 5 10 7 |
R05 | 20 24 30 29 27 24 22 |
R07 | 6 6 5 5 7 7 7 |
R08 | 7 7 7 7 8 10 6 |
R09 | 7 6 7 6 7 6 7 |
R10 | 10 8 8 9 9 7 8 |
R11 | 7 7 7 7 9 6 7 |
R13 | 9 8 7 8 8 8 9 |
R14 | 9 8 7 7 8 8 9 |
R15 | 11 12 10 10 11 12 13 |
R16 | 16 16 16 14 10 13 14 |
R17 | 10 9 9 10 10 10 10 |
R18 | 7 7 8 8 8 9 6 |
R19 | 15 16 15 13 16 15 16 |
R20 | 13 12 15 14 14 15 19 |
R21 | 10 10 10 10 10 9 10 |
R22 | 10 9 9 9 11 10 11 |
R23 | 11 11 11 11 11 11 11 |
R24 | 16 14 17 24 17 17 18 |
R26 | 23 22 15 17 25 21 27 |
Table 1.2006.c GPS week : 2006 MJD: 58286.0-58292.0
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 2006 0 | 29 -31 205 1346 163 5406 83.8 1653 1653 | 1119 0
brd 2006 1 | 45 -36 242 954 92 4446 85.7 1698 1698 | 2577 0
brd 2006 2 | -21 50 176 -66 -29 5979 87.3 1797 1797 | 2171 0
brd 2006 3 | -71 -9 229 -664 -627 3791 83.7 1418 1418 | 5364 0
brd 2006 4 | -60 -8 139 -1012 -619 375 83.1 1564 1564 | 3587 0
brd 2006 5 | 93 0 234 1217 933 -66 84.8 1822 1822 | 4403 0
brd 2006 6 | 40 -11 229 1523 -854 3002 84.6 1711 1711 | 1808 0
-------------+------------------------------------------------------------+----------------
brd 2006 mean| 7 -6 208 471 -134 3276 84.7 1666 1666 | 3004 0
brd 2006 sdev| 60 28 37 1035 617 2350 1.4 139 139 | 1512 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 2.2006.0 GPS week: 2006 Day: 0 MJD: 58286
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 37 -28 -11 .26 26 28 | 10541 -2880 3347 10145
cof n/a| 1 -1 -5 26 -8 -4 -.01 26 27 | 10522 -2890 3360 10159
emx n/a| -2 0 6 10 26 4 .02 24 24 | 14587 -1758 3363 9296
esx n/a| 0 1 0 -11 17 16 -.03 19 16 | 14816 -2971 3361 12699
gfz n/a| 0 2 6 -26 8 61 .03 25 17 | 0 -2855 3370 9980
grg n/a| 0 0 -3 -53 -7 -101 -.17 35 28 | 2485 -2745 3334 9683
iac n/a| 0 0 -4 30 -23 -8 -.09 24 23 | 3103 -1236 4217 9713
mcc n/a| -1 -11 -19 32 -87 1213 -.32 144 144 | --- --- --- ---
Table 2.2006.1 GPS week: 2006 Day: 1 MJD: 58287
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 -8 -88 -3 .23 26 28 | 10403 -1278 3065 10850
cof n/a| -1 2 -6 6 -62 -30 .25 31 33 | 10389 -1258 3064 10853
emx n/a| -2 0 7 53 4 -69 .05 27 27 | -10880 -648 3077 10313
esx n/a| -1 0 0 22 26 5 .01 17 13 | -4102 -3639 3066 12558
gfz n/a| 0 1 5 38 38 9 -.13 26 19 | 0 -1062 3076 10622
grg n/a| -1 -1 0 -51 -7 54 -.33 33 23 | 2004915 -999999 3069 9845
iac n/a| 2 0 -2 -27 13 -47 -.06 25 20 | 3007 -1327 4588 13730
mcc n/a| 0 -7 -25 131 194 1287 -.92 227 227 | --- --- --- ---
Table 2.2006.2 GPS week: 2006 Day: 2 MJD: 58288
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 -2 17 -41 6 .08 25 27 | 8875 -2655 3273 10310
cof n/a| 0 -1 -2 14 -22 -26 .21 28 29 | 8855 -2636 3278 10319
emx n/a| -1 -3 7 10 -13 -44 -.01 24 24 | -12970 -1486 3274 9416
esx n/a| 1 0 -1 0 9 23 .18 18 14 | 5374 -3507 3283 12814
gfz n/a| 1 1 2 25 18 37 -.05 24 20 | 0 -2585 3311 10187
grg n/a| 0 0 -1 -61 8 -78 -.25 25 22 | 3187 -1901 3278 9178
iac n/a| 0 0 -1 28 2 66 -.09 23 23 | 2191 -19 4141 11031
mcc n/a| 5 7 -31 91 -11 954 -.30 137 137 | --- --- --- ---
Table 2.2006.3 GPS week: 2006 Day: 3 MJD: 58289
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 -6 16 -23 1 .15 26 27 | 6281 2704 3892 11763
cof n/a| -1 1 -6 17 0 41 .15 27 27 | 6293 2679 3899 11772
emx n/a| 1 -2 9 27 13 0 .00 25 25 | -13160 971 3925 11471
esx n/a| -1 0 1 -3 42 -17 .11 17 16 | 13529 -120 3908 13884
gfz n/a| 0 2 4 -13 9 38 -.05 25 21 | 0 1592 3966 11719
grg n/a| -1 -1 -2 -53 -1 -48 -.28 22 22 | 3899 1543 3888 10977
iac n/a| 0 0 -3 12 -42 61 -.06 17 16 | 6481 260 4504 11450
mcc n/a| -5 -8 -22 21 -102 1482 .16 161 161 | --- --- --- ---
Table 2.2006.4 GPS week: 2006 Day: 4 MJD: 58290
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 -2 28 -33 4 .10 24 28 | 8291 -569 3770 10200
cof n/a| 0 0 -4 13 -58 -38 .05 30 29 | 8297 -588 3767 10195
emx n/a| -1 0 6 10 -3 25 .04 29 29 | 2729 -141 3734 9631
esx n/a| 0 0 -1 -7 22 -5 .13 17 15 | -5468 1107 3719 11722
gfz n/a| 0 0 1 7 8 57 -.01 28 22 | 0 -928 3676 9642
grg n/a| 0 -2 1 -18 -35 -140 -.37 43 29 | 3260 324 3681 9094
iac n/a| 0 0 0 -39 -5 11 -.13 25 19 | 4859 -223 4083 9714
mcc n/a| 0 4 -16 -59 57 1555 -.47 228 228 | --- --- --- ---
Table 2.2006.5 GPS week: 2006 Day: 5 MJD: 58291
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 -5 -9 -30 -40 .16 28 30 | 8858 916 3247 9950
cof n/a| 0 0 -4 -2 -9 3 .14 31 32 | 8838 940 3245 9954
emx n/a| -3 1 4 -9 -44 45 .02 29 29 | -8269 545 3156 9289
esx n/a| 1 0 0 56 50 11 .13 17 15 | 1342 2013 3146 12109
gfz n/a| -2 0 2 -26 36 67 -.09 25 17 | 0 2147 3002 9718
grg n/a| 2 0 -3 0 -33 -104 -.44 36 27 | 3618 1328 3188 9277
iac n/a| 1 0 3 -44 2 -25 -.04 23 23 | 6092 415 3572 9317
mcc n/a| 4 0 0 -200 -14 1278 -.03 203 203 | --- --- --- ---
Table 2.2006.6 GPS week: 2006 Day: 6 MJD: 58292
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 0 4 -62 7 .23 28 29 | 8433 -2847 4642 10362
cof n/a| 0 0 -1 12 -23 1 .16 32 30 | 8421 -2867 4645 10357
emx n/a| 0 0 3 -7 -44 -18 .06 31 31 | -10581 -1123 3922 9492
esx n/a| 0 0 1 30 46 19 .08 17 15 | 19559 -2208 4206 12219
gfz n/a| 1 -1 2 0 53 -7 -.13 26 24 | 0 -2641 4197 9781
grg n/a| 0 -1 -11 -29 -23 -183 -.35 37 27 | 3321 -2968 4178 8997
iac n/a| 0 -3 3 8 -80 129 -.07 29 30 | 5131 -3623 5796 10047
mcc n/a| -7 -13 -41 36 -223 580 -.63 129 129 | --- --- --- ---
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 3.2006.0 GPS week: 2006 Day: 0 MJD: 58286
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 | 1816 35 30 55 29 42 54 49 --- 19 | 41 38 29 64 84 65 69 --- 51
R02 | 772 12 24 25 19 14 24 13 192 8 | 54 60 49 66 65 54 59 185 56
R03 | 1016 9 10 12 23 15 17 17 140 7 | 61 61 60 71 65 63 59 83 62
R04 | 892 15 12 13 14 18 26 10 --- 7 | 48 50 51 61 50 5 51 --- 53
R05 | 1016 38 22 38 34 28 86 42 --- 20 | 43 48 52 65 43 55 61 --- 48
R07 | 1258 12 15 8 13 15 9 14 159 5 | 51 50 56 56 62 53 55 104 54
R08 | 986 13 16 9 15 16 14 18 --- 6 | 45 47 51 48 52 54 44 --- 47
R09E | 3763 14 11 12 11 14 26 22 --- 7 | 38 40 40 42 47 51 41 --- 41
R10E | 1114 10 14 24 11 22 23 30 --- 9 | 101 102 91 105 112 96 116 --- 103
R11E | 1131 9 18 18 12 15 20 11 140 6 | 38 43 35 46 36 36 35 73 37
R13E | 2555 18 26 25 10 17 29 15 --- 8 | 114 118 111 117 116 111 113 --- 113
R14E | 2214 17 10 22 15 22 25 13 --- 8 | 72 72 69 71 72 77 67 --- 70
R15E | 3340 31 35 21 16 26 33 18 --- 10 | 63 60 65 59 69 71 61 --- 61
R16E | 562 26 25 36 19 38 57 36 --- 15 | 53 57 42 41 45 60 58 --- 43
R17 | 1648 35 34 18 9 22 21 16 --- 9 | 62 63 42 41 30 44 34 --- 40
R18 | 885 13 15 19 14 23 13 10 --- 7 | 51 52 42 54 41 44 50 --- 46
R19 | 1002 51 51 27 12 34 45 28 --- 15 | 76 77 36 32 36 61 28 --- 35
R20 | 1419 37 23 27 22 28 23 29 --- 12 | 52 59 41 54 51 41 41 --- 40
R21 | 1191 34 35 13 17 25 17 16 45 9 | 75 74 47 56 43 49 47 51 50
R22 | 956 35 32 17 10 27 23 9 --- 9 | 53 52 27 28 28 39 32 --- 30
R23 | 980 31 27 22 24 11 25 25 --- 10 | 32 34 36 57 43 34 57 --- 43
R24 | 1182 29 34 23 31 39 56 30 --- 15 | 48 58 44 59 52 55 58 --- 48
XR26 | 3615 25 70 --- --- --- --- 21 --- 23 | 28 69 --- --- --- --- 44 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1653 26 26 24 19 25 35 24 144 |T 56 60 50 58 56 55 55 99 52
WRMS | 1653 28 27 24 16 17 28 23 144 |NE 51 55 44 54 49 47 49 105 45
MEDI | 1131 25 24 21 15 22 24 18 140 |MD 52 58 44 56 50 54 55 83 48
Table 3.2006.1 GPS week: 2006 Day: 1 MJD: 58287
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 | 2632 37 34 56 11 29 34 40 --- 15 | 27 36 40 46 63 41 52 --- 40
R02 | 1296 9 17 23 13 11 14 12 349 6 | 40 48 31 43 46 46 45 181 40
R03 | 700 13 16 13 13 15 22 11 214 6 | 48 52 46 47 53 64 47 142 49
XR04 | 1071 11 11 11 14 15 --- 15 --- 6 | 38 39 40 39 42 --- 41 --- 38
R05 | 1743 31 41 37 41 30 95 70 --- 24 | 30 43 38 62 80 96 41 --- 41
R07 | 911 9 14 18 13 12 17 9 228 6 | 39 36 48 47 45 41 37 134 42
R08 | 795 13 16 16 15 25 14 11 --- 7 | 34 33 35 30 26 34 33 --- 27
R09E | 2677 15 19 14 9 16 14 17 --- 6 | 26 25 23 28 33 23 35 --- 26
R10E | 1057 17 14 18 11 22 21 14 --- 7 | 76 75 78 81 80 82 88 --- 80
R11E | 981 9 14 22 10 22 20 13 182 7 | 33 33 29 33 33 32 27 96 29
R13E | 3321 15 16 22 12 14 28 9 --- 7 | 81 81 75 81 79 90 80 --- 80
R14E | 1255 19 15 18 11 21 19 12 --- 7 | 55 51 43 52 52 56 51 --- 50
R15E | 3180 28 28 29 21 33 29 12 --- 11 | 51 52 43 54 53 55 42 --- 47
R16E | 618 27 37 46 25 46 44 33 --- 16 | 32 50 34 58 61 47 38 --- 40
R17 | 1058 34 37 18 8 24 15 14 --- 8 | 37 37 29 25 22 23 21 --- 23
R18 | 1340 10 21 18 8 20 22 11 --- 6 | 32 43 27 36 29 44 33 --- 31
R19 | 1185 60 63 32 18 35 34 28 --- 15 | 50 53 31 26 30 37 20 --- 23
R20 | 982 28 60 28 25 30 29 27 --- 12 | 33 52 34 35 29 20 33 --- 23
R21 | 1642 34 35 18 11 22 30 21 67 10 | 49 52 35 42 34 37 36 40 35
R22 | 827 30 36 18 9 25 19 12 --- 8 | 33 39 24 30 24 26 28 --- 25
R23 | 864 26 31 26 23 13 29 19 --- 10 | 27 27 32 46 41 28 43 --- 35
R24 | 2280 25 23 25 19 42 41 35 --- 13 | 61 72 54 51 55 72 63 --- 57
XR26 | 3272 24 70 --- --- --- --- 18 --- 21 | 27 69 --- --- --- --- 38 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1698 26 31 27 17 26 33 25 227 |T 41 47 39 45 45 47 42 118 39
WRMS | 1698 28 33 27 13 19 23 20 227 |NE 37 45 36 40 41 43 38 124 34
MEDI | 1185 24 23 18 13 22 22 14 214 |MD 37 48 35 43 42 41 38 134 38
Table 3.2006.2 GPS week: 2006 Day: 2 MJD: 58288
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 | 2295 24 44 47 20 44 32 43 --- 16 | 30 35 34 39 68 26 52 --- 34
R02 | 1888 15 15 13 11 12 15 9 172 5 | 40 47 45 51 47 54 42 182 46
R03 | 1980 9 12 14 11 9 11 15 190 5 | 48 52 53 59 52 58 49 102 52
XR04 | 1076 15 21 15 15 11 --- 17 --- 7 | 41 42 41 59 50 --- 42 --- 46
XR05 | 851 43 56 67 52 --- 162 42 --- 30 | 49 63 36 78 --- 68 76 --- 55
R07 | 889 10 15 9 10 6 13 15 112 5 | 45 48 52 46 48 52 50 143 47
R08 | 576 15 19 15 8 16 17 23 --- 7 | 39 42 43 39 31 40 34 --- 36
R09E | 3342 15 18 13 13 13 11 23 --- 6 | 19 19 16 18 22 19 25 --- 16
R10E | 730 12 16 21 9 17 26 24 --- 8 | 76 80 65 79 83 83 83 --- 77
R11E | 1142 6 19 19 11 20 18 11 100 6 | 32 39 32 36 35 32 29 111 30
R13E | 2534 9 15 15 11 22 15 18 --- 7 | 69 67 74 73 81 69 73 --- 72
R14E | 821 15 16 21 12 15 18 14 --- 7 | 43 46 35 44 38 42 40 --- 38
R15E | 3646 26 25 25 11 31 18 14 --- 9 | 47 52 41 44 49 40 37 --- 40
R16E | 647 26 32 49 25 33 36 38 --- 15 | 42 47 39 38 45 32 42 --- 29
R17 | 772 32 33 20 14 26 12 11 --- 9 | 49 51 37 41 28 33 37 --- 36
R18 | 1524 14 10 16 16 14 22 17 --- 7 | 48 49 44 53 44 31 54 --- 44
R19 | 942 57 64 30 17 33 25 26 --- 14 | 63 70 40 37 33 39 27 --- 34
R20 | 838 31 28 26 26 33 42 36 --- 14 | 31 37 30 41 41 41 36 --- 24
R21 | 1847 36 38 19 11 25 19 20 80 9 | 57 60 39 44 36 35 45 56 40
R22 | 1047 36 28 17 9 24 12 20 --- 9 | 43 35 26 29 23 25 25 --- 24
R23 | 619 21 20 19 29 9 33 18 --- 10 | 34 38 32 55 36 21 42 --- 36
R24 | 2730 34 36 19 39 39 58 32 --- 17 | 48 54 39 50 43 50 47 --- 39
XR26 | 3587 13 36 --- --- --- --- 15 --- 14 | 25 46 --- --- --- --- 24 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1796 25 28 24 18 24 25 23 137 |T 44 48 40 47 44 42 43 118 39
WRMS | 1796 27 29 24 14 20 22 23 137 |NE 43 48 39 48 41 40 42 120 38
MEDI | 1076 15 21 19 12 20 18 18 112 |MD 43 47 39 44 43 40 42 111 38
Table 3.2006.3 GPS week: 2006 Day: 3 MJD: 58289
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 | 1126 38 35 62 31 31 22 23 --- 16 | 26 59 31 78 73 50 54 --- 50
R02 | 1315 19 21 16 9 22 14 9 255 6 | 40 39 52 52 53 44 44 106 45
R03 | 2062 15 12 10 11 11 9 9 177 5 | 49 48 56 60 56 53 49 53 53
XR04 | 2450 10 13 12 16 17 --- 17 --- 7 | 40 39 46 28 34 --- 42 --- 36
XR05 | 601 36 40 81 33 --- 156 42 --- 28 | 62 77 61 75 --- 73 76 --- 60
R07 | 716 11 12 13 7 14 7 13 119 5 | 51 55 53 50 61 56 52 72 52
R08 | 545 13 13 15 8 14 20 20 --- 7 | 43 44 52 53 52 65 44 --- 50
R09E | 3388 19 17 13 8 17 15 13 --- 6 | 17 19 15 20 25 21 21 --- 17
R10E | 1700 18 19 29 17 22 18 16 --- 9 | 72 76 66 70 74 68 72 --- 69
R11E | 964 9 9 18 19 18 9 17 115 7 | 21 17 20 26 19 17 16 85 17
R13E | 2012 16 16 17 15 23 17 20 --- 8 | 43 40 41 50 53 44 43 --- 44
R14E | 670 18 17 19 12 19 10 12 --- 6 | 32 33 26 37 42 30 33 --- 31
R15E | 2019 23 20 30 15 28 22 15 --- 9 | 31 31 27 37 43 31 29 --- 28
R16E | 624 29 29 29 24 41 31 28 --- 13 | 42 45 34 46 57 40 45 --- 36
R17 | 933 33 36 23 12 29 26 14 --- 10 | 49 52 25 32 16 39 22 --- 28
R18 | 770 17 18 26 19 17 16 15 --- 8 | 44 44 38 53 35 38 53 --- 43
R19 | 836 53 46 28 16 31 25 21 --- 13 | 70 65 35 36 26 47 25 --- 33
R20 | 815 30 30 27 24 43 44 22 --- 14 | 36 51 27 44 51 35 38 --- 30
R21 | 844 34 44 21 13 29 23 19 77 10 | 51 59 34 32 27 38 27 42 29
R22 | 1279 35 39 18 8 22 16 15 --- 8 | 49 51 26 29 23 30 25 --- 27
R23 | 821 23 26 19 28 16 33 17 --- 10 | 24 24 32 53 38 18 36 --- 32
XR24 | 2698 25 48 56 40 --- 67 42 --- 24 | 66 103 93 76 --- 91 58 --- 72
XR26 | 3819 21 48 --- --- --- --- 13 --- 17 | 17 47 --- --- --- --- 28 --- 23
------+---------------------------------------------------+-----------------------------------------------
RMS | 1417 26 27 25 17 25 22 17 161 |T 42 48 40 47 42 44 40 71 39
WRMS | 1417 27 27 25 16 21 22 16 161 |NE 44 53 44 50 41 48 42 68 41
MEDI | 964 21 21 19 15 22 20 17 119 |MD 43 47 34 46 42 40 42 72 36
Table 3.2006.4 GPS week: 2006 Day: 4 MJD: 58290
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 | 906 15 50 52 23 34 57 29 --- 15 | 40 40 35 47 56 57 47 --- 40
R02 | 860 12 12 8 12 14 11 16 421 5 | 39 40 43 41 40 46 46 247 40
R03 | 895 9 12 6 13 10 28 12 180 6 | 45 48 47 41 44 68 53 56 46
XR04 | 1941 7 8 7 10 8 --- 10 --- 4 | 38 42 40 46 43 --- 36 --- 40
R05 | 688 32 33 64 23 57 126 74 --- 27 | 63 81 56 83 49 63 88 --- 62
R07 | 1294 10 11 14 14 18 16 17 167 6 | 50 51 54 55 58 50 43 71 51
R08 | 496 15 16 19 16 9 25 19 --- 7 | 39 40 42 58 52 61 49 --- 49
R09E | 3203 14 13 21 11 16 13 11 --- 6 | 16 15 20 25 27 24 22 --- 19
R10E | 2977 15 16 28 14 20 25 18 --- 8 | 54 55 57 53 53 54 45 --- 50
R11E | 759 8 13 25 16 21 29 19 129 8 | 25 32 30 34 30 27 24 74 26
R13E | 1472 14 14 18 12 21 31 11 --- 7 | 56 58 59 59 61 63 52 --- 56
R14E | 766 12 11 25 10 20 23 16 --- 7 | 43 43 38 47 49 53 48 --- 43
R15E | 3588 30 37 24 17 32 29 17 --- 11 | 40 47 45 48 47 47 34 --- 39
R16E | 634 17 30 23 14 25 31 29 --- 10 | 31 49 33 39 42 47 48 --- 35
R17 | 944 32 32 16 9 30 32 19 --- 10 | 47 48 28 27 22 46 20 --- 27
R18 | 744 13 15 22 18 23 18 11 --- 8 | 40 44 36 45 42 38 44 --- 39
R19 | 1232 56 63 27 21 42 32 20 --- 15 | 62 69 34 34 37 40 23 --- 31
R20 | 815 31 30 32 21 40 47 24 --- 13 | 41 43 35 36 41 35 33 --- 31
R21 | 1085 30 27 20 9 30 16 22 74 9 | 52 51 43 42 42 42 29 32 39
R22 | 1028 38 40 20 12 36 24 14 --- 11 | 51 52 28 30 27 40 30 --- 31
R23 | 637 29 26 19 29 13 34 12 --- 11 | 25 30 33 50 37 21 38 --- 33
R24 | 2140 19 47 49 25 28 77 33 --- 16 | 34 47 57 53 49 39 46 --- 36
XR26 | 3283 24 41 --- --- --- --- 25 --- 25 | 16 51 --- --- --- --- 48 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1563 24 30 29 17 28 43 25 228 |T 41 46 40 45 43 45 41 96 38
WRMS | 1563 28 29 29 15 22 29 19 228 |NE 42 48 40 45 42 46 42 101 39
MEDI | 944 15 26 21 14 21 29 18 167 |MD 40 47 38 45 42 46 44 71 39
Table 3.2006.5 GPS week: 2006 Day: 5 MJD: 58291
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 | 1062 33 44 75 19 38 56 50 --- 20 | 34 55 26 38 46 50 51 --- 28
R02 | 644 11 14 12 9 10 14 15 --- 5 | 36 38 33 33 27 35 33 --- 31
R03 | 664 12 18 11 8 17 23 12 224 6 | 41 43 43 38 37 48 47 98 40
XR04 | 1177 18 13 17 21 20 --- 17 --- 9 | 35 36 41 32 31 --- 36 --- 30
R05 | 841 32 43 55 12 38 115 42 --- 23 | 40 39 43 54 55 40 65 --- 45
R07 | 1200 17 19 14 12 20 24 9 295 7 | 37 36 41 53 59 34 47 170 45
R08 | 640 22 17 15 23 17 30 19 --- 9 | 32 38 45 64 58 39 43 --- 46
R09E | 3369 13 10 19 9 13 14 12 --- 6 | 22 24 30 26 32 22 24 --- 24
R10E | 2730 17 16 21 11 14 15 20 --- 7 | 82 83 74 79 78 88 91 --- 81
R11E | 1000 10 9 21 11 14 16 13 155 6 | 30 29 28 32 29 27 30 80 28
R13E | 1237 13 12 17 15 18 29 17 --- 8 | 72 69 65 69 68 75 73 --- 68
R14E | 729 16 15 21 17 18 20 15 --- 8 | 53 53 53 58 56 54 56 --- 53
R15E | 5430 27 36 29 23 28 37 20 --- 12 | 48 50 52 43 50 50 46 --- 43
R16E | 844 22 27 28 26 40 28 27 --- 13 | 27 37 30 42 58 27 36 --- 28
R17 | 1575 35 37 16 6 21 22 22 --- 9 | 41 43 25 29 26 38 28 --- 27
R18 | 842 17 22 20 25 16 25 16 --- 9 | 37 44 34 39 37 41 41 --- 35
R19 | 1018 65 66 26 25 30 14 20 --- 15 | 54 56 34 40 34 24 28 --- 30
R20 | 809 40 48 30 23 38 33 35 --- 14 | 57 65 45 40 34 45 39 --- 37
R21 | 1814 29 25 15 10 29 15 16 56 8 | 68 68 62 64 56 59 58 41 60
R22 | 1085 37 42 15 8 30 20 15 --- 9 | 41 48 28 27 26 26 24 --- 25
R23 | 636 21 21 29 26 9 25 22 --- 10 | 26 29 34 39 29 20 35 --- 29
XR24 | 1118 27 29 33 37 --- 35 37 --- 17 | 28 37 35 46 --- 42 41 --- 28
XR26 | 5797 23 94 --- --- --- --- 18 --- 20 | 19 62 --- --- --- --- 32 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1821 28 31 29 17 25 36 23 203 |T 41 47 40 44 44 42 43 97 38
WRMS | 1821 30 32 29 15 17 27 23 203 |NE 39 46 37 42 39 38 40 103 35
MEDI | 1062 22 22 20 15 20 24 18 155 |MD 37 43 35 40 37 40 41 80 31
Table 3.2006.6 GPS week: 2006 Day: 6 MJD: 58292
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 | 892 45 51 79 27 19 31 57 --- 20 | 65 71 36 62 72 54 75 --- 51
R02 | 1021 7 7 8 11 16 10 12 108 5 | 49 55 48 59 48 54 57 154 52
R03 | 1287 7 10 12 8 12 17 14 110 5 | 57 60 63 59 60 69 66 114 61
XR04 | 911 7 14 11 9 17 --- 22 --- 6 | 51 53 56 51 51 --- 63 --- 53
R05 | 977 22 52 69 20 25 101 43 --- 22 | 42 65 27 47 37 47 53 --- 32
R07 | 1427 14 17 10 8 21 16 17 220 6 | 60 57 65 64 79 56 70 106 64
R08 | 658 11 15 16 10 10 15 19 --- 6 | 50 52 67 60 59 56 55 --- 57
R09E | 4223 12 17 16 11 21 18 16 --- 7 | 33 35 36 40 42 33 34 --- 35
R10E | 2594 18 17 26 10 14 14 28 --- 8 | 88 89 85 94 92 102 103 --- 93
R11E | 1043 9 11 20 10 21 11 14 60 6 | 39 38 38 43 40 41 40 140 39
R13E | 1894 10 11 27 14 18 25 25 --- 8 | 110 117 116 115 114 110 107 --- 111
R14E | 617 9 9 28 13 20 16 29 --- 8 | 74 72 70 70 68 74 65 --- 69
R15E | 3661 22 31 28 14 38 40 29 --- 12 | 67 68 70 63 76 74 53 --- 63
R16E | 744 23 43 25 23 33 46 36 --- 13 | 57 65 44 50 56 42 44 --- 43
R17 | 1767 35 41 20 11 25 15 23 --- 10 | 61 65 34 34 27 37 33 --- 34
R18 | 745 17 18 17 9 13 13 16 --- 6 | 51 51 44 50 43 40 48 --- 45
R19 | 1138 57 50 24 24 41 31 29 --- 16 | 84 79 39 48 40 55 32 --- 43
R20 | 1001 51 58 33 27 44 67 36 --- 19 | 71 77 45 40 36 72 46 --- 42
R21 | 1431 33 36 15 8 30 18 22 90 9 | 96 99 76 86 69 83 69 65 79
R22 | 907 35 31 18 7 33 28 23 --- 11 | 67 65 36 37 21 49 36 --- 37
R23 | 722 26 25 30 28 10 21 19 --- 11 | 35 37 40 64 48 35 61 --- 47
R24 | 1273 34 39 24 29 38 65 53 --- 18 | 39 59 53 73 66 62 41 --- 51
XR26 | 3938 21 56 --- --- --- --- 33 --- 27 | 22 50 --- --- --- --- 39 --- 27
------+---------------------------------------------------+-----------------------------------------------
RMS | 1711 28 32 31 17 26 37 29 129 |T 59 64 54 59 56 59 56 115 53
WRMS | 1711 29 30 31 15 24 27 30 129 |NE 56 62 48 55 50 54 52 109 48
MEDI | 1043 21 25 20 11 21 18 23 108 |MD 57 65 45 59 51 55 53 114 51
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