[IGSREPORT-25943] Wk 2001 IGLOS Final Orbits
acc
acc at igs.org
Sat Jun 2 05:23:48 PDT 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2001 (May 13, 2018 - May 19, 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 2.2001.
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:
igl2001[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2001 in the SP3 format.
igl20017.sum Combination Report for GPS Week 2001.
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 | 5.4 ns
2 | 5.4 ns
3 | 7.3 ns
4 | 7.1 ns
5 | -0.5 ns
6 | 6.0 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
----+--------+---------------
5 | GRG | R07 R09 R13
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 1.2001, 1a.2001).
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 2.2001.0-6)
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 3.2001.0-6).
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 2001 summary. (May 13, 2018 - May 19, 2018)
Table 1.2001.a GPS week : 2001 MJD: 58251.0-58257.0
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 1 6 29 5 23 .02 27 25 | 4897 -121 3602 10229
| 0 1 1 26 11 30 .02 | 2199 1925
cof n/a| 0 0 5 16 9 7 .06 29 27 | 4891 -110 3602 10230
| 1 1 2 36 15 55 .08 | 2192 1935
emx n/a| -1 1 1 -18 -20 -15 .01 22 22 | 199 278 3604 9622
| 1 1 1 16 30 38 .03 | 5838 1374
esx n/a| 0 0 -2 1 -17 -2 .17 15 13 | 8905 -766 3600 12182
| 1 0 2 11 16 22 .02 | 12192 1587
gfz n/a| 0 1 -4 7 28 15 -.01 26 23 | 0 -279 3609 10197
| 1 1 1 35 21 44 .07 | 0 1787
grg n/a| 1 0 2 -45 18 -42 -.34 1572 28 | -263236 671250 6400 47890
| 2 1 3 26 21 36 .04 | 461358 1211266
iac n/a| 1 -1 1 4 2 -7 -.03 19 19 | 6164 503 4352 12576
| 1 0 2 18 29 73 .05 | 1949 539
mcc n/a| 2 -4 0 39 -53 -37 -.31 113 113 | --- --- --- ---
| 7 5 7 94 116 206 .23 | --- ---
Table 1.2001.b GPS week : 2001 MJD: 58251.0-58257.0
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 | 13 15 16 17 13 13 13 |
R02 | 7 6 7 7 8 7 8 |
R03 | 8 8 7 8 8 11 7 |
R04 | 9 9 8 6 7 7 7 |
R05 | --- --- --- 0 0 0 37 |
R07 | 10 10 8 7 8 9 6 |
R08 | 6 8 9 6 7 10 9 |
R09 | 7 7 6 7 7 7 6 |
R10 | 7 9 9 9 8 8 7 |
R11 | 9 9 10 9 9 10 8 |
R13 | 8 10 10 11 12 8 8 |
R14 | 8 11 10 11 10 11 8 |
R15 | 13 15 14 15 16 15 17 |
R16 | 14 16 14 16 16 18 18 |
R17 | 7 8 8 6 8 7 7 |
R18 | 6 7 7 10 7 8 9 |
R19 | 10 10 12 12 12 12 12 |
R20 | 11 10 12 14 13 14 11 |
R21 | 8 8 7 8 8 10 8 |
R22 | 9 7 8 8 8 9 10 |
R23 | 10 11 9 9 8 9 11 |
R24 | 13 12 11 11 13 11 12 |
R26 | 0 0 0 0 0 0 0 |
Table 1.2001.c GPS week : 2001 MJD: 58251.0-58257.0
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 2001 0 | 26 22 165 542 -1666 3388 83.7 1546 1546 | 6493 0
brd 2001 1 | -120 -19 107 522 -3152 4855 82.8 1593 1593 | 5372 0
brd 2001 2 | 44 -35 120 141 255 6514 82.5 1610 1610 | 5442 0
brd 2001 3 | 16 23 191 -452 -420 8000 84.0 1989 1989 | 7304 0
brd 2001 4 | -97 -23 159 1258 -1669 7573 83.2 1926 1926 | 7068 0
brd 2001 5 | -37 33 196 -1529 -24 5412 87.2 1451 1451 | -548 0
brd 2001 6 | 45 -14 106 -1062 -597 4395 83.5 1394 1394 | 5993 0
-------------+------------------------------------------------------------+----------------
brd 2001 mean| -17 -1 149 -82 -1039 5734 83.8 1644 1644 | 5303 0
brd 2001 sdev| 68 27 38 982 1192 1698 1.6 227 227 | 2685 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 2.2001.0 GPS week: 2001 Day: 0 MJD: 58251
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 8 70 20 12 .03 26 25 | 5934 2325 3119 10422
cof n/a| 0 2 5 47 20 2 .05 26 25 | 5922 2347 3119 10426
emx n/a| 0 2 2 -38 17 -40 .03 25 25 | -1685 1780 3120 9791
esx n/a| 0 -1 -2 0 -22 0 .16 12 11 | -2872 1522 3121 12163
gfz n/a| 0 0 -4 -8 42 -6 -.06 25 21 | 0 2064 3125 10106
grg n/a| 0 -1 4 -44 15 -17 -.33 28 23 | 5306 2367 3121 9971
iac n/a| 1 0 0 17 -15 14 -.07 18 18 | 6973 923 3871 10494
mcc n/a| 0 0 7 -107 -14 136 -.21 195 195 | --- --- --- ---
Table 2.2001.1 GPS week: 2001 Day: 1 MJD: 58252
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 9 34 1 22 .02 26 26 | 7299 -1420 3847 9703
cof n/a| 0 0 7 22 -6 16 -.01 28 27 | 7284 -1391 3848 9707
emx n/a| 0 1 0 -27 -66 -22 .02 26 26 | 9584 -728 3841 9372
esx n/a| 0 0 -3 -6 -22 -19 .15 14 12 | 23200 -2165 3833 11756
gfz n/a| 0 2 -5 31 47 18 -.05 24 25 | 0 -944 3849 9392
grg n/a| 1 0 3 -88 2 -57 -.40 32 26 | 5960 -1352 3857 8708
iac n/a| 0 0 0 14 22 42 -.00 19 19 | 3826 1002 4975 18891
mcc n/a| 3 1 5 -32 -149 291 -.60 129 129 | --- --- --- ---
Table 2.2001.2 GPS week: 2001 Day: 2 MJD: 58253
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 5 45 -3 0 .01 25 20 | 5701 -1163 3395 10376
cof n/a| -1 0 10 77 35 -18 .17 31 27 | 5698 -1142 3389 10376
emx n/a| -1 0 0 -1 -42 -30 -.02 21 21 | -6485 -684 3405 9992
esx n/a| 0 1 -3 -11 8 21 .19 14 12 | -4742 -2012 3390 12708
gfz n/a| -1 0 -2 -22 12 -24 -.06 27 20 | 0 -1882 3401 10036
grg n/a| -1 -1 1 -14 49 -55 -.39 34 31 | 5986 -1164 3416 9715
iac n/a| 3 0 0 -1 -35 0 -.03 19 19 | 8222 692 3986 11280
mcc n/a| -5 1 1 119 -200 -125 -.11 93 93 | --- --- --- ---
Table 2.2001.3 GPS week: 2001 Day: 3 MJD: 58254
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 -15 22 27 .05 28 29 | 4950 608 3377 10180
cof n/a| 0 0 4 -29 13 -12 .09 28 28 | 4952 608 3375 10180
emx n/a| -4 1 3 -12 -45 21 .04 23 21 | -2866 1167 3385 9602
esx n/a| 0 0 0 23 -44 -9 .20 14 13 | 21277 -712 3372 12031
gfz n/a| 0 3 -4 -17 -6 38 -.05 27 33 | 0 141 3365 10030
grg n/a| 2 0 0 -38 30 -93 -.34 30 27 | 6970 501 3366 9683
iac n/a| 2 -1 0 -3 54 -38 .00 22 22 | 8072 279 3940 9757
mcc n/a| -5 -6 -5 100 66 -171 -.15 86 86 | --- --- --- ---
Table 2.2001.4 GPS week: 2001 Day: 4 MJD: 58255
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 23 -3 74 .03 27 28 | 5475 1839 4239 10513
cof n/a| 0 2 4 -12 -4 13 .01 29 29 | 5457 1868 4242 10512
emx n/a| 0 1 4 0 0 -7 -.03 20 20 | -3342 2070 4231 9587
esx n/a| -1 0 0 0 -18 -15 .16 16 15 | -2084 1154 4246 11861
gfz n/a| 0 1 -5 -30 46 49 .01 26 23 | 0 1712 4260 10312
grg n/a| 5 -2 0 -57 0 -23 -.34 30 26 | -999999 3027566 4250 10596
iac n/a| 2 -1 -2 31 6 -49 -.02 20 20 | 6099 908 5157 14531
mcc n/a| 3 -5 6 106 30 -314 -.67 107 107 | --- --- --- ---
Table 2.2001.5 GPS week: 2001 Day: 5 MJD: 58256
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 37 0 44 .03 29 29 | 300 -3133 3656 10140
cof n/a| 2 0 4 3 -6 115 .14 30 30 | 309 -3153 3654 10141
emx n/a| -1 0 1 -40 -1 39 -.02 22 22 | -748 -1415 3656 9562
esx n/a| -2 0 -5 5 -2 35 .16 18 15 | 9228 -2407 3642 12450
gfz n/a| -2 1 -3 48 40 80 .09 25 21 | 0 -2833 3655 10771
grg n/a| 1 0 9 -12 -9 -66 -.30 >>>> 35 | -872916 1670592 23219 276864
iac n/a| 1 -2 2 -1 -17 -126 .02 17 17 | 3249 -491 4441 12472
mcc n/a| 12 -13 -14 124 -168 -128 -.25 76 76 | --- --- --- ---
Table 2.2001.6 GPS week: 2001 Day: 6 MJD: 58257
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 3 3 13 0 -19 -.02 25 21 | 4623 91 3585 10273
cof n/a| 0 1 2 8 12 -66 -.05 28 24 | 4619 89 3587 10274
emx n/a| -2 2 1 -10 -7 -73 .03 21 21 | 6935 -243 3593 9450
esx n/a| 0 -1 -2 -1 -21 -25 .16 16 14 | 18328 -744 3597 12306
gfz n/a| 0 2 -2 51 16 -45 .09 24 19 | 0 -213 3609 10737
grg n/a| 0 0 -2 -63 38 16 -.31 32 28 | 6039 242 3576 9693
iac n/a| 0 0 5 -26 3 102 -.13 20 19 | 6710 211 4096 10612
mcc n/a| 12 -6 -3 -33 65 47 -.20 104 104 | --- --- --- ---
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 3.2001.0 GPS week: 2001 Day: 0 MJD: 58251
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 | 566 32 18 40 19 24 46 14 --- 12 | 51 54 42 54 59 48 35 --- 41
R02 | 897 16 17 22 12 19 10 12 193 6 | 39 39 31 39 39 37 32 81 34
R03 | 945 21 22 22 14 19 22 14 85 8 | 58 59 53 45 41 54 39 62 46
R04 | 926 28 24 24 6 16 11 30 --- 9 | 55 52 51 43 45 44 42 --- 43
R07 | 743 23 28 17 8 32 31 21 271 9 | 67 70 61 55 57 73 48 153 55
R08 | 854 18 17 19 6 14 13 16 --- 6 | 76 77 73 72 67 75 66 --- 70
R09 | 1184 16 14 9 11 19 16 16 --- 6 | 36 32 31 33 37 9999 36 --- 32
R10 | 1490 14 12 12 13 26 17 7 --- 6 | 53 53 45 58 38 56 51 --- 50
R11 | 1847 29 26 15 15 25 24 13 214 8 | 62 61 43 51 31 36 34 125 42
R13 | 1713 12 17 12 11 22 36 14 --- 8 | 54 58 46 61 45 129 48 --- 55
R14 | 654 27 26 17 15 24 13 17 --- 8 | 60 65 46 58 41 47 34 --- 47
R15 | 4413 49 51 21 15 35 36 30 --- 13 | 81 85 50 49 32 74 27 --- 48
R16 | 762 25 28 48 10 22 62 18 --- 14 | 75 82 56 68 64 82 65 --- 65
R17E | 1169 24 32 20 7 18 15 12 --- 6 | 73 76 71 71 69 67 68 --- 68
R18E | 1700 11 11 20 11 19 9 12 --- 6 | 35 39 37 39 38 33 41 --- 37
R19E | 1683 38 39 24 11 27 21 14 --- 9 | 68 72 67 79 83 79 65 --- 72
R20E | 1539 22 23 31 17 36 28 22 --- 11 | 97 93 109 101 98 93 108 --- 100
R21E | 1482 20 22 20 12 27 22 16 164 8 | 56 57 52 58 50 48 48 178 51
R22E | 1066 27 26 22 8 27 17 19 --- 8 | 50 48 42 51 55 44 51 --- 47
R23E | 1266 31 38 30 13 19 24 16 --- 9 | 108 105 99 111 105 119 118 --- 110
R24E | 1092 20 20 38 15 33 43 27 --- 12 | 50 53 58 55 57 44 46 --- 47
XR26E | 4403 --- --- --- --- --- --- 2 --- 0 | --- --- --- --- --- --- 55 --- 54
------+---------------------------------------------------+-----------------------------------------------
RMS | 1546 26 26 25 12 25 28 18 195 |T 62 63 55 59 54 64 52 119 55
WRMS | 1546 25 25 25 11 21 23 18 195 |NE 59 60 48 52 45 62 42 105 48
MEDI | 1169 23 23 21 12 24 22 16 193 |MD 58 59 51 55 50 54 48 125 48
Table 3.2001.1 GPS week: 2001 Day: 1 MJD: 58252
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 | 717 41 40 35 25 20 58 24 --- 15 | 43 57 34 41 45 55 26 --- 30
R02 | 795 13 13 18 8 9 22 11 65 6 | 30 29 29 32 27 32 26 104 27
R03 | 698 16 18 20 11 22 24 10 85 7 | 39 39 38 32 27 44 30 70 32
R04 | 612 28 29 27 11 17 11 17 --- 8 | 41 43 41 31 31 37 31 --- 31
R07 | 643 28 26 26 14 13 25 29 163 10 | 50 47 48 39 35 59 38 141 38
R08 | 780 22 22 23 7 13 14 22 --- 7 | 59 56 56 57 51 62 59 --- 56
R09 | 1536 14 18 13 11 26 18 15 --- 7 | 25 27 28 27 33 9999 25 --- 24
R10 | 2085 12 14 17 16 27 28 21 --- 9 | 31 37 29 46 27 47 35 --- 35
R11 | 1693 30 34 14 8 30 13 18 94 8 | 45 48 32 36 22 34 27 96 31
R13 | 2491 12 12 31 12 28 34 17 --- 9 | 39 36 34 35 33 50 34 --- 34
R14 | 784 30 30 16 12 33 32 21 --- 10 | 40 41 38 31 25 54 22 --- 30
R15 | 3729 48 47 21 20 34 46 30 --- 14 | 54 55 46 39 36 57 25 --- 38
R16 | 868 28 33 48 18 29 71 18 --- 15 | 62 60 52 61 55 38 53 --- 52
R17E | 2780 24 34 22 10 23 19 11 --- 8 | 50 56 49 45 53 42 48 --- 45
R18E | 1493 13 12 25 9 17 18 14 --- 7 | 30 31 35 27 24 26 30 --- 25
R19E | 1433 32 34 26 19 21 17 19 --- 10 | 62 65 65 63 66 63 61 --- 61
R20E | 1448 25 27 21 17 22 31 23 --- 10 | 59 65 59 69 74 58 69 --- 62
R21E | 1390 22 30 20 11 26 20 13 189 8 | 49 52 42 44 50 49 48 103 44
R22E | 856 20 23 18 10 24 15 13 --- 7 | 62 64 61 62 64 60 61 --- 60
R23E | 1070 26 30 35 15 19 32 16 --- 10 | 75 79 72 70 72 71 71 --- 70
R24E | 1127 27 36 37 19 24 37 22 --- 12 | 39 41 43 37 31 34 31 --- 30
XR26E | 5044 --- --- --- --- --- --- 2 --- 0 | --- --- --- --- --- --- 48 --- 46
------+---------------------------------------------------+-----------------------------------------------
RMS | 1593 26 28 26 14 24 32 19 128 |T 46 48 44 44 41 48 40 102 40
WRMS | 1593 26 27 26 12 25 26 19 128 |NE 42 44 38 39 34 47 33 102 35
MEDI | 1127 25 29 22 12 23 24 17 94 |MD 45 48 42 39 35 49 34 103 35
Table 3.2001.2 GPS week: 2001 Day: 2 MJD: 58253
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 56 68 23 24 42 52 19 --- 15 | 49 61 24 33 48 45 19 --- 21
R02 | 732 9 12 18 16 11 15 15 89 6 | 30 38 23 43 26 36 21 40 29
R03 | 646 10 15 10 9 25 24 14 75 6 | 47 50 41 43 56 56 43 40 44
R04 | 579 16 25 16 11 26 18 17 --- 7 | 44 54 41 36 26 28 36 --- 34
R07 | 944 14 27 21 10 15 20 22 119 7 | 50 60 52 37 41 66 31 97 40
R08 | 587 16 27 24 15 24 24 21 --- 9 | 73 80 60 72 80 62 56 --- 66
R09 | 2025 10 10 11 8 16 26 9 --- 5 | 20 18 21 19 19 9999 19 --- 17
R10 | 923 8 13 17 9 23 44 16 --- 8 | 38 33 34 40 29 67 33 --- 37
R11 | 747 28 35 22 7 37 16 19 98 9 | 50 55 40 36 26 34 26 69 33
R13 | 1672 16 16 21 11 28 40 23 --- 9 | 39 40 43 46 32 78 39 --- 41
R14 | 689 24 33 13 10 29 31 25 --- 9 | 43 48 35 39 28 50 21 --- 33
R15 | 3893 53 64 18 15 48 37 28 --- 14 | 65 75 45 40 22 58 24 --- 38
R16 | 534 20 47 32 18 20 79 18 --- 14 | 64 77 46 65 63 42 60 --- 56
R17E | 3365 20 20 21 12 19 21 11 --- 7 | 40 39 32 42 42 43 32 --- 36
R18E | 722 10 16 20 8 21 17 14 --- 6 | 30 31 27 33 36 27 34 --- 29
R19E | 1294 37 38 25 20 25 27 21 --- 11 | 42 43 37 36 51 43 39 --- 34
R20E | 2492 25 22 23 17 43 37 25 --- 12 | 59 59 56 67 59 65 71 --- 60
R21E | 1359 19 15 19 9 24 18 13 76 7 | 50 47 49 61 52 47 54 50 52
R22E | 776 21 25 17 9 23 30 12 --- 7 | 62 67 57 69 70 56 64 --- 62
R23E | 1651 19 21 24 17 20 31 16 --- 9 | 73 75 64 72 71 76 65 --- 68
R24E | 1388 28 28 24 15 24 43 17 --- 10 | 35 50 29 41 40 49 32 --- 33
XR26E | 7187 --- --- --- --- --- --- 2 --- 0 | --- --- --- --- --- --- 31 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1609 25 31 21 14 27 34 19 93 |T 47 52 40 46 43 51 38 59 40
WRMS | 1609 20 27 21 12 20 31 19 93 |NE 47 53 38 42 38 51 32 61 37
MEDI | 923 19 25 21 11 24 27 17 89 |MD 47 50 41 41 41 49 33 50 36
Table 3.2001.3 GPS week: 2001 Day: 3 MJD: 58254
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 | 987 56 53 30 32 29 52 19 --- 16 | 51 51 29 29 29 40 17 --- 16
R02 | 1913 17 13 14 7 32 9 17 124 7 | 33 29 33 26 23 27 19 61 23
R03 | 872 8 13 16 8 17 19 33 78 8 | 48 50 50 51 37 50 29 16 43
R04 | 999 14 10 17 10 12 13 17 --- 6 | 44 40 46 31 31 37 25 --- 33
XR05 | ---- 3 >>>> --- --- --- --- --- --- 0 | 54 9999 --- --- --- --- --- --- 58
R07 | 1010 11 10 12 8 26 20 22 66 7 | 55 50 56 53 40 83 35 56 49
R08 | 655 12 13 13 7 13 10 23 --- 6 | 55 54 56 50 57 47 33 --- 48
R09 | 2366 14 18 15 15 13 20 9 --- 6 | 17 23 16 23 32 9999 22 --- 19
R10 | 1261 16 11 14 16 25 30 15 --- 8 | 48 47 38 53 29 58 35 --- 43
R11 | 852 33 34 18 11 33 12 12 101 9 | 52 52 34 38 29 32 33 39 33
R13 | 975 11 22 20 15 25 35 35 --- 10 | 44 46 33 46 34 106 36 --- 39
R14 | 896 34 24 17 13 39 30 21 --- 11 | 50 46 30 36 34 42 21 --- 31
R15 | 4855 60 62 16 9 45 37 25 --- 14 | 69 69 45 34 22 59 23 --- 37
R16 | 729 27 24 58 10 29 56 28 --- 16 | 58 51 40 39 39 57 42 --- 40
R17E | 3783 20 24 14 9 20 15 9 --- 6 | 33 36 28 32 33 31 26 --- 28
R18E | 702 14 14 24 13 18 42 13 --- 9 | 27 28 22 31 25 49 29 --- 25
R19E | 890 36 40 30 21 26 28 24 --- 12 | 64 64 55 59 62 75 64 --- 59
R20E | 3900 33 40 29 15 41 37 36 --- 13 | 33 40 34 30 40 35 38 --- 27
R21E | 1564 23 24 20 10 19 20 15 38 7 | 51 52 46 40 50 37 46 52 42
R22E | 1062 22 23 17 11 24 18 17 --- 7 | 62 60 56 61 55 61 50 --- 56
R23E | 2419 21 22 24 16 22 17 15 --- 8 | 68 72 67 71 79 64 74 --- 69
R24E | 1113 29 28 21 14 25 39 19 --- 10 | 23 39 35 38 44 42 35 --- 31
XR26E | 4626 --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 30 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1989 28 28 23 14 27 30 22 86 |T 47 47 40 41 39 51 34 44 38
WRMS | 1989 29 28 21 13 33 27 22 86 |NE 48 46 38 39 33 53 28 43 36
MEDI | 1010 20 23 17 11 25 20 17 78 |MD 50 50 38 38 34 47 33 52 37
Table 3.2001.4 GPS week: 2001 Day: 4 MJD: 58255
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 | 727 48 42 24 12 23 35 29 --- 12 | 49 45 19 25 31 33 29 --- 20
R02 | 1410 19 32 21 14 21 14 18 169 8 | 36 45 30 25 24 34 25 124 25
R03 | 1070 21 17 16 8 24 19 22 90 8 | 49 49 43 40 31 47 25 48 37
R04 | 990 11 9 9 7 21 28 20 --- 7 | 41 35 38 36 26 48 24 --- 33
XR05 |16649 5 45 --- --- --- --- --- --- 0 | 49 9999 --- --- --- --- --- --- 50
R07 | 851 13 20 18 11 14 28 14 71 7 | 47 51 49 37 34 49 36 112 36
R08 | 736 17 18 10 11 21 11 16 --- 6 | 66 62 58 67 58 58 58 --- 61
R09 | 1776 11 13 9 12 17 22 15 --- 6 | 17 19 19 24 27 9999 27 --- 21
R10 | 925 17 30 11 15 20 25 16 --- 7 | 44 53 28 37 31 52 27 --- 33
R11 | 999 25 26 12 11 33 21 17 106 8 | 46 47 28 38 26 39 28 60 31
R13 | 952 16 17 19 16 32 34 35 --- 11 | 42 47 36 54 30 96 35 --- 42
R14 | 996 40 44 13 10 36 8 17 --- 9 | 52 54 28 36 30 29 27 --- 31
R15 | 3300 56 53 25 29 43 43 22 --- 16 | 62 64 31 40 23 58 27 --- 35
R16 | 1041 33 36 28 13 38 79 21 --- 16 | 65 69 71 58 52 92 62 --- 62
R17E | 3982 17 23 14 16 26 15 15 --- 7 | 42 47 34 40 45 39 32 --- 35
R18E | 810 7 9 14 13 17 28 13 --- 7 | 33 35 31 33 33 47 36 --- 33
R19E | 884 40 48 32 20 32 26 16 --- 12 | 67 69 56 76 68 52 59 --- 62
R20E | 4947 24 25 29 18 27 40 31 --- 12 | 47 51 55 60 55 58 56 --- 51
R21E | 2137 24 20 14 10 23 19 14 61 7 | 43 45 43 47 46 33 45 56 41
R22E | 876 20 21 22 15 17 20 14 --- 8 | 46 45 44 51 50 44 37 --- 44
R23E | 1952 24 25 17 17 12 16 13 --- 7 | 50 54 47 58 50 39 49 --- 49
R24E | 1485 29 33 26 31 27 26 28 --- 12 | 29 32 34 49 52 29 31 --- 31
XR26E | 4595 --- --- --- --- --- --- 4 --- 0 | --- --- --- --- --- --- 30 --- 31
------+---------------------------------------------------+-----------------------------------------------
RMS | 1926 27 29 20 16 26 30 20 107 |T 46 48 39 44 39 48 36 80 38
WRMS | 1926 28 29 20 15 23 26 20 107 |NE 47 49 36 39 32 52 33 86 36
MEDI | 1041 20 25 17 13 23 25 16 90 |MD 46 47 36 40 33 47 31 60 35
Table 3.2001.5 GPS week: 2001 Day: 5 MJD: 58256
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 48 50 26 29 24 19 13 --- 12 | 49 54 33 34 34 20 20 --- 24
R02 | 1032 15 11 15 17 14 19 12 43 7 | 35 42 36 37 43 40 21 74 31
R03 | 1245 22 31 17 25 12 42 21 71 10 | 52 61 52 37 52 58 25 33 39
R04 | 1120 19 22 13 10 17 24 16 --- 7 | 46 53 48 49 37 66 45 --- 46
XR05 |12971 4 25 --- --- --- --- --- --- 0 | 36 9999 --- --- --- --- --- --- 40
R07 | 680 20 21 23 11 13 457 21 62 9 | 55 51 53 61 67 389 50 119 55
R08 | 850 21 22 22 12 22 33 23 --- 9 | 62 65 63 64 58 80 46 --- 58
R09 | 2231 12 16 11 12 19 >>>> 16 --- 7 | 22 24 24 24 28 9999 25 --- 22
R10 | 688 26 22 11 15 23 23 13 --- 8 | 45 47 36 43 33 35 37 --- 35
R11 | 805 22 22 11 19 22 40 17 120 9 | 38 40 32 41 33 36 23 35 29
R13 | 926 15 14 22 11 15 899 17 --- 8 | 36 34 38 38 33 805 31 --- 32
R14 | 1437 36 38 19 12 34 23 22 --- 10 | 45 48 37 36 28 34 20 --- 28
R15 | 1882 63 66 22 13 40 52 19 --- 15 | 53 57 30 28 24 49 18 --- 24
R16 | 673 35 48 47 22 47 77 19 --- 17 | 61 81 45 67 56 81 47 --- 51
R17E | 2795 19 17 17 9 25 22 9 --- 7 | 44 43 37 41 45 45 47 --- 41
R18E | 1224 14 14 14 19 18 31 12 --- 8 | 27 28 30 38 27 30 30 --- 27
R19E | 1567 43 31 26 11 32 32 14 --- 11 | 120 122 118 127 133 129 114 --- 121
R20E | 2435 22 21 28 24 31 60 30 --- 14 | 55 59 63 61 56 52 62 --- 56
R21E | 1742 23 24 23 15 26 37 13 63 9 | 41 42 36 43 43 57 45 66 40
R22E | 638 22 18 25 15 24 21 12 --- 8 | 42 47 35 46 47 51 48 --- 41
R23E | 1528 24 22 22 21 13 21 13 --- 8 | 90 85 86 86 90 96 100 --- 90
R24E | 1480 24 26 18 27 24 32 20 --- 10 | 41 39 41 51 49 34 40 --- 38
XR26E | 4607 --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 45 --- 41
------+---------------------------------------------------+-----------------------------------------------
RMS | 1451 29 30 22 18 25 >>>> 17 76 |T 49 53 46 50 48 109 42 65 43
WRMS | 1451 29 30 22 15 21 35 17 76 |NE 45 50 40 43 40 141 31 65 36
MEDI | 1245 22 22 22 15 23 32 16 63 |MD 45 48 37 43 43 51 40 66 40
Table 3.2001.6 GPS week: 2001 Day: 6 MJD: 58257
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 | 1183 34 35 19 27 23 31 31 --- 12 | 43 58 38 47 39 42 31 --- 32
R02 | 723 14 18 14 16 14 24 18 96 7 | 44 49 36 40 38 50 30 64 37
R03 | 1425 13 13 14 15 18 22 14 105 7 | 68 70 66 54 67 73 54 44 60
R04 | 721 17 17 7 17 21 11 10 --- 6 | 57 58 51 47 58 55 49 --- 49
XR05 |22661 56 50 --- --- 35 --- 56 --- 36 | 39 9999 --- --- 12 --- 23 --- 48
R07 | 736 12 16 11 8 17 21 16 133 6 | 70 71 64 63 66 88 57 149 62
R08 | 671 21 26 22 13 18 23 21 --- 8 | 78 79 76 79 74 92 62 --- 74
R09 | 2586 11 19 11 9 15 16 15 --- 5 | 26 27 26 27 36 9999 33 --- 27
R10 | 1366 12 11 17 15 18 20 15 --- 7 | 57 60 46 61 45 56 51 --- 52
R11 | 928 25 27 16 11 18 14 16 118 7 | 62 64 39 48 34 44 34 52 41
R13 | 950 14 17 17 12 24 28 14 --- 7 | 58 61 58 62 46 207 48 --- 55
R14 | 1704 26 29 14 6 27 15 16 --- 8 | 59 60 41 43 25 47 29 --- 38
R15 | 2795 61 67 15 17 52 56 22 --- 17 | 85 89 41 42 35 78 29 --- 44
R16 | 513 44 54 53 18 28 75 22 --- 18 | 96 103 54 81 54 97 66 --- 70
R17E | 1543 15 16 13 13 19 22 19 --- 7 | 75 80 75 73 79 76 77 --- 74
R18E | 942 12 19 25 11 19 16 27 --- 8 | 42 49 48 50 51 44 44 --- 45
R19E | 1566 29 30 33 20 33 19 25 --- 12 | 149 151 135 147 166 145 153 --- 148
R20E | 862 22 32 16 8 27 46 25 --- 10 | 105 111 104 100 102 116 99 --- 101
R21E | 1361 17 21 19 13 20 28 14 43 8 | 63 63 56 60 62 57 60 80 58
R22E | 652 19 20 24 14 22 45 9 --- 10 | 61 63 52 62 55 57 57 --- 56
R23E | 1507 24 25 16 28 17 36 23 --- 11 | 125 124 116 120 123 137 128 --- 123
R24E | 1741 28 22 16 30 32 21 22 --- 11 | 39 43 39 53 48 39 38 --- 38
XR26E | 4194 --- --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- 71 --- 75
------+---------------------------------------------------+-----------------------------------------------
RMS | 1394 25 28 21 16 24 32 20 104 |T 68 73 60 64 59 80 57 77 61
WRMS | 1394 21 24 21 14 19 28 19 104 |NE 60 65 48 53 44 77 42 77 49
MEDI | 1361 19 21 16 14 20 22 18 105 |MD 61 63 52 60 51 57 51 64 55
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