[IGSREPORT-19905] Wk 1640 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Fri Jul 1 05:05:15 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1640 (Jun 12, 2011 - Jun 18, 2011)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
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 2.1640.
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:
igl1640[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1640 in the SP3 format.
igl16407.sum Combination Report for GPS Week 1640.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
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).
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 | 186.6 ns
1 | 186.7 ns
2 | 183.1 ns
3 | 180.0 ns
4 | 172.4 ns
5 | 175.6 ns
6 | 172.7 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1640, 1a.1640).
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 2.1640.0-6)
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 3.1640.0-6).
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 1640 summary. (Jun 12, 2011 - Jun 18, 2011)
Table 1.1640.a GPS week : 1640 MJD: 55724.0-55730.0
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 249| -1 0 6 -4 -27 37 -.15 28 27 | --- --- --- ---
| 2 1 3 40 30 33 .05 | --- ---
esx 128| -1 1 3 59 -6 -39 .38 20 19 | 179185 190 4903 5056
| 0 1 4 36 31 30 .04 | 5148 3327
gfz 193| 0 0 2 -24 -14 3 -.22 23 20 | 0 862 4904 8302
| 2 1 3 44 37 56 .05 | 0 3082
grg 133| 0 0 -10 -43 31 16 -.11 44 41 | --- --- --- ---
| 2 3 5 15 51 71 .09 | --- ---
iac n/a| 1 0 -6 -25 33 3 -.08 25 25 | 180677 -569 4910 8389
| 2 0 7 17 28 83 .04 | 5589 2295
mcc n/a| -2 0 22 -107 30 104 .01 217 217 | --- --- --- ---
| 5 7 20 104 93 605 .20 | --- ---
Table 1.1640.b GPS week : 1640 MJD: 55724.0-55730.0
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 10 13 20 16 14 14 |
R02 | 13 11 10 17 20 10 10 |
R03 | 11 11 10 10 10 11 10 |
R04 | 120 116 106 75 --- 0 278 |
R05 | 14 23 15 11 13 12 11 |
R06 | 12 12 12 16 15 11 10 |
R07 | 21 18 11 13 12 12 14 |
R08 | 11 13 11 15 12 13 12 |
R09 | 13 13 14 15 15 16 11 |
R10 | 10 11 12 12 9 10 13 |
R11 | 18 16 15 14 20 20 18 |
R12 | 12 13 11 10 13 11 13 |
R13 | 9 15 12 10 13 14 13 |
R15 | 11 9 14 13 13 14 13 |
R16 | 16 12 13 14 14 16 13 |
R17 | 12 13 12 14 12 15 20 |
R18 | 11 12 11 14 12 12 14 |
R19 | 13 12 11 14 12 10 11 |
R20 | 18 20 16 15 13 16 15 |
R21 | 13 12 11 13 12 14 12 |
R22 | 14 14 10 15 16 18 13 |
R23 | 9 11 10 9 16 11 11 |
R24 | 14 14 12 13 10 11 12 |
Table 1.1640.c GPS week : 1640 MJD: 55724.0-55730.0
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 1640 0 | 51 -80 230 1033 -969 -16149 85.3 2664 2664 | 186629 0
brd 1640 1 | -23 15 323 -2917 901 -15440 88.2 2283 2283 | 186653 0
brd 1640 2 | -14 -21 372 729 124 -11080 86.7 2122 2122 | 183140 0
brd 1640 3 | -41 -26 374 2666 540 -12650 88.2 2069 2069 | 179954 0
brd 1640 4 | -15 26 312 587 654 -10440 88.5 1919 1919 | 172359 0
brd 1640 5 | 33 26 287 -803 604 -8366 86.3 2118 2118 | 175556 0
brd 1640 6 | -85 30 197 1357 -153 -12310 85.3 2501 2501 | 172715 0
-------------+------------------------------------------------------------+----------------
brd 1640 mean| -13 -4 299 379 243 -12347 87.0 2239 2239 | 179572 0
brd 1640 sdev| 45 41 66 1781 640 2745 1.4 261 261 | 6164 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 2.1640.0 GPS week: 1640 Day: 0 MJD: 55724
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 249| 0 -1 9 35 -27 29 -.09 26 24 | --- --- --- ---
esx 128| 0 0 7 94 -26 -67 .36 23 20 | 186504 -282 5264 5412
gfz 193| 0 0 5 -32 -43 59 -.31 25 25 | 0 2247 5270 7946
grg 133| 3 -3 -16 -71 92 43 .01 42 38 | --- --- --- ---
iac n/a| -1 0 -11 -48 34 -37 -.04 23 23 | 186647 -632 5280 8067
mcc n/a| -6 -1 22 -75 3 488 .24 220 220 | --- --- --- ---
Table 2.1640.1 GPS week: 1640 Day: 1 MJD: 55725
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 249| 0 1 10 19 23 44 -.25 32 32 | --- --- --- ---
esx 128| -1 1 9 77 -17 -67 .32 18 17 | 184867 2620 4544 4669
gfz 193| -1 -2 1 -58 -29 -11 -.21 24 24 | 0 2639 4531 8343
grg 133| 0 -6 -10 -55 75 -48 -.09 53 45 | --- --- --- ---
iac n/a| 1 1 -16 -36 65 73 -.07 23 23 | 187465 561 4546 8290
mcc n/a| -1 -2 11 16 -130 533 .17 213 213 | --- --- --- ---
Table 2.1640.2 GPS week: 1640 Day: 2 MJD: 55726
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 249| 0 0 7 36 -30 -5 -.14 27 27 | --- --- --- ---
esx 128| -1 0 2 104 40 -42 .34 18 18 | 180840 456 4435 4577
gfz 193| 0 0 7 -93 -73 -39 -.24 21 17 | 0 1096 4430 8514
grg 133| -1 4 -2 -39 69 3 -.04 39 39 | --- --- --- ---
iac n/a| 1 0 -14 -20 39 61 -.08 21 21 | 184880 -3616 4440 8253
mcc n/a| 1 6 57 -55 161 137 -.31 160 160 | --- --- --- ---
Table 2.1640.3 GPS week: 1640 Day: 3 MJD: 55727
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 249| 1 0 4 6 -35 76 -.16 28 28 | --- --- --- ---
esx 128| -2 1 2 51 -26 3 .40 21 21 | 178766 4603 5685 5787
gfz 193| -1 2 1 -16 4 68 -.15 21 20 | 0 4076 5686 9266
grg 133| 2 -2 -16 -33 3 57 -.07 40 37 | --- --- --- ---
iac n/a| 2 -1 -1 -35 38 -135 -.12 30 30 | 179640 2477 5731 9614
mcc n/a| -6 -15 36 -112 75 -1098 -.20 238 238 | --- --- --- ---
Table 2.1640.4 GPS week: 1640 Day: 4 MJD: 55728
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 249| -2 -3 0 -72 -5 81 -.13 30 26 | --- --- --- ---
esx 128| 0 0 0 20 35 -3 .44 21 20 | 175211 -6025 4847 5118
gfz 193| -3 0 3 40 -3 41 -.20 18 15 | 0 -5560 4862 10867
grg 133| -2 2 -11 -37 -39 -106 -.18 46 42 | --- --- --- ---
iac n/a| 6 0 0 -31 -25 -36 -.04 30 30 | 176553 -3573 4830 10940
mcc n/a| 7 -3 2 -169 61 -270 -.02 320 320 | --- --- --- ---
Table 2.1640.5 GPS week: 1640 Day: 5 MJD: 55729
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 249| -3 0 4 -32 -74 3 -.14 26 23 | --- --- --- ---
esx 128| -2 3 -3 7 -35 -67 .39 19 19 | 175002 989 5058 5237
gfz 193| 1 -1 0 16 39 -85 -.20 24 19 | 0 1152 5084 7126
grg 133| 2 2 -8 -27 38 82 -.27 47 40 | --- --- --- ---
iac n/a| 3 1 2 2 52 105 -.12 25 25 | 175239 1065 5036 7258
mcc n/a| -3 7 0 -304 -29 385 .13 189 189 | --- --- --- ---
Table 2.1640.6 GPS week: 1640 Day: 6 MJD: 55730
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 249| -4 0 5 -24 -40 31 -.14 32 29 | --- --- --- ---
esx 128| 0 1 4 61 -14 -30 .41 19 17 | 173106 -1027 4493 4595
gfz 193| 2 1 0 -30 4 -10 -.20 23 20 | 0 386 4471 6056
grg 133| -1 0 -6 -43 -21 82 -.13 41 42 | --- --- --- ---
iac n/a| 1 -1 -4 -9 28 -5 -.12 21 21 | 174320 -270 4510 6301
mcc n/a| -8 3 28 -49 72 552 .07 181 181 | --- --- --- ---
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 3.1640.0 GPS week: 1640 Day: 0 MJD: 55724
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1285 29 33 23 39 30 --- 15 | 34 64 51 38 42 --- 42
R02E | 2189 22 19 27 42 22 --- 12 | 68 77 85 82 70 --- 73
R03 | 2940 15 21 20 33 20 --- 10 | 18 32 35 42 26 --- 23
XR04 | ---- 128 --- --- --- 112 --- 119 | 177 --- --- --- 131 --- 157
R05E | 2371 14 29 13 63 15 --- 13 | 49 59 57 70 53 --- 53
R06E | 3831 18 26 19 38 22 --- 12 | 45 61 58 75 54 --- 53
R07E | 5188 37 39 37 63 35 --- 20 | 63 65 68 90 56 --- 57
R08E | 1309 15 23 20 36 17 391 10 | 33 59 47 45 43 213 42
R09 | 1166 35 17 22 23 25 --- 12 | 25 31 39 42 29 --- 26
R10 | 1698 14 19 23 31 17 --- 10 | 30 32 39 40 31 --- 28
R11 | 2306 41 27 40 46 27 129 17 | 53 65 68 35 40 32 47
R12 | 2095 32 20 19 30 21 --- 12 | 26 38 39 32 32 --- 28
R13 | 2303 21 15 20 17 13 --- 8 | 25 24 24 24 19 --- 15
R15 | 4454 20 20 22 36 16 94 11 | 30 40 38 29 26 43 27
R16 | 3353 25 26 45 39 21 --- 15 | 36 44 47 36 30 --- 32
R17 | 898 28 21 16 44 17 --- 12 | 34 23 28 45 37 --- 25
R18 | 2198 16 8 23 48 20 122 11 | 63 45 49 42 54 48 47
R19 | 1554 12 19 24 56 23 --- 13 | 56 48 60 29 57 --- 49
R20 | 2207 32 29 34 63 27 --- 17 | 74 56 78 35 53 --- 55
R21 | 1937 38 17 12 41 20 --- 13 | 71 42 46 41 38 --- 44
R22 | 1950 25 25 12 25 40 --- 14 | 65 66 44 50 26 --- 45
R23 | 2345 13 8 20 24 19 --- 8 | 41 34 27 30 31 --- 30
R24 | 3969 31 12 30 45 23 --- 14 | 56 33 29 40 19 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 2663 26 23 25 42 23 220 |T 50 47 48 45 43 84 44
WRMS | 2663 24 20 25 38 23 220 |NE 51 40 43 37 39 41 41
MEDI | 2198 25 20 22 39 21 122 |MD 45 44 46 40 38 43 42
Table 3.1640.1 GPS week: 1640 Day: 1 MJD: 55725
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1410 24 10 20 36 22 --- 10 | 27 32 39 47 38 --- 30
R02E | 1102 20 15 23 39 23 --- 11 | 71 80 79 67 79 --- 74
R03 | 2279 15 15 23 46 14 --- 10 | 34 39 46 56 35 --- 37
XR04 | ---- 149 --- --- --- 89 --- 115 | 200 --- --- --- 112 --- 187
R05E | 1293 22 14 24 140 30 --- 23 | 29 45 39 103 35 --- 37
R06E | 2475 16 18 18 54 20 --- 12 | 21 34 36 39 38 --- 29
R07 | 3056 23 29 21 86 29 --- 17 | 63 79 70 74 56 --- 62
R08E | 1869 23 15 27 49 22 389 12 | 23 41 52 54 26 127 34
R09 | 954 31 14 29 44 22 --- 12 | 19 31 49 40 20 --- 26
R10 | 1634 18 19 24 19 26 --- 11 | 25 35 30 36 28 --- 22
R11 | 1339 45 29 25 45 25 126 16 | 26 47 38 39 38 20 30
R12 | 927 44 14 30 24 17 --- 13 | 30 36 45 27 24 --- 26
R13 | 1237 46 16 36 31 21 --- 14 | 23 41 51 31 31 --- 29
R15 | 4847 21 11 23 20 18 55 9 | 28 29 27 27 20 37 22
R16 | 2766 33 15 20 45 16 --- 11 | 32 37 38 50 30 --- 30
R17 | 1478 39 18 28 35 21 --- 13 | 26 39 43 48 19 --- 27
R18 | 2818 22 16 13 53 21 102 11 | 44 48 46 60 46 21 43
R19 | 1646 17 15 26 48 18 --- 11 | 34 46 31 38 28 --- 32
R20 | 3827 50 27 33 70 37 --- 20 | 62 60 69 36 32 --- 45
R21 | 1930 40 20 12 37 12 --- 11 | 49 22 34 29 30 --- 27
R22 | 1363 35 9 21 45 34 --- 14 | 48 38 44 37 27 --- 31
R23 | 1383 28 16 25 27 19 --- 11 | 39 33 14 43 24 --- 22
R24 | 3426 47 15 21 41 19 --- 13 | 48 30 26 35 17 --- 20
------+-----------------------------------------+-------------------------------------
RMS | 2283 32 18 24 53 23 213 |T 43 41 43 46 36 51 40
WRMS | 2283 32 17 24 45 23 213 |NE 45 38 39 39 33 26 38
MEDI | 1634 28 15 23 44 21 102 |MD 32 38 39 39 30 21 30
Table 3.1640.2 GPS week: 1640 Day: 2 MJD: 55726
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1071 27 16 13 46 27 --- 12 | 31 44 41 42 30 --- 32
R02E | 1131 18 13 16 36 16 --- 9 | 76 82 81 80 87 --- 80
R03 | 2204 21 16 19 23 18 --- 9 | 21 44 42 23 26 --- 29
XR04 | ---- 130 --- --- --- 86 --- 106 | 175 --- --- --- 131 --- 156
R05E | 1077 24 18 30 59 23 --- 14 | 48 61 66 72 55 --- 54
R06E | 1223 13 14 17 60 14 --- 12 | 41 45 44 45 45 --- 41
R07 | 1510 14 22 15 42 19 --- 11 | 42 33 51 62 35 --- 38
R08E | 1811 17 22 23 23 24 262 11 | 33 51 50 47 46 209 43
R09 | 2207 33 26 12 40 28 --- 13 | 28 43 34 69 24 --- 31
R10 | 1855 14 14 33 28 23 --- 11 | 24 30 52 35 27 --- 27
R11 | 1312 45 17 25 37 31 153 15 | 47 58 46 42 44 26 41
R12 | 950 32 14 20 28 13 --- 10 | 32 31 28 35 29 --- 26
R13 | 873 29 22 20 27 18 --- 11 | 20 32 30 23 31 --- 20
R15 | 4729 25 21 26 37 29 37 13 | 27 37 32 46 28 30 25
R16 | 1636 35 21 26 37 19 --- 13 | 40 40 54 58 35 --- 38
R17 | 1278 17 9 32 36 24 --- 12 | 25 37 49 37 32 --- 30
R18 | 3368 23 20 21 38 17 97 11 | 45 25 43 44 31 45 32
R19 | 1089 26 11 14 44 16 --- 10 | 46 40 58 34 38 --- 42
R20 | 3886 44 28 23 49 23 --- 16 | 56 32 55 30 33 --- 37
R21 | 1361 25 19 8 37 19 --- 10 | 61 54 48 44 54 --- 49
R22 | 796 30 14 14 32 13 --- 10 | 49 36 35 46 26 --- 32
R23 | 960 21 17 15 35 17 --- 10 | 32 20 29 35 21 --- 20
R24 | 3759 34 18 17 40 18 --- 12 | 50 42 24 29 30 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 2122 27 18 21 39 21 160 |T 45 41 45 44 40 77 41
WRMS | 2122 27 18 17 39 21 160 |NE 45 37 41 39 37 33 39
MEDI | 1312 25 17 19 37 19 97 |MD 41 40 44 42 32 30 32
Table 3.1640.3 GPS week: 1640 Day: 3 MJD: 55727
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2098 30 22 34 28 66 --- 19 | 27 40 46 50 46 --- 31
R02E | 2387 32 20 29 46 47 --- 17 | 158 162 151 155 166 --- 156
R03 | 1661 15 11 22 23 22 --- 9 | 26 33 43 41 33 --- 32
XR04 | ---- 51 --- --- --- 90 --- 74 | 474 --- --- --- 249 --- 442
R05E | 904 21 22 14 37 18 --- 11 | 53 68 63 70 46 --- 57
R06E | 976 29 18 20 74 20 --- 16 | 46 56 62 84 54 --- 53
R07 | 2040 16 22 21 48 17 --- 12 | 52 50 45 50 58 --- 47
R08E | 1289 16 28 22 43 35 440 14 | 46 67 62 49 54 471 52
R09 | 2563 29 17 32 46 23 --- 14 | 29 34 57 38 24 --- 31
R10 | 1089 14 25 11 47 18 --- 11 | 33 35 31 42 37 --- 29
R11 | 3561 37 18 17 28 34 102 13 | 36 39 36 30 35 29 29
R12 | 1276 28 14 23 23 12 --- 10 | 46 40 49 56 38 --- 41
R13 | 863 27 20 17 22 15 --- 10 | 33 28 37 34 18 --- 23
R15 | 4604 30 23 15 41 22 73 12 | 28 40 27 36 29 49 23
R16 | 1271 38 20 21 35 21 --- 13 | 53 69 75 65 48 --- 59
R17 | 2128 23 29 16 38 34 --- 14 | 34 37 31 40 38 --- 27
R18 | 3437 36 25 18 44 18 131 13 | 44 27 36 41 29 73 25
R19 | 880 17 17 16 49 38 --- 13 | 61 59 59 32 71 --- 54
R20 | 2559 26 23 28 36 38 --- 15 | 63 50 37 49 71 --- 48
R21 | 780 29 16 20 28 35 --- 13 | 71 48 43 35 81 --- 53
R22 | 565 45 28 18 34 20 --- 14 | 64 40 35 42 47 --- 36
R23 | 729 14 17 19 25 14 --- 9 | 46 35 35 47 28 --- 34
R24 | 1725 25 17 21 49 21 --- 13 | 42 33 34 44 18 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2069 28 21 21 40 30 238 |T 68 49 49 51 57 155 61
WRMS | 2069 28 21 20 37 30 238 |NE 69 40 41 42 52 50 59
MEDI | 1289 28 20 20 37 22 102 |MD 46 40 43 42 46 49 36
Table 3.1640.4 GPS week: 1640 Day: 4 MJD: 55728
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1793 38 24 16 42 43 --- 15 | 40 53 50 51 39 --- 41
R02 | 2526 36 18 27 35 68 --- 19 | 138 155 164 149 87 --- 139
R03 | 2959 25 19 11 26 16 --- 9 | 27 24 22 29 26 --- 19
R05E | 1222 21 22 12 50 34 386 13 | 80 74 75 95 49 113 70
R06E | 1445 31 18 18 69 23 --- 15 | 52 68 64 108 57 --- 62
R07 | 2858 21 14 17 53 16 --- 11 | 23 28 27 46 24 --- 21
R08E | 2267 19 21 17 42 24 581 11 | 51 58 64 58 39 368 51
R09 | 1278 32 18 15 61 30 --- 14 | 34 44 50 58 27 --- 35
R10 | 1812 16 14 11 35 18 --- 8 | 28 28 27 37 29 --- 24
R11 | 2547 58 39 30 53 17 88 19 | 37 59 44 59 35 45 37
R12 | 1255 26 21 16 26 38 --- 12 | 40 64 63 58 25 --- 49
R13 | 663 24 14 29 27 32 --- 13 | 36 25 37 42 30 --- 26
R15 | 1702 15 14 27 43 30 70 12 | 23 30 23 46 39 34 25
R16 | 631 39 14 19 45 24 --- 13 | 35 30 35 42 31 --- 22
R17 | 1511 21 16 17 46 22 --- 11 | 25 45 42 44 39 --- 34
R18 | 2973 35 15 12 39 23 118 11 | 37 30 27 33 27 76 24
R19 | 672 26 20 14 38 30 --- 12 | 43 37 35 30 51 --- 34
R20 | 2619 26 22 13 38 33 --- 12 | 38 63 55 50 69 --- 51
R21 | 1974 30 17 15 42 20 --- 11 | 62 41 44 39 44 --- 43
R22 | 2005 30 13 20 81 24 --- 16 | 59 46 49 56 47 --- 43
R23 | 1414 29 38 15 54 28 --- 15 | 37 39 33 45 36 --- 22
R24 | 810 18 25 11 27 22 --- 10 | 32 32 25 41 30 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1918 30 21 18 46 30 320 |T 44 48 47 55 40 127 40
WRMS | 1918 26 20 15 42 30 320 |NE 37 39 38 44 36 51 32
MEDI | 1702 26 18 16 42 24 118 |MD 37 41 42 46 36 76 34
Table 3.1640.5 GPS week: 1640 Day: 5 MJD: 55729
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1787 29 21 16 56 25 --- 14 | 34 49 41 53 38 --- 35
R02 | 3059 20 15 19 36 12 --- 9 | 108 111 111 125 119 --- 112
R03 | 3350 27 21 16 27 19 --- 11 | 38 37 33 33 28 --- 29
XR04 | ---- 6 --- --- --- --- --- 0 | 797 --- --- --- --- --- 777
R05 | 1839 17 17 24 39 26 151 11 | 60 69 71 73 72 16 65
R06 | 1174 19 19 12 49 16 --- 11 | 42 46 47 63 50 --- 44
R07 | 2332 11 14 25 51 18 --- 11 | 42 49 41 70 54 --- 44
R08 | 2950 20 12 34 54 14 361 13 | 38 52 45 63 48 182 42
R09 | 697 34 29 27 48 30 --- 16 | 28 42 42 49 25 --- 24
R10 | 1975 12 17 18 40 18 --- 10 | 28 30 30 44 36 --- 25
R11 | 933 53 24 40 49 32 86 19 | 34 30 40 48 26 36 22
R12 | 1650 23 13 15 45 18 --- 10 | 45 35 40 64 41 --- 38
R13 | 2531 24 31 24 35 22 --- 13 | 33 32 35 42 23 --- 24
R15 | 1904 17 26 34 52 18 84 14 | 24 30 36 53 25 21 16
R16 | 1783 32 23 34 59 23 --- 16 | 38 50 59 46 30 --- 37
R17 | 2534 38 14 29 40 33 --- 15 | 31 40 38 36 28 --- 26
R18 | 2704 32 13 13 45 20 100 12 | 36 20 24 35 23 40 20
R19 | 601 23 11 14 34 20 --- 9 | 38 28 31 38 33 --- 29
R20 | 3324 17 20 36 32 45 --- 15 | 32 39 30 34 51 --- 31
R21 | 1095 20 12 17 46 40 --- 13 | 47 46 53 49 47 --- 43
R22 | 2452 29 14 21 86 34 --- 17 | 47 34 45 57 36 --- 34
R23 | 1212 15 20 15 38 23 --- 10 | 38 36 33 39 21 --- 28
R24 | 963 18 23 17 29 25 --- 11 | 22 35 19 36 25 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 2117 26 19 24 47 25 189 |T 73 42 42 52 39 59 68
WRMS | 2117 23 19 19 40 25 189 |NE 79 35 36 43 31 32 71
MEDI | 1839 20 17 19 45 22 100 |MD 38 37 40 48 33 36 31
Table 3.1640.6 GPS week: 1640 Day: 6 MJD: 55730
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1913 36 15 33 37 21 --- 13 | 29 42 49 44 38 --- 34
R02 | 2477 9 12 18 50 10 --- 10 | 78 80 88 111 87 --- 84
R03 | 4882 23 14 14 23 22 --- 9 | 26 32 37 34 25 --- 27
XR04 |17405 372 --- --- --- 207 --- 277 | 547 --- --- --- 516 --- 593
R05 | 3041 23 14 18 34 19 145 10 | 51 56 60 64 50 15 52
R06 | 1182 16 15 16 38 15 --- 9 | 46 43 41 52 40 --- 40
R07 | 3010 22 17 28 57 17 --- 13 | 39 40 46 48 39 --- 35
R08 | 4491 19 24 18 33 22 336 11 | 38 54 51 54 43 144 45
R09 | 1659 26 13 21 42 14 --- 11 | 34 38 29 66 29 --- 31
R10 | 2232 22 20 24 50 16 --- 12 | 23 26 34 30 25 --- 21
R11 | 758 57 19 29 42 33 125 17 | 47 52 54 49 41 44 41
R12 | 1649 36 16 21 50 19 --- 13 | 43 36 44 43 31 --- 33
R13 | 1516 32 18 21 47 20 --- 13 | 34 25 31 59 24 --- 24
R15 | 2241 31 20 29 30 25 83 13 | 20 36 30 27 28 26 23
R16 | 1619 33 18 15 39 25 --- 12 | 57 44 46 44 39 --- 41
R17 | 1517 48 40 24 66 22 --- 19 | 43 41 30 61 34 --- 29
R18 | 4395 41 27 19 26 22 82 13 | 52 28 27 26 24 34 22
R19 | 670 40 16 13 30 15 --- 11 | 54 35 37 33 47 --- 36
R20 | 3708 25 18 43 41 25 --- 15 | 61 49 50 37 68 --- 51
R21 | 943 34 13 22 35 21 --- 11 | 66 45 52 50 49 --- 48
R22 | 2117 38 17 22 27 24 --- 12 | 69 41 43 29 42 --- 41
R23 | 973 23 11 18 46 17 --- 11 | 49 34 30 47 37 --- 31
R24 | 948 14 19 18 40 24 --- 11 | 44 35 37 45 31 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 2500 32 19 23 41 21 181 |T 67 41 43 47 60 52 61
WRMS | 2500 29 17 20 42 21 181 |NE 74 37 38 42 64 34 66
MEDI | 1913 31 17 21 39 21 125 |MD 46 40 41 45 39 34 35
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