[IGSREPORT-20238] Wk 1656 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Oct 20 05:02:11 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1656 (Oct 02, 2011 - Oct 08, 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 2.1656.
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:
igl1656[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1656 in the SP3 format.
igl16567.sum Combination Report for GPS Week 1656.
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). 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 | 166.8 ns
1 | 165.0 ns
2 | 166.7 ns
3 | 167.9 ns
4 | 167.4 ns
5 | 162.7 ns
6 | 165.8 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 1.1656, 1a.1656).
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 2.1656.0-6)
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 3.1656.0-6).
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 1656 summary. (Oct 02, 2011 - Oct 08, 2011)
Table 1.1656.a GPS week : 1656 MJD: 55836.0-55842.0
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 255| -1 0 -3 -4 -67 51 -.16 31 32 | --- --- --- ---
| 1 2 3 31 26 25 .05 | --- ---
emx 146| 1 0 -3 -42 3 14 -.12 36 34 | 165441 -702 5162 8827
| 1 2 2 39 35 73 .06 | 1532 2781
esx 149| -1 0 1 55 63 -44 .40 21 19 | 165534 264 5058 5228
| 0 1 2 20 41 53 .05 | 3172 4034
gfz 196| 0 0 -3 31 0 83 -.22 22 18 | 0 435 4814 7993
| 1 1 2 37 45 30 .05 | 0 2612
grg 130| 0 0 0 -69 -4 32 .17 47 43 | --- --- --- ---
| 3 1 4 71 36 50 .11 | --- ---
iac n/a| 0 0 3 -37 -29 -89 -.15 23 23 | 167281 -512 5055 9188
| 0 1 3 22 17 67 .05 | 1506 1741
mcc n/a| -1 0 37 65 -69 581 .49 147 147 | --- --- --- ---
| 7 8 7 66 61 477 .35 | --- ---
Table 1.1656.b GPS week : 1656 MJD: 55836.0-55842.0
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 | 10 9 8 9 12 13 10 |
R02 | 12 10 11 13 11 11 9 |
R03 | 13 13 15 18 16 15 14 |
R04 | 15 13 13 11 27 15 15 |
R05 | 9 9 12 12 11 11 10 |
R06 | 9 11 11 10 11 11 10 |
R07 | 14 12 13 14 13 10 13 |
R08 | 9 8 10 14 10 13 9 |
R09 | 11 11 11 12 11 12 12 |
R10 | 10 10 11 10 10 9 10 |
R11 | 20 21 19 19 21 24 22 |
R12 | 14 12 18 11 11 10 10 |
R13 | 10 11 9 12 13 15 11 |
R15 | 11 10 13 12 14 14 10 |
R16 | 13 12 11 12 13 12 11 |
R17 | 17 17 10 13 14 15 16 |
R18 | 12 10 11 11 10 12 11 |
R19 | 11 9 14 12 11 13 10 |
R20 | 18 16 19 18 15 11 25 |
R21 | 11 16 15 13 11 10 12 |
R22 | 10 12 12 13 15 13 13 |
R23 | 10 10 8 12 12 12 11 |
R24 | 11 10 10 9 10 10 10 |
Table 1.1656.c GPS week : 1656 MJD: 55836.0-55842.0
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 1656 0 | -44 94 104 -1202 -903 -10620 85.4 2263 2263 | 166823 0
brd 1656 1 | 74 17 39 181 -519 -9749 86.5 2350 2350 | 165045 0
brd 1656 2 | 24 -16 217 -1033 -434 -3715 87.9 1653 1653 | 166718 0
brd 1656 3 | 40 9 80 -1953 -2039 -6598 86.6 1642 1642 | 167918 0
brd 1656 4 | 117 130 93 -2068 -2463 -12850 86.0 1750 1750 | 167427 0
brd 1656 5 | -40 134 304 -3248 -964 -13210 86.7 2489 2489 | 162701 0
brd 1656 6 | -109 32 166 81 -1784 -450 84.7 2630 2630 | 165823 0
-------------+------------------------------------------------------------+----------------
brd 1656 mean| 9 57 143 -1320 -1301 -8170 86.2 2110 2110 | 166065 0
brd 1656 sdev| 78 61 91 1224 791 4790 1.0 418 418 | 1765 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 2.1656.0 GPS week: 1656 Day: 0 MJD: 55836
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 255| -3 1 -4 -11 -95 89 -.14 34 34 | --- --- --- ---
emx 146| 2 -1 -1 -100 12 4 -.08 33 34 | 166341 -551 4965 7706
esx 149| -1 0 3 58 59 -105 .41 20 18 | 166327 341 4912 5082
gfz 196| -1 1 -1 48 36 51 -.27 23 22 | 0 277 4602 7132
grg 130| -2 -1 0 -72 -28 17 .05 36 31 | --- --- --- ---
iac n/a| 1 0 0 -37 -49 10 -.22 23 23 | 167714 377 4922 8029
mcc n/a| -4 3 46 145 -115 145 .12 123 123 | --- --- --- ---
Table 2.1656.1 GPS week: 1656 Day: 1 MJD: 55837
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 255| -1 0 -4 36 -105 22 -.21 30 29 | --- --- --- ---
emx 146| 3 3 0 -23 12 148 -.15 37 39 | 165248 -2167 5309 7945
esx 149| 0 -1 -1 41 9 -56 .43 19 16 | 162419 -111 5133 5340
gfz 196| 0 0 -3 33 41 59 -.29 22 17 | 0 -2488 5087 7439
grg 130| -4 3 -1 -61 10 -3 .05 38 36 | --- --- --- ---
iac n/a| 1 1 5 -56 -30 -71 -.20 23 23 | 167762 -1466 5110 8211
mcc n/a| -6 11 41 11 -43 549 .35 138 138 | --- --- --- ---
Table 2.1656.2 GPS week: 1656 Day: 2 MJD: 55838
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 255| -3 -4 -2 -38 -79 76 -.10 31 32 | --- --- --- ---
emx 146| 1 0 -2 -54 -37 83 -.21 34 30 | 165981 -350 5593 8985
esx 149| 0 0 4 80 35 -107 .42 21 16 | 165004 2869 5375 5489
gfz 196| 1 2 -4 71 49 69 -.16 24 19 | 0 513 4799 8467
grg 130| 1 0 -6 -79 -62 89 .06 52 49 | --- --- --- ---
iac n/a| 0 0 3 -66 -30 -23 -.16 20 20 | 167411 210 5369 9294
mcc n/a| -7 -9 31 54 23 756 .88 193 193 | --- --- --- ---
Table 2.1656.3 GPS week: 1656 Day: 3 MJD: 55839
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 255| -2 -3 -9 -49 -38 24 -.17 32 33 | --- --- --- ---
emx 146| 0 1 -6 -33 60 -47 -.11 38 36 | 165910 2154 6392 12133
esx 149| -1 1 2 54 89 -30 .32 21 22 | 165145 4519 6287 6456
gfz 196| 0 0 -1 68 -25 115 -.24 23 19 | 0 1573 6135 8373
grg 130| 4 0 2 -80 29 -6 .29 46 44 | --- --- --- ---
iac n/a| 0 0 4 -48 -44 -88 -.12 21 21 | 169077 1650 6299 11400
mcc n/a| 7 -12 27 9 -73 1212 .77 236 236 | --- --- --- ---
Table 2.1656.4 GPS week: 1656 Day: 4 MJD: 55840
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 255| 1 -2 -2 -3 -39 56 -.14 32 33 | --- --- --- ---
emx 146| 0 -3 -1 12 -41 -38 -.10 35 34 | 167663 -4854 5073 8786
esx 149| -1 0 0 80 74 -52 .35 23 22 | 172021 -6789 5032 5237
gfz 196| -1 1 -3 -14 0 121 -.18 20 14 | 0 76 4563 8431
grg 130| -2 1 1 -207 -4 101 .28 53 50 | --- --- --- ---
iac n/a| 0 1 3 -9 -29 -178 -.09 23 23 | 168433 -1644 5020 9100
mcc n/a| 9 0 39 11 -156 -143 .71 110 110 | --- --- --- ---
Table 2.1656.5 GPS week: 1656 Day: 5 MJD: 55841
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 255| 0 2 0 10 -51 57 -.14 30 31 | --- --- --- ---
emx 146| 3 0 -7 -85 22 -12 -.02 35 36 | 163325 -2417 4427 8822
esx 149| 0 0 1 50 37 6 .40 22 20 | 162848 -2862 4364 4513
gfz 196| 0 -1 -7 30 -26 58 -.26 20 17 | 0 -2223 4372 8992
grg 130| 1 0 1 19 44 -27 .23 51 44 | --- --- --- ---
iac n/a| 0 2 9 -30 5 -138 -.12 25 25 | 164702 -3430 4354 10263
mcc n/a| -6 8 30 57 -19 505 .64 110 110 | --- --- --- ---
Table 2.1656.6 GPS week: 1656 Day: 6 MJD: 55842
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 255| 0 0 0 24 -62 33 -.25 29 29 | --- --- --- ---
emx 146| 1 -1 -6 -13 -7 -36 -.17 38 28 | 163619 3271 4380 7414
esx 149| -1 0 0 21 135 36 .45 19 17 | 164977 3887 4304 4479
gfz 196| 0 1 0 -21 -74 110 -.16 23 21 | 0 5323 4142 7121
grg 130| -1 2 8 -8 -18 55 .19 52 51 | --- --- --- ---
iac n/a| 1 -1 0 -9 -31 -137 -.13 24 24 | 165874 717 4314 8022
mcc n/a| -3 3 42 171 -103 1047 -.03 118 118 | --- --- --- ---
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 3.1656.0 GPS week: 1656 Day: 0 MJD: 55836
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 856 31 25 22 12 29 22 --- 10 | 37 41 38 35 36 41 --- 33
R02 | 624 44 23 17 24 36 18 --- 11 | 50 22 29 30 25 31 --- 23
XR03E | 4530 --- 14 17 28 48 21 --- 13 | --- 62 76 76 76 66 --- 69
XR04 | 1969 38 --- 27 29 26 31 --- 15 | 20 --- 46 62 47 23 --- 34
R05 | 1796 34 18 15 22 25 11 86 9 | 61 52 38 39 31 43 62 40
R06 | 3430 37 20 16 14 16 14 --- 8 | 54 36 24 34 28 30 --- 29
XR07 | 3437 34 21 30 --- 28 21 --- 13 | 65 54 35 --- 39 42 --- 40
R08 | 2047 28 13 9 22 34 13 65 8 | 47 39 40 43 46 32 35 37
R09E | 865 25 19 21 23 39 18 --- 10 | 63 70 59 65 74 57 --- 59
R10E | 2881 16 24 10 16 44 23 --- 10 | 31 28 27 27 42 23 --- 20
R11E | 1194 43 70 40 24 54 36 126 19 | 53 70 96 77 58 53 142 66
R12E | 1333 24 43 31 26 39 19 --- 13 | 15 23 41 39 45 23 --- 27
R13E | 1708 20 23 14 23 30 18 --- 9 | 40 46 50 60 44 39 --- 45
R15E | 3174 20 18 14 27 26 31 206 10 | 57 65 63 75 65 60 55 62
R16E | 4185 27 26 21 19 54 30 --- 13 | 44 37 43 43 66 38 --- 37
R17 | 1782 57 64 17 32 27 26 --- 16 | 25 60 42 33 38 46 --- 34
R18 | 2043 33 26 15 28 45 14 76 11 | 58 46 33 45 34 28 30 34
R19 | 1349 33 23 15 22 48 11 --- 11 | 48 38 32 39 37 28 --- 31
R20 | 4265 47 48 31 40 23 44 --- 17 | 39 40 37 37 34 26 --- 25
R21 | 958 41 33 12 13 41 10 --- 11 | 51 33 32 31 40 26 --- 30
R22 | 766 31 26 12 21 36 17 --- 10 | 62 39 37 36 37 30 --- 35
R23 | 3039 20 23 21 24 20 19 --- 9 | 45 23 34 35 25 24 --- 26
R24 | 1113 30 28 17 20 22 28 --- 10 | 53 40 45 50 38 34 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 2263 33 33 20 23 36 23 123 |T 46 43 43 45 43 36 64 38
WRMS | 2263 34 34 18 22 31 23 123 |NE 47 40 36 39 35 32 42 32
MEDI | 1796 31 23 17 23 34 19 86 |MD 48 40 38 39 39 32 55 34
Table 3.1656.1 GPS week: 1656 Day: 1 MJD: 55837
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1422 13 13 15 23 36 20 --- 9 | 30 23 28 27 36 34 --- 24
R02 | 577 22 31 11 21 41 19 --- 10 | 33 26 33 36 38 39 --- 29
XR03E | 3208 --- 39 17 19 39 23 --- 12 | --- 131 129 135 145 130 --- 131
XR04 | 2021 28 --- 20 26 30 29 --- 13 | 16 --- 39 46 41 26 --- 27
R05 | 1153 30 19 19 12 28 16 95 9 | 46 42 38 41 29 40 23 36
R06 | 3971 38 27 19 9 32 27 --- 11 | 45 36 30 31 34 31 --- 28
XR07 | 3702 32 29 17 --- 34 15 --- 12 | 50 48 41 --- 36 40 --- 37
R08 | 1627 17 16 12 12 37 16 86 8 | 38 31 40 33 27 41 20 33
R09E | 1476 24 29 22 19 32 26 --- 11 | 55 62 70 69 71 72 --- 64
R10E | 1984 20 21 13 17 48 19 --- 10 | 32 32 28 30 31 24 --- 23
R11E | 1699 35 78 41 45 50 42 235 21 | 41 55 82 85 57 48 132 57
R12E | 1720 18 30 18 21 40 30 --- 11 | 30 42 40 45 44 25 --- 29
R13E | 1536 15 44 19 17 35 22 --- 11 | 36 58 48 43 44 36 --- 39
R15E | 1673 22 22 13 23 39 17 141 10 | 64 61 73 78 75 69 57 68
R16E | 3109 33 29 20 25 40 16 --- 11 | 37 52 49 51 46 46 --- 42
R17 | 2392 61 58 27 27 41 26 --- 17 | 24 47 46 56 30 37 --- 32
R18 | 1049 33 27 16 15 31 12 64 9 | 39 33 14 18 35 19 14 18
R19 | 985 33 17 19 13 24 15 --- 9 | 30 28 25 21 53 20 --- 15
R20 | 5925 26 65 19 27 42 35 --- 15 | 34 35 42 41 40 20 --- 28
XR21 |>>>>> 36 --- 18 30 --- 24 --- 15 | 32 --- 26 37 --- 19 --- 21
R22 | 1014 35 38 13 19 47 13 --- 11 | 34 27 21 13 46 23 --- 16
R23 | 2466 16 45 12 23 30 14 --- 10 | 25 41 23 34 30 16 --- 17
R24 | 2442 31 24 17 17 29 20 --- 9 | 37 34 42 36 42 25 --- 30
------+----------------------------------------------+------------------------------------------
RMS | 2349 30 37 19 22 38 23 138 |T 36 44 43 45 46 38 49 36
WRMS | 2349 29 39 16 17 36 23 138 |NE 34 34 32 33 36 28 19 26
MEDI | 1720 28 29 18 19 36 20 95 |MD 34 41 40 37 40 34 23 29
Table 3.1656.2 GPS week: 1656 Day: 2 MJD: 55838
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1824 19 15 11 16 43 12 --- 7 | 32 48 46 51 32 41 --- 42
R02 | 942 26 25 15 21 42 23 --- 10 | 39 19 36 34 35 29 --- 28
XR03E | 2635 --- 29 19 23 73 25 --- 14 | --- 124 126 128 149 111 --- 121
XR04 | 2679 21 --- 20 23 37 28 --- 12 | 16 --- 36 37 45 30 --- 26
R05 | 1415 39 41 19 21 20 13 105 11 | 46 53 28 21 19 23 66 24
R06 | 2470 35 11 10 20 69 15 --- 11 | 40 36 35 37 55 24 --- 31
XR07 | 8978 32 23 19 --- 57 12 --- 12 | 52 48 37 --- 43 35 --- 35
R08 | 1603 26 20 17 19 48 11 82 9 | 42 40 37 25 35 33 18 30
R09E | 884 24 35 17 22 50 19 --- 11 | 39 40 52 59 48 38 --- 42
R10E | 2368 21 22 12 15 56 27 --- 10 | 16 18 24 25 43 30 --- 19
R11E | 1063 42 67 32 47 49 29 390 19 | 47 64 67 70 43 50 106 49
R12E | 2129 22 20 62 28 73 23 --- 18 | 24 34 65 40 63 32 --- 33
R13E | 1132 17 18 16 18 50 13 --- 8 | 27 29 22 29 43 20 --- 21
R15E | 2056 27 34 14 28 56 25 105 12 | 49 57 54 62 41 34 37 45
R16E | 1299 22 19 12 24 58 21 --- 10 | 28 42 39 38 48 47 --- 35
R17 | 2483 38 20 15 19 30 19 --- 10 | 23 40 33 28 34 28 --- 23
R18 | 1132 34 13 18 9 67 20 82 11 | 45 35 40 33 46 20 19 28
R19 | 1727 42 32 18 16 75 24 --- 13 | 43 37 27 25 57 24 --- 21
R20 | 1852 47 74 22 38 56 32 --- 19 | 43 41 32 28 46 22 --- 20
XR21 |>>>>> 35 --- 16 13 --- 31 --- 14 | 43 --- 35 41 --- 32 --- 33
R22 | 1026 36 47 9 22 33 12 --- 11 | 42 42 24 26 25 22 --- 23
R23 | 1053 26 25 8 16 39 11 --- 8 | 31 19 19 22 31 24 --- 17
R24 | 1318 26 28 14 27 32 15 --- 10 | 34 34 37 43 28 28 --- 29
------+----------------------------------------------+------------------------------------------
RMS | 1653 31 34 21 24 52 20 193 |T 36 42 41 41 45 33 49 33
WRMS | 1653 32 30 16 19 49 20 193 |NE 38 37 33 32 37 27 34 27
MEDI | 1727 26 25 16 21 50 20 105 |MD 39 40 36 34 43 30 37 29
Table 3.1656.3 GPS week: 1656 Day: 3 MJD: 55839
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1578 16 26 12 10 46 17 --- 9 | 42 57 42 46 26 51 --- 42
R02 | 987 20 20 23 16 74 24 --- 13 | 39 33 47 41 54 30 --- 34
XR03E | 2597 --- 56 21 30 55 29 --- 17 | --- 105 109 126 104 92 --- 104
XR04 | 3920 23 --- 20 17 28 26 --- 11 | 21 --- 30 38 45 39 --- 26
R05 | 1209 43 40 20 18 24 16 108 11 | 53 37 26 28 30 37 122 26
R06 | 1535 32 15 19 20 32 20 --- 10 | 52 40 48 40 37 37 --- 38
XR07 | 8511 41 26 19 --- 55 13 --- 14 | 53 49 33 --- 37 28 --- 30
R08 | 1014 31 52 34 21 36 14 88 13 | 52 44 42 27 39 27 30 30
R09E | 681 22 28 20 32 48 18 --- 11 | 54 55 72 56 91 69 --- 60
R10E | 1961 22 20 17 18 38 21 --- 9 | 21 25 33 31 28 32 --- 21
R11E | 1481 42 82 29 27 61 32 494 19 | 73 90 94 77 93 69 308 76
R12E | 1307 25 36 17 21 46 18 --- 11 | 28 29 38 36 59 21 --- 22
R13E | 1104 18 27 21 22 61 14 --- 11 | 51 59 59 53 64 40 --- 47
R15E | 2503 25 28 14 23 55 20 83 11 | 84 87 93 94 95 86 108 87
R16E | 1469 28 29 15 26 53 22 --- 12 | 33 37 45 53 70 31 --- 36
R17 | 3917 50 41 14 26 21 19 --- 12 | 27 27 35 36 30 33 --- 27
R18 | 1288 33 17 16 20 52 18 94 11 | 55 29 34 45 43 18 35 28
R19 | 2209 40 48 18 14 39 15 --- 12 | 43 32 33 23 32 18 --- 21
R20 | 1820 51 65 29 38 38 24 --- 17 | 44 29 35 46 34 30 --- 23
R21 | 714 29 38 32 17 28 31 --- 13 | 42 52 35 30 26 19 --- 23
R22 | 652 34 36 15 25 58 18 --- 12 | 49 43 32 26 53 23 --- 24
R23 | 803 32 22 22 32 28 17 --- 11 | 42 37 25 52 41 17 --- 25
R24 | 974 21 20 13 16 43 20 --- 9 | 35 20 33 39 42 32 --- 29
------+----------------------------------------------+------------------------------------------
RMS | 1641 32 38 21 23 46 20 236 |T 45 46 46 47 51 38 120 38
WRMS | 1641 33 36 22 19 44 20 236 |NE 43 37 35 36 37 29 62 28
MEDI | 1469 29 28 19 21 46 19 94 |MD 43 37 35 40 42 32 108 29
Table 3.1656.4 GPS week: 1656 Day: 4 MJD: 55840
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2210 15 48 24 18 47 20 --- 12 | 40 61 48 30 26 44 --- 37
R02 | 1070 25 21 21 10 56 26 --- 10 | 42 48 41 35 33 31 --- 32
XR03E | 3205 --- 20 28 17 91 21 --- 16 | --- 74 78 95 129 85 --- 84
XR04 | 2312 35 --- 30 75 51 48 --- 26 | 18 --- 23 88 41 22 --- 29
R05 | 703 42 17 17 15 45 15 151 10 | 51 30 33 33 29 33 140 29
R06 | 991 38 13 25 14 42 19 --- 10 | 43 21 26 28 27 25 --- 21
XR07 | 4240 27 32 18 --- 48 17 --- 13 | 36 36 32 --- 51 29 --- 30
R08 | 2249 38 16 16 15 35 16 67 9 | 44 33 33 35 51 21 17 29
R09E | 1039 24 33 15 18 57 21 --- 11 | 26 27 36 37 47 25 --- 27
R10E | 1643 28 19 14 20 41 21 --- 10 | 20 28 29 32 45 23 --- 21
R11E | 1275 51 82 30 32 66 39 130 21 | 64 130 94 107 69 85 188 90
R12E | 734 26 33 22 19 37 21 --- 11 | 19 23 38 35 41 22 --- 23
R13E | 1613 26 31 19 29 54 28 --- 13 | 39 50 43 55 54 25 --- 35
R15E | 2393 18 40 29 29 48 31 78 14 | 78 77 102 105 95 68 46 86
R16E | 1694 34 33 19 15 71 27 --- 13 | 33 52 57 57 74 40 --- 47
R17 | 3911 41 46 32 14 39 19 --- 13 | 26 48 56 45 30 41 --- 38
R18 | 1484 21 24 23 14 42 19 104 9 | 40 26 43 35 38 30 42 32
R19 | 2513 27 19 11 14 68 16 --- 10 | 48 33 32 33 41 25 --- 28
R20 | 1718 27 56 23 28 29 31 --- 14 | 34 42 39 28 33 29 --- 25
R21 | 724 36 26 16 18 37 20 --- 10 | 43 46 31 22 23 24 --- 25
R22 | 988 36 30 31 17 93 19 --- 15 | 46 33 38 26 56 27 --- 26
R23 | 1269 33 19 24 24 63 15 --- 12 | 40 29 32 32 66 19 --- 23
R24 | 1273 22 21 26 17 45 15 --- 10 | 45 47 34 44 34 28 --- 33
------+----------------------------------------------+------------------------------------------
RMS | 1749 32 35 23 20 53 23 110 |T 39 45 44 47 49 34 86 36
WRMS | 1749 33 34 22 14 50 23 110 |NE 39 38 36 36 38 28 66 29
MEDI | 1613 27 26 23 17 48 20 104 |MD 40 36 38 35 41 28 46 29
Table 3.1656.5 GPS week: 1656 Day: 5 MJD: 55841
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1099 14 33 20 14 78 24 --- 13 | 29 51 42 29 44 26 --- 29
R02 | 745 31 31 21 15 39 22 --- 11 | 28 42 29 28 41 21 --- 22
XR03E | 1307 --- 34 19 19 56 31 --- 14 | --- 64 57 65 65 34 --- 51
XR04 | 2534 23 --- 26 30 57 23 --- 15 | 17 --- 28 57 42 19 --- 24
R05 | 966 44 12 14 20 31 18 134 10 | 40 20 22 24 21 22 62 17
R06 | 1063 41 12 22 17 39 15 --- 10 | 35 22 27 31 40 30 --- 23
R07 | 7480 27 21 21 20 28 22 --- 10 | 34 24 30 20 50 34 --- 25
R08 | 1859 32 18 13 12 76 32 84 13 | 37 23 33 29 91 15 15 24
R09E | 1845 28 38 17 20 44 25 --- 12 | 42 38 45 46 62 49 --- 42
R10E | 1197 15 22 15 19 35 17 --- 8 | 20 30 36 30 29 25 --- 24
R11E | 1541 40 97 45 34 48 46 80 23 | 66 80 115 117 79 87 108 91
R12E | 1352 24 19 20 17 40 21 --- 9 | 22 20 35 30 40 25 --- 23
R13E | 2401 30 37 22 15 49 46 --- 14 | 62 67 62 58 42 36 --- 50
R15E | 2873 26 32 23 25 63 29 120 13 | 108 113 117 117 128 107 66 111
R16E | 1647 21 32 22 16 57 22 --- 11 | 30 24 37 33 44 21 --- 24
R17 | 3862 36 52 21 20 72 20 --- 15 | 20 49 43 42 68 26 --- 30
R18 | 1472 24 33 22 25 43 21 123 11 | 45 24 40 45 26 46 16 36
R19 | 1061 18 27 17 33 52 26 --- 12 | 36 33 53 58 44 25 --- 37
R20 | 4295 18 40 20 17 32 27 --- 11 | 21 35 25 34 37 26 --- 21
R21 | 887 36 16 21 9 48 15 --- 10 | 40 31 23 28 27 20 --- 20
R22 | 936 38 27 18 20 57 22 --- 12 | 43 27 25 38 36 23 --- 26
R23 | 1066 37 21 26 19 43 16 --- 11 | 41 41 39 33 28 20 --- 28
R24 | 1253 14 27 15 18 49 16 --- 9 | 30 50 31 31 37 35 --- 30
------+----------------------------------------------+------------------------------------------
RMS | 2488 30 35 22 20 51 25 110 |T 38 41 43 44 48 33 53 35
WRMS | 2488 31 36 20 17 44 25 110 |NE 33 33 32 35 42 25 31 26
MEDI | 1352 27 27 21 19 48 22 120 |MD 35 33 36 33 42 26 62 26
Table 3.1656.6 GPS week: 1656 Day: 6 MJD: 55842
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1105 17 17 21 16 47 27 --- 10 | 42 53 57 50 21 42 --- 44
R02 | 1122 22 18 17 15 50 15 --- 9 | 49 32 32 35 48 38 --- 32
XR03E | 1530 --- 34 13 19 74 15 --- 13 | --- 29 37 37 50 35 --- 32
XR04 | 1592 40 --- 16 39 40 19 --- 15 | 17 --- 38 59 48 26 --- 28
R05 | 815 28 13 11 18 57 20 136 10 | 63 41 38 35 39 44 51 38
R06 | 1218 26 28 6 25 36 17 --- 9 | 53 32 31 35 27 35 --- 31
R07 | 6346 22 18 19 46 53 15 --- 13 | 52 40 30 14 43 39 --- 34
R08 | 1206 33 19 18 8 30 12 110 9 | 50 39 40 33 45 29 22 33
R09E | 1510 22 39 24 26 34 17 --- 11 | 41 48 55 66 54 48 --- 49
R10E | 1445 17 30 13 17 44 19 --- 9 | 25 31 29 32 38 29 --- 25
R11E | 2068 55 85 36 33 40 45 112 22 | 71 84 88 84 78 90 89 79
R12E | 2544 21 24 15 19 36 20 --- 9 | 24 21 34 33 42 22 --- 23
R13E | 2280 21 18 16 22 64 15 --- 10 | 33 28 39 41 33 28 --- 30
R15E | 3436 21 23 17 19 41 27 56 10 | 63 66 68 76 71 73 69 68
R16E | 815 18 25 23 13 56 26 --- 11 | 22 29 40 31 58 25 --- 27
R17 | 6217 32 33 22 33 79 32 --- 15 | 23 40 44 43 57 36 --- 31
R18 | 2347 29 24 14 16 57 13 152 10 | 62 39 45 49 26 40 25 43
R19 | 1572 21 30 17 13 48 19 --- 10 | 56 28 57 47 48 42 --- 44
R20 | 3925 32 112 22 38 96 42 --- 24 | 45 47 59 53 38 43 --- 43
R21 | 783 36 15 15 24 55 21 --- 11 | 55 36 33 43 39 25 --- 32
R22 | 941 37 33 11 22 50 33 --- 13 | 65 28 37 51 52 25 --- 36
R23 | 997 39 17 21 14 37 20 --- 10 | 47 23 23 23 40 18 --- 20
R24 | 1229 21 22 29 16 39 13 --- 10 | 41 36 38 28 39 28 --- 30
------+----------------------------------------------+------------------------------------------
RMS | 2629 29 38 19 23 52 24 118 |T 45 38 43 43 44 37 51 37
WRMS | 2629 29 28 17 21 51 24 118 |NE 48 36 40 39 40 34 32 34
MEDI | 1510 22 24 17 19 48 19 112 |MD 47 36 38 41 43 35 51 32
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