[IGSREPORT-23502] Wk 1837 IGLOS Final Orbits
IGS ACC
igs.acc at noaa.gov
Thu Apr 9 17:08:02 PDT 2015
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1837 (Mar 22, 2015 - Mar 28, 2015)
Contact: igs.acc 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 2.1837.
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:
igl1837[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1837 in the SP3 format.
igl18377.sum Combination Report for GPS Week 1837.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 9.0 ns
1 | 6.6 ns
2 | -0.3 ns
3 | 7.7 ns
4 | 0.9 ns
5 | 0.3 ns
6 | -4.0 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
----+--------+---------------
1 | COD | R11
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 1.1837, 1a.1837).
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 2.1837.0-6)
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 3.1837.0-6).
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 1837 summary. (Mar 22, 2015 - Mar 28, 2015)
Table 1.1837.a GPS week : 1837 MJD: 57103.0-57109.0
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| -2 0 -7 24 -1 39 .31 58 47 | --- --- --- ---
| 1 1 2 32 12 37 .05 | --- ---
cof n/a| -2 0 -10 22 5 37 .34 61 49 | --- --- --- ---
| 1 1 4 32 29 50 .08 | --- ---
esx n/a| 0 0 -2 -4 0 -1 -.02 19 18 | 866 -2183 3898 7860
| 0 1 1 11 23 39 .03 | 7218 3453
gfz n/a| 0 -1 5 33 40 45 .19 20 17 | 0 -1004 3871 7222
| 1 1 2 15 22 34 .04 | 0 2482
grg n/a| -2 2 10 -43 0 42 -.31 35 30 | -999999 -955 3912 58754
| 1 1 2 26 26 97 .08 | 0 2424
iac n/a| 1 0 -5 -20 -20 -56 -.05 19 19 | 4253 -150 3898 7424
| 1 0 2 32 16 67 .03 | 4712 1144
mcc n/a| -4 3 -23 -48 -69 -70 -.40 155 155 | --- --- --- ---
| 6 8 13 146 82 636 .39 | --- ---
Table 1.1837.b GPS week : 1837 MJD: 57103.0-57109.0
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 | 14 16 17 17 16 17 13 |
R02 | 9 12 11 10 12 9 10 |
R03 | 12 11 11 12 11 10 10 |
R04 | 12 11 12 10 11 11 12 |
R05 | 12 17 17 14 15 16 17 |
R06 | 10 11 13 10 12 10 11 |
R07 | 12 14 12 12 12 12 12 |
R08 | 10 11 14 9 12 11 14 |
R09 | 15 14 13 12 14 12 12 |
R10 | 10 12 12 10 12 13 11 |
R11 | 24 13 26 23 22 23 36 |
R12 | 23 25 23 20 23 23 24 |
R13 | 13 10 11 11 12 16 26 |
R14 | 17 19 15 12 17 24 11 |
R15 | 15 16 14 13 12 12 13 |
R16 | 10 9 9 11 9 9 10 |
R17 | 7 10 13 8 9 8 8 |
R18 | 9 8 10 8 9 9 6 |
R19 | 11 8 8 7 9 7 7 |
R20 | 14 11 11 10 10 16 11 |
R21 | 12 9 9 9 7 11 12 |
R22 | 9 9 9 13 9 8 9 |
R23 | 10 12 11 12 10 9 9 |
R24 | 10 10 9 11 10 9 7 |
R25 | 0 0 0 0 0 0 0 |
R26 | 0 0 0 0 0 0 0 |
Table 1.1837.c GPS week : 1837 MJD: 57103.0-57109.0
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 1837 0 | -27 -33 14 -1522 -1157 -6143 84.0 1720 1720 | 9034 0
brd 1837 1 | 24 22 16 -528 -656 -5027 82.5 1996 1996 | 6610 0
brd 1837 2 | -45 112 40 -1201 -631 -3818 84.7 4325 4325 | -262 0
brd 1837 3 | -17 -2 100 984 -114 -5611 84.4 2849 2849 | 7671 0
brd 1837 4 | -67 1 22 1004 -68 -3697 84.7 1726 1726 | 909 0
brd 1837 5 | 3 7 8 292 1207 -1262 85.2 1226 1226 | 266 0
brd 1837 6 | 15 52 -35 -211 929 838 84.2 2207 2207 | -4003 0
-------------+------------------------------------------------------------+----------------
brd 1837 mean| -16 23 23 -168 -70 -3531 84.2 2292 2292 | 2889 0
brd 1837 sdev| 33 47 41 995 863 2507 .9 1026 1026 | 4876 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 2.1837.0 GPS week: 1837 Day: 0 MJD: 57103
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -2 -11 74 -26 -29 .35 59 46 | --- --- --- ---
cof n/a| 0 1 -17 19 -36 -29 .41 60 47 | --- --- --- ---
esx n/a| 1 0 0 -15 -29 12 -.01 19 17 | 5105 2721 3908 6985
gfz n/a| 0 -3 5 8 37 34 .23 19 19 | 0 2375 3861 6297
grg n/a| -3 5 8 1 14 220 -.35 35 35 | -999999 2483 3913 56819
iac n/a| 1 1 -4 -11 3 -103 -.09 18 18 | 9986 1367 3916 6295
mcc n/a| -4 1 -40 -36 10 1082 -.76 256 256 | --- --- --- ---
Table 2.1837.1 GPS week: 1837 Day: 1 MJD: 57104
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 1 -7 39 2 44 .22 58 44 | --- --- --- ---
cof n/a| -3 0 -6 19 12 37 .43 62 47 | --- --- --- ---
esx n/a| 0 0 -1 1 -11 -21 -.01 20 19 | 13352 -3901 3567 6902
gfz n/a| 0 -1 6 37 69 8 .13 20 17 | 0 -2653 3572 6729
grg n/a| -2 3 7 -62 14 83 -.18 35 33 | -999999 -2591 3545 41572
iac n/a| 2 0 -5 -38 -35 -17 -.07 18 18 | 8543 -1786 3573 7277
mcc n/a| -7 4 -7 -157 -113 -189 -.94 148 148 | --- --- --- ---
Table 2.1837.2 GPS week: 1837 Day: 2 MJD: 57105
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 2 -5 21 12 6 .28 59 45 | --- --- --- ---
cof n/a| -4 2 -8 35 -1 -33 .38 63 48 | --- --- --- ---
esx n/a| 1 -1 -1 2 -11 -24 -.07 17 17 | -3683 -2995 4331 7918
gfz n/a| 1 0 3 57 63 23 .14 20 15 | 0 -1775 4297 7192
grg n/a| -2 0 10 -34 -53 -87 -.24 34 31 | -999999 -1672 4393 38068
iac n/a| 0 0 -8 -69 -9 51 -.01 21 21 | -232 75 4313 7446
mcc n/a| -13 7 -20 -144 -199 -627 -.60 140 140 | --- --- --- ---
Table 2.1837.3 GPS week: 1837 Day: 3 MJD: 57106
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 -6 12 4 65 .29 56 52 | --- --- --- ---
cof n/a| 0 1 -6 43 27 54 .21 57 51 | --- --- --- ---
esx n/a| 1 0 -3 -20 -5 9 -.04 18 18 | 4544 -226 3825 7665
gfz n/a| 0 -2 7 29 40 33 .19 20 19 | 0 165 3805 6976
grg n/a| -3 2 11 -35 25 45 -.29 36 32 | -999999 40 3834 77479
iac n/a| 0 0 -5 -2 -32 -58 -.07 15 15 | 9039 -442 3820 7089
mcc n/a| 2 5 -7 246 10 -833 .02 102 102 | --- --- --- ---
Table 2.1837.4 GPS week: 1837 Day: 4 MJD: 57107
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 -6 14 -10 64 .30 58 44 | --- --- --- ---
cof n/a| -2 0 -15 19 35 89 .32 61 47 | --- --- --- ---
esx n/a| 0 0 -3 -11 -6 76 -.03 19 19 | -2931 834 3722 6833
gfz n/a| 0 0 2 24 31 95 .17 20 17 | 0 479 3704 5984
grg n/a| -1 1 14 -83 5 -31 -.35 30 26 | -999999 932 3727 53577
iac n/a| 2 0 -3 29 -21 -163 -.01 19 19 | 1402 595 3742 6107
mcc n/a| 5 -3 -29 7 -127 -263 .08 182 182 | --- --- --- ---
Table 2.1837.5 GPS week: 1837 Day: 5 MJD: 57108
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 -8 -32 0 48 .36 58 45 | --- --- --- ---
cof n/a| 0 0 -10 -42 30 67 .29 63 47 | --- --- --- ---
esx n/a| 0 0 -3 8 41 -26 -.03 19 16 | -8114 -4452 4335 8708
gfz n/a| -3 0 7 30 0 94 .24 21 17 | 0 -345 4261 8095
grg n/a| 0 2 10 -36 -6 51 -.34 35 25 | -999999 -963 4330 63781
iac n/a| 2 0 -2 -8 -40 -72 -.05 19 19 | 1726 576 4334 8325
mcc n/a| -4 18 -37 -171 5 16 -.25 96 96 | --- --- --- ---
Table 2.1837.6 GPS week: 1837 Day: 6 MJD: 57109
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 -3 41 4 73 .36 58 54 | --- --- --- ---
cof n/a| -3 0 -7 63 -28 80 .37 60 55 | --- --- --- ---
esx n/a| 2 2 0 6 18 -38 .02 21 18 | -2211 -7263 3601 10014
gfz n/a| -1 -2 4 46 43 30 .21 21 17 | 0 -5275 3597 9287
grg n/a| -1 0 12 -55 -6 13 -.44 40 28 | -999999 -4919 3644 79988
iac n/a| 0 1 -9 -42 -7 -34 -.04 21 21 | -691 -1440 3588 9430
mcc n/a| -11 -8 -24 -87 -76 318 -.36 160 160 | --- --- --- ---
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 3.1837.0 GPS week: 1837 Day: 0 MJD: 57103
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg iac mcc IGL | cod cof esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1048 67 67 16 23 32 17 --- 13 | 82 92 43 36 39 --- --- 0
R02 | 2337 35 41 16 13 24 15 460 9 | 125 126 112 110 107 --- 53 0
R03 | 663 39 30 18 18 32 25 --- 12 | 104 104 102 82 99 --- --- 0
R04 | 988 49 45 16 26 26 13 --- 11 | 100 98 76 61 71 --- --- 0
R05 | 3338 54 37 18 18 28 22 --- 12 | 105 102 91 77 87 --- --- 0
R06 | 754 39 45 14 17 31 14 --- 10 | 96 98 84 68 65 --- --- 0
R07 | 881 60 56 14 19 26 14 306 11 | 111 111 88 79 66 --- 124 0
R08 | 698 53 61 12 23 22 8 --- 10 | 114 123 105 96 85 --- --- 0
R09 | 816 65 77 29 17 38 18 --- 15 | 31 51 74 57 46 --- --- 0
R10 | 1239 20 27 19 16 25 19 --- 9 | 48 50 41 31 28 --- --- 0
R11 | 3881 155 162 17 24 48 23 --- 23 | 104 110 52 78 81 --- --- 0
R12 | 574 148 136 17 30 42 18 89 22 | 104 97 49 80 71 --- 46 0
R13 | 1137 51 52 20 17 46 17 --- 13 | 63 64 42 37 47 --- --- 0
R14 | 744 30 45 33 26 44 36 --- 17 | 49 67 56 56 50 --- --- 0
R15 | 3122 35 42 21 25 52 23 --- 14 | 50 55 37 28 36 --- --- 0
R16 | 715 22 21 23 15 27 13 --- 10 | 39 44 47 29 25 --- --- 0
R17 | 1386 21 28 10 10 23 15 78 7 | 58 65 59 57 52 --- 70 0
R18 | 1821 28 30 17 13 24 15 91 9 | 60 60 67 58 44 --- 34 0
R19 | 605 33 31 11 14 48 15 --- 11 | 60 59 50 47 66 --- --- 0
R20 | 2721 40 37 24 20 40 22 --- 13 | 59 56 45 44 48 --- --- 0
R21 | 1011 30 35 18 21 33 21 --- 11 | 64 65 57 54 45 --- --- 0
R22 | 603 36 43 16 12 27 14 --- 9 | 70 75 55 49 39 --- --- 0
R23 | 649 22 18 21 15 35 15 --- 10 | 19 26 42 37 17 --- --- 0
R24 | 2352 26 20 19 18 34 12 --- 10 | 57 51 54 45 29 --- --- 0
XR25 |15078 --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- --- 0
XR26 |14714 --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- --- 0
------+----------------------------------------------+------------------------------------------
RMS | 1720 59 60 19 19 35 18 256 |T 73 77 63 58 55 --- 65 ---
WRMS | 1720 46 47 17 19 35 18 256 |NE 73 77 63 58 55 --- 65 ---
MEDI | 1011 36 41 17 18 32 15 91 |MD 63 65 55 56 48 --- 53 ---
Table 3.1837.1 GPS week: 1837 Day: 1 MJD: 57104
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg iac mcc IGL | cod cof esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 771 74 85 18 26 27 23 --- 15 | 69 77 35 31 35 --- --- 0
R02 | 1078 38 40 20 19 23 21 180 11 | 101 102 101 93 88 --- 75 0
R03 | 963 28 32 15 15 33 19 --- 10 | 108 115 105 102 111 --- --- 0
R04 | 786 37 46 15 22 36 8 --- 11 | 75 80 59 60 49 --- --- 0
R05 | 1956 55 94 20 25 54 27 --- 16 | 77 110 62 64 60 --- --- 0
R06 | 1639 42 42 15 19 30 14 --- 10 | 77 77 56 51 56 --- --- 0
R07 | 578 61 64 12 26 37 13 225 13 | 91 91 64 56 66 --- 129 0
R08 | 746 45 44 14 24 27 13 --- 11 | 99 98 73 65 80 --- --- 0
R09 | 774 51 59 23 17 36 22 --- 13 | 27 31 47 33 27 --- --- 0
R10 | 1679 34 42 20 19 28 21 --- 11 | 29 31 33 24 33 --- --- 0
R11 | 779 173 173 19 17 43 15 --- 12 | 96 98 58 71 77 --- --- 0
R12 | 678 135 134 22 28 36 33 104 24 | 89 88 40 53 46 --- 37 0
R13 | 789 34 39 15 18 29 14 --- 10 | 48 54 28 38 40 --- --- 0
R14 | 954 36 41 46 32 48 29 --- 19 | 48 70 77 44 52 --- --- 0
R15 | 8346 31 32 24 26 58 22 --- 15 | 43 44 39 37 38 --- --- 0
R16 | 592 20 20 17 12 32 9 --- 8 | 29 38 34 29 28 --- --- 0
R17 | 597 22 21 18 16 33 14 95 9 | 38 36 43 41 24 --- 48 0
R18 | 1402 23 33 11 13 23 14 82 8 | 41 55 40 42 31 --- 22 0
R19 | 773 13 18 13 13 29 12 --- 7 | 40 43 43 52 50 --- --- 0
R20 | 1273 37 43 21 17 28 16 --- 11 | 42 46 38 30 29 --- --- 0
R21 | 993 28 30 13 19 27 14 --- 9 | 44 42 27 40 22 --- --- 0
R22 | 735 30 33 15 8 32 10 --- 9 | 44 46 37 36 26 --- --- 0
R23 | 642 11 9 22 17 39 22 --- 11 | 18 24 30 25 18 --- --- 0
R24 | 1559 30 31 14 15 34 11 --- 9 | 42 48 34 32 22 --- --- 0
XR25 |14346 --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- --- 0
XR26 | 9779 --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- --- 0
------+----------------------------------------------+------------------------------------------
RMS | 1996 58 62 20 20 35 18 148 |T 58 64 50 47 46 --- 62 ---
WRMS | 1996 44 47 19 17 33 18 148 |NE 58 64 50 47 46 --- 62 ---
MEDI | 789 34 40 17 18 32 14 104 |MD 44 54 40 41 38 --- 48 ---
Table 3.1837.2 GPS week: 1837 Day: 2 MJD: 57105
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg iac mcc IGL | cod cof esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 735 88 94 20 28 25 27 --- 16 | 84 91 45 33 32 --- --- 0
R02 | 6603 39 47 16 20 36 15 87 11 | 110 111 96 93 73 --- 42 0
R03 | 2416 32 40 13 23 27 19 --- 10 | 84 88 71 72 62 --- --- 0
R04 | 1189 44 42 16 21 36 15 --- 11 | 88 85 61 62 64 --- --- 0
R05 | 1046 74 70 18 27 47 26 --- 16 | 105 104 66 65 60 --- --- 0
R06 |13821 39 46 19 19 32 25 --- 12 | 82 86 64 59 45 --- --- 0
R07 | 2958 58 55 15 22 25 13 251 11 | 99 98 75 68 55 --- 68 0
R08 | 764 41 40 20 25 41 20 --- 13 | 95 91 75 73 85 --- --- 0
R09 | 737 54 52 21 14 30 23 --- 12 | 36 39 50 43 33 --- --- 0
R10 | 1054 38 39 17 22 32 16 --- 11 | 42 49 38 26 23 --- --- 0
R11 | 1966 151 158 15 31 64 27 --- 25 | 85 92 52 74 79 --- --- 0
R12 | 639 142 155 16 24 44 29 118 23 | 93 107 53 65 57 --- 25 0
R13 |10570 31 29 18 21 25 21 --- 11 | 46 49 38 35 46 --- --- 0
R14 | 1171 38 47 25 26 33 33 --- 14 | 53 79 76 60 69 --- --- 0
R15 | 6871 31 25 16 25 50 23 --- 13 | 44 39 32 35 27 --- --- 0
R16 | 820 23 24 16 18 21 18 --- 9 | 31 30 34 32 25 --- --- 0
R17 | 569 23 25 25 18 33 25 83 12 | 42 45 55 47 37 --- 35 0
R18 | 3901 21 19 19 12 23 20 85 9 | 51 47 59 43 42 --- 14 0
R19 | 1341 19 23 10 11 24 16 --- 7 | 52 55 47 50 48 --- --- 0
R20 | 916 54 65 14 12 29 16 --- 11 | 57 63 49 52 54 --- --- 0
R21 | 1073 22 27 19 10 29 13 --- 9 | 49 57 52 47 40 --- --- 0
R22 | 2823 46 42 11 9 17 18 --- 9 | 56 54 29 27 29 --- --- 0
R23 | 963 12 20 12 11 40 26 --- 10 | 23 27 27 26 23 --- --- 0
R24 | 934 36 45 16 14 20 11 --- 8 | 50 62 43 39 48 --- --- 0
XR25 |21700 --- --- --- --- --- 7 --- 0 | --- --- --- --- --- --- --- 0
XR26 | ---- --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- --- 0
------+----------------------------------------------+------------------------------------------
RMS | 4324 59 63 17 20 34 21 140 |T 64 68 53 51 48 --- 36 ---
WRMS | 4324 45 48 17 15 31 21 140 |NE 64 68 53 51 48 --- 36 ---
MEDI | 1171 38 42 16 20 30 19 87 |MD 53 62 52 47 46 --- 35 ---
Table 3.1837.3 GPS week: 1837 Day: 3 MJD: 57106
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg iac mcc IGL | cod cof esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 844 99 107 21 24 46 17 --- 17 | 97 108 52 46 32 --- --- 0
R02 | 1547 31 36 12 24 33 11 65 10 | 113 115 110 104 108 --- 64 0
R03 | 1835 24 31 15 25 39 22 --- 11 | 117 114 121 113 139 --- --- 0
R04 | 1637 43 56 15 17 21 18 --- 10 | 98 110 84 76 78 --- --- 0
R05 | 968 59 74 22 22 34 21 --- 13 | 100 109 76 93 85 --- --- 0
R06 | 1534 36 27 15 15 32 12 --- 9 | 92 86 73 70 81 --- --- 0
R07 | 1002 55 65 14 22 30 14 116 11 | 100 107 80 69 67 --- 64 0
R08 | 3085 41 43 17 18 20 11 --- 9 | 101 105 91 74 84 --- --- 0
R09 | 1154 59 56 20 17 33 15 --- 12 | 29 34 59 46 50 --- --- 0
R10 | 1372 35 41 13 24 35 8 --- 10 | 53 61 41 33 30 --- --- 0
R11 | 1382 139 121 19 30 65 17 --- 22 | 89 81 58 74 78 --- --- 0
R12 | 1101 138 129 15 26 33 15 150 20 | 89 83 50 65 58 --- 32 0
R13 | 7164 27 19 15 19 47 11 --- 10 | 42 46 36 43 40 --- --- 0
R14 | 1823 43 37 23 21 32 19 --- 12 | 51 57 67 55 70 --- --- 0
R15 | 4842 36 44 17 28 44 15 --- 12 | 51 59 39 37 51 --- --- 0
R16 | 945 22 26 26 21 30 11 --- 10 | 42 46 50 24 26 --- --- 0
R17 | 1096 19 29 17 15 18 12 75 7 | 44 55 33 48 51 --- 35 0
R18 | 781 24 28 19 12 20 13 77 8 | 47 50 37 37 30 --- 21 0
R19 | 1255 19 21 13 17 17 11 --- 7 | 57 59 59 56 51 --- --- 0
R20 | 8836 28 40 21 9 19 20 --- 9 | 61 85 37 56 43 --- --- 0
R21 | 954 31 27 13 13 39 8 --- 9 | 66 63 50 57 25 --- --- 0
R22 | 1376 39 41 24 12 48 17 --- 12 | 64 64 55 48 25 --- --- 0
R23 | 686 16 22 22 20 50 13 --- 12 | 27 37 41 31 20 --- --- 0
R24 | 1326 36 33 22 12 27 18 --- 10 | 57 56 57 46 64 --- --- 0
XR25 |15890 --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- --- 0
XR26 |15432 --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- --- 0
------+----------------------------------------------+------------------------------------------
RMS | 2849 56 57 18 20 36 15 102 |T 70 74 60 58 57 --- 43 ---
WRMS | 2849 52 51 18 19 32 15 102 |NE 70 74 60 58 57 --- 43 ---
MEDI | 1372 36 37 17 19 33 13 77 |MD 61 63 55 55 51 --- 35 ---
Table 3.1837.4 GPS week: 1837 Day: 4 MJD: 57107
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg iac mcc IGL | cod cof esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 3034 100 112 18 20 24 23 --- 16 | 92 103 33 28 27 --- --- 0
R02 | 1731 32 33 19 22 32 20 98 11 | 110 109 104 102 93 --- 69 0
R03 | 1392 19 26 17 26 31 20 --- 11 | 73 77 75 74 62 --- --- 0
R04 | 723 49 47 12 21 27 18 --- 11 | 99 100 75 70 76 --- --- 0
R05 | 897 68 70 19 26 35 24 --- 15 | 97 100 60 65 72 --- --- 0
R06 | 2163 38 43 15 20 32 23 --- 11 | 88 94 69 72 77 --- --- 0
R07 | 672 57 56 13 19 33 18 354 12 | 92 92 74 68 64 --- 179 0
R08 | 831 47 52 19 19 25 23 --- 12 | 88 92 74 63 66 --- --- 0
R09 | 1187 68 80 31 14 22 18 --- 14 | 31 39 67 45 47 --- --- 0
R10 | 1102 49 45 18 18 36 15 --- 12 | 62 60 36 26 26 --- --- 0
R11 | 920 140 141 18 24 45 14 --- 21 | 87 90 43 55 56 --- --- 0
R12 | 1167 138 131 20 34 46 21 147 22 | 82 78 52 68 60 --- 41 0
R13 | 692 34 40 22 16 34 17 --- 11 | 32 38 25 36 48 --- --- 0
R14 | 1287 31 50 34 28 56 23 --- 17 | 34 46 60 46 79 --- --- 0
R15 | 4288 40 38 23 20 22 18 --- 11 | 51 52 40 30 27 --- --- 0
R16 | 1131 27 32 19 15 21 17 --- 9 | 46 56 43 30 25 --- --- 0
R17 | 1226 15 19 16 24 9 16 60 8 | 42 38 52 35 52 --- 36 0
R18 | 971 24 29 18 15 17 15 78 8 | 45 46 40 24 25 --- 47 0
R19 | 1082 26 31 11 16 28 14 --- 8 | 48 49 39 34 25 --- --- 0
R20 | 3236 34 42 20 17 18 15 --- 9 | 46 34 43 30 38 --- --- 0
R21 | 1725 21 28 11 10 13 16 --- 6 | 57 61 54 60 64 --- --- 0
R22 | 2336 21 23 16 13 28 18 --- 9 | 53 53 53 56 48 --- --- 0
R23 | 752 22 27 15 12 33 16 --- 9 | 27 30 26 22 21 --- --- 0
R24 | 685 30 45 12 15 20 25 --- 9 | 47 59 35 40 34 --- --- 0
XR25 |15482 --- --- --- --- --- 9 --- 0 | --- --- --- --- --- --- --- 0
XR26 |13872 --- --- --- --- --- 9 --- 0 | --- --- --- --- --- --- --- 0
------+----------------------------------------------+------------------------------------------
RMS | 1726 58 61 19 20 30 19 182 |T 63 66 53 49 50 --- 74 ---
WRMS | 1726 44 47 19 17 26 19 182 |NE 63 66 53 49 50 --- 74 ---
MEDI | 1167 34 42 18 19 28 18 98 |MD 53 59 52 45 48 --- 47 ---
Table 3.1837.5 GPS week: 1837 Day: 5 MJD: 57108
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg iac mcc IGL | cod cof esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 845 95 114 15 27 33 17 --- 16 | 73 89 28 31 33 --- --- 0
R02 | 1574 34 40 17 13 21 14 50 9 | 107 108 107 102 100 --- 90 0
R03 | 812 29 28 20 15 23 19 --- 10 | 89 89 90 81 78 --- --- 0
R04 | 883 51 56 14 21 22 19 --- 11 | 95 96 70 75 71 --- --- 0
R05 | 779 55 88 24 38 27 25 --- 15 | 95 116 94 90 90 --- --- 0
R06 | 1308 38 41 19 15 25 13 --- 10 | 97 91 84 84 87 --- --- 0
R07 | 702 52 51 16 19 30 15 155 11 | 110 109 78 81 77 --- 155 0
R08 | 941 43 49 17 19 29 15 --- 11 | 114 119 105 100 88 --- --- 0
R09 | 830 62 54 22 12 18 11 --- 11 | 26 27 52 38 42 --- --- 0
R10 | 729 32 46 28 14 35 17 --- 12 | 50 65 48 31 21 --- --- 0
R11 | 965 150 162 13 20 45 24 --- 23 | 94 105 45 46 53 --- --- 0
R12 | 1085 136 135 19 26 49 23 101 22 | 84 87 41 46 42 --- 77 0
R13 | 1568 63 35 20 24 49 18 --- 15 | 69 67 58 75 96 --- --- 0
R14 | 1315 45 59 22 32 103 25 --- 23 | 37 44 53 51 116 --- --- 0
R15 | 3603 39 43 21 25 24 18 --- 11 | 44 47 41 27 25 --- --- 0
R16 | 743 25 33 16 17 21 12 --- 8 | 41 46 35 26 27 --- --- 0
R17 | 878 23 22 10 17 13 15 69 7 | 35 38 31 37 34 --- 18 0
R18 | 1222 12 11 17 15 21 18 67 8 | 35 35 47 49 40 --- 28 0
R19 | 814 16 15 12 20 6 14 --- 7 | 40 43 36 27 43 --- --- 0
R20 | 706 39 51 36 23 26 33 --- 15 | 34 60 55 51 29 --- --- 0
R21 | 807 31 29 17 18 18 27 --- 10 | 48 49 47 54 41 --- --- 0
R22 | 1084 16 18 13 15 19 16 --- 7 | 45 50 40 61 61 --- --- 0
R23 | 833 14 22 11 14 21 24 --- 9 | 19 22 15 19 14 --- --- 0
R24 | 866 26 21 15 13 28 15 --- 9 | 37 31 28 36 30 --- --- 0
XR25 |11696 --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- --- 0
XR26 |10433 --- --- --- --- --- 5 --- 0 | --- --- --- --- --- --- --- 0
------+----------------------------------------------+------------------------------------------
RMS | 1226 58 63 19 21 35 19 96 |T 63 68 55 54 55 --- 73 ---
WRMS | 1226 45 47 16 17 25 19 96 |NE 63 68 55 54 55 --- 73 ---
MEDI | 878 38 41 17 18 24 17 69 |MD 48 60 47 49 42 --- 77 ---
Table 3.1837.6 GPS week: 1837 Day: 6 MJD: 57109
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof esx gfz grg iac mcc IGL | cod cof esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1122 73 68 15 22 24 12 --- 13 | 87 92 31 28 23 --- --- 0
R02 | 6584 31 25 11 17 36 10 193 9 | 110 106 98 92 80 --- 67 0
R03 | 3141 39 39 16 20 26 14 --- 10 | 78 77 69 59 57 --- --- 0
R04 | 758 46 45 15 25 24 17 --- 11 | 102 103 77 73 66 --- --- 0
R05 | 589 40 24 23 33 48 29 --- 16 | 102 106 78 86 74 --- --- 0
R06 | 2515 31 38 18 22 21 22 --- 11 | 89 95 75 67 68 --- --- 0
R07 | 1182 49 65 21 18 29 17 119 12 | 112 118 87 74 60 --- 88 0
R08 | 836 53 58 26 18 33 18 --- 13 | 122 127 92 87 74 --- --- 0
R09 | 1807 52 58 27 11 23 14 --- 12 | 30 34 72 53 43 --- --- 0
R10 | 1295 31 30 18 12 36 16 --- 10 | 56 57 50 34 32 --- --- 0
R11 | 904 163 161 27 39 137 22 --- 36 | 111 115 47 68 112 --- --- 0
R12 | 2477 146 164 15 25 41 24 230 23 | 114 127 49 64 55 --- 61 0
R13 | 1134 58 63 48 42 45 60 --- 25 | 102 134 119 130 114 --- --- 0
R14 | 1199 31 27 23 16 20 21 --- 10 | 44 51 66 48 52 --- --- 0
R15 | 1317 44 43 29 21 29 18 --- 13 | 58 57 42 28 25 --- --- 0
R16 | 685 23 16 23 20 21 12 --- 9 | 46 44 47 37 37 --- --- 0
R17 | 515 20 24 16 13 21 14 84 8 | 57 57 60 51 52 --- 45 0
R18 | 2783 17 20 11 7 21 9 126 6 | 53 54 56 47 38 --- 56 0
R19 | 860 20 28 11 18 12 9 --- 6 | 55 56 51 39 42 --- --- 0
R20 | 1159 34 29 21 16 28 16 --- 10 | 61 54 51 39 51 --- --- 0
R21 | 1015 21 18 24 16 27 23 --- 11 | 72 71 75 66 47 --- --- 0
R22 | 4592 12 11 18 14 26 18 --- 9 | 74 69 79 80 66 --- --- 0
R23 | 1827 15 17 10 19 31 16 --- 9 | 24 24 30 29 14 --- --- 0
R24 | 847 20 20 11 13 17 13 --- 6 | 57 56 44 48 39 --- --- 0
XR25 |12430 --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- --- 0
XR26 | 8786 --- --- --- --- --- 6 --- 0 | --- --- --- --- --- --- --- 0
------+----------------------------------------------+------------------------------------------
RMS | 2207 58 60 21 21 40 21 160 |T 75 78 64 59 55 --- 63 ---
WRMS | 2207 54 55 18 17 28 21 160 |NE 75 78 64 59 55 --- 63 ---
MEDI | 1182 31 29 18 18 26 16 126 |MD 72 69 60 53 52 --- 61 ---
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