[IGSREPORT-20074] Wk 1648 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 25 10:40:14 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1648 (Aug 07, 2011 - Aug 13, 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 2.1648.
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:
igl1648[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1648 in the SP3 format.
igl16487.sum Combination Report for GPS Week 1648.
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 | 161.7 ns
1 | 162.0 ns
2 | 162.3 ns
3 | 163.4 ns
4 | 159.0 ns
5 | 158.3 ns
6 | 159.9 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 1.1648, 1a.1648).
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 2.1648.0-6)
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 3.1648.0-6).
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 1648 summary. (Aug 07, 2011 - Aug 13, 2011)
Table 1.1648.a GPS week : 1648 MJD: 55780.0-55786.0
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 250| -1 0 0 37 -11 13 -.16 25 26 | --- --- --- ---
| 1 1 3 22 24 32 .04 | --- ---
esx 130| 0 -1 11 -14 -2 -31 .40 21 20 | 161542 -2651 4930 5440
| 1 1 2 36 23 30 .05 | 2960 3649
gfz 192| -1 0 3 -38 -24 47 -.21 22 19 | 0 -1463 4964 9942
| 2 1 4 33 36 27 .04 | 0 3019
grg 129| 1 2 -7 1 31 99 .18 53 51 | --- --- --- ---
| 5 3 4 50 36 47 .14 | --- ---
iac n/a| 1 0 -14 17 30 -66 -.17 24 24 | 162432 -633 4878 9864
| 2 1 6 44 18 57 .01 | 2550 1571
mcc n/a| 0 3 -2 109 58 -113 -.14 131 131 | --- --- --- ---
| 13 10 20 156 210 410 .40 | --- ---
Table 1.1648.b GPS week : 1648 MJD: 55780.0-55786.0
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 10 12 11 15 |
R02 | 14 12 10 12 13 13 13 |
R03 | 11 10 13 15 11 10 14 |
R04 | 21 46 29 37 37 56 0 |
R05 | 14 13 16 13 14 11 13 |
R06 | 11 12 12 9 10 13 13 |
R07 | 14 10 14 13 10 13 13 |
R08 | 12 14 15 12 11 12 13 |
R09 | 14 14 12 12 10 11 13 |
R10 | 9 12 12 12 10 10 9 |
R11 | 19 16 15 17 16 16 20 |
R12 | 16 9 9 10 13 12 13 |
R13 | 14 9 15 14 13 13 14 |
R15 | 10 13 12 24 15 12 12 |
R16 | 11 11 12 13 15 16 15 |
R17 | 16 17 19 16 15 19 20 |
R18 | 12 12 13 20 11 14 11 |
R19 | 9 16 11 12 11 11 11 |
R20 | 14 19 19 20 13 13 15 |
R21 | 13 11 12 14 14 11 9 |
R22 | 18 11 11 11 14 13 10 |
R23 | 19 14 9 11 10 13 11 |
R24 | 13 20 15 14 12 14 16 |
Table 1.1648.c GPS week : 1648 MJD: 55780.0-55786.0
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 1648 0 | 76 30 390 -254 -1202 -8784 88.5 1608 1608 | 161728 0
brd 1648 1 | 16 68 386 -680 1633 -6122 87.3 1648 1648 | 162001 0
brd 1648 2 | -14 53 289 433 10 -1908 86.3 1752 1752 | 162314 0
brd 1648 3 | -52 55 297 126 -2090 -544 83.8 1548 1548 | 163370 0
brd 1648 4 | -22 -34 282 375 -2472 -7074 87.0 2138 2138 | 158971 0
brd 1648 5 | -37 -42 154 853 22 -6213 87.3 1970 1970 | 158332 0
brd 1648 6 | 21 52 222 443 329 -4616 85.7 >>>>> >>>>> | 159939 0
-------------+------------------------------------------------------------+----------------
brd 1648 mean| -1 26 289 185 -538 -5037 86.6 43723 43723 | 160950 0
brd 1648 sdev| 43 45 84 509 1453 2912 1.5 >>>>> >>>>> | 1880 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 2.1648.0 GPS week: 1648 Day: 0 MJD: 55780
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 250| 0 -2 4 71 -17 20 -.12 29 28 | --- --- --- ---
esx 130| 0 0 11 -39 -21 -38 .44 21 20 | 163541 -4634 4596 4768
gfz 192| -1 1 0 -69 0 87 -.19 23 20 | 0 -1801 4655 8745
grg 129| -3 5 -8 96 -14 96 -.02 56 54 | --- --- --- ---
iac n/a| 1 -2 -12 17 34 -97 -.17 22 22 | 162757 -1071 4594 8869
mcc n/a| -2 1 -31 64 -187 198 -.14 156 156 | --- --- --- ---
Table 2.1648.1 GPS week: 1648 Day: 1 MJD: 55781
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 250| 0 0 0 57 -48 48 -.14 29 28 | --- --- --- ---
esx 130| -1 0 6 -52 -25 0 .38 24 22 | 161801 -2544 5265 5428
gfz 192| -2 0 2 -29 36 29 -.16 20 18 | 0 -1830 5484 9134
grg 129| -2 7 -13 15 -14 177 .15 50 48 | --- --- --- ---
iac n/a| 3 0 -4 61 6 -85 -.15 23 23 | 163353 677 5313 9220
mcc n/a| -3 5 -1 195 -183 303 .48 118 118 | --- --- --- ---
Table 2.1648.2 GPS week: 1648 Day: 2 MJD: 55782
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 250| -1 -1 -1 9 -14 -38 -.15 24 24 | --- --- --- ---
esx 130| 0 0 9 -21 -15 -27 .50 20 18 | 161182 228 5310 5546
gfz 192| 0 1 -1 -49 -15 72 -.25 21 16 | 0 1400 5403 15016
grg 129| 2 -3 -5 0 31 99 .08 56 54 | --- --- --- ---
iac n/a| 5 0 -9 75 24 -31 -.16 28 28 | 165349 1571 5303 14515
mcc n/a| 5 1 2 -35 242 268 -.27 108 108 | --- --- --- ---
Table 2.1648.3 GPS week: 1648 Day: 3 MJD: 55783
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 250| -2 0 -5 20 19 -23 -.17 26 25 | --- --- --- ---
esx 130| 1 0 12 -27 2 -86 .33 21 18 | 166630 -6453 5482 5897
gfz 192| -6 0 4 -8 -76 65 -.16 24 23 | 0 -3087 5221 7372
grg 129| 11 0 -9 -73 30 32 .14 54 52 | --- --- --- ---
iac n/a| 4 2 -12 43 28 11 -.18 24 24 | 165329 -2521 5094 7672
mcc n/a| 24 -11 -23 27 113 -614 -.68 117 117 | --- --- --- ---
Table 2.1648.4 GPS week: 1648 Day: 4 MJD: 55784
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 250| -2 0 1 31 20 16 -.25 24 26 | --- --- --- ---
esx 130| 0 -1 12 21 -18 -42 .42 18 18 | 161255 -5466 4449 4565
gfz 192| 0 -1 -2 -36 -29 15 -.24 19 18 | 0 -4449 4535 8520
grg 129| 5 1 1 2 54 136 .19 54 51 | --- --- --- ---
iac n/a| 1 -2 -17 -25 60 -44 -.19 23 23 | 161355 -1878 4442 7994
mcc n/a| -10 10 -7 421 239 -313 .22 122 122 | --- --- --- ---
Table 2.1648.5 GPS week: 1648 Day: 5 MJD: 55785
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 250| 0 2 4 21 -9 43 -.15 23 24 | --- --- --- ---
esx 130| 1 -3 13 -27 22 6 .39 22 19 | 158186 -3692 5289 5502
gfz 192| -2 1 8 9 -48 23 -.22 21 17 | 0 -4221 5290 10139
grg 129| -2 2 -9 -6 52 95 .43 51 51 | --- --- --- ---
iac n/a| 0 0 -22 -24 42 -168 -.16 23 23 | 158411 -1815 5256 9837
mcc n/a| 0 -2 12 92 286 11 -.03 128 128 | --- --- --- ---
Table 2.1648.6 GPS week: 1648 Day: 6 MJD: 55786
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 250| 0 0 0 49 -28 27 -.14 23 24 | --- --- --- ---
esx 130| -1 0 11 48 35 -33 .37 24 21 | 158202 3999 4120 6377
gfz 192| 1 0 9 -86 -35 39 -.23 24 24 | 0 3744 4160 10668
grg 129| 0 3 -8 -21 84 58 .26 49 49 | --- --- --- ---
iac n/a| -2 1 -22 -28 12 -49 -.18 26 26 | 160474 605 4148 10945
mcc n/a| -17 21 29 1 -101 -649 -.52 166 166 | --- --- --- ---
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 3.1648.0 GPS week: 1648 Day: 0 MJD: 55780
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1739 27 25 17 57 19 --- 13 | 54 87 67 42 68 --- 66
R02 | 702 23 11 24 68 21 --- 13 | 57 44 52 36 56 --- 47
R03 | 1695 16 15 22 37 24 --- 10 | 26 29 35 23 27 --- 24
XR04E | 3881 33 25 --- 85 23 --- 21 | 32 68 --- 4 47 --- 47
R05 | 1403 44 17 19 55 17 --- 14 | 75 48 48 43 52 --- 49
R06 | 1041 25 7 21 50 11 --- 10 | 57 49 48 46 53 --- 47
R07 | 1183 23 26 15 60 23 --- 13 | 58 56 58 29 59 --- 54
R08 | 3618 17 24 16 63 13 160 12 | 55 69 48 31 51 27 51
R09 | 1448 40 15 29 37 23 --- 14 | 27 35 36 41 30 --- 25
R10 | 965 14 15 20 28 16 --- 9 | 16 28 31 45 21 --- 21
R11 | 1035 57 38 34 40 23 131 19 | 36 69 56 42 45 41 42
R12 | 1478 39 21 26 65 24 --- 16 | 27 46 43 48 28 --- 30
R13 | 1750 29 27 23 37 26 --- 13 | 26 48 39 29 32 --- 30
R15 | 1763 19 10 19 47 18 173 10 | 23 22 36 40 23 32 21
R16 | 1065 22 14 16 34 25 --- 10 | 28 32 30 29 33 --- 23
R17E | 2566 32 34 19 38 38 --- 16 | 25 46 39 54 35 --- 31
R18E | 1019 23 26 20 40 22 --- 12 | 31 50 47 38 35 --- 36
R19E | 1944 15 15 19 30 15 --- 9 | 67 78 72 70 65 --- 69
R20E | 1597 27 25 25 39 27 --- 13 | 58 57 64 61 50 --- 53
R21E | 1007 20 14 31 43 24 --- 12 | 25 36 39 35 27 --- 27
R22E | 1197 26 22 26 100 19 --- 17 | 26 44 43 62 27 --- 28
R23E | 1076 29 14 19 118 17 --- 18 | 17 32 31 104 19 --- 23
R24E | 1340 23 23 25 44 25 --- 13 | 26 55 57 45 26 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1608 29 21 23 56 22 156 |T 37 49 46 43 39 33 38
WRMS | 1608 28 20 20 54 22 156 |NE 40 47 44 37 41 33 37
MEDI | 1403 25 21 20 44 23 160 |MD 28 48 43 42 35 32 36
Table 3.1648.1 GPS week: 1648 Day: 1 MJD: 55781
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1119 24 34 13 71 12 --- 14 | 32 61 42 35 28 --- 37
R02 | 857 21 16 19 39 27 --- 11 | 34 20 20 32 45 --- 24
R03 | 2817 22 21 17 28 19 --- 10 | 16 38 31 40 20 --- 21
XR04E | 3470 65 90 --- --- 34 --- 46 | 33 106 --- --- 36 --- 54
R05 | 1389 34 27 16 49 17 --- 13 | 54 32 46 51 29 --- 34
R06 | 1036 29 13 16 54 12 --- 11 | 42 27 27 26 28 --- 23
R07 | 1641 15 14 17 46 14 --- 10 | 34 43 48 31 31 --- 35
R08 | 1901 17 17 25 49 31 133 13 | 33 30 44 30 15 24 23
R09 | 1145 37 21 24 31 28 --- 14 | 25 26 38 26 20 --- 19
R10 | 944 20 19 23 39 25 --- 12 | 19 22 36 35 23 --- 19
R11 | 889 53 38 14 42 17 134 16 | 19 56 40 42 36 33 32
R12 | 1374 24 19 14 21 16 --- 9 | 17 26 16 34 25 --- 16
R13 | 1982 25 20 13 27 12 --- 9 | 15 26 20 28 20 --- 12
R15 | 1002 26 12 16 67 15 78 13 | 14 19 21 64 23 16 14
R16 | 1067 32 21 16 27 15 --- 11 | 20 31 25 22 18 --- 17
R17E | 4144 42 32 18 60 30 --- 17 | 26 41 29 50 30 --- 24
R18E | 1033 27 18 21 42 22 --- 12 | 29 48 57 46 33 --- 39
R19E | 1104 29 22 26 59 32 --- 16 | 59 83 83 96 56 --- 71
R20E | 1615 31 35 34 52 39 --- 18 | 47 82 75 50 42 --- 57
R21E | 1222 15 22 20 28 21 --- 10 | 17 40 35 35 18 --- 23
R22E | 1793 19 16 22 29 21 --- 10 | 22 42 47 42 26 --- 30
R23E | 1181 30 22 21 55 22 --- 14 | 13 35 29 45 22 --- 19
R24E | 1173 23 33 16 107 22 --- 19 | 15 44 39 98 20 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1648 29 24 20 50 23 118 |T 27 42 38 43 28 24 29
WRMS | 1648 28 22 18 48 23 118 |NE 26 32 32 35 25 24 23
MEDI | 1181 26 21 17 42 21 133 |MD 25 38 36 35 26 24 24
Table 3.1648.2 GPS week: 1648 Day: 2 MJD: 55782
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 865 26 26 26 70 30 --- 16 | 43 75 77 52 39 --- 57
R02 | 1063 23 15 10 43 22 --- 10 | 46 51 39 42 34 --- 40
R03 | 2975 17 17 26 53 28 --- 13 | 23 27 26 36 18 --- 16
XR04E | 5487 32 48 --- --- 37 --- 28 | 25 75 --- --- 49 --- 55
R05 | 603 29 28 29 74 19 --- 16 | 55 63 45 57 53 --- 48
R06 | 1290 22 14 15 59 26 --- 12 | 58 45 48 54 58 --- 48
R07 | 2058 17 22 14 83 23 --- 14 | 47 58 45 51 45 --- 45
R08 | 1707 21 29 9 70 33 121 14 | 44 53 29 46 30 23 33
R09 | 1037 35 16 14 41 17 --- 11 | 27 36 34 35 26 --- 26
R10 | 1065 12 17 16 55 29 --- 11 | 14 34 34 61 15 --- 24
R11 | 976 34 20 22 45 35 133 14 | 17 42 41 34 39 21 28
R12 | 1478 15 14 11 40 16 --- 8 | 21 23 32 38 29 --- 23
R13 | 1590 25 18 29 50 37 --- 15 | 20 31 28 26 37 --- 19
R15 | 1744 22 16 20 48 22 56 11 | 18 32 34 38 17 18 20
R16 | 1124 28 11 24 46 18 --- 12 | 16 31 28 58 25 --- 21
R17E | 3976 44 23 32 76 31 --- 18 | 24 45 41 88 40 --- 31
R18E | 729 18 16 24 55 29 --- 12 | 27 41 37 48 35 --- 29
R19E | 1350 19 17 17 48 24 --- 11 | 37 53 57 77 40 --- 45
R20E | 893 22 36 25 37 57 --- 18 | 57 89 71 69 39 --- 61
R21E | 1192 20 19 22 50 18 --- 11 | 18 32 50 43 22 --- 28
R22E | 2314 22 16 16 41 26 --- 11 | 26 47 42 52 28 --- 33
R23E | 670 13 15 19 38 16 --- 9 | 22 29 20 44 26 --- 21
R24E | 3039 22 17 25 77 24 --- 14 | 33 37 54 89 31 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1752 24 20 21 56 28 108 |T 31 45 41 51 33 20 34
WRMS | 1752 24 18 16 54 28 108 |NE 32 42 38 44 33 20 32
MEDI | 1290 22 17 20 50 26 121 |MD 26 42 39 48 34 21 31
Table 3.1648.3 GPS week: 1648 Day: 3 MJD: 55783
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1133 9 7 23 46 21 --- 10 | 41 51 64 34 40 --- 45
R02 | 775 18 17 13 57 25 --- 12 | 52 57 57 61 37 --- 48
R03 | 1676 22 18 24 80 18 --- 14 | 17 31 29 64 27 --- 20
XR04E | 3122 31 62 --- --- 51 --- 36 | 29 76 --- --- 48 --- 44
R05 | 879 31 22 14 53 17 --- 12 | 59 57 38 61 38 --- 43
R06 | 1516 17 12 18 40 14 --- 9 | 49 47 59 34 44 --- 46
R07 | 1819 20 10 16 70 20 --- 12 | 56 50 45 55 61 --- 49
R08 | 1333 12 24 24 56 10 146 11 | 46 67 36 30 46 44 45
R09 | 837 31 14 16 54 19 --- 12 | 27 38 33 72 27 --- 28
R10 | 1141 23 11 30 36 25 --- 12 | 13 28 49 34 25 --- 21
R11 | 896 41 23 28 55 31 76 16 | 22 44 49 53 48 42 34
R12 | 1145 26 14 18 37 14 --- 10 | 28 19 26 30 19 --- 16
R13 | 1340 37 20 25 49 20 --- 14 | 26 46 35 28 34 --- 29
XR15 |>>>>> 37 --- 26 101 17 110 23 | 25 --- 31 65 33 23 17
R16 | 1307 31 22 20 49 20 --- 13 | 23 44 48 53 27 --- 29
R17E | 3709 32 18 20 78 30 --- 16 | 21 47 49 78 37 --- 35
R18E | 961 29 48 35 71 29 --- 20 | 36 61 47 58 48 --- 37
R19E | 1208 22 22 18 47 21 --- 12 | 38 52 44 53 38 --- 40
R20E | 1957 36 29 41 44 47 --- 19 | 71 74 82 68 52 --- 61
R21E | 939 30 25 24 44 24 --- 13 | 27 35 36 42 24 --- 23
R22E | 2299 16 14 21 50 21 --- 11 | 24 34 38 64 40 --- 30
R23E | 1138 15 19 23 33 23 --- 10 | 13 25 35 31 20 --- 19
XR24E | 6040 24 22 29 --- 21 --- 14 | 29 36 50 --- 23 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1547 26 21 24 54 24 117 |T 33 46 44 50 36 36 34
WRMS | 1547 25 18 23 52 24 117 |NE 34 44 42 48 36 36 33
MEDI | 1307 26 19 23 50 21 110 |MD 28 46 44 53 37 42 34
Table 3.1648.4 GPS week: 1648 Day: 4 MJD: 55784
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1178 19 27 12 43 27 --- 12 | 34 65 33 42 40 --- 41
R02 | 922 29 17 26 62 12 --- 13 | 39 23 24 55 22 --- 21
R03 | 1243 17 20 15 54 15 --- 10 | 19 26 28 39 25 --- 18
XR04E | 2737 56 56 --- --- 40 --- 36 | 40 60 --- --- 53 --- 50
R05 | 881 34 13 17 68 21 --- 13 | 37 31 29 47 28 --- 24
R06 | 1431 19 16 13 51 17 --- 10 | 39 54 42 50 33 --- 39
R07 | 3503 15 12 16 46 20 --- 9 | 56 51 41 52 55 --- 48
R08 | 1155 13 12 14 49 27 143 10 | 48 36 37 64 60 27 43
R09 | 901 26 14 11 30 18 --- 9 | 27 37 40 41 36 --- 32
R10 | 807 16 13 19 35 20 --- 9 | 13 28 23 37 27 --- 19
R11 | 1052 38 18 33 50 25 96 15 | 13 38 33 39 38 61 24
R12 | 1352 22 16 27 62 20 --- 13 | 29 36 43 59 23 --- 28
R13 | 1011 36 13 19 41 26 --- 12 | 27 31 33 39 36 --- 26
XR15 | 5284 16 25 18 --- 36 107 14 | 18 37 34 --- 36 46 23
R16 | 1583 36 28 16 58 22 --- 14 | 24 45 36 41 24 --- 26
R17E | 3159 27 22 27 39 36 --- 14 | 17 36 45 39 33 --- 26
R18E | 1371 21 16 18 48 18 --- 10 | 23 41 41 60 28 --- 30
R19E | 807 17 15 16 52 18 --- 10 | 32 44 48 45 38 --- 39
R20E | 1143 22 23 19 61 23 --- 13 | 45 43 56 87 49 --- 46
R21E | 819 22 20 11 79 21 --- 13 | 19 35 30 55 19 --- 22
R22E | 1511 17 22 17 70 33 --- 14 | 21 41 44 56 37 --- 31
R23E | 908 14 14 18 32 23 --- 9 | 17 31 37 35 22 --- 23
R24E | 7089 19 23 16 63 19 --- 12 | 21 45 35 37 25 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2138 24 18 19 54 23 122 |T 28 39 36 48 34 44 30
WRMS | 2138 26 18 18 51 23 122 |NE 30 38 34 46 34 44 29
MEDI | 1178 21 17 17 51 21 107 |MD 27 37 36 45 33 46 26
Table 3.1648.5 GPS week: 1648 Day: 5 MJD: 55785
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1448 17 22 15 34 24 --- 10 | 36 60 42 46 46 --- 44
R02 | 865 28 14 19 63 21 --- 13 | 38 23 30 34 24 --- 23
R03 | 1706 15 15 15 50 17 --- 10 | 20 20 21 34 21 --- 17
XR04E | 5761 52 --- --- --- 58 --- 55 | 56 --- --- --- 57 --- 57
R05 | 1266 20 21 9 53 18 --- 11 | 32 44 30 38 28 --- 30
R06 | 1451 20 14 18 64 21 --- 12 | 31 31 43 41 42 --- 33
R07 | 3821 12 23 24 60 21 --- 12 | 37 47 51 30 33 --- 36
R08 | 2115 10 12 15 66 20 157 11 | 36 44 42 52 45 37 39
R09 | 1485 31 10 14 31 20 --- 10 | 23 38 44 45 39 --- 34
R10 | 1133 14 16 19 41 17 --- 9 | 18 27 43 39 23 --- 24
R11 | 765 44 23 27 38 29 91 16 | 11 36 29 51 39 44 24
R12 | 984 24 13 10 52 29 --- 12 | 24 24 23 55 28 --- 21
R13 | 1188 28 25 24 44 15 --- 13 | 22 31 27 30 15 --- 17
XR15 | 3330 21 11 14 --- 32 98 12 | 15 18 16 --- 28 22 13
R16 | 1164 32 26 36 44 27 --- 16 | 33 36 48 32 27 --- 24
R17E | 3704 30 36 37 52 39 --- 18 | 22 45 56 39 26 --- 27
R18E | 1775 15 19 20 71 24 --- 13 | 24 44 41 70 32 --- 33
R19E | 942 18 15 22 48 19 --- 11 | 54 58 62 61 56 --- 56
R20E | 948 21 25 22 46 25 --- 13 | 27 49 49 44 43 --- 37
R21E | 1780 19 20 16 40 19 --- 10 | 17 30 29 54 18 --- 17
R22E | 706 24 17 21 58 19 --- 12 | 21 37 44 88 39 --- 34
R23E | 831 15 29 18 40 29 --- 12 | 11 39 35 39 24 --- 21
R24E | 4704 23 35 18 44 21 --- 13 | 28 52 34 40 25 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1970 23 22 21 51 23 128 |T 27 37 38 45 32 34 29
WRMS | 1970 24 19 17 51 23 128 |NE 26 34 34 40 31 34 27
MEDI | 1448 21 19 18 48 21 98 |MD 24 37 41 41 28 37 27
Table 3.1648.6 GPS week: 1648 Day: 6 MJD: 55786
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1304 21 17 13 74 35 --- 15 | 49 83 71 55 82 --- 66
R02 | 765 14 24 13 61 22 --- 12 | 57 44 47 43 54 --- 47
R03 | 1363 9 14 25 61 35 --- 13 | 26 31 39 34 28 --- 25
XR04E | ---- --- --- --- --- 11 --- 0 | --- --- --- --- 65 --- 94
R05 | 838 26 14 21 60 19 --- 13 | 65 60 68 41 46 --- 53
R06 | 914 13 29 23 45 25 --- 13 | 49 67 48 32 42 --- 45
R07 | 1228 27 20 29 34 26 --- 13 | 58 52 43 37 46 --- 46
R08 | 1869 11 20 13 66 22 244 12 | 45 60 49 39 39 29 44
R09 | 784 30 22 24 18 24 --- 12 | 35 52 44 41 41 --- 38
R10 | 891 13 11 24 27 19 --- 9 | 19 30 30 34 32 --- 25
R11 | 970 49 46 29 44 25 127 20 | 25 76 54 43 42 58 41
R12 | 1039 21 16 25 39 30 --- 12 | 30 42 54 33 34 --- 33
R13 | 1481 23 19 34 36 29 --- 13 | 31 39 63 33 29 --- 33
R15 | 4003 18 12 21 39 32 87 11 | 27 30 39 39 25 24 25
R16 | 1239 33 27 35 33 21 --- 15 | 42 46 34 38 31 --- 32
R17E | 4518 32 48 31 66 34 --- 20 | 26 54 41 58 29 --- 29
R18E | 1488 16 19 20 35 25 --- 11 | 30 38 40 47 34 --- 32
R19E | 1062 15 17 22 43 20 --- 11 | 49 57 59 60 45 --- 50
R20E | 1540 24 23 26 62 28 --- 15 | 36 51 53 78 47 --- 43
R21E | 1774 13 13 13 39 17 --- 9 | 23 32 32 46 32 --- 28
R22E | 905 20 18 13 26 26 --- 10 | 36 49 41 46 38 --- 39
R23E | 1422 10 20 21 46 22 --- 11 | 24 32 39 37 33 --- 27
R24E |>>>>> 20 35 23 64 30 --- 16 | 27 43 37 54 31 --- 30
------+-----------------------------------------+-------------------------------------
RMS |>>>>> 23 24 24 49 26 166 |T 36 48 46 44 40 37 40
WRMS |>>>>> 24 21 24 49 26 166 |NE 39 50 48 38 40 37 39
MEDI | 1239 20 19 23 43 25 127 |MD 31 46 43 41 38 29 38
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