[IGSREPORT-20114] Wk 1650 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Sep 8 06:59:57 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1650 (Aug 21, 2011 - Aug 27, 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 2.1650.
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:
igl1650[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1650 in the SP3 format.
igl16507.sum Combination Report for GPS Week 1650.
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 | 171.5 ns
1 | 171.9 ns
2 | 176.3 ns
3 | 174.6 ns
4 | 177.3 ns
5 | 176.1 ns
6 | 175.8 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
----+--------+---------------
6 | GRG | R04
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 1.1650, 1a.1650).
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 2.1650.0-6)
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 3.1650.0-6).
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 1650 summary. (Aug 21, 2011 - Aug 27, 2011)
Table 1.1650.a GPS week : 1650 MJD: 55794.0-55800.0
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| -2 1 -8 26 -14 -51 -.07 25 24 | --- --- --- ---
| 2 1 5 14 23 26 .03 | --- ---
esx 131| 0 -2 7 9 47 -9 .43 21 19 | 173196 1728 4911 5059
| 1 1 1 23 25 35 .06 | 2295 1659
gfz 193| 1 0 0 -22 5 58 -.18 24 19 | 0 979 4983 8821
| 1 1 2 37 32 39 .05 | 0 2226
grg 130| -1 2 -10 -9 -23 -14 .05 50 49 | --- --- --- ---
| 4 2 6 47 36 33 .09 | --- ---
iac n/a| 1 2 3 3 -30 -2 -.23 23 23 | 175839 -570 4954 8769
| 1 1 7 13 20 71 .06 | 2460 1821
mcc n/a| 6 3 16 56 39 -384 .16 103 103 | --- --- --- ---
| 8 5 12 65 78 221 .39 | --- ---
Table 1.1650.b GPS week : 1650 MJD: 55794.0-55800.0
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 17 12 12 10 11 15 |
R02 | 14 12 11 9 13 10 13 |
R03 | 12 13 9 9 11 11 10 |
R04 | 16 13 12 17 20 14 13 |
R05 | 12 15 15 13 10 11 13 |
R06 | 13 17 13 14 12 10 13 |
R07 | 18 11 17 14 18 15 14 |
R08 | 12 14 13 15 13 10 12 |
R09 | 11 14 12 17 12 10 12 |
R10 | 9 8 10 12 12 12 10 |
R11 | 17 19 21 18 17 16 17 |
R12 | 10 14 11 11 12 12 13 |
R13 | 16 11 15 11 11 13 13 |
R15 | 15 10 10 10 12 12 13 |
R16 | 12 16 13 18 10 11 12 |
R17 | 20 25 16 14 15 12 13 |
R18 | 12 12 11 14 11 9 9 |
R19 | 10 13 13 14 12 9 9 |
R20 | 18 17 20 18 13 19 15 |
R21 | 10 11 10 11 12 14 13 |
R22 | 10 14 12 9 12 11 13 |
R23 | 13 11 11 13 11 13 12 |
R24 | 11 11 11 11 10 11 14 |
Table 1.1650.c GPS week : 1650 MJD: 55794.0-55800.0
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 1650 0 | -81 -26 163 1317 1407 -10540 88.3 1815 1815 | 171544 0
brd 1650 1 | -45 4 113 -123 301 -10200 85.6 2029 2029 | 171910 0
brd 1650 2 | 133 106 278 1016 815 -24630 84.8 2304 2304 | 176256 0
brd 1650 3 | 2 107 167 1091 633 -28250 85.3 2848 2848 | 174634 0
brd 1650 4 | 16 81 193 -1629 -1694 -16370 84.3 2806 2806 | 177253 0
brd 1650 5 | -123 -70 122 -443 -1381 -13180 83.0 2628 2628 | 176080 0
brd 1650 6 | 28 -60 147 -2174 311 -19780 87.0 2344 2344 | 175846 0
-------------+------------------------------------------------------------+----------------
brd 1650 mean| -9 20 169 -134 56 -17564 85.5 2396 2396 | 174789 0
brd 1650 sdev| 83 77 55 1379 1153 6990 1.7 389 389 | 2230 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 2.1650.0 GPS week: 1650 Day: 0 MJD: 55794
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 -13 17 -39 -67 -.11 26 26 | --- --- --- ---
esx 131| -1 -1 5 -8 45 -51 .42 21 18 | 169293 3029 4766 4887
gfz 193| 2 2 0 4 12 36 -.23 21 15 | 0 2788 4878 10575
grg 130| 0 0 -9 -23 9 -44 .21 49 51 | --- --- --- ---
iac n/a| 2 0 8 3 7 84 -.20 25 25 | 173057 1432 4764 9694
mcc n/a| 0 5 0 68 66 -16 -.06 85 85 | --- --- --- ---
Table 2.1650.1 GPS week: 1650 Day: 1 MJD: 55795
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 -17 42 10 -94 -.02 27 26 | --- --- --- ---
esx 131| -2 -2 6 1 70 3 .30 25 23 | 171019 895 4372 4495
gfz 193| 0 0 -3 5 -36 10 -.13 24 20 | 0 -382 4482 8402
grg 130| 4 7 -16 -96 0 -48 .08 51 50 | --- --- --- ---
iac n/a| 0 2 18 -16 -39 78 -.13 27 27 | 172207 -1702 4371 8611
mcc n/a| 10 2 22 -69 -24 -315 .55 102 102 | --- --- --- ---
Table 2.1650.2 GPS week: 1650 Day: 2 MJD: 55796
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 2 -6 32 17 -15 -.12 27 27 | --- --- --- ---
esx 131| 0 0 8 41 48 5 .42 20 17 | 173178 4683 5268 5375
gfz 193| 2 -2 -5 -62 -22 36 -.18 25 19 | 0 4613 5297 11017
grg 130| 0 3 -17 -11 -56 -32 .10 46 48 | --- --- --- ---
iac n/a| 1 2 5 2 -16 -10 -.25 22 22 | 178105 -599 5274 10831
mcc n/a| 19 8 34 45 198 -264 .57 102 102 | --- --- --- ---
Table 2.1650.3 GPS week: 1650 Day: 3 MJD: 55797
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| -3 0 -8 13 -43 -31 -.08 23 24 | --- --- --- ---
esx 131| 1 -1 9 -9 34 41 .46 22 20 | 174179 273 4972 5137
gfz 193| 1 2 1 31 59 127 -.12 25 19 | 0 674 5003 9549
grg 130| -9 3 -15 -10 7 42 -.02 56 58 | --- --- --- ---
iac n/a| 2 0 0 -9 -54 -118 -.22 21 21 | 175187 1924 4963 9273
mcc n/a| 0 9 23 100 8 -437 .36 93 93 | --- --- --- ---
Table 2.1650.4 GPS week: 1650 Day: 4 MJD: 55798
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 -7 13 -20 -58 -.06 25 21 | --- --- --- ---
esx 131| 0 -3 7 14 10 9 .49 19 18 | 175764 1899 5858 6029
gfz 193| 3 0 0 -26 26 93 -.26 26 20 | 0 1462 6075 8197
grg 130| 0 -1 -3 43 -30 -15 .02 45 45 | --- --- --- ---
iac n/a| 1 2 -4 10 -27 -51 -.25 22 22 | 176385 29 6143 8778
mcc n/a| -3 -5 19 95 -30 -530 .16 84 84 | --- --- --- ---
Table 2.1650.5 GPS week: 1650 Day: 5 MJD: 55799
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| -3 0 -7 20 -7 -36 -.07 22 22 | --- --- --- ---
esx 131| 0 -2 5 -12 86 -56 .44 19 18 | 175121 1356 4702 4857
gfz 193| 0 -1 1 -42 -8 63 -.18 23 20 | 0 -138 4699 7171
grg 130| 0 0 0 -15 -87 -20 -.02 50 48 | --- --- --- ---
iac n/a| 0 2 -1 21 -42 14 -.24 20 20 | 178454 -2914 4708 7016
mcc n/a| 2 -3 8 27 15 -400 .07 109 109 | --- --- --- ---
Table 2.1650.6 GPS week: 1650 Day: 6 MJD: 55800
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 2 -1 47 -19 -53 -.06 25 23 | --- --- --- ---
esx 131| 0 -2 6 41 36 -21 .46 19 18 | 173820 -36 4443 4634
gfz 193| 0 0 0 -68 8 44 -.18 22 21 | 0 -2159 4453 6839
grg 130| -2 3 -13 45 -10 17 -.05 53 44 | --- --- --- ---
iac n/a| 0 3 0 13 -40 -17 -.33 24 24 | 177478 -2166 4455 7180
mcc n/a| 14 4 6 129 45 -725 -.54 145 145 | --- --- --- ---
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 3.1650.0 GPS week: 1650 Day: 0 MJD: 55794
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 625 25 14 19 47 34 --- 13 | 47 71 60 47 87 --- 63
R02 | 1033 17 11 11 83 19 --- 13 | 55 56 50 46 66 --- 51
R03 | 1671 17 16 17 36 34 --- 11 | 18 39 31 39 29 --- 26
XR04E | 1675 28 27 --- 41 13 --- 15 | 42 63 --- 56 41 --- 42
R05 | 788 21 12 8 67 20 102 12 | 69 65 55 36 66 26 58
R06 | 2556 26 17 16 66 15 --- 13 | 52 56 49 32 58 --- 47
XR07 | 3128 34 20 30 --- 36 --- 17 | 56 50 58 --- 56 --- 47
R08 | 938 24 19 17 48 15 --- 11 | 81 89 84 51 87 --- 80
R09 | 1297 29 12 17 42 16 --- 11 | 23 30 30 44 20 --- 19
R10 | 1382 13 11 11 36 22 --- 8 | 13 22 18 30 23 --- 14
R11 | 897 40 41 23 40 28 79 17 | 28 73 60 46 59 23 49
R12 | 1304 21 16 19 37 11 --- 9 | 25 32 29 29 26 --- 23
R13 | 970 35 31 25 63 21 --- 16 | 32 50 48 33 29 --- 32
R15 | 5454 30 16 16 68 27 72 14 | 19 35 34 73 19 26 28
R16 | 1455 32 23 17 31 15 --- 11 | 22 34 36 45 28 --- 25
R17E | 1727 37 37 40 38 47 --- 20 | 44 70 74 49 48 --- 50
R18E | 1902 24 25 16 37 26 --- 12 | 67 71 69 68 57 --- 65
R19E | 1168 15 23 13 29 24 --- 10 | 36 49 41 49 43 --- 39
R20E | 1402 37 18 42 45 32 --- 17 | 81 82 67 59 84 --- 71
R21E | 843 20 15 16 30 24 --- 10 | 27 38 33 35 35 --- 29
R22E | 994 18 11 24 31 18 --- 10 | 32 35 45 43 38 --- 35
R23E | 1130 15 27 16 45 34 --- 13 | 83 72 79 98 103 --- 82
R24E | 2254 17 18 15 54 16 --- 11 | 15 22 23 46 22 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 1815 26 21 21 49 25 85 |T 42 52 48 47 48 25 43
WRMS | 1815 26 18 15 51 25 85 |NE 38 50 45 42 46 25 40
MEDI | 1304 24 18 17 41 22 79 |MD 36 50 48 46 43 26 42
Table 3.1650.1 GPS week: 1650 Day: 1 MJD: 55795
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1502 33 37 24 55 26 --- 16 | 35 89 74 43 52 --- 59
XR02 | 738 12 27 19 --- 19 --- 11 | 34 50 30 --- 37 --- 35
R03 | 1803 18 24 28 28 30 --- 12 | 15 31 39 31 22 --- 19
XR04E | 2030 21 23 --- 38 16 --- 13 | 29 39 --- 51 27 --- 26
R05 | 1337 23 22 16 62 31 102 14 | 39 39 28 28 56 22 34
R06 | 2132 15 39 15 72 29 --- 16 | 30 72 51 43 54 --- 45
R07 | 3599 19 14 22 44 20 --- 11 | 38 48 43 28 38 --- 37
R08 | 1439 20 22 20 47 39 --- 14 | 90 75 74 73 92 --- 78
R09 | 1855 38 22 20 42 21 --- 14 | 18 34 35 30 19 --- 19
R10 | 1080 13 11 12 30 18 --- 8 | 19 26 18 24 30 --- 19
R11 | 1681 49 36 25 43 33 119 18 | 33 81 70 46 61 25 55
R12 | 1320 33 32 19 37 16 --- 13 | 16 50 33 38 21 --- 24
R13 | 744 26 18 18 40 17 --- 11 | 16 24 30 31 19 --- 16
R15 | 3959 18 16 14 33 21 65 9 | 13 24 24 30 20 32 14
R16 | 1928 33 29 18 66 16 --- 15 | 21 30 29 60 22 --- 16
R17E | 3176 38 31 59 84 42 --- 24 | 35 60 90 63 35 --- 39
R18E | 1795 21 17 20 43 21 113 11 | 42 44 40 48 40 54 36
R19E | 1162 14 18 18 60 29 --- 13 | 34 43 46 65 41 --- 39
R20E | 1616 31 21 30 61 34 --- 16 | 89 78 81 101 60 --- 75
XR21E | 724 20 17 15 --- 19 --- 10 | 24 34 24 --- 24 --- 22
R22E | 2240 20 20 18 56 32 --- 13 | 40 49 49 54 42 --- 39
R23E | 1075 16 16 18 47 20 --- 11 | 47 67 52 65 57 --- 54
R24E | 1702 27 22 20 28 17 --- 11 | 30 27 30 39 26 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 2029 27 25 24 51 27 102 |T 34 48 45 47 38 33 35
WRMS | 2029 26 23 20 50 27 102 |NE 29 48 41 38 38 26 33
MEDI | 1681 21 22 19 44 21 102 |MD 33 44 39 43 37 25 35
Table 3.1650.2 GPS week: 1650 Day: 2 MJD: 55796
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1464 20 23 19 43 19 --- 11 | 43 49 28 56 28 --- 35
R02 | 816 26 10 14 56 12 --- 11 | 39 30 30 40 35 --- 27
R03 | 3375 20 11 18 29 15 --- 8 | 26 25 25 30 20 --- 19
R04E | 2420 30 25 19 36 16 --- 12 | 36 59 62 71 46 --- 48
R05 | 1197 22 24 16 69 21 90 14 | 56 55 48 44 56 23 47
R06 | 1783 15 17 19 71 13 --- 13 | 43 42 44 28 48 --- 38
R07 | 3123 18 24 32 81 20 --- 16 | 51 62 44 33 47 --- 40
R08 | 980 20 15 20 51 25 --- 12 | 88 84 91 50 59 --- 75
R09 | 1259 35 13 20 35 16 --- 11 | 18 29 29 42 17 --- 19
R10 | 1775 19 14 22 38 15 --- 10 | 19 27 34 34 18 --- 19
R11 | 717 64 36 43 36 23 162 21 | 25 85 81 40 61 31 59
R12 | 1455 29 10 22 31 21 --- 11 | 16 25 36 28 33 --- 22
R13 | 861 38 23 31 49 20 --- 15 | 14 42 45 42 24 --- 24
R15 | 5846 17 16 14 28 22 42 9 | 16 30 27 38 15 23 17
R16 | 2403 37 10 30 28 19 --- 12 | 20 29 54 34 28 --- 26
R17E | 4601 22 32 34 45 25 --- 15 | 38 54 48 47 37 --- 36
R18E | 896 25 15 22 37 18 76 11 | 40 46 45 70 38 30 40
R19E | 786 22 16 30 32 30 --- 12 | 32 47 57 58 42 --- 41
R20E | 2158 23 36 35 51 50 --- 19 | 70 82 63 90 55 --- 62
R21E | 873 18 15 18 35 19 --- 10 | 30 36 38 54 34 --- 32
R22E | 1713 28 12 21 38 27 --- 12 | 30 34 33 48 46 --- 32
R23E | 1134 14 16 19 42 21 --- 10 | 37 48 41 42 42 --- 39
R24E | 2518 20 18 22 45 16 --- 11 | 21 26 26 41 26 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 2303 27 20 25 46 22 102 |T 35 45 44 46 37 26 35
WRMS | 2303 27 17 19 48 22 102 |NE 33 43 44 38 34 25 33
MEDI | 1464 22 16 21 38 20 76 |MD 32 42 44 42 37 23 35
Table 3.1650.3 GPS week: 1650 Day: 3 MJD: 55797
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1104 21 23 14 47 22 --- 11 | 46 55 45 49 38 --- 41
R02 | 877 21 11 15 44 11 --- 9 | 44 43 39 24 39 --- 36
R03 | 5579 9 20 20 33 14 --- 9 | 29 50 31 30 28 --- 31
R04E | 4530 32 30 46 50 21 --- 17 | 46 53 65 61 31 --- 40
R05 | 1054 17 31 16 51 20 86 12 | 67 97 86 58 58 18 73
R06 | 1750 7 13 15 86 27 --- 13 | 50 56 55 43 67 --- 52
R07 | 5533 15 11 21 83 19 --- 13 | 57 54 56 27 67 --- 53
R08 | 1022 11 18 32 72 32 --- 15 | 99 115 121 84 95 --- 102
R09 | 1509 36 15 34 73 22 --- 16 | 26 31 53 60 25 --- 26
R10 | 941 14 11 18 61 27 --- 12 | 28 24 31 62 20 --- 22
R11 | 1469 42 37 29 75 14 143 18 | 21 73 63 74 47 27 47
R12 | 1121 15 17 13 57 16 --- 10 | 22 42 34 32 33 --- 28
R13 | 759 23 20 18 31 17 --- 10 | 26 41 46 43 32 --- 32
R15 | 4827 13 19 17 40 17 52 9 | 26 32 29 36 28 31 25
R16 | 2924 40 26 48 55 13 --- 17 | 25 38 77 61 39 --- 38
R17E | 4626 25 18 31 36 28 --- 13 | 49 64 74 60 50 --- 55
R18E | 1562 23 24 23 69 18 64 14 | 42 42 48 62 38 27 37
R19E | 2355 27 29 27 44 16 --- 13 | 41 48 56 72 35 --- 40
R20E | 4061 24 34 26 48 44 --- 17 | 64 85 81 58 52 --- 61
R21E | 1761 24 18 21 39 12 --- 10 | 32 35 44 56 33 --- 31
R22E | 1971 17 15 16 36 15 --- 9 | 56 52 59 61 50 --- 51
R23E | 890 19 23 20 64 16 --- 12 | 38 38 37 62 43 --- 34
R24E | 2100 16 20 22 48 19 --- 11 | 23 37 36 33 30 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2848 23 22 25 56 21 93 |T 41 52 55 52 42 25 42
WRMS | 2848 24 20 19 58 21 93 |NE 40 53 54 48 44 25 43
MEDI | 1750 21 20 21 50 18 64 |MD 41 48 53 58 38 27 38
Table 3.1650.4 GPS week: 1650 Day: 4 MJD: 55798
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 959 14 10 23 43 17 --- 10 | 38 44 52 35 32 --- 37
R02 | 1530 18 13 21 48 33 --- 12 | 40 44 48 26 58 --- 42
R03 | 5166 23 21 12 41 20 --- 11 | 21 47 34 35 25 --- 28
R04E | 3421 42 24 57 37 30 --- 19 | 41 63 78 42 43 --- 48
R05 | 929 21 17 12 45 12 76 10 | 61 50 53 71 44 24 51
R06 | 809 13 28 12 55 14 --- 12 | 47 77 56 52 49 --- 56
R07 | 4022 33 15 59 50 17 --- 17 | 60 63 93 35 53 --- 58
R08 | 1293 14 27 20 48 23 --- 12 | 53 63 49 68 57 --- 55
R09 | 1503 33 14 22 31 25 --- 12 | 33 28 36 36 25 --- 21
R10 | 1094 21 17 25 31 28 --- 12 | 31 41 54 64 33 --- 37
R11 | 1296 42 33 22 59 24 116 17 | 24 73 59 62 44 19 47
R12 | 1156 26 15 19 55 13 --- 12 | 18 33 27 59 23 --- 22
R13 | 948 26 19 18 37 19 --- 11 | 18 37 36 29 24 --- 23
R15 | 4096 17 16 29 42 24 51 12 | 24 38 37 35 20 23 24
R16 | 1994 15 12 15 47 15 --- 9 | 24 29 31 49 25 --- 24
R17E | 8199 23 21 25 55 37 --- 15 | 49 69 72 70 58 --- 58
R18E | 1222 21 16 23 37 19 81 11 | 44 56 43 48 58 38 48
R19E | 1267 29 19 18 43 20 --- 12 | 27 52 45 73 35 --- 38
R20E | 2634 25 17 28 47 21 --- 12 | 32 49 59 47 51 --- 43
R21E | 2048 32 16 19 39 19 --- 11 | 30 35 34 44 27 --- 26
R22E | 2498 16 22 16 43 23 --- 11 | 40 38 50 77 44 --- 41
R23E | 1717 20 22 17 42 16 --- 11 | 31 43 42 33 36 --- 34
R24E | 1120 21 10 16 44 20 --- 10 | 15 27 37 30 23 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2805 25 19 26 45 22 84 |T 34 47 48 48 38 26 38
WRMS | 2805 21 18 20 45 22 84 |NE 35 47 47 46 36 22 37
MEDI | 1503 21 17 20 43 20 76 |MD 32 44 48 47 36 23 38
Table 3.1650.5 GPS week: 1650 Day: 5 MJD: 55799
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 818 27 16 17 25 19 --- 10 | 30 54 53 56 51 --- 44
R02 | 1590 9 9 13 58 20 --- 10 | 33 40 41 29 45 --- 36
R03 | 2401 15 16 21 54 15 --- 11 | 19 36 35 30 28 --- 25
R04E | 3635 20 15 29 68 18 --- 13 | 34 47 45 80 37 --- 36
R05 | 1136 30 12 15 47 12 116 11 | 47 44 37 46 26 22 36
R06 | 1386 15 20 13 36 17 --- 9 | 40 42 40 64 33 --- 37
R07 | 3818 18 22 38 59 26 --- 15 | 40 30 60 39 38 --- 33
R08 | 1332 13 20 12 50 16 --- 10 | 55 62 67 56 67 --- 60
R09 | 1475 20 16 18 36 14 --- 9 | 16 24 34 44 24 --- 20
R10 | 760 16 13 28 54 22 --- 12 | 27 34 43 59 36 --- 30
R11 | 1464 41 26 26 39 32 106 16 | 30 43 38 38 43 19 33
R12 | 1056 28 10 19 48 21 --- 11 | 29 33 37 36 32 --- 27
R13 | 1683 21 20 29 58 16 --- 13 | 18 34 37 52 25 --- 24
R15 | 1996 23 20 26 40 17 58 11 | 28 29 28 39 18 25 21
R16 | 1312 23 25 19 27 19 --- 11 | 30 54 47 50 33 --- 39
R17E | 9119 23 15 21 38 24 --- 11 | 46 54 52 44 53 --- 48
R18E | 2535 16 15 16 37 13 138 9 | 48 69 51 56 57 32 55
R19E | 2340 13 11 17 39 14 --- 8 | 44 53 49 48 47 --- 46
R20E | 1266 28 36 33 79 34 --- 19 | 76 103 95 71 84 --- 84
R21E | 1392 28 21 34 54 18 --- 14 | 27 38 35 58 34 --- 28
R22E | 1163 17 25 15 39 19 --- 11 | 47 65 53 57 49 --- 50
R23E | 1088 11 22 16 74 19 --- 13 | 27 40 44 69 35 --- 34
R24E | 1194 13 13 23 38 23 --- 10 | 19 34 38 20 22 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 2628 22 19 23 50 20 109 |T 35 46 46 49 39 24 37
WRMS | 2628 22 18 20 48 20 109 |NE 31 39 42 45 35 22 33
MEDI | 1392 20 16 19 47 19 106 |MD 30 42 43 50 36 22 36
Table 3.1650.6 GPS week: 1650 Day: 6 MJD: 55800
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esx gfz grg iac mcc IGL | cod esx gfz grg iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 967 17 20 22 66 33 --- 15 | 46 67 61 71 69 --- 57
R02 | 1565 13 17 18 68 12 --- 12 | 50 48 50 27 45 --- 42
R03 | 2179 19 13 18 40 14 --- 9 | 22 34 34 32 32 --- 27
R04E | 4123 28 12 22 145 23 --- 12 | 36 40 33 92 45 --- 35
R05 | 2383 33 19 14 52 14 196 12 | 68 55 54 31 52 22 52
R06 | 1735 15 18 17 60 21 --- 12 | 54 64 61 30 47 --- 51
R07 | 3166 12 31 29 31 24 --- 13 | 61 69 64 35 69 --- 60
R08 | 959 13 7 16 66 14 --- 11 | 62 60 61 48 64 --- 57
R09 | 887 25 19 25 24 22 --- 11 | 20 38 31 42 23 --- 23
R10 | 800 18 15 19 41 14 --- 10 | 29 29 46 43 37 --- 32
R11 | 1601 48 20 36 46 26 147 17 | 30 75 79 55 66 24 59
R12 | 1023 27 10 15 57 21 --- 12 | 20 28 27 41 24 --- 19
R13 | 1149 32 19 18 42 22 --- 12 | 22 40 32 41 38 --- 28
R15 | 2502 24 9 23 39 37 69 13 | 27 24 30 40 20 21 20
R16 | 1250 31 22 20 24 21 --- 12 | 22 45 43 46 31 --- 32
R17E | 6740 28 23 15 38 30 --- 13 | 56 76 73 81 69 --- 66
R18E | 2565 16 13 14 40 15 139 9 | 53 57 53 70 53 49 54
R19E | 1335 14 11 23 23 18 --- 9 | 47 59 64 53 49 --- 53
R20E | 1164 25 22 33 35 33 --- 14 | 64 71 76 68 78 --- 67
R21E | 2617 27 20 25 37 23 --- 12 | 27 39 45 47 32 --- 30
R22E | 1140 30 28 17 34 20 --- 12 | 44 46 51 70 47 --- 46
R23E | 1128 19 22 23 38 26 --- 12 | 36 43 41 61 33 --- 35
R24E | 1663 17 19 31 35 36 --- 14 | 19 38 36 33 25 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2343 25 19 22 53 24 145 |T 39 49 49 50 45 29 42
WRMS | 2343 23 18 21 44 24 145 |NE 38 48 48 41 44 22 39
MEDI | 1565 24 19 20 40 22 139 |MD 36 46 50 46 45 22 42
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