[IGSREPORT-18771] Wk 1590 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Jul 15 05:23:18 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1590 (Jun 27, 2010 - Jul 03, 2010)
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 centers
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 2.1590.
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:
igl1590[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1590 in the SP3 format.
igl15907.sum Combination Report for GPS Week 1590.
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.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
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.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 420.0 ns
1 | 389.4 ns
2 | 423.7 ns
3 | 472.8 ns
4 | 414.7 ns
5 | 419.0 ns
6 | 390.4 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 1.1590, 1a.1590).
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 2.1590.0-6)
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 3.1590.0-6).
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 1590 summary. (Jun 27, 2010 - Jul 03, 2010)
Table 1.1590.a GPS week : 1590 MJD: 55374.0-55380.0
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]
--------+----------------------------------------------------+------------------------------
bkg 119| 1 -1 -7 -17 36 31 -.11 23 21 | 0 1 1740 1810
| 1 1 6 26 51 102 .03 | 0 38
cod 238| -2 -1 1 43 -23 -15 -.12 14 13 | --- --- --- ---
| 0 1 3 30 30 42 .03 | --- ---
esx 135| 0 1 1 -17 -2 73 .41 23 21 | 69707 191 3951 7830
| 1 1 6 34 34 48 .03 | 29908 3447
gfz 191| 0 0 3 -58 -28 100 -.16 25 23 | 247337 -1098 3943 7844
| 1 1 7 38 71 59 .05 | 27562 2427
iac n/a| 3 0 2 -37 25 -87 -.11 25 25 | 419093 -541 3945 8338
| 1 1 8 24 33 72 .05 | 27145 1781
mcc n/a| 0 6 48 -43 0 -141 .16 197 197 | --- --- --- ---
| 24 14 14 83 159 467 .81 | --- ---
Table 1.1590.b GPS week : 1590 MJD: 55374.0-55380.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 15 16 12 9 11 11 10 |
R02 | 25 23 12 11 9 9 9 |
R03 | 24 22 13 10 9 8 9 |
R04 | 14 13 10 9 9 7 10 |
R05 | 16 14 10 10 10 11 8 |
R07 | 12 10 12 9 11 14 10 |
R08 | 12 9 9 10 9 13 10 |
R10 | 10 14 11 9 9 12 10 |
R11 | 11 14 11 11 8 10 9 |
R13 | 11 10 12 8 14 9 10 |
R14 | 11 11 12 13 11 11 11 |
R15 | 11 17 15 13 15 12 17 |
R17 | 16 13 10 11 14 13 14 |
R18 | 11 12 13 11 10 11 11 |
R19 | 10 10 9 11 13 10 10 |
R20 | 14 13 12 16 12 11 15 |
R21 | 11 10 14 15 12 10 11 |
R22 | 16 13 12 16 13 9 12 |
R23 | 13 10 10 9 9 10 10 |
R24 | 14 14 12 13 9 10 11 |
Table 1.1590.c GPS week : 1590 MJD: 55374.0-55380.0
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 1590 0 | 13 -32 423 -1368 1698 -28830 83.3 2931 2931 | 420026 0
brd 1590 1 | -13 51 413 541 -1206 -24900 86.4 2765 2765 | 389398 0
brd 1590 2 | 16 99 420 1839 -439 -24040 85.4 2667 2667 | 423656 0
brd 1590 3 | -23 -23 416 879 -2335 -18560 86.1 2767 2767 | 472775 0
brd 1590 4 | 35 -2 521 713 -632 -20520 87.8 1994 1994 | 414656 0
brd 1590 5 | 27 -63 444 -88 -1837 -20000 86.2 1947 1947 | 418954 0
brd 1590 6 | 0 -7 357 650 -231 -17990 87.1 2123 2123 | 390447 0
-------------+------------------------------------------------------------+----------------
brd 1590 mean| 7 3 428 452 -711 -22120 86.0 2456 2456 | 418558 0
brd 1590 sdev| 21 55 48 985 1307 3941 1.4 417 417 | 27759 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 2.1590.0 GPS week: 1590 Day: 0 MJD: 55374
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]
--------+----------------------------------------------------+------------------------------
bkg 119| 2 -1 1 -1 97 94 -.11 29 25 | 0 -17 1895 1954
cod 238| -2 0 -5 54 -77 -73 -.13 20 17 | --- --- --- ---
esx 135| 0 3 -11 -19 -37 45 .42 26 25 | 73521 4602 3822 6279
gfz 191| 1 -1 -11 -78 -25 111 -.21 26 21 | 250344 1314 3829 6099
iac n/a| 2 0 16 -33 51 -34 -.10 24 24 | 420454 309 3823 6424
mcc n/a| 49 21 25 -89 -133 -306 .26 211 211 | --- --- --- ---
Table 2.1590.1 GPS week: 1590 Day: 1 MJD: 55375
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]
--------+----------------------------------------------------+------------------------------
bkg 119| 0 1 -19 -52 114 145 -.17 29 25 | 0 -38 1614 1687
cod 238| -2 -2 1 88 -47 -16 -.12 17 16 | --- --- --- ---
esx 135| 1 0 4 -57 -27 66 .44 24 22 | 51989 -659 3774 8421
gfz 191| 0 -1 6 -75 0 205 -.19 26 23 | 218761 -3131 3772 8288
iac n/a| 1 0 12 1 14 -219 -.18 26 26 | 390092 -837 3762 8823
mcc n/a| 0 11 39 -117 98 -887 -.45 413 413 | --- --- --- ---
Table 2.1590.2 GPS week: 1590 Day: 2 MJD: 55376
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]
--------+----------------------------------------------------+------------------------------
bkg 119| 1 -1 -9 -12 23 -110 -.09 23 23 | 0 11 1447 1523
cod 238| -1 -2 -2 23 -9 26 -.11 11 11 | --- --- --- ---
esx 135| -2 3 5 -19 28 155 .40 22 21 | 78190 -2766 3970 7671
gfz 191| 1 0 0 -74 19 118 -.11 22 21 | 253877 -4186 3948 7996
iac n/a| 2 0 5 -22 -19 -147 -.14 28 28 | 424651 -1690 3957 8541
mcc n/a| -28 17 38 -41 245 -495 1.79 321 321 | --- --- --- ---
Table 2.1590.3 GPS week: 1590 Day: 3 MJD: 55377
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]
--------+----------------------------------------------------+------------------------------
bkg 119| 1 -2 -9 20 37 156 -.06 21 21 | 0 -30 1997 2058
cod 238| 0 0 2 -9 -29 -68 -.08 10 10 | --- --- --- ---
esx 135| 0 1 9 30 -1 2 .42 26 23 | 129397 -1632 4601 8446
gfz 191| 0 3 7 -22 60 19 -.13 25 26 | 300973 -1291 4565 8327
iac n/a| 1 -1 -3 -25 73 -11 -.05 28 28 | 471600 1333 4590 9052
mcc n/a| -2 11 58 11 -122 -193 .32 98 98 | --- --- --- ---
Table 2.1590.4 GPS week: 1590 Day: 4 MJD: 55378
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]
--------+----------------------------------------------------+------------------------------
bkg 119| 0 -1 -2 -1 -26 8 -.12 20 20 | 0 -23 1749 1809
cod 238| -2 -1 4 54 -18 -17 -.17 13 13 | --- --- --- ---
esx 135| 0 0 0 -60 57 66 .41 20 20 | 60709 -3787 3827 7782
gfz 191| 1 -1 7 9 -134 48 -.10 23 24 | 242209 -1909 3827 7745
iac n/a| 3 2 -6 -53 -10 -55 -.14 23 23 | 417003 -3635 3838 8482
mcc n/a| -10 10 57 108 -195 237 .15 98 98 | --- --- --- ---
Table 2.1590.5 GPS week: 1590 Day: 5 MJD: 55379
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]
--------+----------------------------------------------------+------------------------------
bkg 119| 3 0 -5 -26 -3 -28 -.12 18 18 | 0 64 1695 1749
cod 238| -3 0 4 53 7 22 -.13 13 12 | --- --- --- ---
esx 135| 0 0 2 -18 -14 66 .38 22 21 | 59283 4997 3710 7805
gfz 191| 2 -1 8 -103 -116 117 -.20 25 26 | 245866 2792 3695 7749
iac n/a| 5 -1 -4 -71 42 -65 -.06 22 22 | 418796 1410 3690 7921
mcc n/a| -7 -11 62 -40 0 419 -.49 116 116 | --- --- --- ---
Table 2.1590.6 GPS week: 1590 Day: 6 MJD: 55380
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]
--------+----------------------------------------------------+------------------------------
bkg 119| 4 -1 -6 -45 12 -47 -.09 18 18 | 0 40 1786 1890
cod 238| -2 0 1 39 7 21 -.10 15 14 | --- --- --- ---
esx 135| 0 0 2 20 -23 108 .36 21 18 | 34861 582 3953 8412
gfz 191| 0 -1 5 -62 0 82 -.20 27 24 | 219329 -1276 3971 8710
iac n/a| 3 0 1 -56 25 -81 -.10 22 22 | 391056 -680 3959 9125
mcc n/a| -2 -16 59 -132 102 236 -.49 124 124 | --- --- --- ---
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 3.1590.0 GPS week: 1590 Day: 0 MJD: 55374
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 3024 25 22 25 26 30 --- 15 | 49 68 65 68 64 --- 59
R02E | 2922 59 33 43 39 39 --- 25 | 70 115 122 119 98 --- 98
R03E | 1369 52 32 44 47 40 --- 24 | 55 83 93 92 80 --- 71
R04E | 891 33 20 22 30 23 --- 14 | 38 51 57 56 55 --- 47
R05E | 1819 34 30 27 29 14 --- 15 | 37 46 48 51 47 --- 37
R07 | 4387 25 13 20 22 24 --- 12 | 24 21 27 21 29 --- 18
R08E | 4563 21 12 23 26 23 346 11 | 40 54 59 58 49 236 48
R10 | 1865 17 18 21 24 14 --- 10 | 22 31 34 23 24 --- 25
R11 | 1344 22 10 24 23 14 --- 10 | 33 31 44 39 34 --- 31
R13 | 2363 13 16 22 21 19 --- 10 | 24 29 35 30 25 --- 23
R14 | 4094 16 15 21 25 23 --- 11 | 19 21 36 36 30 --- 22
R15 | 6716 20 11 23 16 23 94 11 | 23 20 40 31 30 23 22
R17 | 1453 30 19 21 29 36 --- 15 | 47 58 64 66 38 --- 50
R18 | 2130 17 22 23 22 14 --- 11 | 30 36 46 42 31 --- 31
R19 | 1486 18 13 16 15 19 --- 9 | 41 49 54 54 50 --- 46
R20 | 3418 27 19 23 29 26 --- 13 | 29 28 27 34 30 --- 24
R21 | 2364 19 14 26 17 15 --- 10 | 37 40 31 34 31 --- 31
R22 | 1490 34 21 34 30 19 --- 15 | 75 66 59 65 62 --- 63
R23 | 2251 23 18 27 21 20 76 12 | 26 36 47 51 55 110 38
R24 | 1362 29 14 24 16 26 --- 13 | 17 38 48 35 37 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2930 29 20 26 26 24 211 |T 36 46 51 50 44 123 40
WRMS | 2930 25 17 25 21 24 211 |NE 31 36 42 40 36 66 32
MEDI | 2130 23 18 23 24 23 94 |MD 33 38 47 42 37 110 34
Table 3.1590.1 GPS week: 1590 Day: 1 MJD: 55375
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 4340 37 15 22 28 32 --- 15 | 62 63 60 63 49 --- 52
R02 | 2949 63 30 29 36 33 --- 23 | 49 114 114 115 74 --- 85
R03 | 1243 55 20 46 39 32 --- 22 | 43 82 112 103 60 --- 68
R04 | 856 26 18 21 26 20 --- 12 | 39 63 66 67 58 --- 55
R05 | 986 27 19 27 21 23 --- 13 | 37 50 53 48 34 --- 39
R07 | 2275 16 15 22 22 14 --- 10 | 27 24 39 25 26 --- 24
R08 | 2485 19 9 12 13 20 698 8 | 33 38 46 49 43 236 36
R10 | 1082 22 17 35 36 21 --- 14 | 21 28 49 46 16 --- 25
R11 | 1457 24 17 30 33 22 --- 13 | 38 32 48 40 36 --- 33
R13 | 1256 12 11 18 15 24 --- 9 | 21 30 34 34 33 --- 25
R14 | 3235 19 13 13 18 29 --- 11 | 15 24 32 27 35 --- 20
R15 | 8058 37 12 20 20 43 86 16 | 36 31 37 42 25 19 25
R17 | 1311 18 25 16 27 29 --- 13 | 34 37 51 40 54 --- 41
R18 | 883 30 16 15 32 18 --- 11 | 41 31 37 34 45 --- 34
R19 | 1303 16 14 25 20 11 --- 10 | 31 46 61 51 39 --- 42
R20 | 2182 16 22 19 33 30 --- 13 | 21 24 31 40 39 --- 25
R21 | 2831 23 10 17 26 21 --- 10 | 28 35 38 30 37 --- 31
R22 | 1103 19 17 21 14 28 --- 12 | 49 49 38 38 39 --- 40
R23 | 2998 16 15 15 20 24 128 10 | 26 35 36 41 41 53 30
R24 | 1807 26 18 23 14 29 --- 13 | 20 38 37 31 44 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 2764 29 17 24 26 26 413 |T 33 43 50 48 41 102 37
WRMS | 2764 25 16 22 23 26 413 |NE 29 33 40 37 36 36 30
MEDI | 1457 22 16 21 22 24 128 |MD 33 35 39 40 39 53 33
Table 3.1590.2 GPS week: 1590 Day: 2 MJD: 55376
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 4307 24 8 26 17 26 --- 12 | 40 38 54 40 48 --- 38
R02 | 3829 24 11 21 18 32 --- 12 | 51 60 65 53 79 --- 61
R03 | 1173 17 9 20 24 43 --- 13 | 45 41 52 47 63 --- 46
R04 | 1494 16 11 15 16 26 --- 9 | 33 33 52 49 54 --- 38
R05 | 983 15 12 15 20 26 --- 9 | 21 28 30 29 41 --- 26
R07 | 1401 23 9 30 23 18 --- 11 | 31 25 38 32 16 --- 22
R08 | 1062 26 6 14 22 20 486 9 | 36 38 48 38 43 205 39
R10 | 1653 21 12 29 25 16 --- 11 | 30 30 37 20 24 --- 23
R11 | 5098 26 12 22 33 20 --- 11 | 39 26 40 41 26 --- 28
R13 | 835 24 12 23 22 29 --- 12 | 17 26 40 37 35 --- 24
R14 | 2486 16 14 14 9 38 --- 12 | 23 22 31 27 21 --- 19
R15 | 6397 28 17 20 22 40 132 14 | 40 41 28 35 30 45 29
R17 | 1599 21 15 10 20 21 --- 9 | 20 40 39 34 31 --- 33
R18 | 2497 32 14 24 21 26 --- 13 | 16 32 42 39 41 --- 29
R19 | 1189 11 9 25 22 14 --- 9 | 34 36 60 34 43 --- 40
R20 | 1744 29 12 21 27 25 --- 12 | 27 26 29 34 29 --- 21
R21 | 1870 35 8 30 29 21 --- 13 | 31 34 59 56 36 --- 37
R22 | 1034 22 12 19 33 34 --- 12 | 40 37 51 54 60 --- 42
R23 | 1872 15 10 18 19 25 237 9 | 25 18 42 30 19 165 21
R24 | 1871 15 13 26 11 29 --- 11 | 19 32 38 24 16 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 2667 23 11 22 22 28 321 |T 30 33 43 37 37 138 32
WRMS | 2667 23 11 21 21 28 321 |NE 28 30 41 35 30 105 28
MEDI | 1653 22 12 21 22 26 237 |MD 31 32 40 35 35 165 29
Table 3.1590.3 GPS week: 1590 Day: 3 MJD: 55377
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3148 21 10 17 16 19 --- 9 | 44 58 62 56 38 --- 50
R02 | 3630 18 10 20 21 30 --- 10 | 33 43 51 50 59 --- 42
R03 | 2011 18 5 16 22 36 --- 10 | 25 27 34 30 47 --- 26
R04 | 2129 12 8 15 18 28 --- 8 | 27 40 45 36 44 --- 36
R05 | 754 16 6 18 21 30 --- 9 | 26 32 35 35 38 --- 28
R07 | 1423 21 7 21 20 16 --- 9 | 37 32 35 32 29 --- 29
R08 | 6380 22 11 23 25 17 113 10 | 35 45 52 56 25 211 37
R10 | 2085 18 8 22 29 22 --- 9 | 26 27 29 30 27 --- 21
R11 | 2696 20 10 26 21 21 --- 10 | 20 24 32 28 34 --- 20
R13 | 996 12 9 20 31 19 --- 8 | 23 25 31 39 20 --- 22
R14 | 1586 16 12 24 21 42 --- 13 | 22 25 36 25 35 --- 22
R15 | 5677 27 9 32 35 23 64 12 | 19 25 52 55 21 51 24
R17 | 1328 20 12 16 23 31 --- 10 | 32 46 55 56 35 --- 41
R18 | 1546 16 11 13 24 38 --- 11 | 24 24 32 28 23 --- 21
R19 | 1112 24 6 19 23 29 --- 10 | 39 30 38 37 26 --- 28
R20 | 2099 41 12 32 27 33 --- 16 | 26 32 47 44 36 --- 26
R21 | 1336 21 17 47 34 19 --- 15 | 40 51 62 60 41 --- 43
R22 | 1374 30 10 44 26 31 --- 15 | 38 42 60 51 43 --- 39
R23 | 2717 21 7 19 20 21 108 9 | 16 25 36 41 23 69 22
R24 | 3155 16 10 34 29 38 --- 13 | 21 31 47 41 27 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 2767 21 10 26 25 28 98 |T 28 34 43 41 33 110 30
WRMS | 2767 21 10 23 26 28 98 |NE 27 31 42 40 30 60 27
MEDI | 2011 20 10 20 23 28 108 |MD 26 31 38 39 34 69 27
Table 3.1590.4 GPS week: 1590 Day: 4 MJD: 55378
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3649 15 17 26 25 17 --- 11 | 30 30 50 50 30 --- 32
R02 | 2765 17 11 16 23 21 --- 9 | 35 42 49 50 45 --- 40
R03 | 2016 20 12 11 21 21 --- 9 | 20 26 40 37 43 --- 29
R04 | 2648 11 9 16 25 22 --- 8 | 17 29 38 40 35 --- 26
R05 | 891 14 10 17 26 26 --- 9 | 19 26 40 44 37 --- 27
R07 | 2226 16 10 24 20 22 --- 10 | 28 26 43 37 22 --- 26
R08 | 745 15 18 8 25 20 111 9 | 29 32 29 37 32 81 29
R10 | 890 14 10 14 20 25 --- 9 | 24 31 32 33 27 --- 25
R11 | 1454 12 11 13 18 16 --- 7 | 29 31 25 26 25 --- 25
R13 | 1395 18 14 33 22 28 --- 13 | 15 20 36 37 35 --- 21
R14 | 974 18 14 16 19 29 --- 11 | 21 25 22 28 23 --- 18
R15 | 2179 39 9 29 19 18 76 14 | 28 29 29 29 33 24 24
R17 | 1429 27 16 17 16 36 --- 14 | 30 39 42 34 27 --- 31
R18 | 556 22 11 18 13 15 --- 9 | 21 21 30 19 20 --- 17
R19 | 895 26 9 8 31 40 --- 13 | 28 38 47 51 55 --- 39
R20 | 1662 22 18 28 29 12 --- 12 | 20 34 47 43 35 --- 28
R21 | 1029 24 15 26 16 13 --- 11 | 28 23 40 35 21 --- 25
R22 | 1756 20 20 21 24 29 --- 13 | 42 37 37 42 22 --- 29
R23 | 2690 15 9 23 29 13 103 9 | 26 25 31 31 18 34 20
R24 | 3652 13 11 19 29 18 --- 8 | 21 24 34 35 18 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1994 20 13 20 23 23 98 |T 25 29 37 36 30 46 26
WRMS | 1994 20 13 20 24 23 98 |NE 25 28 35 34 27 29 24
MEDI | 1454 17 11 17 22 21 103 |MD 26 29 37 37 27 34 26
Table 3.1590.5 GPS week: 1590 Day: 5 MJD: 55379
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3678 18 11 15 31 28 --- 10 | 34 38 42 47 34 --- 34
R02 | 3011 14 12 22 21 14 --- 9 | 38 56 71 69 51 --- 53
R03 | 1887 10 10 15 24 19 --- 8 | 31 31 41 40 40 --- 33
R04 | 3018 10 9 10 26 16 --- 6 | 16 18 31 30 26 --- 20
R05 | 1025 8 12 24 12 26 --- 10 | 23 20 35 28 32 --- 23
R07 | 1593 23 18 34 22 19 --- 13 | 39 25 49 41 33 --- 31
R08 | 2120 23 15 26 34 25 128 12 | 13 23 33 31 22 103 17
R10 | 2207 15 20 20 22 26 --- 12 | 18 33 32 23 28 --- 24
R11 | 874 15 10 25 36 19 --- 10 | 16 25 38 50 23 --- 21
R13 | 876 14 15 19 26 14 --- 9 | 19 21 23 20 24 --- 17
R14 | 1306 17 14 16 20 29 --- 11 | 15 24 37 27 30 --- 21
R15 | 1154 30 6 18 27 27 77 12 | 28 30 33 29 31 15 28
R17 | 1605 25 13 31 38 24 --- 13 | 16 27 27 22 22 --- 17
R18 | 954 17 12 26 16 18 --- 10 | 24 23 25 14 12 --- 14
R19 | 842 14 11 18 27 27 --- 10 | 18 21 29 24 23 --- 19
R20 | 1452 25 11 27 20 13 --- 11 | 26 24 29 32 20 --- 19
R21 | 950 13 13 22 10 19 --- 9 | 31 21 31 25 32 --- 22
R22 | 1424 11 13 17 26 23 --- 9 | 29 27 32 39 21 --- 24
R23 | 2297 17 13 18 26 19 134 9 | 18 22 30 27 19 35 18
R24 | 2911 24 10 19 21 14 --- 9 | 16 14 25 25 22 --- 12
------+-----------------------------------------+-------------------------------------
RMS | 1946 18 13 22 25 22 116 |T 23 26 34 32 27 51 23
WRMS | 1946 18 12 21 26 22 116 |NE 22 24 31 28 24 25 20
MEDI | 1452 15 12 19 24 19 128 |MD 19 24 32 28 24 35 21
Table 3.1590.6 GPS week: 1590 Day: 6 MJD: 55380
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2511 16 12 18 16 25 --- 10 | 32 34 30 29 33 --- 29
R02 | 2355 15 10 10 13 24 --- 8 | 47 55 56 60 60 --- 52
R03 | 1852 16 12 15 13 16 --- 8 | 43 39 52 47 43 --- 42
R04 | 2320 10 16 24 28 14 --- 9 | 23 26 35 32 35 --- 27
R05 | 1644 12 9 16 14 21 --- 8 | 22 21 29 33 32 --- 22
R07 | 1237 17 13 17 60 24 --- 10 | 28 28 33 38 31 --- 25
R08 | 3680 15 14 19 14 16 120 9 | 29 30 33 26 28 94 25
R10 | 1662 10 16 16 21 23 --- 9 | 21 25 27 21 24 --- 20
R11 | 1454 11 15 19 32 12 --- 8 | 19 29 31 35 21 --- 21
R13 | 2107 23 12 12 32 23 --- 10 | 20 19 27 30 31 --- 21
R14 | 3043 23 13 18 23 21 --- 10 | 20 23 26 25 23 --- 19
R15 | 2681 20 14 43 39 33 79 16 | 23 26 51 32 34 22 26
R17 | 1994 28 11 20 26 36 --- 14 | 29 43 44 46 31 --- 36
R18 | 922 22 17 12 24 20 --- 10 | 18 27 26 21 21 --- 21
R19 | 1172 17 12 15 26 21 --- 9 | 27 30 39 33 34 --- 30
R20 | 3401 21 20 37 17 23 --- 15 | 25 21 40 24 27 --- 22
R21 | 1099 16 22 18 32 13 --- 10 | 30 43 41 52 31 --- 34
R22 | 1282 21 18 22 18 23 --- 12 | 43 49 34 42 41 --- 39
R23 | 1089 13 14 21 27 21 159 10 | 26 33 23 29 31 53 25
R24 | 2013 18 17 14 24 24 --- 10 | 23 32 30 36 29 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2122 18 15 21 27 22 124 |T 27 31 35 34 32 56 28
WRMS | 2122 18 14 18 24 22 124 |NE 25 30 33 33 29 37 26
MEDI | 1852 16 14 18 24 21 120 |MD 25 29 33 32 31 53 25
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