[IGSREPORT-18735] Wk 1588 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Fri Jul 2 06:47:59 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1588 (Jun 13, 2010 - Jun 19, 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 2.1588.
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:
igl1588[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1588 in the SP3 format.
igl15887.sum Combination Report for GPS Week 1588.
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 | 460.4 ns
1 | 410.1 ns
2 | 466.5 ns
3 | 403.7 ns
4 | 408.6 ns
5 | 406.7 ns
6 | 466.9 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 1.1588, 1a.1588).
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 2.1588.0-6)
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 3.1588.0-6).
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 1588 summary. (Jun 13, 2010 - Jun 19, 2010)
Table 1.1588.a GPS week : 1588 MJD: 55360.0-55366.0
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| 3 1 -7 -26 2 -62 -.14 36 35 | 0 0 1744 1812
| 0 2 2 17 43 120 .04 | 0 77
cod 244| -3 0 -4 34 -51 -5 -.17 19 16 | --- --- --- ---
| 0 2 2 23 24 59 .03 | --- ---
esx 140| 1 0 -2 10 59 83 .32 27 25 | 99385 -1869 3960 7447
| 0 1 3 33 23 86 .04 | 30998 3009
gfz 199| 0 0 0 -72 -23 163 -.24 30 30 | 270724 -1891 3993 7469
| 0 2 2 70 70 107 .08 | 31734 3147
iac n/a| 2 0 18 -61 31 31 -.02 36 36 | 432218 -861 3968 8053
| 1 2 4 27 30 55 .04 | 31423 1539
mcc n/a| 0 -4 15 -125 -195 -590 -.27 236 236 | --- --- --- ---
| 11 15 47 327 606 867 .55 | --- ---
Table 1.1588.b GPS week : 1588 MJD: 55360.0-55366.0
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 15 18 18 20 20 18 |
R02 | 27 25 21 20 20 20 19 |
R03 | 27 15 13 14 15 17 18 |
R04 | 23 18 15 13 15 21 16 |
R05 | 26 24 23 18 16 19 19 |
R07 | 62 62 72 34 22 18 13 |
R08 | 27 30 34 30 22 19 16 |
R10 | 20 10 14 12 11 12 12 |
R11 | 12 10 10 12 12 11 12 |
R13 | 10 11 17 10 11 11 13 |
R14 | 12 10 18 14 14 13 11 |
R15 | 13 13 16 28 17 9 11 |
R17 | 20 17 24 20 19 19 14 |
R18 | 13 12 13 11 11 16 15 |
R19 | 12 12 11 12 13 14 12 |
R20 | 18 19 13 18 20 16 12 |
R21 | 13 13 13 13 15 12 9 |
R22 | 10 26 19 13 10 14 17 |
R23 | 10 8 17 11 9 10 13 |
R24 | 12 11 15 15 12 11 16 |
Table 1.1588.c GPS week : 1588 MJD: 55360.0-55366.0
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 1588 0 | 69 -46 392 -1192 -602 -16350 87.8 2216 2216 | 460361 0
brd 1588 1 | -115 60 425 -273 9 -15750 86.8 2417 2417 | 410063 0
brd 1588 2 | 85 -32 378 3425 3364 -12440 86.7 2180 2180 | 466513 0
brd 1588 3 | 14 71 528 1746 -252 -6672 86.2 3302 3302 | 403741 0
brd 1588 4 | -76 83 490 184 -607 -8247 90.2 1978 1978 | 408635 0
brd 1588 5 | -41 -14 459 988 -1964 -9958 87.2 2548 2548 | 406704 0
brd 1588 6 | 44 14 397 -396 -813 -13680 89.3 2092 2092 | 466902 0
-------------+------------------------------------------------------------+----------------
brd 1588 mean| -2 19 438 640 -123 -11871 87.8 2390 2390 | 431845 0
brd 1588 sdev| 76 53 55 1558 1659 3708 1.5 445 445 | 30765 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 2.1588.0 GPS week: 1588 Day: 0 MJD: 55360
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 2 -7 -26 -27 -40 -.19 47 46 | 0 -69 1667 1741
cod 244| -3 -1 -8 45 -43 71 -.18 19 15 | --- --- --- ---
esx 140| 1 0 1 -25 55 10 .33 28 26 | 127966 -931 3538 7080
gfz 199| 0 -3 2 -157 -108 199 -.19 32 32 | 300426 -4322 3523 7472
iac n/a| 3 1 18 -72 25 -47 -.04 37 37 | 461355 -2211 3542 8032
mcc n/a| 0 23 63 -787 239 787 -.31 289 289 | --- --- --- ---
Table 2.1588.1 GPS week: 1588 Day: 1 MJD: 55361
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 3 -10 -54 -19 -102 -.19 44 41 | 0 -8 1458 1529
cod 244| -1 -2 -4 65 -42 27 -.19 18 16 | --- --- --- ---
esx 140| 3 -1 1 19 79 86 .26 23 22 | 82620 1534 3863 8137
gfz 199| -1 2 3 -117 -43 294 -.18 27 27 | 249316 -731 3863 8110
iac n/a| 4 3 12 -91 38 -16 -.03 38 38 | 410378 -901 3855 8470
mcc n/a| -9 -10 25 -189 -352 -1260 -1.25 412 412 | --- --- --- ---
Table 2.1588.2 GPS week: 1588 Day: 2 MJD: 55362
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 0 -7 -33 45 -161 -.12 43 42 | 0 -33 1969 2027
cod 244| -2 1 -5 47 -79 53 -.17 23 20 | --- --- --- ---
esx 140| 1 -3 -3 -9 60 25 .29 25 25 | 142079 -7500 4623 7924
gfz 199| 0 1 0 -21 41 117 -.30 31 31 | 309414 -7583 4641 7626
iac n/a| 0 0 19 -38 48 129 -.03 34 34 | 467954 -2888 4623 8263
mcc n/a| -7 -28 42 -59 -1490 367 -.54 407 407 | --- --- --- ---
Table 2.1588.3 GPS week: 1588 Day: 3 MJD: 55363
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 -10 -15 69 -139 -.16 33 32 | 0 167 1694 1770
cod 244| -3 3 -3 -5 -86 -10 -.16 23 17 | --- --- --- ---
esx 140| 1 0 0 24 43 158 .38 32 28 | 67610 995 3607 7064
gfz 199| 0 1 1 -10 69 222 -.10 28 28 | 241198 1651 3631 6733
iac n/a| 5 -3 25 -22 45 30 -.02 38 38 | 402771 1511 3622 7446
mcc n/a| 20 -10 -47 -55 251 -943 -.28 117 117 | --- --- --- ---
Table 2.1588.4 GPS week: 1588 Day: 4 MJD: 55364
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 2 -2 -1 23 -47 -.12 30 29 | 0 -27 1636 1696
cod 244| -3 0 -4 44 -61 -46 -.22 20 18 | --- --- --- ---
esx 140| 0 0 -4 -26 17 110 .32 26 22 | 77535 -1563 4079 6875
gfz 199| 0 -4 -4 8 34 -25 -.28 29 29 | 247388 -1838 4151 7038
iac n/a| 1 1 20 -47 72 36 -.04 34 34 | 408965 -298 4096 7747
mcc n/a| -7 1 -57 271 -87 -423 .51 55 55 | --- --- --- ---
Table 2.1588.5 GPS week: 1588 Day: 5 MJD: 55365
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 -2 -5 -16 -45 189 -.09 31 31 | 0 -39 1754 1811
cod 244| -3 0 -3 16 -30 -91 -.12 17 15 | --- --- --- ---
esx 140| 0 0 -7 23 89 -24 .29 27 25 | 72894 -2596 3878 7624
gfz 199| 0 0 0 -55 -94 99 -.34 28 28 | 243904 679 3943 7444
iac n/a| 1 0 21 -59 -21 30 -.03 35 35 | 406501 435 3904 8008
mcc n/a| 11 -2 31 -125 19 -1341 -.07 206 206 | --- --- --- ---
Table 2.1588.6 GPS week: 1588 Day: 6 MJD: 55366
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 2 -6 -38 -29 -137 -.14 24 24 | 0 10 2035 2115
cod 244| -2 -1 -1 28 -20 -41 -.17 16 14 | --- --- --- ---
esx 140| 3 1 -2 65 67 219 .36 29 28 | 124997 -3023 4137 7427
gfz 199| 0 -1 0 -156 -60 237 -.28 31 31 | 303426 -1094 4200 7860
iac n/a| 2 0 11 -96 8 55 .07 36 36 | 467606 -1681 4134 8408
mcc n/a| -1 -6 47 63 52 -1320 .08 168 168 | --- --- --- ---
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 3.1588.0 GPS week: 1588 Day: 0 MJD: 55360
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2200 35 11 26 33 36 --- 15 | 26 29 39 38 33 --- 26
R02E | 2074 81 23 46 42 44 --- 27 | 83 70 55 64 89 --- 65
R03E | 1405 71 19 28 28 69 --- 26 | 36 26 26 25 53 --- 22
R04E | 2194 70 26 23 20 46 --- 23 | 32 25 30 34 50 --- 25
R05E | 1478 62 27 47 32 56 --- 26 | 47 38 51 54 56 --- 36
XR07E | ---- --- 45 --- --- 85 --- 61 | --- 50 --- --- 81 --- 51
R08E | 1806 99 17 37 37 32 375 27 | 33 28 29 30 39 209 21
R10 | 1504 39 37 28 42 34 --- 20 | 54 41 30 35 39 --- 31
R11 | 941 24 11 27 26 25 --- 12 | 36 42 44 55 34 --- 37
R13 | 1696 17 13 18 31 23 --- 10 | 33 30 37 47 41 --- 33
R14 | 2273 22 13 21 19 28 --- 12 | 29 20 28 27 37 --- 22
R15 | 6004 30 13 26 19 21 162 12 | 34 32 31 29 28 306 25
R17 | 958 33 24 26 43 55 --- 20 | 41 52 62 60 33 --- 47
R18 | 1285 23 14 22 42 34 --- 13 | 24 47 53 65 35 --- 39
R19 | 2058 20 15 22 26 27 --- 12 | 36 32 55 53 54 --- 40
R20 | 3132 44 19 17 26 48 --- 18 | 60 70 67 83 88 --- 67
R21 | 1159 26 16 26 30 22 --- 12 | 58 66 65 87 64 --- 62
R22 | 1261 22 15 19 30 15 --- 10 | 55 64 64 66 80 --- 63
R23 | 578 17 16 20 38 17 --- 10 | 35 34 45 61 48 --- 37
R24 | 2190 32 12 26 33 17 --- 12 | 38 49 67 71 46 --- 49
------+-----------------------------------------+-------------------------------------
RMS | 2216 47 19 28 32 37 289 |T 41 42 46 51 51 257 39
WRMS | 2216 46 15 26 32 37 289 |NE 41 44 49 56 48 306 42
MEDI | 1696 32 16 26 31 32 162 |MD 36 38 45 54 46 209 37
Table 3.1588.1 GPS week: 1588 Day: 1 MJD: 55361
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 3010 34 11 19 29 42 --- 14 | 34 25 36 37 40 --- 26
R02E | 3992 92 19 30 43 30 --- 25 | 44 36 41 53 48 --- 36
R03E | 1735 39 14 18 29 34 --- 14 | 18 18 23 36 39 --- 18
R04E | 940 44 15 20 27 51 --- 18 | 26 17 22 31 56 --- 20
R05E | 1615 35 33 23 24 71 --- 23 | 36 47 66 55 73 --- 47
XR07E |10514 89 54 --- --- 133 --- 61 | 73 63 --- --- 64 --- 53
R08E | 2953 108 27 25 38 41 141 29 | 36 34 41 42 49 157 28
R10 | 1128 13 17 13 19 25 --- 10 | 23 21 24 25 24 --- 18
R11 | 957 22 12 21 26 18 --- 10 | 25 33 40 39 33 --- 31
R13 | 1228 26 9 20 27 20 --- 10 | 42 29 50 42 53 --- 40
R14 | 1925 20 10 14 26 29 --- 10 | 28 25 36 44 33 --- 24
R15 | 6574 24 15 28 19 23 630 12 | 29 34 44 32 27 179 30
R17 | 1761 33 11 32 15 44 --- 16 | 16 26 59 49 26 --- 30
R18 | 1990 22 20 19 16 24 --- 12 | 12 32 27 33 35 --- 21
R19 | 1564 26 16 19 39 27 --- 12 | 26 21 29 48 35 --- 23
R20 | 2153 38 15 27 23 54 --- 18 | 57 64 82 82 82 --- 68
R21 | 1246 23 13 29 26 23 --- 12 | 40 52 78 77 40 --- 53
R22 | 941 57 29 36 23 65 --- 25 | 19 28 74 62 99 --- 47
R23 | 1007 16 10 15 31 19 302 8 | 24 34 37 43 26 89 29
R24 | 1582 31 11 16 24 19 --- 10 | 54 37 45 55 39 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 2416 44 18 23 27 38 412 |T 33 33 44 46 46 141 34
WRMS | 2416 41 16 22 27 38 412 |NE 30 33 48 48 42 134 35
MEDI | 1615 31 15 20 26 29 302 |MD 28 32 41 43 39 157 30
Table 3.1588.2 GPS week: 1588 Day: 2 MJD: 55362
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1502 42 22 20 42 38 --- 17 | 25 35 37 39 39 --- 26
R02E | 2345 50 24 31 31 42 --- 21 | 47 36 38 38 57 --- 33
R03E | 993 27 16 18 36 28 --- 12 | 29 18 35 43 45 --- 24
R04E | 3109 30 16 23 40 37 --- 15 | 19 20 27 37 44 --- 20
R05E | 1585 52 22 36 32 48 --- 22 | 40 59 68 70 91 --- 57
XR07E | 2501 100 70 --- --- 137 --- 72 | 53 93 --- --- 99 --- 66
R08E | 2855 116 43 30 58 36 207 34 | 37 28 39 42 47 101 27
R10 | 1645 12 18 22 14 40 --- 14 | 23 25 23 19 36 --- 18
R11 | 1499 17 18 19 22 14 --- 10 | 26 37 45 44 31 --- 33
R13 | 1132 19 25 24 35 44 --- 16 | 27 37 49 51 32 --- 33
R14 | 1537 33 32 21 27 35 --- 17 | 20 30 28 32 36 --- 22
R15 | 5146 40 20 23 33 33 --- 16 | 32 31 39 45 27 --- 25
R17 | 2718 46 28 37 32 55 --- 23 | 36 41 57 49 31 --- 38
R18 | 1960 33 16 18 14 25 --- 13 | 13 25 31 25 45 --- 24
R19 | 1515 23 11 19 10 19 --- 10 | 26 22 31 33 43 --- 27
R20 | 1967 34 17 12 34 29 --- 13 | 32 35 42 60 48 --- 35
R21 | 1571 23 20 23 14 23 --- 13 | 39 52 72 62 63 --- 55
R22 | 1757 50 30 27 30 26 --- 19 | 43 46 65 52 67 --- 51
R23 | 1233 21 27 33 24 31 537 16 | 35 30 49 41 46 14 33
R24 | 1291 33 15 30 23 21 --- 14 | 35 44 55 56 33 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 2180 43 23 25 31 34 407 |T 31 37 43 44 48 57 34
WRMS | 2180 42 20 25 31 34 407 |NE 29 35 45 43 41 14 33
MEDI | 1585 33 20 23 31 33 207 |MD 32 35 39 43 44 14 33
Table 3.1588.3 GPS week: 1588 Day: 3 MJD: 55363
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1329 34 24 30 45 38 --- 17 | 25 31 37 41 31 --- 22
R02E | 1248 48 26 26 36 40 --- 20 | 43 39 37 49 66 --- 37
R03E | 872 20 15 22 22 37 --- 13 | 15 39 36 40 46 --- 27
R04E | 3144 27 11 27 29 28 --- 13 | 23 25 35 40 35 --- 22
R05E | 806 25 16 42 36 37 --- 17 | 21 31 47 40 45 --- 27
R07E | 1918 50 53 58 --- 75 --- 33 | 44 71 46 --- 41 --- 33
R08E | 1894 75 42 42 37 45 117 30 | 41 32 44 32 39 63 22
R10 | 1489 9 20 24 11 24 --- 11 | 23 24 35 18 26 --- 19
R11 | 992 15 14 20 21 32 --- 11 | 28 35 49 41 44 --- 34
R13 | 2735 19 9 10 20 27 --- 9 | 36 29 31 47 43 --- 30
R14 | 1412 26 23 16 14 30 --- 14 | 28 28 32 32 31 --- 23
R15 |11508 36 21 64 37 69 --- 27 | 39 42 95 70 38 --- 45
R17 | 1836 38 20 38 23 47 --- 20 | 31 55 67 41 34 --- 43
R18 | 2093 16 16 28 18 12 --- 11 | 30 23 55 46 38 --- 32
R19 | 1838 27 10 17 17 29 --- 12 | 15 33 39 35 59 --- 30
R20 | 5653 30 18 27 25 47 --- 17 | 22 46 42 38 54 --- 32
R21 | 1605 25 18 22 33 23 --- 12 | 22 52 43 43 48 --- 38
R22 | 1997 30 21 21 31 17 --- 13 | 33 50 66 71 50 --- 47
R23 | 976 18 12 25 26 17 --- 10 | 21 28 49 50 37 --- 30
R24 | 619 30 21 27 29 23 --- 14 | 33 49 42 56 38 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 3301 33 23 32 28 38 117 |T 28 38 46 43 42 63 31
WRMS | 3301 32 17 28 28 38 117 |NE 27 38 49 45 41 --- 33
MEDI | 1605 27 18 26 26 30 117 |MD 28 33 42 41 39 63 30
Table 3.1588.4 GPS week: 1588 Day: 4 MJD: 55364
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1949 37 27 26 36 46 --- 19 | 24 34 38 42 39 --- 23
R02E | 764 39 30 23 38 43 --- 19 | 32 48 48 53 50 --- 39
R03E | 998 35 14 25 33 30 --- 15 | 17 23 40 35 42 --- 24
R04E | 2478 30 16 23 27 36 --- 15 | 21 19 36 37 39 --- 17
R05E | 885 30 13 36 53 32 --- 16 | 28 22 52 56 42 --- 29
R07E | 957 35 28 32 --- 57 --- 21 | 33 53 53 --- 42 --- 34
R08E | 2376 56 31 19 31 45 55 22 | 36 18 27 21 51 67 21
R10 | 956 18 13 20 18 25 --- 11 | 21 23 26 29 24 --- 18
R11 | 751 16 18 21 35 29 --- 12 | 32 27 41 47 33 --- 28
R13 | 2209 18 18 18 24 21 --- 10 | 22 27 33 35 32 --- 24
R14 | 1296 30 12 15 18 34 --- 13 | 24 17 28 27 29 --- 17
R15 | 4273 23 22 27 28 43 --- 16 | 24 28 49 46 27 --- 26
R17 | 1203 39 26 36 32 26 --- 18 | 57 66 33 32 50 --- 47
R18 | 878 26 15 13 19 24 --- 11 | 23 33 30 33 44 --- 28
R19 | 3413 17 20 18 18 31 --- 12 | 34 20 36 36 45 --- 27
R20 | 2941 34 28 41 22 36 --- 20 | 19 31 45 29 49 --- 27
R21 | 1726 23 22 34 24 26 --- 15 | 28 42 50 46 50 --- 36
R22 | 1779 19 12 18 22 21 --- 10 | 67 54 64 71 62 --- 58
R23 | 845 11 13 18 28 18 --- 8 | 41 36 45 47 43 --- 38
R24 | 1918 19 9 29 30 22 --- 12 | 32 36 51 54 25 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1978 30 20 26 29 34 55 |T 30 32 41 40 40 67 29
WRMS | 1978 29 18 22 29 34 55 |NE 32 33 40 40 39 --- 31
MEDI | 1296 26 18 23 28 30 55 |MD 28 28 40 37 42 67 27
Table 3.1588.5 GPS week: 1588 Day: 5 MJD: 55365
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 969 39 20 23 35 54 --- 19 | 24 19 29 39 48 --- 21
R02E | 866 45 18 36 30 44 --- 20 | 42 34 49 43 46 --- 33
R03E | 1454 39 16 29 45 31 --- 16 | 21 39 50 38 36 --- 32
R04E | 2119 33 22 36 25 57 --- 21 | 27 38 62 54 40 --- 33
R05E | 1879 35 18 27 37 51 --- 18 | 39 20 50 50 52 --- 28
R07E | 873 26 20 38 --- 40 --- 17 | 41 26 39 --- 36 --- 27
R08E | 1144 41 16 28 24 48 71 18 | 34 17 28 26 51 72 17
R10 | 1381 28 14 23 17 20 --- 12 | 25 29 32 21 24 --- 22
R11 | 871 19 14 20 21 19 --- 10 | 26 29 36 38 33 --- 26
R13 | 1052 15 16 15 28 30 --- 11 | 29 25 27 45 33 --- 26
R14 | 1695 17 23 21 12 29 --- 13 | 28 17 31 22 27 --- 20
R15 | 9064 15 8 12 22 29 283 9 | 22 27 36 32 29 180 24
R17 | 1464 43 17 33 32 43 --- 19 | 49 46 57 37 24 --- 40
R18 | 1219 40 13 35 25 22 --- 16 | 38 30 41 37 37 --- 28
R19 | 3696 25 16 31 25 27 --- 14 | 19 30 48 29 20 --- 20
R20 | 1091 27 22 29 26 32 --- 15 | 40 34 55 32 34 --- 34
R21 | 744 30 10 24 15 14 --- 11 | 30 41 64 42 41 --- 41
R22 | 974 29 20 23 38 28 --- 14 | 28 52 54 65 33 --- 42
R23 | 1130 15 11 25 25 20 --- 10 | 30 37 49 44 36 --- 36
R24 | 2419 19 16 21 22 21 --- 11 | 40 33 42 36 55 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 2548 31 17 27 28 35 206 |T 31 31 43 38 36 126 29
WRMS | 2548 31 15 25 28 35 206 |NE 31 33 44 36 32 180 30
MEDI | 1144 28 16 25 25 29 71 |MD 29 30 42 38 36 72 28
Table 3.1588.6 GPS week: 1588 Day: 6 MJD: 55366
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1114 23 17 24 44 60 --- 17 | 19 26 36 30 44 --- 19
R02E | 657 33 21 29 32 51 --- 18 | 65 52 42 45 73 --- 53
R03E | 1258 40 14 40 40 28 --- 17 | 16 28 41 33 37 --- 23
R04E | 1517 24 16 36 38 41 --- 16 | 24 19 35 40 29 --- 18
R05E | 2848 33 22 40 26 40 --- 18 | 35 21 55 38 47 --- 29
R07E | 1338 16 15 27 --- 37 --- 13 | 38 27 41 --- 33 --- 25
R08E | 1393 26 15 40 54 35 51 16 | 27 21 43 36 38 74 19
R10 | 1243 24 13 21 21 23 --- 11 | 23 27 38 32 23 --- 22
R11 | 2047 20 16 25 22 22 --- 11 | 27 29 51 49 43 --- 30
R13 | 704 16 16 32 16 25 --- 12 | 24 31 36 33 24 --- 25
R14 | 1101 17 16 19 22 26 --- 10 | 25 27 31 33 26 --- 21
R15 | 6841 18 8 17 29 33 232 10 | 22 17 28 30 27 45 18
R17 | 1015 14 12 19 42 53 --- 14 | 60 63 58 54 36 --- 54
R18 | 829 20 12 40 30 36 --- 15 | 28 37 53 50 41 --- 34
R19 | 2269 15 11 20 20 40 --- 12 | 27 29 36 41 55 --- 31
R20 | 903 21 10 15 29 39 --- 12 | 35 41 48 51 54 --- 41
R21 | 1234 17 13 15 30 16 --- 9 | 48 65 64 56 60 --- 59
R22 | 613 31 27 26 14 30 --- 16 | 39 58 67 66 56 --- 52
R23 | 966 22 20 24 31 26 --- 13 | 35 46 50 56 41 --- 40
R24 | 2314 33 13 38 28 28 --- 16 | 35 46 70 60 54 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 2092 24 16 29 31 36 168 |T 32 35 46 43 42 59 33
WRMS | 2092 24 14 28 31 36 168 |NE 32 39 48 47 41 45 36
MEDI | 1234 21 15 25 29 33 51 |MD 27 29 42 41 41 45 29
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