[IGSREPORT-18836] Wk 1593 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 5 05:38:41 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1593 (Jul 18, 2010 - Jul 24, 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 2.1593.
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:
igl1593[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1593 in the SP3 format.
igl15937.sum Combination Report for GPS Week 1593.
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 | 423.1 ns
1 | 379.3 ns
2 | 442.1 ns
3 | 394.5 ns
4 | 387.6 ns
5 | 472.9 ns
6 | 474.2 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 1.1593, 1a.1593).
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 2.1593.0-6)
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 3.1593.0-6).
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 1593 summary. (Jul 18, 2010 - Jul 24, 2010)
Table 1.1593.a GPS week : 1593 MJD: 55395.0-55401.0
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 120| 2 0 -5 -15 0 20 -.12 22 22 | 0 -71 2058 2210
| 1 1 2 10 20 126 .03 | 0 374
cod 237| -2 0 -3 51 -17 1 -.10 13 12 | --- --- --- ---
| 1 1 2 9 24 54 .02 | --- ---
esx 143| 0 -1 0 -56 29 24 .40 25 23 | 81798 1079 4129 7989
| 1 2 3 31 53 50 .02 | 46111 2773
gfz 192| 0 0 -4 -76 -6 77 -.14 25 24 | 261363 735 4127 7841
| 2 1 2 49 50 54 .09 | 39890 1895
iac n/a| 3 0 11 -46 16 -51 -.06 24 24 | 425206 -391 4121 8350
| 1 1 10 12 13 49 .01 | 40175 1725
mcc n/a| -1 -1 72 -45 -32 -448 -.13 100 100 | --- --- --- ---
| 3 5 11 66 65 378 .41 | --- ---
Table 1.1593.b GPS week : 1593 MJD: 55395.0-55401.0
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 | 12 10 11 12 11 9 12 |
R02 | 9 11 12 10 11 10 10 |
R03 | 13 7 11 11 10 9 11 |
R04 | 12 11 9 14 12 10 11 |
R05 | 10 9 13 11 14 11 11 |
R07 | 13 9 11 10 15 10 11 |
R08 | 13 10 9 10 10 9 8 |
R10 | 11 11 10 12 13 11 9 |
R11 | 10 10 12 19 13 15 16 |
R13 | 9 8 8 7 15 10 11 |
R14 | 12 14 13 11 10 12 14 |
R15 | 18 17 12 17 15 13 14 |
R17 | 15 15 17 19 17 10 11 |
R18 | 12 11 10 9 7 9 7 |
R19 | 11 9 8 29 10 8 8 |
R20 | 12 15 12 13 11 11 14 |
R21 | 11 9 11 9 8 21 9 |
R22 | 13 11 8 10 10 11 21 |
R23 | 11 11 11 9 10 9 10 |
R24 | 9 11 8 10 11 13 8 |
Table 1.1593.c GPS week : 1593 MJD: 55395.0-55401.0
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 1593 0 | 25 129 791 -489 3077 -36110 87.1 3114 3114 | 423141 0
brd 1593 1 | -170 -87 556 4756 -2493 -21920 87.1 2504 2504 | 379308 0
brd 1593 2 | 30 -115 617 656 -2052 -17580 82.5 2261 2261 | 442080 0
brd 1593 3 | 139 11 517 -2574 -864 -9221 84.4 1920 1920 | 394460 0
brd 1593 4 | 12 -9 511 1060 3423 -14130 86.7 2185 2185 | 387576 0
brd 1593 5 | 17 -116 711 1285 -185 -15700 85.2 2396 2396 | 472863 0
brd 1593 6 | -140 -47 540 415 -2789 -25110 83.6 3554 3554 | 474212 0
-------------+------------------------------------------------------------+----------------
brd 1593 mean| -12 -33 606 729 -269 -19967 85.2 2562 2562 | 424805 0
brd 1593 sdev| 107 87 107 2203 2571 8796 1.8 572 572 | 39641 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 2.1593.0 GPS week: 1593 Day: 0 MJD: 55395
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 120| 2 1 -5 -4 43 21 -.09 18 18 | 0 193 1657 1799
cod 237| -4 0 -6 56 -26 39 -.10 15 15 | --- --- --- ---
esx 143| 0 0 -6 -109 18 28 .41 27 26 | 88462 -16 4065 9335
gfz 192| 1 -2 -5 -18 72 82 -.10 28 29 | 260590 -321 4055 9291
iac n/a| 4 0 26 -23 18 -89 -.05 24 24 | 423027 109 4039 9694
mcc n/a| -1 4 55 28 -34 -536 -.40 111 111 | --- --- --- ---
Table 2.1593.1 GPS week: 1593 Day: 1 MJD: 55396
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 120| 3 0 -8 -29 -6 -43 -.10 23 23 | 0 51 2164 2249
cod 237| -3 1 -5 44 -19 14 -.11 12 12 | --- --- --- ---
esx 143| 0 0 -4 -9 40 71 .38 22 21 | 26468 4279 4605 9393
gfz 192| -2 -1 -6 -37 -39 85 -.30 26 21 | 214420 2738 4571 9374
iac n/a| 4 -2 20 -56 8 -58 -.05 21 21 | 378173 2588 4621 9740
mcc n/a| 2 -4 72 -16 -22 -153 -.31 132 132 | --- --- --- ---
Table 2.1593.2 GPS week: 1593 Day: 2 MJD: 55397
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 120| 1 1 -1 -24 -18 36 -.14 21 21 | 0 -852 3692 4227
cod 237| -2 0 -2 66 3 -46 -.13 12 11 | --- --- --- ---
esx 143| -1 -3 1 -66 2 74 .43 19 18 | 102128 -1475 4449 7274
gfz 192| -3 0 1 -54 -45 56 -.17 23 22 | 280196 -1324 4469 7114
iac n/a| 2 0 5 -52 28 -48 -.05 23 23 | 443351 -1303 4447 7537
mcc n/a| -3 2 91 -28 12 -968 -.33 92 92 | --- --- --- ---
Table 2.1593.3 GPS week: 1593 Day: 3 MJD: 55398
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 120| -1 -1 -3 -22 -3 120 -.17 22 22 | 0 -214 1781 1873
cod 237| -2 0 0 47 -65 -71 -.10 16 13 | --- --- --- ---
esx 143| 1 1 1 -32 81 25 .39 28 21 | 40360 -927 4120 7041
gfz 192| 0 1 -2 -92 12 122 -.17 26 26 | 230232 1894 4135 6851
iac n/a| 4 0 1 -45 36 -22 -.06 27 27 | 394832 -131 4113 7272
mcc n/a| 3 -9 78 -70 -168 -850 -.28 75 75 | --- --- --- ---
Table 2.1593.4 GPS week: 1593 Day: 4 MJD: 55399
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 120| 2 0 -3 -1 -10 176 -.09 21 21 | 0 29 1657 1745
cod 237| -2 -1 0 45 -21 -42 -.09 13 12 | --- --- --- ---
esx 143| 1 0 1 -51 16 -68 .38 24 25 | 42438 2218 4341 8271
gfz 192| 0 0 -3 -51 -5 0 -.15 25 25 | 224717 787 4332 7903
iac n/a| 2 0 0 -35 9 -77 -.04 26 26 | 388231 -1076 4322 8714
mcc n/a| -1 -6 77 -32 39 -510 .12 77 77 | --- --- --- ---
Table 2.1593.5 GPS week: 1593 Day: 5 MJD: 55400
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 120| 1 0 -4 -14 -7 -218 -.11 20 20 | 0 254 1792 1849
cod 237| -3 1 -2 40 -1 69 -.06 11 11 | --- --- --- ---
esx 143| 1 -6 -1 -52 103 52 .41 31 28 | 139263 5056 3779 7686
gfz 192| 0 0 -5 -118 -73 162 -.02 26 23 | 308232 3013 3785 7303
iac n/a| 1 1 7 -50 -4 42 -.07 22 22 | 472763 126 3771 7877
mcc n/a| -4 0 69 -17 -14 -183 .69 91 91 | --- --- --- ---
Table 2.1593.6 GPS week: 1593 Day: 6 MJD: 55401
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 120| 4 -2 -8 -11 3 50 -.13 26 25 | 0 41 1665 1729
cod 237| -1 1 -5 59 7 47 -.11 11 11 | --- --- --- ---
esx 143| -2 -3 0 -73 -58 -10 .40 26 23 | 133468 -1577 3544 6925
gfz 192| 3 0 -7 -159 34 30 -.09 24 24 | 311159 -1642 3542 7051
iac n/a| 4 2 16 -59 19 -104 -.06 22 22 | 476069 -3055 3537 7619
mcc n/a| -7 2 65 -179 -41 62 -.40 126 126 | --- --- --- ---
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 3.1593.0 GPS week: 1593 Day: 0 MJD: 55395
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 5151 14 19 24 38 28 --- 12 | 15 30 28 35 33 --- 21
R02 | 4557 14 13 22 20 11 --- 8 | 16 22 37 33 32 --- 22
R03 | 987 19 11 41 16 19 --- 13 | 22 30 58 31 25 --- 27
R04 | 3787 25 15 23 33 21 --- 12 | 24 25 46 36 19 --- 21
R05 | 1696 18 16 20 21 15 --- 10 | 17 16 30 20 18 --- 15
R07 | 2570 14 11 38 23 26 --- 13 | 22 22 51 30 18 --- 22
R08 | 2765 13 14 33 44 27 152 12 | 21 23 43 32 20 49 20
R10 | 1995 16 10 29 21 18 --- 10 | 21 20 34 29 21 --- 18
R11 | 2859 13 12 25 19 18 --- 9 | 38 33 47 39 40 --- 33
R13 | 3579 12 17 18 24 18 --- 9 | 12 25 27 33 14 --- 16
R14 | 4038 21 13 29 31 22 --- 12 | 23 29 50 48 34 --- 30
R15 | 4749 19 17 27 37 54 49 17 | 18 28 29 29 25 29 19
R17 | 2248 34 16 20 30 31 --- 15 | 35 53 52 58 61 --- 47
R18 | 1629 13 15 37 34 20 --- 12 | 20 31 45 36 37 --- 27
R19 | 1476 11 16 23 29 23 --- 10 | 30 37 32 37 42 --- 31
R20 | 3268 22 14 30 17 18 --- 12 | 26 35 45 40 37 --- 32
R21 | 2178 17 14 25 21 17 --- 10 | 30 33 34 33 35 --- 30
R22 | 3105 25 16 27 22 24 --- 13 | 33 34 28 20 32 --- 28
R23 | 2786 16 20 22 29 14 107 10 | 20 42 36 35 32 51 30
R24 | 2747 16 12 17 22 17 --- 9 | 22 30 38 27 29 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 3113 18 15 27 28 24 111 |T 23 29 39 34 30 43 25
WRMS | 3113 18 15 26 29 24 111 |NE 23 29 39 34 30 43 25
MEDI | 2765 16 14 25 23 19 107 |MD 22 30 37 33 32 49 26
Table 3.1593.1 GPS week: 1593 Day: 1 MJD: 55396
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2997 16 13 10 16 25 --- 9 | 16 24 28 30 25 --- 20
R02 | 1441 22 16 16 37 20 --- 10 | 17 40 32 37 32 --- 28
R03 | 1468 13 7 14 19 12 --- 6 | 34 27 19 24 23 --- 23
R04 | 2620 20 14 23 30 20 --- 11 | 29 22 30 32 19 --- 17
R05 | 1257 19 12 16 25 15 --- 9 | 16 25 24 31 18 --- 17
R07 | 4545 18 7 18 36 18 --- 8 | 19 25 34 39 21 --- 22
R08 | 2374 22 8 20 23 18 180 9 | 26 18 20 23 13 70 15
R10 | 2678 15 10 23 20 23 --- 10 | 15 17 33 25 17 --- 15
R11 | 2147 18 11 27 19 16 --- 10 | 34 34 53 50 40 --- 37
R13 | 4659 14 10 17 16 15 --- 8 | 14 20 29 21 13 --- 15
R14 | 4116 35 13 30 33 22 --- 14 | 15 28 43 35 38 --- 27
R15 | 2633 37 14 31 24 36 36 16 | 15 18 47 36 22 42 21
R17 | 1291 40 15 19 27 30 --- 14 | 21 40 37 40 30 --- 31
R18 | 1550 28 11 21 21 20 --- 11 | 13 30 45 33 31 --- 25
R19 | 1356 17 10 20 27 18 --- 9 | 20 20 34 29 27 --- 20
R20 | 2833 30 18 27 24 28 --- 14 | 15 26 36 29 29 --- 22
R21 | 964 14 9 22 31 19 --- 9 | 27 28 39 48 38 --- 29
R22 | 1416 24 13 26 26 17 --- 11 | 29 27 36 32 33 --- 25
R23 | 1361 22 16 20 18 16 137 10 | 18 30 28 28 27 91 22
R24 | 1140 21 14 22 29 22 --- 11 | 13 20 24 24 23 --- 15
------+-----------------------------------------+-------------------------------------
RMS | 2503 23 12 22 26 21 132 |T 20 25 33 32 25 67 22
WRMS | 2503 23 12 21 21 21 132 |NE 20 25 33 32 25 67 22
MEDI | 1550 20 12 20 24 19 137 |MD 17 25 33 31 25 70 22
Table 3.1593.2 GPS week: 1593 Day: 2 MJD: 55397
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1266 19 13 16 26 27 --- 10 | 13 24 29 27 18 --- 15
R02 | 1156 19 17 16 15 29 --- 11 | 19 22 31 27 33 --- 18
R03 | 1542 21 14 23 20 19 --- 11 | 22 26 32 25 22 --- 18
R04 | 2288 22 14 10 17 16 --- 9 | 19 23 22 22 15 --- 14
R05 | 1317 30 15 22 27 21 --- 12 | 19 21 34 36 25 --- 17
R07 | 4713 25 7 18 25 23 --- 10 | 24 20 27 29 27 --- 18
R08 | 3032 18 10 13 21 18 83 8 | 16 12 23 21 18 72 12
R10 | 2838 14 12 17 22 27 --- 10 | 9 11 28 22 34 --- 12
R11 | 1814 24 11 26 20 22 --- 11 | 63 68 72 62 55 --- 64
R13 | 3970 11 8 19 14 19 --- 8 | 14 15 32 24 14 --- 13
R14 | 2864 27 14 20 21 27 --- 12 | 19 34 36 41 17 --- 23
R15 | 2702 25 13 16 14 28 81 11 | 26 29 22 14 19 47 16
R17 | 1016 37 18 24 33 42 --- 17 | 33 48 53 54 32 --- 40
R18 | 1520 20 12 18 23 16 --- 9 | 20 22 25 40 25 --- 18
R19 | 763 14 10 13 21 17 --- 7 | 26 27 47 52 36 --- 30
R20 | 1755 22 9 27 28 23 --- 11 | 15 20 41 40 28 --- 21
R21 | 1774 15 14 21 20 22 --- 10 | 16 22 25 23 24 --- 15
R22 | 1959 16 7 16 30 17 --- 8 | 15 20 29 35 21 --- 17
R23 | 500 15 9 27 30 20 109 10 | 26 23 35 27 32 72 24
R24 | 1275 13 11 14 23 16 --- 7 | 19 21 24 26 29 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 2260 21 12 19 23 23 92 |T 21 25 33 32 26 63 21
WRMS | 2260 21 11 18 22 23 92 |NE 21 25 33 32 26 63 21
MEDI | 1755 19 12 18 21 21 83 |MD 19 22 29 27 25 72 18
Table 3.1593.3 GPS week: 1593 Day: 3 MJD: 55398
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1301 21 12 24 32 25 --- 11 | 21 18 40 37 20 --- 16
R02 | 1512 19 9 17 15 22 --- 9 | 16 19 26 17 23 --- 15
R03 | 1455 19 17 21 25 20 --- 11 | 28 31 40 43 28 --- 26
R04 | 1684 29 19 17 25 28 --- 13 | 33 32 18 31 22 --- 15
R05 | 1889 24 15 14 27 20 --- 10 | 18 24 20 31 23 --- 15
R07 | 3882 19 8 24 28 17 --- 10 | 24 18 28 25 19 --- 18
R08 | 2387 18 11 15 21 21 60 9 | 30 18 24 31 20 30 17
R10 | 3136 16 15 23 17 27 --- 11 | 24 14 33 21 26 --- 18
R11 | 1527 35 29 26 34 37 --- 18 | 42 56 49 51 44 --- 41
R13 | 1517 15 7 16 17 13 --- 7 | 23 18 20 21 10 --- 11
R14 | 1626 15 11 15 17 30 --- 10 | 19 24 28 28 26 --- 19
R15 | 1781 27 22 26 23 42 79 16 | 20 25 35 28 19 34 16
R17 | 1038 26 21 25 40 54 --- 18 | 30 41 54 59 53 --- 39
R18 | 2514 16 13 18 26 15 --- 9 | 26 28 27 30 24 --- 21
R19 | 1000 37 21 89 21 31 --- 28 | 32 30 109 32 32 --- 41
R20 | 1236 20 19 20 25 30 --- 12 | 17 26 36 32 26 --- 21
R21 | 721 13 10 18 31 20 --- 8 | 14 23 27 29 17 --- 15
R22 | 2775 22 13 17 24 15 --- 10 | 23 20 26 25 21 --- 14
R23 | 1134 17 9 20 27 18 83 9 | 22 26 37 25 19 43 22
R24 | 839 13 12 28 18 15 --- 10 | 20 27 36 21 35 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1919 22 16 28 26 27 75 |T 24 25 35 30 25 35 21
WRMS | 1919 22 13 21 26 27 75 |NE 24 25 35 30 25 35 21
MEDI | 1517 19 13 20 25 21 79 |MD 23 24 28 29 23 34 18
Table 3.1593.4 GPS week: 1593 Day: 4 MJD: 55399
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2622 20 11 22 14 22 --- 10 | 24 22 25 21 23 --- 16
R02 | 2244 19 15 19 13 24 --- 11 | 12 27 42 31 21 --- 21
R03 | 2673 15 9 18 20 26 --- 9 | 14 22 39 27 22 --- 21
R04 | 1739 24 13 20 23 29 --- 12 | 15 27 41 36 24 --- 21
R05 | 2682 25 10 27 22 35 --- 13 | 21 19 37 29 28 --- 14
R07 | 3007 29 12 37 33 21 --- 14 | 21 34 54 31 31 --- 29
R08 | 1399 23 12 17 33 21 84 10 | 29 17 27 17 25 28 18
R10 | 5629 15 12 36 26 25 --- 13 | 15 20 40 34 15 --- 15
R11 | 1632 15 19 23 32 35 --- 13 | 72 69 74 69 65 --- 68
R13 | 1479 34 10 29 38 28 --- 14 | 11 23 40 35 18 --- 16
R14 | 2076 19 9 17 24 26 --- 10 | 18 25 33 29 27 --- 23
R15 | 1700 32 11 24 18 36 78 14 | 37 29 34 29 36 19 27
R17 | 1305 27 23 32 33 39 --- 17 | 24 40 44 38 38 --- 32
R18 | 1473 12 8 17 20 14 --- 7 | 21 22 21 31 20 --- 17
R19 | 952 15 13 23 23 19 --- 10 | 19 34 31 30 23 --- 22
R20 | 1136 15 13 24 22 26 --- 11 | 14 23 45 36 35 --- 22
R21 | 1082 14 13 12 27 17 --- 8 | 15 24 20 26 21 --- 16
R22 | 1164 17 12 17 23 24 --- 9 | 18 31 21 26 15 --- 19
R23 | 906 15 11 27 15 18 68 10 | 14 26 34 26 23 30 19
R24 | 1421 21 12 22 24 22 --- 10 | 20 26 46 23 35 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 2184 21 13 24 25 26 77 |T 21 28 37 31 27 25 23
WRMS | 2184 21 12 25 25 26 77 |NE 21 28 37 31 27 25 23
MEDI | 1479 19 12 22 23 24 78 |MD 18 25 37 29 23 28 21
Table 3.1593.5 GPS week: 1593 Day: 5 MJD: 55400
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2351 19 9 23 19 17 --- 9 | 18 26 35 27 26 --- 22
R02 | 2668 14 13 26 34 16 --- 9 | 22 30 27 38 18 --- 20
R03 | 2614 13 9 18 19 24 --- 9 | 27 19 34 31 25 --- 20
R04 | 1782 10 9 28 14 26 --- 10 | 32 14 41 21 16 --- 16
R05 | 1854 25 10 17 20 27 --- 11 | 24 21 32 22 36 --- 17
R07 | 1601 15 11 22 28 22 --- 9 | 39 31 21 25 30 --- 28
R08 | 566 19 9 24 30 14 112 9 | 40 20 35 35 23 19 21
R10 | 6511 24 16 24 22 16 --- 11 | 34 14 31 19 17 --- 16
R11 | 1791 26 17 36 29 34 --- 15 | 79 67 74 68 44 --- 63
R13 | 1405 19 10 26 29 12 --- 9 | 22 18 33 32 22 --- 17
R14 | 4515 27 10 28 27 25 --- 12 | 19 37 47 38 32 --- 28
R15 | 1831 30 8 36 25 23 90 13 | 30 27 32 34 16 25 21
R17 | 2239 17 9 23 23 21 --- 9 | 36 35 45 42 27 --- 33
R18 | 1188 14 7 27 29 15 --- 8 | 38 25 30 26 23 --- 25
R19 | 839 9 9 21 25 18 --- 8 | 25 22 39 25 23 --- 22
R20 | 885 15 11 29 24 25 --- 11 | 23 17 39 25 29 --- 18
R21 | 1080 34 16 78 32 18 --- 21 | 17 20 80 27 24 --- 20
R22 | 1240 16 10 34 27 18 --- 10 | 33 22 38 37 19 --- 18
R23 | 1508 14 8 15 21 24 65 8 | 25 19 26 29 27 30 19
R24 | 1246 16 14 35 23 28 --- 13 | 29 29 27 24 28 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2395 20 11 31 26 22 91 |T 30 25 38 31 25 24 23
WRMS | 2395 20 11 28 23 22 91 |NE 30 25 38 31 25 24 23
MEDI | 1601 16 10 26 25 21 90 |MD 27 22 34 27 24 25 20
Table 3.1593.6 GPS week: 1593 Day: 6 MJD: 55401
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2799 31 7 22 27 23 --- 11 | 29 18 32 29 24 --- 16
R02 | 4031 24 12 17 23 21 --- 10 | 19 19 31 33 23 --- 16
R03 | 4070 29 9 23 36 17 --- 10 | 29 21 26 31 17 --- 17
R04 | 2695 22 12 25 14 23 --- 11 | 30 23 28 20 25 --- 22
R05 | 5664 19 9 23 20 25 --- 10 | 25 18 27 23 27 --- 19
R07 | 1120 17 13 25 28 20 --- 10 | 30 28 34 30 24 --- 25
R08 | 635 19 7 12 20 16 154 7 | 35 26 34 25 25 28 26
R10 | 7165 17 9 20 13 14 --- 8 | 24 18 24 23 19 --- 15
R11 | 3548 37 14 34 35 33 --- 16 | 71 68 47 59 54 --- 57
R13 | 3189 20 13 24 15 18 --- 10 | 20 23 17 23 16 --- 13
R14 | 3756 39 16 17 22 22 --- 13 | 34 35 41 31 41 --- 33
R15 | 3099 35 10 27 13 25 122 13 | 31 34 42 39 31 37 32
R17 | 5237 15 9 27 37 27 --- 11 | 39 42 61 47 43 --- 43
R18 | 1249 15 7 8 16 16 --- 6 | 33 29 39 38 23 --- 28
R19 | 655 15 8 18 22 18 --- 8 | 33 28 29 22 28 --- 27
R20 | 1094 40 12 28 21 23 --- 14 | 18 32 41 29 28 --- 24
R21 | 1183 18 10 17 19 21 --- 9 | 23 24 48 30 33 --- 26
R22 | 3929 34 17 66 19 26 --- 20 | 25 30 29 38 29 --- 20
R23 | 4329 16 15 13 31 24 94 10 | 24 23 31 41 34 33 22
R24 | 2625 19 10 17 25 13 --- 8 | 20 29 32 35 27 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 3553 26 11 26 24 22 126 |T 29 28 34 32 28 32 25
WRMS | 3553 25 11 23 24 22 126 |NE 29 28 34 32 28 32 25
MEDI | 3099 19 10 22 21 21 122 |MD 29 26 32 30 27 33 24
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