[IGSREPORT-18734] Wk 1587 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Fri Jul 2 06:31:06 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1587 (Jun 06, 2010 - Jun 12, 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 2.1587.
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:
igl1587[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1587 in the SP3 format.
igl15877.sum Combination Report for GPS Week 1587.
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 | 400.9 ns
1 | 397.7 ns
2 | 456.2 ns
3 | 403.1 ns
4 | 404.5 ns
5 | 370.6 ns
6 | 372.4 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 1.1587, 1a.1587).
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 2.1587.0-6)
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 3.1587.0-6).
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 1587 summary. (Jun 06, 2010 - Jun 12, 2010)
Table 1.1587.a GPS week : 1587 MJD: 55353.0-55359.0
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| 2 0 -8 0 2 -63 -.16 37 36 | 0 -4 1725 1800
| 2 1 2 31 37 112 .06 | 0 52
cod 246| -2 0 -1 25 -46 23 -.15 19 15 | --- --- --- ---
| 2 1 2 18 24 46 .04 | --- ---
esx 138| 0 0 3 12 78 57 .31 26 24 | 72074 -162 3958 8371
| 1 1 3 44 25 57 .10 | 29303 3222
gfz 202| 0 0 1 -52 18 56 -.32 28 28 | 238528 -834 3957 8095
| 2 2 1 41 63 54 .12 | 28460 2892
iac n/a| 1 0 2 -34 8 -8 -.06 33 33 | 401209 -498 3958 8783
| 1 2 4 30 44 35 .08 | 28648 1548
mcc n/a| 2 -2 35 -85 86 382 .32 291 291 | --- --- --- ---
| 10 10 18 98 142 826 .70 | --- ---
Table 1.1587.b GPS week : 1587 MJD: 55353.0-55359.0
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 | 17 18 23 22 20 19 18 |
R02 | 17 15 18 26 24 24 29 |
R03 | 15 13 17 21 26 26 27 |
R04 | 16 15 14 24 26 24 22 |
R05 | 20 20 17 17 22 31 30 |
R07 | --- --- --- 0 53 35 74 |
R08 | 27 26 23 22 20 21 27 |
R10 | 13 10 11 13 12 12 23 |
R11 | 9 9 13 15 9 12 10 |
R13 | 9 9 10 9 9 8 15 |
R14 | 11 10 12 13 12 12 12 |
R15 | 15 22 17 16 12 11 12 |
R17 | 14 16 19 18 22 16 14 |
R18 | 10 17 9 15 10 10 10 |
R19 | 12 13 7 11 14 12 9 |
R20 | 11 17 16 17 13 11 13 |
R21 | 14 13 8 11 11 8 12 |
R22 | 10 12 13 13 10 15 13 |
R23 | 10 13 12 11 8 13 10 |
R24 | 10 12 8 13 13 11 12 |
Table 1.1587.c GPS week : 1587 MJD: 55353.0-55359.0
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 1587 0 | 81 76 508 -1261 -360 -18250 85.2 1341 1341 | 400922 0
brd 1587 1 | -77 105 302 134 -2396 -18870 86.1 1765 1765 | 397655 0
brd 1587 2 | 114 -88 354 -1927 -947 -15340 85.6 47120 47120 | 456233 0
brd 1587 3 | -11 -20 259 -2684 1032 -15290 87.2 2433 2433 | 403123 0
brd 1587 4 | 109 15 243 1495 420 -19350 86.7 2852 2852 | 404548 0
brd 1587 5 | 58 -62 328 304 -1976 -19270 84.8 2821 2821 | 370641 0
brd 1587 6 | 41 -116 346 -1190 -1956 -15280 83.5 2343 2343 | 372447 0
-------------+------------------------------------------------------------+----------------
brd 1587 mean| 45 -12 334 -732 -883 -17378 85.6 8667 8667 | 400795 0
brd 1587 sdev| 69 83 87 1444 1308 1973 1.2 16964 16964 | 28330 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 2.1587.0 GPS week: 1587 Day: 0 MJD: 55353
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 -10 21 -60 -109 -.09 33 35 | 0 -7 1605 1692
cod 246| -1 -1 -4 18 -14 17 -.10 16 13 | --- --- --- ---
esx 138| 4 2 6 -4 100 21 .24 21 20 | 79004 -2180 3842 9370
gfz 202| 3 3 1 -57 -62 70 -.50 27 27 | 238155 -3193 3842 9335
iac n/a| 0 2 4 -51 -76 21 -.17 32 32 | 401799 -1778 3850 9852
mcc n/a| 6 5 49 -24 -44 354 -.18 146 146 | --- --- --- ---
Table 2.1587.1 GPS week: 1587 Day: 1 MJD: 55354
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 0 -9 2 19 14 -.11 33 34 | 0 69 1721 1782
cod 246| 1 0 -3 10 -35 2 -.14 19 17 | --- --- --- ---
esx 138| 2 1 5 52 83 44 .33 27 26 | 73441 3070 4198 9166
gfz 202| 0 -1 2 -95 103 -34 -.35 27 27 | 231727 3292 4211 8085
iac n/a| 0 0 3 -30 15 -37 -.08 28 28 | 398700 181 4191 8764
mcc n/a| -11 3 57 -216 95 1184 .58 171 171 | --- --- --- ---
Table 2.1587.2 GPS week: 1587 Day: 2 MJD: 55355
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 -9 29 6 -227 -.20 31 32 | 0 -52 1768 1843
cod 246| -2 0 0 9 -57 90 -.22 19 15 | --- --- --- ---
esx 138| 0 0 7 -46 86 165 .50 24 22 | 128455 -3914 4154 8352
gfz 202| 0 -1 0 -7 24 110 -.17 28 28 | 294231 -4070 4145 8245
iac n/a| 1 -1 -3 24 -2 -71 -.08 29 29 | 456705 -2128 4144 8869
mcc n/a| -4 -9 29 23 23 1478 -.04 207 207 | --- --- --- ---
Table 2.1587.3 GPS week: 1587 Day: 3 MJD: 55356
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 -3 15 -29 -120 -.24 36 35 | 0 64 1735 1807
cod 246| -3 -1 -2 60 -54 53 -.16 22 17 | --- --- --- ---
esx 138| 0 1 3 -45 109 58 .22 27 27 | 70146 -3180 3890 8248
gfz 202| 0 0 0 -49 -14 78 -.37 28 28 | 241752 -2057 3892 8341
iac n/a| 1 0 0 -19 23 1 .09 32 32 | 403124 637 3878 8894
mcc n/a| 8 -13 1 -49 211 860 -.08 277 277 | --- --- --- ---
Table 2.1587.4 GPS week: 1587 Day: 4 MJD: 55357
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| 5 1 -8 -19 29 105 -.23 36 34 | 0 -10 1743 1813
cod 246| -4 0 0 14 -60 -59 -.09 17 13 | --- --- --- ---
esx 138| 0 -1 1 53 83 68 .29 28 24 | 71138 -1314 4042 7376
gfz 202| 1 0 3 -111 -26 71 -.25 29 29 | 244454 -2905 4035 7350
iac n/a| 4 0 -1 -58 27 -16 -.00 38 38 | 405786 -1787 4068 8071
mcc n/a| -4 -3 44 -58 -31 -716 1.56 381 381 | --- --- --- ---
Table 2.1587.5 GPS week: 1587 Day: 5 MJD: 55358
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 14 52 -116 -.11 39 35 | 0 -59 1734 1824
cod 246| -2 0 0 27 -84 21 -.14 18 14 | --- --- --- ---
esx 138| 0 2 0 28 49 66 .25 26 23 | 43230 3823 3918 8467
gfz 202| 1 2 2 -47 102 102 -.40 25 25 | 208686 1651 3910 8105
iac n/a| 0 -5 4 -61 70 13 -.04 38 38 | 369023 2080 3894 9128
mcc n/a| 2 -13 39 -40 7 -374 .83 505 505 | --- --- --- ---
Table 2.1587.6 GPS week: 1587 Day: 6 MJD: 55359
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 -12 -62 -2 12 -.14 50 46 | 0 -37 1770 1840
cod 246| -4 1 -2 36 -19 40 -.17 19 15 | --- --- --- ---
esx 138| -1 0 -2 48 40 -23 .35 27 25 | 39106 2558 3665 7621
gfz 202| -3 -1 0 0 5 -3 -.18 29 29 | 210696 1443 3669 7210
iac n/a| 4 1 9 -42 3 25 -.10 34 34 | 373327 -697 3684 7906
mcc n/a| 19 14 27 -232 342 -107 -.40 353 353 | --- --- --- ---
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 3.1587.0 GPS week: 1587 Day: 0 MJD: 55353
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1300 32 19 28 25 43 --- 17 | 26 20 38 32 44 --- 24
R02E | 1235 45 22 22 28 35 --- 17 | 54 40 51 38 44 --- 43
R03E | 1038 34 10 19 38 43 --- 15 | 35 29 48 38 46 --- 31
R04E | 898 37 15 16 34 46 --- 16 | 42 22 38 44 56 --- 31
R05E | 1048 39 24 33 49 45 --- 19 | 43 24 57 61 54 --- 34
R08E | 1006 81 35 25 30 45 145 27 | 39 37 42 36 49 92 33
R10 | 1899 30 15 18 15 28 --- 12 | 29 22 30 25 43 --- 25
R11 | 732 20 8 17 30 16 --- 8 | 31 37 40 47 30 --- 33
R13 | 890 26 8 12 25 17 --- 9 | 26 34 38 34 33 --- 32
R14 | 2185 17 9 19 23 29 --- 10 | 31 29 35 35 42 --- 30
R15 | 2606 41 13 20 19 28 81 14 | 27 40 41 34 37 106 35
R17 | 1472 22 22 9 17 37 --- 13 | 47 68 66 52 42 --- 57
R18 | 1372 22 11 12 32 25 --- 10 | 36 44 53 62 58 --- 45
R19 | 939 14 9 27 22 27 --- 11 | 56 64 85 74 58 --- 66
R20 | 1399 21 15 18 21 25 --- 11 | 32 29 46 42 39 --- 31
R21 | 1100 29 7 26 25 33 --- 13 | 42 62 80 62 54 --- 60
R22 | 1116 22 12 20 21 15 --- 9 | 64 73 73 79 74 --- 70
R23 | 644 20 16 15 21 19 190 10 | 36 41 40 36 44 234 38
R24 | 832 19 10 17 17 21 --- 9 | 53 60 69 56 59 --- 60
------+-----------------------------------------+-------------------------------------
RMS | 1341 33 16 21 27 32 146 |T 39 40 51 46 47 144 40
WRMS | 1341 35 13 20 27 32 146 |NE 36 42 47 43 41 234 40
MEDI | 1100 26 13 19 25 28 145 |MD 36 37 46 42 44 106 34
Table 3.1587.1 GPS week: 1587 Day: 1 MJD: 55354
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2108 36 27 19 41 39 --- 17 | 20 20 25 36 44 --- 17
R02E | 1601 30 17 25 22 32 --- 15 | 59 22 37 26 48 --- 34
R03E | 1026 26 14 19 16 28 --- 12 | 45 21 24 22 43 --- 27
R04E | 2275 28 12 28 29 32 --- 14 | 25 24 27 37 36 --- 20
R05E | 960 31 23 23 35 52 --- 19 | 35 26 22 40 54 --- 22
R08E | 2427 81 39 25 52 25 121 26 | 39 34 33 43 34 62 25
R10 | 1342 14 14 20 20 23 --- 10 | 28 18 21 26 29 --- 17
R11 | 1900 13 16 14 19 18 --- 9 | 26 37 31 33 31 --- 29
R13 | 858 22 10 15 17 13 --- 8 | 34 37 34 33 41 --- 36
R14 | 1750 19 9 14 15 25 --- 9 | 24 20 23 22 35 --- 20
R15 | 1571 51 24 48 21 29 94 21 | 26 45 72 39 33 101 40
R17 | 1889 29 25 24 29 33 --- 16 | 37 53 43 45 36 --- 41
R18 | 1479 41 18 22 13 34 --- 16 | 22 29 47 36 55 --- 31
R19 | 919 20 20 27 25 19 --- 12 | 58 47 62 47 47 --- 48
R20 | 2327 21 17 48 34 23 --- 16 | 24 39 63 41 20 --- 30
R21 | 2512 30 12 31 27 14 --- 12 | 39 50 55 55 43 --- 45
R22 | 2246 27 16 24 27 18 --- 12 | 29 41 58 60 54 --- 44
R23 | 1739 30 11 31 17 20 253 13 | 37 35 34 37 36 97 31
R24 | 1028 23 11 34 25 15 --- 12 | 40 44 71 34 48 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1765 33 19 27 27 28 171 |T 34 33 41 37 40 86 31
WRMS | 1765 34 17 26 27 28 171 |NE 31 37 42 35 35 97 33
MEDI | 1739 28 16 24 25 25 121 |MD 34 35 34 37 41 97 31
Table 3.1587.2 GPS week: 1587 Day: 2 MJD: 55355
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 972 55 34 27 44 41 --- 23 | 37 32 29 36 42 --- 25
R02E | 2180 46 18 26 38 34 --- 18 | 58 35 41 38 52 --- 39
R03E | 658 43 21 21 25 34 --- 17 | 37 47 54 51 62 --- 44
R04E | 1614 29 17 22 23 31 --- 14 | 30 14 40 41 42 --- 23
R05E | 869 33 17 26 35 40 --- 16 | 42 42 42 56 50 --- 37
R08E | 3144 58 33 34 36 33 122 23 | 41 29 38 37 46 100 26
R10 | 2574 12 15 20 24 24 --- 10 | 22 25 40 40 31 --- 25
R11 | 4509 15 17 16 24 34 --- 12 | 36 38 48 50 31 --- 36
R13 | 1729 18 13 19 23 22 --- 10 | 28 42 45 45 33 --- 35
R14 | 858 21 19 17 17 24 --- 11 | 24 40 39 28 32 --- 30
R15 | 2811 36 17 26 18 35 151 16 | 25 41 40 30 34 65 30
R17 | 1089 29 10 48 25 33 --- 18 | 41 72 110 71 48 --- 68
R18 | 1334 16 10 15 11 20 --- 9 | 49 39 51 44 49 --- 43
R19 | 957 10 10 10 10 18 --- 7 | 37 35 38 32 32 --- 32
R20 | 1762 22 25 28 51 32 --- 15 | 20 22 51 66 40 --- 29
R21 |>>>>> 13 10 13 16 17 --- 7 | 42 54 55 48 51 --- 49
R22 | 2997 22 25 20 20 18 --- 12 | 50 70 57 55 43 --- 55
R23 | 2815 30 12 25 15 18 301 12 | 26 32 61 40 43 211 39
R24 | 1604 16 8 14 35 16 --- 7 | 38 39 54 32 47 --- 43
------+-----------------------------------------+-------------------------------------
RMS |47119 31 19 24 28 29 207 |T 35 39 49 44 42 125 37
WRMS |47119 32 15 22 28 29 207 |NE 30 40 58 47 39 211 40
MEDI | 1729 22 17 21 24 31 151 |MD 37 39 45 41 43 100 36
Table 3.1587.3 GPS week: 1587 Day: 3 MJD: 55356
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1418 46 36 28 32 43 --- 22 | 28 29 41 34 42 --- 24
R02E | 1227 64 39 34 58 43 --- 26 | 58 42 51 49 57 --- 45
R03E | 1011 49 27 26 31 40 --- 20 | 46 44 68 53 59 --- 48
R04E | 3499 61 19 43 26 38 --- 23 | 22 30 45 34 58 --- 28
R05E | 910 41 19 25 17 35 --- 17 | 41 34 61 45 60 --- 40
XR07E | ---- --- 6 --- --- --- --- 0 | --- 37 --- --- --- --- 32
R08E | 3062 60 28 20 27 42 159 22 | 50 39 38 46 57 194 38
R10 | 3633 17 10 28 29 33 --- 13 | 25 19 36 25 41 --- 21
R11 | 5131 25 17 29 22 31 --- 14 | 37 42 44 47 39 --- 36
R13 | 1495 15 14 16 18 17 --- 9 | 38 43 50 40 34 --- 39
R14 | 961 21 19 28 20 19 --- 13 | 28 34 45 37 31 --- 29
R15 | 1889 25 20 26 32 39 286 16 | 39 50 45 39 44 210 42
R17 | 848 46 20 29 39 28 --- 17 | 70 60 52 37 36 --- 50
R18 | 1632 20 16 31 35 32 --- 14 | 49 54 77 51 50 --- 54
R19 | 1220 19 12 16 20 25 --- 10 | 55 41 46 51 31 --- 40
R20 | 1978 20 23 35 18 33 --- 16 | 33 36 33 38 51 --- 31
R21 | 3038 25 15 17 23 17 --- 10 | 37 46 47 47 39 --- 39
R22 | 2950 21 24 20 22 24 --- 13 | 49 79 54 56 59 --- 60
R23 | 2654 14 17 19 19 22 350 10 | 44 36 46 44 53 407 40
R24 | 2337 26 17 23 15 25 --- 13 | 45 37 71 50 68 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 2433 36 22 27 28 32 277 |T 41 41 50 43 47 270 39
WRMS | 2433 35 17 27 28 32 277 |NE 42 41 48 41 44 407 39
MEDI | 1889 25 19 26 23 32 286 |MD 41 39 46 45 50 210 39
Table 3.1587.4 GPS week: 1587 Day: 4 MJD: 55357
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1038 32 24 32 30 56 --- 20 | 53 32 42 45 50 --- 34
R02E | 849 57 28 37 36 53 --- 24 | 50 35 63 58 59 --- 37
R03E | 1085 52 23 40 43 69 --- 25 | 40 47 48 37 70 --- 43
R04E | 6850 69 29 30 36 55 --- 26 | 39 20 37 31 51 --- 21
R05E | 1693 42 20 28 28 65 --- 22 | 62 59 80 66 55 --- 58
XR07E | ---- --- 36 --- --- 77 --- 52 | --- 33 --- --- 26 --- 22
R08E | 3725 55 17 22 27 45 407 20 | 40 27 41 40 57 161 33
R10 | 2707 26 13 22 17 25 --- 12 | 26 36 41 31 33 --- 27
R11 | 4830 19 13 13 15 20 --- 9 | 32 28 38 27 29 --- 28
R13 | 2015 17 9 19 23 17 --- 8 | 26 27 43 41 32 --- 28
R14 | 1074 16 16 21 26 29 --- 11 | 27 26 31 30 41 --- 24
R15 | 1336 20 10 24 29 31 143 12 | 26 28 49 41 39 105 31
R17 | 1116 53 13 49 53 42 --- 22 | 54 64 97 87 49 --- 64
R18 | 1358 17 16 12 17 20 --- 9 | 41 47 34 44 47 --- 41
R19 | 2304 17 10 34 13 31 --- 13 | 35 52 76 56 43 --- 50
R20 | 4629 27 15 22 22 27 --- 12 | 39 30 25 35 35 --- 23
R21 | 2015 24 12 24 18 20 --- 11 | 39 49 51 53 35 --- 42
R22 | 2304 23 13 15 31 16 --- 9 | 36 55 54 67 42 --- 47
R23 | 2551 9 9 19 30 18 499 8 | 27 30 41 40 28 239 29
R24 | 2109 28 13 32 31 16 --- 13 | 24 44 52 41 32 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 2851 36 17 28 29 38 381 |T 37 38 49 45 42 168 35
WRMS | 2851 34 13 24 29 38 381 |NE 32 35 46 43 35 239 33
MEDI | 2015 26 13 24 28 29 407 |MD 39 33 43 41 41 161 33
Table 3.1587.5 GPS week: 1587 Day: 5 MJD: 55358
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1282 34 19 17 26 58 --- 18 | 47 44 26 31 44 --- 31
R02E | 1362 66 26 26 37 50 --- 23 | 65 52 56 56 68 --- 51
R03E | 2079 53 22 44 21 66 --- 26 | 30 48 68 42 63 --- 46
R04E | 6084 60 31 31 44 51 --- 24 | 35 38 35 34 45 --- 26
R05E | 3575 79 29 50 31 63 --- 31 | 50 66 87 59 76 --- 61
XR07E | ---- --- 25 --- --- 50 --- 35 | --- 41 --- --- 51 --- 41
R08E | 1082 59 24 26 27 41 522 21 | 55 42 47 47 64 76 44
R10 | 1795 16 19 23 21 21 --- 11 | 22 38 27 30 28 --- 26
R11 | 3537 24 14 26 25 21 --- 12 | 42 36 41 34 37 --- 34
R13 | 2671 12 8 17 22 19 --- 8 | 25 39 41 34 32 --- 33
R14 | 1929 15 9 22 19 34 --- 11 | 20 30 35 35 38 --- 26
R15 | 4279 21 11 17 24 30 128 11 | 39 40 46 33 48 97 39
R17 | 1396 37 18 21 29 37 --- 15 | 57 54 61 47 33 --- 50
R18 | 1522 27 12 11 14 17 --- 9 | 21 40 34 28 41 --- 34
R19 | 3158 21 18 25 18 18 --- 12 | 18 39 37 34 36 --- 29
R20 | 4274 21 17 20 17 20 --- 11 | 13 31 28 27 17 --- 18
R21 | 2959 18 9 14 18 18 --- 8 | 36 36 30 30 38 --- 31
R22 | 1053 42 7 25 17 29 --- 14 | 40 40 46 44 55 --- 40
R23 | 1666 25 14 28 27 28 691 13 | 19 31 46 45 25 242 26
R24 | 1538 11 18 18 20 26 --- 11 | 29 38 29 45 35 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2821 39 18 26 25 38 505 |T 34 41 43 38 43 138 35
WRMS | 2821 35 14 23 25 38 505 |NE 29 37 40 38 31 242 31
MEDI | 1929 25 18 23 22 29 522 |MD 35 39 41 34 38 97 33
Table 3.1587.6 GPS week: 1587 Day: 6 MJD: 55359
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1083 29 15 28 27 48 --- 17 | 28 31 45 42 42 --- 30
R02E | 1282 92 27 34 25 54 --- 28 | 117 38 53 49 68 --- 53
R03E | 615 80 29 24 32 59 --- 27 | 44 46 47 42 61 --- 44
R04E | 3326 64 25 28 38 43 --- 22 | 37 30 39 43 45 --- 27
R05E | 2099 90 34 36 32 54 --- 29 | 54 50 69 57 58 --- 49
XR07E | ---- --- 57 --- --- 94 --- 73 | --- 36 --- --- 39 --- 30
R08E | 1178 99 19 36 31 29 490 26 | 40 41 47 49 53 55 42
R10M | 1854 56 28 35 24 45 --- 22 | 65 49 54 46 67 --- 45
R11 | 2171 17 12 22 32 18 --- 9 | 33 30 43 39 29 --- 30
R13 | 2222 38 14 34 37 22 --- 15 | 22 34 39 43 32 --- 28
R14 | 2750 18 17 19 19 25 --- 11 | 27 26 32 27 39 --- 25
R15M | 5064 30 9 19 21 28 93 12 | 34 46 52 49 53 87 45
R17 | 1401 37 12 15 25 32 --- 13 | 62 60 65 58 49 --- 57
R18M | 1583 24 15 14 21 15 --- 9 | 61 76 73 74 77 --- 72
R19M | 2935 16 9 18 20 18 --- 8 | 47 57 63 57 55 --- 55
R20 | 4027 31 12 16 34 31 --- 12 | 24 27 36 48 45 --- 30
R21M | 2207 19 16 27 19 15 --- 11 | 51 50 69 57 66 --- 56
R22M | 1227 19 16 36 45 13 --- 13 | 48 57 83 89 65 --- 62
R23 | 495 13 15 26 29 12 --- 10 | 29 33 41 42 25 --- 29
R24 | 1403 16 21 23 29 18 --- 11 | 34 48 49 38 39 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 2342 50 19 27 29 34 352 |T 45 43 52 49 50 71 42
WRMS | 2342 46 15 25 29 34 352 |NE 33 36 43 42 36 --- 34
MEDI | 1854 30 16 26 29 28 93 |MD 40 41 49 48 49 55 42
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