[IGSREPORT-19774] Wk 1634 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Fri May 20 00:08:15 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1634 (May 01, 2011 - May 07, 2011)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.1634.
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:
igl1634[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1634 in the SP3 format.
igl16347.sum Combination Report for GPS Week 1634.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics initially.
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 409.5 ns
1 | 364.8 ns
2 | 378.6 ns
3 | 415.3 ns
4 | 389.6 ns
5 | 404.1 ns
6 | 365.4 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
3 | IAC | ALL (high Transformation - See Table 2)
4 | IAC | R04
5 | IAC | R04
6 | BKG | R04
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.1634, 1a.1634).
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 2.1634.0-6)
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 3.1634.0-6).
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 1634 summary. (May 01, 2011 - May 07, 2011)
Table 1.1634.a GPS week : 1634 MJD: 55682.0-55688.0
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 153| 2 -1 0 57 24 -40 -.08 48 44 | 0 574 2703 2909
| 1 2 6 37 71 92 .08 | 0 757
cod 247| -1 1 -4 12 -19 5 -.16 26 23 | --- --- --- ---
| 1 2 1 19 26 34 .07 | --- ---
esx 143| 0 0 0 15 48 -12 .40 16 16 | 19064 -2489 4793 9969
| 1 1 2 30 38 18 .03 | 23298 3128
gfz 193| 0 -2 2 -57 -49 48 -.32 20 18 | 224889 -2503 4801 10378
| 1 1 1 27 33 26 .06 | 55680 2992
grg 134| 0 2 -16 -10 -30 57 -.04 47 45 | --- --- --- ---
| 1 3 5 63 63 61 .12 | --- ---
iac n/a| 0 1 6 0 -36 -72 -.13 53 53 | 390548 -549 4796 10457
| 1 1 15 51 39 84 .11 | 21554 1999
Table 1.1634.b GPS week : 1634 MJD: 55682.0-55688.0
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 13 12 13 11 11 13 |
R02 | 12 11 14 10 11 11 11 |
R03 | 13 10 13 10 12 11 11 |
R04 | 101 253 163 0 127 133 86 |
R05 | 10 11 13 15 11 12 11 |
R06 | 10 12 13 12 13 13 11 |
R07 | 0 0 0 0 0 23 16 |
R08 | 12 12 11 11 11 11 9 |
R09 | 17 14 13 10 9 9 11 |
R10 | 13 13 12 13 13 10 13 |
R11 | 22 20 22 26 18 17 12 |
R12 | 13 13 14 16 8 13 16 |
R13 | 14 12 16 11 11 10 14 |
R15 | 17 15 14 12 15 16 14 |
R16 | 19 17 13 12 11 14 10 |
R17 | 16 17 22 17 21 21 23 |
R18 | 13 17 11 11 9 19 13 |
R19 | 15 19 14 10 12 10 14 |
R20 | 23 21 24 14 19 23 18 |
R21 | 18 15 8 10 10 11 12 |
R22 | 10 15 13 13 12 10 10 |
R23 | 12 13 14 14 9 10 12 |
R24 | 15 13 12 20 12 11 11 |
Table 1.1634.c GPS week : 1634 MJD: 55682.0-55688.0
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 1634 0 | -64 64 309 -1866 -756 -9168 84.7 1925 1925 | 409484 0
brd 1634 1 | 50 47 417 -1421 448 -9170 84.8 1611 1611 | 364754 0
brd 1634 2 | 14 12 263 -308 -939 -12840 85.9 1828 1828 | 378620 0
brd 1634 3 | 53 7 247 -886 41 -17840 82.7 2078 2078 | 415279 0
brd 1634 4 | -13 100 299 519 -201 -20070 85.8 2139 2139 | 389572 0
brd 1634 5 | -130 20 282 1961 794 -17200 86.3 1979 1979 | 404052 0
brd 1634 6 | -18 15 375 1495 17 -20380 83.8 2655 2655 | 365433 0
-------------+------------------------------------------------------------+----------------
brd 1634 mean| -15 38 313 -72 -85 -15238 84.8 2030 2030 | 389599 0
brd 1634 sdev| 65 34 61 1454 616 4827 1.3 325 325 | 20758 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 2.1634.0 GPS week: 1634 Day: 0 MJD: 55682
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 153| 3 -6 -5 81 -66 6 -.17 64 61 | 0 800 2843 3091
cod 247| -1 2 -3 18 -15 -21 -.25 25 24 | --- --- --- ---
esx 143| 0 0 0 -24 39 -12 .43 17 16 | 54215 -5385 4739 7976
gfz 193| 0 -3 -1 -41 1 35 -.26 22 17 | 264808 -2956 4734 8022
grg 134| -2 0 -8 46 85 61 -.03 44 44 | --- --- --- ---
iac n/a| 1 1 11 -6 -11 -16 -.05 48 48 | 409646 -686 4731 8767
Table 2.1634.1 GPS week: 1634 Day: 1 MJD: 55683
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 153| 3 -4 -4 74 99 -119 -.05 58 52 | 0 1431 2846 3075
cod 247| 0 0 -7 1 -26 -7 -.05 25 25 | --- --- --- ---
esx 143| 0 0 4 53 121 11 .36 18 17 | -2765 316 4702 9440
gfz 193| -1 0 2 -92 -105 89 -.43 22 22 | 218292 2331 4697 9760
grg 134| -1 0 -12 39 -70 133 .13 55 53 | --- --- --- ---
iac n/a| 1 0 0 15 -76 -125 .02 45 45 | 364271 2246 4704 10196
Table 2.1634.2 GPS week: 1634 Day: 2 MJD: 55684
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 153| 3 -1 0 65 -64 -22 -.01 56 46 | 0 1407 2750 2914
cod 247| -1 0 -3 31 -18 28 -.21 24 20 | --- --- --- ---
esx 143| -2 0 1 11 55 -18 .40 17 17 | 4109 -6228 5571 8605
gfz 193| 2 0 3 -102 -39 51 -.32 21 19 | 107951 -5275 5609 8817
grg 134| -1 3 -14 -74 -58 3 .09 48 48 | --- --- --- ---
iac n/a| -2 4 4 49 26 -213 -.11 55 55 | 380417 -3828 5555 9000
Table 2.1634.3 GPS week: 1634 Day: 3 MJD: 55685
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 153| 4 -2 -5 82 41 -169 -.03 37 34 | 0 -77 2242 2417
cod 247| 0 0 -2 42 -63 -7 -.12 35 30 | --- --- --- ---
esx 143| 0 1 1 -9 54 1 .38 14 13 | 34889 -998 4854 8555
gfz 193| 0 -1 1 -38 -38 77 -.33 18 22 | 269894 -4078 4863 8896
grg 134| -1 8 -15 0 -68 132 -.01 53 53 | --- --- --- ---
iac n/a| 1 1 38 37 -72 50 -.09 63 63 | 415062 -147 4822 8863
Table 2.1634.4 GPS week: 1634 Day: 4 MJD: 55686
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 153| 2 1 5 -24 93 120 -.19 39 37 | 0 619 2821 3055
cod 247| -3 6 -3 -7 -16 -8 -.15 25 20 | --- --- --- ---
esx 143| 0 0 -2 50 15 -47 .39 15 14 | 21860 607 4855 8389
gfz 193| 3 -4 1 -42 -51 18 -.23 19 17 | 241422 -583 4852 8359
grg 134| 2 1 -23 -69 15 74 -.11 47 44 | --- --- --- ---
iac n/a| 1 -1 8 -32 -13 -30 -.28 53 53 | 389659 1252 4775 8899
Table 2.1634.5 GPS week: 1634 Day: 5 MJD: 55687
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 153| 0 0 2 67 74 -47 .01 38 37 | 0 -666 2847 3113
cod 247| -4 1 -4 -3 -27 75 -.10 26 23 | --- --- --- ---
esx 143| 0 0 -1 33 50 -9 .40 17 15 | 32002 -7 4452 17874
gfz 193| 0 -3 5 -43 -74 22 -.31 18 14 | 255269 -799 4478 20868
grg 134| 0 0 -22 -80 -17 22 -.13 40 40 | --- --- --- ---
iac n/a| 2 2 -3 -99 -38 -85 -.11 57 57 | 409842 -1951 4669 19137
Table 2.1634.6 GPS week: 1634 Day: 6 MJD: 55688
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 153| 1 0 12 55 -3 -54 -.12 43 43 | 0 507 2573 2700
cod 247| -2 -1 -6 3 27 -18 -.21 23 21 | --- --- --- ---
esx 143| 0 2 1 -5 0 -11 .46 16 17 | -10861 -5731 4384 8946
gfz 193| 1 -1 1 -43 -39 46 -.37 19 16 | 216592 -6166 4376 7930
grg 134| 1 3 -17 65 -101 -27 -.21 39 36 | --- --- --- ---
iac n/a| 0 0 -11 29 -72 -85 -.26 52 52 | 364942 -735 4320 8342
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 3.1634.0 GPS week: 1634 Day: 0 MJD: 55682
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac IGL | bkg cod esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1699 65 10 9 21 42 38 12 | 66 60 53 61 65 68 56
R02 | 1022 50 16 13 19 38 41 11 | 57 62 52 51 68 55 52
R03E | 2637 37 34 19 15 38 35 13 | 82 64 76 78 71 60 70
XR04 |10578 --- 64 --- --- --- 159 101 | --- 173 --- --- --- 268 141
R05 | 1508 42 22 12 11 31 31 10 | 88 96 83 86 92 94 87
R06 | 2274 31 10 12 17 49 46 10 | 117 111 111 111 134 129 112
XR07 | ---- --- 4 --- --- --- --- 0 | --- 599 --- --- --- --- 601
R08 | 887 45 13 14 14 32 49 11 | 84 82 88 78 94 88 82
R09E | 1752 88 23 19 30 42 41 17 | 54 27 40 49 49 34 34
R10E | 1661 59 17 16 19 33 41 13 | 121 124 144 132 108 111 131
R11E | 1964 81 43 31 32 50 71 22 | 139 89 129 117 110 120 113
R12E | 919 48 20 20 15 36 42 12 | 77 45 63 61 53 37 54
R13E | 2055 78 16 17 16 40 38 14 | 61 34 47 44 27 27 40
R15E | 3134 62 23 12 31 39 68 16 | 46 21 37 32 49 59 29
R16E | 732 105 21 24 25 45 46 18 | 121 58 57 72 73 71 62
R17 | 4011 56 15 16 25 52 74 16 | 59 51 56 65 60 89 56
R18 | 775 49 21 17 18 38 44 12 | 58 59 56 46 69 49 49
R19 | 669 33 39 18 27 35 43 15 | 61 51 46 65 32 45 45
R20 | 3577 97 57 15 34 82 45 22 | 96 79 84 97 73 94 83
R21 | 532 109 23 9 18 39 40 17 | 75 77 66 80 71 79 69
R22 | 458 36 21 11 14 67 30 9 | 89 75 76 76 56 77 74
R23 | 816 37 12 12 13 20 59 11 | 51 40 41 43 40 43 37
R24 | 1565 34 23 26 18 42 56 14 | 50 42 63 56 62 30 46
------+-----------------------------------------+-------------------------------------
RMS | 1924 64 25 17 22 44 48 |T 78 92 69 71 69 78 92
WRMS | 1924 61 24 16 17 44 48 |NE 82 82 74 77 89 86 76
MEDI | 1565 50 21 16 18 39 43 |MD 75 62 63 65 68 68 62
Table 3.1634.1 GPS week: 1634 Day: 1 MJD: 55683
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac IGL | bkg cod esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 877 31 27 25 11 51 44 13 | 60 40 57 54 63 54 48
R02 | 1195 26 20 13 12 56 46 11 | 53 69 61 68 68 72 63
R03E | 1127 38 17 13 9 38 30 9 | 104 78 85 91 90 66 83
XR04 |12431 --- 169 --- --- --- 378 253 | --- 245 --- --- --- 261 131
R05 | 1154 31 24 12 23 46 29 11 | 107 101 106 100 113 90 101
R06 | 1797 36 19 10 24 35 45 12 | 135 113 121 126 146 121 121
XR07 | ---- --- 4 --- --- 349 --- 0 | --- 448 --- --- 536 --- 450
R08 | 1381 42 18 22 14 46 31 11 | 106 102 90 92 69 86 93
R09E | 1331 69 22 16 18 54 38 14 | 89 43 45 38 36 42 39
R10E | 2519 62 11 8 19 53 43 12 | 115 88 103 102 111 87 97
R11E | 1530 60 25 25 37 44 72 19 | 105 78 103 93 90 89 89
R12E | 1227 32 27 17 15 45 48 12 | 50 45 42 39 45 40 38
R13E | 954 60 19 12 16 38 35 12 | 76 39 51 48 37 25 42
R15E | 1802 61 30 13 24 44 43 15 | 79 26 39 41 30 46 32
R16E | 968 85 22 18 36 51 32 17 | 132 72 89 63 55 88 78
R17 | 2924 68 35 19 21 69 52 17 | 61 44 64 53 39 65 53
R18 | 731 80 31 18 20 45 39 16 | 85 32 50 41 51 41 38
R19 | 704 88 34 23 14 51 56 18 | 49 39 32 44 45 58 30
R20 | 3441 82 47 26 32 69 44 20 | 90 66 57 82 66 93 68
R21 | 1135 54 23 13 21 45 57 14 | 109 70 76 88 64 73 76
R22 | 482 45 22 14 26 61 55 14 | 76 56 62 53 46 85 58
R23 | 1519 49 19 20 17 83 37 12 | 65 33 48 46 76 61 41
R24 | 1492 55 15 18 22 96 42 13 | 91 53 50 67 87 48 53
------+-----------------------------------------+-------------------------------------
RMS | 1610 58 25 18 22 55 45 |T 87 86 68 68 89 76 83
WRMS | 1610 52 25 17 22 53 45 |NE 88 80 86 87 97 84 83
MEDI | 1227 55 22 17 20 51 43 |MD 89 66 61 63 64 66 63
Table 3.1634.2 GPS week: 1634 Day: 2 MJD: 55684
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac IGL | bkg cod esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1313 28 19 24 23 31 38 12 | 41 47 44 47 46 62 44
R02 | 1388 36 15 18 25 31 63 13 | 66 56 59 60 56 63 55
R03E | 1720 42 15 12 24 49 64 13 | 69 54 58 60 46 50 53
XR04M |12440 --- 85 --- --- --- 311 163 | --- 195 --- --- --- 177 132
R05 | 812 26 34 17 24 34 29 12 | 74 72 71 64 93 82 66
R06 | 1433 40 21 12 23 36 61 13 | 113 94 94 93 115 84 92
XR07M | ---- --- 4 --- --- --- --- 0 | --- 535 --- --- --- --- 535
R08M | 1159 41 9 10 20 37 49 11 | 83 70 73 85 86 69 73
R09E | 1120 59 22 21 17 30 31 13 | 52 23 44 40 47 33 32
R10E | 2926 46 18 14 22 32 32 11 | 93 91 90 92 91 69 86
R11E | 1217 80 48 28 21 47 64 21 | 99 77 99 91 94 72 81
R12E | 1072 42 23 13 24 29 58 13 | 43 43 47 51 54 31 40
R13E | 812 39 18 18 25 53 86 16 | 48 32 44 43 54 47 33
R15E | 3728 56 17 18 27 60 51 14 | 70 26 47 30 56 35 32
R16E | 729 44 24 14 14 48 49 12 | 88 34 42 41 46 48 38
R17M | 2642 100 29 18 27 57 86 21 | 64 41 53 67 43 80 46
R18M | 1014 30 20 12 20 44 50 11 | 51 48 40 36 47 32 37
R19M | 781 38 11 8 26 54 78 14 | 60 45 52 66 40 65 48
R20M | 3669 141 34 18 14 59 43 23 | 151 63 55 63 68 64 62
R21M | 965 26 15 12 11 66 28 8 | 77 74 70 78 71 84 73
R22M | 497 48 16 14 14 46 58 12 | 56 53 43 53 50 69 45
R23M | 2725 44 27 27 18 66 37 14 | 39 35 47 35 70 38 31
R24M | 1131 20 29 19 15 63 36 11 | 49 38 52 43 60 55 42
------+-----------------------------------------+-------------------------------------
RMS | 1828 56 24 17 21 48 55 |T 70 80 58 58 63 64 77
WRMS | 1828 46 20 17 19 48 55 |NE 73 67 67 66 77 72 64
MEDI | 1159 42 20 17 22 47 50 |MD 66 53 52 60 56 63 48
Table 3.1634.3 GPS week: 1634 Day: 3 MJD: 55685
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac IGL | bkg cod esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1026 29 28 17 20 43 42 12 | 59 43 59 55 47 55 53
R02 | 1762 31 14 10 17 49 41 10 | 73 100 91 93 92 88 89
R03E | 2747 23 26 11 16 32 60 10 | 76 80 87 84 85 82 83
XR04 | 9302 --- 5 --- --- --- 324 0 | --- 164 --- --- --- 203 171
R05 | 1446 28 38 16 29 48 96 15 | 108 96 78 91 77 63 89
R06 | 935 26 34 11 18 38 65 12 | 98 86 89 94 93 96 92
XR07 | ---- --- 5 --- --- 187 --- 0 | --- 743 --- --- 725 --- 743
R08 | 767 34 21 11 14 57 72 10 | 86 92 93 83 78 75 88
R09E | 900 27 29 6 11 56 71 9 | 61 48 66 56 45 75 58
R10E | 4822 43 27 12 12 30 52 12 | 123 84 109 100 93 95 102
R11E | 1952 63 73 25 33 72 81 25 | 132 100 147 155 125 139 137
R12E | 614 52 28 14 24 69 53 15 | 74 30 52 46 61 49 43
R13E | 1240 33 21 11 17 55 71 11 | 54 43 50 60 81 47 51
R15E | 3900 29 29 13 15 47 58 11 | 56 37 37 45 52 45 35
R16E | 668 41 23 8 16 42 60 12 | 94 60 72 63 76 82 68
R17 | 3549 48 46 15 15 58 57 16 | 74 37 46 47 45 61 43
R18 | 2673 41 14 16 6 62 45 11 | 102 68 66 76 70 69 72
R19 | 790 27 15 9 19 58 54 9 | 40 47 53 64 42 68 51
R20 | 1249 50 25 13 16 72 67 14 | 84 94 86 76 114 107 85
R21 | 1179 27 17 12 17 55 65 10 | 59 65 58 77 63 102 62
R22 | 611 31 28 10 23 39 46 12 | 65 54 59 54 64 82 53
R23 | 1829 34 42 15 13 55 72 14 | 147 115 129 118 99 127 124
R24 | 1699 28 71 27 11 52 78 20 | 45 72 62 45 72 73 44
------+-----------------------------------------+-------------------------------------
RMS | 2077 37 35 14 18 53 63 |T 81 102 75 75 104 85 105
WRMS | 2077 34 30 13 22 53 63 |NE 84 81 79 83 77 75 80
MEDI | 1249 31 27 12 16 55 60 |MD 74 72 66 76 76 75 72
Table 3.1634.4 GPS week: 1634 Day: 4 MJD: 55686
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac IGL | bkg cod esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 687 18 24 15 20 26 42 10 | 43 40 48 33 39 49 37
R02 | 1685 20 17 8 20 33 61 10 | 63 55 65 73 57 64 62
R03E | 3039 27 19 11 26 27 49 11 | 79 70 71 77 67 67 71
XR04 | 1472 204 78 --- --- --- 316 127 | 221 145 --- --- --- 220 152
R05 | 1449 28 27 18 17 25 34 11 | 54 46 36 49 55 45 42
R06 | 1131 22 26 16 22 56 59 12 | 45 43 40 41 60 53 38
XR07 |10644 --- 5 --- --- --- --- 0 | --- 395 --- --- --- --- 393
R08 | 1318 41 16 11 15 35 54 11 | 58 41 53 41 41 44 42
R09E | 1114 28 16 7 15 38 44 9 | 46 34 39 35 46 39 34
R10E | 6218 54 17 8 16 24 63 13 | 115 66 73 68 71 78 72
R11E | 1239 34 57 29 18 70 34 18 | 135 87 144 124 118 107 120
R12E | 1343 30 12 8 18 50 19 8 | 44 33 37 38 49 44 34
R13E | 981 33 19 17 19 42 40 11 | 59 45 52 49 49 53 46
R15E | 1590 47 29 18 22 45 57 14 | 56 31 45 48 45 34 36
R16E | 858 38 18 11 25 38 38 11 | 61 44 53 48 40 52 47
R17 | 2284 84 45 18 19 40 85 21 | 70 48 65 58 63 90 51
R18 | 4448 31 16 8 13 43 36 8 | 79 55 64 58 48 60 59
R19 | 634 37 15 16 19 79 53 11 | 92 47 66 62 49 36 59
R20 | 1065 67 43 17 24 56 74 19 | 219 215 231 236 237 197 223
R21 | 1727 21 21 8 10 42 56 9 | 64 72 70 69 61 74 68
R22 | 610 46 16 18 9 53 46 11 | 80 46 37 45 56 48 43
R23 | 510 21 9 9 20 31 49 9 | 205 212 209 217 209 193 210
R24 | 855 22 11 13 15 74 76 11 | 52 49 55 54 46 30 50
------+-----------------------------------------+-------------------------------------
RMS | 2138 39 25 15 19 47 53 |T 88 83 73 72 71 76 86
WRMS | 2138 37 20 14 17 44 53 |NE 51 46 47 49 52 52 44
MEDI | 1318 31 18 13 19 42 49 |MD 63 48 55 54 55 53 51
Table 3.1634.5 GPS week: 1634 Day: 5 MJD: 55687
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac IGL | bkg cod esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 887 22 25 14 16 32 54 11 | 41 34 45 41 42 51 38
R02 | 1488 33 15 11 15 40 51 11 | 68 79 92 83 68 64 80
R03E | 3140 26 21 11 24 35 41 11 | 77 73 83 86 97 77 79
XR04 | 1212 171 102 --- --- --- 254 132 | 193 130 --- --- --- 187 168
R05 | 1361 20 31 18 21 58 41 12 | 53 57 57 48 60 45 50
R06 | 1579 19 20 29 12 16 52 12 | 68 59 76 59 70 65 63
XR07 | 2790 --- 31 19 46 53 77 22 | --- 454 13 30 333 16 459
R08 | 2590 19 24 10 22 43 45 11 | 54 54 54 43 67 45 48
R09E | 1214 19 20 13 16 35 30 9 | 48 31 47 55 34 47 43
R10E | 4379 30 14 13 10 19 52 10 | 51 53 60 54 50 68 53
R11E | 1326 36 37 19 16 48 84 16 | 94 73 87 83 65 91 80
R12E | 1712 52 18 13 14 35 37 12 | 64 26 48 39 42 34 38
R13E | 1226 37 16 12 14 35 24 9 | 76 55 65 63 64 47 60
R15E | 1910 33 37 10 28 51 76 16 | 53 42 53 52 27 38 46
R16E | 1159 27 25 14 23 31 67 13 | 85 58 71 58 47 78 62
R17 | 1715 70 33 15 28 59 97 21 | 41 27 28 51 54 82 27
R18 | 4169 25 46 39 16 34 71 18 | 33 39 54 32 40 30 28
R19 | 1034 31 15 13 12 60 39 9 | 63 42 52 52 36 44 48
R20 | 1321 98 39 19 24 48 61 23 | 372 334 334 341 343 339 342
R21 | 835 20 19 16 20 40 43 10 | 78 76 75 91 82 95 80
R22 | 646 24 15 14 11 36 56 10 | 48 43 49 44 44 40 43
R23 | 1031 22 9 15 17 26 48 9 | 276 283 291 281 290 278 283
R24 | 1071 15 19 8 13 31 67 10 | 48 57 46 42 54 56 45
------+-----------------------------------------+-------------------------------------
RMS | 1978 38 25 17 18 40 57 |T 90 94 80 78 91 83 98
WRMS | 1978 37 23 15 14 40 57 |NE 57 57 67 57 60 56 57
MEDI | 1326 26 21 14 16 35 52 |MD 63 57 54 52 54 56 53
Table 3.1634.6 GPS week: 1634 Day: 6 MJD: 55688
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac IGL | bkg cod esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1192 32 26 10 26 38 55 13 | 43 42 48 46 51 65 45
R02 | 870 18 17 13 20 26 51 10 | 62 76 70 75 77 63 69
R03E | 2618 38 21 11 19 29 33 10 | 81 91 89 89 85 79 86
XR04 | 1399 357 47 --- --- --- 159 86 | 258 107 --- --- --- 207 126
R05 | 1192 27 20 7 18 30 59 11 | 69 75 71 76 76 67 72
R06 | 1740 30 21 9 19 56 48 11 | 94 95 103 116 79 94 102
XR07 | 3191 --- 19 21 31 58 53 16 | --- 440 19 37 315 22 437
R08 | 2112 15 12 9 18 30 47 9 | 91 96 91 98 90 87 93
R09E | 877 34 27 13 23 29 20 11 | 54 43 49 45 40 45 43
R10E | 3867 32 26 14 23 49 58 13 | 69 73 74 71 73 87 71
R11E | 745 37 25 17 18 58 45 12 | 94 87 113 98 95 108 100
R12E | 1624 55 28 22 14 35 72 16 | 85 38 59 52 36 41 48
R13E | 2332 74 15 12 9 48 36 14 | 80 48 59 54 45 40 52
R15E | 6524 42 26 13 28 57 51 14 | 73 61 53 56 50 46 55
R16E | 1325 24 19 10 17 36 43 9 | 98 80 81 75 67 81 79
R17 | 5136 101 31 18 28 42 86 22 | 69 48 53 56 61 97 46
R18 | 4662 26 12 16 16 29 72 12 | 71 66 53 65 61 49 58
R19 | 1139 36 26 25 15 32 49 13 | 73 60 37 49 50 38 46
R20 | 2792 45 35 35 13 40 60 17 | 395 419 425 421 415 415 418
R21 | 592 48 14 14 16 30 51 12 | 118 89 87 98 98 130 94
R22 | 1198 30 22 10 14 38 41 10 | 88 62 62 67 65 70 64
R23 | 1256 35 21 15 24 41 36 11 | 368 362 360 363 358 359 362
R24 | 908 41 21 14 12 28 41 11 | 76 48 48 52 45 29 46
------+-----------------------------------------+-------------------------------------
RMS | 2655 43 23 16 19 39 52 |T 114 113 95 98 106 100 113
WRMS | 2655 43 21 17 16 36 52 |NE 67 72 73 78 70 72 72
MEDI | 1399 35 21 13 18 36 51 |MD 80 75 62 67 67 70 71
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