[IGSREPORT-19264] Wk 1612 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Dec 16 07:03:57 PST 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1612 (Nov 28, 2010 - Dec 04, 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 2.1612.
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:
igl1612[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1612 in the SP3 format.
igl16127.sum Combination Report for GPS Week 1612.
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 | 341.0 ns
1 | 327.1 ns
2 | 314.2 ns
3 | 321.5 ns
4 | 325.2 ns
5 | 319.8 ns
6 | 320.4 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 1.1612, 1a.1612).
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 2.1612.0-6)
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 3.1612.0-6).
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 1612 summary. (Nov 28, 2010 - Dec 04, 2010)
Table 1.1612.a GPS week : 1612 MJD: 55528.0-55534.0
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 134| 0 0 9 7 -18 -124 -.12 31 30 | 0 590 5694 6438
| 1 1 3 44 29 58 .04 | 0 2504
cod 233| -1 0 -2 32 24 12 -.08 14 12 | --- --- --- ---
| 0 0 4 15 16 26 .03 | --- ---
esx 148| -1 0 -6 -33 -30 52 .34 26 23 | 6516 1210 5642 14633
| 1 1 4 34 35 57 .08 | 9497 3839
gfz 190| -2 0 -5 -74 -21 -6 -.32 31 28 | 150815 1302 5711 14761
| 2 2 7 33 95 43 .08 | 8764 3140
iac n/a| 3 0 9 -26 -11 74 -.18 33 33 | 325020 -795 5671 15074
| 2 1 10 37 28 30 .05 | 8813 2150
mcc n/a| 4 -1 63 -21 15 357 -.43 185 185 | --- --- --- ---
| 13 8 13 113 175 608 .26 | --- ---
Table 1.1612.b GPS week : 1612 MJD: 55528.0-55534.0
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 | 16 15 19 23 20 19 19 |
R02 | 16 22 15 17 23 21 18 |
R05 | 14 15 15 17 22 22 23 |
R06 | 27 20 14 18 19 22 21 |
R07 | 19 20 19 17 22 27 31 |
R08 | 15 14 17 17 17 20 27 |
R09 | 10 10 11 12 12 14 10 |
R10 | 10 9 10 10 13 16 14 |
R11 | 19 21 15 12 12 20 18 |
R12 | 7 10 10 8 10 10 11 |
R13 | 10 10 9 11 10 9 9 |
R15 | 13 15 10 14 13 12 11 |
R16 | 10 10 12 10 9 10 14 |
R17 | 4587 0 0 --- --- --- --- |
R18 | 13 11 11 7 12 8 13 |
R19 | 9 11 9 11 11 14 12 |
R20 | 22 16 16 9 13 16 12 |
R21 | 14 12 7 10 13 9 9 |
R22 | 14 19 11 8 9 15 11 |
R23 | 12 16 11 9 11 9 10 |
R24 | 12 11 10 9 10 11 11 |
Table 1.1612.c GPS week : 1612 MJD: 55528.0-55534.0
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 1612 0 | 7 37 101 -1268 293 -16780 85.1 1733 1733 | 340973 0
brd 1612 1 | 83 -78 18 -1624 -1028 -16680 87.4 1886 1886 | 327130 0
brd 1612 2 | 5 -37 79 -386 -1244 -16140 84.5 2090 2090 | 314177 0
brd 1612 3 | 106 103 121 35 2061 -11510 86.8 2599 2599 | 321526 0
brd 1612 4 | -36 -182 -11 -901 -1091 -13350 84.1 3385 3385 | 325158 0
brd 1612 5 | -26 -65 150 -251 -1634 -16840 85.0 2416 2416 | 319795 0
brd 1612 6 | 19 33 266 629 54 -19790 84.5 2360 2360 | 320376 0
-------------+------------------------------------------------------------+----------------
brd 1612 mean| 22 -26 103 -538 -369 -15870 85.3 2352 2352 | 324162 0
brd 1612 sdev| 53 94 91 779 1280 2684 1.3 547 547 | 8489 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 2.1612.0 GPS week: 1612 Day: 0 MJD: 55528
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 134| 0 1 14 -40 -1 -121 -.11 29 29 | 0 2695 5267 6053
cod 233| -2 0 -4 54 36 -9 -.06 14 14 | --- --- --- ---
esx 148| 0 0 -1 13 -49 87 .38 28 23 | 19383 -2108 5405 10802
gfz 190| -4 -1 -2 -91 55 7 -.38 32 28 | 165991 -2994 5472 11128
iac n/a| 4 0 -1 -68 -3 105 -.24 28 28 | 341895 -3672 5393 10793
mcc n/a| 24 5 69 -125 178 -78 -.33 216 216 | --- --- --- ---
Table 2.1612.1 GPS week: 1612 Day: 1 MJD: 55529
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 134| 3 1 12 4 -41 -213 -.10 31 30 | 0 -825 5798 6444
cod 233| -2 0 -5 24 15 40 -.09 13 11 | --- --- --- ---
esx 148| 1 1 -15 -53 -4 88 .42 32 27 | -7614 4725 5148 11942
gfz 190| -4 -2 -21 -47 85 3 -.32 35 28 | 149814 2535 5223 11976
iac n/a| 4 1 18 -19 -11 53 -.17 32 32 | 326825 317 5146 12445
mcc n/a| 14 12 52 7 213 -214 -.84 166 166 | --- --- --- ---
Table 2.1612.2 GPS week: 1612 Day: 2 MJD: 55530
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 134| 1 -1 5 74 -14 -20 -.16 24 23 | 0 188 5620 6458
cod 233| -1 0 -10 18 7 0 -.09 15 13 | --- --- --- ---
esx 148| 0 0 -2 -70 -18 -54 .44 22 20 | -4791 3575 7836 15208
gfz 190| 0 -3 -4 -68 -31 -60 -.32 27 29 | 138308 2268 8126 15485
iac n/a| 4 -1 26 -2 3 82 -.26 33 33 | 314854 -1045 7938 15926
mcc n/a| 2 -2 48 -13 -4 -253 -.17 172 172 | --- --- --- ---
Table 2.1612.3 GPS week: 1612 Day: 3 MJD: 55531
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 134| -1 -1 7 -20 7 -116 -.03 28 27 | 0 3151 6520 7592
cod 233| 0 0 -2 51 0 -21 -.08 13 11 | --- --- --- ---
esx 148| -1 1 -7 -8 -31 108 .21 21 20 | 7702 3493 6409 17770
gfz 190| -1 1 -8 -123 18 30 -.38 36 30 | 144936 2747 6449 18050
iac n/a| 0 0 14 -52 20 54 -.15 30 30 | 322829 -978 6574 18155
mcc n/a| -13 -14 74 -149 -178 378 -.32 228 228 | --- --- --- ---
Table 2.1612.4 GPS week: 1612 Day: 4 MJD: 55532
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 134| 0 -1 7 -41 19 -136 -.17 30 28 | 0 3093 5014 5562
cod 233| 0 0 0 38 33 -2 -.03 14 10 | --- --- --- ---
esx 148| -1 1 -6 -7 -93 77 .30 28 26 | 11579 -5535 4329 14986
gfz 190| 1 0 -2 -95 14 -69 -.23 28 20 | 156131 -3240 4293 14984
iac n/a| 0 -2 4 -68 4 121 -.16 33 33 | 328938 -2747 4288 15254
mcc n/a| -9 0 63 -114 152 1456 -.62 140 140 | --- --- --- ---
Table 2.1612.5 GPS week: 1612 Day: 5 MJD: 55533
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 134| 0 -1 9 45 -44 -107 -.13 34 32 | 0 -3485 6454 7115
cod 233| 0 2 0 22 39 35 -.10 16 13 | --- --- --- ---
esx 148| -3 0 -4 -74 -35 51 .30 25 23 | 8934 298 4880 17588
gfz 190| -5 2 4 -19 -110 46 -.39 30 31 | 148064 2891 4890 17590
iac n/a| 3 -2 4 20 -26 37 -.18 37 37 | 318865 2971 4846 17967
mcc n/a| 10 -7 54 112 -17 645 -.58 166 166 | --- --- --- ---
Table 2.1612.6 GPS week: 1612 Day: 6 MJD: 55534
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 134| 0 2 7 27 -56 -154 -.13 43 41 | 0 -682 5190 5845
cod 233| 0 0 3 20 35 43 -.12 16 11 | --- --- --- ---
esx 148| -2 -3 -8 -32 16 10 .31 25 22 | 10421 4027 5487 14136
gfz 190| 0 -1 -4 -76 -182 -3 -.20 29 28 | 152464 4911 5525 14118
iac n/a| 6 0 -2 8 -65 68 -.10 36 36 | 320936 -413 5513 14983
mcc n/a| 4 -1 84 130 -229 567 -.12 205 205 | --- --- --- ---
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 3.1612.0 GPS week: 1612 Day: 0 MJD: 55528
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2450 35 12 25 27 44 --- 16 | 76 75 74 71 90 --- 75
R02E | 2644 31 21 21 32 41 --- 16 | 108 131 132 129 130 --- 125
R05E | 2810 30 12 27 35 34 403 14 | 97 97 104 110 80 129 93
XR06E | 3416 49 32 36 --- --- --- 26 | 42 37 51 --- --- --- 36
R07E | 1814 36 18 42 --- 42 --- 19 | 20 24 55 --- 53 --- 31
R08E | 871 37 11 26 25 31 195 14 | 22 26 38 38 46 66 27
R09 | 1192 11 6 17 21 30 --- 9 | 25 29 36 38 35 --- 28
R10 | 1364 14 10 13 18 27 --- 9 | 34 31 36 33 53 --- 34
R11 | 1141 39 22 42 46 34 87 19 | 37 58 65 70 54 28 51
R12 | 723 14 8 15 24 15 --- 7 | 25 28 29 35 28 --- 25
R13 | 1732 11 12 26 27 20 --- 10 | 27 28 39 37 28 --- 26
R15 | 2247 29 7 34 33 21 117 12 | 40 28 35 42 41 41 31
R16 | 649 23 9 17 13 22 --- 9 | 32 37 41 36 34 --- 33
XR17 |>>>>> --- --- 2791 --- 5900 --- 4587 | --- --- 2 --- 1 --- 9999
R18 | 2113 31 18 14 48 23 --- 12 | 44 55 68 67 50 --- 53
R19 | 803 19 7 14 48 22 --- 8 | 41 54 70 72 56 --- 54
R20 | 1724 54 16 58 21 22 --- 21 | 42 43 71 53 51 --- 43
R21 | 1011 26 23 27 22 19 --- 13 | 43 70 69 72 44 --- 56
R22 | 2268 31 8 32 26 24 --- 13 | 33 54 74 69 37 --- 49
R23 | 1645 35 7 15 22 23 109 11 | 26 50 57 63 59 122 46
R24 | 1241 13 14 27 46 25 --- 11 | 42 53 67 82 56 --- 52
------+-----------------------------------------+-------------------------------------
RMS | 1732 29 14 28 32 28 216 |T 42 50 57 62 51 77 48
WRMS | 1732 29 14 23 28 28 216 |NE 35 44 50 54 41 63 41
MEDI | 1724 30 12 26 26 24 117 |MD 37 43 57 63 50 66 43
Table 3.1612.1 GPS week: 1612 Day: 1 MJD: 55529
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1168 29 9 34 40 39 --- 15 | 69 76 93 92 98 --- 80
R02E | 2834 58 28 30 31 45 --- 22 | 87 118 118 113 110 --- 107
R05E | 859 25 12 34 37 39 235 14 | 64 71 77 89 74 124 67
XR06E | 2142 28 17 45 --- --- --- 19 | 27 32 37 --- --- --- 23
R07E | 2971 27 19 42 --- 54 --- 19 | 18 27 40 --- 54 --- 26
R08E | 2470 28 13 23 41 39 219 14 | 28 22 34 46 43 49 22
R09 | 2550 21 9 19 36 24 --- 10 | 24 31 40 50 26 --- 26
R10 | 1947 19 8 15 28 23 --- 9 | 30 24 34 32 35 --- 26
R11 | 844 39 20 59 36 35 91 20 | 29 53 85 77 52 22 48
R12 | 557 24 8 19 21 20 --- 9 | 27 28 36 40 32 --- 26
R13 | 1222 15 7 26 16 24 --- 9 | 23 24 39 32 29 --- 23
R15 | 2587 39 15 31 58 30 118 15 | 33 26 37 58 32 33 24
R16 | 1537 27 8 22 14 17 --- 10 | 24 38 44 40 23 --- 31
XR17 | ---- --- 4 --- --- --- --- 0 | --- 9999 --- --- --- --- 9999
R18 | 1942 17 13 29 15 16 --- 10 | 30 35 66 47 35 --- 38
R19 | 863 18 11 26 36 29 --- 11 | 24 25 46 54 35 --- 27
R20 | 1401 37 11 30 31 41 --- 16 | 14 20 48 42 43 --- 23
R21 | 2735 28 10 29 27 22 --- 11 | 19 41 54 52 39 --- 37
R22 | 1213 39 13 47 43 40 --- 18 | 17 37 65 70 32 --- 28
R23 | 1213 42 12 40 45 26 111 16 | 15 39 68 77 27 53 32
R24 | 1927 22 12 26 48 16 --- 10 | 20 29 49 59 26 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1885 31 13 32 35 32 166 |T 31 39 55 59 44 56 37
WRMS | 1885 30 11 27 28 32 166 |NE 23 32 50 52 33 36 29
MEDI | 1537 27 12 29 36 29 118 |MD 24 31 46 52 35 49 26
Table 3.1612.2 GPS week: 1612 Day: 2 MJD: 55530
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1108 38 15 34 41 50 --- 19 | 79 86 111 89 114 --- 93
R02E | 2142 22 20 25 29 41 --- 15 | 50 52 80 64 61 --- 55
R05E | 943 30 17 21 43 43 164 15 | 44 70 66 90 68 105 58
XR06E | 2808 28 11 22 --- --- --- 14 | 59 39 37 --- --- --- 42
R07E | 2398 36 18 40 --- 43 --- 19 | 21 27 37 --- 45 --- 19
R08E | 2752 26 24 22 25 47 247 16 | 28 24 27 31 45 43 19
R09 | 4256 27 12 13 23 23 --- 10 | 32 32 37 31 28 --- 29
R10 | 2601 22 9 16 21 23 --- 9 | 31 28 35 36 38 --- 26
R11 | 1074 26 20 33 27 24 97 15 | 52 55 69 63 44 30 51
R12 | 1016 17 11 24 33 15 --- 10 | 22 24 45 43 29 --- 27
R13 | 875 16 10 21 18 19 --- 9 | 27 32 46 37 35 --- 31
R15 | 2597 21 14 14 25 21 124 10 | 33 26 38 32 40 44 26
R16 | 1641 15 13 25 34 30 --- 11 | 22 34 52 40 25 --- 31
XR17 | ---- --- 6 --- --- --- --- 0 | --- 9999 --- --- --- --- 9999
R18 | 1086 26 5 13 33 33 --- 11 | 32 48 50 44 57 --- 44
R19 | 645 14 10 15 29 27 --- 9 | 30 41 42 58 42 --- 37
R20 | 1372 32 14 18 8 51 --- 16 | 36 36 45 38 45 --- 36
R21 | 3142 9 11 10 17 21 --- 7 | 40 53 47 50 35 --- 44
R22 | 649 18 9 18 26 30 --- 10 | 30 36 41 32 39 --- 32
R23 | 1189 13 21 17 20 25 189 11 | 28 42 38 36 31 103 29
R24 | 3231 26 11 13 17 22 --- 10 | 38 42 52 51 49 --- 42
------+-----------------------------------------+-------------------------------------
RMS | 2089 24 15 22 27 33 172 |T 36 41 49 48 45 65 38
WRMS | 2089 23 13 20 29 33 172 |NE 32 37 45 42 38 59 34
MEDI | 1372 22 12 18 25 27 164 |MD 32 36 45 40 42 44 32
Table 3.1612.3 GPS week: 1612 Day: 3 MJD: 55531
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 3038 42 29 18 28 68 --- 22 | 55 74 60 52 83 --- 61
R02E | 2580 36 11 32 30 43 --- 17 | 102 108 95 111 126 --- 104
R05E | 1528 37 18 25 35 44 312 17 | 66 90 91 93 78 334 82
XR06E | 2765 38 14 25 32 --- --- 17 | 40 54 61 33 --- --- 48
R07E | 4200 37 12 30 75 44 --- 17 | 17 34 49 67 52 --- 31
R08E | 3936 47 17 22 28 35 241 17 | 34 30 40 37 41 115 26
R09 | 4274 27 10 19 18 26 --- 11 | 46 40 50 36 36 --- 40
R10 | 2609 28 9 12 11 18 --- 9 | 26 31 32 34 32 --- 28
R11 | 2281 24 17 24 26 22 89 12 | 48 62 51 50 49 35 52
R12 | 1299 16 8 11 11 24 --- 8 | 34 34 26 24 33 --- 29
R13 | 888 15 10 23 29 25 --- 10 | 28 34 48 49 32 --- 33
R15 | 2968 37 12 24 29 21 154 13 | 38 39 40 30 41 82 34
R16 | 1363 28 9 14 30 21 --- 10 | 37 35 42 46 37 --- 35
R18 | 1094 8 8 10 13 21 --- 7 | 62 54 62 60 66 --- 59
R19 | 1181 21 14 25 71 12 --- 10 | 43 52 71 92 58 --- 55
R20 | 1702 14 11 13 19 26 --- 9 | 53 46 49 48 42 --- 45
R21 | 4634 12 10 23 38 21 --- 9 | 52 59 74 89 47 --- 58
R22 | 959 11 12 16 30 16 --- 8 | 45 50 60 48 52 --- 50
R23 | 1222 18 10 16 19 15 271 8 | 27 36 36 36 30 201 31
R24 | 2036 21 13 15 54 14 --- 9 | 31 50 54 91 42 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 2598 28 13 21 36 30 228 |T 44 50 54 56 51 153 47
WRMS | 2598 27 11 20 30 30 228 |NE 40 44 49 52 42 106 42
MEDI | 2036 24 11 19 29 22 241 |MD 40 46 50 48 42 115 44
Table 3.1612.4 GPS week: 1612 Day: 4 MJD: 55532
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 2483 22 16 34 40 65 --- 20 | 59 53 58 73 77 --- 56
R02E | 3184 54 21 42 51 50 --- 22 | 57 54 47 71 72 --- 51
R05E | 1322 41 27 36 31 56 224 22 | 35 71 66 73 60 172 55
R06E | 8778 47 22 23 23 40 --- 18 | 56 43 52 42 35 --- 47
XR07E | 8023 34 21 --- 71 43 --- 21 | 23 28 --- 62 50 --- 28
R08E | 4045 44 20 22 28 35 117 17 | 42 26 42 48 48 143 31
R09 | 4035 33 9 26 20 21 --- 12 | 27 37 47 46 35 --- 34
R10 | 4022 36 11 27 22 23 --- 13 | 28 33 42 39 28 --- 30
R11 | 4005 24 11 23 26 27 132 11 | 59 52 58 48 60 45 54
R12 | 2003 18 9 23 18 18 --- 9 | 29 25 29 24 30 --- 24
R13 | 2778 15 8 24 16 22 --- 9 | 31 32 40 37 38 --- 32
R15 | 5014 23 10 22 24 38 118 13 | 26 31 28 38 42 69 28
R16 | 1225 22 8 15 21 24 --- 9 | 26 29 34 28 35 --- 28
R18 | 895 27 6 36 33 17 --- 12 | 38 48 82 76 51 --- 51
R19 | 1311 25 7 31 31 14 --- 11 | 39 48 65 66 45 --- 46
R20 | 1834 27 12 29 34 24 --- 12 | 49 49 44 65 36 --- 42
R21 | 3193 13 9 41 21 25 --- 13 | 42 45 85 52 40 --- 50
R22 | 881 21 9 14 24 23 --- 9 | 49 36 40 37 27 --- 35
R23 | 795 13 9 28 29 25 49 10 | 23 27 38 38 46 63 28
R24 | 1369 18 13 18 23 20 --- 9 | 41 49 47 50 46 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 3385 30 14 28 28 33 140 |T 38 40 49 50 45 98 39
WRMS | 3385 28 10 26 20 33 140 |NE 36 38 48 46 39 59 37
MEDI | 2483 24 10 26 24 24 118 |MD 38 37 47 48 42 69 35
Table 3.1612.5 GPS week: 1612 Day: 5 MJD: 55533
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1137 23 16 16 20 66 --- 18 | 41 40 57 47 76 --- 49
R02E | 3760 59 17 27 29 44 --- 20 | 92 98 80 82 108 --- 92
R05E | 1136 46 26 26 36 58 269 21 | 46 64 61 67 56 130 52
R06E | 3402 53 26 30 25 47 --- 21 | 47 51 66 36 38 --- 51
R07E | 1644 55 26 34 41 76 --- 26 | 23 34 34 50 65 --- 25
R08E | 4648 47 21 30 36 44 119 19 | 46 27 48 36 56 41 32
R09 | 3655 40 20 14 21 18 --- 13 | 40 33 43 42 31 --- 32
R10 | 2669 31 9 34 35 36 --- 15 | 26 27 48 43 36 --- 28
XR11 |13067 34 20 --- 42 35 144 19 | 40 65 --- 48 48 40 51
R12 | 2195 27 12 18 23 16 --- 10 | 27 34 40 30 31 --- 31
R13 | 1883 18 12 19 14 17 --- 9 | 34 29 40 31 31 --- 29
R15 | 2052 18 8 22 19 32 129 11 | 20 29 36 32 31 58 26
R16 | 1266 20 10 16 29 23 --- 9 | 26 33 36 39 25 --- 28
R18 | 1372 11 9 17 19 19 --- 8 | 43 45 43 49 48 --- 44
R19 | 2394 32 8 38 41 9 --- 13 | 32 46 80 82 40 --- 50
R20 | 3598 31 20 28 45 30 --- 15 | 30 51 38 77 42 --- 40
R21 | 772 19 7 19 27 15 --- 8 | 43 49 60 56 56 --- 50
R22 | 774 21 10 40 33 28 --- 14 | 29 37 67 43 21 --- 38
R23 | 942 18 14 10 21 18 81 8 | 30 21 29 24 32 70 23
R24 | 1002 28 16 12 29 17 --- 10 | 32 44 42 40 45 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 2416 34 16 25 30 37 166 |T 37 42 49 47 45 67 40
WRMS | 2416 32 13 23 31 37 166 |NE 32 38 46 45 36 56 36
MEDI | 1883 28 14 22 29 28 129 |MD 32 37 43 43 40 58 38
Table 3.1612.6 GPS week: 1612 Day: 6 MJD: 55534
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01E | 1194 28 17 24 34 60 --- 18 | 47 46 62 47 84 --- 53
R02E | 3764 49 14 28 26 42 --- 17 | 93 102 91 79 88 --- 93
R05E | 1803 72 18 27 35 47 263 22 | 59 44 46 60 50 113 39
R06E | 1303 64 14 25 32 48 --- 20 | 49 41 48 43 40 --- 41
R07E | 1200 61 36 58 66 70 --- 30 | 24 38 70 45 61 --- 34
R08E | 4749 89 32 24 27 50 224 27 | 33 39 34 36 51 51 30
R09 | 1798 20 9 20 28 26 --- 10 | 29 41 44 51 37 --- 36
R10 | 3856 36 12 16 23 39 --- 14 | 31 36 38 41 49 --- 33
R11 | 2973 48 16 37 23 28 216 17 | 47 54 70 48 47 39 50
R12 | 2052 29 12 20 26 18 --- 10 | 29 27 33 36 33 --- 27
R13 | 1518 26 7 18 18 16 --- 9 | 29 34 45 34 30 --- 33
R15 | 1413 17 9 19 15 31 150 10 | 31 32 40 41 38 60 32
R16 | 593 23 7 33 22 31 --- 13 | 27 32 50 48 31 --- 31
R18 | 1378 40 7 22 21 27 --- 13 | 42 56 79 68 70 --- 60
R19 | 3779 38 7 22 25 11 --- 11 | 44 62 80 81 55 --- 61
R20 | 3237 26 10 20 28 30 --- 11 | 38 53 66 71 55 --- 53
R21 | 1162 14 11 11 20 26 --- 9 | 53 68 66 77 53 --- 62
R22 | 959 23 14 15 37 25 --- 10 | 46 66 70 56 43 --- 58
R23 | 1018 15 10 20 18 21 150 9 | 38 40 48 44 36 78 39
R24 | 1049 39 14 10 25 14 --- 11 | 24 52 54 59 52 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 2360 43 16 25 29 36 205 |T 40 48 56 53 50 68 45
WRMS | 2360 41 11 22 28 36 205 |NE 36 46 55 53 44 59 44
MEDI | 1413 29 12 20 25 28 216 |MD 38 41 50 48 49 60 39
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