[IGSREPORT-17805] Wk 1547 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Sep 17 04:51:26 PDT 2009
******************************************************************************
IGS Electronic Report 17 Sep 04:51:52 PDT 2009 Message Number 17805
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1547 (Aug 30, 2009 - Sep 05, 2009)
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 2.1547.
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:
igl1547[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1547 in the SP3 format.
igl15477.sum Combination Report for GPS Week 1547.
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 | 158.9 ns
1 | 218.2 ns
2 | 95.1 ns
3 | 217.9 ns
4 | 216.6 ns
5 | 161.9 ns
6 | 219.1 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 1.1547, 1a.1547).
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 2.1547.0-6)
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 3.1547.0-6).
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 1547 summary. (Aug 30, 2009 - Sep 05, 2009)
Table 1.1547.a GPS week : 1547 MJD: 55073.0-55079.0
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 108| 1 -1 -6 10 -10 3 -.16 35 35 | 0 1 3013 3445
| 1 2 3 32 47 199 .04 | 0 525
cod 228| -2 0 3 12 -12 138 -.20 18 16 | --- --- --- ---
| 1 1 2 28 10 35 .06 | --- ---
esx 138| 0 1 9 -47 23 -59 .43 29 26 | 109892 1125 5669 10400
| 2 2 2 29 17 77 .07 | 49784 3859
iac n/a| 1 0 -8 -2 2 -197 .01 35 35 | 183718 131 5595 10072
| 1 1 3 37 26 67 .08 | 48969 2625
mcc n/a| 0 0 43 25 -4 516 -.11 99 99 | --- --- --- ---
| 7 3 12 55 53 327 .35 | --- ---
Table 1.1547.b GPS week : 1547 MJD: 55073.0-55079.0
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
------+------------------------------------+------------------------------------------
R02 | 8 8 12 10 11 9 13 |
R03 | 12 11 9 10 10 13 12 |
R07 | 12 10 13 17 15 16 12 |
R08 | 15 12 11 9 17 14 12 |
R10 | 15 12 10 12 21 15 14 |
R11 | 14 18 16 14 13 15 13 |
R13 | 10 10 9 11 13 13 9 |
R14 | 16 10 12 14 14 13 14 |
R15 | 11 10 9 12 11 11 11 |
R17 | 17 18 17 23 25 25 24 |
R18 | 22 17 18 18 20 22 20 |
R19 | 20 17 13 19 19 23 29 |
R20 | 21 18 18 22 21 25 27 |
R21 | 21 22 23 22 23 20 16 |
R22 | 20 157 --- --- --- --- --- |
R23 | 26 22 30 22 26 25 23 |
R24 | 16 13 17 16 14 16 12 |
Table 1.1547.c GPS week : 1547 MJD: 55073.0-55079.0
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 1547 0 | 42 38 342 -2487 -266 -11970 90.6 2941 2941 | 158926 0
brd 1547 1 | 2830 ---- 1897 -100200 -8413 52750 128.0 >>>>> >>>>> | 218160 0
brd 1547 2 | -29 6 230 -2585 -1149 -1423 88.6 2671 2671 | 95091 0
brd 1547 3 | -192 44 309 345 -601 5957 92.9 2673 2673 | 217859 0
brd 1547 4 | 37 -89 114 1116 2541 4721 93.7 2871 2871 | 216629 0
brd 1547 5 | -81 -130 305 1768 -682 1133 91.5 3803 3803 | 161915 0
brd 1547 6 | 68 -36 374 -2656 -1692 4644 89.1 4496 4496 | 219148 0
-------------+------------------------------------------------------------+----------------
brd 1547 mean| 382 -1781 510 -14956 -1466 7973 96.3 >>>>> >>>>> | 183961 0
brd 1547 sdev| 1083 4638 617 37635 3348 20670 14.1 >>>>> >>>>> | 47670 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 2.1547.0 GPS week: 1547 Day: 0 MJD: 55073
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 108| 1 -1 -10 4 -4 191 -.20 37 37 | 0 -940 3270 3772
cod 228| -1 0 4 -17 -17 92 -.12 17 15 | --- --- --- ---
esx 138| -3 1 8 -14 8 -93 .43 33 33 | 70953 7333 7518 11898
iac n/a| 1 0 -3 5 56 -196 -.04 33 33 | 154350 4146 7541 12220
mcc n/a| 5 -2 53 8 -71 -12 -.25 94 94 | --- --- --- ---
Table 2.1547.1 GPS week: 1547 Day: 1 MJD: 55074
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 108| 2 -5 -8 -20 -33 -25 -.17 29 29 | 0 377 2889 3212
cod 228| -2 0 1 44 -4 128 -.18 17 13 | --- --- --- ---
esx 138| -4 1 13 -72 25 -48 .48 27 24 | 146612 283 5226 8912
iac n/a| 2 -1 -7 9 -6 -217 -.07 32 32 | 219743 -3270 5215 8933
mcc n/a| 1 2 42 59 -27 130 .13 86 86 | --- --- --- ---
Table 2.1547.2 GPS week: 1547 Day: 2 MJD: 55075
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 108| 1 -1 -2 29 18 -102 -.15 37 34 | 0 227 2735 3148
cod 228| -3 2 7 -10 -1 175 -.16 16 13 | --- --- --- ---
esx 138| 0 -3 6 -43 12 -35 .37 32 27 | 20161 5192 4855 10139
iac n/a| 0 0 -14 21 -22 -189 .06 30 30 | 93437 2506 4845 9173
mcc n/a| -3 2 21 -79 53 694 .28 104 104 | --- --- --- ---
Table 2.1547.3 GPS week: 1547 Day: 3 MJD: 55076
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 108| 1 0 -2 62 30 -37 -.17 32 32 | 0 -52 4459 5289
cod 228| -1 2 1 -15 -1 149 -.17 18 14 | --- --- --- ---
esx 138| 0 0 10 -90 18 -14 .43 31 27 | 147043 -764 4979 9817
iac n/a| 0 -2 -6 38 -9 -261 .06 35 35 | 217770 591 4988 9923
mcc n/a| -7 0 51 72 -65 580 -.02 131 131 | --- --- --- ---
Table 2.1547.4 GPS week: 1547 Day: 4 MJD: 55077
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 108| 0 1 -4 -34 52 231 -.09 37 37 | 0 -398 2816 3172
cod 228| -4 -2 5 45 -25 102 -.24 21 20 | --- --- --- ---
esx 138| 2 0 5 -51 7 -129 .38 33 29 | 139371 1277 6320 9548
iac n/a| 3 -2 -9 -27 15 -265 .06 34 34 | 216292 75 6125 9287
mcc n/a| -7 -6 58 44 19 875 -.76 94 94 | --- --- --- ---
Table 2.1547.5 GPS week: 1547 Day: 5 MJD: 55078
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 108| -1 0 -7 22 -60 118 -.19 35 34 | 0 177 2174 2499
cod 228| -3 -1 0 9 -21 130 -.23 22 19 | --- --- --- ---
esx 138| 4 4 11 -54 46 -162 .37 26 23 | 96237 -3179 5468 10592
iac n/a| 0 1 -11 12 1 -188 .11 44 44 | 162958 -2583 5320 9148
mcc n/a| 3 1 39 78 62 676 .11 89 89 | --- --- --- ---
Table 2.1547.6 GPS week: 1547 Day: 6 MJD: 55079
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 108| 3 -1 -7 8 -75 -350 -.17 39 39 | 0 622 2754 3027
cod 228| -1 -1 2 35 -18 189 -.29 19 16 | --- --- --- ---
esx 138| 0 1 8 -6 48 70 .55 23 21 | 148867 -2262 5321 11896
iac n/a| 0 0 -8 -74 -17 -63 -.08 36 36 | 221478 -542 5137 11820
mcc n/a| 11 1 39 -1 1 672 -.23 96 96 | --- --- --- ---
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 3.1547.0 GPS week: 1547 Day: 0 MJD: 55073
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1664 13 9 19 18 --- 8 | 38 28 25 17 --- 25
R03 | 5300 22 12 28 23 --- 11 | 38 34 33 25 --- 29
R07 | 3963 25 12 20 28 --- 12 | 32 32 34 28 --- 26
R08 | 2011 47 19 16 17 103 15 | 38 35 33 20 32 27
R10 | 1564 26 16 37 26 --- 14 | 30 23 27 38 --- 22
R11 | 1230 21 17 32 29 106 14 | 34 27 36 25 22 24
R13 | 847 16 15 18 21 --- 10 | 32 23 20 31 --- 21
R14 | 1072 27 20 44 17 --- 15 | 33 20 31 25 --- 19
R15 | 1865 19 13 28 18 57 11 | 27 17 25 25 18 16
R17E | 945 19 17 34 43 --- 16 | 48 30 46 47 --- 32
R18E | 1379 64 19 36 40 --- 22 | 40 26 43 42 --- 30
R19E | 1396 36 22 35 47 --- 19 | 39 36 50 56 --- 36
R20E | 1722 46 23 40 45 --- 21 | 32 21 39 45 --- 25
R21E | 2117 47 24 41 42 --- 21 | 41 36 46 57 --- 31
R22E | 2557 52 19 26 42 --- 19 | 5 111 5 27 --- 109
R23E | 8216 63 18 53 51 103 25 | 42 42 43 62 48 37
R24E | 933 28 16 39 27 --- 15 | 28 36 55 32 --- 30
------+------------------------------------+--------------------------------
RMS | 2941 37 17 33 33 94 |T 33 33 34 35 30 31
WRMS | 2941 37 15 33 33 94 |NE 33 26 29 26 24 23
MEDI | 1664 27 17 34 28 103 |MD 34 30 34 31 22 27
Table 3.1547.1 GPS week: 1547 Day: 1 MJD: 55074
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 12 11 17 16 --- 8 | 17 27 26 19 --- 21
R03 |>>>>> 30 13 10 23 --- 11 | 42 31 35 29 --- 32
R07 |>>>>> 19 12 22 17 --- 10 | 26 30 57 36 --- 35
R08 |>>>>> 25 13 27 17 82 11 | 21 25 56 23 17 28
R10 |10492 15 13 27 24 --- 11 | 31 32 34 24 --- 25
R11 |>>>>> 33 17 35 41 111 18 | 16 15 45 15 15 15
R13 |>>>>> 14 9 17 27 --- 9 | 23 24 34 15 --- 20
R14 |11015 19 12 15 22 --- 9 | 26 26 40 32 --- 27
R15 |>>>>> 19 12 24 15 55 10 | 19 17 29 20 15 17
R17E |>>>>> 33 19 30 46 --- 18 | 21 18 27 46 --- 15
R18E |>>>>> 28 22 29 41 --- 17 | 36 23 38 42 --- 26
R19E |>>>>> 26 24 20 44 --- 16 | 32 53 30 52 --- 45
R20E |>>>>> 35 19 31 40 --- 17 | 24 17 33 33 --- 18
R21E |>>>>> 56 26 28 40 --- 21 | 37 44 57 56 --- 41
XR22E |22947 --- 62 --- 257 --- 156 | --- 93 --- 23 --- 114
R23E |>>>>> 46 17 46 46 88 22 | 52 36 48 50 43 37
R24E |>>>>> 20 18 26 28 --- 13 | 17 26 43 37 --- 22
------+------------------------------------+--------------------------------
RMS |>>>>> 29 17 27 32 86 |T 27 31 39 32 22 31
WRMS |>>>>> 29 13 24 32 86 |NE 24 25 39 23 15 24
MEDI |>>>>> 25 17 26 28 82 |MD 24 26 35 32 15 26
Table 3.1547.2 GPS week: 1547 Day: 2 MJD: 55075
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1802 22 11 28 24 --- 11 | 47 41 43 34 --- 37
R03 | 3822 22 9 19 18 --- 9 | 21 30 41 28 --- 26
R07 | 5622 25 14 32 19 --- 12 | 27 37 59 38 --- 36
R08 | 1507 28 15 25 13 120 11 | 18 36 37 24 34 25
R10 | 1751 23 10 16 19 --- 9 | 32 29 39 33 --- 29
R11 | 1868 32 15 41 27 108 16 | 20 24 54 21 26 23
R13 | 1418 18 11 18 19 --- 9 | 33 27 33 38 --- 29
R14 | 3504 22 15 23 22 --- 11 | 24 27 35 23 --- 22
R15 | 2020 12 9 18 20 65 8 | 17 22 33 32 27 21
R17E | 1817 49 13 30 31 --- 17 | 34 21 25 45 --- 23
R18E | 2620 34 17 33 42 --- 17 | 24 13 42 42 --- 19
R19E | 1807 15 13 21 38 --- 13 | 38 27 24 38 --- 29
R20E | 1964 41 16 43 27 --- 17 | 25 30 58 32 --- 27
R21E | 860 67 25 29 42 --- 23 | 36 38 38 52 --- 32
R23E | 2147 73 26 69 49 113 29 | 57 46 81 56 42 39
R24E | 3848 42 18 26 36 --- 17 | 31 41 45 26 --- 27
------+------------------------------------+--------------------------------
RMS | 2670 37 16 32 30 104 |T 30 30 42 35 32 27
WRMS | 2670 34 13 27 30 104 |NE 26 30 41 30 29 27
MEDI | 1868 25 14 26 24 108 |MD 27 29 39 33 27 27
Table 3.1547.3 GPS week: 1547 Day: 3 MJD: 55076
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2585 23 9 17 24 --- 10 | 38 29 35 28 --- 29
R03 | 5805 23 13 15 21 --- 10 | 54 55 50 46 --- 50
R07 | 1957 24 23 34 36 --- 16 | 38 36 49 63 --- 38
R08 | 1032 17 7 17 21 135 8 | 40 40 43 43 57 37
R10 | 1170 30 11 13 29 --- 12 | 34 38 30 51 --- 33
R11 | 2381 23 15 31 27 131 13 | 26 35 52 30 31 30
R13 | 1418 17 14 26 22 --- 11 | 31 25 39 36 --- 27
R14 | 2087 23 12 40 19 --- 14 | 47 37 44 43 --- 36
R15 | 1658 14 13 22 31 46 11 | 29 25 37 32 36 24
R17E | 1240 55 34 25 42 --- 23 | 44 35 41 61 --- 34
R18E | 3243 31 23 25 46 --- 18 | 32 23 35 53 --- 26
R19E | 2647 35 14 34 52 --- 19 | 49 59 30 91 --- 62
R20E | 4228 47 24 40 42 --- 21 | 27 35 47 43 --- 31
R21E | 952 39 26 44 43 --- 21 | 30 35 57 42 --- 31
R23E | 1742 50 22 42 44 175 22 | 50 47 52 57 86 40
R24E | 3461 27 9 45 28 --- 16 | 22 52 88 37 --- 46
------+------------------------------------+--------------------------------
RMS | 2673 32 18 31 35 130 |T 36 37 45 47 52 35
WRMS | 2673 32 14 27 35 130 |NE 37 35 42 41 41 33
MEDI | 1957 24 14 26 29 131 |MD 34 35 43 43 36 33
Table 3.1547.4 GPS week: 1547 Day: 4 MJD: 55077
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2586 29 14 11 21 --- 11 | 42 47 42 47 --- 41
R03 | 5155 23 12 16 17 --- 9 | 38 40 35 24 --- 32
R07 | 3907 29 23 23 29 --- 15 | 31 39 40 28 --- 27
R08 | 1724 26 26 35 28 105 16 | 28 46 38 38 58 33
R10 | 977 39 19 59 21 --- 20 | 32 31 52 40 --- 25
R11 | 1341 28 11 25 25 106 12 | 23 28 36 31 40 23
R13 | 1427 18 16 27 31 --- 13 | 33 33 50 32 --- 30
R14 | 2397 27 17 25 29 --- 14 | 25 28 26 27 --- 21
R15 | 1713 16 18 20 23 46 11 | 24 30 37 38 32 28
R17E | 1078 65 30 39 44 --- 25 | 46 24 56 56 --- 32
R18E | 3048 29 24 29 54 --- 20 | 36 35 54 64 --- 36
XR19E | 2536 32 20 --- 31 --- 19 | 31 39 --- 56 --- 35
R20E | 1771 52 21 39 33 --- 20 | 29 24 50 42 --- 28
R21E | 1386 39 32 31 57 --- 23 | 28 31 33 32 --- 23
R23E | 2076 64 21 54 47 106 26 | 35 44 58 54 74 38
R24E | 6228 35 13 29 22 --- 14 | 33 42 48 36 --- 36
------+------------------------------------+--------------------------------
RMS | 2870 37 21 33 34 94 |T 32 35 43 40 51 30
WRMS | 2870 37 20 29 34 94 |NE 30 35 39 33 43 28
MEDI | 1771 29 19 29 29 105 |MD 31 33 42 38 40 30
Table 3.1547.5 GPS week: 1547 Day: 5 MJD: 55078
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1013 16 10 16 20 --- 8 | 31 31 44 29 --- 31
R03 | 5865 21 19 24 25 --- 13 | 48 50 44 54 --- 45
R07 | 5257 32 29 18 33 --- 16 | 19 42 39 32 --- 27
R08 | 2807 22 19 14 44 86 14 | 45 50 46 36 32 43
R10 | 1874 24 19 26 39 --- 15 | 25 26 50 42 --- 29
R11 | 1152 19 16 18 54 84 15 | 27 29 34 45 32 26
R13 | 1732 14 14 22 38 --- 12 | 31 27 34 27 --- 24
R14 | 1697 23 11 27 29 --- 13 | 30 29 44 34 --- 30
R15 | 3599 8 18 20 22 45 10 | 27 34 28 37 36 27
R17E | 770 62 31 16 63 --- 24 | 21 31 30 58 --- 23
R18E | 1532 40 26 33 62 --- 22 | 40 36 62 67 --- 41
XR19E | 2467 26 23 --- 53 --- 23 | 37 42 --- 63 --- 39
R20E | 2278 46 30 40 61 --- 24 | 24 50 76 60 --- 45
R21E | 2982 43 28 15 55 --- 20 | 39 27 35 37 --- 25
R23E | 3391 54 24 47 50 122 25 | 31 41 68 60 36 41
R24E | 9682 41 17 23 27 --- 15 | 25 30 43 45 --- 32
------+------------------------------------+--------------------------------
RMS | 3802 35 22 26 44 89 |T 31 35 45 45 34 33
WRMS | 3802 34 19 23 44 89 |NE 31 35 40 37 33 31
MEDI | 2278 24 19 22 39 84 |MD 30 31 44 42 32 30
Table 3.1547.6 GPS week: 1547 Day: 6 MJD: 55079
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2166 20 20 24 26 --- 13 | 46 43 37 36 --- 36
R03 | 7782 18 15 26 21 --- 12 | 32 42 39 38 --- 34
R07 | 4445 33 16 14 16 --- 11 | 23 50 42 45 --- 36
R08 | 3852 22 17 10 33 76 11 | 35 52 46 41 36 42
R10 | 3703 32 24 18 27 --- 14 | 30 28 25 35 --- 19
R11 | 2081 25 12 27 24 89 12 | 19 41 50 25 33 32
R13 | 2865 24 14 10 11 --- 8 | 40 32 40 31 --- 33
R14 | 1317 28 16 30 21 --- 13 | 30 34 35 27 --- 25
R15 | 3550 17 11 21 28 61 11 | 26 31 38 44 36 29
R17E | 1090 61 26 38 49 --- 24 | 34 35 44 59 --- 35
R18E | 1419 59 19 17 47 --- 20 | 26 41 43 58 --- 37
XR19E | 2472 43 23 --- 60 --- 29 | 36 34 --- 58 --- 33
R20E | 5549 75 24 32 59 --- 26 | 27 39 53 70 --- 35
R21E | 2471 38 21 15 40 --- 16 | 34 34 34 39 --- 27
R23E | 9095 44 24 28 62 140 22 | 39 39 48 73 37 40
R24E | 6316 24 18 14 30 --- 12 | 47 54 52 47 --- 49
------+------------------------------------+--------------------------------
RMS | 4495 39 19 23 36 96 |T 32 39 41 45 35 33
WRMS | 4495 39 16 21 36 96 |NE 31 39 39 35 35 31
MEDI | 2865 28 18 21 28 76 |MD 32 39 42 41 36 34
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