[IGSREPORT-18570] Wk 1581 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu May 13 05:15:28 PDT 2010
******************************************************************************
IGS Electronic Report 13 May 05:15:41 PDT 2010 Message Number 18570
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1581 (Apr 25, 2010 - May 01, 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 2.1581.
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:
igl1581[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1581 in the SP3 format.
igl15817.sum Combination Report for GPS Week 1581.
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 | 416.7 ns
1 | 468.9 ns
2 | 473.9 ns
3 | 477.2 ns
4 | 475.2 ns
5 | 477.9 ns
6 | 474.4 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 1.1581, 1a.1581).
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 2.1581.0-6)
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 3.1581.0-6).
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 1581 summary. (Apr 25, 2010 - May 01, 2010)
Table 1.1581.a GPS week : 1581 MJD: 55311.0-55317.0
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 124| 0 0 1 0 7 -27 -.11 30 30 | 0 -20 1694 1762
| 1 1 4 18 29 98 .06 | 0 89
cod 246| -1 0 10 46 -17 29 -.15 18 16 | --- --- --- ---
| 1 1 4 19 17 38 .02 | --- ---
esx 149| 0 0 7 -48 23 59 .45 29 26 | 128934 303 3840 7337
| 2 1 4 32 16 84 .04 | 23419 3157
iac n/a| 0 1 -31 -23 15 -89 -.11 37 37 | 466775 -514 3833 7750
| 1 1 5 33 30 213 .07 | 22141 1208
mcc n/a| 1 0 59 -36 31 -461 .50 150 150 | --- --- --- ---
| 7 13 14 105 144 280 .57 | --- ---
Table 1.1581.b GPS week : 1581 MJD: 55311.0-55317.0
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 | 11 7 11 11 13 13 10 |
R02 | 10 9 10 12 13 9 15 |
R03 | 10 9 13 10 17 16 15 |
R04 | 8 11 10 9 20 13 16 |
R05 | 8 13 9 8 10 16 13 |
R06 | --- --- --- --- 0 78 84 |
R07 | 11 8 10 9 12 14 11 |
R08 | 8 10 12 12 13 18 12 |
R10 | 20 16 19 23 27 26 21 |
R11 | 32 25 20 23 25 32 23 |
R13 | 21 18 16 17 18 18 25 |
R14 | 18 21 21 23 32 25 23 |
R15 | 19 18 15 16 25 23 23 |
R17 | 14 16 14 15 17 18 19 |
R18 | 8 16 17 18 25 18 11 |
R19 | 13 8 10 16 18 20 13 |
R20 | 10 10 12 13 23 14 13 |
R21 | 13 9 13 16 14 12 10 |
R22 | 11 15 13 14 21 18 14 |
R23 | 9 12 12 13 20 21 15 |
R24 | 9 6 14 18 17 16 11 |
Table 1.1581.c GPS week : 1581 MJD: 55311.0-55317.0
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 1581 0 | -5 10 314 -965 1098 -15590 86.4 2435 2435 | 416743 0
brd 1581 1 | 50 40 210 -816 -340 -14800 86.7 2350 2350 | 468901 0
brd 1581 2 | 0 5 282 -731 -1553 -16030 86.6 2032 2032 | 473877 0
brd 1581 3 | 13 60 243 -385 -1296 -17720 86.0 2059 2059 | 477157 0
brd 1581 4 | -79 28 186 -157 -2439 -16270 87.8 1922 1922 | 475149 0
brd 1581 5 | -30 -14 248 -45 41 -12650 87.6 2033 2033 | 477874 0
brd 1581 6 | -80 -72 196 172 -1773 -5851 86.9 1928 1928 | 474371 0
-------------+------------------------------------------------------------+----------------
brd 1581 mean| -18 8 240 -418 -894 -14130 86.9 2108 2108 | 466296 0
brd 1581 sdev| 48 43 46 430 1218 3966 .6 202 202 | 22042 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 2.1581.0 GPS week: 1581 Day: 0 MJD: 55311
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 124| 1 0 4 9 32 10 -.15 32 27 | 0 -17 1584 1652
cod 246| -1 1 6 34 -20 -20 -.14 17 13 | --- --- --- ---
esx 149| 1 0 8 -3 1 77 .43 23 20 | 78421 -182 3666 6733
iac n/a| 0 1 -30 -46 16 -44 -.06 29 29 | 417016 -1170 3684 7674
mcc n/a| 0 2 49 -2 24 -260 -.09 91 91 | --- --- --- ---
Table 2.1581.1 GPS week: 1581 Day: 1 MJD: 55312
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 124| 2 0 5 28 -28 73 -.22 27 27 | 0 122 1771 1824
cod 246| -2 -1 7 15 0 -7 -.18 16 13 | --- --- --- ---
esx 149| 0 0 7 -68 50 -11 .49 23 19 | 129823 4278 3826 6444
iac n/a| 1 3 -24 22 -2 -13 -.15 29 29 | 469103 1732 3844 6739
mcc n/a| -3 10 48 -26 -85 -38 .13 80 80 | --- --- --- ---
Table 2.1581.2 GPS week: 1581 Day: 2 MJD: 55313
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 124| 0 1 2 -14 -31 -40 -.11 25 25 | 0 -132 1708 1773
cod 246| -3 -1 8 72 10 74 -.14 18 15 | --- --- --- ---
esx 149| 0 -1 9 -41 37 105 .49 27 24 | 133537 -1628 3760 6355
iac n/a| 0 1 -28 -13 -26 -151 -.11 29 29 | 474121 -1789 3698 6880
mcc n/a| -1 4 60 64 -123 -406 .15 103 103 | --- --- --- ---
Table 2.1581.3 GPS week: 1581 Day: 3 MJD: 55314
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 124| 1 0 0 11 23 -24 -.12 23 22 | 0 69 1588 1648
cod 246| 0 0 4 55 -32 58 -.13 20 19 | --- --- --- ---
esx 149| -1 1 11 -103 24 124 .39 29 27 | 144960 3357 3710 7925
iac n/a| 0 1 -29 -28 58 -235 -.13 39 39 | 477056 483 3691 7705
mcc n/a| 12 8 82 3 251 -613 .23 116 116 | --- --- --- ---
Table 2.1581.4 GPS week: 1581 Day: 4 MJD: 55315
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 124| -1 -2 4 -16 10 36 -.08 40 40 | 0 -99 1664 1766
cod 246| 0 2 14 34 -15 59 -.17 22 22 | --- --- --- ---
esx 149| 0 0 -1 -59 7 161 .46 33 31 | 147856 2459 3927 8300
iac n/a| 2 4 -34 15 -10 -450 .01 46 46 | 476829 -1007 3950 8654
mcc n/a| -10 15 61 16 119 -935 1.56 144 144 | --- --- --- ---
Table 2.1581.5 GPS week: 1581 Day: 5 MJD: 55316
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 124| 2 -1 -1 -23 44 -16 -.03 33 33 | 0 -53 1748 1811
cod 246| 0 2 14 65 -38 44 -.16 18 16 | --- --- --- ---
esx 149| -2 0 9 -27 17 -84 .43 41 36 | 139051 -4346 3818 8473
iac n/a| 0 -1 -42 -62 44 59 -.14 46 46 | 478117 -723 3796 8712
mcc n/a| 6 -18 72 -261 140 -513 .78 205 205 | --- --- --- ---
Table 2.1581.6 GPS week: 1581 Day: 6 MJD: 55317
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 124| -2 -1 -5 1 0 -232 -.09 33 32 | 0 -33 1798 1862
cod 246| -1 0 17 46 -24 -1 -.14 18 16 | --- --- --- ---
esx 149| 3 -1 4 -35 24 45 .45 27 26 | 128891 -1813 4175 7129
iac n/a| -1 0 -33 -53 29 207 -.20 39 39 | 475184 -1129 4172 7888
mcc n/a| 6 -17 41 -48 -108 -458 .76 310 310 | --- --- --- ---
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 3.1581.0 GPS week: 1581 Day: 0 MJD: 55311
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1252 27 11 16 24 --- 11 | 20 38 42 36 --- 32
R02 | 1098 13 20 16 18 --- 10 | 22 33 23 26 --- 23
R03 | 1901 12 14 23 21 --- 10 | 24 19 27 29 --- 19
R04 | 1966 8 12 16 18 --- 8 | 32 33 25 46 --- 30
R05 | 1479 14 10 14 18 --- 8 | 37 31 29 33 --- 31
R07 | 2642 24 10 22 19 --- 10 | 33 28 36 35 --- 28
R08 | 2066 11 13 11 16 61 7 | 24 34 34 28 28 28
R10E | 990 27 27 20 57 --- 19 | 45 34 35 26 --- 26
R11E | 3945 96 28 49 37 --- 32 | 53 32 57 45 --- 37
R13E | 1525 51 27 30 37 --- 20 | 37 23 44 46 --- 29
R14E | 1358 37 21 23 42 --- 17 | 31 40 42 52 --- 33
R15E | 7418 42 19 32 40 111 18 | 34 18 34 44 27 23
R17 | 2266 23 12 17 42 --- 13 | 59 49 50 19 --- 42
R18 | 1857 14 7 18 17 --- 8 | 36 36 39 21 --- 28
R19 | 889 22 21 19 23 --- 12 | 41 53 52 43 --- 45
R20 | 1836 13 13 19 24 --- 9 | 25 36 42 41 --- 31
R21 | 1136 22 10 28 29 --- 12 | 47 54 63 43 --- 50
R22 | 972 21 9 26 19 --- 11 | 48 49 49 32 --- 41
R23 | 1679 12 9 16 26 94 9 | 33 36 37 42 36 35
R24 | 1151 13 14 19 17 --- 9 | 40 39 37 34 --- 35
------+------------------------------------+--------------------------------
RMS | 2435 32 17 23 29 91 |T 36 35 39 36 30 32
WRMS | 2435 27 13 20 29 91 |NE 34 37 39 33 32 33
MEDI | 1525 21 13 19 23 94 |MD 34 34 37 35 28 31
Table 3.1581.1 GPS week: 1581 Day: 1 MJD: 55312
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1010 8 8 12 16 --- 6 | 18 23 24 19 --- 19
R02 | 2376 10 15 8 25 --- 8 | 21 26 34 21 --- 21
R03 | 1290 18 10 17 18 --- 9 | 25 30 34 28 --- 26
R04 | 2903 17 16 21 19 --- 10 | 15 28 36 35 --- 24
R05 | 2214 18 23 26 17 --- 12 | 42 37 43 37 --- 36
R07 | 1265 15 8 16 15 --- 7 | 34 34 31 41 --- 32
R08 | 2199 15 11 25 13 74 9 | 20 21 40 25 29 23
R10E | 2829 24 19 18 47 --- 16 | 30 28 36 43 --- 23
R11E | 4016 58 26 44 45 --- 24 | 21 31 47 33 --- 26
R13E | 1367 39 27 23 32 --- 17 | 32 17 36 29 --- 20
R14E | 2774 47 19 36 44 --- 20 | 35 30 56 44 --- 34
R15E | 4257 44 16 27 34 105 17 | 37 26 33 44 54 26
R17 | 1399 28 18 25 42 --- 16 | 42 32 45 24 --- 30
R18 | 2598 24 19 31 38 --- 16 | 45 29 33 19 --- 19
R19 | 1152 18 10 13 11 --- 7 | 46 44 48 37 --- 42
R20 | 3362 16 15 10 24 --- 9 | 17 33 37 28 --- 27
R21 | 1157 9 15 14 24 --- 9 | 36 45 37 33 --- 35
R22 | 754 35 16 20 34 --- 15 | 30 28 40 17 --- 22
R23 | 2254 25 11 18 32 53 12 | 29 41 43 48 46 37
R24 | 1466 12 9 13 9 --- 6 | 28 26 31 28 --- 24
------+------------------------------------+--------------------------------
RMS | 2349 27 16 23 29 80 |T 30 30 38 31 43 27
WRMS | 2349 27 13 19 29 80 |NE 29 31 37 29 37 27
MEDI | 2199 18 15 18 24 74 |MD 30 29 36 29 46 26
Table 3.1581.2 GPS week: 1581 Day: 2 MJD: 55313
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1420 16 14 27 13 --- 10 | 22 30 32 32 --- 24
XR02 |12442 15 11 --- 15 --- 9 | 29 29 --- 40 --- 29
R03 | 1020 17 15 27 32 --- 13 | 23 23 45 41 --- 24
R04 | 2633 24 11 17 17 --- 10 | 23 24 35 32 --- 24
R05 | 2671 16 12 20 16 --- 9 | 19 33 34 32 --- 26
R07 | 1783 12 11 23 23 --- 10 | 32 28 32 29 --- 26
R08 | 1232 23 16 18 28 134 12 | 27 32 30 39 41 27
R10E | 3430 36 27 19 45 --- 18 | 47 29 33 52 --- 33
R11E | 2455 29 17 48 47 --- 20 | 30 22 60 39 --- 28
R13E | 1398 19 24 29 35 --- 15 | 28 46 45 37 --- 33
R14E | 2687 43 24 32 49 --- 21 | 31 30 35 40 --- 23
R15E | 1460 32 17 24 29 97 14 | 39 21 25 37 39 22
R17 | 609 30 15 23 25 --- 13 | 40 40 43 20 --- 31
R18 | 1818 42 22 27 22 --- 17 | 30 44 63 42 --- 40
R19 | 1742 12 15 21 19 --- 9 | 28 43 47 37 --- 36
R20 | 3913 10 22 25 24 --- 12 | 29 38 28 37 --- 29
R21 | 934 27 16 25 23 --- 13 | 30 46 61 33 --- 39
R22 | 1105 28 20 17 23 --- 13 | 53 49 44 39 --- 43
R23 | 1614 14 13 25 27 66 11 | 14 31 27 36 27 18
R24 | 891 13 15 40 23 --- 13 | 42 39 46 50 --- 38
------+------------------------------------+--------------------------------
RMS | 2032 25 18 27 29 103 |T 30 33 40 37 35 29
WRMS | 2032 25 15 24 29 103 |NE 29 35 40 35 34 30
MEDI | 1614 19 15 25 23 97 |MD 29 31 35 37 39 28
Table 3.1581.3 GPS week: 1581 Day: 3 MJD: 55314
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1722 18 14 19 27 --- 11 | 24 27 43 30 --- 25
R02 | 2034 18 11 31 19 --- 11 | 33 35 50 33 --- 33
R03 | 846 17 10 22 20 --- 9 | 31 22 28 32 --- 21
R04 | 1321 14 13 12 23 --- 8 | 25 36 36 27 --- 28
R05 | 1874 13 10 19 14 --- 8 | 48 44 55 44 --- 44
R07 | 2975 11 11 20 23 --- 9 | 50 54 60 48 --- 50
R08 | 1542 19 15 22 26 155 11 | 39 42 39 24 36 32
R10E | 3468 43 27 36 58 --- 23 | 60 31 41 60 --- 33
R11E | 2046 31 24 47 65 --- 23 | 39 26 70 55 --- 34
R13E | 1721 17 30 26 48 --- 17 | 39 49 48 30 --- 38
R14E | 3605 37 17 26 75 --- 22 | 37 30 52 40 --- 30
R15E | 1262 23 20 32 41 82 16 | 38 37 43 43 39 33
R17 | 930 24 18 19 42 --- 14 | 42 35 43 39 --- 35
R18 | 1337 38 34 19 19 --- 18 | 55 42 43 30 --- 37
R19 | 2163 24 17 29 42 --- 15 | 59 47 79 26 --- 53
R20 | 3471 9 21 33 24 --- 13 | 26 33 48 28 --- 28
R21 | 959 15 26 29 42 --- 15 | 49 60 57 45 --- 47
R22 | 1763 19 23 28 23 --- 13 | 71 64 66 57 --- 61
R23 | 1147 10 15 27 37 97 12 | 32 37 32 51 39 34
R24 | 1387 26 9 49 37 --- 18 | 32 42 89 39 --- 42
------+------------------------------------+--------------------------------
RMS | 2058 23 20 29 39 115 |T 41 39 51 39 38 36
WRMS | 2058 22 19 27 39 115 |NE 41 41 51 36 37 38
MEDI | 1721 18 17 26 27 97 |MD 39 37 48 39 39 34
Table 3.1581.4 GPS week: 1581 Day: 4 MJD: 55315
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1000 21 18 28 25 --- 13 | 24 34 52 27 --- 30
R02 | 2480 20 17 24 31 --- 13 | 40 28 43 42 --- 32
R03 | 1394 27 18 41 29 --- 17 | 26 27 66 41 --- 29
R04 | 1300 40 13 47 31 --- 19 | 27 26 61 50 --- 30
R05 | 1902 16 15 15 21 --- 9 | 27 35 33 31 --- 27
XR06 | ---- --- 9 --- --- --- 0 | --- 319 --- --- --- 324
R07 | 2425 17 17 19 28 --- 11 | 27 36 45 32 --- 29
R08 | 3184 24 14 20 37 209 13 | 27 28 40 45 28 26
R10E | 1471 75 27 40 44 --- 27 | 35 36 51 50 --- 34
R11E | 2295 68 19 33 50 --- 24 | 37 22 53 45 --- 28
R13E | 1396 29 28 28 37 --- 17 | 29 27 43 37 --- 26
R14E | 1349 73 16 32 93 --- 31 | 43 28 50 45 --- 26
R15E | 2751 28 27 49 67 70 24 | 37 38 47 38 30 25
R17 | 1283 39 18 23 39 --- 16 | 30 46 56 27 --- 36
R18 | 2291 41 41 30 61 --- 25 | 35 39 58 80 --- 30
XR19 | 959 --- 14 34 28 --- 18 | --- 26 45 19 --- 25
R20 | 2787 43 21 43 55 --- 22 | 41 55 59 72 --- 48
R21 | 710 20 14 33 25 --- 13 | 36 39 56 27 --- 35
R22 | 1706 42 29 23 52 --- 20 | 49 69 63 29 --- 49
R23 | 1191 26 28 39 45 116 19 | 25 33 58 49 21 33
R24 | 1227 19 21 29 48 --- 17 | 53 46 49 72 --- 49
------+------------------------------------+--------------------------------
RMS | 1922 40 22 33 46 144 |T 34 49 51 42 26 46
WRMS | 1922 40 22 31 46 144 |NE 33 55 52 42 24 52
MEDI | 1396 28 18 30 37 116 |MD 35 35 51 41 28 30
Table 3.1581.5 GPS week: 1581 Day: 5 MJD: 55316
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1352 16 14 28 33 --- 12 | 18 30 41 27 --- 21
R02 | 1955 16 9 17 21 --- 8 | 28 41 44 38 --- 35
R03 | 1266 15 16 45 41 --- 16 | 24 26 42 42 --- 18
R04 | 1888 26 14 30 24 --- 13 | 34 31 35 41 --- 23
R05 | 1375 20 13 53 22 --- 15 | 28 28 43 24 --- 25
XR06 | ---- 104 56 --- --- --- 77 | 39 153 --- --- --- 156
R07 | 1570 19 12 40 33 --- 14 | 35 38 66 29 --- 36
R08 | 3923 33 14 51 29 275 17 | 35 28 48 34 32 26
R10E | 1284 67 25 30 50 --- 25 | 34 37 37 54 --- 31
R11E | 1424 78 25 45 74 --- 31 | 38 26 57 57 --- 27
R13E | 1283 32 25 20 51 --- 18 | 30 40 42 53 --- 34
R14E | 778 32 21 49 82 --- 25 | 25 29 55 61 --- 26
R15E | 2693 21 27 36 77 44 23 | 31 25 50 31 36 23
R17 | 2117 38 16 47 25 --- 17 | 61 50 38 44 --- 44
R18 | 2318 27 9 57 38 --- 18 | 25 23 69 36 --- 25
R19 | 703 22 13 62 40 --- 19 | 59 36 57 48 --- 35
R20 | 4778 18 12 23 44 --- 13 | 28 40 53 57 --- 38
R21 | 1091 19 14 21 28 --- 11 | 42 54 47 36 --- 42
R22 | 1049 36 25 38 29 --- 18 | 37 52 55 44 --- 42
R23 | 1412 15 17 59 59 221 21 | 26 30 85 45 23 27
R24 | 1172 29 17 21 46 --- 15 | 46 23 46 39 --- 29
------+------------------------------------+--------------------------------
RMS | 2032 33 18 41 46 205 |T 34 40 50 42 30 36
WRMS | 2032 33 16 36 46 205 |NE 35 42 51 38 27 38
MEDI | 1375 26 16 38 38 221 |MD 34 31 47 41 32 29
Table 3.1581.6 GPS week: 1581 Day: 6 MJD: 55317
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2413 22 15 11 24 --- 10 | 29 24 31 30 --- 24
R02 | 1166 20 13 35 37 --- 15 | 27 27 39 36 --- 25
R03 | 1008 29 22 16 39 --- 15 | 23 22 24 38 --- 19
R04 | 2251 39 17 25 31 --- 15 | 38 30 41 37 --- 29
R05 | 1412 19 16 31 23 --- 13 | 27 31 58 33 --- 30
XR06 | ---- 116 59 --- --- --- 84 | 36 168 --- --- --- 170
R07 | 1049 14 14 23 25 --- 11 | 27 23 31 34 --- 23
R08 | 2848 21 12 23 26 335 11 | 32 33 37 34 35 28
R10E | 2917 48 21 34 50 --- 21 | 52 53 59 58 --- 50
R11E | 1169 57 23 33 52 --- 23 | 27 43 60 69 --- 42
R13E | 1975 67 27 25 55 --- 25 | 37 29 32 54 --- 25
R14E | 881 30 13 37 74 --- 22 | 49 28 40 51 --- 25
R15E | 1364 35 19 36 67 45 22 | 54 35 30 46 30 32
R17 | 3278 39 23 23 47 --- 18 | 78 83 65 42 --- 69
R18 | 955 23 15 17 16 --- 10 | 32 46 39 32 --- 33
R19 | 873 27 12 28 27 --- 13 | 27 40 53 27 --- 34
R20 | 3745 20 17 28 23 --- 12 | 49 34 53 32 --- 37
R21 | 1708 20 13 14 23 --- 10 | 54 69 59 56 --- 59
R22 | 1124 25 21 27 23 --- 13 | 40 59 54 34 --- 45
R23 | 823 13 21 36 32 417 15 | 26 40 60 43 13 34
R24 | 1473 26 12 19 22 --- 11 | 42 35 38 42 --- 35
------+------------------------------------+--------------------------------
RMS | 1928 33 18 27 39 310 |T 38 45 45 41 26 41
WRMS | 1928 32 16 26 39 310 |NE 36 47 45 36 24 43
MEDI | 1364 26 17 25 27 335 |MD 36 35 40 37 30 33
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