[IGSREPORT-17854] Wk 1549 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Oct 1 05:04:27 PDT 2009
******************************************************************************
IGS Electronic Report 01 Oct 05:04:55 PDT 2009 Message Number 17854
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1549 (Sep 13, 2009 - Sep 19, 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 2.1549.
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:
igl1549[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1549 in the SP3 format.
igl15497.sum Combination Report for GPS Week 1549.
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 | 230.9 ns
1 | 239.5 ns
2 | 164.7 ns
3 | 235.2 ns
4 | 235.6 ns
5 | 241.7 ns
6 | 245.2 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 1.1549, 1a.1549).
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 2.1549.0-6)
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 3.1549.0-6).
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 1549 summary. (Sep 13, 2009 - Sep 19, 2009)
Table 1.1549.a GPS week : 1549 MJD: 55087.0-55093.0
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 107| 1 0 -6 11 -23 46 -.15 28 24 | 0 450 3709 4259
| 1 1 2 18 30 83 .09 | 0 713
cod 227| -1 0 1 20 -9 75 -.14 18 14 | --- --- --- ---
| 1 0 1 28 21 20 .03 | --- ---
esx 128| 1 0 10 -18 64 -27 .49 28 24 | 138597 -885 6522 11889
| 0 1 2 24 18 79 .10 | 24186 4769
iac n/a| 0 0 -4 -33 -17 -138 -.09 25 25 | 227087 142 6453 11331
| 1 1 2 13 21 66 .11 | 26668 2580
mcc n/a| 0 5 17 7 -26 349 -.19 214 214 | --- --- --- ---
| 11 11 20 113 134 490 .34 | --- ---
Table 1.1549.b GPS week : 1549 MJD: 55087.0-55093.0
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 | 9 0 15 13 11 14 11 |
R03 | 11 11 9 10 8 11 11 |
R07 | 10 12 11 11 10 10 7 |
R08 | 15 8 11 9 11 11 15 |
R10 | 12 11 11 12 16 18 14 |
R11 | 12 8 14 13 10 11 10 |
R13 | 9 10 11 12 12 10 10 |
R14 | 11 11 9 12 9 12 16 |
R15 | 9 10 11 7 15 15 10 |
R17 | 16 9 9 12 11 17 24 |
R18 | 12 11 9 12 13 16 12 |
R19 | 19 22 12 12 15 13 21 |
R20 | 17 17 14 16 17 22 19 |
R21 | 14 12 13 9 15 17 34 |
R23 | 15 17 13 15 22 13 17 |
R24 | 13 13 24 23 17 30 30 |
Table 1.1549.c GPS week : 1549 MJD: 55087.0-55093.0
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 1549 0 | 144 16 209 1760 -5133 -5061 96.1 3215 3215 | 230882 0
brd 1549 1 |-1129 ---- -7849 -49140 -7994 83320 <<<< >>>>> >>>>> | 239459 0
brd 1549 2 | 59 34 242 -3860 -2976 -20140 89.0 3299 3299 | 164701 0
brd 1549 3 | 30 22 327 -356 -359 -15460 85.3 3242 3242 | 235226 0
brd 1549 4 | -112 -11 337 -1646 -3979 -7859 90.6 2903 2903 | 235576 0
brd 1549 5 | -73 -44 309 -1572 -609 -5457 91.1 2360 2360 | 241688 0
brd 1549 6 | 7 75 265 -2112 496 -5553 88.0 2672 2672 | 245206 0
-------------+------------------------------------------------------------+----------------
brd 1549 mean| -153 -2232 -879 -8132 -2936 3398 8.6 >>>>> >>>>> | 227534 0
brd 1549 sdev| 438 5947 3073 18163 3036 35716 215.5 >>>>> >>>>> | 28100 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 2.1549.0 GPS week: 1549 Day: 0 MJD: 55087
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 107| 1 0 -4 0 -10 -84 -.20 23 24 | 0 70 2721 3099
cod 227| -1 0 1 53 -18 87 -.17 13 12 | --- --- --- ---
esx 128| 3 -1 11 -58 69 63 .48 28 24 | 157686 -8057 5088 10282
iac n/a| 2 3 -2 -32 -22 -165 -.01 27 27 | 231059 -1950 4943 9081
mcc n/a| 7 11 48 40 -8 509 -.24 112 112 | --- --- --- ---
Table 2.1549.1 GPS week: 1549 Day: 1 MJD: 55088
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 107| 2 -2 -4 20 15 0 -.16 21 21 | 0 -59 3725 4654
cod 227| -1 0 0 -4 -21 105 -.08 12 11 | --- --- --- ---
esx 128| 1 1 12 -13 58 29 .54 30 27 | 146706 6504 8601 15962
iac n/a| 1 0 -7 -44 -26 -242 .05 24 24 | 236814 4285 8276 15479
mcc n/a| 0 10 28 53 -70 102 -.20 103 103 | --- --- --- ---
Table 2.1549.2 GPS week: 1549 Day: 2 MJD: 55089
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 107| 4 0 -9 30 -4 45 -.19 26 23 | 0 748 4578 5066
cod 227| -2 0 1 -16 -38 82 -.14 14 12 | --- --- --- ---
esx 128| 1 0 8 0 69 -23 .48 24 22 | 85004 -2468 8632 11583
iac n/a| 0 0 -2 -4 -25 -156 -.01 26 26 | 167584 -486 8627 11519
mcc n/a| 1 19 19 25 97 -80 -.57 409 409 | --- --- --- ---
Table 2.1549.3 GPS week: 1549 Day: 3 MJD: 55090
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 107| 3 -1 -8 24 -43 120 -.12 21 21 | 0 471 2756 3329
cod 227| -3 1 -1 -4 -6 84 -.12 19 16 | --- --- --- ---
esx 128| 2 1 15 10 83 -189 .46 28 25 | 148752 1680 4665 9693
iac n/a| 0 0 0 -34 -12 -103 -.09 21 21 | 233473 1881 4672 8689
mcc n/a| -16 4 0 79 74 260 -.27 296 296 | --- --- --- ---
Table 2.1549.4 GPS week: 1549 Day: 4 MJD: 55091
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 107| 0 0 -9 -7 -74 -16 -.18 25 24 | 0 -336 3187 3602
cod 227| 0 0 2 29 -16 51 -.18 21 17 | --- --- --- ---
esx 128| 1 0 9 -13 79 -33 .41 22 21 | 144887 2440 4922 10343
iac n/a| 0 1 -4 -33 -30 -30 -.11 25 25 | 234569 1849 4919 9806
mcc n/a| -7 -4 1 -151 31 1095 .47 170 170 | --- --- --- ---
Table 2.1549.5 GPS week: 1549 Day: 5 MJD: 55092
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 107| 2 0 -4 -13 -39 128 .04 36 30 | 0 412 4772 5260
cod 227| 0 0 4 47 21 57 -.14 21 14 | --- --- --- ---
esx 128| 2 0 9 -7 63 -8 .40 31 25 | 140812 -3325 7184 14179
iac n/a| 1 -1 -4 -42 -34 -165 -.14 24 24 | 240889 -2630 7187 13899
mcc n/a| 0 -15 -6 -145 -6 828 -.46 120 120 | --- --- --- ---
Table 2.1549.6 GPS week: 1549 Day: 6 MJD: 55093
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 107| 0 -2 -2 28 -5 128 -.23 41 26 | 0 1845 4225 4803
cod 227| 0 0 2 39 15 56 -.12 25 18 | --- --- --- ---
esx 128| 0 -3 8 -41 26 -32 .69 32 22 | 146334 -2974 6563 11182
iac n/a| -1 0 -7 -41 29 -107 -.29 27 27 | 245223 -1955 6551 10845
mcc n/a| 20 9 33 149 -304 -265 -.03 289 289 | --- --- --- ---
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 3.1549.0 GPS week: 1549 Day: 0 MJD: 55087
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 | 3785 --- 6 16 17 --- 9 | --- 28 35 39 --- 33
R03 | 4114 24 12 18 22 --- 10 | 19 36 41 39 --- 31
R07 | 1462 20 8 27 18 --- 10 | 26 47 59 37 --- 41
R08 | 1661 33 17 24 30 100 14 | 26 45 50 23 27 34
R10 | 4199 17 13 26 28 --- 11 | 24 37 32 24 --- 26
R11 | 3629 24 12 25 24 100 12 | 35 42 61 42 49 41
R13 | 3878 17 9 15 20 --- 8 | 22 27 31 29 --- 24
R14 | 1634 23 12 22 23 --- 11 | 23 28 42 32 --- 27
R15 | 4342 15 10 18 23 79 9 | 23 21 30 33 26 22
R17E | 2056 22 17 45 25 --- 15 | 67 69 78 68 --- 66
R18E | 2104 26 13 24 24 --- 12 | 24 22 33 36 --- 22
XR19E | 919 31 19 --- 33 --- 19 | 32 37 --- 49 --- 32
R20E | 1773 22 14 44 41 --- 17 | 27 33 66 50 --- 35
R21E | 1502 18 10 35 34 --- 13 | 70 73 76 69 --- 69
R23E | 5478 33 17 32 28 155 15 | 36 41 48 47 282 35
R24E | 3375 24 20 20 23 --- 12 | 181 210 192 203 --- 198
------+------------------------------------+--------------------------------
RMS | 3214 23 13 28 27 112 |T 42 49 58 51 96 46
WRMS | 3214 24 12 24 27 112 |NE 24 34 42 33 34 31
MEDI | 2104 23 12 24 24 100 |MD 26 37 48 39 27 33
Table 3.1549.1 GPS week: 1549 Day: 1 MJD: 55088
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR02 |>>>>> --- --- --- 14 --- 0 | --- --- --- 35 --- 41
R03 |>>>>> 25 7 29 19 --- 11 | 19 29 30 37 --- 25
R07 |>>>>> 22 19 21 24 --- 12 | 14 40 36 25 --- 28
R08 |>>>>> 12 11 14 19 89 8 | 28 21 31 26 47 22
R10 | ---- 15 10 35 22 --- 11 | 28 23 36 21 --- 20
R11 |>>>>> 13 6 26 16 94 8 | 22 29 40 33 56 26
R13 |>>>>> 24 13 20 17 --- 10 | 23 31 39 23 --- 25
R14 |>>>>> 21 8 29 22 --- 10 | 22 22 36 36 --- 23
R15 |>>>>> 18 7 20 30 76 10 | 23 22 29 36 21 23
R17E |>>>>> 17 9 20 23 --- 9 | 32 45 52 40 --- 38
R18E |>>>>> 20 13 28 23 --- 11 | 25 22 38 40 --- 24
XR19E |>>>>> 36 26 --- 31 --- 21 | 19 29 --- 37 --- 21
R20E |>>>>> 27 18 47 32 --- 16 | 28 44 72 49 --- 40
R21E |>>>>> 18 9 29 28 --- 11 | 47 54 70 54 --- 51
R23E |>>>>> 34 14 50 31 139 17 | 29 39 62 39 339 33
R24E |>>>>> 25 13 34 25 --- 12 | 162 184 167 190 --- 176
------+------------------------------------+--------------------------------
RMS |>>>>> 21 12 30 24 103 |T 34 42 52 45 115 38
WRMS |>>>>> 21 11 27 24 103 |NE 22 27 34 30 41 25
MEDI |>>>>> 21 11 28 23 89 |MD 25 29 38 36 47 25
Table 3.1549.2 GPS week: 1549 Day: 2 MJD: 55089
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 6338 35 16 16 33 --- 14 | 16 29 49 37 --- 22
R03 | 3308 20 9 18 13 --- 8 | 16 28 38 30 --- 25
R07 | 2675 12 13 23 24 --- 10 | 35 37 33 19 --- 27
R08 | 779 19 11 29 18 141 11 | 21 35 44 27 68 28
R10 | 2532 27 13 17 16 --- 10 | 22 23 24 21 --- 17
R11 | 2768 13 17 21 40 136 14 | 40 34 42 61 79 39
R13 | 1826 17 11 23 27 --- 11 | 22 31 38 24 --- 24
R14 | 1198 17 11 16 17 --- 8 | 33 24 39 35 --- 28
R15 | 3074 28 7 22 22 72 11 | 22 21 31 28 37 22
R17E | 1572 25 9 10 19 --- 9 | 45 52 59 56 --- 51
R18E | 1719 13 11 16 19 --- 8 | 22 36 43 41 --- 33
R19E | 872 18 16 23 27 --- 12 | 27 50 187 49 --- 41
R20E | 2932 26 13 33 26 --- 14 | 32 40 60 45 --- 40
R21E | 3107 21 14 29 26 --- 12 | 69 77 73 76 --- 70
R23E | 7423 18 11 32 27 792 12 | 39 35 45 33 497 32
R24E | 2728 63 27 40 38 --- 24 | 76 125 149 109 --- 114
------+------------------------------------+--------------------------------
RMS | 3299 26 14 24 26 409 |T 33 42 59 43 170 38
WRMS | 3299 23 12 22 26 409 |NE 25 29 37 31 61 25
MEDI | 2675 19 11 22 24 136 |MD 27 35 43 35 68 28
Table 3.1549.3 GPS week: 1549 Day: 3 MJD: 55090
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 4356 18 26 30 16 --- 13 | 14 30 47 49 --- 35
R03 | 6959 18 13 26 13 --- 10 | 24 35 36 31 --- 28
R07 | 4277 19 12 26 17 --- 10 | 26 39 57 46 --- 39
R08 | 1027 15 6 28 12 123 9 | 41 32 61 40 45 40
R10 | 2800 17 17 29 18 --- 11 | 33 45 50 44 --- 39
R11 | 2013 20 14 29 24 112 12 | 42 43 71 47 47 46
R13 | 2203 14 13 34 22 --- 12 | 37 46 72 31 --- 42
R14 | 1933 25 15 26 18 --- 12 | 18 28 37 32 --- 24
R15 | 3115 13 6 14 16 92 7 | 40 35 40 54 33 40
R17E | 1126 20 18 21 20 --- 11 | 58 63 56 51 --- 55
R18E | 992 19 17 17 26 --- 11 | 41 41 53 60 --- 44
R19E | 669 23 17 21 18 --- 11 | 27 44 186 41 --- 36
R20E | 1295 34 17 36 23 --- 16 | 44 54 67 58 --- 52
R21E | 1361 14 15 19 16 --- 9 | 57 64 73 56 --- 61
R23E | 4979 29 20 21 29 560 14 | 26 45 41 43 300 34
R24E | 4489 24 43 55 34 --- 23 | 149 149 114 121 --- 131
------+------------------------------------+--------------------------------
RMS | 3241 21 19 28 21 296 |T 42 49 66 50 106 46
WRMS | 3241 21 16 25 21 296 |NE 30 37 52 41 41 37
MEDI | 2013 19 15 26 18 112 |MD 37 43 56 46 45 40
Table 3.1549.4 GPS week: 1549 Day: 4 MJD: 55091
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 3430 21 12 22 16 --- 10 | 15 28 38 27 --- 25
R03 | 7684 15 14 12 14 --- 8 | 22 23 34 22 --- 21
R07 | 3108 15 13 16 25 --- 10 | 31 26 34 24 --- 25
R08 | 846 13 18 21 19 79 10 | 19 29 34 37 38 25
R10 | 4062 22 35 25 24 --- 16 | 34 38 39 30 --- 30
R11 | 1842 14 19 17 19 59 10 | 43 35 50 36 47 39
R13 | 1367 14 13 24 26 --- 11 | 24 36 38 43 --- 32
R14 | 2999 13 10 14 21 --- 9 | 42 38 43 31 --- 35
R15 | 2063 25 19 27 29 144 14 | 22 25 48 31 33 25
R17E | 868 21 11 15 26 --- 11 | 45 49 54 52 --- 46
R18E | 1428 29 21 16 20 --- 12 | 36 41 54 48 --- 42
R19E | 751 27 27 24 20 --- 14 | 47 65 134 52 --- 57
R20E | 1043 34 19 32 29 --- 16 | 53 60 72 60 --- 58
R21E | 1917 19 32 16 30 --- 14 | 78 89 76 60 --- 73
R23E | 1628 53 28 32 32 293 21 | 29 44 36 39 174 29
R24E | 2796 34 24 17 36 --- 16 | 95 109 129 138 --- 114
------+------------------------------------+--------------------------------
RMS | 2902 25 21 21 25 170 |T 39 45 57 45 73 42
WRMS | 2902 24 17 21 25 170 |NE 28 30 39 31 39 28
MEDI | 1842 21 19 17 24 79 |MD 34 38 43 37 38 32
Table 3.1549.5 GPS week: 1549 Day: 5 MJD: 55092
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 2664 25 13 37 22 --- 13 | 30 30 68 27 --- 34
R03 | 5305 18 10 33 16 --- 11 | 21 21 43 30 --- 24
R07 | 2475 24 9 16 18 --- 9 | 23 21 26 25 --- 19
R08 | 698 8 15 28 21 73 11 | 33 24 45 30 37 26
R10 | 4060 36 36 20 26 --- 18 | 17 38 34 27 --- 24
R11 | 1453 16 8 26 24 45 11 | 35 34 51 28 40 31
R13 | 792 12 15 22 19 --- 10 | 28 29 44 34 --- 30
R14 | 1980 17 14 24 24 --- 11 | 26 22 33 21 --- 19
R15 | 903 18 26 26 26 149 14 | 31 41 54 41 40 38
R17E | 1873 26 20 38 35 --- 17 | 54 65 71 48 --- 55
R18E | 1203 32 27 32 22 --- 16 | 36 50 63 57 --- 44
R19E | 747 33 11 27 16 --- 12 | 31 41 137 38 --- 37
R20E | 2160 64 24 45 20 --- 22 | 40 63 81 55 --- 57
R21E | 1160 57 19 24 14 --- 17 | 71 82 82 80 --- 75
R23E | 1278 26 15 28 25 168 13 | 27 40 39 34 286 32
R24E | 3185 81 39 49 44 --- 30 | 181 224 229 221 --- 211
------+------------------------------------+--------------------------------
RMS | 2360 36 21 31 24 120 |T 42 51 68 49 100 47
WRMS | 2360 30 14 25 24 120 |NE 27 28 44 29 39 27
MEDI | 1453 25 15 27 22 73 |MD 31 38 51 34 40 32
Table 3.1549.6 GPS week: 1549 Day: 6 MJD: 55093
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 | 1554 11 22 24 15 --- 11 | 16 26 28 21 --- 21
R03 | 8410 16 16 23 22 --- 11 | 27 33 45 26 --- 28
R07 | 1848 18 9 8 14 --- 7 | 17 29 31 41 --- 27
R08 | 853 29 18 15 37 103 15 | 32 27 36 36 48 23
R10 | 2945 31 20 25 22 --- 14 | 23 36 48 43 --- 35
R11 | 950 17 12 19 18 117 9 | 41 41 55 32 72 40
R13 | 785 17 15 19 16 --- 9 | 34 34 44 33 --- 34
R14 | 1603 31 20 30 32 --- 16 | 39 31 46 22 --- 27
R15 | 1981 19 14 14 23 96 10 | 23 27 36 35 73 28
R17E | 1881 44 15 62 39 --- 24 | 65 78 110 72 --- 75
R18E | 995 27 16 17 23 --- 12 | 50 60 72 57 --- 57
R19E | 760 45 27 46 27 --- 20 | 47 81 219 72 --- 75
R20E | 3201 47 27 32 26 --- 19 | 62 69 88 77 --- 70
R21 | 898 76 57 53 50 --- 34 | 120 157 148 103 --- 125
R23E | 909 26 25 39 23 548 16 | 42 50 71 58 398 51
R24E | 1797 99 45 27 23 --- 30 | 129 204 191 191 --- 181
------+------------------------------------+--------------------------------
RMS | 2671 41 25 32 27 289 |T 47 61 79 57 147 56
WRMS | 2671 26 18 22 27 289 |NE 28 31 41 32 64 29
MEDI | 1554 27 18 24 23 103 |MD 39 36 48 41 72 35
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