[IGSREPORT-16062] Wk 1469 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Fri Mar 21 05:02:28 PDT 2008
******************************************************************************
IGS Electronic Report 21 Mar 05:02:35 PDT 2008 Message Number 16062
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1469 (Mar 02, 2008 - Mar 08, 2008)
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 2.1469.
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:
igl1469[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1469 in the SP3 format.
igl14697.sum Combination Report for GPS Week 1469.
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 | 1247.5 ns
1 | 1251.5 ns
2 | 1190.9 ns
3 | 1256.3 ns
4 | 1200.7 ns
5 | 1160.4 ns
6 | 1152.9 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
----+--------+---------------
0 | COD | R17
1 | ESX | R08 R13
3 | ESX | R08 R09 R15
4 | ESX | R09
5 | ESX | R11 R15
5 | IAC | R04 R07 R13
6 | ESX | R09
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 1.1469, 1a.1469).
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 2.1469.0-6)
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 3.1469.0-6).
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 1469 summary. (Mar 02, 2008 - Mar 08, 2008)
Table 1.1469.a GPS week : 1469 MJD: 54527.0-54533.0
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 66| 1 0 0 -27 -13 25 -.11 33 33 | 0 211 2407 2477
| 1 2 5 24 31 155 .07 | 0 267
cod 173| 0 1 1 24 0 25 -.07 28 27 | --- --- --- ---
| 1 2 3 24 40 70 .07 | --- ---
esx 107| 0 0 2 93 -30 -1 .39 374 66 | -71787 -4003 7032 13906
| 7 5 7 89 130 144 .15 | 52135 3941
iac n/a| 0 -2 -3 -60 -17 -131 .03 87 87 | 1208105 -1017 6596 13828
| 6 4 7 53 51 197 .08 | 44419 3855
mcc n/a| 56 5 -24 -206 -279 -2560 1.55 639 639 | --- --- --- ---
| 64 17 107 1067 1043 4572 2.16 | --- ---
Table 1.1469.b GPS week : 1469 MJD: 54527.0-54533.0
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 16 22 15 20 27 21 |
R04 | 14 15 15 16 18 43 106 |
R06 | 18 19 20 19 22 23 38 |
R07 | 25 18 24 29 22 23 34 |
R08 | 27 24 16 16 38 35 37 |
R09 | 28 18 29 17 14 26 23 |
R10 | 19 12 17 18 21 58 20 |
R11 | 36 20 23 20 19 44 43 |
R13 | 21 20 28 23 19 19 122 |
R14 | 13 21 16 16 12 38 40 |
R15 | 23 21 23 23 30 28 24 |
R17E | 94 30 28 20 30 68 32 |
R19E | 21 16 27 18 18 19 24 |
R20E | 20 23 20 26 32 24 20 |
R23E | 26 15 29 33 25 23 21 |
R24E | 15 16 21 22 22 32 22 |
Table 1.1469.c GPS week : 1469 MJD: 54527.0-54533.0
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 1469 0 | 209 307 361 -4713 6083 -17310 93.7 5139 5139 | 1247472 0
brd 1469 1 | -166 14 362 -3318 408 -14020 97.7 5911 5911 | 1251515 0
brd 1469 2 | 30 -36 74 16 1736 -15430 99.9 6300 6300 | 1190903 0
brd 1469 3 | -91 -145 363 -4102 -606 -18080 93.6 6103 6103 | 1256339 0
brd 1469 4 | 290 23 456 310 -177 -20090 91.2 5531 5531 | 1200712 0
brd 1469 5 | 131 371 423 -2944 1323 -25040 100.6 8270 8270 | 1160403 0
brd 1469 6 | -254 101 137 921 1975 -12530 101.1 7578 7578 | 1152864 0
-------------+------------------------------------------------------------+----------------
brd 1469 mean| 21 91 311 -1975 1534 -17500 96.8 6404 6404 | 1208601 0
brd 1469 sdev| 201 186 145 2321 2226 4183 4.0 1123 1123 | 43658 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 2.1469.0 GPS week: 1469 Day: 0 MJD: 54527
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 66| -1 -1 7 -9 0 -165 -.09 24 25 | 0 49 2295 2372
cod 173| 0 0 2 48 22 33 -.04 27 24 | --- --- --- ---
esx 107| 8 -4 0 82 -121 91 .25 79 45 | -25376 2352 6678 14966
iac n/a| -7 -1 -12 -81 -66 126 .06 44 44 | 1246345 -857 6364 14769
mcc n/a| -6 -2 25 -25 40 1625 -.78 112 112 | --- --- --- ---
Table 2.1469.1 GPS week: 1469 Day: 1 MJD: 54528
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 66| 0 -1 2 -11 -52 126 -.14 27 26 | 0 266 2360 2441
cod 173| 2 0 6 0 65 -26 -.07 22 22 | --- --- --- ---
esx 107| 9 -8 -5 19 -15 -67 .37 153 56 | -15217 -9424 7529 13907
iac n/a| -1 1 -12 -50 -41 -6 .02 32 32 | 1253855 -8655 6676 13276
mcc n/a| 4 -3 16 -103 -163 2304 -1.02 138 138 | --- --- --- ---
Table 2.1469.2 GPS week: 1469 Day: 2 MJD: 54529
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 66| 1 -2 0 -36 46 55 -.07 28 29 | 0 0 2731 2814
cod 173| 0 0 -3 43 -42 -7 -.06 20 21 | --- --- --- ---
esx 107| 8 4 5 0 -228 -7 .20 91 73 | -88989 -3209 8156 15159
iac n/a| -3 2 4 -36 66 -63 .05 45 45 | 1187640 1422 7667 14924
mcc n/a| 49 32 -28 420 -233 1136 1.03 315 315 | --- --- --- ---
Table 2.1469.3 GPS week: 1469 Day: 3 MJD: 54530
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 66| 1 0 -7 -64 -27 72 -.07 31 28 | 0 -125 2245 2299
cod 173| 0 3 -1 49 17 36 -.09 23 22 | --- --- --- ---
esx 107| -6 0 16 62 -78 219 .42 246 81 | -24026 -3461 6290 12996
iac n/a| -2 -2 8 -36 -21 -332 -.03 43 43 | 1254984 -1344 6196 13381
mcc n/a| 148 -14 -102 -2161 953 -4158 1.81 563 563 | --- --- --- ---
Table 2.1469.4 GPS week: 1469 Day: 4 MJD: 54531
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 66| 1 1 4 -31 -6 -217 -.14 38 33 | 0 640 2593 2661
cod 173| -1 0 2 28 -36 128 -.17 30 28 | --- --- --- ---
esx 107| -4 6 6 66 87 -81 .51 148 51 | -76785 -6848 5723 13650
iac n/a| -1 -3 -5 -17 -14 11 -.01 36 36 | 1203950 -958 5362 13871
mcc n/a| -2 -10 0 4 -264 -5565 1.28 1138 1138 | --- --- --- ---
Table 2.1469.5 GPS week: 1469 Day: 5 MJD: 54532
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 66| 4 -3 -5 8 -27 112 -.25 40 39 | 0 454 2242 2311
cod 173| -1 4 4 2 12 89 -.10 28 29 | --- --- --- ---
esx 107| -4 1 -3 257 163 -229 .62 863 79 | -129312 -6385 5395 11090
iac n/a| 13 0 -2 -174 -78 -262 .18 254 254 | 1156601 3950 5306 11429
mcc n/a| 64 14 -211 1255 -2449 ---- 3.64 1671 1671 | --- --- --- ---
Table 2.1469.6 GPS week: 1469 Day: 6 MJD: 54533
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 66| 3 3 -4 -44 -27 194 -.02 46 50 | 0 198 2385 2443
cod 173| -1 4 -1 -3 -35 -78 .05 49 46 | --- --- --- ---
esx 107| -4 0 -1 167 -16 66 .35 1041 78 | -142805 -1046 9457 15576
iac n/a| 4 -11 -6 -29 30 -392 -.08 155 155 | 1153361 -683 8603 15151
mcc n/a| 135 21 129 -838 160 -3035 4.88 535 535 | --- --- --- ---
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 3.1469.0 GPS week: 1469 Day: 0 MJD: 54527
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6095 16 26 58 18 --- 16 | 58 59 99 55 --- 58
R04 | 2937 15 11 61 21 --- 14 | 52 51 76 82 --- 45
R06 | 3376 31 15 25 49 --- 18 | 67 62 63 50 --- 58
R07 | 1766 38 28 80 44 74 24 | 38 38 85 44 365 25
R08 | 6447 16 19 105 63 --- 26 | 27 37 84 37 --- 29
R09 |10602 33 42 72 64 --- 28 | 14 72 345 42 --- 32
R10 | 2722 14 15 79 35 --- 18 | 26 33 54 33 --- 25
R11 | 4943 27 36 163 44 --- 36 | 43 44 196 65 --- 52
XR13 | 9549 16 28 --- 44 --- 20 | 26 33 --- 45 --- 31
R14 | 1391 17 26 25 20 --- 13 | 16 35 30 53 --- 22
R15 | 4699 28 36 72 39 67 23 | 31 48 359 33 140 27
XR17 | 7692 41 737 --- 147 --- 93 | 142 556 --- 118 --- 129
R19 | 1274 21 24 86 30 --- 21 | 44 47 90 43 --- 40
R20 | 3281 25 18 40 61 --- 20 | 59 61 86 52 --- 56
R23 | 4538 23 30 97 54 --- 26 | 79 83 141 73 --- 82
R24 | 8156 22 27 24 30 166 15 | 100 103 112 120 113 105
------+------------------------------------+--------------------------------
RMS | 5138 24 27 79 44 112 |T 51 85 130 59 206 51
WRMS | 5138 25 24 45 44 112 |NE 51 85 130 59 206 51
MEDI | 4538 22 26 72 44 74 |MD 43 48 86 50 140 40
Table 3.1469.1 GPS week: 1469 Day: 1 MJD: 54528
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4848 28 22 43 25 --- 16 | 29 47 68 48 --- 39
R04 | 3356 21 22 39 24 --- 14 | 41 63 51 78 --- 47
R06 | 1748 30 22 49 35 --- 18 | 52 57 85 54 --- 53
R07 | 1748 19 25 42 40 84 17 | 50 43 74 72 256 45
R08 | 7101 36 26 271 38 --- 23 | 51 47 101 50 --- 44
R09 |13955 24 16 63 31 --- 18 | 20 44 180 36 --- 36
R10 | 1714 21 11 36 19 --- 11 | 34 34 74 29 --- 34
R11 | 6061 24 15 59 43 --- 19 | 46 47 62 38 --- 35
R13 | 8778 24 31 492 27 --- 20 | 19 30 429 40 --- 14
R14 | 1533 30 24 75 23 --- 20 | 29 34 76 66 --- 36
R15 | 3643 26 23 62 41 154 20 | 20 36 357 39 104 25
XR17 |10520 35 24 --- --- --- 29 | 106 296 --- --- --- 106
R19 | 1041 30 18 46 24 --- 16 | 53 55 53 52 --- 49
R20 | 2633 36 19 68 45 --- 22 | 53 63 81 51 --- 55
R23 | 4931 24 17 43 27 --- 15 | 79 85 82 83 --- 80
R24 | 8565 19 26 33 31 162 15 | 76 68 77 89 149 74
------+------------------------------------+--------------------------------
RMS | 5911 27 22 153 32 138 |T 47 65 123 55 169 48
WRMS | 5911 26 22 56 32 138 |NE 47 65 123 55 169 48
MEDI | 3643 24 22 49 31 154 |MD 46 47 77 51 149 44
Table 3.1469.2 GPS week: 1469 Day: 2 MJD: 54529
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4046 35 21 68 50 --- 22 | 21 37 65 41 --- 27
R04 | 3671 19 18 56 25 --- 14 | 50 44 52 102 --- 44
R06 | 1258 33 13 58 50 --- 20 | 24 38 55 55 --- 28
R07 | 1691 43 22 49 60 269 23 | 32 28 68 48 252 23
R08 | 7399 18 18 63 33 --- 16 | 33 31 229 35 --- 28
R09 |12623 25 23 131 58 --- 29 | 25 27 259 64 --- 17
R10 | 1364 31 18 49 35 --- 17 | 30 41 64 61 --- 35
R11 | 8859 12 29 91 51 --- 23 | 47 63 115 55 --- 49
R13 |14549 26 17 140 38 --- 27 | 29 32 171 64 --- 40
R14 | 1628 22 17 70 18 --- 15 | 20 28 40 47 --- 22
R15 | 4292 31 17 95 41 234 22 | 21 18 169 50 170 26
XR17 |10327 30 36 --- 58 --- 28 | 68 147 --- 71 --- 77
R19E | 1954 31 20 124 45 --- 26 | 60 61 127 48 --- 51
R20E | 2436 22 20 79 44 --- 20 | 60 73 93 60 --- 62
R23 | 757 31 23 137 49 --- 29 | 65 68 109 79 --- 60
R24 | 4854 23 19 67 58 414 21 | 74 89 99 108 261 84
------+------------------------------------+--------------------------------
RMS | 6300 28 20 91 45 315 |T 41 51 114 61 227 42
WRMS | 6300 29 21 73 45 315 |NE 38 49 115 62 227 40
MEDI | 3671 26 19 70 45 269 |MD 32 38 99 55 252 35
Table 3.1469.3 GPS week: 1469 Day: 3 MJD: 54530
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4709 14 12 55 31 --- 15 | 57 54 52 40 --- 48
R04 | 5817 30 24 38 23 --- 16 | 54 31 60 91 --- 34
R06 | 1039 39 25 36 32 --- 18 | 58 53 70 42 --- 50
R07 | 2452 32 19 89 77 757 29 | 25 38 101 86 355 37
R08 | 5928 12 19 827 34 --- 15 | 71 65 664 67 --- 56
R09 | 9315 23 14 280 38 --- 17 | 16 28 434 53 --- 23
R10 | 1770 22 17 63 37 --- 18 | 28 47 49 54 --- 35
R11 | 5759 31 24 61 34 --- 19 | 27 68 184 64 --- 54
R13 |12237 21 19 95 31 --- 22 | 35 32 112 65 --- 27
R14 | 2388 27 24 42 24 --- 16 | 48 42 50 76 --- 46
R15 |12725 32 13 307 52 388 22 | 23 21 558 56 120 19
XR17E |10405 18 23 --- 43 --- 20 | 47 83 --- 43 --- 41
R19E | 2050 24 18 60 36 --- 18 | 60 74 54 59 --- 60
R20E | 1059 38 40 73 37 --- 25 | 61 79 103 78 --- 72
R23E | 2386 48 30 87 81 --- 32 | 137 110 159 70 --- 106
R24E | 2998 43 29 57 32 477 22 | 79 109 101 94 242 91
------+------------------------------------+--------------------------------
RMS | 6103 31 23 246 43 563 |T 51 58 183 64 239 49
WRMS | 6103 28 22 81 43 563 |NE 40 43 212 63 237 39
MEDI | 2998 27 19 63 34 477 |MD 48 53 101 64 242 46
Table 3.1469.4 GPS week: 1469 Day: 4 MJD: 54531
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4542 22 28 57 33 --- 19 | 34 60 65 20 --- 37
R04 | 5569 37 25 40 29 --- 18 | 39 29 69 88 --- 32
R06 | 1457 27 32 42 48 --- 21 | 31 44 57 60 --- 41
R07 | 4477 35 21 60 41 1878 22 | 41 37 79 58 377 43
R08 | 6667 78 43 110 31 --- 37 | 58 29 154 70 --- 42
R09 |11332 12 22 503 20 --- 13 | 28 36 638 46 --- 30
R10 | 3381 32 31 40 40 --- 20 | 32 33 35 50 --- 19
R11 | 3863 30 17 53 36 --- 19 | 31 31 187 38 --- 26
R13 | 9452 25 20 56 31 --- 18 | 35 42 104 83 --- 37
R14 | 1157 14 16 33 22 --- 12 | 24 16 56 44 --- 24
R15 | 4923 39 12 113 38 304 30 | 27 43 554 35 103 42
XR17E |12005 34 34 --- 56 --- 29 | 56 84 --- 75 --- 57
XR19E | 1510 19 26 --- 30 --- 18 | 55 63 --- 36 --- 49
R20E | 1619 43 61 70 48 --- 32 | 44 86 92 63 --- 58
R23E | 5336 52 29 56 41 --- 25 | 61 50 79 52 --- 44
R24E | 3036 39 28 48 37 511 21 | 77 100 103 103 184 91
------+------------------------------------+--------------------------------
RMS | 5531 38 30 148 36 1137 |T 42 48 162 57 221 42
WRMS | 5531 33 28 51 36 1137 |NE 34 36 181 53 240 33
MEDI | 4477 32 26 56 36 511 |MD 35 42 79 52 184 41
Table 3.1469.5 GPS week: 1469 Day: 5 MJD: 54532
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5535 49 35 65 46 --- 27 | 41 67 97 48 --- 51
R04 | 5108 69 25 96 632 --- 43 | 26 62 124 561 --- 49
R06 | 1769 33 26 63 58 --- 23 | 42 53 78 46 --- 49
R07 | 6193 23 27 52 400 2769 22 | 23 33 57 383 687 26
R08 | 7383 62 28 110 37 --- 34 | 47 62 138 72 --- 57
R09 |16697 20 24 98 40 --- 26 | 18 31 704 49 --- 31
R10 | 2402 48 53 106 242 --- 57 | 35 57 97 245 --- 32
R11 |12028 21 35 1382 156 --- 43 | 25 25 9999 177 --- 25
R13 |11092 30 19 36 435 --- 19 | 44 47 100 385 --- 46
R14 | 974 21 23 31 187 --- 37 | 28 21 37 197 --- 29
R15 |13344 46 20 2908 67 566 28 | 37 24 9999 58 328 20
XR17E |13788 47 42 --- 243 --- 67 | 37 71 --- 257 --- 52
XR19E | 1471 28 18 --- 44 --- 19 | 53 43 --- 60 --- 45
R20E | 2864 31 23 59 72 --- 23 | 42 87 110 83 --- 66
R23E | 7080 32 25 57 65 --- 22 | 66 62 103 76 --- 66
R24E | 3876 32 15 73 131 623 32 | 53 56 100 168 214 61
------+------------------------------------+--------------------------------
RMS | 8269 40 28 863 254 1671 |T 38 50 145 179 409 44
WRMS | 8269 39 29 79 254 1671 |NE 33 43 159 201 507 37
MEDI | 5535 32 25 65 72 623 |MD 37 53 100 83 328 46
Table 3.1469.6 GPS week: 1469 Day: 6 MJD: 54533
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7353 21 27 58 55 --- 21 | 42 66 69 30 --- 47
R04 | 2713 65 105 71 446 --- 105 | 44 62 75 410 --- 45
R06 | 2575 67 31 67 114 --- 38 | 40 72 75 69 --- 53
R07 | 7195 33 34 112 75 535 34 | 39 37 83 100 733 38
R08 | 8171 71 48 74 66 --- 36 | 44 41 148 49 --- 47
R09 |12722 33 31 3713 36 --- 23 | 12 51 9999 50 --- 29
R10 | 1078 26 15 55 52 --- 19 | 44 53 55 51 --- 44
R11 | 7609 33 37 170 47 --- 42 | 34 27 336 39 --- 39
R13 |13382 80 98 467 216 --- 122 | 28 57 498 175 --- 75
R14 | 592 36 31 31 168 --- 40 | 14 20 47 174 --- 33
XR15 | 7872 30 18 --- 62 550 24 | 19 44 --- 57 247 31
XR17E | 8233 23 26 --- 97 --- 31 | 65 104 --- 105 --- 63
XR19E | 1742 30 24 --- 55 --- 23 | 67 48 --- 64 --- 51
R20E | 2186 28 21 55 45 --- 19 | 53 76 69 60 --- 58
R23E |11236 30 25 55 45 --- 20 | 47 46 70 66 --- 46
R24E | 5341 21 26 50 68 --- 22 | 97 110 106 123 --- 103
------+------------------------------------+--------------------------------
RMS | 7578 46 49 1040 155 535 |T 43 57 135 101 490 50
WRMS | 7578 50 46 78 155 535 |NE 32 48 154 109 490 43
MEDI | 7195 30 27 67 62 535 |MD 42 51 75 64 247 46
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