[IGSREPORT-17040] Wk 1513 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jan 22 05:14:55 PST 2009
******************************************************************************
IGS Electronic Report 22 Jan 05:14:58 PST 2009 Message Number 17040
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1513 (Jan 04, 2009 - Jan 10, 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 2.1513.
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:
igl1513[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1513 in the SP3 format.
igl15137.sum Combination Report for GPS Week 1513.
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 | 319.4 ns
1 | 321.1 ns
2 | 332.6 ns
3 | 324.0 ns
4 | 315.2 ns
5 | 297.3 ns
6 | 311.4 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 1.1513, 1a.1513).
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 2.1513.0-6)
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 3.1513.0-6).
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 1513 summary. (Jan 04, 2009 - Jan 10, 2009)
Table 1.1513.a GPS week : 1513 MJD: 54835.0-54841.0
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 86| 0 0 10 13 -9 -47 -.14 31 28 | 0 56 2794 2951
| 1 2 5 44 77 188 .04 | 0 351
cod 242| -1 1 -4 21 16 17 -.09 18 15 | --- --- --- ---
| 1 1 3 18 27 54 .04 | --- ---
esx 139| 1 -1 -3 -51 -1 23 .41 31 26 | 110177 3448 6971 12700
| 3 2 5 51 45 60 .12 | 11409 6205
iac n/a| 0 0 2 -10 -47 -1 -.08 30 30 | 318605 -1034 6803 12637
| 2 1 11 29 35 107 .05 | 11236 3105
mcc n/a| -1 -1 15 76 40 1190 -.28 341 341 | --- --- --- ---
| 12 5 19 146 126 552 .42 | --- ---
Table 1.1513.b GPS week : 1513 MJD: 54835.0-54841.0
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
------+------------------------------------+------------------------------------------
R04 | 13 22 20 19 25 18 14 |
R06 | 18 18 18 15 20 18 16 |
R07 | 16 15 16 14 13 12 21 |
R10 | 15 12 11 17 15 13 11 |
R11 | 11 8 9 11 14 16 13 |
R13 | 18 17 11 8 11 11 10 |
R14 | 13 12 17 9 8 8 12 |
R15 | 11 9 11 16 9 10 10 |
R17 | 15 13 15 12 21 16 12 |
R18 | 15 17 13 13 12 12 31 |
R19 | 10 12 13 9 12 17 14 |
R20 | 13 14 17 15 16 18 15 |
R21 | 13 14 11 10 13 11 13 |
R22 | 14 15 13 13 16 21 14 |
R23 | 27 23 22 11 16 18 18 |
R24 | 15 16 13 32 29 14 19 |
Table 1.1513.c GPS week : 1513 MJD: 54835.0-54841.0
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 1513 0 | -34 60 85 -321 -2086 -26850 93.1 3291 3291 | 319390 0
brd 1513 1 | 46 120 186 -2618 -1832 -26870 89.4 3398 3398 | 321137 0
brd 1513 2 | -93 156 120 -4074 3347 -13460 89.6 2478 2478 | 332556 0
brd 1513 3 | 50 -88 83 -98 1784 -13180 86.3 2621 2621 | 323969 0
brd 1513 4 | 125 47 98 -2713 4194 -12200 92.0 3624 3624 | 315227 0
brd 1513 5 | -52 14 83 -1738 4918 -17850 92.2 4661 4661 | 297349 0
brd 1513 6 | 69 -42 54 -225 -706 -20360 89.3 3227 3227 | 311428 0
-------------+------------------------------------------------------------+----------------
brd 1513 mean| 16 38 101 -1684 1374 -18681 90.3 3328 3328 | 317293 0
brd 1513 sdev| 77 86 42 1535 2919 6282 2.3 719 719 | 11053 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 2.1513.0 GPS week: 1513 Day: 0 MJD: 54835
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 86| -2 2 16 22 -151 228 -.17 32 32 | 0 1 2544 2602
cod 242| -1 3 0 32 72 19 -.12 17 15 | --- --- --- ---
esx 139| 0 -1 -3 5 78 -13 .49 28 24 | 97468 10764 6904 10663
iac n/a| 2 0 -12 -23 -99 -217 -.01 32 32 | 319019 2738 6918 10692
mcc n/a| 3 5 28 0 17 557 .00 374 374 | --- --- --- ---
Table 2.1513.1 GPS week: 1513 Day: 1 MJD: 54836
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 86| 0 2 20 -59 -26 -233 -.16 32 31 | 0 770 4634 5146
cod 242| -3 0 -1 36 22 124 -.12 19 17 | --- --- --- ---
esx 139| 5 0 -3 21 -9 61 .53 29 24 | 128490 1276 9907 16835
iac n/a| 3 1 -13 -30 -19 -20 -.18 27 27 | 325985 -4451 9781 16698
mcc n/a| -21 -11 46 69 269 595 .23 179 179 | --- --- --- ---
Table 2.1513.2 GPS week: 1513 Day: 2 MJD: 54837
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 86| 2 -2 6 36 69 78 -.11 27 26 | 0 -7 2649 2848
cod 242| -2 0 -2 17 3 -17 -.09 17 17 | --- --- --- ---
esx 139| 0 -3 -5 -79 -29 -8 .34 29 26 | 118204 43 8206 17447
iac n/a| 0 1 1 -24 -53 21 -.11 31 31 | 334032 141 7969 17486
mcc n/a| 16 1 6 20 -57 1868 -.40 510 510 | --- --- --- ---
Table 2.1513.3 GPS week: 1513 Day: 3 MJD: 54838
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 86| -1 -1 6 38 -36 -101 -.16 35 27 | 0 -110 2255 2322
cod 242| 0 0 -5 29 21 16 -.03 16 13 | --- --- --- ---
esx 139| 2 0 -6 -112 32 21 .27 28 24 | 111272 1503 5114 8290
iac n/a| -3 3 10 -6 -66 19 -.06 31 31 | 324122 -2504 4497 8352
mcc n/a| -6 3 3 34 -63 1951 -.30 564 564 | --- --- --- ---
Table 2.1513.4 GPS week: 1513 Day: 4 MJD: 54839
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 86| 0 0 8 2 59 96 -.06 28 23 | 0 214 2319 2369
cod 242| 0 3 -8 39 4 -30 -.07 21 18 | --- --- --- ---
esx 139| -1 0 -5 -60 -15 -66 .33 31 26 | 109211 8585 5541 12362
iac n/a| 3 -1 14 -43 -70 -14 -.06 37 37 | 317581 970 5481 12875
mcc n/a| 7 -1 5 -112 -11 1154 -1.09 455 455 | --- --- --- ---
Table 2.1513.5 GPS week: 1513 Day: 5 MJD: 54840
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 86| 0 -2 8 -19 51 -107 -.16 27 27 | 0 -235 2606 2702
cod 242| 0 0 -6 -9 -16 -29 -.14 17 12 | --- --- --- ---
esx 139| -3 0 -4 -35 -61 119 .58 37 30 | 95457 -6728 6248 10003
iac n/a| 1 0 6 14 2 79 -.07 27 27 | 299775 -5405 6115 10003
mcc n/a| -3 -2 -10 347 161 1002 -.36 167 167 | --- --- --- ---
Table 2.1513.6 GPS week: 1513 Day: 6 MJD: 54841
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 86| 0 -1 5 76 -31 -293 -.13 33 28 | 0 -236 2554 2671
cod 242| 0 2 -5 1 5 42 -.07 17 14 | --- --- --- ---
esx 139| 4 -6 8 -102 -6 51 .38 37 30 | 111141 8694 6883 13304
iac n/a| -1 -2 8 41 -24 121 -.10 29 29 | 309723 1268 6865 12353
mcc n/a| -6 -6 26 175 -29 1203 -.03 138 138 | --- --- --- ---
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 3.1513.0 GPS week: 1513 Day: 0 MJD: 54835
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 7746 20 13 30 26 --- 12 | 33 50 59 41 --- 43
R06E | 3085 47 16 40 20 --- 17 | 54 62 83 62 --- 63
R07E | 1900 35 14 31 33 --- 15 | 26 26 41 39 --- 26
R10 | 2964 34 26 17 21 --- 14 | 21 24 28 30 --- 22
R11 | 2717 18 11 18 31 140 11 | 23 32 46 46 62 33
R13 | 1076 42 14 43 29 --- 18 | 24 20 39 26 --- 19
R14 | 2720 22 8 29 30 --- 12 | 25 31 45 28 --- 27
R15 | 3165 22 19 18 18 61 11 | 28 31 37 29 24 26
R17 | 1434 35 19 29 23 --- 15 | 45 79 85 64 --- 69
R18 | 903 35 13 35 23 --- 15 | 40 55 71 48 --- 51
R19 | 1262 18 11 11 29 --- 10 | 41 52 53 38 --- 46
R20 | 1217 23 16 11 36 --- 12 | 35 47 53 47 --- 44
R21 | 1266 18 24 20 24 --- 12 | 55 79 67 63 --- 68
R22 | 822 21 12 23 40 --- 13 | 66 89 78 97 --- 82
R23 | 1467 56 21 38 72 --- 26 | 45 40 42 43 --- 25
R24 | 7419 36 19 22 24 630 14 | 303 310 305 317 206 308
------+------------------------------------+--------------------------------
RMS | 3291 32 17 28 32 374 |T 54 64 70 63 97 59
WRMS | 3291 32 15 24 32 374 |NE 57 68 73 67 97 63
MEDI | 1467 23 14 23 26 140 |MD 35 47 53 43 62 43
Table 3.1513.1 GPS week: 1513 Day: 1 MJD: 54836
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 1528 52 23 46 29 --- 21 | 29 48 75 46 --- 44
R06E | 4521 31 20 42 28 --- 17 | 53 69 92 68 --- 69
R07E | 1401 34 16 29 28 --- 15 | 34 27 36 38 --- 28
R10 | 2644 28 12 21 23 --- 12 | 22 29 36 28 --- 24
R11 | 1525 15 11 12 16 156 8 | 23 29 31 31 65 25
R13 | 2049 20 18 42 32 --- 16 | 23 30 55 31 --- 25
R14 | 2628 28 16 14 25 --- 12 | 28 20 44 34 --- 24
R15 | 4156 20 13 13 14 49 8 | 22 22 28 24 23 17
R17 | 1030 32 13 17 26 --- 13 | 36 54 54 60 --- 50
R18 | 1469 24 29 31 33 --- 17 | 26 43 38 30 --- 27
R19 | 1119 17 12 22 28 --- 11 | 33 36 49 30 --- 34
R20 | 1346 18 24 27 24 --- 14 | 28 24 31 16 --- 18
R21 | 1359 22 22 28 25 --- 14 | 23 48 48 34 --- 34
R22 | 827 44 20 16 19 --- 15 | 44 60 54 48 --- 47
R23 | 1018 45 29 40 49 --- 23 | 31 33 58 51 --- 28
R24 |10603 46 16 25 16 264 15 | 263 265 282 265 392 267
------+------------------------------------+--------------------------------
RMS | 3398 32 19 29 27 179 |T 44 52 63 52 160 47
WRMS | 3398 31 17 24 27 179 |NE 46 53 62 52 160 47
MEDI | 1469 28 16 25 25 156 |MD 28 33 48 34 65 28
Table 3.1513.2 GPS week: 1513 Day: 2 MJD: 54837
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2808 49 14 35 36 --- 19 | 30 47 60 46 --- 41
R06E | 5045 32 20 37 38 --- 17 | 39 50 72 48 --- 48
R07E | 1393 32 19 31 33 --- 16 | 30 20 49 40 --- 25
R10 | 1828 17 13 22 24 --- 10 | 27 21 35 29 --- 21
R11 | 1580 17 12 16 18 146 9 | 27 33 26 37 100 27
R13 | 2931 23 12 24 18 --- 11 | 17 33 49 32 --- 29
R14 | 2047 23 19 52 17 --- 17 | 20 35 74 30 --- 33
R15 | 3293 24 10 26 17 77 11 | 20 18 33 22 22 16
R17 | 886 36 11 28 24 --- 14 | 56 67 91 56 --- 65
R18 | 1671 17 17 32 23 --- 13 | 33 39 28 47 --- 30
R19 | 1986 21 20 17 29 --- 12 | 36 56 39 28 --- 40
R20 | 1671 18 11 34 50 --- 17 | 37 29 60 22 --- 28
R21 | 1929 20 16 24 16 --- 11 | 42 50 57 42 --- 44
R22 | 1167 28 12 20 30 --- 13 | 45 58 64 57 --- 53
R23 | 1373 26 38 24 55 --- 21 | 20 40 29 30 --- 15
R24 | 4025 28 16 22 24 868 12 | 289 321 315 310 460 310
------+------------------------------------+--------------------------------
RMS | 2478 27 17 29 31 510 |T 48 57 67 54 194 51
WRMS | 2478 26 17 26 31 510 |NE 51 61 69 57 194 54
MEDI | 1828 23 14 24 24 146 |MD 30 39 49 37 100 30
Table 3.1513.3 GPS week: 1513 Day: 3 MJD: 54838
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 981 47 12 36 44 --- 19 | 38 33 59 46 --- 34
R06E | 6872 23 16 37 32 --- 15 | 66 73 89 75 --- 73
R07E | 1242 22 15 24 39 --- 14 | 30 28 39 48 --- 28
R10 | 2292 41 9 34 38 --- 17 | 43 37 51 35 --- 34
R11 | 1741 16 11 22 27 105 10 | 20 29 37 35 63 25
R13 | 2134 13 8 20 18 --- 8 | 27 28 22 28 --- 21
R14 | 1550 22 11 18 16 --- 9 | 38 52 56 53 --- 47
R15 | 1752 26 9 41 36 86 16 | 26 30 61 32 19 29
R17 | 1559 33 11 18 24 --- 12 | 57 71 69 66 --- 65
R18 | 1045 19 20 26 22 --- 12 | 25 48 47 28 --- 35
R19 | 2700 16 12 8 26 --- 9 | 38 53 54 47 --- 48
R20 | 2436 28 14 31 36 --- 15 | 28 41 41 40 --- 33
R21 | 883 17 11 16 27 --- 10 | 52 59 59 46 --- 53
R22 | 1007 19 11 26 33 --- 12 | 50 58 79 35 --- 53
R23 | 2638 22 13 22 24 --- 11 | 30 41 40 27 --- 29
R24 | 4045 98 40 37 35 968 32 | 150 248 245 187 263 215
------+------------------------------------+--------------------------------
RMS | 2621 35 16 28 31 564 |T 44 58 65 51 115 51
WRMS | 2621 27 13 24 31 564 |NE 44 61 66 50 115 52
MEDI | 1741 22 11 24 27 105 |MD 38 41 54 40 63 34
Table 3.1513.4 GPS week: 1513 Day: 4 MJD: 54839
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 1946 41 22 43 70 --- 25 | 29 34 70 28 --- 31
R06E |10411 38 25 45 31 --- 20 | 51 64 88 72 --- 63
R07E | 1177 17 16 28 30 --- 13 | 34 30 51 42 --- 32
R10 | 3148 29 25 23 26 --- 15 | 18 35 42 35 --- 25
R11 | 1590 17 18 23 36 90 13 | 20 42 37 31 39 28
R13 | 1158 19 17 21 16 --- 10 | 28 40 40 26 --- 31
R14 | 1063 13 10 16 13 --- 7 | 22 29 33 32 --- 26
R15 | 2638 13 15 17 20 58 9 | 18 29 32 39 29 25
R17 | 1908 25 25 43 54 --- 21 | 39 71 88 18 --- 51
R18 | 763 22 15 26 16 --- 11 | 29 42 42 31 --- 32
R19 | 2981 18 21 20 20 --- 11 | 30 48 39 26 --- 33
R20 | 1633 27 17 30 38 --- 16 | 35 43 25 41 --- 31
R21 | 1363 22 14 22 29 --- 12 | 49 56 56 53 --- 50
R22 | 979 15 24 30 39 --- 15 | 51 64 74 38 --- 51
R23 | 4687 22 24 23 38 --- 15 | 21 34 42 26 --- 25
R24 | 5836 63 32 52 53 781 29 | 328 333 348 360 142 335
------+------------------------------------+--------------------------------
RMS | 3623 28 21 31 37 455 |T 50 62 69 56 70 54
WRMS | 3623 23 18 26 37 455 |NE 52 66 69 58 70 57
MEDI | 1633 22 18 23 30 90 |MD 29 42 42 32 39 31
Table 3.1513.5 GPS week: 1513 Day: 5 MJD: 54840
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3456 46 21 29 30 --- 18 | 37 55 69 37 --- 43
R06E |15048 44 16 43 22 --- 17 | 64 74 87 80 --- 73
R07E | 1438 20 9 31 22 --- 11 | 41 32 41 37 --- 32
R10 | 2673 23 15 28 25 --- 12 | 23 22 51 38 --- 25
R11 | 1957 21 15 48 31 78 16 | 15 23 52 27 26 17
R13 | 1091 22 10 28 19 --- 11 | 26 28 47 19 --- 24
R14 | 1052 19 6 19 10 --- 7 | 19 27 27 35 --- 24
R15 | 2526 21 9 25 17 48 10 | 16 20 47 23 39 21
R17 | 1824 27 14 23 42 --- 15 | 27 39 43 45 --- 35
R18 | 1124 25 8 18 27 --- 11 | 18 24 48 45 --- 27
R19 | 1707 25 15 49 34 --- 17 | 17 44 71 19 --- 34
R20 | 1626 42 15 31 34 --- 17 | 31 54 62 48 --- 46
R21 | 2323 22 12 13 24 --- 10 | 33 37 44 63 --- 40
R22 | 1000 22 26 71 19 --- 20 | 39 47 76 44 --- 41
R23 | 2767 11 32 53 22 --- 18 | 30 27 75 44 --- 34
R24 | 7949 21 21 24 28 275 13 | 156 166 153 171 289 161
------+------------------------------------+--------------------------------
RMS | 4660 27 17 37 26 167 |T 37 44 62 48 118 42
WRMS | 4660 27 12 30 26 167 |NE 34 42 61 47 118 40
MEDI | 1824 22 15 28 24 78 |MD 27 32 51 38 39 34
Table 3.1513.6 GPS week: 1513 Day: 6 MJD: 54841
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4240 26 20 27 26 --- 14 | 42 40 46 41 --- 37
R06E |10366 36 15 36 24 --- 15 | 98 104 126 107 --- 106
R07E | 785 70 16 33 19 --- 21 | 56 40 46 41 --- 39
R10 | 1247 23 9 22 27 --- 11 | 19 20 32 37 --- 21
R11 | 1984 17 15 34 23 68 12 | 26 35 50 35 56 31
R13 | 1516 19 11 22 17 --- 9 | 28 25 24 22 --- 22
R14 | 1381 15 12 32 26 --- 12 | 23 28 45 32 --- 28
R15 | 3134 21 6 13 28 93 10 | 21 29 30 37 49 27
R17 | 1318 32 8 17 29 --- 12 | 40 58 62 50 --- 50
R18 | 1211 24 38 100 39 --- 31 | 26 37 57 47 --- 31
R19 | 905 24 23 9 32 --- 13 | 30 61 54 28 --- 43
R20 | 1509 42 7 33 24 --- 15 | 35 56 71 58 --- 52
R21 | 1181 28 10 26 26 --- 12 | 66 59 65 49 --- 56
R22 | 1020 34 14 18 34 --- 14 | 51 73 73 73 --- 65
R23 | 1473 30 12 48 41 --- 18 | 49 53 77 27 --- 46
R24 | 3178 43 21 33 38 209 18 | 241 242 234 239 275 238
------+------------------------------------+--------------------------------
RMS | 3226 33 17 37 29 138 |T 53 60 68 57 126 55
WRMS | 3226 28 14 30 29 138 |NE 50 59 67 56 126 54
MEDI | 1381 26 12 27 26 93 |MD 35 40 54 41 56 39
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