[IGSREPORT-16917] Wk 1507 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 11 05:49:56 PST 2008
******************************************************************************
IGS Electronic Report 11 Dec 05:49:59 PST 2008 Message Number 16917
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1507 (Nov 23, 2008 - Nov 29, 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 2.1507.
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:
igl1507[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1507 in the SP3 format.
igl15077.sum Combination Report for GPS Week 1507.
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 | 480.0 ns
1 | 464.0 ns
2 | 461.5 ns
3 | 454.9 ns
4 | 446.4 ns
5 | 444.2 ns
6 | 438.5 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
----+--------+---------------
3 | IAC | R11
6 | ESX | R04
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 1.1507, 1a.1507).
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 2.1507.0-6)
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 3.1507.0-6).
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 1507 summary. (Nov 23, 2008 - Nov 29, 2008)
Table 1.1507.a GPS week : 1507 MJD: 54793.0-54799.0
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 91| 0 0 12 -20 32 -86 -.20 39 38 | 0 -50 2339 2436
| 1 1 4 43 23 89 .08 | 0 98
cod 241| -3 0 -4 -2 9 21 -.15 27 24 | --- --- --- ---
| 2 2 2 32 29 59 .06 | --- ---
esx 135| 1 -1 -12 19 -26 104 .45 53 42 | 143281 4777 6159 15113
| 4 3 6 48 79 80 .10 | 7067 5684
iac n/a| 3 0 3 -24 -18 -11 -.09 41 41 | 456894 -724 6279 15475
| 1 2 4 44 15 74 .07 | 13152 3287
mcc n/a| -5 -6 8 49 -3 1836 .69 389 389 | --- --- --- ---
| 18 12 20 294 229 1357 .64 | --- ---
Table 1.1507.b GPS week : 1507 MJD: 54793.0-54799.0
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 | 16 16 17 19 20 18 14 |
R06 | 23 18 24 20 17 26 23 |
R07 | 12 14 13 13 14 15 16 |
R10 | 40 34 24 23 39 30 22 |
R11 | 0 0 0 219 42 21 26 |
R13 | 24 30 26 32 40 30 29 |
R14 | 27 27 31 37 27 26 21 |
R15 | 23 23 23 29 26 26 24 |
R17 | 19 15 12 18 16 20 22 |
R18 | 13 14 12 17 12 12 18 |
R19 | 13 14 16 16 18 17 16 |
R20 | 13 15 13 16 18 16 14 |
R21 | 27 12 24 20 14 19 34 |
R22 | 16 14 19 27 18 14 22 |
R23 | 16 20 20 21 15 21 21 |
R24 | 19 24 14 21 19 20 16 |
Table 1.1507.c GPS week : 1507 MJD: 54793.0-54799.0
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 1507 0 | -44 69 -64 -1349 2573 -10800 92.4 4002 4002 | 479957 0
brd 1507 1 | 20 44 -57 -151 588 -6586 93.9 3475 3475 | 463993 0
brd 1507 2 | -68 -73 -91 -2685 -854 -7229 93.5 3820 3820 | 461506 0
brd 1507 3 | -1 10 -17 1071 1731 -13390 91.9 4484 4484 | 454921 0
brd 1507 4 | -52 -95 -15 3256 1437 -13330 92.3 4956 4956 | 446432 0
brd 1507 5 | -62 -126 -82 3021 -592 -14820 92.4 8413 8413 | 444173 0
brd 1507 6 | 82 -85 -114 -1823 -1715 -10990 90.4 6496 6496 | 438516 0
-------------+------------------------------------------------------------+----------------
brd 1507 mean| -18 -36 -63 191 452 -11020 92.4 5092 5092 | 455642 0
brd 1507 sdev| 55 76 36 2344 1560 3148 1.1 1770 1770 | 14174 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 2.1507.0 GPS week: 1507 Day: 0 MJD: 54793
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 91| 0 -1 12 38 -1 -61 -.19 44 45 | 0 -154 2424 2534
cod 241| -4 1 -4 -41 -16 9 -.15 21 19 | --- --- --- ---
esx 135| 7 -4 -14 25 126 42 .51 46 41 | 147223 3982 6430 13388
iac n/a| 0 3 4 0 -30 -11 -.12 42 42 | 478711 1076 6452 12284
mcc n/a| -11 -9 0 81 54 -843 1.49 461 461 | --- --- --- ---
Table 2.1507.1 GPS week: 1507 Day: 1 MJD: 54794
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 91| 0 0 17 -51 22 54 -.08 39 35 | 0 -137 2211 2268
cod 241| -5 0 -3 26 23 -36 -.10 25 20 | --- --- --- ---
esx 135| 0 -5 -2 64 0 79 .43 41 37 | 132802 5553 6397 15728
iac n/a| 4 3 -3 -63 1 -44 -.16 37 37 | 465587 -3289 6422 15020
mcc n/a| 21 -24 3 394 -421 1565 1.04 228 228 | --- --- --- ---
Table 2.1507.2 GPS week: 1507 Day: 2 MJD: 54795
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 91| 1 1 11 -87 51 -169 -.17 34 32 | 0 -52 2198 2379
cod 241| -5 -1 -7 52 -3 22 -.21 26 23 | --- --- --- ---
esx 135| 0 1 -7 92 -66 215 .33 39 34 | 138184 6581 5393 13658
iac n/a| 4 1 2 -95 3 -18 -.02 38 38 | 461983 -3485 5375 11784
mcc n/a| 5 -18 42 434 94 2710 .45 237 237 | --- --- --- ---
Table 2.1507.3 GPS week: 1507 Day: 3 MJD: 54796
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 91| 2 0 15 5 67 -10 -.20 34 36 | 0 129 2229 2320
cod 241| -6 0 -5 -27 -31 105 -.22 32 29 | --- --- --- ---
esx 135| 6 4 -20 -8 -8 10 .63 44 42 | 141424 13450 6484 14588
iac n/a| 2 -3 6 31 -33 -144 -.15 49 49 | 456328 1497 6507 15953
mcc n/a| -35 -4 27 -83 295 3400 1.45 477 477 | --- --- --- ---
Table 2.1507.4 GPS week: 1507 Day: 4 MJD: 54797
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 91| 2 0 5 16 35 -106 -.21 44 44 | 0 -11 2435 2499
cod 241| 1 1 -2 -14 18 28 -.18 36 30 | --- --- --- ---
esx 135| 0 -3 -14 -22 -27 123 .37 38 38 | 153571 4768 5909 13578
iac n/a| 2 1 4 -16 -27 2 -.15 49 49 | 447399 -1079 5995 14574
mcc n/a| -13 -1 13 54 -67 2298 .11 370 370 | --- --- --- ---
Table 2.1507.5 GPS week: 1507 Day: 5 MJD: 54798
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 91| 1 -3 7 -29 12 -205 -.18 38 36 | 0 -117 2758 2846
cod 241| -2 4 0 -1 23 82 -.07 24 23 | --- --- --- ---
esx 135| -5 -3 -19 28 -110 56 .42 52 48 | 148999 -5907 6134 17210
iac n/a| 3 0 8 -42 -13 38 .00 39 39 | 448814 -4420 6217 18591
mcc n/a| -3 1 -10 -131 140 2296 -.06 906 906 | --- --- --- ---
Table 2.1507.6 GPS week: 1507 Day: 6 MJD: 54799
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 91| 0 -1 16 -33 39 -106 -.36 38 38 | 0 -11 2122 2209
cod 241| -3 0 -4 -12 54 -61 -.11 26 24 | --- --- --- ---
esx 135| -1 0 -8 -43 -98 206 .47 110 52 | 140765 5014 6371 17643
iac n/a| 3 0 0 13 -30 96 -.05 35 35 | 439437 4632 6990 20124
mcc n/a| 2 12 -16 -400 -117 1428 .32 43 43 | --- --- --- ---
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 3.1507.0 GPS week: 1507 Day: 0 MJD: 54793
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1273 25 21 37 28 --- 15 | 29 43 48 29 --- 27
R06 |13296 71 21 35 27 --- 23 | 76 83 87 77 --- 70
R07 | 1394 20 18 20 28 --- 12 | 48 56 42 44 --- 46
R10E | 2225 92 29 98 71 --- 40 | 37 36 69 78 --- 35
XR11E | ---- --- 5 --- --- 1153 0 | --- 136 --- --- 9999 135
R13E | 1958 49 25 48 49 --- 23 | 56 62 64 58 --- 53
R14E | 2432 58 27 37 66 --- 26 | 51 59 65 63 --- 55
R15E | 1116 25 31 34 63 202 22 | 26 22 43 54 29 24
R17 | 1805 30 24 45 34 --- 18 | 54 66 58 63 --- 54
R18 | 2878 27 16 27 19 --- 12 | 60 60 65 67 --- 59
R19 | 1484 28 13 22 26 --- 12 | 37 51 55 61 --- 48
R20 | 1167 20 18 33 21 --- 13 | 40 39 61 54 --- 43
R21 | 837 31 23 86 47 --- 27 | 47 69 63 59 --- 56
R22 | 806 31 12 35 39 --- 16 | 58 56 64 68 --- 58
R23 | 1295 35 19 38 15 --- 15 | 51 39 59 36 --- 38
R24 | 5079 48 13 27 46 620 19 | 62 61 66 57 437 55
------+------------------------------------+--------------------------------
RMS | 4002 44 21 46 42 461 |T 48 58 60 57 233 53
WRMS | 4002 45 19 41 42 461 |NE 51 56 60 55 437 50
MEDI | 1484 31 19 35 34 620 |MD 51 56 63 59 29 53
Table 3.1507.1 GPS week: 1507 Day: 1 MJD: 54794
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1016 18 26 35 25 --- 15 | 29 28 54 36 --- 28
R06 |11123 42 28 24 23 --- 17 | 78 83 74 79 --- 74
R07 | 589 30 16 35 13 --- 14 | 36 38 34 34 --- 32
R10E | 1501 86 29 64 54 --- 33 | 46 38 70 58 --- 34
XR11E | ---- --- 4 --- --- 432 0 | --- 173 --- --- 102 167
R13E | 2105 33 32 86 49 --- 29 | 36 51 47 54 --- 32
R14E | 1374 26 39 39 71 --- 27 | 43 57 46 51 --- 43
R15E | 1015 31 29 35 56 70 22 | 24 30 40 54 26 28
R17 | 858 29 19 31 24 --- 14 | 45 49 31 34 --- 36
R18 | 2463 24 15 32 24 --- 13 | 43 55 44 44 --- 43
R19 | 958 20 16 30 27 --- 13 | 19 39 40 44 --- 31
R20 | 1036 29 17 18 37 --- 15 | 32 31 35 47 --- 29
R21 | 554 28 14 22 20 --- 12 | 40 50 70 50 --- 46
R22 | 784 28 20 28 21 --- 13 | 56 40 55 43 --- 42
R23 | 912 38 37 37 22 --- 20 | 20 56 32 28 --- 25
R24 | 5993 65 16 46 34 314 23 | 33 69 84 75 230 61
------+------------------------------------+--------------------------------
RMS | 3475 39 25 41 37 227 |T 38 55 50 48 119 46
WRMS | 3475 35 20 37 37 227 |NE 39 48 50 46 230 40
MEDI | 1016 29 19 35 25 314 |MD 36 49 46 47 102 34
Table 3.1507.2 GPS week: 1507 Day: 2 MJD: 54795
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1019 12 33 37 23 --- 16 | 26 29 58 25 --- 28
R06 |13405 56 30 32 39 --- 23 | 85 89 87 64 --- 75
R07 | 2457 19 22 28 20 --- 13 | 55 42 47 36 --- 42
R10E | 1556 45 28 46 44 --- 23 | 36 38 43 56 --- 27
XR11E |11078 --- 7 --- --- 431 0 | --- 182 --- --- 103 195
R13E | 1789 43 35 26 67 --- 25 | 62 48 73 89 --- 56
R14E | 1726 39 32 77 61 --- 30 | 52 54 52 65 --- 41
R15E | 929 36 24 53 43 76 22 | 28 26 54 43 27 22
R17 | 1314 25 12 25 13 --- 11 | 34 41 52 35 --- 34
R18 | 1363 30 17 18 17 --- 12 | 36 64 66 53 --- 52
R19 | 923 19 31 32 19 --- 15 | 33 68 47 33 --- 43
R20 | 1434 20 16 24 26 --- 12 | 45 35 37 47 --- 36
R21 | 538 42 29 57 36 --- 23 | 50 59 73 48 --- 41
R22 | 704 21 32 27 43 --- 18 | 45 42 83 86 --- 54
R23 | 2081 43 26 26 42 --- 20 | 36 39 39 62 --- 36
R24 | 3318 33 15 26 21 327 14 | 56 89 103 84 331 81
------+------------------------------------+--------------------------------
RMS | 3820 34 26 39 38 237 |T 45 59 60 55 153 53
WRMS | 3820 32 23 34 38 237 |NE 45 54 62 52 331 47
MEDI | 1434 33 26 28 36 327 |MD 45 42 54 53 103 41
Table 3.1507.3 GPS week: 1507 Day: 3 MJD: 54796
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1079 32 25 47 23 --- 19 | 46 50 77 50 --- 45
R06 |14976 34 36 28 38 --- 20 | 68 85 90 71 --- 71
R07 | 3018 17 27 24 22 --- 13 | 23 45 37 29 --- 28
R10E | 2162 48 30 33 46 --- 23 | 45 37 42 53 --- 30
XR11E | 9145 220 216 --- 591 401 218 | 114 73 --- 86 159 156
R13E | 1114 36 22 40 103 --- 31 | 81 60 54 140 --- 67
R14E | 1705 63 39 68 89 --- 37 | 43 47 81 104 --- 47
R15E | 677 48 43 65 47 96 29 | 43 31 82 58 32 34
R17 | 1309 19 18 39 49 --- 18 | 56 61 70 86 --- 60
R18 | 694 26 19 30 40 --- 16 | 45 65 68 59 --- 54
R19 | 837 17 25 38 32 --- 16 | 57 69 102 56 --- 66
R20 | 1101 20 24 37 29 --- 15 | 43 66 73 48 --- 52
R21 | 799 26 30 47 33 --- 19 | 49 54 96 45 --- 53
R22 | 744 23 56 63 35 --- 27 | 46 67 79 78 --- 52
R23 | 801 30 35 38 41 --- 20 | 26 43 57 57 --- 30
R24 | 7193 38 34 34 35 668 20 | 33 73 81 56 520 52
------+------------------------------------+--------------------------------
RMS | 4483 34 32 44 49 477 |T 51 57 72 67 237 56
WRMS | 4483 36 29 42 49 477 |NE 44 61 75 57 520 51
MEDI | 1101 30 30 38 38 401 |MD 45 60 77 57 159 52
Table 3.1507.4 GPS week: 1507 Day: 4 MJD: 54797
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 993 23 19 50 34 --- 19 | 27 28 49 33 --- 27
R06 |12027 33 25 32 23 --- 16 | 165 164 175 168 --- 166
R07 | 5443 11 26 31 20 --- 13 | 28 35 39 35 --- 26
R10E | 4478 103 34 53 68 --- 39 | 32 47 52 102 --- 43
R11E | 9102 79 81 40 83 78 42 | 100 91 31 95 210 70
R13E | 1344 60 57 70 89 --- 40 | 53 49 69 88 --- 40
R14E | 2769 40 42 29 68 --- 26 | 49 44 40 76 --- 36
R15E | 1947 28 29 34 79 54 26 | 33 26 44 78 36 31
R17 | 1285 32 25 26 26 --- 16 | 63 45 80 55 --- 55
R18 | 922 23 14 19 23 --- 11 | 50 62 58 65 --- 57
R19 | 887 29 31 37 16 --- 17 | 38 63 50 53 --- 45
R20 | 956 28 25 29 43 --- 18 | 64 60 70 34 --- 52
R21 | 958 24 15 32 23 --- 14 | 50 48 55 63 --- 47
R22 | 744 16 30 30 41 --- 17 | 31 52 50 39 --- 31
R23 | 859 34 9 34 18 --- 15 | 29 39 47 38 --- 33
R24 | 9755 33 43 25 20 634 19 | 65 44 54 56 385 46
------+------------------------------------+--------------------------------
RMS | 4956 44 36 38 49 370 |T 54 56 60 67 210 50
WRMS | 4956 44 30 38 49 370 |NE 55 58 66 58 385 53
MEDI | 1285 29 26 32 26 78 |MD 49 47 50 56 210 43
Table 3.1507.5 GPS week: 1507 Day: 5 MJD: 54798
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1122 26 10 66 21 --- 18 | 32 31 100 28 --- 33
R06 |15253 45 27 74 40 --- 26 | 140 169 215 173 --- 167
R07 | 4236 17 18 51 20 --- 15 | 25 33 59 27 --- 26
R10E | 4424 51 38 59 66 --- 30 | 43 47 62 89 --- 46
R11E |23174 37 22 39 46 47 20 | 36 68 33 72 133 56
R13E | 3513 41 42 74 58 --- 30 | 68 72 64 69 --- 57
R14E | 4978 57 16 50 58 --- 25 | 61 49 57 65 --- 37
R15E | 2385 44 27 53 58 63 25 | 22 20 52 63 27 23
R17 | 1225 32 36 43 24 --- 19 | 81 47 75 65 --- 58
R18 | 1361 18 15 30 23 --- 12 | 45 41 63 64 --- 46
R19 | 764 40 27 32 14 --- 16 | 30 36 58 35 --- 34
R20 | 1612 25 15 46 31 --- 16 | 32 49 47 45 --- 37
R21 | 803 32 12 62 25 --- 18 | 36 21 77 22 --- 24
R22 | 1050 32 21 20 24 --- 14 | 25 43 58 40 --- 35
R23 | 1259 53 17 41 35 --- 20 | 31 27 49 40 --- 18
R24 |16465 34 17 62 33 1567 20 | 35 35 85 58 317 38
------+------------------------------------+--------------------------------
RMS | 8412 38 24 52 39 906 |T 46 49 72 59 159 45
WRMS | 8412 36 23 48 39 906 |NE 46 48 80 54 317 46
MEDI | 1612 34 18 50 31 63 |MD 35 41 59 58 133 37
Table 3.1507.6 GPS week: 1507 Day: 6 MJD: 54799
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1652 21 15 379 24 --- 14 | 34 30 141 37 --- 30
R06 |15407 55 24 59 28 --- 23 | 124 136 131 130 --- 128
R07 | 2113 32 23 39 17 --- 16 | 26 35 40 28 --- 26
R10E | 3210 44 29 36 42 --- 21 | 36 44 58 91 --- 52
R11E |14114 53 24 58 48 44 25 | 49 74 35 61 112 68
R13E | 2534 43 48 47 59 --- 29 | 72 61 49 73 --- 56
R14E | 4174 34 31 43 38 --- 20 | 68 46 54 59 --- 47
R15E | 2070 33 31 47 53 42 23 | 31 19 26 56 23 22
R17 | 902 42 34 47 34 --- 22 | 90 56 60 76 --- 64
R18 | 2247 38 19 38 31 --- 17 | 54 54 57 65 --- 53
R19 | 734 20 10 47 31 --- 15 | 55 58 70 38 --- 49
R20 | 933 38 15 23 21 --- 14 | 39 50 57 55 --- 46
R21 | 906 33 35 130 21 --- 34 | 51 55 97 51 --- 51
R22 | 698 34 19 76 27 --- 22 | 40 60 90 49 --- 49
R23 | 2633 50 20 56 24 --- 21 | 28 35 66 28 --- 25
R24 |13318 21 17 51 26 --- 16 | 58 52 89 69 --- 61
------+------------------------------------+--------------------------------
RMS | 6495 38 26 110 35 43 |T 53 54 70 60 67 51
WRMS | 6495 38 24 52 35 43 |NE 54 56 81 56 --- 52
MEDI | 2113 34 23 47 28 42 |MD 49 52 58 56 23 49
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