[IGSREPORT-16895] Wk 1506 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 4 05:16:58 PST 2008
******************************************************************************
IGS Electronic Report 04 Dec 05:17:01 PST 2008 Message Number 16895
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1506 (Nov 16, 2008 - Nov 22, 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 2.1506.
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:
igl1506[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1506 in the SP3 format.
igl15067.sum Combination Report for GPS Week 1506.
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 | 507.7 ns
1 | 497.1 ns
2 | 433.0 ns
3 | 488.0 ns
4 | 430.4 ns
5 | 417.1 ns
6 | 379.0 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 1.1506, 1a.1506).
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 2.1506.0-6)
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 3.1506.0-6).
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 1506 summary. (Nov 16, 2008 - Nov 22, 2008)
Table 1.1506.a GPS week : 1506 MJD: 54786.0-54792.0
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 75| 0 1 13 13 0 -97 -.16 44 40 | 0 -48 2381 2470
| 2 1 7 28 63 259 .07 | 0 85
cod 243| -2 0 -5 -10 23 57 -.16 24 21 | --- --- --- ---
| 2 1 2 21 30 88 .05 | --- ---
esx 128| 0 0 -10 8 8 67 .41 39 36 | 106741 3230 6112 15487
| 2 4 6 49 37 80 .07 | 45801 4668
iac n/a| 3 0 11 -31 -28 -51 -.04 39 39 | 451551 -1006 5941 12402
| 2 1 5 20 35 60 .06 | 47739 3331
mcc n/a| -5 -1 11 -250 -90 1536 -.39 308 308 | --- --- --- ---
| 22 56 37 418 535 1434 1.25 | --- ---
Table 1.1506.b GPS week : 1506 MJD: 54786.0-54792.0
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 | 14 14 12 15 21 18 18 |
R06 | 25 22 20 30 17 21 29 |
R07 | 13 19 17 8 13 15 11 |
R09 | 0 --- --- --- --- --- --- |
R10 | 26 22 29 31 24 31 28 |
R11 | 27 23 21 26 25 50 --- |
R13 | 25 27 45 24 22 30 31 |
R14 | 23 23 24 23 24 23 22 |
R15 | 27 25 24 27 23 26 24 |
R17 | 15 16 17 15 18 17 21 |
R18 | 14 13 19 15 13 15 13 |
R19 | 11 14 13 16 17 15 14 |
R20 | 11 16 14 18 15 14 13 |
R21 | 15 16 16 13 19 21 22 |
R22 | 17 18 11 16 14 12 18 |
R23 | 14 15 24 35 15 20 23 |
R24 | 19 13 29 32 17 19 18 |
Table 1.1506.c GPS week : 1506 MJD: 54786.0-54792.0
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 1506 0 | 63 99 0 -1917 141 -16870 96.3 5195 5195 | 507726 0
brd 1506 1 | -107 -59 -50 -3351 2859 -19940 89.1 4005 4005 | 497070 0
brd 1506 2 | -132 -76 35 -414 -20 -15470 94.6 5259 5259 | 433004 0
brd 1506 3 | -146 53 -131 -1525 -1198 -19730 94.7 5247 5247 | 487982 0
brd 1506 4 | -2 -35 -122 -2431 -2347 -21220 94.0 7056 7056 | 430402 0
brd 1506 5 | 40 -15 -45 -896 -1992 -15920 91.3 4482 4482 | 417064 0
brd 1506 6 | 127 36 -140 -77 -3708 -10820 92.2 3549 3549 | 378968 0
-------------+------------------------------------------------------------+----------------
brd 1506 mean| -22 0 -64 -1516 -895 -17138 93.2 4970 4970 | 450316 0
brd 1506 sdev| 107 64 68 1157 2131 3546 2.4 1136 1136 | 47946 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 2.1506.0 GPS week: 1506 Day: 0 MJD: 54786
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 75| -2 0 -1 16 21 -67 -.22 43 41 | 0 -188 2712 2765
cod 243| -1 1 -5 24 18 60 -.11 20 16 | --- --- --- ---
esx 128| 5 4 -6 12 60 151 .42 46 46 | 157018 1832 7622 23147
iac n/a| 1 0 15 -39 -55 -156 -.01 34 34 | 508178 -168 6331 16976
mcc n/a| 14 1 -17 14 3 516 .51 255 255 | --- --- --- ---
Table 2.1506.1 GPS week: 1506 Day: 1 MJD: 54787
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 75| 5 2 8 26 106 202 -.17 44 43 | 0 -6 2201 2318
cod 243| -4 0 -8 -10 -30 6 -.16 20 16 | --- --- --- ---
esx 128| -1 -4 0 -21 -58 -7 .42 37 33 | 160681 3414 5985 14778
iac n/a| 5 -1 9 -8 20 -104 -.05 37 37 | 500262 -2746 5991 11699
mcc n/a| -1 12 14 237 -126 765 .11 123 123 | --- --- --- ---
Table 2.1506.2 GPS week: 1506 Day: 2 MJD: 54788
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 75| 1 -1 19 -7 -5 5 -.11 38 31 | 0 50 2183 2275
cod 243| -1 0 -5 -14 20 -33 -.17 22 18 | --- --- --- ---
esx 128| -2 8 -11 26 17 127 .54 55 40 | 91137 2424 5820 13829
iac n/a| 1 -1 7 -43 -90 -18 -.01 47 47 | 435876 -4242 5812 11289
mcc n/a| -17 9 0 26 -128 1360 1.02 237 237 | --- --- --- ---
Table 2.1506.3 GPS week: 1506 Day: 3 MJD: 54789
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 75| -2 3 15 12 40 -31 -.15 52 39 | 0 6 2197 2259
cod 243| 0 1 -2 -45 9 34 -.17 29 21 | --- --- --- ---
esx 128| -1 -3 -18 12 -11 5 .38 34 33 | 141737 2287 5386 13740
iac n/a| 4 0 14 1 -14 -16 -.11 45 45 | 488217 5 5328 11148
mcc n/a| -29 -7 43 -757 887 2540 .33 331 331 | --- --- --- ---
Table 2.1506.4 GPS week: 1506 Day: 4 MJD: 54790
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 75| -1 2 17 66 -20 -3 -.24 39 38 | 0 -112 2487 2543
cod 243| -4 0 -6 -15 33 25 -.23 25 24 | --- --- --- ---
esx 128| 1 0 -11 -39 1 47 .39 28 28 | 78049 8485 5462 12955
iac n/a| 3 -1 20 -28 -7 -67 -.04 42 42 | 428587 2449 5478 10001
mcc n/a| -31 -107 39 -805 -232 3191 -2.57 536 536 | --- --- --- ---
Table 2.1506.5 GPS week: 1506 Day: 5 MJD: 54791
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 75| 0 0 19 5 -81 -158 -.19 46 42 | 0 -99 2345 2476
cod 243| -4 1 -8 4 67 62 -.09 26 24 | --- --- --- ---
esx 128| 0 -2 -5 -37 25 -22 .39 36 36 | 72576 9049 6743 15543
iac n/a| 0 1 4 -49 -18 7 -.11 36 36 | 417696 3266 6772 15191
mcc n/a| 31 87 -50 -10 -945 3021 -1.36 466 466 | --- --- --- ---
Table 2.1506.6 GPS week: 1506 Day: 6 MJD: 54792
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 75| 0 1 16 -21 -58 -631 -.02 47 44 | 0 13 2542 2655
cod 243| -4 0 -3 -15 45 243 -.19 28 24 | --- --- --- ---
esx 128| -2 -2 -15 104 25 169 .30 37 33 | 45989 -4881 5767 14417
iac n/a| 5 1 7 -51 -30 -1 .05 35 35 | 382042 -5607 5879 10514
mcc n/a| -5 -5 53 -460 -92 -639 -.75 208 208 | --- --- --- ---
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 3.1506.0 GPS week: 1506 Day: 0 MJD: 54786
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1723 25 17 37 24 --- 14 | 36 35 31 27 --- 27
R06 |10055 51 35 53 41 --- 24 | 276 283 251 264 --- 271
R07 | 8070 25 17 31 22 --- 13 | 26 24 29 25 --- 19
XR09E |11153 --- --- 12 --- --- 0 | --- --- 42 --- --- 44
R10E | 1752 54 29 43 58 --- 25 | 59 36 47 73 --- 42
R11E | 8428 45 24 80 50 89 27 | 41 32 52 61 11 32
R13E | 2615 62 25 51 45 --- 24 | 45 42 93 61 --- 43
R14E | 4845 41 24 55 48 --- 23 | 44 39 71 57 --- 39
R15E | 8062 73 22 59 49 52 27 | 59 32 33 64 29 35
R17 | 1757 35 13 42 18 --- 14 | 39 54 66 28 --- 42
R18 | 2592 41 16 36 11 --- 14 | 70 65 68 55 --- 61
R19 | 1170 28 6 34 12 --- 11 | 74 76 75 61 --- 70
R20 | 1185 26 11 15 22 --- 10 | 34 54 49 48 --- 45
R21 | 4568 27 14 35 34 --- 15 | 45 58 71 55 --- 50
R22 | 3377 30 21 51 20 --- 16 | 77 81 94 85 --- 78
R23 | 1034 39 14 35 17 --- 14 | 65 43 41 38 --- 41
R24 | 6872 53 20 45 22 429 19 | 237 249 257 246 195 246
------+------------------------------------+--------------------------------
RMS | 5195 43 20 46 34 255 |T 76 75 80 78 78 69
WRMS | 5195 41 16 46 34 255 |NE 89 92 93 84 195 86
MEDI | 3377 39 17 42 22 89 |MD 45 43 66 57 29 43
Table 3.1506.1 GPS week: 1506 Day: 1 MJD: 54787
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2056 24 22 25 28 --- 14 | 22 32 43 32 --- 26
R06 |11929 61 20 49 28 --- 22 | 268 310 315 292 --- 298
R07 | 5946 64 10 25 28 --- 18 | 49 25 28 26 --- 20
R10E | 2235 47 21 35 50 --- 21 | 68 37 55 57 --- 38
R11E | 1346 48 21 40 53 98 22 | 35 28 53 53 12 28
R13E | 1428 63 20 48 63 --- 27 | 42 39 86 66 --- 34
R14E | 2374 44 27 41 51 --- 22 | 38 39 59 55 --- 31
R15E | 3123 52 25 50 54 70 25 | 31 26 52 48 37 23
R17 | 2593 22 28 32 28 --- 16 | 25 37 42 20 --- 23
R18 | 1138 37 16 21 16 --- 13 | 56 52 41 29 --- 42
R19 | 1154 28 14 32 25 --- 13 | 64 58 71 48 --- 57
R20 | 2899 45 11 26 29 --- 15 | 31 32 47 34 --- 28
R21 | 4248 24 18 47 20 --- 16 | 26 33 72 28 --- 33
R22 | 1434 42 23 37 26 --- 18 | 45 60 54 64 --- 51
R23 | 897 35 19 30 24 --- 15 | 73 36 54 34 --- 40
R24 | 3445 25 12 30 23 175 12 | 177 161 173 173 109 167
------+------------------------------------+--------------------------------
RMS | 4005 44 20 37 37 123 |T 65 62 77 66 52 58
WRMS | 4005 42 16 33 37 123 |NE 76 76 85 70 109 71
MEDI | 2235 42 20 32 28 98 |MD 42 37 54 48 37 33
Table 3.1506.2 GPS week: 1506 Day: 2 MJD: 54788
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1665 24 19 19 19 --- 12 | 34 41 32 29 --- 30
R06 |19461 34 29 26 46 --- 19 | 233 253 253 231 --- 243
R07 | 1636 30 21 33 35 --- 16 | 22 37 44 24 --- 25
R10E | 2700 74 22 47 57 --- 29 | 48 43 58 58 --- 42
R11E | 1069 23 15 35 66 71 20 | 30 31 44 49 13 26
R13E | 1329 27 34 153 87 --- 45 | 54 32 143 78 --- 40
R14E | 1766 28 20 39 75 --- 23 | 24 32 54 77 --- 31
R15E | 1671 29 26 53 65 76 24 | 31 27 59 68 40 28
R17 | 1044 23 25 41 28 --- 16 | 26 53 63 25 --- 38
R18 | 1819 37 22 52 17 --- 19 | 26 51 85 48 --- 45
R19 | 1146 26 12 31 22 --- 12 | 46 55 59 43 --- 49
R20 | 2227 28 18 24 28 --- 14 | 24 50 43 38 --- 36
R21 | 3601 32 10 45 26 --- 16 | 21 42 74 58 --- 41
R22 | 1425 23 14 23 15 --- 11 | 39 53 51 51 --- 46
R23 | 1925 46 25 64 36 --- 23 | 26 35 78 26 --- 27
R24 | 3580 68 31 57 46 397 28 | 295 328 334 309 293 314
------+------------------------------------+--------------------------------
RMS | 5259 38 22 55 47 237 |T 61 72 92 75 115 66
WRMS | 5259 31 18 40 47 237 |NE 72 90 101 80 293 81
MEDI | 1671 28 21 39 35 76 |MD 30 42 59 49 40 38
Table 3.1506.3 GPS week: 1506 Day: 3 MJD: 54789
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 974 30 13 34 22 --- 14 | 24 34 49 30 --- 29
R06 |19180 67 48 47 40 --- 29 | 243 290 265 244 --- 262
R07 | 1498 12 11 17 14 --- 8 | 29 21 27 24 --- 19
R10E | 2573 84 19 40 65 --- 30 | 72 59 54 67 --- 51
R11E | 1385 30 32 43 67 --- 25 | 39 41 49 58 --- 33
R13E | 1122 40 24 39 61 --- 23 | 35 63 76 69 --- 53
R14E | 1055 26 20 33 68 --- 22 | 25 23 30 80 --- 27
R15E | 2415 50 29 37 70 136 27 | 21 35 54 80 87 34
R17 | 1312 24 27 21 31 --- 15 | 28 38 52 32 --- 35
R18 | 942 39 16 21 27 --- 14 | 37 62 70 62 --- 55
R19 | 1345 41 16 27 23 --- 15 | 32 59 76 30 --- 48
R20 | 1299 30 16 31 45 --- 18 | 31 50 74 29 --- 44
R21 | 1961 25 24 21 17 --- 13 | 33 63 54 50 --- 48
R22 | 2647 27 16 40 20 --- 15 | 50 59 60 55 --- 52
R23 | 1982 102 59 32 27 --- 34 | 57 65 52 27 --- 31
R24 | 5638 90 46 37 44 448 31 | 129 221 220 174 311 190
------+------------------------------------+--------------------------------
RMS | 5247 52 29 34 45 331 |T 55 73 78 69 199 63
WRMS | 5247 39 21 33 45 331 |NE 63 87 90 68 311 73
MEDI | 1385 30 20 33 31 136 |MD 33 59 54 55 87 44
Table 3.1506.4 GPS week: 1506 Day: 4 MJD: 54790
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1032 39 35 42 27 --- 21 | 44 41 44 23 --- 25
R06 |26006 39 26 23 31 --- 17 | 134 143 123 135 --- 132
R07 | 1957 12 23 25 22 --- 12 | 34 31 40 30 --- 25
R10E | 2092 62 17 37 45 --- 23 | 57 31 38 54 --- 36
R11E | 1988 46 25 35 65 --- 24 | 38 37 33 55 --- 33
R13E | 1258 42 18 25 65 --- 22 | 36 31 35 61 --- 32
R14E | 1277 32 36 27 66 --- 24 | 22 59 45 64 --- 40
R15E | 3625 30 26 30 69 172 23 | 18 36 28 72 28 25
R17 | 2098 37 31 27 27 --- 17 | 32 55 61 30 --- 45
R18 | 859 31 13 26 21 --- 13 | 39 41 56 29 --- 40
R19 | 1834 44 28 21 19 --- 16 | 33 52 42 34 --- 35
R20 | 2755 34 19 21 31 --- 15 | 36 42 59 45 --- 43
R21 | 1412 52 23 14 37 --- 18 | 33 58 48 52 --- 44
R22 | 1948 22 28 26 11 --- 14 | 50 77 55 47 --- 57
R23 | 2463 40 13 23 28 --- 15 | 38 40 52 34 --- 34
R24 | 7914 41 18 24 38 739 17 | 314 303 307 312 188 306
------+------------------------------------+--------------------------------
RMS | 7055 39 25 28 42 536 |T 59 67 66 67 108 59
WRMS | 7055 38 24 28 42 536 |NE 71 80 80 70 188 71
MEDI | 1957 39 23 25 31 172 |MD 36 41 45 47 28 36
Table 3.1506.5 GPS week: 1506 Day: 5 MJD: 54791
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 912 43 35 20 24 --- 18 | 33 27 29 35 --- 24
R06 |15108 44 29 44 31 --- 21 | 222 208 214 189 --- 205
R07 | 1868 28 32 22 17 --- 15 | 24 25 36 25 --- 16
R10E | 2016 80 30 58 48 --- 30 | 55 41 46 58 --- 38
XR11E |10741 95 52 --- 70 --- 49 | 57 54 --- 66 --- 52
R13E | 1521 56 38 41 67 --- 29 | 35 48 66 70 --- 43
R14E | 1706 32 24 40 55 --- 22 | 34 48 39 66 --- 37
R15E | 2759 34 26 42 66 292 25 | 29 17 38 69 34 26
R17 | 1949 43 13 41 18 --- 17 | 23 34 62 41 --- 32
R18 | 1176 28 18 38 19 --- 15 | 44 26 58 31 --- 33
R19 | 1300 33 23 20 29 --- 15 | 28 45 45 31 --- 32
R20 | 3028 37 22 18 17 --- 13 | 32 56 29 42 --- 37
R21 | 1394 60 25 31 27 --- 20 | 23 57 70 66 --- 49
R22 | 1042 26 16 23 19 --- 12 | 56 60 58 40 --- 51
R23 | 2159 58 25 35 14 --- 19 | 31 27 57 40 --- 29
R24 | 5297 47 14 42 25 591 18 | 214 236 254 241 253 235
------+------------------------------------+--------------------------------
RMS | 4481 46 26 36 36 466 |T 58 63 73 69 143 58
WRMS | 4481 42 24 36 36 466 |NE 66 72 82 71 253 67
MEDI | 1868 43 25 38 25 292 |MD 33 45 57 42 34 37
Table 3.1506.6 GPS week: 1506 Day: 6 MJD: 54792
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 1004 35 28 34 26 --- 17 | 40 32 28 34 --- 27
R06 |10385 77 36 54 32 --- 29 | 137 158 151 124 --- 137
R07 | 1956 19 16 24 16 --- 11 | 36 33 37 37 --- 29
R10E | 1936 78 30 32 50 --- 27 | 42 24 35 68 --- 28
R13E | 2142 73 39 46 55 --- 30 | 80 53 82 61 --- 58
R14E | 1999 30 30 30 56 --- 22 | 56 29 35 69 --- 40
R15E | 1074 43 33 34 54 208 24 | 35 25 32 43 38 20
R17 | 2960 47 31 32 33 --- 20 | 48 44 69 29 --- 42
R18 | 2454 28 18 25 21 --- 13 | 60 41 54 50 --- 46
R19 | 632 10 23 33 22 --- 14 | 57 49 79 41 --- 52
R20 | 2743 26 14 32 20 --- 13 | 47 50 46 52 --- 46
R21 | 1528 51 34 41 28 --- 22 | 33 90 96 78 --- 74
R22 | 860 17 22 47 33 --- 18 | 65 74 73 73 --- 66
R23 | 2050 50 30 53 27 --- 23 | 37 42 62 24 --- 26
R24 | 5719 53 19 28 20 --- 17 | 278 281 297 285 --- 283
------+------------------------------------+--------------------------------
RMS | 3548 47 28 37 35 208 |T 70 68 78 71 38 64
WRMS | 3548 44 24 33 35 208 |NE 76 81 90 75 --- 75
MEDI | 1999 43 30 33 28 208 |MD 48 44 62 52 38 46
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