[IGSREPORT-18878] Wk 1595 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Aug 19 04:45:00 PDT 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1595 (Aug 01, 2010 - Aug 07, 2010)
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 2.1595.
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:
igl1595[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1595 in the SP3 format.
igl15957.sum Combination Report for GPS Week 1595.
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 | 359.5 ns
1 | 459.1 ns
2 | 458.4 ns
3 | 459.2 ns
4 | 404.5 ns
5 | 411.6 ns
6 | 458.3 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 1.1595, 1a.1595).
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 2.1595.0-6)
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 3.1595.0-6).
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 1595 summary. (Aug 01, 2010 - Aug 07, 2010)
Table 1.1595.a GPS week : 1595 MJD: 55409.0-55415.0
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 117| 2 0 -6 -4 -4 25 -.13 26 23 | 0 55 1877 2005
| 1 1 2 23 33 144 .04 | 0 221
cod 232| -3 0 -1 38 -9 -23 -.11 15 14 | --- --- --- ---
| 0 1 3 22 28 24 .02 | --- ---
esx 136| 0 0 -2 -36 8 3 .39 25 23 | 98970 782 4042 8071
| 2 3 3 40 24 64 .04 | 36871 3355
gfz 193| 0 0 -4 -56 -17 42 -.14 27 25 | 262697 206 4046 7540
| 2 2 4 35 37 62 .05 | 39608 3983
iac n/a| 3 0 12 -41 1 44 -.08 26 26 | 429980 -237 4040 8077
| 1 1 8 20 14 78 .03 | 38778 1433
mcc n/a| 0 -3 61 -13 73 -81 -.02 153 153 | --- --- --- ---
| 12 18 10 225 74 375 .25 | --- ---
Table 1.1595.b GPS week : 1595 MJD: 55409.0-55415.0
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 | 11 8 13 16 15 11 12 |
R02 | 10 10 7 10 12 9 11 |
R03 | 12 12 11 13 13 11 9 |
R04 | 11 8 9 12 10 8 11 |
R05 | 10 12 10 11 13 11 10 |
R07 | 13 12 13 12 10 10 12 |
R08 | 12 10 12 14 11 11 9 |
R10 | 9 10 11 11 12 11 11 |
R11 | 24 17 20 16 15 18 16 |
R13 | 9 12 14 12 13 13 14 |
R14 | 17 14 15 13 11 13 15 |
R15 | 14 8 12 14 15 10 8 |
R17 | 11 16 14 14 14 11 13 |
R18 | 12 10 10 8 12 9 7 |
R19 | 12 9 11 16 9 15 10 |
R20 | 20 19 26 16 12 14 15 |
R21 | 15 13 9 10 17 11 11 |
R22 | 28 25 15 13 12 7 8 |
R23 | 22 19 15 10 14 9 9 |
R24 | 35 13 10 12 9 9 10 |
Table 1.1595.c GPS week : 1595 MJD: 55409.0-55415.0
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 1595 0 | -196 -121 553 182 -622 -6533 87.5 19420 19420 | 359515 0
brd 1595 1 | 105 -64 551 879 -1626 -12350 88.9 13850 13850 | 459121 0
brd 1595 2 | 167 78 415 841 -286 -8208 90.0 3341 3341 | 458369 0
brd 1595 3 | -24 -41 609 -1711 13 -13520 88.1 3196 3196 | 459212 0
brd 1595 4 | -1 -165 549 604 -556 -16050 84.0 2720 2720 | 404466 0
brd 1595 5 | -36 34 587 -591 -777 -18080 87.5 2013 2013 | 411575 0
brd 1595 6 | -17 7 402 89 -126 -21080 84.6 1738 1738 | 458307 0
-------------+------------------------------------------------------------+----------------
brd 1595 mean| 0 -38 524 42 -568 -13688 87.2 6611 6611 | 430080 0
brd 1595 sdev| 115 86 82 926 544 5205 2.2 7057 7057 | 39300 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 2.1595.0 GPS week: 1595 Day: 0 MJD: 55409
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 117| 0 0 -4 -38 4 -26 -.11 36 26 | 0 99 2194 2597
cod 232| -2 0 -5 62 -22 -24 -.11 17 14 | --- --- --- ---
esx 136| -3 -3 -8 -95 26 71 .47 31 27 | 33133 299 3993 8027
gfz 193| 0 1 -12 -7 -15 56 -.14 31 34 | 188571 408 4049 7479
iac n/a| 4 0 18 -56 -6 18 -.07 26 26 | 359654 129 4017 8190
mcc n/a| -24 10 40 -78 152 -569 -.24 136 136 | --- --- --- ---
Table 2.1595.1 GPS week: 1595 Day: 1 MJD: 55410
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 117| 5 -2 -1 -8 -61 51 -.11 35 27 | 0 108 1501 1624
cod 232| -4 0 -1 52 28 -46 -.13 15 14 | --- --- --- ---
esx 136| 0 -3 -4 -74 25 -56 .39 27 25 | 122075 -2497 3856 8972
gfz 193| -6 0 -6 -13 16 -43 -.16 30 23 | 293521 -4162 3830 7229
iac n/a| 5 1 7 -37 -3 94 -.06 21 21 | 458631 -1100 3817 7778
mcc n/a| -1 22 59 -333 18 -376 -.20 135 135 | --- --- --- ---
Table 2.1595.2 GPS week: 1595 Day: 2 MJD: 55411
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 117| 3 -1 -9 -20 -39 207 -.13 27 26 | 0 222 1971 2067
cod 232| -2 0 -2 26 29 -39 -.08 14 13 | --- --- --- ---
esx 136| 2 0 0 14 3 -37 .35 30 29 | 121863 782 4565 9109
gfz 193| 1 -1 -5 -54 -79 -26 -.05 26 20 | 289007 270 4568 8133
iac n/a| 3 1 12 -38 -18 -71 -.03 26 26 | 457535 1959 4591 8768
mcc n/a| -3 -6 63 -82 -31 -49 -.09 245 245 | --- --- --- ---
Table 2.1595.3 GPS week: 1595 Day: 3 MJD: 55412
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 117| 2 0 -8 -19 6 213 -.09 27 27 | 0 34 2107 2180
cod 232| -4 2 0 34 -16 -26 -.11 15 15 | --- --- --- ---
esx 136| 4 -2 0 6 -4 -78 .35 22 21 | 128878 4096 3719 6316
gfz 193| 1 3 -2 -110 -59 50 -.11 26 26 | 290875 1339 3724 6183
iac n/a| 2 -1 6 -68 2 19 -.12 26 26 | 458484 408 3721 6729
mcc n/a| 11 -37 59 421 70 -410 -.21 231 231 | --- --- --- ---
Table 2.1595.4 GPS week: 1595 Day: 4 MJD: 55413
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 117| 0 0 -6 12 30 -76 -.19 24 24 | 0 -1 1669 1741
cod 232| -3 0 4 67 -39 -42 -.11 17 18 | --- --- --- ---
esx 136| 0 -1 1 -47 18 13 .39 23 21 | 76853 -2122 3779 6952
gfz 193| 1 -2 3 -68 4 57 -.22 25 27 | 240750 -4007 3784 7057
iac n/a| 1 0 -1 -44 26 145 -.12 22 22 | 406055 -1099 3770 7705
mcc n/a| 6 -8 64 40 113 193 .23 110 110 | --- --- --- ---
Table 2.1595.5 GPS week: 1595 Day: 5 MJD: 55414
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 117| 3 -1 -7 22 15 -176 -.17 18 18 | 0 -384 1652 1713
cod 232| -2 -1 0 18 -39 23 -.11 13 12 | --- --- --- ---
esx 136| 0 3 -2 -25 28 90 .38 20 18 | 79416 -1508 4252 8251
gfz 193| 0 2 -4 -75 6 147 -.14 27 29 | 246371 -154 4254 8221
iac n/a| 3 0 18 -42 10 118 -.07 31 31 | 411664 -2459 4237 8680
mcc n/a| 14 -4 73 -62 166 399 -.09 103 103 | --- --- --- ---
Table 2.1595.6 GPS week: 1595 Day: 6 MJD: 55415
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 117| 1 0 -8 22 15 -13 -.09 14 14 | 0 311 2046 2118
cod 232| -2 0 -3 8 -5 -11 -.12 15 14 | --- --- --- ---
esx 136| 0 3 0 -36 -38 23 .40 24 24 | 130572 6430 4134 8875
gfz 193| -1 0 -5 -64 7 52 -.17 22 17 | 289784 7752 4117 8480
iac n/a| 2 0 24 -3 2 -15 -.08 26 26 | 457843 497 4133 8691
mcc n/a| -4 -5 69 0 23 239 .43 113 113 | --- --- --- ---
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 3.1595.0 GPS week: 1595 Day: 0 MJD: 55409
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2118 27 14 20 15 19 --- 11 | 25 28 34 23 21 --- 22
R02 | 1687 26 14 18 23 16 --- 10 | 18 29 26 21 20 --- 18
R03 | 1161 22 13 27 27 20 --- 11 | 19 21 30 23 23 --- 13
R04 | 1952 25 14 14 22 24 --- 11 | 23 27 22 30 22 --- 20
R05 | 2000 16 10 23 22 21 --- 10 | 28 27 27 30 23 --- 21
R07 | 2398 25 13 31 71 23 --- 13 | 16 35 39 68 25 --- 26
R08 | 1725 30 15 17 24 22 119 12 | 21 37 29 25 28 58 26
R10 | 2131 11 14 15 26 20 --- 9 | 32 21 33 31 35 --- 26
R11 | 2067 59 21 37 41 54 --- 24 | 46 41 48 32 18 --- 28
R13 | 6899 19 9 20 20 16 --- 9 | 26 23 38 23 18 --- 19
R14 | 2840 42 19 24 21 35 --- 17 | 30 33 39 39 44 --- 30
R15 | 4143 19 13 42 32 15 44 13 | 13 16 43 38 23 16 18
R17 | 1957 19 11 21 20 22 --- 10 | 43 47 59 53 59 --- 48
R18 | 2763 31 11 27 15 18 --- 12 | 74 71 81 74 72 --- 71
R19 | 1649 24 15 31 20 17 --- 12 | 73 51 62 64 72 --- 60
R20 |83848 45 27 38 31 31 --- 19 | 52 63 44 63 63 --- 52
R21 | 1477 38 15 36 30 18 --- 15 | 51 36 46 29 50 --- 40
R22 | 2172 70 29 61 34 41 --- 27 | 285 224 218 229 287 --- 247
R23 | 2662 65 21 37 46 30 198 21 | 269 317 334 334 297 278 306
XR24 | 8483 82 40 --- 47 29 --- 35 | 191 120 --- 110 146 --- 142
------+-----------------------------------------+-------------------------------------
RMS |19420 36 17 31 31 26 136 |T 66 63 65 66 67 117 61
WRMS |19420 26 14 27 34 26 136 |NE 66 63 65 66 67 117 61
MEDI | 2118 26 14 27 24 21 119 |MD 30 35 39 32 28 58 26
Table 3.1595.1 GPS week: 1595 Day: 1 MJD: 55410
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1306 19 8 19 26 13 --- 8 | 25 20 29 30 23 --- 20
R02 | 1440 25 13 21 21 15 --- 10 | 18 25 27 22 21 --- 14
R03 | 2068 23 9 29 17 24 --- 12 | 16 20 35 22 19 --- 13
R04 | 2120 16 10 17 20 15 --- 8 | 15 14 24 23 13 --- 10
R05 | 1876 30 13 21 22 24 --- 12 | 25 32 36 35 28 --- 25
R07 | 1551 34 17 17 52 18 --- 12 | 28 29 32 65 13 --- 18
R08 | 1681 29 14 14 49 12 115 9 | 22 29 23 36 24 21 23
R10 | 2388 11 11 27 20 20 --- 10 | 27 18 27 29 17 --- 15
R11 | 1201 39 20 32 31 32 --- 17 | 31 26 30 34 24 --- 22
R13 | 3584 26 13 29 28 17 --- 11 | 17 17 34 24 20 --- 16
R14 | 3269 43 12 27 20 15 --- 13 | 39 47 75 65 50 --- 50
R15 | 3185 17 10 20 14 13 43 8 | 14 18 26 20 20 11 12
R17 | 1511 34 20 28 34 33 --- 16 | 35 35 49 56 48 --- 40
R18 | 5594 20 13 13 29 22 --- 10 | 40 37 40 45 42 --- 37
R19 | 2666 14 16 12 25 15 --- 8 | 35 33 42 47 53 --- 38
R20 |60943 38 24 38 33 33 --- 18 | 61 50 53 55 56 --- 48
R21 | 910 17 18 33 22 20 --- 13 | 29 27 31 23 33 --- 24
R22 | 1098 81 21 48 44 28 --- 24 | 126 121 112 114 118 --- 114
R23 | 3845 61 18 40 26 18 200 19 | 308 294 303 307 301 219 298
R24 | 1833 36 18 22 25 20 --- 13 | 63 63 21 71 71 --- 62
------+-----------------------------------------+-------------------------------------
RMS |13851 35 15 27 30 21 135 |T 48 47 52 56 49 83 44
WRMS |13851 27 14 25 23 21 135 |NE 48 47 52 56 49 83 44
MEDI | 1876 26 13 22 25 18 115 |MD 28 29 32 35 24 21 23
Table 3.1595.2 GPS week: 1595 Day: 2 MJD: 55411
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 876 23 14 32 24 24 --- 13 | 14 30 50 30 26 --- 25
R02 | 1472 14 7 11 21 18 --- 7 | 11 18 20 23 22 --- 13
R03 | 2721 17 10 28 9 19 --- 10 | 11 19 36 23 20 --- 15
R04 | 3631 20 9 15 39 16 --- 8 | 16 27 23 34 18 --- 17
R05 | 1143 18 5 28 29 19 --- 10 | 32 32 46 41 40 --- 33
R07 | 2938 22 23 24 20 21 --- 13 | 14 35 26 20 16 --- 20
R08 | 1619 28 16 16 23 22 115 12 | 17 32 25 22 29 39 21
R10 | 4120 27 13 20 14 16 --- 10 | 19 21 26 20 20 --- 15
R11 | 1366 56 13 37 28 32 --- 19 | 37 37 42 28 26 --- 27
R13 | 3142 29 16 35 23 23 --- 14 | 26 21 37 20 20 --- 19
R14 | 3240 33 22 30 28 16 --- 14 | 18 37 30 42 29 --- 24
R15 | 4963 21 9 20 18 34 38 12 | 20 23 29 27 20 8 18
R17 | 902 29 13 18 24 34 --- 13 | 40 46 53 66 61 --- 49
R18 | 7188 19 14 13 36 24 --- 10 | 19 22 27 43 33 --- 20
R19 | 1668 11 12 27 27 23 --- 10 | 28 27 35 30 30 --- 22
R20 | 1817 39 26 69 37 54 --- 26 | 78 80 49 67 90 --- 71
R21 | 1122 15 8 24 18 16 --- 8 | 28 30 42 28 37 --- 31
R22 | 2825 28 11 27 24 37 --- 14 | 97 58 57 61 84 --- 67
R23 | 4811 29 12 43 41 23 406 15 | 119 125 153 148 125 255 127
R24 | 5680 15 10 26 16 23 --- 10 | 54 38 29 38 41 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 3340 27 14 30 26 26 245 |T 34 37 41 40 39 100 33
WRMS | 3340 26 13 29 20 26 245 |NE 34 37 41 40 39 100 33
MEDI | 2721 22 12 26 24 23 115 |MD 20 30 35 30 29 39 22
Table 3.1595.3 GPS week: 1595 Day: 3 MJD: 55412
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 926 21 22 28 24 40 --- 16 | 19 29 39 27 21 --- 20
R02 | 1352 20 16 13 24 20 --- 10 | 13 36 25 33 29 --- 25
R03 | 3002 20 18 17 27 31 --- 12 | 19 42 28 30 41 --- 28
R04 | 3263 23 15 26 20 22 --- 12 | 19 17 29 22 15 --- 13
R05 | 1273 29 13 18 30 15 --- 11 | 30 26 31 29 22 --- 23
R07 | 4191 26 12 22 32 22 --- 11 | 23 30 38 32 23 --- 25
R08 | 1099 23 25 22 17 22 140 13 | 24 39 28 27 23 75 22
R10 | 4611 16 12 24 15 25 --- 11 | 23 17 34 20 26 --- 17
R11 | 1788 33 17 30 35 28 --- 15 | 27 48 56 45 41 --- 39
R13 | 3218 38 13 16 27 15 --- 12 | 32 13 31 37 18 --- 16
R14 | 1139 38 14 19 28 16 --- 12 | 39 34 52 47 35 --- 36
R15 | 1762 26 11 21 14 39 58 14 | 22 23 28 28 21 12 18
R17 | 743 27 11 12 20 42 --- 14 | 44 40 41 40 43 --- 39
R18 | 6582 17 11 10 32 18 --- 8 | 34 32 40 36 38 --- 33
R19 | 1054 42 11 30 19 26 --- 15 | 24 29 56 41 44 --- 32
R20 | 909 33 21 28 39 30 --- 16 | 40 49 48 53 51 --- 41
R21 | 1156 21 15 11 37 20 --- 9 | 41 34 35 34 29 --- 30
R22 | 4115 35 15 18 22 23 --- 13 | 75 76 61 65 81 --- 71
R23 | 4629 16 11 20 13 19 371 9 | 190 181 170 177 178 429 180
R24 | 6066 24 12 28 18 17 --- 12 | 48 34 29 44 61 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 3196 27 15 22 26 26 231 |T 39 41 44 43 42 172 37
WRMS | 3196 27 15 21 26 26 231 |NE 39 41 44 43 42 172 37
MEDI | 1762 24 13 20 24 22 140 |MD 27 34 35 34 29 75 28
Table 3.1595.4 GPS week: 1595 Day: 4 MJD: 55413
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1470 17 32 29 14 21 --- 15 | 25 23 40 20 25 --- 15
R02 | 1396 26 12 23 26 19 --- 11 | 19 29 43 45 35 --- 26
R03 | 3456 14 20 29 16 21 --- 12 | 19 39 39 27 14 --- 21
R04 | 2041 25 11 10 25 19 --- 9 | 33 27 23 34 13 --- 19
R05 | 1098 27 20 21 22 22 --- 13 | 28 34 27 33 40 --- 26
R07 | 3205 25 16 12 20 13 --- 10 | 19 27 20 29 15 --- 16
R08 | 859 25 14 15 38 18 94 10 | 20 42 44 46 29 55 33
R10 | 2471 28 12 22 28 23 --- 12 | 23 16 26 21 26 --- 14
R11 | 1177 29 24 25 28 25 --- 15 | 32 45 48 36 27 --- 35
R13 | 2069 20 13 32 18 21 --- 13 | 30 26 49 29 21 --- 27
R14 | 1380 27 10 18 24 17 --- 10 | 23 49 48 46 40 --- 37
R15 | 3386 21 13 37 31 30 56 15 | 17 22 44 41 17 15 17
R17 | 771 25 18 24 31 29 --- 13 | 26 34 47 32 30 --- 31
R18 | 4656 18 25 22 15 14 --- 12 | 25 36 29 28 21 --- 24
R19 | 699 19 10 14 19 20 --- 9 | 35 26 27 30 27 --- 25
R20 | 1502 23 12 18 30 26 --- 11 | 68 72 56 66 70 --- 65
R21 | 1537 30 23 31 24 34 --- 17 | 25 42 26 32 43 --- 30
R22 | 4299 20 7 26 22 26 --- 12 | 60 44 53 40 42 --- 45
R23 | 4133 36 18 22 20 14 155 13 | 116 125 126 125 118 184 121
R24 | 5236 18 15 14 31 16 --- 9 | 32 23 36 36 36 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 2720 24 17 23 25 22 110 |T 33 39 42 39 34 84 32
WRMS | 2720 24 18 21 27 22 110 |NE 33 39 42 39 34 84 32
MEDI | 1537 25 14 22 24 21 94 |MD 25 34 40 33 27 55 26
Table 3.1595.5 GPS week: 1595 Day: 5 MJD: 55414
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1486 19 16 11 17 30 --- 10 | 12 26 31 22 16 --- 18
R02 | 1066 12 12 14 22 28 --- 9 | 18 23 21 19 20 --- 15
R03 | 1678 21 7 21 32 28 --- 11 | 15 28 46 46 39 --- 29
R04 | 1673 16 7 17 24 16 --- 8 | 22 25 29 38 22 --- 22
R05 | 931 13 12 9 24 40 --- 10 | 32 37 31 31 35 --- 31
R07 | 1540 16 10 11 37 37 --- 10 | 12 22 27 27 22 --- 17
R08 | 2179 20 20 14 24 20 107 11 | 9 31 22 36 13 27 15
R10 | 1618 20 13 21 17 22 --- 10 | 17 27 36 37 20 --- 22
R11 | 1213 24 18 19 39 68 --- 17 | 16 32 33 32 32 --- 21
R13 | 1471 20 11 30 19 27 --- 12 | 20 28 52 37 35 --- 28
R14 | 1262 27 7 11 30 45 --- 12 | 48 56 56 67 72 --- 55
R15 | 1769 13 8 25 24 22 81 10 | 20 17 43 33 17 14 18
R17 | 813 16 10 23 40 26 --- 10 | 30 28 45 51 35 --- 31
R18 | 2844 15 12 18 28 23 --- 9 | 25 29 26 24 29 --- 22
R19 | 950 12 21 38 20 21 --- 14 | 27 27 36 33 36 --- 22
R20 | 1781 26 10 24 35 39 --- 13 | 40 56 59 53 54 --- 51
R21 | 868 25 8 16 19 31 --- 11 | 23 29 25 25 35 --- 24
R22 | 2046 12 10 13 24 19 --- 7 | 68 58 59 52 59 --- 58
R23 | 3115 16 13 16 17 18 119 8 | 128 140 135 137 129 152 133
R24 | 5065 12 11 20 32 17 --- 8 | 34 20 20 31 28 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 2013 18 13 20 27 31 103 |T 30 36 41 41 37 64 32
WRMS | 2013 18 12 18 29 31 103 |NE 30 36 41 41 37 64 32
MEDI | 1540 16 11 17 24 26 107 |MD 22 28 33 33 32 27 22
Table 3.1595.6 GPS week: 1595 Day: 6 MJD: 55415
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2001 15 20 23 19 29 --- 12 | 23 34 33 30 15 --- 22
R02 | 1048 14 9 19 17 30 --- 10 | 19 21 22 18 19 --- 17
R03 | 1135 10 15 21 15 19 --- 9 | 18 25 27 23 25 --- 19
R04 | 1395 17 18 18 29 19 --- 10 | 25 38 43 41 22 --- 30
R05 | 1507 8 17 23 26 18 --- 9 | 28 45 23 27 33 --- 30
R07 | 2438 14 21 26 27 21 --- 11 | 22 35 30 45 18 --- 24
R08 | 2868 10 13 13 25 24 121 8 | 14 31 21 33 19 56 18
R10 | 1583 8 16 19 16 32 --- 11 | 16 17 19 19 39 --- 18
R11 | 1927 21 16 30 30 46 --- 16 | 18 25 27 22 21 --- 14
R13 | 1256 15 15 33 14 32 --- 13 | 28 28 36 33 20 --- 24
R14 | 1230 18 13 32 20 41 --- 14 | 29 35 51 44 33 --- 33
R15 | 1370 11 10 10 20 20 89 7 | 19 18 26 22 20 18 17
R17 | 839 23 14 28 36 19 --- 12 | 48 43 39 48 46 --- 42
R18 | 1782 8 7 14 14 19 --- 6 | 27 27 31 24 31 --- 26
R19 | 1068 15 14 25 20 17 --- 10 | 29 21 37 31 28 --- 24
R20 | 1249 24 10 36 22 29 --- 14 | 56 60 55 66 64 --- 56
R21 | 1145 13 9 30 24 25 --- 11 | 22 29 37 24 33 --- 26
R22 | 1143 11 11 15 12 15 --- 7 | 70 59 51 52 61 --- 59
R23 | 1146 9 17 21 12 16 125 9 | 135 138 147 138 143 151 139
R24 | 3729 8 14 24 14 22 --- 9 | 40 28 32 29 39 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 1737 14 14 24 22 26 113 |T 34 37 39 38 36 75 33
WRMS | 1737 14 14 24 17 26 113 |NE 34 37 39 38 36 75 33
MEDI | 1256 13 14 23 20 21 121 |MD 25 29 32 30 28 56 24
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