[IGSREPORT-19216] Wk 1610 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Fri Dec 3 05:11:50 PST 2010
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1610 (Nov 14, 2010 - Nov 20, 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 2.1610.
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:
igl1610[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1610 in the SP3 format.
igl16107.sum Combination Report for GPS Week 1610.
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 | 354.7 ns
1 | 339.6 ns
2 | 359.8 ns
3 | 421.3 ns
4 | 372.0 ns
5 | 357.9 ns
6 | 407.5 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 1.1610, 1a.1610).
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 2.1610.0-6)
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 3.1610.0-6).
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 1610 summary. (Nov 14, 2010 - Nov 20, 2010)
Table 1.1610.a GPS week : 1610 MJD: 55514.0-55520.0
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 120| 3 0 14 4 -5 -7 -.09 30 29 | 0 783 9741 11701
| 2 1 2 36 16 75 .17 | 0 2053
cod 230| -2 0 -4 48 7 -22 -.05 14 12 | --- --- --- ---
| 0 1 3 27 10 30 .04 | --- ---
esx 143| -1 -1 -8 -19 -15 -5 .34 28 23 | 20627 1261 4944 9163
| 3 1 5 19 13 33 .06 | 32109 4900
gfz 189| 0 -1 -9 -64 -6 -64 -.17 39 30 | 204570 1043 4961 9053
| 1 2 6 76 46 37 .12 | 29033 5642
iac n/a| 4 0 5 -51 4 49 -.14 27 27 | 373471 -1147 4939 9826
| 1 2 8 30 10 80 .08 | 29723 1706
mcc n/a| 15 -3 36 -108 109 1136 -.22 240 240 | --- --- --- ---
| 21 4 23 167 80 672 .47 | --- ---
Table 1.1610.b GPS week : 1610 MJD: 55514.0-55520.0
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 | 15 10 13 12 13 14 13 |
R02 | 10 9 10 10 8 8 10 |
R05 | 18 14 9 12 8 10 9 |
R07 | 12 10 12 12 10 14 14 |
R08 | 15 9 10 9 11 9 10 |
R09 | 16 16 13 12 11 17 10 |
R10 | 17 13 24 18 12 11 10 |
R11 | 19 13 29 41 19 18 15 |
R12 | 16 10 11 12 20 28 10 |
R13 | 14 11 13 17 12 14 8 |
R15 | 11 7 12 20 15 11 11 |
R16 | 15 13 16 13 13 19 10 |
R17 | 7 10 15 16 18 12 17 |
R18 | 13 9 10 9 8 11 12 |
R19 | 12 13 12 14 13 13 9 |
R20 | 10 13 16 13 19 13 12 |
R21 | 13 9 13 10 10 12 17 |
R22 | 18 13 10 16 14 11 18 |
R23 | 12 13 14 9 12 11 10 |
R24 | 14 14 14 14 11 9 14 |
Table 1.1610.c GPS week : 1610 MJD: 55514.0-55520.0
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 1610 0 | 114 -68 128 -1982 -241 -21980 87.7 2016 2016 | 354739 0
brd 1610 1 | 57 114 171 -1389 162 -23480 86.5 2379 2379 | 339620 0
brd 1610 2 | -2 50 210 323 -1089 -26510 84.0 2684 2684 | 359774 0
brd 1610 3 | 32 59 343 187 -1614 -22070 88.2 3144 3144 | 421308 0
brd 1610 4 | 8 73 172 1503 -914 -16340 83.1 2621 2621 | 371977 0
brd 1610 5 | -24 61 125 -523 -4365 -14600 83.6 2381 2381 | 357882 0
brd 1610 6 | -37 -109 252 3471 -831 -17190 82.1 2156 2156 | 407530 0
-------------+------------------------------------------------------------+----------------
brd 1610 mean| 21 25 200 227 -1270 -20310 85.0 2483 2483 | 373261 0
brd 1610 sdev| 52 81 77 1835 1480 4329 2.4 374 374 | 29938 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 2.1610.0 GPS week: 1610 Day: 0 MJD: 55514
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 120| 0 1 12 -45 -29 -7 .11 28 27 | 0 1222 6217 7659
cod 230| -1 0 -1 72 7 21 -.06 16 15 | --- --- --- ---
esx 143| 3 -1 -15 -39 -6 -4 .30 30 23 | 301 -4475 4536 9330
gfz 189| 0 0 -11 -55 -38 -59 -.26 37 28 | 193668 -4305 4593 9519
iac n/a| 4 0 6 -63 2 -41 -.26 27 27 | 356032 -3172 4531 10317
mcc n/a| 29 -3 67 -401 42 1640 -.80 208 208 | --- --- --- ---
Table 2.1610.1 GPS week: 1610 Day: 1 MJD: 55515
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 120| 1 -1 10 -33 0 41 -.02 22 22 | 0 141 11876 13958
cod 230| -1 0 -4 76 11 -47 -.09 12 11 | --- --- --- ---
esx 143| -1 0 -11 -39 -14 5 .31 23 20 | -24233 -423 5125 8665
gfz 189| -1 -4 -15 -165 -66 -18 -.18 40 26 | 171532 567 5125 8644
iac n/a| 3 1 13 -80 7 22 -.17 25 25 | 338589 -947 5134 9721
mcc n/a| 54 3 58 -178 256 2076 -.79 236 236 | --- --- --- ---
Table 2.1610.2 GPS week: 1610 Day: 2 MJD: 55516
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 120| 6 -1 17 5 -16 -9 -.02 29 27 | 0 1307 6152 7705
cod 230| -3 1 -3 76 20 -62 -.04 17 14 | --- --- --- ---
esx 143| -3 0 -9 -12 -21 51 .33 28 25 | 18337 -267 4643 9732
gfz 189| -1 -1 -10 -169 27 -89 -.12 35 26 | 195030 -3036 4651 9809
iac n/a| 4 0 -1 -80 -5 71 -.18 28 28 | 360968 -2110 4638 10706
mcc n/a| -11 -5 35 -56 78 886 .21 230 230 | --- --- --- ---
Table 2.1610.3 GPS week: 1610 Day: 3 MJD: 55517
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 120| 7 3 15 -1 19 12 .08 35 30 | 0 2426 8962 11056
cod 230| -2 -2 0 48 18 -46 -.10 17 12 | --- --- --- ---
esx 143| -7 -3 -2 7 -38 -4 .31 29 24 | 64609 -267 5441 8503
gfz 189| -1 0 0 -26 74 -52 -.26 49 38 | 252584 491 5437 8283
iac n/a| 7 2 -7 -37 22 123 -.16 32 32 | 420197 -1217 5409 8946
mcc n/a| 11 -5 31 144 154 1392 -.22 274 274 | --- --- --- ---
Table 2.1610.4 GPS week: 1610 Day: 4 MJD: 55518
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 120| 1 1 16 45 -14 -136 -.22 30 28 | 0 -2162 14552 16938
cod 230| -1 0 -3 32 2 -11 -.06 14 12 | --- --- --- ---
esx 143| -1 -2 -9 3 -15 -55 .44 28 25 | 14742 10325 4850 8394
gfz 189| 1 -2 -10 -49 -34 -86 -.34 37 27 | 195291 12518 4856 8339
iac n/a| 3 0 1 -48 -4 163 -.17 24 24 | 369968 2281 4852 8972
mcc n/a| 4 1 28 -38 116 1259 .42 243 243 | --- --- --- ---
Table 2.1610.5 GPS week: 1610 Day: 5 MJD: 55519
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 120| 3 0 14 11 -3 -56 -.30 37 35 | 0 3783 7735 9105
cod 230| -2 1 -6 6 -3 -9 -.03 12 10 | --- --- --- ---
esx 143| 0 0 0 -20 7 4 .29 28 24 | 9296 5173 4617 8735
gfz 189| 0 1 -2 -25 -1 -122 -.07 36 29 | 186882 3091 4678 8261
iac n/a| 2 -4 10 7 13 59 -.00 29 29 | 359831 -1930 4607 9199
mcc n/a| 6 -10 39 -66 8 667 -.01 255 255 | --- --- --- ---
Table 2.1610.6 GPS week: 1610 Day: 6 MJD: 55520
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 120| 1 -1 17 51 5 105 -.28 31 32 | 0 -1232 12697 15489
cod 230| -1 -1 -9 27 -7 0 .01 11 10 | --- --- --- ---
esx 143| 0 0 -7 -36 -17 -36 .41 27 22 | 61342 -1238 5398 10785
gfz 189| -2 1 -18 38 -6 -21 -.00 36 35 | 237006 -2025 5393 10517
iac n/a| 3 2 17 -57 -4 -54 -.06 24 24 | 408714 -935 5407 10922
mcc n/a| 11 -4 -4 -163 107 33 -.36 234 234 | --- --- --- ---
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 3.1610.0 GPS week: 1610 Day: 0 MJD: 55514
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 1420 30 16 27 19 33 --- 15 | 42 48 52 53 64 --- 49
R02 | 1527 24 11 13 22 23 --- 10 | 39 24 28 30 39 --- 28
R05 | 1931 37 24 28 32 34 168 17 | 19 35 31 26 29 65 21
R07 | 1974 23 13 26 --- 20 --- 11 | 22 25 32 --- 27 --- 20
R08 | 1684 39 20 16 18 22 256 14 | 23 27 26 26 38 85 25
R09E | 3339 28 15 36 33 33 --- 15 | 59 54 67 52 56 --- 53
R10E | 3186 36 17 26 37 42 --- 17 | 40 53 45 39 48 --- 45
R11E | 2740 34 22 46 56 31 274 18 | 91 102 114 121 105 179 99
R12E | 1877 30 15 33 35 36 --- 16 | 53 56 71 66 53 --- 53
R13E | 1124 20 11 32 38 31 --- 13 | 53 73 73 82 66 --- 65
R15E | 3303 13 15 29 28 18 192 11 | 22 30 35 31 31 26 24
R16E | 3062 31 14 35 32 27 --- 15 | 51 52 59 65 54 --- 52
R17 | 873 14 7 12 59 15 --- 6 | 42 53 50 61 51 --- 48
R18 | 1118 34 11 21 24 26 199 13 | 36 51 72 69 68 140 55
R19 | 1530 28 11 20 25 22 --- 11 | 46 66 74 68 73 --- 64
R20 | 1667 20 11 17 27 20 --- 9 | 32 43 51 55 62 --- 46
R21 | 1704 16 13 34 59 26 --- 12 | 47 60 57 76 61 --- 54
R22 | 790 24 25 54 37 18 --- 18 | 57 70 83 64 52 --- 59
R23 | 855 25 13 25 30 20 119 11 | 28 44 57 56 41 68 40
R24 | 1092 26 22 28 44 18 --- 13 | 18 51 52 73 43 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 2016 28 16 30 37 27 208 |T 41 50 56 58 53 93 46
WRMS | 2016 27 15 23 28 27 208 |NE 35 47 52 54 51 89 44
MEDI | 1667 26 14 27 32 23 192 |MD 40 51 52 61 52 68 48
Table 3.1610.1 GPS week: 1610 Day: 1 MJD: 55515
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2142 19 11 15 21 27 --- 10 | 36 35 44 46 49 --- 37
R02 | 1336 16 9 22 16 15 --- 8 | 26 29 35 23 26 --- 26
R05 | 1318 31 9 33 27 21 267 13 | 28 33 41 36 36 96 28
R07 | 1830 19 10 14 31 23 --- 9 | 19 24 28 55 29 --- 21
R08 | 1769 19 7 15 24 22 295 8 | 21 25 26 36 35 132 23
R09E | 2950 26 19 33 33 33 --- 15 | 29 26 35 39 32 --- 21
R10E | 5324 28 14 23 20 26 --- 12 | 53 67 80 71 57 --- 63
R11E | 4679 19 13 31 29 28 311 13 | 76 79 100 92 80 226 81
R12E | 1487 18 11 18 34 27 --- 10 | 32 30 31 51 35 --- 28
R13E | 1257 18 9 23 42 24 --- 10 | 42 51 61 64 50 --- 49
R15E | 2763 13 10 13 35 16 158 7 | 32 36 46 41 37 28 36
R16E | 2052 21 12 31 42 23 --- 12 | 31 43 60 68 43 --- 39
R17 | 1473 19 11 14 80 24 --- 9 | 26 44 35 102 54 --- 38
R18 | 1232 20 12 16 66 13 167 8 | 33 49 32 64 41 152 39
R19 | 1727 31 7 15 54 35 --- 13 | 37 50 48 54 78 --- 50
R20 | 3257 9 20 17 27 37 --- 12 | 37 30 48 67 42 --- 35
R21 | 1168 13 15 17 35 16 --- 9 | 42 23 26 45 34 --- 25
R22 | 1206 11 16 33 23 28 --- 13 | 39 51 37 42 42 --- 40
R23 | 1317 37 11 18 29 24 159 13 | 20 35 35 44 35 90 28
R24 | 1460 28 7 41 55 16 --- 14 | 13 23 57 64 24 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 2378 22 12 23 40 25 236 |T 33 39 45 55 42 120 36
WRMS | 2378 22 11 20 26 25 236 |NE 29 35 38 51 41 117 32
MEDI | 1487 19 11 18 31 24 167 |MD 32 35 37 51 37 96 35
Table 3.1610.2 GPS week: 1610 Day: 2 MJD: 55516
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 2839 25 14 22 21 28 --- 12 | 41 31 40 52 57 --- 39
R02 | 534 18 13 20 20 18 --- 10 | 26 25 26 34 31 --- 23
R05 | 3490 12 11 20 18 20 110 9 | 17 25 43 27 29 106 23
R07 | 2743 22 12 15 26 29 --- 11 | 26 36 40 42 35 --- 30
R08 | 800 22 14 13 18 15 81 9 | 33 33 40 35 42 115 34
R09E | 2421 25 14 25 53 24 --- 12 | 46 38 56 57 48 --- 42
R10E | 3872 59 31 43 51 36 --- 24 | 37 93 108 104 65 --- 74
R11E | 5255 61 31 61 53 51 --- 29 | 75 137 165 157 130 --- 123
R12E | 1618 19 12 15 21 28 --- 11 | 45 43 54 49 42 --- 42
R13E | 2051 31 20 18 26 20 --- 13 | 47 88 82 91 68 --- 73
R15E | 2921 23 15 22 42 25 --- 12 | 32 35 46 58 31 --- 32
R16E | 2245 29 20 27 38 32 --- 15 | 43 63 67 75 58 --- 55
R17 | 2566 24 20 25 23 33 --- 14 | 36 56 66 61 55 --- 52
R18 | 2118 25 9 16 28 21 422 10 | 32 45 57 50 62 269 46
R19 | 3182 29 13 18 22 21 --- 11 | 39 66 53 73 70 --- 56
R20 | 2219 25 16 14 58 46 --- 15 | 44 45 53 82 76 --- 52
R21 | 1462 18 14 35 43 20 --- 13 | 32 39 74 45 43 --- 44
R22 | 764 20 12 21 14 19 --- 10 | 51 57 60 61 55 --- 53
R23 | 938 27 14 35 28 22 120 14 | 28 35 46 49 36 133 31
R24 | 4096 15 18 35 41 24 --- 13 | 26 51 35 65 39 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2684 29 17 27 35 28 230 |T 37 52 60 63 53 155 47
WRMS | 2684 27 14 25 26 28 230 |NE 33 42 49 52 49 155 40
MEDI | 2245 24 14 21 26 24 110 |MD 36 43 53 57 48 115 42
Table 3.1610.3 GPS week: 1610 Day: 3 MJD: 55517
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3420 31 14 15 27 27 --- 12 | 40 47 43 58 58 --- 45
R02 | 1788 19 8 21 27 19 --- 9 | 30 29 24 43 26 --- 25
R05 | 3199 15 17 28 22 22 93 12 | 29 35 30 35 29 44 27
R07 | 3166 25 14 19 156 26 --- 11 | 28 35 41 148 35 --- 32
R08 | 619 20 8 12 16 22 74 8 | 22 27 28 35 35 46 25
R09E | 2857 24 17 17 45 24 --- 11 | 51 72 70 66 61 --- 63
R10 | 5270 41 14 42 39 30 --- 18 | 53 86 104 97 71 --- 78
R11 | 3156 101 41 69 73 81 525 40 | 75 139 165 172 86 377 109
R12E | 2694 30 12 24 20 20 --- 12 | 54 52 67 61 54 --- 52
R13 | 3078 44 22 24 31 28 --- 16 | 34 72 71 71 39 --- 53
R15 | 4402 40 22 24 26 51 --- 19 | 34 45 57 44 51 --- 43
R16E | 1729 22 20 29 22 19 --- 13 | 36 60 71 69 62 --- 57
R17 | 2581 30 13 23 63 43 --- 15 | 50 56 51 51 84 --- 58
R18 | 1193 21 10 18 15 13 289 8 | 37 49 61 52 51 157 49
R19 | 3722 35 16 25 16 23 --- 13 | 49 66 72 66 59 --- 60
R20 | 3774 23 14 25 29 26 --- 12 | 49 61 61 72 75 --- 59
R21 | 4347 23 10 20 34 19 --- 10 | 42 63 65 78 75 --- 61
R22 | 863 23 12 43 31 26 --- 15 | 44 50 80 58 51 --- 53
R23 | 939 12 9 18 34 23 55 9 | 37 41 48 43 45 75 41
R24 | 4516 25 15 18 37 35 --- 13 | 25 39 52 57 76 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 3143 35 17 29 49 32 274 |T 40 56 63 68 56 139 51
WRMS | 3143 30 12 24 38 32 274 |NE 37 46 51 54 55 80 45
MEDI | 3078 24 14 23 29 24 93 |MD 37 50 61 58 54 75 52
Table 3.1610.4 GPS week: 1610 Day: 4 MJD: 55518
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 4867 33 11 19 31 27 --- 12 | 34 39 42 44 46 --- 38
R02 | 1893 12 10 12 16 18 --- 7 | 34 28 25 26 32 --- 27
R05 | 2505 19 9 13 25 18 80 8 | 28 20 27 33 31 55 22
R07 | 2807 21 13 22 55 15 --- 10 | 27 32 39 81 36 --- 31
R08 | 1410 25 10 23 25 23 70 11 | 38 34 40 41 44 42 35
R09E | 1232 26 17 12 31 19 --- 10 | 45 54 55 61 50 --- 47
R10 | 4417 15 14 31 26 22 --- 12 | 64 67 72 64 65 --- 65
R11 | 2145 57 16 35 70 24 461 18 | 81 98 99 99 86 214 89
R12E | 2016 33 19 50 47 41 --- 20 | 48 64 93 91 45 --- 57
R13 | 2866 33 6 26 25 17 --- 11 | 57 59 65 57 63 --- 58
R15 | 2852 33 9 11 20 41 --- 14 | 41 36 48 46 39 --- 38
R16E | 642 30 18 19 32 21 --- 12 | 43 56 66 69 48 --- 49
R17 | 2540 31 18 41 45 36 --- 17 | 57 60 60 64 48 --- 51
R18 | 2103 12 8 20 29 17 263 8 | 45 36 46 42 48 149 39
R19 | 736 33 17 22 26 19 --- 12 | 26 48 53 54 35 --- 38
R20 | 2925 51 15 39 46 32 --- 19 | 31 68 94 95 79 --- 67
R21 | 3937 25 14 20 42 12 --- 10 | 38 66 67 77 55 --- 57
R22 | 1099 27 15 44 46 11 --- 14 | 48 52 100 70 63 --- 61
R23 | 934 17 16 31 32 17 51 11 | 39 24 54 49 34 90 31
R24 | 3142 20 15 21 32 20 --- 10 | 34 49 33 55 58 --- 43
------+-----------------------------------------+-------------------------------------
RMS | 2620 30 14 28 37 24 243 |T 42 49 58 60 50 110 47
WRMS | 2620 28 12 25 27 24 243 |NE 37 43 53 54 47 84 42
MEDI | 2145 26 14 22 31 19 80 |MD 39 49 54 57 48 90 43
Table 3.1610.5 GPS week: 1610 Day: 5 MJD: 55519
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 3174 47 9 17 23 33 --- 14 | 28 41 44 46 52 --- 39
R02 | 1792 19 6 18 13 18 --- 8 | 27 24 30 32 27 --- 24
R05 | 1297 20 9 13 12 32 100 10 | 23 30 30 32 42 89 28
R07E | 2369 37 15 18 58 34 --- 13 | 35 37 39 58 46 --- 33
R08 | 2631 22 7 11 16 25 98 8 | 32 27 33 27 32 76 28
R09 | 1857 60 14 30 36 30 --- 17 | 56 83 92 98 70 --- 76
R10 | 2966 24 10 17 28 27 --- 10 | 29 30 41 35 37 --- 31
R11 | 1772 49 17 35 68 35 400 17 | 74 64 63 72 63 193 60
R12 | 2046 51 23 81 41 38 --- 27 | 65 73 98 93 58 --- 68
R13 | 2733 38 6 33 18 25 --- 13 | 41 43 68 54 37 --- 44
R15 | 4935 29 10 21 28 26 --- 11 | 25 26 32 33 29 --- 24
R16 | 1308 63 19 27 28 37 --- 19 | 44 94 101 99 69 --- 81
R17 | 3395 28 11 16 49 34 --- 12 | 66 51 39 37 30 --- 45
R18 | 1371 28 10 20 27 28 377 11 | 25 26 52 40 52 253 35
R19 | 925 26 16 28 68 27 --- 13 | 30 35 24 69 28 --- 25
R20 | 1068 34 6 22 17 32 --- 12 | 37 48 64 49 57 --- 51
R21 | 1744 37 10 20 23 21 --- 11 | 35 54 59 54 59 --- 52
R22 | 910 37 12 20 23 17 --- 11 | 24 49 47 53 54 --- 44
R23 | 1072 35 6 18 46 26 65 11 | 16 36 38 51 51 130 34
R24 | 3513 14 9 24 16 16 --- 8 | 37 35 42 36 31 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2381 37 12 28 36 29 255 |T 37 45 51 53 46 148 42
WRMS | 2381 35 10 24 29 29 255 |NE 31 38 41 43 42 137 36
MEDI | 1792 34 10 20 27 27 100 |MD 32 37 42 49 46 130 35
Table 3.1610.6 GPS week: 1610 Day: 6 MJD: 55520
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz iac mcc IGL | bkg cod esx gfz iac mcc IGL
------+-----------------------------------------+-------------------------------------
R01 | 979 30 15 21 31 31 --- 13 | 40 42 44 46 59 --- 42
R02 | 1388 22 10 19 24 19 --- 9 | 27 30 36 28 40 --- 30
R05 | 998 22 10 15 23 20 128 9 | 24 31 29 31 32 106 26
R07E | 4717 39 13 35 44 21 --- 14 | 34 40 46 54 36 --- 36
R08 | 3802 18 11 23 17 18 65 9 | 35 30 26 37 32 86 28
R09 | 2115 23 10 20 27 21 --- 9 | 55 47 45 54 56 --- 48
R10 | 2508 22 12 18 28 23 --- 10 | 69 73 81 70 71 --- 72
R11 | 2212 32 16 34 40 31 231 15 | 65 65 88 94 66 275 65
R12 | 1818 21 12 16 31 23 --- 10 | 50 51 54 51 43 --- 47
R13 | 1618 20 8 16 34 17 --- 8 | 28 32 39 42 31 --- 30
R15 | 2369 25 12 17 24 27 --- 11 | 40 42 49 46 45 --- 42
R16 | 2307 21 10 21 36 22 --- 9 | 58 58 62 62 50 --- 55
R17 | 2010 39 13 27 11 44 --- 16 | 51 58 68 55 63 --- 58
R18 | 1167 21 12 30 19 24 244 11 | 41 50 58 57 71 320 53
R19 | 1553 17 8 16 78 23 --- 8 | 44 58 54 83 53 --- 53
R20 | 2225 32 9 25 42 21 --- 11 | 40 58 60 67 63 --- 55
R21 | 1214 52 8 50 22 15 --- 17 | 40 72 103 79 68 --- 70
R22 | 874 43 13 54 44 22 --- 18 | 50 72 118 92 79 --- 77
R23 | 1142 33 7 16 40 16 376 9 | 31 56 59 71 62 204 53
R24 | 1867 50 6 29 53 16 --- 14 | 28 60 73 84 60 --- 56
------+-----------------------------------------+-------------------------------------
RMS | 2155 31 11 27 36 24 234 |T 42 51 59 60 54 198 49
WRMS | 2155 32 10 22 35 24 234 |NE 37 51 60 60 56 179 50
MEDI | 1818 23 10 21 31 21 231 |MD 40 51 54 55 56 204 53
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