[IGSREPORT-19728] Wk 1632 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Fri May 6 09:04:56 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1632 (Apr 17, 2011 - Apr 23, 2011)
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
center's 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 2.1632.
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:
igl1632[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1632 in the SP3 format.
igl16327.sum Combination Report for GPS Week 1632.
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. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics initially.
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
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.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
ftp://igs.org/igscb/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
ftp://igs.org/igscb/station/general/igs08.atx
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 | 381.5 ns
1 | 335.9 ns
2 | 365.0 ns
3 | 360.6 ns
4 | 374.2 ns
5 | 324.3 ns
6 | 343.7 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
----+--------+---------------
0 | BKG | R03 R10 R11
1 | BKG | R09 R11 R13
2 | BKG | R09 R12 R16
6 | BKG | R22
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 1.1632, 1a.1632).
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 2.1632.0-6)
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 3.1632.0-6).
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 1632 summary. (Apr 17, 2011 - Apr 23, 2011)
Table 1.1632.a GPS week : 1632 MJD: 55668.0-55674.0
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 151| 2 6 10 -99 54 219 -.31 72 57 | 0 882 2793 3009
| 4 3 12 54 68 102 .10 | 0 843
cod 243| 0 0 0 33 -14 -35 -.21 24 24 | --- --- --- ---
| 1 2 3 37 25 33 .04 | --- ---
esx 138| 0 0 1 30 38 -22 .38 19 17 | 3659 -563 4746 8364
| 0 1 2 19 22 31 .05 | 21781 3846
gfz 189| 0 0 0 -50 -32 -11 -.21 22 20 | 181500 -571 4734 8416
| 1 2 3 49 28 26 .08 | 20230 3339
grg 131| -1 -3 -15 16 -8 55 .10 53 50 | --- --- --- ---
| 2 2 10 37 79 68 .16 | --- ---
iac n/a| -2 0 -12 -20 -49 11 .03 54 54 | 355654 -667 4741 8685
| 2 2 6 27 29 195 .08 | 21419 886
mcc n/a| 0 -2 36 62 55 710 -.06 152 152 | --- --- --- ---
| 7 10 17 75 69 281 .32 | --- ---
Table 1.1632.b GPS week : 1632 MJD: 55668.0-55674.0
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 | 16 12 13 12 15 14 12 |
R02 | 14 13 10 13 13 13 14 |
R03 | 13 14 14 17 11 12 12 |
R04 | 602 272 1011 327 111 152 113 |
R05 | 16 18 16 13 16 18 15 |
R06 | 14 16 17 16 12 14 13 |
R07 | 13 15 13 12 12 10 12 |
R08 | 20 16 12 15 14 14 12 |
R09 | 14 13 13 14 14 15 15 |
R10 | 20 14 12 12 14 10 13 |
R11 | 20 23 21 17 16 20 16 |
R12 | 15 17 14 10 11 12 13 |
R13 | 14 18 17 12 12 16 14 |
R15 | 14 17 16 18 14 21 15 |
R16 | 13 16 16 12 15 16 15 |
R17 | 20 28 19 20 16 12 13 |
R18 | 16 17 21 16 17 11 16 |
R19 | 16 17 17 12 13 13 13 |
R20 | 15 18 15 24 18 20 25 |
R21 | 12 20 14 15 18 13 14 |
R22 | 12 13 15 12 13 12 14 |
R23 | 14 17 11 13 20 13 11 |
R24 | 16 22 15 13 13 11 12 |
Table 1.1632.c GPS week : 1632 MJD: 55668.0-55674.0
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 1632 0 | 0 31 243 -3137 -53 -6035 84.8 1829 1829 | 381501 0
brd 1632 1 | 0 94 270 -1480 -832 -8036 86.7 2141 2141 | 335883 0
brd 1632 2 | -24 -80 195 853 -430 -16100 84.5 2065 2065 | 365016 0
brd 1632 3 | -56 -8 223 -198 -1396 -19260 83.4 1879 1879 | 360560 0
brd 1632 4 | 13 -64 232 2979 -696 -23310 83.5 2448 2448 | 374193 0
brd 1632 5 | 23 -18 288 -389 -1758 -15960 85.5 2339 2339 | 324312 0
brd 1632 6 | 19 -8 407 -925 75 -12360 86.0 2415 2415 | 343732 0
-------------+------------------------------------------------------------+----------------
brd 1632 mean| -3 -7 265 -328 -727 -14437 84.9 2159 2159 | 355028 0
brd 1632 sdev| 28 58 69 1911 671 6095 1.3 250 250 | 20960 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 2.1632.0 GPS week: 1632 Day: 0 MJD: 55668
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 151| -2 10 -5 -66 88 156 -.36 74 70 | 0 2469 2956 3060
cod 243| 0 1 2 61 -25 9 -.20 25 22 | --- --- --- ---
esx 138| 1 -2 3 54 47 -35 .39 19 18 | 28154 -4598 4982 8602
gfz 189| 0 1 0 -148 -16 9 -.35 23 19 | 205317 -2690 4960 8667
grg 131| -3 -3 -13 -38 34 149 .04 49 49 | --- --- --- ---
iac n/a| -4 -1 -11 -1 -28 -52 .09 61 61 | 383529 -2050 4970 8866
mcc n/a| -1 3 14 23 53 858 -.57 201 201 | --- --- --- ---
Table 2.1632.1 GPS week: 1632 Day: 1 MJD: 55669
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 151| 4 1 21 -37 -12 370 -.23 87 61 | 0 827 2668 2802
cod 243| 0 -1 1 52 8 -31 -.23 26 30 | --- --- --- ---
esx 138| 1 0 2 26 18 10 .35 24 22 | -19504 2644 4625 8976
gfz 189| -1 -1 -1 -59 -4 5 -.09 23 18 | 156562 3996 4634 8893
grg 131| 2 -3 -21 20 138 0 -.06 56 53 | --- --- --- ---
iac n/a| -4 0 -8 -41 -21 -319 .07 64 64 | 336717 -281 4659 8872
mcc n/a| 3 -11 40 182 -50 871 .06 182 182 | --- --- --- ---
Table 2.1632.2 GPS week: 1632 Day: 2 MJD: 55670
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 151| 5 11 16 -134 29 245 -.25 110 57 | 0 420 2173 2300
cod 243| 0 0 1 10 -4 -47 -.16 22 23 | --- --- --- ---
esx 138| 0 -2 2 50 19 -52 .37 18 16 | 16506 4377 4487 7852
gfz 189| -1 1 -4 -10 -20 -16 -.24 22 26 | 185885 1239 4469 7995
grg 131| -2 -2 -29 38 -46 78 .41 52 46 | --- --- --- ---
iac n/a| -1 3 -21 -3 -94 189 .03 69 69 | 366005 -638 4481 8318
mcc n/a| -3 -20 52 120 107 960 .23 164 164 | --- --- --- ---
Table 2.1632.3 GPS week: 1632 Day: 3 MJD: 55671
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 151| 6 7 -6 -78 174 340 -.42 63 57 | 0 -239 2989 3297
cod 243| 0 -2 5 40 -56 -7 -.26 22 23 | --- --- --- ---
esx 138| 0 0 -2 8 61 5 .38 17 16 | 11724 -2944 4395 8232
gfz 189| 1 -2 4 -55 -50 -19 -.13 19 18 | 186726 -1732 4411 8371
grg 131| -4 -4 -25 77 8 -3 .15 55 48 | --- --- --- ---
iac n/a| -1 1 -19 19 -29 -65 -.04 59 59 | 361846 -1042 4387 8522
mcc n/a| -10 -3 56 13 62 815 -.47 150 150 | --- --- --- ---
Table 2.1632.4 GPS week: 1632 Day: 4 MJD: 55672
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 151| -4 4 23 -74 -29 189 -.22 51 44 | 0 686 2969 3178
cod 243| 0 -2 2 76 -11 -28 -.21 22 23 | --- --- --- ---
esx 138| 0 2 0 3 8 -36 .47 20 18 | 24245 -5210 5436 8924
gfz 189| 0 0 0 -56 -7 9 -.23 24 22 | 204570 -5098 5426 8765
grg 131| -2 -7 -16 0 -72 -15 .13 55 55 | --- --- --- ---
iac n/a| -4 -1 -14 -57 -29 12 .14 45 45 | 373975 -1349 5423 9114
mcc n/a| 12 0 47 77 -18 266 .14 103 103 | --- --- --- ---
Table 2.1632.5 GPS week: 1632 Day: 5 MJD: 55673
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 151| 0 2 10 -103 59 134 -.26 52 48 | 0 1325 3308 3773
cod 243| -2 3 -6 26 19 -92 -.17 25 25 | --- --- --- ---
esx 138| 0 1 1 37 45 13 .39 21 18 | -26092 -881 4770 8421
gfz 189| 3 -3 2 -8 -40 -2 -.21 22 20 | 155978 -2634 4728 8474
grg 131| 2 -2 -5 26 -20 42 .06 53 46 | --- --- --- ---
iac n/a| 0 -4 -4 -14 -73 26 .03 36 36 | 324353 310 4753 9022
mcc n/a| 0 1 28 64 147 341 .13 115 115 | --- --- --- ---
Table 2.1632.6 GPS week: 1632 Day: 6 MJD: 55674
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 151| 4 4 16 -202 74 104 -.46 68 62 | 0 688 2491 2655
cod 243| -3 0 -1 -35 -30 -53 -.23 27 27 | --- --- --- ---
esx 138| 0 0 3 29 67 -64 .33 16 14 | -9419 2667 4529 7545
gfz 189| 0 2 -6 -12 -85 -66 -.20 23 18 | 175463 2918 4516 7750
grg 131| -2 1 0 -9 -99 139 -.05 52 51 | --- --- --- ---
iac n/a| 0 0 -7 -41 -70 290 -.09 40 40 | 343159 377 4518 8086
mcc n/a| 5 11 15 -47 86 858 .02 149 149 | --- --- --- ---
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 3.1632.0 GPS week: 1632 Day: 0 MJD: 55668
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1429 71 18 15 17 58 72 --- 15 | 51 37 40 44 45 69 --- 37
R02 | 1194 38 24 19 28 57 43 --- 13 | 44 45 36 28 37 31 --- 31
R03E | 3085 146 18 16 18 65 54 --- 13 | 72 28 42 48 53 45 --- 38
XR04 |15450 --- 308 --- --- --- 1176 --- 602 | --- 560 --- --- --- 403 --- 493
R05 | 1759 36 39 18 31 52 42 265 15 | 40 46 30 29 57 42 45 27
R06 | 3046 42 28 25 20 36 37 --- 13 | 62 45 25 24 39 30 --- 25
R07 | 1758 40 17 12 26 59 59 --- 12 | 70 42 34 42 50 61 --- 36
R08 | 941 83 21 19 50 52 50 105 19 | 54 37 37 42 35 53 38 34
R09E | 875 44 22 20 17 56 58 --- 13 | 69 21 26 28 32 33 --- 19
R10E | 1469 127 30 21 32 43 82 --- 20 | 84 39 41 25 44 38 --- 28
R11E | 2294 140 39 21 25 53 75 99 20 | 138 42 72 68 51 45 35 56
R12E | 747 81 16 12 19 37 44 --- 14 | 71 20 30 34 34 34 --- 24
R13E | 1037 43 19 17 19 56 66 --- 13 | 63 51 64 64 72 75 --- 57
R15E | 2451 71 21 11 17 45 46 149 13 | 88 31 30 26 58 31 35 28
R16E | 1159 34 19 18 18 39 64 --- 12 | 38 35 49 51 41 60 --- 42
R17 | 2359 88 31 20 21 51 88 --- 20 | 37 37 27 26 43 57 --- 21
R18 | 2585 53 22 22 13 45 82 279 16 | 75 58 50 45 26 57 76 47
R19 | 1298 53 18 28 18 36 68 --- 15 | 87 62 50 59 49 46 --- 54
R20 | 2940 62 30 16 15 41 54 --- 15 | 67 60 41 41 23 43 --- 43
R21 | 1098 38 19 13 25 43 53 --- 12 | 83 61 62 58 43 50 --- 58
R22 | 824 42 19 17 9 49 60 --- 12 | 65 67 59 63 37 67 --- 59
R23 | 661 58 24 14 16 55 62 226 14 | 73 46 45 51 38 59 29 45
R24 | 1479 62 31 22 24 43 39 --- 15 | 63 53 46 39 48 48 --- 41
------+----------------------------------------------+------------------------------------------
RMS | 1829 74 25 19 23 49 61 201 |T 67 66 42 42 43 64 43 58
WRMS | 1829 70 22 18 19 49 61 201 |NE 62 83 41 42 40 74 47 70
MEDI | 1469 53 22 18 19 49 59 149 |MD 67 45 41 42 43 48 35 38
Table 3.1632.1 GPS week: 1632 Day: 1 MJD: 55669
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1074 38 15 12 13 49 58 --- 11 | 54 29 46 41 37 57 --- 37
R02 | 765 61 17 14 20 38 36 --- 12 | 32 28 38 38 43 41 --- 31
R03E | 4644 42 14 13 32 60 61 --- 14 | 47 23 24 31 40 38 --- 21
XR04 |13149 --- 139 --- --- --- 535 --- 271 | --- 382 --- --- --- 504 --- 295
R05 | 1938 60 30 25 36 92 57 240 18 | 56 38 49 51 49 38 25 38
R06 | 2710 46 38 18 28 39 27 --- 15 | 45 33 33 33 39 30 --- 23
R07 | 1856 36 23 26 32 52 40 --- 14 | 50 29 26 22 38 46 --- 21
R08 | 1759 74 22 12 20 29 56 79 15 | 80 30 26 28 27 51 34 22
R09E | 848 155 12 12 17 45 61 --- 12 | 74 25 32 28 40 46 --- 26
R10E | 4530 63 14 13 18 41 55 --- 13 | 69 29 41 46 35 62 --- 38
R11E | 2738 208 32 34 32 53 78 111 22 | 200 40 68 63 53 50 22 49
R12E | 1094 70 20 23 26 52 60 --- 16 | 57 17 40 35 35 43 --- 24
R13E | 1520 132 17 19 19 48 85 --- 17 | 102 105 114 128 101 118 --- 110
R15E | 2074 96 18 13 16 34 52 128 16 | 76 29 24 25 38 28 19 21
R16E | 823 67 11 17 21 55 73 --- 15 | 78 30 36 36 52 41 --- 31
R17 | 2066 116 52 44 27 77 90 --- 28 | 71 31 56 52 44 55 --- 32
R18 | 3133 40 12 20 17 69 97 185 16 | 84 43 53 41 40 56 37 42
R19 | 947 81 8 21 13 51 73 --- 16 | 92 36 32 36 50 54 --- 36
R20 | 1809 83 31 27 19 53 43 --- 17 | 48 28 40 32 37 19 --- 27
R21 | 1213 41 46 42 22 64 52 --- 20 | 31 38 59 54 59 41 --- 35
R22 | 1334 29 13 24 15 58 63 --- 12 | 64 46 44 48 35 47 --- 44
R23 | 828 29 26 34 19 59 80 268 17 | 35 36 51 46 54 35 24 34
R24 | 655 85 43 29 30 64 66 --- 22 | 79 49 32 34 39 30 --- 24
------+----------------------------------------------+------------------------------------------
RMS | 2140 87 26 24 23 56 64 182 |T 69 51 43 43 44 66 26 46
WRMS | 2140 61 30 22 18 53 64 182 |NE 58 58 41 39 42 73 30 49
MEDI | 1759 63 20 20 20 52 61 128 |MD 64 31 40 36 40 46 24 32
Table 3.1632.2 GPS week: 1632 Day: 2 MJD: 55670
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 743 25 25 14 21 37 67 --- 13 | 60 38 43 45 36 55 --- 38
R02 | 969 44 13 10 16 33 39 --- 10 | 44 39 51 55 40 51 --- 45
R03E | 4508 46 14 17 27 43 59 --- 13 | 66 38 46 61 64 54 --- 46
XR04 |11496 --- 457 --- --- --- 2234 --- 1011 | --- 299 --- --- --- 9999 --- 274
R05 | 2813 53 32 18 19 65 65 196 15 | 47 47 31 39 52 40 29 31
R06 | 1520 50 26 17 38 48 67 --- 17 | 52 37 28 44 33 59 --- 31
R07 | 1033 37 23 8 28 56 41 --- 12 | 34 24 29 35 45 34 --- 21
R08 | 2146 33 20 15 18 30 54 40 11 | 45 34 24 22 37 42 31 22
R09E | 589 392 19 11 17 45 60 --- 12 | 229 22 29 41 20 33 --- 27
R10E | 5698 44 11 11 18 25 59 --- 11 | 53 29 25 32 34 67 --- 27
R11E | 1900 76 41 34 25 55 57 130 20 | 127 39 63 61 39 51 35 49
R12E | 857 173 15 14 20 64 70 --- 14 | 141 22 29 31 53 42 --- 22
R13E | 2341 78 17 14 33 90 55 --- 16 | 91 88 102 109 71 74 --- 93
R15E | 1144 53 29 15 23 39 69 157 15 | 46 18 47 54 55 32 19 34
R16E | 685 170 13 12 15 42 96 --- 16 | 121 36 42 41 51 61 --- 36
R17 | 1473 71 27 24 17 45 88 --- 18 | 84 26 44 30 54 81 --- 25
R18 | 2003 74 15 31 29 53 110 117 21 | 96 55 82 44 34 50 53 56
R19 | 692 72 15 21 16 56 77 --- 16 | 117 69 62 73 61 49 --- 67
R20 | 1673 53 24 10 21 57 75 --- 15 | 93 47 48 59 39 33 --- 48
R21 | 550 44 17 15 14 48 84 --- 14 | 40 50 61 53 34 38 --- 47
R22 | 858 59 21 16 19 48 66 --- 14 | 41 55 36 50 33 52 --- 41
R23 | 723 31 16 11 14 47 57 258 10 | 65 44 40 35 38 37 33 38
R24 | 811 42 30 24 21 71 62 --- 15 | 73 55 37 37 47 43 --- 38
------+----------------------------------------------+------------------------------------------
RMS | 2065 110 22 18 22 52 69 164 |T 80 52 45 47 44 49 33 50
WRMS | 2065 57 23 16 26 46 69 164 |NE 63 61 44 44 41 47 36 54
MEDI | 1144 53 20 15 19 48 66 130 |MD 65 39 42 44 39 49 31 38
Table 3.1632.3 GPS week: 1632 Day: 3 MJD: 55671
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1021 60 17 14 15 32 40 --- 11 | 88 25 31 26 28 57 --- 30
R02 | 951 52 28 12 13 32 49 --- 13 | 50 37 28 28 33 50 --- 26
R03E | 5126 95 21 19 24 42 39 --- 16 | 80 32 54 57 74 45 --- 42
XR04 |10570 --- 171 --- --- --- 623 --- 327 | --- 342 --- --- --- 837 --- 315
R05 | 2619 58 18 12 21 70 51 132 13 | 49 46 38 49 70 25 26 37
R06 | 826 52 21 24 18 64 80 --- 16 | 33 52 35 52 73 39 --- 38
R07 | 1798 36 18 24 20 113 35 --- 12 | 50 21 25 43 108 47 --- 24
R08 | 1209 42 30 18 31 51 43 53 14 | 48 36 22 32 45 38 63 20
R09E | 743 37 24 15 14 50 70 --- 13 | 137 45 31 32 51 49 --- 31
R10E | 3617 45 14 20 16 31 54 --- 12 | 49 38 41 41 46 41 --- 36
R11E | 1350 51 40 22 30 47 36 152 16 | 63 47 76 54 56 61 43 55
R12E | 1841 45 10 13 8 38 50 --- 10 | 67 26 33 25 41 41 --- 27
R13E | 1504 44 17 13 21 35 43 --- 11 | 115 113 124 116 121 137 --- 119
R15E | 1405 97 14 13 21 45 72 159 17 | 122 30 35 35 59 42 28 33
R16E | 1010 45 13 11 15 29 59 --- 11 | 69 23 30 28 34 31 --- 23
R17 | 1878 111 27 18 21 64 65 --- 19 | 70 38 59 43 54 97 --- 46
R18 | 1381 51 22 25 16 48 76 88 15 | 59 52 41 53 58 52 86 41
R19 | 1077 42 23 14 8 69 52 --- 11 | 64 54 49 49 41 44 --- 48
R20 | 1074 120 35 18 17 46 101 --- 23 | 119 62 45 42 50 78 --- 45
R21 | 833 49 16 18 16 42 81 --- 15 | 87 53 73 72 36 46 --- 62
R22 | 632 41 20 18 13 66 48 --- 11 | 78 64 47 50 44 59 --- 52
R23 | 1713 56 19 8 22 58 53 242 13 | 59 44 30 48 48 55 32 36
R24 | 1158 62 19 9 12 68 51 --- 12 | 64 60 51 57 42 36 --- 47
------+----------------------------------------------+------------------------------------------
RMS | 1879 63 22 17 19 55 59 150 |T 73 58 45 46 55 87 46 53
WRMS | 1879 57 23 16 18 48 59 150 |NE 65 65 41 46 52 104 51 57
MEDI | 1350 51 20 15 16 47 52 132 |MD 64 45 38 43 48 47 32 38
Table 3.1632.4 GPS week: 1632 Day: 4 MJD: 55672
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 2212 55 20 13 31 53 40 --- 14 | 46 28 36 40 36 43 --- 24
R02 | 1268 30 21 13 28 32 44 --- 12 | 52 32 30 20 35 37 --- 21
R03E | 6508 46 18 17 16 46 25 --- 11 | 36 26 39 45 52 52 --- 31
XR04 |12741 --- 66 --- --- --- 183 --- 110 | --- 290 --- --- --- 358 --- 228
R05 | 2405 43 37 22 28 36 31 75 15 | 35 46 23 31 46 40 25 27
R06 | 1308 34 24 18 17 45 41 --- 12 | 45 37 45 25 60 23 --- 31
R07 | 2752 26 21 14 24 83 41 --- 11 | 44 24 34 40 73 25 --- 27
R08 | 917 47 15 13 34 63 41 85 13 | 44 26 22 29 47 45 43 22
R09E | 561 63 17 11 17 47 42 --- 13 | 82 19 32 29 53 37 --- 21
R10E | 3548 51 21 16 23 65 50 --- 14 | 52 39 24 37 70 32 --- 25
R11E | 1691 40 30 28 28 50 46 92 16 | 42 48 65 72 40 55 63 53
R12E | 2351 42 18 19 19 41 22 --- 11 | 62 29 40 38 44 44 --- 31
R13E | 1470 41 17 12 24 55 37 --- 11 | 76 58 79 82 90 80 --- 71
R15E | 3971 47 30 17 21 51 31 94 13 | 46 39 36 31 46 40 51 30
R16E | 2605 50 22 19 22 31 51 --- 14 | 50 25 39 49 26 32 --- 32
R17 | 1809 62 19 22 21 60 53 --- 15 | 42 25 50 46 56 74 --- 37
R18 | 1347 23 29 36 20 40 63 89 17 | 39 43 28 41 47 61 96 27
R19 | 1441 41 21 18 14 42 47 --- 12 | 44 58 28 49 40 63 --- 41
R20 | 1906 59 24 29 26 79 65 --- 18 | 74 69 90 52 54 33 --- 61
R21 | 981 64 20 21 35 63 64 --- 18 | 117 62 83 77 48 36 --- 68
R22 | 825 55 14 14 12 69 45 --- 12 | 114 58 62 68 55 54 --- 63
R23 | 2781 103 19 26 27 47 40 161 20 | 112 43 31 44 48 40 72 35
R24 | 909 33 21 14 31 72 40 --- 13 | 47 43 24 23 52 46 --- 28
------+----------------------------------------------+------------------------------------------
RMS | 2447 51 22 20 24 55 45 103 |T 59 50 42 44 50 58 58 44
WRMS | 2447 44 23 18 22 55 45 103 |NE 61 58 41 41 49 65 59 49
MEDI | 1809 46 21 17 23 50 42 89 |MD 46 39 36 40 48 43 51 31
Table 3.1632.5 GPS week: 1632 Day: 5 MJD: 55673
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1940 51 24 17 28 36 31 --- 14 | 52 21 24 31 29 26 --- 21
R02 | 874 56 14 14 23 43 31 --- 12 | 47 31 33 34 46 38 --- 29
R03E | 6825 52 14 15 27 43 23 --- 12 | 61 22 31 40 47 32 --- 24
XR04 |12501 --- 113 --- --- --- 202 --- 152 | --- 290 --- --- --- 138 --- 245
R05 | 2437 68 38 20 21 33 43 52 17 | 43 32 31 30 27 27 16 20
R06 | 2659 36 35 12 22 55 33 --- 13 | 35 40 43 36 55 16 --- 33
R07 | 1334 31 18 14 13 66 26 --- 9 | 30 24 24 26 73 21 --- 19
R08 | 1271 43 30 19 18 38 38 76 14 | 37 26 28 29 26 31 36 23
R09E | 484 41 19 19 29 36 51 --- 15 | 65 23 44 50 28 22 --- 33
R10E | 1755 41 18 14 17 27 19 --- 10 | 60 44 43 40 43 33 --- 38
R11E | 683 50 50 36 26 75 37 88 19 | 49 35 87 66 61 46 38 56
R12E | 1796 57 12 16 11 72 32 --- 12 | 39 21 29 29 56 33 --- 22
R13E | 1582 77 20 22 19 42 37 --- 16 | 54 73 88 77 70 76 --- 73
R15E | 2043 88 28 20 39 48 53 116 21 | 102 39 61 73 63 30 26 50
R16E | 3004 61 23 28 31 83 28 --- 16 | 54 22 47 55 46 32 --- 31
R17 | 3079 41 23 13 17 35 34 --- 12 | 42 27 24 25 45 43 --- 21
R18 | 1441 28 10 19 14 24 42 164 11 | 36 35 57 47 40 40 61 42
R19 | 1387 36 16 23 21 45 38 --- 12 | 60 51 46 50 38 37 --- 44
R20 | 2462 21 34 45 22 35 66 --- 20 | 84 57 46 64 48 62 --- 52
R21 | 1739 38 31 12 17 99 33 --- 12 | 73 54 66 53 44 88 --- 62
R22 | 1029 56 24 17 13 63 21 --- 12 | 112 57 52 53 59 64 --- 59
R23 | 2104 61 21 17 10 42 30 152 13 | 88 29 52 58 68 48 39 48
R24 | 1421 53 13 15 15 48 18 --- 10 | 60 29 35 54 41 32 --- 36
------+----------------------------------------------+------------------------------------------
RMS | 2338 52 25 21 22 53 36 115 |T 58 47 45 46 47 44 36 47
WRMS | 2338 48 25 18 20 46 36 115 |NE 57 53 40 42 45 47 38 50
MEDI | 1755 50 23 17 19 43 33 88 |MD 54 32 43 47 46 33 36 36
Table 3.1632.6 GPS week: 1632 Day: 6 MJD: 55674
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx gfz grg iac mcc IGL | bkg cod esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 674 51 11 15 24 60 35 --- 11 | 41 39 33 46 41 42 --- 34
R02 | 782 55 23 15 35 57 28 --- 13 | 46 36 33 35 40 36 --- 30
R03E | 5688 45 20 10 21 32 46 --- 12 | 39 23 34 33 24 30 --- 26
XR04 |14727 --- 49 --- --- --- 176 --- 113 | --- 522 --- --- --- 128 --- 508
R05 | 1249 49 36 8 32 38 37 67 14 | 63 49 28 41 40 31 25 29
R06 | 1633 42 31 17 22 31 34 --- 13 | 52 42 41 35 42 27 --- 34
R07 | 1851 49 26 15 22 48 30 --- 12 | 29 24 31 40 40 32 --- 27
R08 | 1806 50 24 10 19 35 39 63 12 | 58 27 25 29 33 31 39 23
R09E | 1917 74 28 19 20 56 29 --- 14 | 83 28 44 42 40 23 --- 32
R10E | 2193 75 26 10 22 44 20 --- 13 | 68 61 59 51 53 54 --- 53
R11E | 917 43 40 24 31 45 32 97 16 | 69 30 67 67 49 41 33 49
R12E | 3108 57 21 11 22 --- 36 --- 12 | 47 26 42 39 --- 33 --- 32
R13E | 1120 91 19 14 12 38 33 --- 14 | 54 43 51 51 47 56 --- 46
R15E | 2543 76 27 23 18 35 26 152 14 | 107 46 44 34 39 37 30 39
R16E | 3306 61 27 14 35 32 35 --- 14 | 63 27 39 29 47 36 --- 27
R17 | 5376 73 30 11 10 59 21 --- 12 | 103 29 61 53 41 58 --- 51
R18 | 1003 65 39 23 15 32 38 268 16 | 65 54 29 33 40 50 99 31
R19 | 1120 55 25 12 13 67 42 --- 12 | 74 57 41 44 35 35 --- 44
R20 | 2529 110 43 19 35 56 90 --- 25 | 77 55 55 47 59 46 --- 49
R21 | 1628 46 26 13 11 69 57 --- 13 | 103 74 70 64 69 64 --- 69
R22 | 1074 139 19 25 19 114 38 --- 14 | 140 80 86 72 32 68 --- 78
R23 | 1310 36 14 9 20 40 41 147 10 | 77 48 46 44 41 83 54 50
R24 | 1803 60 21 10 16 29 38 --- 12 | 92 51 50 51 50 73 --- 52
------+----------------------------------------------+------------------------------------------
RMS | 2415 68 27 16 23 52 40 149 |T 70 63 45 44 42 48 46 61
WRMS | 2415 62 27 14 18 51 40 149 |NE 72 79 44 45 43 53 54 73
MEDI | 1803 55 26 14 20 44 36 97 |MD 65 43 42 42 41 41 33 39
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