[IGSREPORT-19681] Wk 1630 IGLOS Final Orbits
Jim Ray
igs.acc at noaa.gov
Thu Apr 21 11:33:10 PDT 2011
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1630 (Apr 03, 2011 - Apr 09, 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 2.1630.
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:
igl1630[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1630 in the SP3 format.
igl16307.sum Combination Report for GPS Week 1630.
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) the absolute antenna
model was introduced (IGSMAIL #5438). The antenna phase center offsets and
phase center variations are given in the file:
ftp://igscb.jpl.nasa.gov/pub/station/general/igs05.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 | 386.2 ns
1 | 394.8 ns
2 | 393.4 ns
3 | 356.0 ns
4 | 366.6 ns
5 | 381.2 ns
6 | 368.0 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 | GFZ | R21
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 1.1630, 1a.1630).
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 2.1630.0-6)
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 3.1630.0-6).
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 1630 summary. (Apr 03, 2011 - Apr 09, 2011)
Table 1.1630.a GPS week : 1630 MJD: 55654.0-55660.0
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| 1 2 4 -53 -10 -31 -.22 48 43 | 0 1105 3333 3678
| 3 4 3 40 46 39 .10 | 0 522
cod 243| 0 0 12 92 -40 -16 -.12 26 26 | --- --- --- ---
| 1 1 2 22 42 35 .05 | --- ---
esx 142| -2 0 2 -43 -40 -30 .44 21 20 | 17186 549 5238 9019
| 1 1 2 27 52 13 .04 | 16561 2751
gfz 193| 0 0 4 -33 39 19 -.16 25 23 | 216115 -823 5239 8968
| 1 1 2 49 95 40 .08 | 16958 2622
grg 133| -2 -5 11 -283 -361 85 .03 58 57 | --- --- --- ---
| 5 5 2 536 594 86 .13 | --- ---
iac n/a| 2 0 -36 7 83 94 -.21 38 38 | -19481 -1350 147364 292371
| 2 0 3 28 18 70 .09 | 669898 1335
mcc n/a| -5 -3 58 1 63 486 -.16 187 187 | --- --- --- ---
| 2 5 7 87 94 170 .37 | --- ---
Table 1.1630.b GPS week : 1630 MJD: 55654.0-55660.0
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 | 13 10 10 10 12 9 11 |
R02 | 11 10 11 15 12 11 11 |
R03 | 14 14 14 18 17 11 16 |
R04 | --- --- --- --- --- 0 0 |
R05 | 11 13 15 13 15 12 19 |
R06 | 16 12 12 14 9 10 12 |
R07 | 17 11 11 13 12 11 13 |
R08 | 9 13 14 9 13 11 10 |
R09 | 15 12 12 14 16 14 15 |
R10 | 20 13 14 16 16 16 17 |
R11 | 21 24 18 23 23 28 20 |
R12 | 12 10 15 16 13 13 15 |
R13 | 15 16 16 17 19 15 15 |
R15 | 18 14 14 15 14 14 12 |
R16 | 13 13 16 15 16 15 16 |
R17 | 19 13 22 21 18 23 21 |
R18 | 19 11 11 10 14 16 15 |
R19 | 14 12 13 13 9 20 12 |
R20 | 19 20 21 22 19 15 23 |
R21 | 76 26 31 18 11 10 13 |
R22 | 17 15 14 24 14 13 13 |
R23 | 10 12 13 12 16 11 12 |
R24 | 10 13 13 11 10 14 15 |
Table 1.1630.c GPS week : 1630 MJD: 55654.0-55660.0
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 1630 0 | -61 -59 418 1521 383 -15140 85.0 3080 3080 | 386246 0
brd 1630 1 | -44 56 384 -1240 -575 -14680 87.6 3110 3110 | 394785 0
brd 1630 2 | 8 8 341 -1766 504 -8591 88.9 2628 2628 | 393412 0
brd 1630 3 | -104 18 316 -1018 446 -7852 86.5 2424 2424 | 355988 0
brd 1630 4 | -25 61 280 -2009 -487 -11680 85.4 2067 2067 | 366550 0
brd 1630 5 | 75 -9 281 -956 -1554 -17390 88.2 2027 2027 | 381176 0
brd 1630 6 | -35 -86 401 -126 -1308 -14740 89.4 1947 1947 | 367976 0
-------------+------------------------------------------------------------+----------------
brd 1630 mean| -26 -1 346 -799 -370 -12867 87.3 2469 2469 | 378019 0
brd 1630 sdev| 56 55 56 1190 850 3588 1.7 490 490 | 14795 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 2.1630.0 GPS week: 1630 Day: 0 MJD: 55654
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| 7 0 3 -66 -24 -71 -.28 51 49 | 0 910 2631 2853
cod 243| 1 0 15 88 -11 -30 -.02 25 24 | --- --- --- ---
esx 142| -3 0 0 -73 3 -20 .43 24 22 | 28160 -3517 5822 8297
gfz 193| 1 -2 5 8 -59 -2 -.08 24 20 | 229909 -3413 5807 8193
grg 133| -6 -5 12 40 102 72 -.02 43 42 | --- --- --- ---
iac n/a| -1 0 -42 41 93 113 -.08 39 39 | 388021 -3196 5818 8759
mcc n/a| -6 -9 60 32 -1 575 -.54 189 189 | --- --- --- ---
Table 2.1630.1 GPS week: 1630 Day: 1 MJD: 55655
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 0 0 -48 -56 -42 -.25 41 35 | 0 272 3685 4208
cod 243| -2 2 14 112 43 12 -.12 27 29 | --- --- --- ---
esx 142| -1 0 5 -26 54 -38 .42 17 17 | 36634 3882 5646 8900
gfz 193| 3 -1 3 -50 -129 -10 -.20 24 27 | 234489 3265 5638 9058
grg 133| 0 0 8 97 66 123 -.02 46 46 | --- --- --- ---
iac n/a| 0 0 -35 -1 85 65 -.20 34 34 | -999999 974 5583 999999
mcc n/a| -6 -8 58 -19 142 448 -.59 249 249 | --- --- --- ---
Table 2.1630.2 GPS week: 1630 Day: 2 MJD: 55656
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 -1 2 -89 13 28 -.30 44 38 | 0 740 3400 3785
cod 243| 0 -1 10 104 -66 -7 -.10 26 29 | --- --- --- ---
esx 142| -4 2 3 -38 -76 -42 .44 20 19 | 30840 -852 5069 8143
gfz 193| 0 0 2 -55 105 -1 -.10 24 25 | 234412 -3528 5073 8353
grg 133| 2 -1 13 87 111 16 .01 49 46 | --- --- --- ---
iac n/a| 4 0 -35 23 105 123 -.24 38 38 | -999999 -474 999999 999999
mcc n/a| 1 4 58 -44 -52 399 -.28 128 128 | --- --- --- ---
Table 2.1630.3 GPS week: 1630 Day: 3 MJD: 55657
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 -3 6 -76 24 19 -.32 58 50 | 0 1174 3354 3800
cod 243| 1 0 12 86 -65 -73 -.08 26 23 | --- --- --- ---
esx 142| -4 0 0 -70 -94 -31 .45 25 23 | -7214 -1455 4456 10351
gfz 193| -1 2 5 -14 126 45 -.13 25 20 | 195329 -3020 4457 9613
grg 133| 6 -3 14 28 -125 16 .14 54 54 | --- --- --- ---
iac n/a| 4 -1 -33 37 53 99 -.13 39 39 | 356894 -2386 4472 9706
mcc n/a| -4 2 71 121 35 246 -.12 145 145 | --- --- --- ---
Table 2.1630.4 GPS week: 1630 Day: 4 MJD: 55658
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 7 -83 0 -42 -.19 40 34 | 0 1559 3625 3944
cod 243| 0 0 8 46 -68 -14 -.13 24 24 | --- --- --- ---
esx 142| -1 -1 1 -51 -60 -25 .52 25 25 | 1369 3245 5951 10584
gfz 193| 0 -3 8 41 59 -27 -.12 25 20 | 202241 1291 5975 10819
grg 133| -7 -2 8 -194 -398 -14 -.11 56 53 | --- --- --- ---
iac n/a| 3 0 -37 -29 79 198 -.27 38 38 | 366457 -1368 5973 10861
mcc n/a| -5 -2 48 94 127 361 -.09 170 170 | --- --- --- ---
Table 2.1630.5 GPS week: 1630 Day: 5 MJD: 55659
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| 3 6 10 29 51 -61 -.15 49 42 | 0 1844 3060 3325
cod 243| 1 1 14 112 -66 37 -.17 28 27 | --- --- --- ---
esx 142| 0 -1 2 -52 -69 -48 .39 19 18 | 22593 -49 5211 8975
gfz 193| 0 0 0 -57 83 56 -.16 25 21 | 215744 266 5207 9185
grg 133| -2 -8 12 -756 -809 204 -.04 66 68 | --- --- --- ---
iac n/a| 4 -2 -35 9 97 93 -.35 38 38 | 382351 -1495 5211 9535
mcc n/a| -5 -8 60 -37 202 649 .52 200 200 | --- --- --- ---
Table 2.1630.6 GPS week: 1630 Day: 6 MJD: 55660
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 9 4 -36 -79 -50 -.03 54 56 | 0 1242 3576 3831
cod 243| -1 0 9 94 -51 -38 -.17 28 29 | --- --- --- ---
esx 142| 0 -1 3 7 -43 -9 .43 18 18 | 7922 2590 4512 7885
gfz 193| 0 0 7 -108 89 80 -.33 27 25 | 200684 -625 4519 7557
grg 133| -7 -16 11 -1287 -1477 181 .26 94 91 | --- --- --- ---
iac n/a| 1 0 -30 -25 68 -34 -.22 38 38 | 369908 -1506 4495 7742
mcc n/a| -7 -1 52 -133 -11 727 -.01 226 226 | --- --- --- ---
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 3.1630.0 GPS week: 1630 Day: 0 MJD: 55654
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 | 3427 48 14 21 21 46 34 --- 12 | 53 41 62 62 32 35 --- 48
R02 | 1812 43 21 14 11 35 22 --- 10 | 50 45 46 41 29 45 --- 41
R03E | 2624 34 17 22 27 --- 45 --- 14 | 56 62 76 76 --- 55 --- 65
R05 | 1054 32 23 19 15 61 21 47 10 | 81 64 53 45 73 58 39 55
R06 | 1363 48 25 26 37 30 24 --- 15 | 59 47 33 51 29 41 --- 39
R07 | 1826 46 35 40 27 48 22 --- 17 | 77 60 45 45 57 44 --- 46
R08 | 2588 23 8 16 12 29 29 121 8 | 60 52 46 48 44 53 52 49
R09E | 2446 49 24 20 26 56 34 --- 14 | 49 21 40 38 38 31 --- 27
R10E | 1878 74 23 22 24 32 71 --- 20 | 43 22 27 25 32 28 --- 20
R11E | 1255 66 42 34 38 50 42 398 21 | 127 78 117 109 76 79 193 97
R12E | 1312 36 20 19 21 43 35 --- 12 | 36 27 42 43 53 38 --- 32
R13E | 732 40 20 20 29 32 46 --- 14 | 51 23 40 40 31 39 --- 28
R15E | 5709 65 25 22 23 29 55 152 17 | 36 17 33 37 31 24 40 20
R16E | 4836 39 25 18 19 38 37 --- 13 | 42 23 38 41 47 31 --- 29
R17 | 6102 66 29 36 24 54 47 --- 18 | 67 37 78 46 54 45 --- 46
R18 | 2485 55 33 26 31 49 59 65 19 | 64 43 43 33 45 26 49 31
R19 | 1470 43 22 22 18 35 40 --- 13 | 62 50 43 39 52 41 --- 40
R20 | 6473 71 40 30 20 43 35 --- 18 | 60 44 24 31 27 28 --- 24
XR21 |>>>>> 142 50 --- 514 --- 150 --- 76 | 232 152 --- 398 --- 47 --- 124
R22 | 534 77 29 25 20 62 23 --- 16 | 69 60 44 40 31 32 --- 40
R23 | 1915 28 15 19 17 37 24 105 9 | 52 47 41 34 38 35 27 36
R24 | 1864 31 21 15 18 28 22 --- 10 | 43 35 26 22 30 34 --- 25
------+----------------------------------------------+------------------------------------------
RMS | 3079 51 25 24 24 43 39 189 |T 66 47 47 61 42 40 66 43
WRMS | 3079 49 24 22 20 42 39 189 |NE 73 55 44 66 41 40 41 46
MEDI | 1878 46 23 22 21 38 35 105 |MD 56 44 43 41 38 38 40 39
Table 3.1630.1 GPS week: 1630 Day: 1 MJD: 55655
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 | 4827 27 22 9 24 38 24 --- 10 | 42 35 36 34 39 34 --- 30
R02 | 3142 26 16 16 17 30 27 --- 9 | 27 36 49 52 31 27 --- 38
R03E | 2060 36 29 16 23 --- 36 --- 13 | 60 49 50 54 --- 50 --- 45
R05 | 1372 34 33 20 21 51 24 44 13 | 67 51 59 59 50 46 27 53
R06 | 1009 40 27 12 13 56 24 --- 11 | 44 41 28 28 54 20 --- 25
R07 | 2082 31 29 16 16 41 22 --- 11 | 52 56 35 36 28 38 --- 39
R08 | 3472 45 15 22 19 37 33 65 13 | 56 42 31 39 59 49 47 36
R09E | 1909 30 20 14 26 37 30 --- 11 | 39 25 32 35 48 21 --- 23
R10E | 885 23 16 9 29 25 49 --- 13 | 41 29 25 36 31 34 --- 24
R11E | 1609 85 42 21 47 58 50 562 23 | 84 44 65 82 71 50 283 55
R12E | 1162 25 21 12 17 53 28 --- 10 | 50 35 37 40 33 36 --- 34
R13E | 755 56 19 24 20 68 45 --- 16 | 50 25 48 37 75 39 --- 29
R15E | 7464 42 23 15 27 36 36 159 13 | 52 23 24 31 35 26 50 19
R16E | 3971 37 21 16 24 39 35 --- 12 | 40 20 35 35 44 25 --- 25
R17 | 3289 28 15 9 30 59 48 --- 13 | 44 41 50 61 63 44 --- 45
R18 | 2400 24 33 13 22 59 17 102 11 | 49 36 36 40 33 22 38 28
R19 | 1406 21 32 20 16 35 23 --- 11 | 24 38 27 32 40 39 --- 27
R20 | 5567 90 29 26 21 56 34 --- 20 | 74 44 27 36 30 30 --- 33
XR21 | 2507 49 28 --- --- --- 35 --- 26 | 114 64 --- --- --- 34 --- 65
R22 | 670 20 49 22 16 53 32 --- 15 | 38 40 34 26 43 30 --- 21
R23 | 3197 29 23 23 22 23 28 121 12 | 34 37 30 47 42 36 72 30
R24 | 2392 35 14 12 30 36 35 --- 12 | 55 30 32 33 28 36 --- 29
------+----------------------------------------------+------------------------------------------
RMS | 3110 41 27 17 24 46 34 249 |T 51 38 37 41 43 34 86 34
WRMS | 3110 35 29 17 27 46 34 249 |NE 51 42 36 40 41 34 46 35
MEDI | 2082 31 23 16 22 39 32 102 |MD 49 37 35 36 40 34 47 30
Table 3.1630.2 GPS week: 1630 Day: 2 MJD: 55656
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 | 6061 37 15 7 17 45 25 --- 9 | 36 28 37 44 67 44 --- 32
R02 | 1784 17 27 26 12 43 17 --- 11 | 38 50 35 40 48 37 --- 35
R03E | 1856 41 17 16 18 --- 48 --- 13 | 95 83 91 91 --- 94 --- 87
R05 | 1102 29 32 31 18 46 30 119 14 | 29 42 25 42 46 46 48 25
R06 | 855 48 23 13 18 46 25 --- 12 | 105 49 59 61 60 45 --- 57
R07 | 2333 28 22 12 30 66 16 --- 11 | 48 49 43 21 38 39 --- 33
R08 | 3394 34 25 16 40 29 22 48 14 | 35 43 40 31 31 29 61 28
R09E | 1747 26 18 17 23 33 39 --- 12 | 39 19 40 37 37 36 --- 27
R10E | 2839 40 12 22 18 43 48 --- 13 | 46 20 34 26 45 37 --- 22
R11E | 2539 49 35 20 22 70 60 185 17 | 92 48 72 67 56 57 299 60
R12E | 1817 70 16 18 20 43 34 --- 15 | 97 39 37 42 34 32 --- 37
R13E | 1080 64 20 25 19 64 40 --- 16 | 89 28 39 44 57 49 --- 38
R15E | 3390 31 15 15 33 34 46 62 14 | 41 27 33 35 43 32 68 26
R16E | 1627 44 21 20 30 49 48 --- 15 | 47 27 47 42 33 34 --- 32
R17 | 2441 56 39 25 41 74 65 --- 21 | 43 22 37 49 47 58 --- 25
R18 | 1510 31 21 18 20 40 22 180 10 | 49 34 37 18 40 34 38 28
R19 | 1219 46 30 19 20 34 21 --- 13 | 59 50 30 25 38 30 --- 30
R20 | 4640 74 41 18 33 44 50 --- 20 | 81 36 43 58 42 28 --- 37
XR21 | 940 42 45 --- --- 358 44 --- 31 | 57 69 --- --- 109 30 --- 47
R22 | 1872 44 34 21 19 48 22 --- 14 | 50 49 35 35 44 44 --- 34
R23 | 3011 34 34 22 18 36 24 107 13 | 46 36 36 28 35 22 80 24
R24 | 1650 34 22 19 19 56 37 --- 12 | 31 42 38 32 65 35 --- 31
------+----------------------------------------------+------------------------------------------
RMS | 2627 44 26 20 24 49 38 128 |T 56 40 42 41 48 40 99 36
WRMS | 2627 38 29 19 25 46 38 128 |NE 50 42 38 37 50 37 56 33
MEDI | 1817 40 22 19 20 45 34 107 |MD 47 39 37 40 44 36 61 32
Table 3.1630.3 GPS week: 1630 Day: 3 MJD: 55657
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 | 4159 44 13 9 18 51 28 --- 10 | 64 36 54 47 47 48 --- 45
R02 | 1404 45 23 30 26 37 30 --- 14 | 77 45 41 71 40 32 --- 45
R03E | 2404 89 19 21 25 --- 47 --- 18 | 112 90 108 109 --- 89 --- 96
R05 | 1659 49 17 25 18 45 31 105 12 | 108 65 88 65 88 77 39 74
R06 | 779 52 23 19 21 50 34 --- 13 | 36 49 52 60 64 55 --- 46
R07 | 3880 45 15 24 22 60 31 --- 12 | 77 47 61 55 51 39 --- 50
R08 | 3236 29 18 13 18 51 20 100 9 | 48 54 45 34 52 38 50 40
R09E | 1333 49 14 25 23 45 43 --- 14 | 70 31 44 47 64 44 --- 37
R10E | 3873 69 13 20 25 38 50 --- 16 | 65 23 24 34 38 36 --- 18
R11E | 4698 68 54 23 28 68 62 109 22 | 80 35 70 69 66 70 86 54
R12E | 2147 72 17 23 26 44 36 --- 15 | 59 27 45 42 45 41 --- 29
R13E | 1062 54 25 20 34 53 49 --- 16 | 77 37 46 67 51 42 --- 43
R15E | 2751 40 20 23 30 46 43 80 14 | 54 27 32 32 45 36 37 25
R16E | 890 32 26 26 26 57 44 --- 15 | 39 20 52 41 58 44 --- 29
R17 | 2520 45 48 15 43 48 60 --- 21 | 57 55 64 73 69 70 --- 54
R18 | 1326 44 12 15 18 74 17 286 9 | 44 48 46 50 69 38 34 42
R19 | 549 63 15 18 18 41 24 --- 12 | 49 40 38 46 45 35 --- 36
R20 | 2594 106 42 18 32 37 38 --- 21 | 144 41 50 75 42 30 --- 50
R21 | 725 68 34 32 29 74 35 --- 18 | 82 63 44 105 64 52 --- 48
R22 | 1421 63 39 69 17 67 35 --- 23 | 88 68 90 73 46 48 --- 63
R23 | 1936 51 15 14 22 64 28 75 11 | 73 45 50 49 77 31 40 43
R24 | 926 35 19 18 18 50 28 --- 11 | 59 44 38 36 58 44 --- 38
------+----------------------------------------------+------------------------------------------
RMS | 2423 58 26 25 25 54 39 145 |T 71 45 53 58 56 47 47 45
WRMS | 2423 50 23 23 20 54 39 145 |NE 71 50 54 59 58 45 40 48
MEDI | 1659 49 19 20 23 50 35 100 |MD 65 44 46 50 52 42 39 43
Table 3.1630.4 GPS week: 1630 Day: 4 MJD: 55658
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 | 1778 29 20 25 20 75 26 --- 11 | 28 38 62 47 97 39 --- 40
R02 | 1185 28 24 25 19 37 29 --- 12 | 33 33 26 25 60 33 --- 20
R03E | 2168 45 22 23 31 --- 50 --- 16 | 73 65 67 85 --- 75 --- 67
R05 | 1755 31 36 18 19 41 40 42 14 | 60 48 55 50 82 42 21 44
R06 | 691 29 14 9 15 28 19 --- 8 | 56 47 43 39 56 50 --- 42
R07 | 2234 18 17 28 27 43 23 --- 11 | 31 32 30 46 55 34 --- 28
R08 | 1882 40 20 17 26 48 24 140 12 | 82 43 65 62 53 48 26 55
R09E | 1632 40 24 24 28 57 45 --- 15 | 45 22 40 34 55 40 --- 24
R10E | 1875 49 16 24 31 46 46 --- 16 | 44 21 34 37 44 34 --- 24
R11E | 5820 74 42 36 41 73 45 79 23 | 59 35 78 65 69 48 78 49
R12E | 2358 25 13 15 22 63 50 --- 12 | 33 26 34 36 54 42 --- 26
R13E | 2155 73 17 29 29 39 39 --- 18 | 71 24 38 32 45 32 --- 26
R15E | 1690 37 13 21 28 62 40 118 13 | 39 23 27 42 59 32 33 22
R16E | 1776 48 19 26 24 47 48 --- 16 | 65 24 32 33 44 49 --- 27
R17 | 1711 31 40 12 32 71 59 --- 18 | 47 35 39 60 62 53 --- 36
R18 | 1972 37 33 31 17 45 16 359 14 | 41 39 34 29 64 18 31 23
R19 | 621 28 12 16 18 38 18 --- 9 | 44 28 38 51 49 28 --- 34
R20 | 1562 63 29 31 15 93 54 --- 18 | 68 28 54 50 71 17 --- 37
R21 | 718 32 16 29 17 35 17 --- 11 | 61 49 30 58 55 35 --- 36
R22 | 1442 26 35 19 25 58 36 --- 14 | 38 61 57 30 52 35 --- 45
R23 | 1268 18 14 47 21 69 43 59 15 | 44 34 68 56 59 42 24 43
R24 | 1565 21 15 24 13 56 22 --- 9 | 42 42 45 33 63 44 --- 37
------+----------------------------------------------+------------------------------------------
RMS | 2066 40 24 25 25 56 38 170 |T 50 36 45 45 59 39 35 35
WRMS | 2066 34 24 25 20 53 38 170 |NE 48 39 46 45 62 37 25 37
MEDI | 1711 31 19 24 22 48 39 79 |MD 44 34 39 42 56 39 26 36
Table 3.1630.5 GPS week: 1630 Day: 5 MJD: 55659
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 | 1369 30 18 13 11 58 21 --- 8 | 49 29 47 35 85 33 --- 36
R02 | 1230 43 24 12 19 51 22 --- 11 | 31 37 38 25 96 30 --- 28
R03E | 3169 22 17 14 27 --- 33 --- 11 | 92 81 83 96 --- 69 --- 82
XR04 | 9832 --- 12 --- --- --- --- --- 0 | --- 346 --- --- --- --- --- 351
R05 | 850 20 33 15 14 43 34 64 12 | 36 35 34 37 85 23 15 28
R06 | 738 21 23 14 15 75 26 --- 9 | 30 42 38 41 111 27 --- 35
R07 | 1711 41 12 14 23 47 27 --- 11 | 42 30 35 44 105 40 --- 31
R08 | 1337 37 25 15 17 51 25 175 11 | 52 39 38 39 89 33 31 34
R09E | 1225 42 18 18 24 69 43 --- 13 | 41 22 41 47 85 41 --- 30
R10E | 1311 62 19 19 24 110 45 --- 15 | 59 19 35 23 91 35 --- 20
R11E | 3584 111 47 37 41 71 63 73 28 | 46 43 81 73 91 71 59 55
R12E | 2331 26 23 19 24 94 45 --- 13 | 32 21 43 34 86 34 --- 26
R13E | 1715 31 28 15 30 96 47 --- 14 | 42 25 58 60 93 40 --- 41
R15E | 2921 44 18 17 33 56 36 154 14 | 38 30 47 54 90 32 23 35
R16E | 2131 57 25 13 24 66 36 --- 14 | 85 20 53 41 82 37 --- 39
R17 | 2095 54 42 19 45 45 76 --- 22 | 59 31 36 55 83 46 --- 33
R18 | 3586 58 33 24 21 49 33 418 16 | 61 41 37 29 92 19 26 27
R19 | 1286 73 41 29 23 60 38 --- 19 | 72 30 35 23 103 24 --- 21
R20 | 1147 63 20 13 22 87 45 --- 15 | 57 37 51 54 97 35 --- 44
R21 | 923 32 17 11 22 47 18 --- 9 | 66 36 28 43 86 39 --- 35
R22 | 2127 36 34 14 30 42 23 --- 13 | 62 59 42 27 90 31 --- 40
R23 | 2325 34 24 19 18 51 19 49 11 | 36 44 40 21 98 32 18 30
R24 | 1563 30 35 24 18 58 29 --- 13 | 58 46 43 45 94 42 --- 40
------+----------------------------------------------+------------------------------------------
RMS | 2027 49 28 19 25 66 38 200 |T 52 49 44 43 92 36 28 49
WRMS | 2027 42 27 18 21 68 38 200 |NE 50 58 38 37 93 32 22 54
MEDI | 1711 37 24 15 23 58 33 73 |MD 49 36 40 41 91 34 23 35
Table 3.1630.6 GPS week: 1630 Day: 6 MJD: 55660
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 | 1799 37 11 12 13 60 43 --- 11 | 40 32 40 37 146 48 --- 35
R02 | 992 38 19 7 27 73 25 --- 10 | 54 43 32 30 149 44 --- 34
R03E | 2567 47 17 21 28 --- 55 --- 15 | 106 90 95 104 --- 89 --- 93
XR04 |10046 --- 9 --- --- --- --- --- 0 | --- 237 --- --- --- --- --- 239
R05 | 1176 40 44 33 45 83 12 109 18 | 55 50 46 53 119 41 29 39
R06 | 777 50 28 12 18 69 18 --- 11 | 42 48 28 42 137 42 --- 35
R07 | 1324 42 20 16 28 104 29 --- 12 | 53 41 39 47 142 35 --- 36
R08 | 1918 34 17 8 26 95 25 212 10 | 55 46 39 42 131 43 44 40
R09E | 957 61 28 19 23 99 36 --- 15 | 66 15 38 38 113 41 --- 29
R10E | 775 57 23 20 16 113 59 --- 16 | 34 19 27 16 108 41 --- 14
R11E | 1289 64 45 22 43 169 46 101 20 | 60 26 64 79 123 67 67 51
R12E | 1669 30 27 23 29 89 48 --- 15 | 29 21 38 37 109 42 --- 23
R13E | 899 30 21 20 29 98 51 --- 14 | 37 19 41 40 128 39 --- 28
R15E | 2455 45 16 11 24 80 36 178 12 | 50 43 33 32 133 30 31 30
R16E | 2528 56 25 14 33 88 49 --- 16 | 67 27 42 46 140 35 --- 32
R17 | 1696 58 44 23 34 52 62 --- 20 | 46 36 38 41 137 55 --- 31
R18 | 4378 70 30 15 20 80 32 448 15 | 66 53 31 51 164 27 32 35
R19 | 1197 37 28 17 21 100 30 --- 12 | 35 44 26 29 137 36 --- 26
R20 | 3384 117 38 26 28 98 38 --- 22 | 45 45 23 21 151 31 --- 21
R21 | 780 66 19 14 20 81 18 --- 12 | 59 57 24 73 158 37 --- 40
R22 | 2252 51 26 16 22 87 20 --- 12 | 63 71 41 39 146 39 --- 45
R23 | 1978 52 21 22 13 104 19 91 12 | 82 51 39 53 133 41 31 45
R24 | 1200 38 39 18 20 94 38 --- 14 | 53 50 31 30 128 28 --- 31
------+----------------------------------------------+------------------------------------------
RMS | 1947 54 28 18 27 94 38 226 |T 54 50 38 44 134 42 39 44
WRMS | 1947 56 29 18 25 91 38 226 |NE 53 60 34 42 141 39 34 48
MEDI | 1669 47 25 17 24 89 36 109 |MD 53 44 38 40 137 41 31 35
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