[IGSREPORT-28677] Wk 2208 IGLOS Final Orbits
acc
acc at igs.org
Mon May 23 10:34:49 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2208 (May 01, 2022 - May 07, 2022)
Contact: acc at igs.org
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 2.2208.
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:
igl2208[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2208 in the SP3 format.
igl22087.sum Combination Report for GPS Week 2208.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
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 until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
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:
https://files.igs.org/pub/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:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | -0.9 ns
1 | -0.0 ns
2 | -0.1 ns
3 | -0.1 ns
4 | -0.0 ns
5 | 0.4 ns
6 | 0.1 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
----+--------+---------------
2 | GRG | R13
3 | GRG | R13
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 1.2208, 1a.2208).
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 2.2208.0-6)
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 3.2208.0-6).
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 2208 summary. (May 01, 2022 - May 07, 2022)
Table 1.2208.a GPS week : 2208 MJD: 59700.0-59706.0
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -1 16 -23 21 .14 25 19 | 36531 -223 3304 8613
| 1 1 1 16 12 17 .03 | 1308 926
emx n/a| 0 1 7 19 -4 -45 .10 43 32 | -340 273 3254 8404
| 1 0 1 21 26 18 .08 | 11091 1011
esx n/a| 1 0 2 8 20 -36 -.09 36 22 | 466 -44 3251 11283
| 1 2 1 9 21 28 .08 | 12050 634
gfz n/a| 1 0 -1 -4 -6 0 -.07 36 19 | 0 -265 3286 8282
| 1 1 2 16 16 31 .10 | 0 813
grg n/a| 0 -1 -3 -41 33 52 .21 58 24 | -5 -379 3260 7968
| 1 0 5 19 21 53 .09 | 221 721
iac n/a| -1 0 -3 7 -26 -12 -.23 28 26 | 2309 -677 3263 9061
| 1 2 2 30 33 81 .09 | 484 882
Table 1.2208.b GPS week : 2208 MJD: 59700.0-59706.0
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 13 15 17 18 13 11 |
R02 | 12 9 9 8 6 8 15 |
R03 | 6 8 8 8 7 6 10 |
R04 | 10 9 8 10 9 8 9 |
R05 | 8 7 9 11 10 11 9 |
R07 | 8 9 10 10 9 7 6 |
R08 | 8 9 6 8 8 8 6 |
R09 | 9 7 8 8 8 8 8 |
R11 | 11 10 9 9 7 8 10 |
R12 | 12 10 15 19 10 8 9 |
R13 | 18 14 18 15 17 14 17 |
R14 | 11 9 8 9 9 10 8 |
R15 | 11 9 9 8 7 7 8 |
R17 | 9 11 9 7 8 9 8 |
R18 | 12 11 11 8 9 8 10 |
R19 | 20 27 27 31 26 21 26 |
R20 | 25 27 29 26 30 25 23 |
R21 | 11 10 9 12 9 10 8 |
R22 | 35 31 30 36 27 30 33 |
R24 | 10 12 14 11 12 9 10 |
Table 1.2208.c GPS week : 2208 MJD: 59700.0-59706.0
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 2208 0 | -70 91 221 309 -754 -3327 83.0 1825 1825 | -868 0
brd 2208 1 | 16 68 121 60 -548 -5557 83.4 1704 1704 | -7 0
brd 2208 2 | 42 35 75 -999 1589 -4911 83.2 1822 1822 | -107 0
brd 2208 3 | -5 -87 174 34 284 -10650 83.0 1527 1527 | -80 0
brd 2208 4 | 66 -4 92 -668 -387 1292 83.1 1460 1460 | -5 0
brd 2208 5 | 9 -84 233 -103 -1087 5024 83.7 1687 1687 | 439 0
brd 2208 6 | -8 20 81 -384 755 9161 82.2 1606 1606 | 94 0
-------------+------------------------------------------------------------+----------------
brd 2208 mean| 7 5 142 -250 -21 -1281 83.1 1661 1661 | -76 0
brd 2208 sdev| 43 69 66 459 946 6817 .5 139 139 | 394 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 2.2208.0 GPS week: 2208 Day: 0 MJD: 59700
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 -1 30 -13 9 .17 25 17 | 36337 -1434 3668 8803
emx n/a| -1 2 5 17 -42 -37 .09 41 33 | -272 -901 3584 8437
esx n/a| 1 1 0 5 16 -10 -.03 33 24 | 8975 -936 3585 11785
gfz n/a| 2 2 -2 4 7 -15 -.21 32 17 | 0 -1992 3639 8303
grg n/a| 1 -1 -1 -57 47 48 .07 36 30 | -66 -1859 3594 8350
iac n/a| -2 -5 -2 18 -60 45 -.15 34 32 | 1817 -1648 3607 9211
Table 2.2208.1 GPS week: 2208 Day: 1 MJD: 59701
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 -1 2 -45 18 .12 29 21 | 36708 -934 3576 8999
emx n/a| 0 0 9 2 -4 -32 .10 40 32 | 8843 -1242 3509 8845
esx n/a| -1 -2 4 20 39 -40 -.05 29 23 | 15138 -20 3521 11960
gfz n/a| 0 0 1 14 -9 -12 -.14 39 24 | 0 268 3576 8624
grg n/a| 2 -1 -9 -40 62 105 .21 32 30 | -63 -336 3529 8485
iac n/a| 0 1 0 33 -39 -53 -.16 30 28 | 2334 113 3540 9519
Table 2.2208.2 GPS week: 2208 Day: 2 MJD: 59702
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 18 -25 13 .17 27 20 | 35155 698 3446 8694
emx n/a| 2 0 9 25 -20 -39 .19 45 34 | 8513 885 3395 8508
esx n/a| 2 0 2 20 -10 -51 -.05 37 20 | 1176 -576 3373 10828
gfz n/a| 0 -1 -4 -15 -4 -36 -.15 35 23 | 0 -265 3386 8353
grg n/a| 0 -2 -4 -59 45 21 .22 93 23 | -6 -331 3376 8050
iac n/a| 0 0 -2 -38 8 48 -.30 28 28 | 2360 -310 3376 9213
Table 2.2208.3 GPS week: 2208 Day: 3 MJD: 59703
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 3 -1 10 -22 15 .12 27 22 | 34792 224 4047 8788
emx n/a| -2 1 8 -16 4 -36 .13 46 29 | -788 264 3948 8575
esx n/a| 2 -2 2 4 50 -60 -.24 35 22 | 1826 308 3935 11566
gfz n/a| 0 0 1 -8 18 17 -.02 38 17 | 0 14 3975 8521
grg n/a| 0 -1 -11 -65 9 -47 .31 153 25 | -357 291 3958 8109
iac n/a| -3 0 -1 52 -61 90 -.24 27 25 | 2050 -1209 3946 9151
Table 2.2208.4 GPS week: 2208 Day: 4 MJD: 59704
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]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 46 -5 60 .16 26 20 | 38105 -988 2809 8523
emx n/a| -3 1 8 34 40 -39 -.08 46 31 | -19423 375 2823 8375
esx n/a| 3 1 1 -4 30 15 -.10 36 20 | -5182 -313 2836 11212
gfz n/a| 2 0 -3 -29 -4 35 .01 36 15 | 0 -438 2863 8370
grg n/a| 0 -1 0 -23 8 104 .23 31 22 | 125 -571 2828 7609
iac n/a| 0 0 -6 -16 -46 -151 -.19 24 22 | 3057 -1768 2836 8962
Table 2.2208.5 GPS week: 2208 Day: 5 MJD: 59705
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 -3 7 -28 20 .18 21 18 | 38202 1020 2947 7965
emx n/a| 0 1 6 49 -18 -87 .15 40 30 | -9874 1494 2924 7736
esx n/a| 2 0 1 8 5 -61 -.00 38 22 | -22699 986 2923 10761
gfz n/a| 0 -1 0 -13 -25 -31 -.05 35 18 | 0 333 2944 7746
grg n/a| -1 -2 0 -20 15 78 .29 26 18 | 374 -53 2943 7392
iac n/a| 0 0 -3 2 -1 -48 -.39 23 21 | 2791 -442 2951 8439
Table 2.2208.6 GPS week: 2208 Day: 6 MJD: 59706
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]
--------+----------------------------------------------------+------------------------------
cod n/a| -3 0 -3 1 -25 11 .09 19 17 | 36424 -149 2641 8524
emx n/a| 1 0 8 21 9 -43 .10 45 31 | 10619 1038 2599 8354
esx n/a| 0 3 2 3 11 -48 -.13 40 21 | 4028 242 2586 10875
gfz n/a| 3 -2 -1 15 -26 39 .07 35 17 | 0 224 2622 8061
grg n/a| 0 0 1 -21 46 57 .13 32 22 | -44 205 2593 7785
iac n/a| 0 0 -7 3 18 -21 -.20 28 26 | 1755 525 2590 8936
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 3.2208.0 GPS week: 2208 Day: 0 MJD: 59700
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 918 31 30 23 18 36 36 13 | 55 49 53 58 41 52 48
R02M | 3894 8 15 18 14 56 25 11 | 47 46 46 52 47 44 43
R03 | 708 6 14 10 14 23 14 6 | 27 27 26 32 37 32 28
XR04 | 767 7 11 22 --- 25 30 10 | 30 28 32 --- 45 21 26
R05 | 842 14 19 17 22 19 21 8 | 27 32 27 29 31 36 24
R07 | 900 10 15 16 20 11 32 8 | 43 43 43 53 39 58 43
R08 | 681 12 19 20 15 16 25 8 | 40 42 51 50 41 46 42
R09E | 3515 17 26 15 17 18 24 8 | 44 37 47 50 34 49 42
XR11E | 2369 --- 24 11 13 25 33 11 | --- 31 28 22 29 34 22
R12E | 1226 14 28 21 20 13 49 11 | 135 141 136 143 137 154 138
R13E | 928 37 48 39 43 37 26 17 | 80 80 88 91 123 88 81
R14E | 1154 12 27 20 24 25 34 10 | 57 57 58 57 61 55 54
R15E | 1326 10 35 18 14 36 26 10 | 105 109 111 116 119 112 110
R17 | 727 17 25 10 14 20 32 9 | 50 20 34 48 48 40 39
R18 | 2282 14 30 22 27 34 41 12 | 42 23 53 43 52 47 42
R19 | 1245 22 76 24 55 57 32 20 | 60 51 39 97 68 51 51
R20 | 2222 53 82 66 35 40 46 24 | 95 26 44 83 82 54 55
R21 | 1722 12 37 23 10 12 40 10 | 72 46 55 68 69 84 64
R22 | 1283 62 74 96 89 81 57 34 | 36 54 108 49 49 69 41
R24 | 2600 15 33 14 25 21 31 10 | 61 38 52 60 57 46 50
------+-----------------------------------------+-------------------------------------
RMS | 1824 25 41 33 32 36 34 |T 58 49 56 63 60 58 52
WRMS | 1824 17 33 24 17 30 32 |NE 48 35 47 55 51 48 42
MEDI | 1226 14 27 20 20 25 32 |MD 50 42 47 53 48 49 43
Table 3.2208.1 GPS week: 2208 Day: 1 MJD: 59701
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 1007 32 26 31 20 27 33 13 | 26 28 43 40 20 36 26
R02M | 4357 12 5 19 16 31 27 9 | 26 24 30 35 34 30 25
R03 | 867 15 17 13 18 17 26 8 | 17 17 32 32 33 34 21
XR04 | 760 9 13 18 --- 22 24 9 | 16 16 23 --- 27 16 15
R05 | 771 18 8 13 16 13 20 7 | 19 20 21 23 26 28 16
R07 | 1163 13 11 11 22 26 30 9 | 20 22 27 32 27 29 21
R08 | 768 12 13 16 18 17 32 8 | 21 20 28 28 21 29 19
R09E | 3131 14 22 12 13 16 20 7 | 26 30 33 35 30 38 29
XR11E | 3111 --- 19 9 22 20 23 9 | --- 21 25 36 23 25 22
R12E | 1085 14 30 14 16 16 37 10 | 65 65 69 72 80 86 69
R13E | 779 19 43 31 34 26 37 14 | 58 61 62 66 133 62 56
R14E | 606 14 25 21 18 22 20 9 | 48 45 60 59 59 42 50
R15E | 1016 13 31 13 28 17 18 9 | 61 56 58 69 66 61 59
R17 | 811 19 26 14 32 21 33 11 | 31 20 22 40 32 31 21
R18 | 1780 14 38 19 19 36 17 11 | 33 25 30 31 35 30 25
R19 | 1931 24 86 34 107 61 30 27 | 23 58 40 83 40 27 29
R20 | 942 73 76 63 49 39 36 26 | 57 32 39 48 41 40 29
R21 | 924 20 36 16 12 20 31 10 | 47 35 38 42 54 47 41
R22 | 1089 69 63 73 81 78 44 31 | 39 43 48 36 36 57 31
R24 | 2342 20 47 17 29 21 25 12 | 36 24 38 40 39 35 31
------+-----------------------------------------+-------------------------------------
RMS | 1704 29 40 29 39 32 30 |T 35 33 38 44 42 39 31
WRMS | 1704 21 32 23 24 30 28 |NE 29 27 32 39 34 33 24
MEDI | 1007 15 26 16 20 21 27 |MD 31 25 33 40 34 34 26
Table 3.2208.2 GPS week: 2208 Day: 2 MJD: 59702
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 1491 41 25 42 23 28 32 15 | 50 46 56 43 41 46 42
R02M | 4639 13 17 18 20 21 31 9 | 38 43 41 43 50 38 37
R03 | 898 13 15 17 11 13 25 7 | 29 31 29 28 27 39 28
XR04 | 1054 15 12 8 --- 14 25 8 | 34 31 37 --- 27 33 29
R05 | 938 21 16 21 16 16 22 8 | 36 33 47 41 35 46 36
R07 | 672 17 13 13 13 14 44 10 | 41 44 39 42 36 64 43
R08 | 843 7 12 10 17 15 14 5 | 35 32 36 33 33 36 32
R09E | 2894 14 14 12 23 19 19 7 | 23 26 27 38 28 32 25
XR11E | 3829 --- 19 14 12 23 21 9 | --- 35 34 35 37 38 33
R12E | 1317 19 32 19 27 65 18 15 | 65 69 64 72 102 76 69
R13E | 1057 26 45 31 39 368 37 17 | 50 51 57 66 341 70 52
R14E | 608 8 22 21 19 21 17 8 | 49 39 53 57 54 53 48
R15E | 1727 10 28 12 26 19 17 8 | 58 52 60 63 63 63 58
R17 | 737 12 33 14 19 15 22 8 | 44 33 33 46 47 49 41
R18 | 1374 7 36 26 22 25 30 11 | 39 30 44 42 53 47 37
R19 | 2043 29 102 42 85 66 25 27 | 54 41 53 94 73 44 50
R20 | 2778 64 82 96 52 39 28 28 | 86 33 55 85 62 67 54
R21 | 1183 15 38 19 14 16 21 9 | 79 66 72 76 75 91 76
R22 | 1000 48 87 86 65 84 28 30 | 37 89 83 49 63 45 45
R24 | 1347 34 35 12 29 17 43 13 | 61 48 46 54 52 69 51
------+-----------------------------------------+-------------------------------------
RMS | 1821 27 45 37 35 93 28 |T 47 43 48 53 64 52 44
WRMS | 1821 20 34 20 23 23 28 |NE 47 42 47 53 48 52 43
MEDI | 1183 15 25 18 22 19 25 |MD 44 39 46 46 50 46 42
Table 3.2208.3 GPS week: 2208 Day: 3 MJD: 59703
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 960 43 21 43 34 39 27 16 | 53 48 58 54 47 40 45
R02M | 3186 13 11 19 16 32 14 8 | 29 26 38 38 38 33 29
R03 | 985 13 13 20 13 13 27 8 | 28 33 36 43 43 46 36
XR04 | 983 16 21 18 --- 23 22 10 | 28 33 26 --- 36 29 24
R05 | 976 26 22 18 15 29 27 10 | 34 30 46 43 32 51 34
R07 | 733 17 18 16 13 14 41 10 | 33 39 36 41 35 60 39
R08 | 741 15 15 11 19 20 19 7 | 42 43 43 51 41 55 45
R09E | 2731 13 22 12 20 18 17 7 | 20 29 27 37 22 23 21
XR11E | 3391 --- 25 16 13 16 15 8 | --- 24 29 31 24 27 24
R12E | 1650 27 36 16 15 103 22 19 | 47 42 44 49 117 42 45
R13E | 743 27 40 24 34 621 26 15 | 43 48 49 62 558 43 42
R14E | 976 14 23 15 17 21 29 9 | 65 65 67 67 71 51 62
R15E | 1644 13 27 12 23 18 16 8 | 36 39 37 49 48 47 40
R17 | 742 17 28 9 13 13 12 7 | 41 26 36 32 49 31 34
R18 | 917 10 29 22 10 21 16 8 | 31 32 47 32 44 39 35
R19 | 949 32 115 59 94 62 45 30 | 56 49 55 107 66 35 46
R20 | 1760 47 89 82 52 34 36 26 | 80 58 31 85 87 77 60
R21 | 1040 15 40 32 15 16 31 11 | 64 39 47 63 68 81 60
R22 | 2518 55 70 78 97 134 35 35 | 38 89 97 55 126 56 57
R24 | 829 27 46 11 14 12 23 10 | 47 41 34 35 41 31 33
------+-----------------------------------------+-------------------------------------
RMS | 1527 27 46 35 38 153 27 |T 42 41 44 51 79 44 40
WRMS | 1527 22 29 22 17 25 25 |NE 43 42 44 53 55 49 41
MEDI | 976 17 25 18 16 21 23 |MD 41 39 38 49 44 42 39
Table 3.2208.4 GPS week: 2208 Day: 4 MJD: 59704
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 1227 36 27 56 44 43 20 17 | 35 48 51 46 39 42 33
R02M | 1248 8 8 16 14 12 12 5 | 30 34 38 40 31 31 31
R03 | 1181 12 13 17 10 16 19 6 | 19 17 29 24 26 32 22
XR04 | 1594 19 20 22 --- 8 18 9 | 19 20 21 --- 16 13 12
R05 | 1323 17 17 19 23 24 25 9 | 18 20 26 22 30 27 17
R07 | 959 16 17 8 7 19 32 8 | 30 29 34 31 29 49 32
R08 | 1812 13 14 14 20 27 10 7 | 39 32 40 40 49 35 37
R09E | 2492 16 17 11 20 21 22 8 | 24 30 31 39 28 30 26
XR11E | 2293 --- 12 11 10 18 17 7 | --- 16 23 21 20 21 16
R12E | 1479 27 31 24 17 15 11 9 | 44 37 54 47 53 55 44
R13E | 773 32 57 36 53 27 25 17 | 42 57 59 79 73 46 44
R14E | 1208 13 25 15 15 21 24 8 | 37 38 42 42 52 44 39
R15E | 2402 8 26 13 19 13 11 6 | 36 31 38 43 43 37 37
R17 | 805 15 35 9 15 13 17 8 | 47 27 36 43 44 39 38
R18 | 812 13 23 22 10 21 28 9 | 31 27 41 36 32 51 31
R19 | 1774 48 116 43 54 41 37 25 | 59 52 41 62 36 52 35
R20 | 1387 52 98 94 71 55 36 30 | 89 74 53 96 88 58 64
R21 | 1323 13 37 19 13 17 19 9 | 71 50 55 67 72 72 64
R22 | 1255 42 38 71 89 75 31 27 | 37 52 72 41 47 62 43
R24 | 1418 13 55 17 12 30 23 11 | 63 38 51 59 72 76 59
------+-----------------------------------------+-------------------------------------
RMS | 1460 26 46 36 36 31 24 |T 40 36 41 46 44 43 36
WRMS | 1460 20 31 20 15 22 22 |NE 43 36 41 47 45 47 37
MEDI | 1323 16 25 17 17 21 20 |MD 37 32 40 42 39 42 35
Table 3.2208.5 GPS week: 2208 Day: 5 MJD: 59705
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 943 26 14 33 32 32 26 12 | 31 37 52 49 39 46 38
R02M | 1246 15 17 19 17 14 24 8 | 53 56 55 53 51 59 53
R03 | 876 15 10 8 10 10 18 6 | 12 14 18 16 18 19 13
XR04 | 1007 18 18 18 --- 11 15 8 | 16 15 16 --- 16 22 12
R05 | 856 21 20 29 32 13 29 11 | 16 13 34 37 18 26 11
R07 | 927 13 11 14 16 13 16 6 | 16 18 23 24 22 24 17
R08 | 2275 14 23 21 16 16 18 8 | 33 22 35 32 36 44 33
R09E | 2480 16 17 12 19 17 17 7 | 29 30 30 37 26 37 29
XR11E | 2326 --- 17 16 10 13 19 7 | --- 19 31 26 24 23 22
R12E | 2082 13 29 16 16 12 17 7 | 70 67 67 73 78 77 70
R13E | 1228 27 43 34 36 28 20 13 | 61 63 64 63 73 65 59
R14E | 1600 14 42 18 11 29 16 10 | 60 45 58 58 74 48 56
R15E | 3008 10 26 13 24 11 11 7 | 58 53 63 74 59 60 59
R17 | 1087 8 40 22 14 10 21 9 | 34 24 30 34 39 47 33
R18 | 1450 13 23 22 15 19 17 8 | 28 24 32 20 37 26 24
R19 | 1679 28 95 35 40 52 32 21 | 44 40 34 41 51 58 39
R20 | 1583 45 71 93 61 22 22 24 | 59 53 67 72 54 47 49
R21 | 1878 14 37 19 17 23 25 10 | 53 44 47 52 67 43 50
R22 | 1996 37 57 96 98 63 47 30 | 27 42 66 41 54 49 31
R24 | 1235 15 44 16 24 12 12 9 | 47 35 34 50 49 46 43
------+-----------------------------------------+-------------------------------------
RMS | 1687 21 40 38 35 26 23 |T 39 35 42 44 44 43 37
WRMS | 1687 18 30 22 18 18 21 |NE 32 28 36 38 38 37 29
MEDI | 1450 15 23 19 17 14 18 |MD 34 35 34 41 39 46 33
Table 3.2208.6 GPS week: 2208 Day: 6 MJD: 59706
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01M | 1063 22 9 27 35 23 21 10 | 62 60 62 67 59 68 61
R02M | 2147 18 27 34 24 38 51 14 | 134 134 120 144 100 147 128
R03 | 860 18 14 15 11 14 41 9 | 30 32 37 36 42 56 36
XR04 | 1095 18 15 13 --- 20 17 8 | 34 29 23 --- 28 21 25
R05 | 823 15 21 26 22 14 16 8 | 29 32 38 33 31 31 26
R07 | 1007 11 11 10 17 12 17 6 | 46 46 44 49 43 63 46
R08 | 2059 7 13 14 17 12 13 5 | 52 46 52 52 51 58 51
R09E | 1914 15 19 12 21 17 17 7 | 33 32 36 41 29 33 32
XR11E | 1879 --- 17 10 14 26 20 9 | --- 32 32 37 36 38 32
R12E | 1211 12 29 17 25 19 13 8 | 107 101 104 108 113 108 106
R13E | 960 18 43 48 55 25 43 17 | 92 96 100 121 100 105 96
R14E | 1469 11 24 20 17 17 19 7 | 64 64 78 73 70 71 68
R15E | 2453 10 30 13 13 21 24 8 | 89 75 89 96 97 98 90
R17 | 1110 9 36 15 14 13 18 8 | 59 33 44 58 57 56 52
R18 | 1378 15 42 12 16 21 20 9 | 52 31 54 48 60 50 48
R19 | 2075 20 117 53 56 63 48 26 | 68 43 45 101 74 82 62
R20 | 1786 39 85 80 46 31 26 23 | 101 31 48 104 91 81 73
R21 | 1309 19 33 11 10 13 20 8 | 88 63 73 80 87 81 79
R22 | 2551 39 53 114 89 88 40 32 | 31 71 129 40 67 63 50
R24 | 957 12 44 22 22 15 18 10 | 64 42 52 70 59 65 57
------+-----------------------------------------+-------------------------------------
RMS | 1606 19 45 40 35 32 28 |T 65 54 63 71 64 68 60
WRMS | 1606 17 31 21 17 22 26 |NE 54 41 53 61 57 58 50
MEDI | 1309 15 27 15 21 19 20 |MD 62 43 52 67 59 63 52
More information about the IGSREPORT
mailing list