[IGSREPORT-29487] Wk 2276 IGLOS Final Orbits
acc
acc at igs.org
Fri Sep 8 05:04:27 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2276 (Aug 20, 2023 - Aug 26, 2023)
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 2.2276.
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:
igl2276[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2276 in the SP3 format.
igl22767.sum Combination Report for GPS Week 2276.
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.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
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).
The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 | -13.9 ns
1 | -13.0 ns
2 | -11.3 ns
3 | -10.2 ns
4 | -12.3 ns
5 | -2.4 ns
6 | 0.4 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 1.2276, 1a.2276).
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 2.2276.0-6)
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 3.2276.0-6).
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 2276 summary. (Aug 20, 2023 - Aug 26, 2023)
Table 1.2276.a GPS week : 2276 MJD: 60176.0-60182.0
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| -1 0 1 -3 -15 17 .00 16 13 | 19211 -388 3268 9180
| 0 0 0 9 11 15 .03 | 5371 2246
esa n/a| -1 0 4 -9 13 3 -.22 31 23 | -10560 361 3270 7870
| 1 0 1 10 14 21 .04 | 9328 2393
gfz n/a| 0 0 -2 40 -2 5 -.16 24 15 | 0 -544 3283 8367
| 0 1 1 9 10 49 .03 | 0 2375
grg n/a| 2 0 -4 -25 11 -37 .35 22 18 | -8976 -358 3283 7889
| 1 1 1 17 15 33 .04 | 6209 2741
jgx n/a| 0 1 3 13 22 -76 -.30 27 26 | 20140 -390 3272 8448
| 1 1 1 21 16 47 .03 | 5293 2876
Table 1.2276.b GPS week : 2276 MJD: 60176.0-60182.0
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 | 25 23 23 25 25 25 24 |
R02 | 8 11 6 8 8 9 9 |
R03 | 8 9 8 6 7 9 9 |
R04 | 11 7 9 9 9 7 10 |
R05 | 13 9 7 7 6 8 7 |
R07 | 10 10 12 9 9 7 9 |
R08 | 8 8 10 17 10 8 10 |
R09 | 6 6 9 7 6 10 8 |
R11 | 9 8 8 7 9 6 6 |
R12 | 8 7 9 6 6 6 7 |
R13 | 18 16 15 17 17 13 20 |
R14 | 5 7 8 7 5 7 8 |
R15 | 9 8 7 11 8 10 8 |
R16 | 9 12 10 8 10 11 10 |
R17 | 9 11 9 8 9 11 10 |
R18 | 8 8 9 9 7 9 9 |
R19 | 22 21 21 31 14 21 24 |
R20 | 36 37 32 32 29 30 32 |
R21 | 13 9 9 9 11 8 10 |
R22 | 9 8 9 9 8 8 9 |
R24 | 10 9 9 9 13 14 12 |
R25 | 10 12 12 17 12 11 12 |
Table 1.2276.c GPS week : 2276 MJD: 60176.0-60182.0
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 2276 0 | -16 -1 149 740 -777 1052 81.1 1865 1865 | -13933 0
brd 2276 1 | -16 40 187 -428 -11 6854 79.4 1947 1947 | -12953 0
brd 2276 2 | -39 7 183 -680 99 2343 78.9 1535 1535 | -11315 0
brd 2276 3 | 8 -22 106 485 441 3556 79.5 1166 1166 | -10175 0
brd 2276 4 | 2 48 50 -917 -792 -1958 80.9 1241 1241 | -12298 0
brd 2276 5 | 63 -32 167 636 585 -1614 81.1 1147 1147 | -2399 0
brd 2276 6 | 46 70 82 -361 -722 3498 79.0 1333 1333 | 385 0
-------------+------------------------------------------------------------+----------------
brd 2276 mean| 6 15 132 -75 -168 1961 80.0 1462 1462 | -8955 0
brd 2276 sdev| 36 38 53 679 592 3108 1.0 330 330 | 5615 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 2.2276.0 GPS week: 2276 Day: 0 MJD: 60176
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| -2 0 0 -10 -34 -5 -.01 17 12 | 15219 -1183 3529 9675
esa n/a| -1 0 6 -9 15 32 -.19 34 29 | -17532 -17 3529 11390
gfz n/a| 0 1 -4 45 15 55 -.12 22 16 | 0 -1188 3492 9092
grg n/a| 1 -3 -2 -19 13 -90 .32 25 19 | -13656 -691 3506 8610
jgx n/a| 1 1 2 5 19 -18 -.25 28 28 | 15949 -506 3551 9220
Table 2.2276.1 GPS week: 2276 Day: 1 MJD: 60177
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 -4 -6 19 -.01 15 13 | 15357 -563 3223 9475
esa n/a| -1 0 6 -1 0 20 -.21 31 24 | -12548 624 3226 6929
gfz n/a| 0 1 -3 37 -12 48 -.15 25 14 | 0 -62 3251 8812
grg n/a| 5 -1 -3 -6 25 -66 .34 23 17 | -13226 -214 3275 8132
jgx n/a| 2 0 4 -11 33 -100 -.34 30 30 | 16438 -1100 3251 8770
Table 2.2276.2 GPS week: 2276 Day: 2 MJD: 60178
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 11 -15 8 .05 16 12 | 17771 100 2857 9597
esa n/a| -3 -1 5 -15 9 12 -.23 30 22 | -12964 1118 2856 6776
gfz n/a| -1 1 -5 46 0 50 -.22 24 15 | 0 -580 2889 8632
grg n/a| 4 -1 -5 -45 14 -45 .37 19 17 | -11211 -613 2891 8108
jgx n/a| -3 0 4 -13 -9 -125 -.30 24 24 | 18581 331 2916 9092
Table 2.2276.3 GPS week: 2276 Day: 3 MJD: 60179
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| -2 0 2 3 -24 14 .01 17 13 | 16445 -165 3041 7961
esa n/a| -1 0 3 10 36 -15 -.22 30 21 | -8007 492 3037 7273
gfz n/a| 0 0 -2 33 -17 8 -.15 27 11 | 0 -1078 3023 7460
grg n/a| 3 0 -5 -43 31 -14 .32 25 25 | -9915 -873 3003 7192
jgx n/a| 0 0 4 35 33 -137 -.35 21 21 | 18239 -753 2861 7900
Table 2.2276.4 GPS week: 2276 Day: 4 MJD: 60180
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 3 -9 -5 28 .03 15 12 | 15748 2231 2959 8831
esa n/a| 0 -1 3 -21 27 -14 -.25 30 21 | -24077 3807 2951 6733
gfz n/a| 0 0 -1 40 3 -28 -.18 17 12 | 0 3168 2883 8181
grg n/a| 1 0 -4 -31 -17 -3 .44 23 17 | -14490 3919 2938 7548
jgx n/a| -1 1 3 25 29 -68 -.30 26 26 | 16369 3338 2976 8298
Table 2.2276.5 GPS week: 2276 Day: 5 MJD: 60181
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 0 -14 -4 10 -.01 16 13 | 27311 -4705 3636 9667
esa n/a| 1 0 2 -8 0 13 -.19 28 21 | 4159 -4278 3658 8227
gfz n/a| 0 -1 0 26 -7 -18 -.15 24 16 | 0 -4746 3717 8287
grg n/a| 2 0 -3 0 8 -39 .34 21 17 | -106 -5245 3673 7924
jgx n/a| 0 3 0 18 39 -61 -.30 31 31 | 28755 -5846 3736 8100
Table 2.2276.6 GPS week: 2276 Day: 6 MJD: 60182
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 2 1 -16 44 -.05 17 13 | 26629 1568 3636 9059
esa n/a| -1 0 3 -18 4 -23 -.29 30 21 | -2951 786 3634 7766
gfz n/a| 0 0 -3 54 0 -75 -.16 29 19 | 0 676 3727 8110
grg n/a| 1 0 -4 -31 7 -1 .33 19 15 | -234 1209 3699 7709
jgx n/a| 0 0 3 38 16 -21 -.28 26 25 | 26651 1803 3614 7756
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 3.2276.0 GPS week: 2276 Day: 0 MJD: 60176
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 667 27 89 26 19 32 25 | 114 53 116 104 72 97
R02 | 676 8 17 11 17 28 7 | 73 59 78 75 51 71
R03 | 1008 10 23 8 13 25 7 | 77 57 73 78 55 72
R04 | 858 14 25 23 16 24 11 | 91 80 91 92 79 87
R05 | 1535 11 34 26 14 30 12 | 80 73 99 94 70 85
R07 | 1936 13 20 13 21 34 9 | 80 70 84 72 57 76
R08 | 679 9 10 14 21 23 8 | 70 62 82 68 57 70
R09 | 892 8 12 12 11 13 6 | 44 51 48 46 44 46
R11 | 975 13 16 16 15 19 8 | 54 60 52 50 49 53
R12 | 914 9 17 9 22 12 8 | 48 47 53 58 43 51
R13 | 749 14 35 28 46 60 18 | 73 59 62 69 57 65
R14 | 799 5 7 8 12 10 5 | 59 58 54 57 52 57
R15 | 803 9 15 16 19 9 8 | 63 59 60 70 54 61
R16 | 1707 17 19 9 14 15 8 | 116 101 102 111 108 107
R17E | 849 12 13 13 23 --- 9 | 78 78 82 88 --- 80
R18E | 1843 8 16 8 20 16 7 | 60 63 64 72 63 63
R19E | 1635 36 37 42 31 48 21 | 35 48 58 51 52 40
R20E | 5740 44 89 55 64 49 35 | 55 102 88 64 69 56
R21E | 1193 11 26 23 31 15 13 | 89 85 92 96 90 89
R22E | 3809 11 15 11 21 11 8 | 19 25 24 33 19 21
R24E | 864 12 19 18 22 20 10 | 130 127 134 142 133 132
XR25E |10076 5 15 --- --- --- 10 | 30 33 --- --- --- 30
------+------------------------------------+--------------------------------
RMS | 1864 17 34 22 25 28 |T 69 65 76 75 63 68
WRMS | 1864 12 29 16 19 28 |NE 74 63 75 74 60 71
MEDI | 914 11 17 14 20 20 |MD 70 59 78 72 57 65
Table 3.2276.1 GPS week: 2276 Day: 1 MJD: 60177
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 771 28 77 23 21 23 22 | 72 28 60 59 45 54
R02 | 728 13 18 29 14 21 11 | 51 50 79 55 47 57
R03 | 1327 7 25 13 15 27 8 | 53 38 56 58 37 50
R04 | 980 9 13 10 15 23 6 | 66 65 58 59 54 61
R05 | 1149 10 19 14 17 14 8 | 48 46 59 64 53 53
R07 | 1548 20 23 11 14 23 10 | 54 40 47 47 34 46
R08 | 1125 10 14 18 14 27 8 | 46 39 49 43 34 43
R09 | 682 9 10 12 10 11 6 | 30 35 34 35 30 32
R11 | 867 11 17 10 13 13 7 | 47 55 52 36 44 46
R12 | 1415 10 13 12 12 17 6 | 33 31 36 31 26 31
R13 | 798 19 44 14 34 53 16 | 58 38 41 53 41 48
R14 | 911 5 15 13 11 14 6 | 37 39 36 36 34 36
R15 | 1253 11 10 19 13 12 8 | 36 44 56 41 39 42
R16 | 1760 23 16 22 13 22 11 | 86 72 71 82 69 76
R17E | 893 12 22 17 22 --- 10 | 83 83 83 84 --- 81
R18E | 1982 10 16 12 17 12 8 | 53 57 54 52 51 52
R19E | 1096 22 44 50 24 42 20 | 46 41 67 49 45 44
R20E | 6558 27 81 74 73 90 36 | 62 87 115 58 76 68
R21E | 1236 9 17 17 18 14 8 | 73 72 75 79 72 73
R22E | 3151 16 6 12 17 19 8 | 20 27 33 33 26 25
R24E | 1015 13 18 15 15 11 9 | 101 109 110 106 105 105
XR25E |10337 8 17 --- --- --- 12 | 21 26 --- --- --- 22
------+------------------------------------+--------------------------------
RMS | 1947 15 31 25 23 30 |T 53 51 60 55 48 52
WRMS | 1947 13 24 14 17 30 |NE 51 44 52 49 41 48
MEDI | 1125 11 17 14 15 19 |MD 51 41 56 53 44 48
Table 3.2276.2 GPS week: 2276 Day: 2 MJD: 60178
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 903 22 78 24 19 46 22 | 81 30 83 86 39 69
R02 | 810 7 12 8 13 20 6 | 57 47 53 52 41 52
R03 | 1093 12 13 10 15 14 7 | 63 54 62 52 49 56
R04 | 1399 11 13 16 22 21 9 | 77 71 78 76 77 74
R05 | 1179 9 16 14 12 21 7 | 69 73 69 75 58 70
R07 | 763 12 36 17 15 38 11 | 65 52 82 82 53 69
R08 | 726 9 24 25 13 15 10 | 56 48 74 57 49 57
R09 | 1230 17 16 14 11 23 8 | 30 31 34 29 31 29
R11 | 1199 12 15 16 11 12 7 | 32 35 34 34 35 32
R12 | 1484 8 13 15 20 15 8 | 42 45 46 54 46 45
R13 | 527 19 34 22 29 42 15 | 51 44 42 47 38 44
R14 | 1149 10 13 20 11 12 8 | 49 46 33 42 45 42
R15 | 939 12 10 10 17 25 7 | 52 62 60 61 48 57
R16 | 1020 13 16 18 21 16 10 | 101 106 104 97 96 100
R17E | 1170 6 22 13 16 --- 8 | 58 65 58 63 --- 58
R18E | 1661 8 18 11 20 21 8 | 53 59 59 56 45 54
R19E | 1182 25 38 48 33 --- 20 | 52 58 78 55 --- 55
R20E | 4393 45 68 70 33 --- 31 | 62 63 94 74 --- 61
R21E | 751 9 17 15 21 19 9 | 65 70 77 74 69 69
R22E | 2733 14 14 20 14 16 9 | 30 34 35 40 29 31
R24E | 907 11 14 18 14 13 8 | 92 95 94 97 94 93
XR25E |11593 8 16 --- --- --- 12 | 25 29 --- --- --- 25
------+------------------------------------+--------------------------------
RMS | 1535 16 30 24 19 24 |T 57 55 64 62 52 56
WRMS | 1535 12 22 15 17 24 |NE 58 53 61 60 50 56
MEDI | 1149 11 16 16 16 19 |MD 56 52 62 57 46 56
Table 3.2276.3 GPS week: 2276 Day: 3 MJD: 60179
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 747 31 83 21 21 37 24 | 87 45 83 84 45 70
R02 | 596 11 19 9 14 33 7 | 53 52 60 69 34 57
R03 | 830 7 14 10 9 22 6 | 53 40 56 52 35 50
R04 | 1192 12 14 16 22 18 9 | 55 43 53 43 46 48
R05 | 1142 9 13 14 12 16 7 | 54 47 52 56 43 51
R07 | 1342 12 24 10 13 16 8 | 68 63 74 74 62 69
R08 | 739 22 34 40 17 20 17 | 57 54 104 86 62 73
R09 | 1194 6 15 14 10 20 6 | 20 24 35 26 17 25
R11 | 860 11 11 11 10 18 6 | 32 34 30 28 35 30
R12 | 1769 9 12 7 8 12 5 | 39 44 42 41 44 40
R13 | 678 14 31 28 41 --- 16 | 52 35 38 57 --- 43
R14 | 1307 9 9 14 12 10 6 | 46 46 51 41 48 45
R15 | 650 10 11 16 29 13 10 | 52 55 53 67 55 55
R16 | 1020 12 20 13 11 15 8 | 62 88 75 71 73 71
R17E | 968 6 20 11 16 --- 7 | 69 70 63 68 --- 66
R18E | 1602 8 18 15 20 11 8 | 34 41 33 41 32 34
R19E | 1559 31 46 78 48 38 30 | 40 54 108 45 39 52
R20E | 1506 45 61 58 62 --- 32 | 60 48 87 48 --- 52
R21E | 924 12 17 17 19 18 9 | 44 38 44 53 37 43
R22E | 1652 15 15 13 16 19 8 | 20 27 25 33 25 23
R24E | 1079 12 20 14 19 17 9 | 124 131 138 127 128 129
XR25 |13500 12 24 --- --- --- 17 | 27 47 --- --- --- 33
------+------------------------------------+--------------------------------
RMS | 1166 17 30 27 25 21 |T 52 51 62 57 47 52
WRMS | 1166 13 21 11 25 21 |NE 52 47 57 56 46 51
MEDI | 1079 12 18 14 16 18 |MD 52 46 53 53 43 50
Table 3.2276.4 GPS week: 2276 Day: 4 MJD: 60180
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 536 23 95 19 26 40 24 | 88 55 93 94 64 80
R02 | 824 8 15 9 21 25 7 | 59 53 65 64 43 60
R03 | 1557 11 13 10 15 28 7 | 67 56 56 68 44 61
R04 | 1017 8 14 16 24 29 9 | 77 76 77 74 73 75
R05 | 1196 8 9 9 12 12 5 | 67 68 72 73 61 69
R07 | 870 17 24 11 11 23 9 | 75 53 70 72 58 68
R08 | 899 11 29 12 18 15 9 | 65 53 77 81 63 69
R09 | 1385 9 8 10 12 12 5 | 27 33 32 25 32 28
R11 | 852 16 20 11 11 21 8 | 38 32 30 31 28 31
R12 | 1834 9 16 7 10 17 6 | 46 43 39 42 49 42
XR13 | 820 23 36 14 --- --- 16 | 41 45 34 --- --- 33
R14 | 916 8 7 8 9 16 5 | 52 63 66 51 54 57
R15 | 1186 8 18 8 20 16 7 | 57 46 53 61 47 54
R16 | 1030 13 26 11 19 15 9 | 116 132 112 124 120 118
R17E | 858 8 24 7 23 --- 8 | 68 65 71 80 --- 69
R18E | 1570 8 20 8 15 11 7 | 55 58 52 55 50 53
R19E | 1813 18 29 21 30 30 13 | 46 67 69 53 52 54
R20E | 1506 41 56 52 57 64 29 | 64 83 101 65 68 66
R21E | 1441 13 23 17 22 17 10 | 64 59 75 75 59 67
R22E | 1020 14 7 14 15 21 8 | 33 35 48 42 32 39
R24E | 1475 16 20 15 35 19 12 | 112 106 116 139 123 116
XR25 |14563 7 17 --- --- --- 11 | 30 35 --- --- --- 30
------+------------------------------------+--------------------------------
RMS | 1241 15 30 17 23 26 |T 61 59 67 68 58 60
WRMS | 1241 12 20 12 17 26 |NE 62 57 62 66 56 60
MEDI | 1030 11 20 11 18 19 |MD 59 55 69 65 54 60
Table 3.2276.5 GPS week: 2276 Day: 5 MJD: 60181
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 544 21 83 30 23 43 24 | 79 31 88 80 52 69
R02 | 707 10 18 18 11 21 8 | 49 41 57 55 49 49
R03 | 1774 13 22 11 11 28 8 | 60 41 51 59 41 53
R04 | 1305 10 14 8 13 34 6 | 68 60 57 66 57 63
R05 | 1396 11 9 14 19 17 8 | 60 55 62 52 49 56
R07 | 865 9 19 7 15 31 7 | 58 49 55 64 45 56
R08 | 834 12 19 12 13 17 8 | 51 42 40 53 38 45
R09 | 834 16 14 18 20 17 10 | 32 30 26 36 30 28
R11 | 637 8 9 15 9 14 6 | 30 39 33 28 34 31
R12 | 1268 5 14 8 15 12 6 | 32 39 36 35 28 34
R13 | 897 22 24 19 24 --- 13 | 37 38 37 30 --- 34
R14 | 694 12 7 9 14 16 6 | 33 45 49 46 36 41
R15 | 903 14 12 21 16 24 9 | 40 35 45 38 34 38
R16 | 1118 19 11 25 16 16 11 | 114 109 109 120 110 112
R17E | 884 11 22 12 28 --- 10 | 82 85 87 93 --- 85
R18E | 1285 8 16 17 21 11 9 | 50 52 53 57 44 50
R19E | 1535 28 40 50 18 47 20 | 42 47 64 46 44 42
R20E | 1452 33 60 67 46 88 30 | 60 46 105 55 53 60
R21E | 1121 8 20 8 19 16 8 | 78 75 72 85 76 76
R22E | 1259 15 10 12 14 13 7 | 22 28 32 33 27 26
R24E | 1661 12 26 19 35 22 13 | 124 139 134 127 131 128
XR25E |12610 7 15 --- --- --- 11 | 23 26 --- --- --- 22
------+------------------------------------+--------------------------------
RMS | 1146 16 28 24 21 31 |T 55 52 61 59 51 54
WRMS | 1146 13 21 16 17 31 |NE 53 46 53 54 46 50
MEDI | 1118 12 16 15 16 17 |MD 50 42 55 55 44 49
Table 3.2276.6 GPS week: 2276 Day: 6 MJD: 60182
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 687 25 79 23 20 41 23 | 118 54 118 117 85 102
R02 | 739 10 20 8 17 12 8 | 69 60 73 77 57 69
R03 | 1558 11 25 9 16 22 9 | 86 62 83 94 68 82
R04 | 1278 15 15 20 14 12 9 | 92 78 73 87 83 83
R05 | 1083 15 13 12 9 15 7 | 80 69 76 78 67 76
R07 | 860 12 14 20 17 12 9 | 88 73 92 84 76 84
R08 | 829 11 13 28 13 25 9 | 75 73 102 89 70 83
R09 | 755 12 16 17 13 13 8 | 39 37 30 32 36 34
R11 | 620 8 11 11 9 15 5 | 40 45 38 41 45 40
R12 | 1292 8 15 16 10 11 7 | 50 48 49 50 47 48
R13 | 1992 34 42 30 29 52 19 | 65 44 42 44 28 48
R14 | 887 11 8 19 10 10 7 | 52 55 54 52 53 52
R15 | 618 10 11 14 15 11 7 | 58 60 62 69 61 61
R16 | 1017 15 14 24 13 15 9 | 127 122 118 128 127 124
R17 | 806 12 18 18 21 --- 10 | 74 76 73 75 --- 72
R18E | 914 9 19 20 10 13 8 | 63 72 70 71 64 67
R19E | 2321 33 42 58 30 44 23 | 47 45 85 54 42 48
R20E | 1684 34 67 81 43 61 32 | 78 79 115 62 69 70
R21E | 1247 10 16 20 19 9 9 | 104 103 102 105 102 102
R22E | 2047 13 9 21 14 16 8 | 20 31 41 38 34 29
R24E | 2308 13 22 24 22 19 11 | 125 132 131 130 127 128
XR25 |15084 7 16 --- --- --- 11 | 28 30 --- --- --- 28
------+------------------------------------+--------------------------------
RMS | 1332 17 30 29 19 26 |T 71 65 77 75 67 69
WRMS | 1332 13 21 19 15 25 |NE 74 62 72 74 64 70
MEDI | 1017 12 16 20 15 15 |MD 69 60 73 75 64 69
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