[IGSREPORT-29894] Wk 2313 IGLOS Final Orbits
acc
acc at igs.org
Tue May 28 01:52:41 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2313 (May 05, 2024 - May 11, 2024)
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 2.2313.
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:
igl2313[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2313 in the SP3 format.
igl23137.sum Combination Report for GPS Week 2313.
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).
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 | 1.2 ns
1 | 0.7 ns
2 | 0.4 ns
3 | -0.3 ns
4 | 5.9 ns
5 | 1.3 ns
6 | 4.9 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 | ESA | R20
1 | ESA | R20
2 | ESA | R20
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 1.2313, 1a.2313).
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 2.2313.0-6)
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 3.2313.0-6).
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 2313 summary. (May 05, 2024 - May 11, 2024)
Table 1.2313.a GPS week : 2313 MJD: 60435.0-60441.0
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 3 -3 -17 33 .10 18 16 | 10900 242 3995 33404
| 1 1 1 17 14 27 .03 | 1593 2152
esa n/a| -1 0 1 0 -14 4 -.06 38 25 | 1573 1227 2965 7355
| 1 1 1 9 18 24 .02 | 3003 2612
gfz n/a| 1 0 1 14 -2 -5 .02 21 15 | 0 -239 2934 7045
| 1 1 1 19 15 34 .06 | 0 2313
grg n/a| 1 0 0 -44 10 13 .32 32 26 | 8294 -83 4053 33775
| 1 1 2 17 23 33 .05 | 1988 2253
iac n/a| -2 0 -4 19 3 7 -.15 27 24 | 9799 398 4099 35078
| 2 2 2 26 25 84 .05 | 2602 1390
jgx n/a| -1 0 -7 0 31 -99 -.19 28 27 | 6600 465 2977 7424
| 1 2 3 21 18 69 .04 | 1909 2325
Table 1.2313.b GPS week : 2313 MJD: 60435.0-60441.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 15 15 14 13 16 15 15 |
R02 | 6 5 6 6 7 6 10 |
R03 | 6 6 8 7 8 6 8 |
R04 | 7 7 7 7 7 8 7 |
R05 | 7 8 6 7 6 8 9 |
R07 | 4 7 7 7 8 7 8 |
R08 | 5 6 7 7 8 6 9 |
R09 | 8 8 14 12 12 9 10 |
R11 | 6 6 7 10 8 7 8 |
R12 | 8 8 7 9 13 8 8 |
R13 | 12 13 15 22 19 23 21 |
R14 | 6 6 8 12 9 7 9 |
R15 | 6 8 8 14 11 8 6 |
R16 | 7 7 8 18 12 10 13 |
R17 | 9 6 6 6 9 10 10 |
R18 | 7 10 7 9 9 8 8 |
R19 | 19 19 17 19 17 19 20 |
R20 | 21 21 26 28 25 33 33 |
R21 | 8 9 8 7 8 9 7 |
R22 | 6 7 6 7 6 7 8 |
R24 | 8 10 8 11 10 8 9 |
R25 | 9 11 9 13 11 18 11 |
R26 | 24 32 30 35 26 31 26 |
Table 1.2313.c GPS week : 2313 MJD: 60435.0-60441.0
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 2313 0 | 148 -74 246 659 1125 -2489 79.0 1881 1881 | 1223 0
brd 2313 1 | -12 -17 261 -183 531 -854 77.7 1896 1896 | 721 0
brd 2313 2 | -7 13 197 1325 2349 -596 81.1 1718 1718 | 434 0
brd 2313 3 | 42 -4 42 2293 2804 5487 81.4 2029 2029 | -314 0
brd 2313 4 | 3 -80 174 2958 2123 5703 81.6 2233 2233 | 5852 0
brd 2313 5 | 58 9 173 -711 865 6813 79.7 2504 2504 | 1318 0
brd 2313 6 | -68 26 98 -1202 480 6593 79.9 2507 2507 | 4871 0
-------------+------------------------------------------------------------+----------------
brd 2313 mean| 23 -18 170 733 1468 2950 80.1 2109 2109 | 2015 0
brd 2313 sdev| 68 42 77 1549 942 4058 1.4 312 312 | 2366 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 2.2313.0 GPS week: 2313 Day: 0 MJD: 60435
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 3 -15 -12 -7 .11 18 18 | 12215 -1575 3503 27907
esa n/a| -2 -1 2 0 -27 -21 -.05 40 26 | 3790 -887 2939 8180
gfz n/a| 1 0 2 27 -3 1 .07 18 14 | 0 -1950 2937 8396
grg n/a| 0 2 0 -32 -3 18 .29 25 22 | 6950 -2184 3560 28016
iac n/a| 1 -3 -1 33 -14 74 -.16 17 16 | 8098 -187 3573 29419
jgx n/a| 0 0 -7 3 48 -114 -.19 24 24 | 9674 -2338 2972 8702
Table 2.2313.1 GPS week: 2313 Day: 1 MJD: 60436
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 -13 -37 16 .14 17 15 | 10340 317 3805 32359
esa n/a| -2 0 3 9 4 25 -.09 39 22 | 1396 812 3017 6981
gfz n/a| 2 0 0 25 5 -53 -.00 19 15 | 0 -202 3015 7324
grg n/a| 3 1 4 -25 33 53 .29 25 21 | 6955 30 3856 32803
iac n/a| -1 -1 -6 30 15 66 -.13 19 18 | 7885 220 3876 34170
jgx n/a| -1 0 -5 -22 30 -169 -.23 29 29 | 5900 420 3101 7639
Table 2.2313.2 GPS week: 2313 Day: 2 MJD: 60437
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 6 -10 -18 80 .09 17 14 | 10580 349 3770 31814
esa n/a| -3 -2 -1 -4 -36 39 -.08 43 28 | -646 1925 2975 7679
gfz n/a| 0 0 0 41 -13 50 .09 15 12 | 0 501 2976 6617
grg n/a| 1 0 3 -61 37 -37 .38 31 24 | 6067 497 3835 31903
iac n/a| -2 4 -2 21 42 -105 -.23 21 20 | 8286 782 3839 33412
jgx n/a| -2 -1 -11 -22 9 -163 -.20 33 33 | 6846 816 3055 6974
Table 2.2313.3 GPS week: 2313 Day: 3 MJD: 60438
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 -17 -7 49 .14 19 14 | 8281 -2102 4276 33118
esa n/a| -1 0 2 -2 -8 2 -.06 36 25 | 4371 -1798 2854 7558
gfz n/a| 3 -1 3 17 -15 -23 .04 24 16 | 0 -3463 2666 7281
grg n/a| 1 -1 -1 -25 -7 3 .35 49 46 | 7290 -3093 4256 33397
iac n/a| -6 3 -4 -5 2 52 -.20 26 28 | 7017 375 4405 34720
jgx n/a| -2 -2 -6 9 32 -133 -.16 28 28 | 5176 -2991 2678 7501
Table 2.2313.4 GPS week: 2313 Day: 4 MJD: 60439
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 3 2 17 2 37 .12 18 15 | 11252 3754 4240 34550
esa n/a| 0 -1 0 9 -35 2 -.07 35 22 | 4889 5265 2896 8432
gfz n/a| 1 0 4 -1 -10 24 .01 19 13 | 0 2851 2919 7317
grg n/a| 0 0 0 -71 10 4 .23 36 24 | 10749 3034 4348 35163
iac n/a| -2 -1 -7 -7 26 4 -.11 28 26 | 12559 2793 4356 36295
jgx n/a| 0 -1 -10 15 6 -99 -.21 29 29 | 6361 2897 2910 7461
Table 2.2313.5 GPS week: 2313 Day: 5 MJD: 60440
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 3 -8 -35 39 .06 18 16 | 10332 -1333 4205 36654
esa n/a| -1 0 2 6 -7 12 -.02 34 24 | 582 -602 3118 7126
gfz n/a| 1 2 0 2 28 -11 -.03 25 17 | 0 -1721 3074 7177
grg n/a| 0 -2 1 -46 -23 57 .29 32 24 | 8991 -1180 4268 37217
iac n/a| -2 3 -5 -4 -24 -115 -.09 34 26 | 11115 -1892 4301 38496
jgx n/a| 0 -2 -2 33 55 -41 -.13 28 24 | 3963 2673 3121 8057
Table 2.2313.6 GPS week: 2313 Day: 6 MJD: 60441
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 -1 5 24 -13 19 .07 21 19 | 13305 2286 4170 37431
esa n/a| 0 -1 0 -15 7 -31 -.06 36 25 | -3371 3877 2960 5530
gfz n/a| 0 0 1 -13 -9 -26 -.07 24 16 | 0 2309 2954 5207
grg n/a| 3 0 -1 -47 28 -6 .38 27 23 | 11060 2309 4253 37932
iac n/a| 0 1 -6 65 -24 77 -.14 41 34 | 13634 699 4343 39038
jgx n/a| -2 4 -9 -13 38 23 -.23 28 24 | 8283 1784 3005 5635
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 3.2313.0 GPS week: 2313 Day: 0 MJD: 60435
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 837 41 56 18 19 20 28 14 | 95 42 85 74 72 68 73
R02M | 1297 11 17 11 10 19 9 6 | 73 72 73 72 68 67 70
R03 | 1098 13 17 11 10 17 10 6 | 79 84 80 88 84 75 80
R04 | 601 12 17 12 22 15 18 7 | 82 77 76 68 72 62 72
R05 | 595 13 15 10 22 22 13 7 | 82 75 78 69 90 69 77
R07M | 1327 6 7 8 13 9 10 4 | 78 72 73 86 83 70 76
R08M | 823 13 10 12 8 13 12 5 | 74 82 76 79 83 76 78
R09E | 4211 20 10 14 26 18 17 8 | 67 57 61 51 54 63 57
R11E | 1915 13 13 13 13 11 16 6 | 49 46 50 47 46 46 46
R12E | 2689 13 16 15 17 22 17 7 | 219 215 227 228 226 231 223
R13E | 2192 21 31 35 22 24 26 12 | 56 68 78 78 61 57 62
R14E | 1117 15 16 10 16 9 11 5 | 148 155 151 160 145 156 152
R15E | 1778 10 14 17 18 13 9 6 | 78 85 80 86 81 82 81
R16E | 1478 9 27 12 15 12 11 6 | 63 66 57 70 63 65 62
XR17 | 1947 6 19 23 18 14 --- 8 | 30 30 39 37 29 --- 30
R18 | 1208 15 15 14 12 19 20 7 | 25 27 27 27 27 21 23
R19 | 3379 35 26 23 74 27 47 18 | 44 43 49 44 36 44 38
R20 | 1933 25 150 36 50 18 67 21 | 78 56 88 91 82 63 76
R21M | 803 12 26 19 15 12 21 8 | 45 39 44 53 43 40 43
R22M | 2418 11 15 15 10 9 17 6 | 23 31 27 32 25 31 25
R24M | 933 16 26 15 10 20 19 8 | 38 33 38 41 39 29 35
XR25M |15772 12 13 --- --- 13 --- 9 | 25 24 --- --- 23 --- 22
XR26M |13329 33 --- --- 19 42 --- 23 | 31 --- --- 39 79 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1881 18 40 18 25 17 24 |T 68 67 74 73 70 70 67
WRMS | 1881 18 26 14 22 16 24 |NE 60 56 62 60 60 55 56
MEDI | 1478 13 16 14 16 17 17 |MD 67 57 73 69 68 63 62
Table 3.2313.1 GPS week: 2313 Day: 1 MJD: 60436
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 677 41 43 23 29 14 39 15 | 60 41 56 54 54 44 49
R02M | 1180 9 13 8 10 7 18 5 | 39 33 34 40 35 45 36
R03 | 709 14 10 11 14 13 14 5 | 47 52 55 54 44 54 49
R04 | 631 11 13 10 15 18 19 6 | 53 57 50 63 49 48 52
R05 | 1020 16 12 16 28 19 14 8 | 58 63 68 58 67 60 61
R07M | 1085 13 6 21 16 21 15 7 | 53 48 39 59 57 46 48
R08M | 957 11 11 9 12 17 20 6 | 45 57 54 49 55 41 49
R09E | 3660 13 15 15 25 19 18 7 | 54 47 52 47 57 60 51
R11E | 1394 12 11 10 14 12 20 6 | 37 37 39 37 39 42 36
R12E | 4574 9 15 14 24 17 21 7 | 218 220 210 214 223 214 216
XR13E | 1518 22 30 35 23 14 --- 13 | 47 63 76 54 46 --- 53
R14E | 1580 12 16 16 13 12 13 6 | 118 112 115 116 115 112 114
R15E | 1640 16 16 18 19 19 12 7 | 69 67 73 73 71 67 68
R16E | 1007 11 20 19 15 11 16 7 | 48 51 47 56 48 51 48
XR17 | 1836 5 16 7 14 12 --- 5 | 24 23 22 27 24 --- 22
R18 | 908 20 12 12 18 33 27 9 | 21 22 32 30 37 19 24
R19 | 2438 28 47 38 58 19 58 18 | 27 42 41 24 25 25 25
R20 | 1778 22 147 33 44 37 71 21 | 35 46 42 44 37 58 43
R21M | 1245 11 23 26 21 9 22 8 | 41 36 51 52 41 42 42
R22M | 2842 13 10 21 15 9 19 6 | 18 22 32 26 21 26 20
R24M | 608 16 22 10 22 26 31 9 | 31 37 32 37 39 35 32
XR25M |13635 15 8 --- --- 19 --- 10 | 18 20 --- --- 28 --- 19
XR26M |12839 37 --- --- 29 59 --- 31 | 29 --- --- 32 68 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1896 17 39 19 25 19 29 |T 51 54 58 56 55 57 52
WRMS | 1896 15 22 15 21 18 29 |NE 37 43 44 42 40 44 39
MEDI | 1394 13 15 16 18 17 19 |MD 45 46 50 49 46 46 48
Table 3.2313.2 GPS week: 2313 Day: 2 MJD: 60437
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1251 33 41 11 38 17 46 13 | 67 44 61 63 51 45 54
R02M | 1432 7 19 8 14 17 17 6 | 63 55 64 67 64 55 60
R03 | 742 10 16 16 27 11 21 7 | 62 62 66 80 63 65 64
R04 | 892 18 8 9 24 18 19 7 | 70 61 57 62 55 59 60
R05 | 1357 10 16 9 16 13 16 5 | 66 79 72 60 69 68 68
R07M | 671 10 11 14 21 15 25 7 | 71 60 69 83 72 60 68
R08M | 759 7 11 13 9 17 28 6 | 64 59 63 60 67 59 61
R09E | 3843 18 19 18 66 37 22 13 | 64 58 68 96 58 64 61
R11E | 1660 13 13 10 15 19 29 7 | 43 42 45 40 48 44 42
R12E | 2245 10 16 14 15 14 18 6 | 211 216 212 211 211 214 212
XR13E | 2031 27 33 33 35 18 --- 15 | 70 78 85 77 63 --- 71
R14E | 1459 12 17 15 28 22 13 8 | 172 168 169 176 165 169 169
R15E | 2100 14 14 17 21 24 20 8 | 94 93 95 93 102 92 94
R16E | 1062 10 27 18 16 13 20 8 | 70 72 67 62 71 65 66
XR17 | 1002 12 12 15 8 12 --- 6 | 27 29 34 28 22 --- 24
R18 | 998 14 17 10 11 14 22 6 | 26 20 21 29 22 25 21
R19 | 1537 34 42 23 63 26 47 17 | 33 32 38 39 37 42 31
R20 | 1851 31 165 25 64 43 99 25 | 62 76 47 38 32 79 45
R21M | 1632 10 23 15 19 21 18 7 | 30 35 36 38 31 33 32
R22M | 2810 13 12 11 12 14 17 5 | 22 32 37 34 24 26 26
R24M | 805 17 27 8 13 23 20 8 | 35 31 29 30 31 25 26
XR25M |13331 11 14 --- --- 12 --- 8 | 27 24 --- --- 34 --- 26
XR26M |11274 27 --- --- 32 62 --- 30 | 37 --- --- 33 72 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 1717 17 43 15 31 21 33 |T 64 64 68 68 63 67 61
WRMS | 1717 14 28 12 24 20 33 |NE 49 51 47 48 42 56 44
MEDI | 1459 13 16 14 19 17 20 |MD 63 58 63 60 58 59 60
Table 3.2313.3 GPS week: 2313 Day: 3 MJD: 60438
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 2134 30 43 10 40 16 28 13 | 213 207 213 221 215 221 212
R02M | 2447 10 10 12 14 16 16 6 | 67 77 78 67 61 73 70
R03 | 726 6 12 19 11 20 22 7 | 62 60 71 65 74 55 63
R04 | 1078 18 7 10 14 12 20 6 | 61 49 49 54 44 46 49
R05 | 2174 16 13 16 11 13 17 6 | 54 61 65 63 54 52 56
R07M | 941 10 12 16 14 13 24 6 | 69 73 83 77 75 64 72
R08M | 751 8 10 21 12 11 23 6 | 74 69 84 74 68 67 72
R09E | 4990 21 24 15 54 25 20 11 | 55 59 63 70 68 51 55
R11E | 1726 13 14 19 50 20 19 9 | 53 54 58 70 60 57 53
R12E | 869 11 12 20 25 27 24 9 | 301 298 294 300 303 301 299
R13E | 1690 32 36 52 106 17 56 21 | 74 79 86 112 66 80 70
R14E | 1496 9 17 16 70 33 15 12 | 134 141 142 155 130 139 136
R15E | 819 14 26 27 36 54 16 13 | 100 107 99 97 102 99 97
R16E | 940 15 21 33 96 46 32 17 | 61 69 72 112 68 76 63
XR17 | 864 6 16 7 16 16 --- 6 | 34 34 34 41 41 --- 34
R18 | 747 18 21 18 26 17 19 8 | 32 33 44 50 42 42 36
R19 | 2560 30 46 22 75 36 52 18 | 33 36 35 42 42 41 29
R20 | 2793 34 128 44 75 27 39 28 | 65 47 75 74 55 62 53
R21M | 1264 7 16 22 12 11 22 7 | 43 34 41 41 45 41 39
R22M | 3267 14 19 12 22 12 18 7 | 25 27 26 26 27 29 23
R24M | 1238 15 24 25 23 33 25 11 | 50 54 49 47 57 48 46
XR25M |19149 13 14 --- --- 24 --- 12 | 24 31 --- --- 43 --- 27
XR26M |15621 35 --- --- 43 65 --- 34 | 110 --- --- 121 140 --- 117
------+-----------------------------------------+-------------------------------------
RMS | 2030 19 36 24 49 26 28 |T 78 77 83 89 81 82 77
WRMS | 2030 14 25 16 46 28 28 |NE 48 45 53 55 50 49 45
MEDI | 1496 14 16 19 25 20 22 |MD 61 59 71 70 61 57 56
Table 3.2313.4 GPS week: 2313 Day: 4 MJD: 60439
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 893 37 51 21 46 24 36 16 | 568 560 559 571 570 571 565
R02M | 2255 9 16 11 16 19 17 6 | 54 51 57 58 43 45 51
R03 | 972 14 9 13 15 31 16 7 | 41 45 57 45 65 46 48
R04 | 1240 16 19 10 18 21 15 7 | 56 52 48 42 48 46 48
R05 | 1915 8 15 9 18 14 17 5 | 51 52 48 44 54 57 50
R07M | 1531 12 18 12 24 23 17 7 | 62 69 70 83 76 63 68
R08M | 952 10 19 10 18 26 19 7 | 108 112 112 106 116 108 109
R09E | 5248 21 14 29 40 20 29 11 | 48 41 57 47 45 45 42
R11E | 2107 11 14 16 31 12 26 8 | 117 117 110 133 114 116 116
R12E | 551 12 14 20 51 50 22 12 | 209 210 214 229 196 208 209
R13E | 1103 43 45 28 50 40 48 18 | 91 78 101 96 77 60 84
R14E | 1561 15 16 15 39 11 17 8 | 133 143 141 149 132 139 138
R15E | 1432 9 19 21 60 17 22 11 | 97 101 106 120 101 96 100
R16E | 1215 16 29 23 40 29 23 11 | 81 93 88 113 70 82 83
XR17 | 952 9 25 12 9 31 --- 9 | 34 27 37 39 59 --- 35
R18 | 613 20 13 16 16 30 19 9 | 30 33 36 32 38 28 30
R19 | 4562 19 30 21 61 29 70 17 | 47 52 40 63 49 61 46
R20 | 3554 18 120 34 52 60 38 25 | 70 58 78 81 88 75 69
R21M | 960 7 23 16 13 18 26 7 | 32 27 36 40 29 30 30
R22M | 2822 10 13 12 14 18 13 6 | 11 20 22 29 21 20 16
R24M | 1485 13 21 22 14 22 32 9 | 39 47 49 46 41 37 40
XR25M |21639 11 19 --- --- 17 --- 10 | 29 21 --- --- 22 --- 22
XR26M |15962 24 --- --- 23 56 --- 25 | 381 --- --- 379 400 --- 385
------+-----------------------------------------+-------------------------------------
RMS | 2232 18 35 19 36 28 29 |T 103 91 98 115 106 96 103
WRMS | 2232 15 22 13 24 26 29 |NE 47 45 49 49 57 52 46
MEDI | 1485 13 19 16 23 23 22 |MD 56 52 57 63 65 60 51
Table 3.2313.5 GPS week: 2313 Day: 5 MJD: 60440
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 739 30 44 20 40 32 35 15 | 977 975 968 977 970 975 974
R02M | 1481 11 12 11 13 20 16 6 | 60 51 54 48 58 48 52
R03 | 2778 11 10 11 17 25 9 6 | 50 45 58 59 49 52 51
R04 | 961 16 15 14 7 21 22 7 | 53 51 45 46 47 44 46
R05 | 2288 17 9 18 20 24 16 7 | 49 43 39 45 53 42 42
R07M | 1317 11 18 7 23 23 15 7 | 57 49 58 66 68 57 57
R08M | 937 7 14 9 18 24 13 6 | 184 185 182 187 181 192 185
R09E | 5888 21 17 20 28 16 14 9 | 57 58 65 42 56 54 54
R11E | 2467 12 15 13 16 26 14 7 | 182 188 190 179 195 185 186
R12E | 1772 12 15 11 21 15 24 7 | 275 265 261 271 272 264 268
R13E | 1282 29 50 59 67 45 58 23 | 79 82 106 99 76 67 79
R14E | 1536 11 16 8 14 23 17 6 | 145 143 145 147 146 147 145
R15E | 1882 11 12 23 19 17 14 7 | 82 85 90 87 85 84 84
R16E | 1055 19 18 25 18 40 17 10 | 70 68 71 75 84 77 70
XR17 | 880 8 10 15 26 38 --- 10 | 38 37 39 43 46 --- 36
R18 | 780 16 14 8 22 27 18 7 | 39 37 43 46 46 38 39
R19 | 5577 31 39 23 78 31 46 19 | 48 62 54 53 36 34 42
R20 | 2461 34 117 68 51 94 70 32 | 52 58 81 52 75 71 49
R21M | 1526 11 21 26 8 28 18 8 | 31 30 46 36 40 35 34
R22M | 3268 13 14 14 21 22 10 7 | 16 19 25 30 26 25 19
R24M | 1690 11 18 14 20 33 14 8 | 30 38 35 40 47 36 33
XR25M |19043 16 19 --- --- 41 --- 17 | 22 34 --- --- 58 --- 29
XR26M |16895 25 --- --- 24 79 --- 31 | 668 --- --- 661 683 --- 668
------+-----------------------------------------+-------------------------------------
RMS | 2504 18 34 25 32 34 28 |T 141 118 126 149 147 126 140
WRMS | 2504 16 24 17 24 26 24 |NE 47 47 51 49 50 46 43
MEDI | 1690 13 15 14 20 26 16 |MD 57 51 58 53 58 54 52
Table 3.2313.6 GPS week: 2313 Day: 6 MJD: 60441
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 764 33 48 23 35 27 28 14 | 9999 9999 9999 9999 9999 9999 9999
R02M | 2905 9 17 31 15 30 25 9 | 70 62 91 70 85 60 72
R03 | 3517 15 17 23 7 22 10 7 | 71 66 89 75 75 64 73
R04 | 1234 19 8 10 11 33 15 7 | 82 70 69 66 70 65 69
R05 | 959 24 15 10 21 27 17 8 | 82 68 73 61 74 62 69
R07M | 1150 11 15 17 20 30 15 8 | 77 71 81 89 83 74 78
R08M | 758 17 15 9 20 39 24 9 | 280 279 279 282 280 277 280
R09E | 5481 12 19 19 28 31 19 9 | 64 65 74 53 71 68 63
R11E | 3233 15 19 16 17 25 9 7 | 237 233 235 236 238 241 236
R12E | 3079 10 22 12 16 28 18 7 | 262 270 261 264 259 267 263
R13E | 970 29 48 51 26 89 40 20 | 95 97 134 107 148 95 107
R14E | 2053 11 14 11 13 52 12 8 | 151 151 153 155 162 149 152
R15E | 1669 9 15 10 14 18 16 6 | 95 97 100 100 98 93 96
R16E | 1049 21 27 34 14 41 32 12 | 79 66 78 79 76 77 72
XR17 | 1554 10 17 11 19 43 --- 9 | 57 51 55 64 67 --- 56
R18 | 751 12 28 12 13 35 15 8 | 58 51 53 57 76 51 55
R19 | 3483 35 34 23 72 55 37 20 | 68 57 71 72 84 65 64
R20 | 3299 50 121 55 55 78 78 32 | 109 67 102 114 110 98 95
R21M | 1042 10 14 7 11 19 26 6 | 49 51 55 56 45 50 50
R22M | 3226 18 15 16 19 26 12 7 | 42 43 38 52 42 40 41
R24M | 2419 12 20 19 15 21 31 9 | 58 55 59 68 71 58 59
XR25M |15661 10 15 --- --- 22 --- 10 | 41 47 --- --- 50 --- 43
XR26M |15582 24 --- --- 19 73 --- 26 | 992 --- --- 980 998 --- 990
------+-----------------------------------------+-------------------------------------
RMS | 2507 21 36 24 27 41 28 |T 141 96 107 147 148 102 140
WRMS | 2507 19 25 16 23 34 24 |NE 75 61 73 72 79 67 68
MEDI | 2053 15 17 16 17 30 18 |MD 77 66 78 75 76 68 72
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