[IGSREPORT-29805] Wk 2305 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 1 23:59:10 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2305 (Mar 10, 2024 - Mar 16, 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 2.2305.
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:
igl2305[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2305 in the SP3 format.
igl23057.sum Combination Report for GPS Week 2305.
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 | 4.1 ns
1 | 7.2 ns
2 | 5.2 ns
3 | 8.9 ns
4 | 5.8 ns
5 | 4.7 ns
6 | 3.6 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 | ALL | R25
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 1.2305, 1a.2305).
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 2.2305.0-6)
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 3.2305.0-6).
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 2305 summary. (Mar 10, 2024 - Mar 16, 2024)
Table 1.2305.a GPS week : 2305 MJD: 60379.0-60385.0
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 0 -6 -17 60 .13 19 15 | 1611 36 3470 7739
| 0 1 1 12 17 16 .02 | 1185 2214
esa n/a| 0 -1 1 -33 14 -9 -.02 24 17 | 1670 -649 3456 7980
| 1 1 1 10 12 24 .01 | 6379 2401
gfz n/a| 1 1 0 25 17 3 .03 25 16 | 0 70 3472 7263
| 1 0 1 15 18 21 .07 | 0 2329
grg n/a| 1 0 2 8 -5 15 .28 25 17 | 5459 -10 3471 6867
| 0 0 2 15 18 42 .05 | 1172 2244
iac n/a| -1 0 -2 -8 -8 -22 -.28 22 18 | 7333 -85 3474 7865
| 1 1 2 12 21 30 .09 | 1673 1288
jgx n/a| 0 0 0 24 -3 -81 -.15 28 28 | 3695 243 3545 7485
| 1 1 3 18 20 82 .03 | 1751 2329
Table 1.2305.b GPS week : 2305 MJD: 60379.0-60385.0
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 | 11 13 13 14 14 10 12 |
R02 | 5 7 8 7 7 6 5 |
R03 | 6 5 8 8 8 6 7 |
R04 | 7 5 6 6 6 7 5 |
R05 | 8 6 6 4 7 9 7 |
R07 | 8 7 7 6 7 6 6 |
R08 | 9 5 7 8 7 7 7 |
R09 | 9 6 8 8 9 7 8 |
R11 | 5 7 9 8 8 8 6 |
R12 | 7 9 7 8 7 9 8 |
R13 | 14 13 16 15 14 15 17 |
R14 | 7 6 7 6 5 7 8 |
R15 | 8 8 6 9 8 7 7 |
R16 | 9 9 9 7 9 8 8 |
R17 | 7 8 8 11 8 13 13 |
R18 | 8 7 7 8 9 7 16 |
R19 | 16 16 23 16 18 20 19 |
R20 | 30 27 29 23 28 28 27 |
R21 | 7 7 7 8 7 9 16 |
R22 | 8 6 8 7 7 8 6 |
R24 | 8 9 9 9 9 10 15 |
R25 | --- 13 11 11 12 10 10 |
R26 | --- --- --- --- --- 0 0 |
Table 1.2305.c GPS week : 2305 MJD: 60379.0-60385.0
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 2305 0 | -11 67 130 -1827 1098 564 80.1 1683 1683 | 4125 0
brd 2305 1 | 14 70 110 -1641 1335 -42 80.4 1623 1623 | 7240 0
brd 2305 2 | 6 37 133 493 998 -3528 79.9 1661 1661 | 5249 0
brd 2305 3 | 48 28 174 432 822 -5155 76.8 2013 2013 | 8929 0
brd 2305 4 | 16 86 163 1373 -1543 1150 78.5 1566 1566 | 5837 0
brd 2305 5 | -20 -75 96 1526 -1845 1501 79.9 1745 1745 | 4724 0
brd 2305 6 | 130 -22 115 1350 239 278 79.5 1754 1754 | 3629 0
-------------+------------------------------------------------------------+----------------
brd 2305 mean| 26 27 132 243 157 -747 79.3 1720 1720 | 5676 0
brd 2305 sdev| 50 57 28 1418 1312 2552 1.3 144 144 | 1859 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 2.2305.0 GPS week: 2305 Day: 0 MJD: 60379
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 -21 -35 61 .13 22 16 | 351 -1364 3408 6557
esa n/a| 0 0 0 -20 6 -39 -.03 25 17 | -7854 -1292 3400 7829
gfz n/a| 0 1 -2 37 17 -30 .02 26 15 | 0 -1219 3407 6640
grg n/a| 0 0 -1 -19 22 -12 .28 23 18 | 4482 -1245 3401 6303
iac n/a| 0 -1 0 -19 -24 -11 -.23 22 17 | 6074 -1298 3400 6932
jgx n/a| -3 0 0 46 -4 24 -.17 26 26 | 2133 -1508 3409 6750
Table 2.2305.1 GPS week: 2305 Day: 1 MJD: 60380
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 0 6 -20 27 .16 22 15 | 2844 972 3357 7245
esa n/a| 0 0 1 -24 -5 -7 -.01 22 15 | -2414 -1472 3271 7304
gfz n/a| 1 0 1 0 -5 0 -.08 23 14 | 0 1800 3239 6715
grg n/a| 1 0 -1 0 -3 -47 .33 20 17 | 6161 1729 3260 6197
iac n/a| -1 0 0 -19 15 3 -.20 21 14 | 9522 -129 3382 7478
jgx n/a| 0 0 -1 49 26 10 -.18 25 25 | 5231 1620 3376 6726
Table 2.2305.2 GPS week: 2305 Day: 2 MJD: 60381
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 -1 1 -23 -41 56 .11 18 14 | 1040 -2262 3256 8280
esa n/a| 0 -1 1 -50 33 15 -.05 28 18 | 8068 -2925 3245 7396
gfz n/a| 2 1 0 50 45 0 -.03 30 16 | 0 -2716 3297 7023
grg n/a| 1 -1 3 26 2 38 .31 23 18 | 6318 -2586 3297 6504
iac n/a| -1 1 -4 -19 -19 -60 -.19 26 18 | 6625 -651 3254 8164
jgx n/a| 0 1 -3 0 7 -127 -.19 25 25 | 3091 -1591 3350 7393
Table 2.2305.3 GPS week: 2305 Day: 3 MJD: 60382
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 6 -11 80 .12 18 17 | 1627 4252 2932 7664
esa n/a| -1 -2 2 -43 7 8 -.01 23 18 | 10994 4313 2930 7188
gfz n/a| 1 0 -3 23 19 15 .03 19 15 | 0 4032 2872 6879
grg n/a| 0 0 3 16 -38 5 .32 23 16 | 6828 3729 2880 6572
iac n/a| 0 0 -2 -11 18 -25 -.25 21 15 | 8920 2202 2928 7736
jgx n/a| 0 3 -4 29 8 -113 -.13 28 28 | 4785 4124 2939 7058
Table 2.2305.4 GPS week: 2305 Day: 4 MJD: 60383
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 0 -6 -1 71 .13 19 15 | 3030 520 3512 8355
esa n/a| 1 -2 1 -25 26 -44 -.01 26 18 | -73 21 3511 7664
gfz n/a| 4 1 1 21 31 -15 .02 28 21 | 0 812 3514 7935
grg n/a| 0 0 3 24 -14 87 .28 26 18 | 5453 596 3508 7397
iac n/a| -2 -1 -4 10 -32 13 -.29 17 15 | 8534 -640 3519 8577
jgx n/a| 0 -1 0 11 -23 -213 -.12 32 32 | 5031 1156 3556 8124
Table 2.2305.5 GPS week: 2305 Day: 5 MJD: 60384
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 0 6 60 .14 18 15 | 2345 -1775 4330 8256
esa n/a| 0 0 2 -35 15 11 -.02 23 16 | -221 -2449 4344 9593
gfz n/a| 1 0 -1 24 -4 31 .08 26 15 | 0 -1853 4429 7836
grg n/a| 1 -1 2 3 -6 21 .20 23 17 | 5559 -2172 4394 7513
iac n/a| 0 -1 -4 -4 -23 -66 -.32 20 18 | 6677 -1186 4313 8244
jgx n/a| 0 0 2 17 -35 -89 -.11 33 33 | 4877 -2630 4482 8173
Table 2.2305.6 GPS week: 2305 Day: 6 MJD: 60385
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 -6 -18 66 .15 17 12 | 46 -87 3495 7816
esa n/a| 1 -1 -1 -35 13 -10 -.01 23 16 | 3190 -743 3494 8890
gfz n/a| 2 1 -1 19 22 21 .14 25 15 | 0 -361 3551 7814
grg n/a| 1 -1 5 6 -2 14 .23 35 18 | 3414 -122 3558 7583
iac n/a| -4 -1 -3 3 6 -11 -.46 27 27 | 4979 1107 3527 7926
jgx n/a| 0 1 4 16 -3 -63 -.17 32 32 | 718 532 3706 8176
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 3.2305.0 GPS week: 2305 Day: 0 MJD: 60379
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 803 35 18 18 28 16 19 10 | 79 50 54 70 62 54 60
R02 | 1031 10 9 10 10 13 14 5 | 46 41 38 39 43 37 40
R03 | 1561 16 13 16 9 12 12 6 | 57 55 51 63 57 55 55
R04 | 699 17 14 10 15 11 23 7 | 70 63 68 65 59 61 64
R05M | 2278 19 14 22 22 21 7 8 | 45 44 40 38 46 37 39
R07 | 820 12 19 13 13 27 17 7 | 72 77 61 70 80 65 70
R08 | 1264 18 18 17 16 12 30 8 | 58 61 51 62 54 52 56
R09 | 2293 16 21 12 28 15 22 8 | 32 37 39 38 33 30 31
R11 | 1388 10 9 12 9 9 18 5 | 19 25 30 32 28 20 24
R12M | 987 16 18 14 20 13 17 7 | 58 71 63 44 59 51 57
R13M | 884 21 41 42 27 23 30 14 | 94 63 129 102 107 34 95
R14 | 1469 6 16 14 20 21 9 6 | 88 101 85 82 100 83 89
R15 | 2101 12 15 19 15 13 25 7 | 101 105 109 97 96 85 98
R16 | 1711 13 31 13 17 19 13 8 | 90 90 85 89 92 81 86
XR17E | 852 14 13 11 15 12 --- 6 | 66 58 63 63 61 --- 60
R18E | 1080 20 21 15 14 23 14 8 | 41 34 31 35 42 25 32
R19E | 2132 20 32 50 24 35 45 16 | 82 91 103 93 71 93 84
R20E | 1814 63 74 68 64 58 73 29 | 169 215 235 172 195 164 186
R21E | 1880 17 12 16 13 12 17 6 | 60 57 61 69 62 57 60
R22E | 3147 17 8 23 14 22 12 7 | 35 35 39 37 41 33 34
R24E | 1917 17 11 18 25 11 16 7 | 108 110 111 109 111 106 108
------+-----------------------------------------+-------------------------------------
RMS | 1683 22 25 26 23 22 26 |T 68 70 73 69 69 61 66
WRMS | 1683 16 17 15 18 17 26 |NE 63 65 61 63 64 56 61
MEDI | 1469 17 16 16 16 15 17 |MD 60 61 61 65 59 54 60
Table 3.2305.1 GPS week: 2305 Day: 1 MJD: 60380
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1761 44 27 16 14 18 39 12 | 48 43 37 35 34 47 35
R02 | 1051 13 20 7 14 12 19 6 | 30 37 33 29 34 26 30
R03 | 1198 10 12 13 11 11 13 5 | 43 39 48 41 40 37 40
R04 | 453 13 12 14 9 8 15 5 | 51 49 53 46 46 41 47
R05M | 2030 11 13 16 13 8 16 6 | 29 28 29 39 27 24 27
R07 | 587 9 14 20 9 22 11 7 | 53 56 39 57 59 51 52
R08 | 1943 15 8 9 6 8 16 5 | 44 43 47 55 46 38 45
R09 | 2078 15 8 16 17 13 11 6 | 30 35 39 33 42 30 33
R11 | 2556 15 13 10 24 14 16 7 | 24 28 23 37 21 21 22
R12M | 910 8 26 13 32 7 14 8 | 77 92 87 71 77 78 79
XR13M | 1809 19 39 24 22 23 --- 13 | 77 64 86 78 87 --- 77
R14 | 1660 9 12 11 20 11 16 6 | 77 83 81 70 82 72 77
R15 | 1692 12 15 17 19 9 23 7 | 83 83 91 77 81 70 80
R16 | 1054 19 26 18 14 12 24 8 | 70 74 77 70 70 57 68
XR17E | 1768 15 13 14 19 18 --- 8 | 66 64 67 76 57 --- 64
R18E | 723 10 19 13 19 10 16 6 | 30 30 33 35 27 26 27
R19E | 1957 22 34 45 36 32 33 15 | 58 49 74 63 66 60 55
R20E | 1445 58 58 70 36 69 68 27 | 115 147 150 123 120 128 122
R21E | 1686 19 17 14 11 13 16 6 | 52 54 45 53 49 50 49
R22E | 2410 17 9 13 13 17 10 6 | 29 27 34 34 33 27 28
R24E | 1559 18 13 16 24 20 18 8 | 116 112 111 110 114 122 112
XR25E |15063 13 --- --- --- 13 --- 13 | 21 --- --- --- 23 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 1622 22 22 23 20 21 25 |T 55 58 61 58 56 52 54
WRMS | 1622 15 15 14 17 14 25 |NE 50 52 53 51 52 44 49
MEDI | 1686 15 14 14 17 13 16 |MD 51 49 48 55 46 47 47
Table 3.2305.2 GPS week: 2305 Day: 2 MJD: 60381
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 2105 23 39 22 42 24 24 13 | 55 46 56 73 52 41 51
R02 | 985 20 20 16 14 10 24 8 | 29 36 29 24 25 24 23
R03 | 1686 12 17 18 24 12 17 7 | 45 43 35 61 49 44 44
R04 | 705 10 17 9 11 14 10 5 | 58 50 56 54 52 61 54
R05M | 1008 15 8 21 10 12 15 6 | 37 39 35 39 40 32 35
R07 | 714 16 8 19 12 13 19 6 | 57 51 42 44 56 44 48
R08 | 2981 11 14 9 19 18 18 6 | 51 52 46 50 44 44 46
R09 | 1710 15 17 14 21 20 17 8 | 16 29 30 19 32 28 20
R11 | 2905 10 13 17 36 12 19 8 | 16 17 21 32 22 16 15
R12M | 1405 7 18 16 13 13 21 6 | 93 102 99 90 93 90 93
XR13M | 1967 19 49 40 27 15 --- 15 | 79 52 111 111 78 --- 84
R14 | 772 10 20 10 12 17 16 6 | 68 78 66 81 68 61 69
R15 | 1717 10 19 9 11 11 18 6 | 81 84 84 82 89 73 81
R16 | 791 14 23 15 13 22 26 8 | 74 60 75 71 86 59 69
XR17E | 1568 15 13 17 18 16 --- 8 | 61 58 69 65 55 --- 60
R18E | 784 13 21 13 21 12 12 7 | 27 27 21 30 29 24 23
R19E | 1701 30 52 79 48 43 42 22 | 48 71 106 44 53 51 47
R20E | 2485 38 81 83 36 81 63 29 | 67 91 117 58 88 67 65
R21E | 1350 12 17 22 14 13 18 7 | 38 34 44 41 40 34 35
R22E | 1820 22 13 12 13 23 22 8 | 36 47 46 54 52 60 46
R24E | 945 18 15 12 23 26 22 9 | 82 86 88 86 72 90 82
XR25E |12099 15 18 --- --- 15 --- 11 | 14 26 --- --- 24 --- 17
------+-----------------------------------------+-------------------------------------
RMS | 1660 18 28 30 23 26 25 |T 51 53 60 57 54 49 50
WRMS | 1660 14 18 16 18 18 25 |NE 49 50 48 51 52 45 46
MEDI | 1568 15 17 16 18 15 19 |MD 51 50 56 54 52 44 47
Table 3.2305.3 GPS week: 2305 Day: 3 MJD: 60382
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1675 31 41 33 33 19 24 14 | 82 68 70 81 80 76 72
R02 | 832 16 10 13 14 10 27 7 | 40 35 31 30 36 30 31
R03 | 1766 15 10 19 21 7 22 7 | 56 44 44 50 47 42 45
R04 | 659 17 13 9 11 16 10 6 | 54 46 39 44 36 44 42
R05M | 863 6 9 10 10 10 11 4 | 46 45 40 42 43 43 42
R07 | 632 4 15 11 11 18 22 6 | 54 50 57 53 59 44 52
R08 | 2045 14 15 9 21 18 26 7 | 46 44 36 48 28 35 37
R09 | 1331 24 25 12 15 11 15 8 | 24 34 27 23 24 21 20
R11 | 2544 12 22 10 27 14 22 8 | 26 27 37 48 37 31 31
R12M | 1893 12 20 19 16 13 27 8 | 96 97 98 89 99 82 94
XR13M | 1162 15 40 25 40 24 --- 14 | 77 57 90 81 94 --- 79
R14 | 1276 5 17 7 10 13 17 5 | 63 74 66 63 61 70 65
R15 | 1082 23 20 12 21 13 27 8 | 73 69 58 61 55 42 58
R16 | 620 15 24 12 16 13 17 7 | 78 75 81 65 83 68 74
XR17E | 1005 20 13 19 34 18 --- 10 | 52 50 55 53 44 --- 48
R18E | 1937 12 19 16 29 10 22 8 | 31 31 37 34 29 34 29
R19E | 2746 28 32 28 45 39 47 16 | 58 58 73 69 66 71 58
R20E | 5269 34 50 43 37 62 73 22 | 102 114 119 92 104 106 100
R21E | 1112 11 18 23 24 13 13 8 | 55 51 63 61 55 58 54
R22E | 2462 15 11 12 12 20 18 6 | 50 48 52 49 53 44 48
R24E | 1794 14 18 20 26 17 20 8 | 97 96 95 100 102 95 96
XR25E |15217 16 10 --- --- 17 --- 10 | 37 33 --- --- 35 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2013 18 23 19 23 21 28 |T 58 56 60 58 57 54 54
WRMS | 2013 17 18 15 16 15 28 |NE 51 49 47 48 46 42 45
MEDI | 1331 15 18 13 21 14 22 |MD 54 50 57 53 53 44 48
Table 3.2305.4 GPS week: 2305 Day: 4 MJD: 60383
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1072 31 34 43 30 14 27 13 | 95 76 72 88 82 94 83
R02 | 550 12 17 22 16 11 19 7 | 35 38 34 38 21 24 28
R03 | 1767 7 12 20 29 13 16 7 | 42 45 37 45 44 37 40
R04 | 532 8 19 9 18 10 14 6 | 54 45 52 48 52 54 50
R05M | 715 12 15 8 20 9 29 7 | 41 40 35 33 33 40 35
R07 | 894 9 19 14 14 17 20 7 | 53 46 51 52 62 54 52
R08 | 793 13 10 12 15 12 30 7 | 51 46 53 53 48 40 47
R09 | 890 20 31 16 16 14 27 9 | 26 42 32 22 32 27 24
R11 | 1849 14 21 17 16 13 23 7 | 25 25 41 36 41 32 31
R12M | 1362 11 21 17 13 12 21 7 | 100 114 90 101 106 106 102
R13M | 1086 22 29 25 45 21 38 13 | 79 58 77 66 76 37 68
R14 | 724 8 10 9 8 15 17 5 | 78 81 76 82 90 73 80
R15 | 957 21 13 10 10 14 26 7 | 83 80 86 87 81 75 81
R16 | 940 23 20 17 19 17 20 8 | 80 67 72 71 66 64 69
XR17E | 1799 13 15 19 18 12 --- 7 | 41 39 48 46 39 --- 39
R18E | 1687 15 18 19 28 14 26 8 | 25 29 30 34 30 39 26
R19E | 850 23 46 32 41 29 71 18 | 51 63 57 62 53 52 48
R20E | 2477 44 65 93 57 37 74 27 | 67 93 113 101 70 75 71
R21E | 752 14 16 15 22 14 17 7 | 37 41 35 50 44 40 39
R22E | 3665 14 12 12 20 17 11 6 | 47 48 50 52 46 52 47
R24E | 2995 17 25 15 18 16 22 8 | 65 49 55 64 62 55 57
XR25E |14815 19 15 --- --- 14 --- 11 | 16 27 --- --- 25 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 1566 19 26 28 26 17 32 |T 54 54 56 58 54 53 51
WRMS | 1566 15 18 21 18 15 32 |NE 52 51 53 53 53 48 50
MEDI | 957 14 18 17 18 14 22 |MD 51 46 52 52 48 52 47
Table 3.2305.5 GPS week: 2305 Day: 5 MJD: 60384
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1282 26 19 17 28 16 17 9 | 103 101 102 99 99 103 101
R02 | 928 12 6 9 7 15 20 5 | 34 30 29 29 19 41 28
R03 | 873 10 15 13 15 9 17 6 | 39 52 40 53 45 39 43
R04 | 947 11 17 21 12 15 11 6 | 48 70 66 51 45 59 55
R05M | 630 11 26 19 19 22 11 8 | 36 55 53 39 27 40 39
R07 | 820 8 19 8 16 14 16 6 | 42 44 46 44 46 48 43
R08 | 1300 9 9 16 10 17 23 6 | 43 46 41 37 49 42 41
R09 | 1040 19 18 17 13 14 15 7 | 27 37 39 30 26 33 29
R11 | 1629 18 15 18 14 18 17 7 | 21 21 24 26 27 22 19
R12M | 1147 13 22 19 28 11 17 8 | 117 125 128 121 118 119 120
XR13M | 1287 22 47 21 31 16 --- 14 | 77 45 73 69 74 --- 68
R14 | 615 15 19 11 15 11 18 6 | 61 76 70 63 63 60 65
R15 | 700 17 13 11 13 10 24 6 | 77 85 77 81 76 68 77
R16 | 1456 15 24 14 25 14 17 8 | 74 62 80 86 70 69 72
XR17E | 2078 16 12 27 44 18 --- 12 | 42 36 43 58 41 --- 37
R18E | 1271 12 15 15 17 15 18 6 | 27 25 26 33 29 27 23
R19E | 762 28 34 49 49 29 76 20 | 69 78 89 65 81 79 71
R20E | 3415 40 64 84 41 39 97 28 | 129 143 152 136 135 130 128
R21E | 1252 19 13 14 32 16 15 8 | 51 48 56 53 53 50 50
R22E | 3186 12 9 13 21 25 13 7 | 42 45 48 52 47 42 44
R24E | 4163 16 18 12 24 34 20 10 | 85 93 89 87 74 93 84
XR25E |11462 15 10 --- --- 14 --- 9 | 18 26 --- --- 23 --- 20
XR26 | ---- 4 --- --- --- --- --- 0 | 17 --- --- --- --- --- 17
------+-----------------------------------------+-------------------------------------
RMS | 1745 18 23 26 23 20 33 |T 55 61 65 62 57 61 55
WRMS | 1745 15 16 15 17 18 33 |NE 43 52 51 50 46 48 44
MEDI | 1252 15 17 16 19 15 17 |MD 43 48 56 53 47 50 44
Table 3.2305.6 GPS week: 2305 Day: 6 MJD: 60385
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 971 25 32 21 36 16 19 11 | 109 89 99 109 101 89 98
R02 | 877 7 10 14 7 10 13 4 | 45 43 49 43 44 34 42
R03 | 2343 5 19 16 18 15 11 6 | 58 53 64 70 66 58 60
R04 | 1236 7 11 11 10 13 11 4 | 71 70 73 67 65 64 68
R05M | 909 16 15 15 17 18 9 7 | 53 56 44 42 47 47 47
R07 | 672 7 17 11 19 12 10 5 | 62 69 65 61 66 61 63
R08 | 1961 13 15 13 9 14 19 6 | 57 63 53 58 52 49 54
R09 | 1401 17 17 13 19 12 20 7 | 32 48 42 33 38 37 35
R11 | 1518 11 13 7 15 23 14 6 | 29 31 31 33 46 21 29
R12M | 1740 10 24 12 25 9 23 8 | 177 180 179 169 176 172 176
XR13M | 1269 21 50 39 32 23 --- 17 | 99 60 115 88 104 --- 92
R14 | 650 7 18 13 10 27 22 7 | 82 96 87 80 82 73 82
R15 | 1432 13 16 10 11 22 21 7 | 103 109 100 101 91 87 98
R16 | 1420 19 21 17 16 16 11 7 | 98 98 103 94 94 91 96
XR17E | 1277 12 20 11 52 35 --- 13 | 48 49 47 41 59 --- 45
R18E | 933 16 12 15 63 67 20 15 | 29 26 22 47 65 29 25
R19E | 1761 28 36 49 37 32 68 19 | 66 59 91 78 66 71 65
R20E | 2450 38 60 70 29 45 99 27 | 139 169 170 150 163 143 151
R21E | 995 20 12 32 91 19 19 16 | 108 112 106 151 117 111 112
R22E | 3698 12 12 10 23 13 12 6 | 72 76 75 76 73 74 73
R24E | 2850 15 18 25 70 43 21 14 | 89 89 86 118 110 93 92
XR25E |13595 13 15 --- --- 12 --- 9 | 35 38 --- --- 34 --- 35
XR26 |24578 4 --- --- --- --- --- 0 | 16 --- --- --- --- --- 16
------+-----------------------------------------+-------------------------------------
RMS | 1753 17 23 25 35 27 32 |T 72 76 81 81 79 73 71
WRMS | 1753 12 16 15 18 27 32 |NE 59 68 66 64 64 57 58
MEDI | 1420 13 17 14 19 16 19 |MD 66 63 75 76 66 71 65
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