[IGSREPORT-30053] Wk 2327 IGLOS Final Orbits
acc
acc at igs.org
Sun Sep 1 23:25:09 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2327 (Aug 11, 2024 - Aug 17, 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 2.2327.
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:
igl2327[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2327 in the SP3 format.
igl23277.sum Combination Report for GPS Week 2327.
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 | 6.6 ns
1 | 3.4 ns
2 | 5.2 ns
3 | 7.8 ns
4 | 9.1 ns
5 | 8.8 ns
6 | 8.6 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 | IAC | R18
1 | IAC | R18
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 1.2327, 1a.2327).
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 2.2327.0-6)
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 3.2327.0-6).
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 2327 summary. (Aug 11, 2024 - Aug 17, 2024)
Table 1.2327.a GPS week : 2327 MJD: 60533.0-60539.0
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 2 -14 -26 57 .10 16 12 | -236 -850 3082 10345
| 0 1 1 21 16 23 .02 | 633 1800
esa n/a| -1 -1 3 -21 26 -1 -.14 30 21 | 6448 -521 3069 7909
| 0 1 1 15 6 20 .06 | 5363 1794
gfz n/a| 0 0 -2 36 15 -25 -.02 27 14 | 0 -997 3098 8107
| 1 1 1 21 15 27 .06 | 0 1954
grg n/a| 2 0 3 -5 -2 -16 .44 24 17 | 6349 -884 3108 9652
| 1 1 2 20 10 42 .04 | 1970 1910
iac n/a| 0 0 -8 9 5 -44 -.19 97 28 | 7939 -400 3060 9917
| 1 0 1 25 25 27 .05 | 1666 858
jgx n/a| 0 0 0 -7 -4 -8 -.23 29 29 | 3602 -986 3100 8246
| 1 1 0 19 25 35 .05 | 764 1951
Table 1.2327.b GPS week : 2327 MJD: 60533.0-60539.0
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 | 18 18 18 15 18 16 15 |
R02 | 10 8 7 7 7 9 7 |
R03 | 6 7 8 7 7 8 7 |
R04 | 7 8 7 7 7 6 8 |
R05 | 8 7 8 8 8 7 7 |
R07 | 7 7 7 7 9 8 7 |
R08 | 8 9 7 7 7 9 9 |
R09 | 7 7 6 7 6 6 5 |
R11 | 6 8 7 8 7 7 7 |
R12 | 7 6 7 7 7 6 6 |
R14 | 5 5 6 5 5 5 6 |
R15 | 7 6 7 7 6 7 6 |
R16 | 8 8 7 7 8 9 8 |
R17 | 8 8 7 7 6 6 6 |
R18 | 7 8 7 6 7 7 7 |
R19 | 16 19 18 18 22 22 15 |
R20 | 24 28 32 33 32 25 30 |
R21 | 7 8 6 8 7 8 8 |
R22 | 7 6 6 7 6 7 6 |
R24 | 9 9 10 8 8 8 8 |
R25 | 8 10 11 10 11 9 11 |
R26 | 28 30 35 32 28 24 26 |
Table 1.2327.c GPS week : 2327 MJD: 60533.0-60539.0
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 2327 0 | 14 -3 86 -32 896 -828 81.8 1621 1621 | 6614 0
brd 2327 1 | -84 -56 103 -1518 -707 2247 83.0 1635 1635 | 3431 0
brd 2327 2 | 93 -50 138 597 1113 -1867 81.3 1466 1466 | 5249 0
brd 2327 3 | 50 23 32 -88 1442 -578 83.3 4519 4519 | 7750 0
brd 2327 4 | -55 7 2 -4 -516 2023 82.3 1827 1827 | 9049 0
brd 2327 5 | -48 17 -14 10 1980 2011 80.8 1846 1846 | 8773 0
brd 2327 6 | 0 32 -38 -1085 1072 5058 82.4 1926 1926 | 8589 0
-------------+------------------------------------------------------------+----------------
brd 2327 mean| -4 -4 44 -302 754 1152 82.1 2120 2120 | 7065 0
brd 2327 sdev| 63 35 66 730 998 2379 .9 1069 1069 | 2095 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 2.2327.0 GPS week: 2327 Day: 0 MJD: 60533
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 -20 -30 74 .12 13 11 | -331 2460 3016 10014
esa n/a| 0 0 4 -12 23 -1 -.22 29 23 | 5360 2779 3011 7217
gfz n/a| 4 0 0 81 -4 -73 -.06 31 16 | 0 2736 3074 7558
grg n/a| 0 0 2 26 10 -11 .45 21 17 | 3960 2680 3091 9527
iac n/a| 0 1 -9 -13 -9 -47 -.24 41 19 | 7291 511 2999 9596
jgx n/a| 1 -2 -1 -27 3 -41 -.29 26 26 | 3650 2719 3052 7765
Table 2.2327.1 GPS week: 2327 Day: 1 MJD: 60534
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 2 13 0 65 .13 15 13 | 517 -3265 3072 9521
esa n/a| -1 -2 4 -34 19 -15 -.15 35 23 | 10047 -2862 3063 8771
gfz n/a| 0 1 -4 37 12 -31 .02 26 15 | 0 -3744 3068 8983
grg n/a| 3 -1 0 -33 -2 24 .37 24 17 | 5083 -3769 3064 8275
iac n/a| -2 0 -6 -32 21 -33 -.22 529 84 | 5729 -1846 3070 9561
jgx n/a| 0 1 0 -24 -35 -40 -.19 31 34 | 3480 -3773 3084 9056
Table 2.2327.2 GPS week: 2327 Day: 2 MJD: 60535
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 6 -10 80 .08 17 12 | -1086 -1608 2830 10060
esa n/a| -1 0 5 -38 17 31 -.04 38 23 | 7363 -260 2832 7138
gfz n/a| 0 0 -1 13 35 12 .01 23 13 | 0 -1610 2847 7613
grg n/a| 1 0 5 -10 -22 -47 .42 22 16 | 4087 -1266 2838 9853
iac n/a| 0 0 -8 31 -21 -56 -.20 19 17 | 5879 -3 2805 9595
jgx n/a| 0 1 -2 5 10 -28 -.26 34 34 | 2752 -1433 2886 7740
Table 2.2327.3 GPS week: 2327 Day: 3 MJD: 60536
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 0 -31 -38 60 .09 15 12 | -383 -1377 3038 11458
esa n/a| -1 0 3 -25 33 -20 -.12 30 19 | 12480 -1549 3010 8518
gfz n/a| 1 -2 0 32 38 -30 -.08 28 13 | 0 -1352 3018 8645
grg n/a| 3 1 7 13 -1 -23 .42 23 17 | 6578 -1234 3036 11048
iac n/a| -2 1 -9 -3 9 -31 -.22 22 16 | 8407 -1102 3003 10942
jgx n/a| 1 1 0 21 -8 -29 -.28 32 32 | 4269 -1410 3009 8817
Table 2.2327.4 GPS week: 2327 Day: 4 MJD: 60537
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 2 -24 -22 22 .06 15 11 | 618 -858 3049 10385
esa n/a| -1 -2 4 -23 24 6 -.11 26 20 | 4948 -880 3026 7325
gfz n/a| 0 0 -2 42 9 -10 .08 29 13 | 0 -1549 3090 7268
grg n/a| 4 1 2 -5 4 -35 .48 30 21 | 8121 -1229 3103 9502
iac n/a| 0 0 -11 21 -17 -45 -.11 25 20 | 9369 -282 3028 9700
jgx n/a| 0 1 -1 -9 27 26 -.24 31 31 | 4926 -1554 3082 7330
Table 2.2327.5 GPS week: 2327 Day: 5 MJD: 60538
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 4 -43 -41 70 .08 16 13 | -828 280 3114 10149
esa n/a| 0 -2 4 6 33 -25 -.15 25 18 | 9079 482 3102 8244
gfz n/a| -1 0 -3 22 8 -37 -.03 28 16 | 0 -232 3159 8350
grg n/a| 0 1 2 -9 -10 50 .46 23 19 | 8305 -230 3157 9516
iac n/a| 0 1 -9 27 52 -95 -.16 24 19 | 9081 498 3097 9835
jgx n/a| 2 0 0 6 -40 8 -.19 26 26 | 3102 -214 3157 8499
Table 2.2327.6 GPS week: 2327 Day: 6 MJD: 60539
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 -3 -44 27 .10 17 14 | -160 -1584 3455 10830
esa n/a| 0 -3 1 -20 29 14 -.20 30 21 | -4137 -1357 3440 8154
gfz n/a| 0 0 -1 27 6 -9 -.09 23 12 | 0 -1233 3434 8338
grg n/a| 1 0 4 -20 5 -72 .46 26 14 | 8313 -1142 3473 9846
iac n/a| -1 0 -8 31 1 -3 -.16 22 19 | 9823 -578 3419 10193
jgx n/a| 1 0 0 -27 10 46 -.17 23 23 | 3038 -1242 3436 8517
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 3.2327.0 GPS week: 2327 Day: 0 MJD: 60533
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 712 20 79 31 21 38 43 17 | 132 56 141 133 146 98 120
R02 | 768 10 21 14 16 34 29 9 | 90 76 95 82 108 69 87
R03 | 1866 8 15 15 11 13 21 6 | 94 78 97 94 91 72 89
R04 | 606 10 17 15 15 17 16 6 | 86 82 75 90 86 71 82
R05 | 837 11 24 22 11 21 21 8 | 91 76 100 89 103 78 90
R07 | 789 14 13 15 16 11 25 7 | 90 69 79 88 83 62 80
R08 | 577 7 24 21 22 19 21 8 | 87 73 104 94 102 71 88
R09 | 2340 14 18 16 15 22 11 7 | 57 57 56 56 54 54 55
R11 | 1385 11 12 19 14 12 14 6 | 45 44 33 44 44 42 42
R12 | 720 7 16 14 15 21 24 7 | 42 39 42 43 50 31 39
R14 | 1497 8 13 13 14 7 16 5 | 132 141 140 140 134 135 136
R15 | 1105 10 22 9 19 17 9 6 | 55 48 52 60 45 50 51
R16 | 1452 12 20 21 20 18 13 7 | 55 50 52 42 52 48 48
R17E | 815 8 22 18 28 15 14 8 | 133 125 129 146 134 132 132
R18E | 1753 5 20 21 9 161 11 6 | 49 44 47 55 700 47 47
R19E | 2594 19 42 66 29 29 37 16 | 64 87 81 56 66 69 61
R20E | 3557 28 51 97 49 29 70 24 | 77 72 128 78 69 60 66
R21E | 1336 10 18 16 21 19 12 7 | 111 108 114 121 106 113 111
R22E | 1599 12 9 20 15 21 19 7 | 28 34 36 42 31 34 31
R24E | 2238 12 26 17 27 12 19 8 | 114 104 110 129 116 115 114
XR25E |11525 9 14 --- --- 12 --- 8 | 20 29 --- --- 24 --- 22
XR26 | 9969 21 --- --- 34 63 --- 27 | 61 --- --- 48 76 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 1621 13 29 31 21 41 26 |T 77 71 85 82 110 72 74
WRMS | 1621 11 23 16 17 19 26 |NE 79 68 82 78 83 67 76
MEDI | 1385 10 20 17 16 19 19 |MD 77 72 81 82 83 69 66
Table 3.2327.1 GPS week: 2327 Day: 1 MJD: 60534
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1122 21 92 29 26 21 50 18 | 101 41 105 106 97 68 89
R02 | 710 8 18 15 19 20 26 8 | 62 49 65 53 69 48 58
R03 | 1119 9 25 14 12 10 19 6 | 62 47 65 68 54 56 58
R04 | 794 9 18 16 18 17 26 7 | 60 60 59 74 63 49 59
R05 | 1024 15 19 16 15 8 18 6 | 74 57 68 61 65 65 65
R07 | 1856 8 21 12 17 16 20 7 | 61 52 63 50 66 51 57
R08 | 885 11 16 26 24 18 27 9 | 61 55 83 59 75 53 64
R09 | 2574 17 19 20 14 8 11 6 | 49 54 59 40 54 47 50
R11 | 1645 19 22 16 14 19 21 8 | 33 36 43 31 39 34 34
R12 | 764 7 12 14 18 11 20 6 | 26 36 25 36 30 23 27
R14 | 2193 13 8 15 7 8 12 5 | 137 142 140 135 133 135 136
R15 | 947 12 18 9 8 12 15 5 | 37 30 26 31 33 34 30
R16 | 837 14 18 16 14 16 27 7 | 36 30 31 28 27 45 29
R17E | 1045 9 25 13 29 15 20 8 | 92 92 94 100 90 81 90
R18E | 1780 12 20 13 16 2364 20 8 | 29 27 28 34 9999 26 25
R19E | 2739 25 54 53 27 34 57 18 | 61 84 89 67 62 85 62
R20E | 3461 36 81 73 62 51 87 28 | 53 112 88 47 36 78 50
R21E | 731 11 22 16 25 16 17 8 | 73 77 82 84 76 75 76
R22E | 1385 13 10 13 15 15 14 6 | 22 29 29 30 22 31 24
R24E | 1412 8 26 24 33 10 12 8 | 66 65 62 77 67 59 64
XR25E |10640 12 20 --- --- 12 --- 10 | 22 29 --- --- 22 --- 20
XR26 | 8936 35 --- --- 26 57 --- 30 | 40 --- --- 26 46 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1634 15 35 26 24 529 31 |T 57 57 65 58 58 57 54
WRMS | 1634 13 23 15 17 84 34 |NE 59 53 64 57 60 54 56
MEDI | 1122 12 20 16 18 16 20 |MD 60 52 63 53 62 51 57
Table 3.2327.2 GPS week: 2327 Day: 2 MJD: 60535
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1778 21 95 26 24 23 34 17 | 117 50 115 119 112 80 103
R02 | 1472 8 15 10 18 19 25 7 | 69 62 73 72 82 59 70
R03 | 1051 14 21 12 9 17 29 7 | 79 66 68 73 83 57 72
R04 | 924 9 19 12 19 15 22 7 | 69 62 76 81 83 58 71
R05 | 1160 10 20 20 18 14 29 8 | 76 62 84 77 81 60 74
R07 | 1558 10 22 17 10 11 19 6 | 76 56 85 70 65 65 70
R08 | 929 11 11 12 25 17 16 7 | 72 65 63 54 73 60 64
R09 | 1926 14 22 13 11 12 13 6 | 32 33 32 39 34 28 30
R11 | 997 11 14 16 15 15 19 6 | 21 24 25 28 17 27 19
R12 | 716 12 16 15 22 12 16 7 | 37 45 31 51 38 44 38
R14 | 2614 4 11 18 12 12 16 5 | 89 91 89 92 87 89 89
R15 | 992 7 16 18 11 15 19 6 | 40 44 57 48 51 40 45
R16 | 633 16 20 9 19 10 8 6 | 42 44 37 31 41 40 37
R17E | 869 11 19 11 22 17 18 7 | 64 68 64 62 58 62 61
R18E | 1095 12 18 16 11 15 17 6 | 30 35 32 35 702 30 28
R19E | 1620 33 48 45 28 26 55 17 | 40 53 44 53 34 62 35
R20E | 2411 47 109 66 57 53 115 32 | 50 134 78 56 38 87 49
R21E | 783 8 23 12 16 9 11 5 | 53 59 48 45 48 45 48
R22E | 1922 13 10 13 15 14 13 6 | 29 29 35 35 30 29 29
R24E | 1712 11 28 17 34 15 21 9 | 57 69 60 65 58 51 56
XR25E |14528 15 13 --- --- 16 --- 10 | 27 16 --- --- 13 --- 16
XR26 | 9360 42 --- --- 31 67 --- 35 | 34 --- --- 50 87 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1466 17 38 23 22 19 34 |T 54 55 59 58 87 53 52
WRMS | 1466 12 23 13 16 17 34 |NE 60 54 64 63 66 54 59
MEDI | 1160 11 19 15 18 15 19 |MD 50 56 60 54 58 57 49
Table 3.2327.3 GPS week: 2327 Day: 3 MJD: 60536
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 797 15 68 27 16 30 25 14 | 120 67 126 116 128 95 110
R02 | 1048 7 11 19 17 20 22 7 | 78 75 85 75 91 64 78
R03 | 2220 12 14 7 17 14 23 6 | 92 74 85 83 86 71 83
R04 | 568 11 15 11 12 20 24 7 | 85 78 78 75 93 63 79
R05 | 988 11 13 12 17 29 22 8 | 85 80 93 78 108 72 86
R07 | 969 14 15 12 15 7 23 6 | 90 76 77 81 81 64 79
R08 | 781 8 14 24 12 9 18 6 | 76 79 97 79 82 72 80
R09 | 1008 14 15 13 12 19 22 7 | 30 31 31 35 32 43 31
R11 | 1020 14 17 14 18 7 28 7 | 32 44 43 41 30 38 34
R12 | 812 12 18 14 20 18 7 7 | 39 35 35 51 43 43 38
R14 | 2145 9 12 12 13 14 7 5 | 64 68 61 72 70 65 65
R15 |19248 11 12 20 14 15 16 6 | 44 52 62 51 39 49 47
R16 | 688 11 17 22 18 10 17 7 | 46 56 60 45 47 43 47
R17E | 858 8 16 16 23 14 15 6 | 65 68 64 65 60 70 63
R18E | 976 13 17 10 16 10 15 6 | 32 35 40 40 385 41 35
R19E | 2004 20 53 57 29 39 38 17 | 49 54 70 68 60 67 50
R20E | 3051 44 80 88 63 57 113 32 | 42 92 91 48 47 54 41
R21E | 743 12 18 16 26 13 15 7 | 53 62 60 66 56 48 55
R22E | 1829 12 17 12 16 16 11 6 | 39 43 40 37 42 36 37
R24E | 1308 12 18 11 31 13 16 8 | 40 46 43 43 37 38 37
XR25E |13000 11 18 --- --- 12 --- 9 | 28 43 --- --- 26 --- 30
XR26 |10576 30 --- --- 28 70 --- 31 | 44 --- --- 43 79 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 4519 15 30 28 23 22 32 |T 57 59 67 61 78 56 57
WRMS | 4519 12 19 13 17 16 32 |NE 66 62 71 66 72 60 64
MEDI | 1008 12 17 14 17 14 18 |MD 46 62 62 65 60 54 50
Table 3.2327.4 GPS week: 2327 Day: 4 MJD: 60537
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 690 30 71 26 32 25 30 17 | 107 50 96 108 102 74 88
R02 | 642 8 8 17 23 23 17 7 | 67 66 76 57 82 58 67
R03 | 3051 10 12 15 18 22 19 7 | 74 64 65 71 84 57 68
R04 | 812 11 12 15 25 19 14 7 | 72 72 69 60 73 61 68
R05 | 646 12 18 16 20 22 12 7 | 71 74 82 79 93 72 77
R07 | 728 12 22 22 15 14 28 8 | 77 60 89 82 73 55 72
R08 | 790 8 12 18 16 20 17 6 | 70 65 87 85 83 64 73
R09 | 883 11 12 8 18 13 15 5 | 36 35 38 38 41 33 35
R11 | 1775 14 7 14 16 18 22 7 | 28 31 32 28 29 39 27
R12 | 1494 10 10 17 26 10 12 6 | 35 42 50 51 37 38 40
R14 | 1805 8 11 14 15 17 5 5 | 79 85 78 83 86 82 81
R15 | 1410 8 7 12 19 17 22 6 | 44 46 49 41 52 28 42
R16 | 1091 11 16 18 26 25 19 8 | 41 56 58 31 60 33 45
R17E | 1144 9 13 14 14 14 10 5 | 67 61 71 68 61 58 64
R18E | 1706 10 14 13 25 15 16 6 | 31 32 35 36 152 29 29
R19E | 1766 27 42 73 25 51 66 21 | 49 66 93 61 48 75 54
R20E | 4952 32 65 86 91 67 95 31 | 46 62 84 66 59 51 42
R21E | 1018 11 18 14 21 15 11 6 | 57 56 56 54 50 54 53
R22E | 2784 12 13 11 15 14 13 5 | 23 27 25 34 23 23 22
R24E | 1037 14 12 16 36 14 11 8 | 69 69 61 73 68 61 65
XR25E |13095 13 16 --- --- 15 --- 10 | 25 22 --- --- 15 --- 18
XR26 |17460 22 --- --- 32 61 --- 27 | 35 --- --- 29 49 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 1827 15 26 29 30 25 31 |T 54 54 64 58 64 52 52
WRMS | 1827 11 20 13 21 20 31 |NE 59 57 66 60 67 53 58
MEDI | 1144 11 13 15 21 17 16 |MD 49 60 65 60 60 55 53
Table 3.2327.5 GPS week: 2327 Day: 5 MJD: 60538
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 562 38 60 20 18 13 35 15 | 95 54 73 77 74 56 71
R02 | 753 8 15 25 20 19 26 8 | 65 63 82 83 69 56 67
R03 | 1743 9 12 17 19 20 24 7 | 69 67 80 85 80 64 72
R04 | 775 11 11 13 16 8 12 5 | 64 65 59 58 58 62 60
R05 | 778 11 15 12 21 17 16 6 | 63 62 60 80 72 57 64
R07 | 735 11 25 12 19 16 20 7 | 69 54 68 77 74 55 65
R08 | 862 17 17 20 17 27 24 9 | 60 64 79 82 83 59 69
R09 | 685 9 12 14 16 6 15 5 | 48 57 50 63 48 52 51
R11 | 1954 17 16 12 12 7 20 6 | 43 47 38 55 45 38 43
R12 | 1598 7 13 14 14 15 19 6 | 23 23 28 31 25 25 22
R14 | 1850 8 8 16 13 15 10 5 | 55 57 64 56 51 57 55
R15 | 1213 10 13 13 23 21 13 7 | 38 43 31 50 39 39 38
R16 | 1122 12 19 14 15 35 11 8 | 40 48 36 39 62 39 41
R17E | 1218 11 12 13 20 10 12 6 | 52 49 47 50 49 41 47
R18E | 1038 7 17 13 22 18 11 6 | 25 27 20 24 243 20 20
R19E | 2186 27 48 65 39 56 52 21 | 65 73 54 70 76 64 59
R20E | 4941 32 54 80 55 51 67 25 | 36 72 101 43 52 35 42
R21E | 1172 9 21 19 18 17 15 7 | 43 43 45 53 43 41 42
R22E | 3771 17 14 12 20 16 12 7 | 18 25 19 36 25 20 20
R24E | 1170 12 21 21 27 11 13 8 | 49 50 46 57 51 42 47
XR25E |17891 11 14 --- --- 11 --- 8 | 27 35 --- --- 24 --- 28
XR26 |14716 18 --- --- 31 51 --- 24 | 51 --- --- 40 51 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 1845 16 25 28 23 24 26 |T 49 51 54 57 63 46 48
WRMS | 1845 13 18 16 19 19 26 |NE 55 54 57 62 59 50 54
MEDI | 1172 11 15 14 19 16 15 |MD 49 54 50 56 51 42 47
Table 3.2327.6 GPS week: 2327 Day: 6 MJD: 60539
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 554 24 74 22 18 23 29 15 | 134 56 132 127 133 96 116
R02 | 741 8 12 12 11 18 23 6 | 92 83 94 83 101 71 87
R03 | 1556 17 13 12 11 10 24 7 | 94 75 83 88 90 71 83
R04 | 489 9 15 17 11 18 29 8 | 85 88 85 81 94 70 83
R05 | 712 17 15 16 16 17 14 7 | 89 90 97 86 93 82 88
R07 | 1882 12 18 19 10 17 18 7 | 97 77 91 89 101 72 88
R08 | 1210 13 26 14 11 33 16 9 | 86 74 98 93 114 80 90
R09 | 1007 11 13 11 11 10 11 5 | 52 58 52 58 47 54 52
R11 | 1082 20 13 12 10 17 16 7 | 41 48 45 49 41 42 42
R12 | 1203 7 24 9 11 16 13 6 | 31 36 32 40 34 34 31
R14 | 1790 10 9 15 12 13 15 5 | 77 80 81 79 78 79 78
R15 | 805 8 15 11 14 20 12 6 | 43 40 39 51 42 41 42
R16 | 899 16 29 11 14 24 14 8 | 60 58 51 56 74 54 57
R17E | 1615 7 15 14 17 12 16 6 | 85 75 77 88 80 70 79
R18E | 1120 11 20 14 14 19 14 6 | 28 29 20 29 262 15 22
R19E | 2144 29 46 37 34 31 31 15 | 74 80 78 72 72 77 68
R20E | 5533 43 67 76 92 58 63 30 | 57 128 141 70 75 85 75
R21E | 921 13 20 21 23 12 14 7 | 56 59 56 61 58 58 56
R22E | 3538 15 15 10 15 12 14 6 | 16 20 21 22 16 19 15
R24E | 2103 15 23 13 25 16 16 8 | 79 72 74 87 81 74 77
XR25E |15841 15 16 --- --- 17 --- 11 | 33 30 --- --- 17 --- 25
XR26 |18747 19 --- --- 29 55 --- 25 | 41 --- --- 36 66 --- 44
------+-----------------------------------------+-------------------------------------
RMS | 1926 17 30 23 26 22 23 |T 65 64 72 68 80 62 63
WRMS | 1926 14 21 12 14 19 23 |NE 73 66 75 72 79 65 70
MEDI | 1203 13 16 14 14 17 16 |MD 60 72 77 72 75 70 68
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