[IGSREPORT-29514] Wk 2278 IGLOS Final Orbits
acc
acc at igs.org
Wed Sep 27 04:57:30 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2278 (Sep 03, 2023 - Sep 09, 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 2.2278.
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:
igl2278[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2278 in the SP3 format.
igl22787.sum Combination Report for GPS Week 2278.
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 | -1.0 ns
1 | -2.0 ns
2 | -4.9 ns
3 | 0.9 ns
4 | 0.5 ns
5 | 1.4 ns
6 | -0.2 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
2 | GFZ | R22
5 | COD | R19
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 1.2278, 1a.2278).
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 2.2278.0-6)
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 3.2278.0-6).
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 2278 summary. (Sep 03, 2023 - Sep 09, 2023)
Table 1.2278.a GPS week : 2278 MJD: 60190.0-60196.0
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 2 3 -12 27 .03 24 13 | 484050 4655 252359 292899
| 0 0 1 17 15 20 .04 | 769779 7954
esa n/a| -1 0 1 2 13 8 -.21 27 21 | 1749 1080 3151 8475
| 0 1 1 15 18 17 .03 | 4937 1618
gfz n/a| -1 1 0 26 10 18 -.09 25 15 | 0 348 3168 9189
| 0 1 1 11 11 11 .05 | 0 1576
grg n/a| 2 -1 -5 -34 3 -60 .23 24 16 | 464039 4940 254239 291919
| 0 1 1 16 17 25 .03 | 796669 8590
iac n/a| 0 1 -6 -1 35 -26 -1.98 41 38 | 451078 3234 252337 292733
| 2 4 3 43 29 101 1.57 | 770437 7477
jgx n/a| 0 1 3 20 20 -76 -.32 32 32 | 35519 203 3230 9316
| 1 1 1 20 16 46 .04 | 4512 1606
Table 1.2278.b GPS week : 2278 MJD: 60190.0-60196.0
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 | 22 20 20 19 19 19 24 |
R02 | 8 6 11 8 7 6 7 |
R03 | 11 7 9 8 6 6 7 |
R04 | 7 7 8 7 6 7 8 |
R05 | 6 9 8 7 8 7 7 |
R07 | 9 7 7 8 8 8 7 |
R08 | 10 12 6 9 13 8 9 |
R09 | 8 9 7 8 7 7 7 |
R11 | 6 9 8 7 8 6 8 |
R12 | 7 6 7 6 8 8 7 |
R13 | 17 17 17 18 19 17 21 |
R14 | 6 6 8 6 8 7 6 |
R15 | 9 7 7 9 10 11 8 |
R16 | 10 10 8 12 9 10 12 |
R17 | 10 7 10 9 8 7 10 |
R18 | 7 9 7 7 9 8 10 |
R19 | 21 30 24 24 20 24 32 |
R20 | 34 35 33 28 33 34 59 |
R21 | 9 6 7 13 11 7 9 |
R22 | 8 7 12 14 17 29 9 |
R24 | 9 11 9 15 9 9 11 |
R25 | 14 14 11 14 0 --- --- |
Table 1.2278.c GPS week : 2278 MJD: 60190.0-60196.0
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 2278 0 | -5 10 160 420 1105 2785 80.9 1448 1448 | -1029 0
brd 2278 1 | 28 102 92 122 1762 1489 79.2 1550 1550 | -1999 0
brd 2278 2 | -55 31 111 -1419 54 -905 82.0 1718 1718 | -4877 0
brd 2278 3 | -26 -33 26 -1654 822 23 81.5 1665 1665 | 866 0
brd 2278 4 | 63 -47 26 2329 -40 -215 80.2 1445 1445 | 479 0
brd 2278 5 | 28 -32 138 1465 -2918 -700 80.3 1623 1623 | 1368 0
brd 2278 6 | 33 18 108 1977 -1620 -2438 79.9 1888 1888 | -196 0
-------------+------------------------------------------------------------+----------------
brd 2278 mean| 9 7 94 463 -119 5 80.6 1619 1619 | -769 0
brd 2278 sdev| 40 51 51 1576 1635 1696 1.0 157 157 | 2144 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 2.2278.0 GPS week: 2278 Day: 0 MJD: 60190
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 6 -38 21 -.03 15 12 | 32105 -1416 3102 10920
esa n/a| 0 0 0 -22 21 7 -.26 29 21 | 9235 -1209 3102 10058
gfz n/a| -1 0 3 27 26 4 -.13 25 19 | 0 -1485 3155 10019
grg n/a| 2 0 -6 -13 24 -31 .27 20 15 | -661 -1464 3145 9481
iac n/a| -4 3 -11 1 26 -45 -3.20 47 46 | 2427 -2904 3087 10513
jgx n/a| 0 0 4 15 21 -138 -.34 33 33 | 32835 -1880 3177 10116
Table 2.2278.1 GPS week: 2278 Day: 1 MJD: 60191
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 4 -2 -19 16 .05 17 12 | 30336 -635 3395 14213
esa n/a| -2 0 2 -9 2 7 -.21 30 22 | -1905 252 3253 12551
gfz n/a| 0 1 -2 27 21 12 -.08 23 13 | 0 -344 3311 12987
grg n/a| 3 -2 -6 -30 11 -52 .27 26 15 | -3578 -556 3314 12486
iac n/a| 2 8 -8 -25 68 142 -3.02 50 45 | -1485 -576 3303 13631
jgx n/a| -1 1 5 35 21 -100 -.32 31 31 | 30253 -473 3428 13293
Table 2.2278.2 GPS week: 2278 Day: 2 MJD: 60192
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 32 -12 9 .02 14 10 | 26426 -108 2776 9604
esa n/a| 0 1 4 -3 46 30 -.16 30 30 | -4444 238 2778 6744
gfz n/a| -1 3 -1 13 12 23 -.12 25 16 | 0 -743 2807 8200
grg n/a| 2 -2 -4 -34 -13 -41 .19 23 17 | -7129 -674 2791 7951
iac n/a| 3 -4 -5 82 21 -135 -3.31 47 44 | -4906 218 2745 9301
jgx n/a| 0 0 5 23 50 -104 -.39 35 35 | 30930 -597 2856 8349
Table 2.2278.3 GPS week: 2278 Day: 3 MJD: 60193
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 -17 11 17 .09 18 13 | 1537644 14673 861836 999999
esa n/a| 0 3 1 15 23 -6 -.24 23 20 | 7437 2193 3199 8007
gfz n/a| 0 2 1 25 -8 37 -.08 25 16 | 0 1859 3223 8277
grg n/a| 4 -2 -5 -17 -24 -63 .24 23 16 | 1617180 17481 875015 999999
iac n/a| 0 2 -10 -37 -10 -106 -3.42 49 46 | 1506194 13832 861816 999999
jgx n/a| 0 0 4 -2 22 -85 -.36 36 36 | 35339 1255 3264 8381
Table 2.2278.4 GPS week: 2278 Day: 4 MJD: 60194
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 16 -2 27 .05 19 13 | 1680836 17430 889126 999999
esa n/a| -1 0 1 0 6 -1 -.17 23 19 | -195 2118 3466 7556
gfz n/a| -1 0 0 12 4 7 -.14 25 14 | 0 1157 3425 10177
grg n/a| 1 0 -7 -38 0 -46 .22 22 19 | 1643193 17156 889163 999999
iac n/a| 0 0 -7 -43 64 -90 -.25 30 27 | 1648353 14216 889144 999999
jgx n/a| -4 2 0 16 -1 -57 -.31 30 30 | 37376 1322 3540 10395
Table 2.2278.5 GPS week: 2278 Day: 5 MJD: 60195
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 31 .04 47 13 | 38790 3101 3275 8328
esa n/a| 0 0 1 13 -1 34 -.21 21 16 | 1914 3588 3259 7644
gfz n/a| 0 0 0 39 10 22 .00 26 13 | 0 2746 3266 7832
grg n/a| 3 0 -4 -62 20 -96 .25 29 17 | -608 3228 3276 7325
iac n/a| 2 -2 -6 20 17 -26 -.36 31 25 | 3234 372 3277 8393
jgx n/a| 0 2 3 -1 7 -58 -.27 27 27 | 39597 2730 3301 7820
Table 2.2278.6 GPS week: 2278 Day: 6 MJD: 60196
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 -14 -8 71 .02 37 16 | 42216 -455 3003 7236
esa n/a| -1 1 0 22 -6 -11 -.19 34 21 | 201 386 3005 6768
gfz n/a| -1 0 -1 43 3 24 -.10 26 14 | 0 -748 2992 6837
grg n/a| 1 0 -4 -44 8 -93 .20 26 14 | -121 -590 2971 6198
iac n/a| -2 3 0 -7 61 76 -.32 35 30 | 3734 -2516 2993 7299
jgx n/a| 0 3 1 55 22 6 -.28 34 32 | 42306 -936 3047 6864
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 3.2278.0 GPS week: 2278 Day: 0 MJD: 60190
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 746 25 70 21 29 63 42 21 | 120 60 114 120 157 92 105
R02 | 790 8 17 11 15 53 14 7 | 83 73 82 87 125 77 81
R03 | 1530 10 26 8 25 44 21 10 | 86 73 87 107 125 77 88
R04 | 1467 11 13 8 12 42 23 6 | 91 84 86 91 117 77 88
R05 | 722 9 8 9 10 42 17 5 | 77 74 73 77 108 66 75
R07 | 711 9 22 18 10 62 20 8 | 81 67 85 81 130 65 79
R08 | 1901 12 16 24 13 46 30 9 | 77 73 104 90 119 71 85
R09 | 957 9 19 17 11 57 13 8 | 63 70 60 66 63 68 63
R11 | 1190 10 10 13 10 55 15 6 | 43 50 54 46 52 52 47
R12 | 1905 12 15 13 11 49 26 7 | 57 63 67 59 101 52 60
R13 | 1165 22 35 27 31 51 40 16 | 72 47 67 67 104 47 64
R14 | 777 8 12 10 11 44 16 5 | 53 58 61 60 92 49 57
R15 | 809 8 27 10 16 42 21 9 | 73 57 76 82 107 70 72
R16 | 694 17 17 18 15 44 17 10 | 62 49 55 52 97 59 53
R17E | 1347 8 17 21 21 27 --- 9 | 53 47 49 65 56 --- 52
R18E | 2148 8 17 9 12 32 16 6 | 38 39 34 39 37 39 36
R19E | 1370 24 47 50 26 45 48 21 | 81 82 84 85 89 75 78
R20E | 2148 38 67 81 46 41 101 33 | 154 184 143 130 153 195 144
R21E | 1385 11 19 12 17 34 20 8 | 45 40 40 45 41 42 40
R22E | 2294 14 7 15 17 52 21 8 | 34 31 87 43 35 32 34
R24E | 2127 11 12 16 19 32 25 8 | 51 53 55 57 53 51 53
XR25E |13860 8 20 --- --- 58 --- 13 | 39 24 --- --- 28 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1447 15 29 25 20 47 33 |T 69 63 74 73 90 67 67
WRMS | 1447 12 21 19 15 46 33 |NE 74 64 76 77 106 65 72
MEDI | 1347 10 17 15 15 44 21 |MD 63 58 73 67 97 65 63
Table 3.2278.1 GPS week: 2278 Day: 1 MJD: 60191
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1068 24 68 22 15 68 43 20 | 94 54 99 89 128 84 85
R02 | 1110 4 12 12 11 61 22 5 | 66 58 71 64 108 57 65
R03 | 1886 7 14 9 15 46 17 6 | 62 62 64 75 96 64 64
R04 | 2087 10 15 7 10 49 30 6 | 71 66 69 74 97 62 70
R05 | 717 16 19 12 16 53 26 9 | 59 53 57 65 98 54 57
R07 | 773 10 17 12 8 58 28 7 | 58 55 59 62 97 53 58
R08 | 1352 16 11 32 13 46 26 11 | 60 66 87 66 101 65 68
R09 | 1178 10 24 8 16 59 18 8 | 62 84 64 61 60 75 66
R11 | 1379 12 10 18 16 51 15 8 | 44 52 55 51 38 50 48
R12 | 2077 7 11 12 10 43 17 5 | 49 52 46 50 80 51 48
R13 | 1465 18 37 27 39 55 56 17 | 67 60 82 66 110 68 68
R14 | 612 7 11 11 12 37 16 6 | 54 60 48 58 81 54 54
R15 | 469 9 16 8 14 48 17 7 | 67 62 66 67 107 64 65
R16 | 701 19 22 12 14 47 18 10 | 59 55 52 57 88 64 53
R17E | 1040 10 10 13 12 26 --- 6 | 35 36 32 35 28 --- 33
R18E | 2533 12 20 14 16 31 19 9 | 35 33 35 35 31 36 32
R19E | 2311 46 43 64 53 51 51 30 | 56 82 103 74 76 57 60
R20E | 2215 34 81 51 81 69 68 35 | 90 99 101 112 83 101 86
R21E | 1412 10 11 7 14 36 26 6 | 51 51 49 48 42 52 48
R22E | 1834 12 11 12 13 52 17 7 | 30 34 102 39 26 33 33
R24E | 1812 13 18 23 23 28 29 11 | 36 34 40 38 32 39 33
XR25E |11995 10 18 --- --- 52 --- 13 | 31 27 --- --- 29 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 1550 17 30 23 26 50 31 |T 56 56 65 61 74 59 55
WRMS | 1550 12 22 13 15 45 31 |NE 62 59 65 64 92 61 62
MEDI | 1379 10 16 12 14 49 22 |MD 58 55 64 62 81 57 57
Table 3.2278.2 GPS week: 2278 Day: 2 MJD: 60192
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 784 24 66 25 18 38 39 20 | 103 57 99 97 110 79 91
R02 | 625 7 22 30 16 67 24 11 | 74 68 100 74 129 68 77
R03 | 1180 13 21 16 11 44 24 8 | 78 63 68 74 105 65 71
R04 | 1659 7 16 15 19 40 30 8 | 76 71 82 86 104 66 78
R05 | 1291 7 20 9 18 48 17 8 | 71 68 71 81 108 64 71
R07 | 621 6 18 13 8 56 29 6 | 65 58 70 62 112 51 64
R08 | 1499 8 10 13 11 45 25 6 | 62 63 59 65 101 56 62
R09 | 980 9 11 14 13 55 19 6 | 71 72 67 75 79 74 70
R11 | 1674 10 17 17 8 57 19 7 | 54 58 55 52 69 60 54
R12 | 1941 5 11 10 21 37 20 7 | 55 52 56 60 92 56 55
R13 | 895 12 38 27 42 41 --- 17 | 72 65 67 86 100 --- 72
R14 | 640 10 8 23 10 36 19 8 | 54 59 73 55 92 54 58
R15 | 1094 5 11 15 17 32 24 7 | 65 69 67 66 93 59 65
R16 | 956 14 19 10 12 40 10 8 | 68 63 60 64 102 65 63
R17E | 847 9 20 20 21 33 --- 9 | 37 35 42 49 49 --- 37
R18E | 2282 9 16 12 10 37 26 6 | 36 37 42 37 40 42 36
R19E | 2839 30 50 50 39 51 83 23 | 59 49 62 52 56 41 42
R20E | 4465 30 75 69 59 78 79 32 | 84 112 98 81 72 78 80
R21E | 2024 8 12 17 13 38 16 7 | 56 55 58 49 57 57 54
XR22E | 7606 9 --- 444 15 68 --- 12 | 40 --- 384 50 36 --- 43
R24E | 831 8 17 20 15 39 21 8 | 41 45 44 43 47 44 40
XR25E |14629 7 16 --- --- 60 --- 11 | 38 29 --- --- 38 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1718 14 30 25 23 47 35 |T 61 59 82 64 81 59 60
WRMS | 1718 10 30 16 17 44 35 |NE 69 63 71 71 99 62 67
MEDI | 1180 9 17 17 15 41 24 |MD 62 59 67 64 92 59 62
Table 3.2278.3 GPS week: 2278 Day: 3 MJD: 60193
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 611 17 52 32 20 50 28 18 | 89 52 105 95 124 72 84
R02 | 1513 10 15 15 12 52 18 7 | 62 69 59 55 103 50 61
R03 | 1249 8 20 10 15 42 26 8 | 70 68 80 85 104 56 74
R04 | 1000 13 13 12 8 48 25 7 | 71 65 60 65 101 54 65
R05 | 1733 12 11 14 11 41 21 7 | 64 63 71 70 98 57 66
R07 | 655 10 18 15 10 51 20 7 | 71 64 79 71 104 57 70
R08 | 1403 16 12 18 16 43 24 9 | 58 58 76 78 105 54 66
R09 | 747 11 9 21 9 53 11 7 | 26 27 30 30 34 31 27
R11 | 1280 10 8 12 15 59 14 7 | 19 23 23 24 32 20 20
R12 | 1324 8 11 7 13 34 17 6 | 47 51 54 61 84 47 52
R13 | 722 26 37 26 31 36 60 17 | 76 51 48 66 88 54 59
R14 | 682 11 11 8 11 37 22 6 | 47 59 59 54 82 43 53
R15 | 1321 16 10 20 11 39 22 8 | 53 64 75 64 98 54 62
R16 | 1701 16 13 20 31 51 18 12 | 58 64 69 46 101 49 56
R17E | 1027 13 11 21 17 34 --- 9 | 32 34 29 35 35 --- 30
R18E | 1866 11 14 10 14 40 28 7 | 29 36 36 31 30 30 31
R19E | 2447 27 39 65 30 61 76 24 | 58 61 89 52 58 64 53
R20E | 3897 45 53 44 52 89 87 28 | 70 73 65 59 90 72 54
R21E | 2897 22 16 16 32 46 28 13 | 45 49 48 72 51 49 49
XR22E |17007 13 --- --- 14 54 --- 14 | 20 --- --- 31 25 --- 23
R24E | 1041 16 9 28 38 51 25 14 | 35 30 44 49 41 36 31
XR25 |11887 12 15 --- --- 58 --- 13 | 32 33 --- --- 34 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1664 18 23 25 23 49 36 |T 51 52 59 56 73 49 50
WRMS | 1664 13 20 16 16 46 36 |NE 57 55 63 61 89 49 58
MEDI | 1321 13 13 16 15 48 24 |MD 53 58 59 59 84 54 53
Table 3.2278.4 GPS week: 2278 Day: 4 MJD: 60194
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 550 28 54 12 22 38 47 19 | 89 58 81 89 101 63 76
R02 | 1623 11 10 14 10 17 20 6 | 57 58 49 58 63 47 55
R03 | 3017 7 9 15 10 23 15 6 | 61 63 54 60 70 56 58
R04 | 918 10 9 11 12 13 14 6 | 70 66 66 67 62 66 67
R05 | 1661 12 14 14 17 15 26 8 | 64 61 62 57 57 46 60
R07 | 1117 7 21 6 16 15 28 8 | 67 55 65 80 58 51 66
R08 | 916 15 25 32 13 12 18 13 | 62 57 95 77 68 60 70
R09 | 1317 10 9 16 9 25 15 6 | 55 58 56 56 45 59 55
R11 | 1203 15 10 10 18 20 13 8 | 30 39 37 39 37 38 34
R12 | 1012 9 11 14 17 17 13 7 | 47 55 52 47 45 42 49
R13 | 917 27 35 28 41 29 33 19 | 57 35 45 40 47 41 43
R14 | 721 11 13 19 8 26 9 7 | 41 42 32 37 47 38 37
R15 | 873 10 12 15 26 40 12 9 | 58 60 64 76 88 60 63
R16 | 952 12 15 21 14 31 21 9 | 55 61 75 54 74 49 60
R17E | 1692 10 13 15 15 10 --- 7 | 28 30 26 34 29 --- 27
R18E | 1260 10 15 20 15 22 18 8 | 31 29 30 33 42 31 28
R19E | 1575 31 29 46 25 61 61 19 | 50 56 72 40 41 45 44
R20E | 2336 57 48 69 53 60 74 33 | 80 74 69 56 76 54 50
R21E | 1063 9 13 24 25 20 22 10 | 61 68 69 64 63 62 63
XR22E | 3430 15 --- --- 17 33 --- 16 | 35 --- --- 36 36 --- 32
R24E | 1803 14 9 18 16 29 24 8 | 31 29 28 38 29 27 30
XR25 |13676 2 --- --- --- 26 --- 0 | 34 --- --- --- 44 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1444 19 23 25 22 30 30 |T 52 52 56 54 55 49 50
WRMS | 1444 13 19 14 19 27 30 |NE 58 54 59 59 61 51 56
MEDI | 1203 11 13 15 16 23 20 |MD 55 57 56 56 47 49 50
Table 3.2278.5 GPS week: 2278 Day: 5 MJD: 60195
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 797 29 48 22 17 32 47 18 | 88 61 84 77 79 55 75
R02 | 1100 5 9 12 12 19 21 5 | 61 61 70 60 63 51 62
R03 | 2681 9 12 7 11 10 27 5 | 62 55 58 61 52 41 58
R04 | 603 12 13 11 11 19 20 7 | 66 70 68 66 71 70 67
R05 | 2123 9 12 13 10 20 17 6 | 55 63 65 62 66 51 60
R07 | 797 8 16 7 19 34 10 7 | 61 52 52 68 77 57 57
R08 | 1052 11 14 18 12 25 16 8 | 54 55 67 64 67 62 58
R09 | 1365 10 10 13 15 14 17 7 | 39 54 49 46 45 42 45
R11 | 871 10 8 7 13 26 16 5 | 31 37 33 31 33 40 31
R12 | 869 9 16 9 18 17 8 7 | 44 43 45 56 44 51 45
R13 | 1584 23 26 20 49 40 56 17 | 43 33 39 46 50 32 36
R14 | 728 11 11 8 13 24 21 6 | 37 38 37 39 45 33 37
R15 | 707 15 15 14 32 27 8 11 | 56 56 64 80 67 60 61
R16 | 771 15 22 12 15 33 14 9 | 56 59 65 65 73 59 59
R17E | 1341 8 13 9 14 15 --- 6 | 18 24 21 27 24 --- 19
R18E | 1221 8 15 17 16 27 13 8 | 29 30 24 30 31 25 25
R19E | 2108 198 29 33 41 74 46 24 | 202 55 50 54 74 43 46
R20E | 1432 46 42 51 95 61 50 34 | 82 85 102 64 106 55 74
R21E | 951 7 13 14 11 16 20 7 | 38 49 45 46 39 38 43
R22E | 4215 39 24 85 26 26 --- 29 | 22 24 137 27 20 --- 33
R24E | 1913 12 12 16 21 14 17 8 | 27 29 27 39 29 28 27
------+-----------------------------------------+-------------------------------------
RMS | 1622 47 21 26 29 31 27 |T 55 49 57 52 55 47 48
WRMS | 1622 13 16 13 17 25 27 |NE 53 52 56 58 59 50 53
MEDI | 1100 11 14 13 15 25 17 |MD 54 54 52 56 52 51 46
Table 3.2278.6 GPS week: 2278 Day: 6 MJD: 60196
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 670 27 72 28 23 16 35 24 | 120 56 124 114 115 86 103
R02 | 758 8 10 12 13 25 18 6 | 79 75 83 78 80 69 78
R03 | 917 11 12 7 13 12 26 6 | 82 69 74 81 78 56 76
R04 | 645 17 8 14 15 28 32 8 | 87 81 77 78 89 70 79
R05 | 2039 15 9 13 8 17 14 7 | 74 83 89 81 80 71 81
R07 | 1163 12 14 8 12 17 10 7 | 83 70 79 83 89 69 78
R08 | 1276 10 23 10 17 14 14 9 | 74 68 92 89 88 81 80
R09 | 1285 10 10 15 11 17 13 7 | 48 58 53 51 51 53 51
R11 | 790 17 13 16 9 18 19 8 | 34 43 41 36 43 40 37
R12 | 1383 12 11 9 13 28 13 6 | 54 52 53 61 64 54 54
R13 | 994 34 30 28 48 17 67 21 | 71 48 53 60 59 46 56
R14 | 635 10 7 12 9 13 20 5 | 48 50 43 47 48 41 46
R15 | 819 9 19 9 16 19 17 8 | 69 59 69 78 80 64 68
R16 | 691 22 20 18 16 53 14 11 | 69 61 58 60 89 57 59
R17 | 1588 17 12 14 21 20 --- 9 | 38 35 35 36 40 --- 32
R18E | 1444 18 17 16 19 23 15 10 | 28 29 24 30 31 23 25
R19E | 2171 51 44 61 59 44 43 31 | 50 73 81 96 65 58 65
R20E | 3515 146 114 75 62 119 100 59 | 255 91 86 160 220 47 132
R21E | 1002 12 17 17 14 13 16 9 | 46 50 53 47 47 48 48
R22E | 5777 18 14 12 15 21 11 8 | 24 21 47 35 30 15 28
R24E | 1630 11 14 24 19 27 23 10 | 34 35 37 43 34 32 34
------+-----------------------------------------+-------------------------------------
RMS | 1888 37 34 26 26 35 34 |T 69 57 64 68 72 54 62
WRMS | 1888 16 21 14 14 30 32 |NE 70 62 70 71 75 61 67
MEDI | 1163 15 14 14 15 19 17 |MD 69 58 58 61 65 54 59
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