[IGSREPORT-29679] Wk 2294 IGLOS Final Orbits
acc
acc at igs.org
Fri Jan 12 06:14:43 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2294 (Dec 24, 2023 - Dec 30, 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 2.2294.
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:
igl2294[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2294 in the SP3 format.
igl22947.sum Combination Report for GPS Week 2294.
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 | 0.1 ns
1 | -1.3 ns
2 | 0.5 ns
3 | 0.3 ns
4 | -0.8 ns
5 | -1.0 ns
6 | 0.1 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
----+--------+---------------
6 | 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 1.2294, 1a.2294).
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 2.2294.0-6)
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 3.2294.0-6).
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 2294 summary. (Dec 24, 2023 - Dec 30, 2023)
Table 1.2294.a GPS week : 2294 MJD: 60302.0-60308.0
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 -5 -24 -14 73 .13 24 19 | 43659 -582 3339 11557
| 0 1 3 9 12 20 .04 | 2292 1750
esa n/a| 0 0 0 -22 7 6 -.12 36 28 | 1226 -1365 3185 7891
| 1 1 1 15 12 35 .04 | 1616 1839
gfz n/a| 0 0 0 25 1 4 -.03 21 14 | 0 -630 3219 7718
| 1 1 1 19 18 27 .06 | 0 1560
grg n/a| 1 -3 0 -10 -5 -61 .27 36 26 | 794 -715 3383 10821
| 1 1 3 33 16 43 .08 | 2454 1656
jgx n/a| 0 1 4 15 9 -47 -.16 23 23 | 45833 -850 3242 8011
| 1 1 1 14 18 36 .03 | 1562 1964
Table 1.2294.b GPS week : 2294 MJD: 60302.0-60308.0
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 21 19 26 21 15 13 |
R02 | 7 7 7 7 12 19 12 |
R03 | 8 8 9 10 11 15 8 |
R04 | 11 10 11 7 14 14 8 |
R05 | 8 11 9 9 14 15 8 |
R07 | 8 8 7 9 11 13 7 |
R08 | 8 8 8 8 12 15 10 |
R09 | 7 9 7 7 6 8 8 |
R11 | 7 7 6 7 6 6 8 |
R12 | 7 8 7 7 7 7 7 |
R13 | 20 17 21 20 16 19 20 |
R14 | 8 8 8 7 6 6 6 |
R15 | 9 10 8 8 9 6 7 |
R16 | 11 9 9 10 10 9 7 |
R17 | 8 8 8 10 6 9 9 |
R18 | 9 8 8 10 7 7 10 |
R19 | 24 25 28 27 21 21 25 |
R20 | 32 29 36 36 31 36 35 |
R21 | 8 9 7 10 10 8 9 |
R22 | 8 9 10 5 7 7 7 |
R24 | 12 9 10 11 11 12 10 |
R25 | 12 13 0 0 12 17 16 |
R26 | 17 17 31 15 43 --- --- |
Table 1.2294.c GPS week : 2294 MJD: 60302.0-60308.0
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 2294 0 | 0 -18 -27 443 90 -4225 79.8 1809 1809 | 146 0
brd 2294 1 | -19 12 -81 -1579 1583 -1144 81.9 1594 1594 | -1275 0
brd 2294 2 | -15 15 -130 -516 1352 -1197 81.0 1821 1821 | 506 0
brd 2294 3 | -33 11 -77 1284 1331 2449 79.7 1768 1768 | 271 0
brd 2294 4 | -42 -12 -41 970 479 988 80.1 1673 1673 | -752 0
brd 2294 5 | 93 -60 54 1614 -1295 11 81.0 1940 1940 | -980 0
brd 2294 6 | 59 -40 135 -67 -607 5429 79.4 1533 1533 | 125 0
-------------+------------------------------------------------------------+----------------
brd 2294 mean| 6 -13 -23 306 419 330 80.4 1733 1733 | -279 0
brd 2294 sdev| 51 28 90 1117 1092 3062 .9 141 141 | 703 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 2.2294.0 GPS week: 2294 Day: 0 MJD: 60302
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 -7 2 82 .14 25 19 | 41279 824 3497 8542
esa n/a| 0 0 -1 -22 21 31 -.17 32 21 | 2062 -221 3486 7835
gfz n/a| 0 0 0 -13 7 3 -.01 18 12 | 0 291 3548 8016
grg n/a| 1 -5 0 27 -30 -32 .33 31 26 | 227 -329 3547 7700
jgx n/a| 0 1 3 25 9 -127 -.14 25 25 | 44693 -452 3532 8261
Table 2.2294.1 GPS week: 2294 Day: 1 MJD: 60303
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 -4 -22 -25 68 .14 22 19 | 47937 -3551 4186 31987
esa n/a| 0 0 -2 -48 -16 -5 -.08 36 27 | 4333 -4129 3073 7039
gfz n/a| -1 0 0 18 20 -32 -.07 19 14 | 0 -2741 3099 7436
grg n/a| 3 -4 -3 -1 -12 -33 .32 34 25 | 6329 -3325 4278 32193
jgx n/a| 0 1 5 23 -12 -18 -.15 21 20 | 44810 -3033 3196 7245
Table 2.2294.2 GPS week: 2294 Day: 2 MJD: 60304
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 -35 -10 30 .12 17 14 | 41084 976 3376 8761
esa n/a| 0 0 0 -2 6 15 -.07 40 36 | 1495 -46 3422 8554
gfz n/a| 0 2 0 47 -16 16 -.11 27 14 | 0 1373 3418 8410
grg n/a| 1 -5 2 0 14 -34 .26 31 25 | -382 1290 3451 7982
jgx n/a| 0 1 4 20 -4 -39 -.15 25 25 | 43825 956 3517 8798
Table 2.2294.3 GPS week: 2294 Day: 3 MJD: 60305
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 -2 -7 -31 -18 88 .06 24 18 | 43459 818 3296 7150
esa n/a| 3 0 0 -26 6 33 -.14 37 37 | 562 799 3300 6950
gfz n/a| 0 1 -1 31 7 45 -.07 28 16 | 0 588 3325 7127
grg n/a| 0 -3 -2 13 -5 -117 .28 31 25 | -500 902 3277 6360
jgx n/a| -2 2 6 -12 40 -35 -.13 23 23 | 45599 1373 3325 7407
Table 2.2294.4 GPS week: 2294 Day: 4 MJD: 60306
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 -16 -30 83 .18 28 18 | 43895 -1474 3060 8055
esa n/a| 0 1 1 -25 14 28 -.10 33 28 | 187 -2600 3049 7609
gfz n/a| 1 -1 1 34 5 17 .04 17 15 | 0 -1610 3081 7572
grg n/a| 2 -1 -5 -34 -15 -110 .16 41 28 | -215 -1244 3095 6815
jgx n/a| 0 0 4 9 27 -54 -.17 21 21 | 48352 -2309 3110 7964
Table 2.2294.5 GPS week: 2294 Day: 5 MJD: 60307
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 -10 -27 -21 81 .09 31 24 | 43422 -1903 3283 8316
esa n/a| -1 0 -2 -2 16 6 -.16 31 22 | 524 -2948 3293 8745
gfz n/a| 1 1 0 28 16 10 .06 20 16 | 0 -2226 3340 7905
grg n/a| 0 -2 6 -71 -2 -91 .17 53 30 | 94 -2203 3332 7614
jgx n/a| 0 0 3 8 7 -26 -.15 18 18 | 46986 -3193 3401 8489
Table 2.2294.6 GPS week: 2294 Day: 6 MJD: 60308
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 -26 0 80 .17 21 21 | 44543 233 2681 8093
esa n/a| 0 2 0 -28 4 -66 -.16 44 22 | -575 -416 2676 8511
gfz n/a| 2 0 0 31 -30 -28 -.03 21 15 | 0 -87 2728 7563
grg n/a| 0 -4 -1 -9 15 -12 .37 31 21 | 7 -98 2703 7085
jgx n/a| 0 1 3 30 -1 -29 -.23 26 26 | 46566 703 2616 7913
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 3.2294.0 GPS week: 2294 Day: 0 MJD: 60302
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 985 36 39 34 30 35 17 | 111 111 112 106 115 108
R02 | 758 11 13 9 19 15 7 | 85 92 83 90 69 84
R03E | 2199 16 13 13 15 17 7 | 91 87 94 89 83 88
R04E | 1170 17 13 21 18 31 10 | 135 126 137 126 119 128
R05E | 1269 15 15 15 12 18 7 | 84 85 81 89 68 81
R07E | 952 7 13 15 14 22 7 | 117 122 119 118 107 116
R08E | 3140 12 14 20 12 18 8 | 78 79 88 83 74 80
R09 | 678 19 10 15 14 9 7 | 52 56 62 52 59 55
R11 | 2628 17 11 8 16 18 7 | 42 50 50 49 54 47
R12 | 1086 14 20 10 14 13 7 | 88 95 87 81 87 86
R13 | 3101 51 22 31 40 51 20 | 92 67 70 67 27 73
R14 | 735 13 13 17 21 13 8 | 74 79 81 65 72 74
R15 | 1096 20 18 10 20 20 8 | 108 97 96 89 93 96
R16 | 1022 27 17 21 20 18 10 | 110 97 93 103 97 97
XR17 | 660 11 20 11 10 --- 7 | 80 73 79 76 --- 77
R18 | 532 14 11 19 8 24 8 | 70 76 78 70 73 72
R19 | 1387 36 64 13 69 47 23 | 108 95 99 115 102 100
R20 | 4004 55 104 25 83 33 31 | 121 99 108 121 104 101
R21 | 759 9 16 9 24 16 7 | 79 76 76 87 78 77
R22 | 1236 20 9 11 18 15 7 | 62 65 62 63 66 62
R24 | 1995 15 28 16 35 21 11 | 83 71 79 89 70 77
XR25 |13740 12 10 --- --- --- 11 | 76 41 --- --- --- 78
XR26 |>>>>> 15 --- --- 19 --- 17 | 60 --- --- 77 --- 65
------+------------------------------------+--------------------------------
RMS | 1808 25 32 18 31 25 |T 87 83 87 86 80 83
WRMS | 1808 19 21 12 26 25 |NE 81 76 80 80 75 77
MEDI | 1170 15 14 15 18 18 |MD 84 79 83 87 74 80
Table 3.2294.1 GPS week: 2294 Day: 1 MJD: 60303
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 836 40 45 41 50 36 21 | 105 102 106 104 99 99
R02 | 632 11 13 16 21 12 7 | 77 79 70 82 43 74
R03E | 1872 19 17 13 14 14 8 | 91 79 80 85 82 82
R04E | 472 23 12 13 18 23 9 | 123 120 114 112 110 115
R05E | 1583 20 17 15 35 20 10 | 104 102 96 83 77 92
R07E | 703 8 19 15 18 20 8 | 111 116 114 115 105 111
R08E | 2835 13 12 17 17 14 7 | 75 79 79 84 72 76
R09 | 816 15 16 20 20 12 8 | 32 36 44 36 37 35
R11 | 1616 15 17 6 15 12 6 | 41 48 40 47 44 42
R12 | 1281 12 19 16 16 18 8 | 71 76 73 66 68 70
XR13 | 1258 23 28 20 48 --- 17 | 65 68 71 57 --- 66
R14 | 712 6 25 10 30 11 8 | 62 67 61 54 62 60
R15 | 788 24 15 8 34 15 9 | 86 75 75 74 72 75
R16 | 563 25 20 12 12 18 9 | 91 80 69 79 76 77
XR17 | 647 10 16 7 20 --- 7 | 37 29 34 40 --- 34
R18 | 753 10 27 11 11 18 8 | 35 39 30 34 34 31
R19 | 672 32 89 25 79 31 25 | 81 69 69 74 75 73
R20 | 4060 50 98 40 70 43 29 | 64 48 58 68 64 52
R21 | 747 7 20 18 19 19 8 | 41 37 43 48 36 40
R22 | 2301 13 7 15 36 16 9 | 29 27 39 33 34 30
R24 | 1638 15 30 10 24 11 8 | 40 38 31 34 31 33
XR25 |19842 11 14 --- --- --- 12 | 89 75 --- --- --- 92
XR26 |>>>>> 13 --- --- 22 --- 17 | 33 --- --- 50 --- 39
------+------------------------------------+--------------------------------
RMS | 1594 22 36 19 34 21 |T 68 67 66 66 64 65
WRMS | 1594 19 27 14 25 20 |NE 57 55 53 54 52 54
MEDI | 836 15 17 15 20 18 |MD 71 69 69 66 68 70
Table 3.2294.2 GPS week: 2294 Day: 2 MJD: 60304
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 892 27 48 37 39 45 19 | 136 136 138 130 134 133
R02 | 997 8 14 13 22 11 7 | 113 111 118 116 69 114
R03E | 1734 16 22 15 16 19 8 | 110 107 105 113 114 109
R04E | 630 23 17 11 29 20 10 | 147 146 143 142 138 142
R05E | 1976 13 13 17 28 19 9 | 164 164 169 155 143 163
R07E | 1576 13 20 12 10 14 7 | 132 124 128 129 127 128
R08E | 1037 14 15 18 21 12 8 | 108 106 110 114 108 108
R09 | 1953 14 14 12 10 17 7 | 80 89 92 88 91 87
R11 | 1388 10 10 14 16 10 6 | 90 90 96 90 96 92
R12 | 1719 13 18 9 21 9 7 | 122 128 124 122 129 124
XR13 | 812 22 35 42 47 --- 21 | 124 117 124 116 --- 122
R14 | 709 12 22 19 14 9 7 | 109 110 106 106 108 107
R15 | 756 13 18 13 21 13 7 | 133 126 131 130 128 129
R16 | 666 14 16 19 16 19 8 | 127 131 138 132 126 130
XR17 | 704 11 19 8 16 --- 7 | 97 90 90 93 --- 93
R18 | 689 10 17 12 19 18 7 | 92 89 99 94 93 93
R19 | 1206 27 89 31 74 57 27 | 111 100 107 123 137 114
R20 | 5669 34 125 89 66 45 36 | 105 92 127 116 102 105
R21 | 972 7 16 12 17 15 6 | 94 86 94 101 86 91
R22 | 1894 15 15 14 36 18 10 | 87 102 86 125 87 93
R24 | 1237 20 23 14 18 25 10 | 96 88 86 105 81 90
XR25 |12187 4 --- --- --- --- 0 | 103 --- --- --- --- 104
XR26 | ---- 22 --- --- 42 --- 30 | 66 --- --- 112 --- 81
------+------------------------------------+--------------------------------
RMS | 1821 17 40 27 31 25 |T 110 111 114 116 110 110
WRMS | 1821 14 36 14 25 25 |NE 102 103 107 110 102 104
MEDI | 1037 14 18 14 21 18 |MD 109 107 110 116 108 108
Table 3.2294.3 GPS week: 2294 Day: 3 MJD: 60305
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 736 45 38 59 65 49 26 | 113 110 121 131 109 109
R02 | 855 12 14 12 16 11 6 | 80 80 82 83 43 78
R03E | 1958 14 25 21 23 14 9 | 83 82 80 79 79 78
R04E | 526 19 12 8 14 15 7 | 93 83 86 95 85 87
R05E | 2040 17 13 14 24 14 8 | 116 109 119 103 122 110
R07E | 1185 19 18 16 20 18 9 | 93 82 91 95 84 87
R08E | 732 13 12 20 10 14 7 | 62 60 62 64 57 59
R09 | 3504 15 14 15 8 12 6 | 36 37 44 36 35 36
R11 | 1047 11 8 17 17 9 6 | 28 30 34 32 30 28
R12 | 1944 15 14 15 15 10 7 | 53 48 45 35 39 42
XR13 | 660 22 37 35 45 --- 20 | 65 55 57 62 --- 58
R14 | 733 13 21 6 19 11 7 | 59 61 50 44 47 50
R15 | 730 17 21 12 19 10 8 | 61 64 52 45 47 51
R16 | 917 23 15 16 15 22 9 | 69 66 65 51 46 57
XR17 | 1039 21 15 14 14 --- 9 | 52 45 47 47 --- 46
R18 | 685 16 23 16 24 18 9 | 45 52 45 48 41 43
R19 | 1230 50 85 32 70 32 27 | 93 48 85 84 68 74
R20 | 4651 53 108 83 58 57 36 | 98 49 102 96 86 79
R21 | 791 11 27 27 13 13 9 | 51 41 57 50 45 47
R22 | 1522 12 10 11 10 7 5 | 29 31 32 35 31 30
R24 | 1503 13 29 14 31 18 10 | 52 41 52 61 44 48
XR25 |15037 7 --- --- --- --- 0 | 186 --- --- --- --- 187
XR26 | ---- 13 --- --- 18 --- 15 | 41 --- --- 52 --- 41
------+------------------------------------+--------------------------------
RMS | 1768 24 37 28 31 23 |T 72 60 67 64 59 66
WRMS | 1768 18 37 16 25 23 |NE 64 49 56 53 46 58
MEDI | 1039 15 18 16 18 14 |MD 62 55 57 52 47 57
Table 3.2294.4 GPS week: 2294 Day: 4 MJD: 60306
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 755 52 28 32 69 32 20 | 156 155 163 138 152 153
XR02 | 716 17 15 10 42 --- 11 | 94 84 78 108 --- 86
R03E | 1600 13 25 20 40 18 11 | 104 105 114 136 106 110
R04E | 621 21 23 16 59 27 14 | 119 112 116 156 112 117
XR05E | 1494 19 23 12 46 --- 13 | 125 125 134 150 --- 130
R07E | 1185 17 17 14 43 24 11 | 148 153 154 176 139 151
R08E | 950 16 15 14 54 18 11 | 90 86 88 132 82 90
R09 | 3733 16 9 13 12 9 6 | 40 44 44 43 43 41
R11 | 831 13 13 11 6 10 5 | 46 44 44 44 43 43
R12 | 2635 19 12 12 9 8 6 | 90 82 86 84 88 85
XR13 | 628 33 32 19 32 --- 16 | 65 58 64 86 --- 67
R14 | 616 10 12 9 19 13 6 | 62 56 63 59 55 59
R15 | 730 21 15 13 6 21 8 | 95 84 82 88 89 86
R16 | 991 15 16 17 19 26 9 | 99 103 107 102 96 100
XR17 | 1172 10 14 8 12 --- 6 | 63 60 59 66 --- 60
R18 | 785 13 18 10 17 12 6 | 54 62 57 55 56 56
R19 | 2210 44 56 19 68 34 21 | 81 67 74 83 87 75
R20 | 1637 72 101 31 71 33 30 | 112 60 79 95 90 84
R21 | 627 15 22 19 23 21 10 | 65 58 71 68 57 63
R22 | 2080 14 7 10 29 12 7 | 47 58 60 89 50 57
R24 | 2316 16 31 10 36 20 10 | 66 56 55 76 51 58
XR25 |13527 10 13 --- --- --- 11 | 94 98 --- --- --- 93
XR26 | ---- 32 --- --- 56 --- 42 | 80 --- --- 116 --- 89
------+------------------------------------+--------------------------------
RMS | 1672 28 33 17 41 21 |T 86 82 85 97 82 84
WRMS | 1672 18 28 15 28 21 |NE 73 67 68 78 67 70
MEDI | 991 16 16 13 32 20 |MD 90 67 78 88 87 85
Table 3.2294.5 GPS week: 2294 Day: 5 MJD: 60307
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01E | 536 34 38 31 27 21 15 | 112 102 111 107 105 105
XR02 | 690 17 24 15 79 --- 18 | 115 113 117 174 --- 120
R03E | 1127 26 14 20 79 16 14 | 105 99 98 105 101 98
R04E | 1516 22 16 12 78 15 13 | 210 207 204 181 206 202
R05E | 2298 21 13 24 81 18 15 | 161 163 163 182 165 159
R07E | 1472 23 13 12 67 16 12 | 193 185 190 180 190 187
R08E | 820 18 21 30 67 19 14 | 134 127 132 115 128 126
R09 | 3795 20 14 9 9 19 7 | 36 42 40 38 38 36
R11 | 809 11 10 12 17 5 5 | 52 50 55 55 47 51
R12 | 1937 19 14 7 20 13 7 | 73 64 64 63 64 65
XR13 | 1270 44 24 25 39 --- 18 | 67 59 70 69 --- 66
R14 | 1294 15 10 6 17 12 5 | 59 60 61 62 59 60
R15 | 1004 15 11 8 11 9 5 | 82 71 78 77 74 76
R16 | 535 24 20 7 11 22 9 | 84 79 84 76 73 78
XR17 | 1513 15 19 13 16 --- 9 | 45 39 42 43 --- 40
R18 | 1211 13 13 9 17 14 6 | 41 36 34 50 31 36
R19 | 5186 36 58 35 74 24 21 | 46 55 46 59 48 43
R20 | 1552 98 95 41 105 43 36 | 64 61 59 49 60 57
R21 | 577 18 19 11 29 7 7 | 47 36 34 53 44 39
R22 | 1515 15 10 10 30 7 6 | 29 32 35 38 28 30
R24 | 758 20 30 18 41 18 11 | 43 37 41 49 33 38
XR25 |16828 19 14 --- --- --- 16 | 144 86 --- --- --- 145
------+------------------------------------+--------------------------------
RMS | 1940 31 31 20 53 18 |T 88 81 83 86 83 84
WRMS | 1940 24 22 16 30 18 |NE 64 57 57 63 49 61
MEDI | 1270 19 14 12 30 16 |MD 67 61 64 63 60 65
Table 3.2294.6 GPS week: 2294 Day: 6 MJD: 60308
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1053 29 30 25 22 18 12 | 141 156 163 145 147 149
XR02 | 782 15 13 20 31 --- 11 | 97 94 95 100 --- 95
R03E | 1034 14 15 15 19 13 7 | 148 138 137 131 133 137
R04E | 1533 12 15 19 14 16 8 | 271 273 269 255 262 267
R05E | 1541 16 13 16 17 17 8 | 178 181 178 163 166 174
R07E | 981 11 12 11 16 17 7 | 232 229 229 217 218 225
R08E | 1366 14 20 24 15 21 10 | 150 155 155 140 147 149
R09 | 2439 20 18 11 14 15 8 | 35 37 34 36 35 32
R11 | 1120 12 14 16 19 12 7 | 47 55 53 54 52 50
R12 | 1355 12 11 14 18 10 6 | 91 84 89 82 80 84
R13 | 1281 48 24 11 55 44 19 | 91 78 78 75 20 78
R14 | 1146 8 11 8 16 14 5 | 79 83 84 72 74 78
R15 | 850 15 14 10 12 12 6 | 106 91 98 101 95 98
R16 | 686 13 14 10 15 14 6 | 105 97 103 103 94 100
XR17 | 1596 16 22 11 14 --- 9 | 66 51 54 61 --- 57
R18 | 1618 10 15 17 14 31 9 | 55 57 56 58 43 52
R19 | 3789 29 68 27 67 50 24 | 97 75 94 107 83 86
R20 | 1528 43 162 56 79 66 35 | 130 87 139 131 109 122
R21 | 615 9 24 20 16 20 9 | 72 60 78 81 68 71
R22 | 1319 17 8 12 14 10 6 | 32 34 36 32 32 32
R24 | 526 14 28 19 21 14 10 | 69 49 71 75 52 62
XR25 |12603 14 16 --- --- --- 15 | 133 80 --- --- --- 132
------+------------------------------------+--------------------------------
RMS | 1533 21 44 21 31 26 |T 110 102 109 105 100 105
WRMS | 1533 21 22 15 21 26 |NE 81 69 77 77 64 76
MEDI | 1281 14 15 16 16 16 |MD 97 83 94 100 83 86
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