[IGSREPORT-29533] Wk 2280 IGLOS Final Orbits
acc
acc at igs.org
Mon Oct 9 04:05:37 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2280 (Sep 17, 2023 - Sep 23, 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 2.2280.
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:
igl2280[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2280 in the SP3 format.
igl22807.sum Combination Report for GPS Week 2280.
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 | -1.1 ns
1 | 0.3 ns
2 | -1.3 ns
3 | 1.0 ns
4 | -0.0 ns
5 | 0.4 ns
6 | -1.2 ns
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 1.2280, 1a.2280).
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 2.2280.0-6)
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 3.2280.0-6).
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 2280 summary. (Sep 17, 2023 - Sep 23, 2023)
Table 1.2280.a GPS week : 2280 MJD: 60204.0-60210.0
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 4 6 -8 29 .03 17 13 | 65958 -922 13531 134083
| 0 0 1 22 6 16 .02 | 63236 1924
esa n/a| -1 0 -1 -15 -16 7 -.17 24 17 | 1109 -743 2933 7436
| 0 0 1 11 8 22 .03 | 4630 2112
gfz n/a| 0 1 1 32 -4 5 -.07 23 14 | 0 -862 2945 7949
| 1 1 1 15 11 20 .02 | 0 1892
grg n/a| 1 -1 -6 -26 24 -62 .19 21 15 | -53 -811 2935 7472
| 1 1 1 15 15 37 .04 | 297 1858
jgx n/a| -1 2 3 -8 18 -18 -.28 32 31 | 45086 -1054 2954 8112
| 1 1 3 25 19 56 .04 | 1351 1910
Table 1.2280.b GPS week : 2280 MJD: 60204.0-60210.0
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 | 13 14 15 11 9 13 14 |
R02 | 6 6 6 6 6 8 6 |
R03 | 5 9 8 6 9 7 6 |
R04 | 9 9 9 9 5 8 9 |
R05 | 8 7 5 11 5 6 8 |
R07 | 6 8 9 11 6 7 6 |
R08 | 10 10 9 7 6 7 9 |
R09 | 9 10 7 11 9 8 11 |
R11 | 10 8 7 7 7 9 10 |
R12 | 6 7 6 6 10 7 9 |
R13 | 19 16 16 17 18 17 15 |
R14 | 7 6 6 8 8 5 6 |
R15 | 9 9 11 7 8 6 10 |
R16 | 8 8 10 10 9 12 9 |
R17 | 8 7 8 9 9 8 8 |
R18 | 10 10 9 7 7 8 11 |
R19 | 16 18 25 22 28 26 30 |
R20 | 29 33 31 34 37 35 32 |
R21 | 9 7 7 12 6 7 8 |
R22 | 10 8 8 7 7 8 7 |
R24 | 9 10 10 10 8 11 10 |
R25 | 0 12 14 12 22 13 11 |
R26 | 112 88 131 125 142 140 90 |
Table 1.2280.c GPS week : 2280 MJD: 60204.0-60210.0
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 2280 0 | -27 0 19 1687 476 3757 80.7 1974 1974 | -1124 0
brd 2280 1 | -5 -48 -9 1340 2337 2740 83.8 1755 1755 | 276 0
brd 2280 2 | -3 43 28 418 406 -1519 79.7 1645 1645 | -1274 0
brd 2280 3 | -17 30 41 -2029 1368 -543 79.5 1696 1696 | 1012 0
brd 2280 4 | 10 39 45 -1614 421 -1416 79.9 1521 1521 | -38 0
brd 2280 5 | 6 46 128 52 584 -6169 79.6 1550 1550 | 411 0
brd 2280 6 | 10 40 188 -242 -651 -4916 80.3 1686 1686 | -1185 0
-------------+------------------------------------------------------------+----------------
brd 2280 mean| -3 21 62 -55 706 -1152 80.5 1689 1689 | -274 0
brd 2280 sdev| 14 34 69 1389 929 3632 1.5 150 150 | 915 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 2.2280.0 GPS week: 2280 Day: 0 MJD: 60204
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 -21 -12 6 .06 15 11 | 209333 -2306 77149 885439
esa n/a| 0 0 -2 3 -12 23 -.19 24 21 | 1612 -993 3006 6385
gfz n/a| 0 2 0 46 16 18 -.09 19 13 | 0 -1790 3005 6924
grg n/a| 2 -1 -4 -10 20 -100 .18 21 18 | -295 -1886 2984 6370
jgx n/a| 0 0 0 0 40 -8 -.29 28 26 | 44584 -2267 3056 6998
Table 2.2280.1 GPS week: 2280 Day: 1 MJD: 60205
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 5 -14 -10 39 .04 18 14 | 41801 286 3045 9127
esa n/a| -1 0 -1 -15 -22 -16 -.17 21 17 | -1735 -5 3027 8056
gfz n/a| 0 2 2 29 -16 -28 -.04 21 16 | 0 14 3030 7716
grg n/a| 0 -1 -7 -19 46 -16 .22 22 17 | 194 -206 3019 7115
jgx n/a| -1 3 0 -4 17 -38 -.27 34 33 | 45167 -352 3056 7873
Table 2.2280.2 GPS week: 2280 Day: 2 MJD: 60206
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 29 -14 33 .01 18 14 | 40478 -2461 2582 9473
esa n/a| 0 0 0 -7 -12 0 -.17 25 20 | 4572 -2245 2576 6910
gfz n/a| 0 1 0 36 -14 20 -.06 20 12 | 0 -2656 2576 8899
grg n/a| 3 -1 -3 -49 30 -55 .19 19 16 | -258 -2444 2568 8293
jgx n/a| -3 0 4 -10 11 -33 -.36 32 32 | 43528 -2319 2574 8986
Table 2.2280.3 GPS week: 2280 Day: 3 MJD: 60207
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 27 -3 15 .02 17 13 | 40893 2265 2730 8381
esa n/a| 0 1 -3 -28 -34 -24 -.15 27 19 | -4860 2801 2739 7595
gfz n/a| 1 1 4 10 -1 -17 -.06 22 14 | 0 2490 2786 8030
grg n/a| 0 0 -7 -16 24 -9 .16 19 15 | -455 2691 2758 7358
jgx n/a| -3 4 2 3 4 -105 -.25 37 38 | 43879 2434 2792 8190
Table 2.2280.4 GPS week: 2280 Day: 4 MJD: 60208
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 5 29 -15 34 .02 20 11 | 44240 -1512 2923 8895
esa n/a| 0 0 0 -27 -10 14 -.13 23 15 | 1665 -1876 2920 6732
gfz n/a| 0 0 0 13 -7 23 -.09 22 11 | 0 -961 2925 7912
grg n/a| 1 -4 -6 -30 37 -87 .24 23 15 | 297 -1380 2955 7309
jgx n/a| 0 1 5 -29 34 -8 -.28 29 29 | 46954 -1410 2950 8102
Table 2.2280.5 GPS week: 2280 Day: 5 MJD: 60209
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 -8 3 22 .00 16 10 | 43373 305 2817 8409
esa n/a| -2 0 0 -15 -15 31 -.22 27 16 | 8876 688 2811 7934
gfz n/a| 2 1 2 43 3 10 -.05 27 16 | 0 -83 2803 7705
grg n/a| 2 -1 -8 -14 4 -68 .15 19 13 | 237 112 2771 7521
jgx n/a| 0 0 1 -48 34 -16 -.25 32 32 | 46853 -134 2793 7934
Table 2.2280.6 GPS week: 2280 Day: 6 MJD: 60210
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 6 3 -6 56 .03 18 15 | 41590 -3035 3475 8861
esa n/a| -1 1 0 -18 -11 26 -.18 22 15 | -2364 -3574 3455 8443
gfz n/a| 0 1 0 49 -12 10 -.08 27 17 | 0 -3048 3493 8457
grg n/a| 2 0 -6 -42 7 -97 .22 21 15 | -93 -2570 3496 8338
jgx n/a| 0 4 8 33 -14 84 -.27 29 29 | 44638 -3336 3458 8704
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 3.2280.0 GPS week: 2280 Day: 0 MJD: 60204
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 547 17 40 16 12 30 12 | 89 59 85 82 73 79
R02 | 674 7 14 11 9 24 6 | 43 46 49 54 38 47
R03 | 697 6 9 8 12 13 5 | 46 46 45 58 35 48
R04 | 563 16 10 21 9 34 9 | 48 45 38 42 40 42
R05 | 913 9 18 14 13 12 8 | 46 54 42 48 38 45
R07 | 1380 5 16 8 7 18 5 | 55 49 59 50 40 53
R08 | 2910 12 22 16 16 18 9 | 54 52 68 61 45 58
R09 | 2803 14 12 15 16 14 8 | 63 65 54 51 55 57
R11 | 1648 14 17 14 21 26 9 | 35 39 24 21 24 27
R12 | 1958 8 11 8 14 16 6 | 79 73 78 91 68 80
R13 | 1402 20 46 21 43 68 18 | 98 54 87 99 72 85
R14 | 1272 9 7 14 17 18 7 | 75 74 69 83 67 74
R15 | 762 12 21 10 16 13 8 | 93 71 85 94 81 86
R16 | 916 8 21 6 14 19 7 | 88 88 94 92 76 89
R17E | 867 9 12 12 18 --- 7 | 48 49 53 56 --- 50
R18E | 1083 13 15 17 20 17 9 | 85 84 82 85 82 83
R19E | 2723 17 38 21 35 47 15 | 89 89 91 91 95 84
R20E | 3651 37 59 58 45 54 28 | 99 118 124 111 118 104
R21E | 806 12 17 12 18 14 8 | 38 46 36 40 38 38
R22E | 5096 18 13 18 18 9 10 | 62 61 60 63 57 60
R24E | 567 13 15 12 18 19 8 | 114 120 111 131 120 118
XR25E |17823 2 --- --- --- --- 0 | 66 --- --- --- --- 66
XR26 |69261 103 --- 120 --- --- 111 | 439 --- 589 --- --- 507
------+------------------------------------+--------------------------------
RMS | 1973 15 24 19 21 28 |T 84 65 91 71 63 86
WRMS | 1973 11 21 13 18 26 |NE 90 58 97 66 53 91
MEDI | 1272 12 16 14 16 18 |MD 66 59 68 63 57 66
Table 3.2280.1 GPS week: 2280 Day: 1 MJD: 60205
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 721 21 35 20 18 52 14 | 61 49 73 65 61 60
R02 | 943 12 8 8 12 18 6 | 43 49 53 52 46 48
R03 | 810 12 12 14 21 24 9 | 42 46 42 54 36 44
R04 | 512 20 14 12 7 24 8 | 39 40 36 37 34 36
R05 | 936 10 13 12 8 20 6 | 38 45 37 39 41 38
R07 | 2889 11 7 20 13 30 8 | 49 59 71 48 43 56
R08 | 1457 18 10 21 14 18 9 | 50 63 64 53 53 56
R09 | 2392 12 13 21 19 16 9 | 56 63 58 56 57 56
R11 | 1569 11 8 10 19 14 7 | 48 45 50 32 43 43
R12 | 1497 7 10 13 13 23 6 | 66 67 61 64 56 63
R13 | 1781 22 34 21 33 49 16 | 82 62 65 84 73 71
R14 | 1249 5 8 12 11 23 5 | 72 71 78 69 57 72
R15 | 1395 14 17 14 13 18 8 | 78 71 76 75 67 74
R16 | 634 14 11 15 12 16 7 | 71 78 78 75 71 74
R17E | 891 9 9 12 18 --- 7 | 81 83 86 85 --- 83
R18E | 806 10 15 17 23 25 9 | 88 93 92 93 87 90
R19E | 1878 32 25 28 39 57 18 | 91 104 105 96 105 96
R20E | 1302 43 64 61 54 89 32 | 110 114 101 119 137 102
R21E | 1177 12 10 15 8 10 6 | 39 38 48 44 41 41
R22E | 5004 15 8 12 14 11 7 | 84 83 80 84 78 82
R24E | 591 22 12 13 19 18 10 | 130 126 123 120 123 124
XR25E |12310 9 13 --- --- --- 11 | 86 71 --- --- --- 87
XR26 |12774 84 --- 91 --- --- 87 | 342 --- 394 --- --- 362
------+------------------------------------+--------------------------------
RMS | 1754 18 21 21 22 34 |T 80 69 85 68 65 80
WRMS | 1754 14 17 16 17 33 |NE 75 57 82 57 52 76
MEDI | 1302 12 12 14 14 20 |MD 71 63 71 65 57 71
Table 3.2280.2 GPS week: 2280 Day: 2 MJD: 60206
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 928 24 41 16 20 42 15 | 73 44 63 67 62 60
R02 | 754 13 10 5 10 17 5 | 38 45 42 47 33 42
R03 | 937 16 12 9 14 31 7 | 40 43 56 56 34 49
R04 | 661 14 13 13 19 17 8 | 43 50 55 39 51 45
R05 | 1345 7 10 6 11 9 5 | 41 46 42 37 38 40
R07 | 1775 15 13 14 16 25 8 | 36 45 47 29 24 38
R08 | 1275 19 8 18 7 21 8 | 41 50 64 49 44 51
R09 | 2224 14 9 13 14 13 7 | 29 33 40 42 33 34
R11 | 900 12 11 14 9 15 7 | 31 33 30 28 29 28
R12 | 1940 9 10 8 9 18 5 | 62 71 69 64 58 66
R13 | 2046 17 41 18 28 41 15 | 80 48 84 87 58 75
R14 | 1105 9 8 9 12 25 5 | 69 66 64 64 51 65
R15 | 1296 10 29 14 16 21 10 | 78 62 85 88 68 78
R16 | 762 16 22 12 15 22 9 | 72 70 77 79 61 73
R17E | 954 13 16 13 14 --- 8 | 41 35 45 45 --- 39
R18E | 909 15 17 15 17 15 9 | 58 63 61 64 60 60
R19E | 1934 37 39 47 45 75 24 | 43 44 73 47 54 42
R20E | 1772 42 71 58 35 74 30 | 71 77 100 49 73 65
R21E | 1062 10 13 11 16 16 7 | 31 33 32 41 31 32
R22E | 4477 17 10 7 15 18 7 | 18 26 24 30 24 22
R24E | 720 15 17 13 20 17 9 | 68 70 69 62 64 66
XR25E |10269 11 16 --- --- --- 13 | 21 26 --- --- --- 22
XR26 |10753 139 --- 123 --- --- 131 | 313 --- 449 --- --- 384
------+------------------------------------+--------------------------------
RMS | 1645 18 25 20 19 32 |T 60 49 75 53 47 64
WRMS | 1645 14 20 12 15 32 |NE 69 50 84 55 46 75
MEDI | 1275 15 13 13 15 18 |MD 43 45 61 49 51 49
Table 3.2280.3 GPS week: 2280 Day: 3 MJD: 60207
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 580 17 28 14 18 53 11 | 90 63 80 82 73 79
R02 | 623 9 10 11 10 14 5 | 63 58 54 61 57 59
R03 | 1193 8 13 9 13 23 6 | 66 60 59 71 53 64
R04 | 840 18 11 6 17 18 8 | 63 54 55 60 54 58
R05 | 1663 13 22 19 21 22 10 | 60 63 78 78 59 68
R07 | 753 14 23 28 11 23 11 | 69 75 66 68 53 67
R08 | 841 10 14 11 10 18 6 | 66 74 64 74 56 68
R09 | 2020 17 21 21 17 21 11 | 51 53 68 51 53 53
R11 | 1049 12 10 16 7 13 7 | 61 58 51 56 56 56
R12 | 1723 9 9 4 16 14 6 | 76 76 83 91 81 81
R13 | 2288 18 43 18 33 52 16 | 96 73 87 80 81 84
R14 | 2000 6 21 11 14 18 7 | 82 95 78 80 70 82
R15 | 962 9 16 12 14 20 7 | 86 77 81 93 77 84
R16 | 866 14 23 14 13 21 9 | 82 81 83 81 73 81
R17E | 995 11 15 18 17 --- 8 | 100 106 112 109 --- 105
R18E | 921 7 15 10 12 20 6 | 76 75 78 77 73 76
R19E | 2512 28 41 48 36 79 22 | 68 73 96 74 78 72
R20E | 2537 49 83 60 39 101 33 | 82 98 107 84 90 79
R21E | 869 12 17 29 17 13 11 | 59 55 78 71 58 64
R22E | 4318 12 11 10 12 13 6 | 51 58 58 61 49 56
R24E | 650 14 13 12 23 22 9 | 152 149 145 169 147 153
XR25 |14172 9 15 --- --- --- 12 | 58 46 --- --- --- 59
XR26 |11459 113 --- 137 --- --- 124 | 322 --- 469 --- --- 383
------+------------------------------------+--------------------------------
RMS | 1695 17 27 22 19 37 |T 86 73 96 79 69 88
WRMS | 1695 13 19 14 15 38 |NE 88 68 97 73 64 91
MEDI | 1049 12 15 14 16 20 |MD 69 73 78 77 59 72
Table 3.2280.4 GPS week: 2280 Day: 4 MJD: 60208
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 725 17 12 15 16 35 9 | 70 63 58 57 64 61
R02 | 944 11 12 8 9 15 6 | 36 41 36 37 39 36
R03 | 1323 13 15 17 19 32 9 | 45 35 34 50 32 39
R04 | 650 9 8 9 8 20 5 | 47 43 42 50 40 45
R05 | 940 7 10 7 10 18 5 | 38 37 41 51 37 41
R07 | 776 10 8 11 9 15 5 | 43 40 41 45 34 42
R08 | 2142 8 9 13 8 29 6 | 38 39 44 38 23 39
R09 | 1071 16 15 11 21 11 9 | 26 33 30 21 25 25
R11 | 1131 11 9 11 13 20 6 | 26 27 25 33 28 26
R12 | 1496 10 17 7 27 16 9 | 65 59 69 89 59 69
R13 | 1999 18 43 19 39 37 18 | 92 68 90 99 97 85
R14 | 913 7 15 14 14 19 7 | 72 76 64 71 55 70
R15 | 1135 8 15 13 17 28 7 | 79 77 82 70 62 76
R16 | 902 11 14 15 18 13 8 | 70 67 73 58 68 66
R17E | 1325 15 17 14 16 --- 9 | 50 67 59 67 --- 58
R18E | 1253 8 15 13 11 28 7 | 40 35 42 46 38 39
R19E | 1863 28 35 57 68 57 28 | 62 68 99 48 60 62
R20E | 2232 69 73 65 35 65 36 | 70 91 94 62 58 60
R21E | 875 8 12 10 8 14 5 | 33 29 32 40 31 32
R22E | 3777 13 8 12 14 13 7 | 28 32 31 39 33 30
R24E | 702 14 15 15 13 21 8 | 97 107 100 107 113 101
XR25 |11824 20 24 --- --- --- 22 | 38 32 --- --- --- 34
XR26 |11242 134 --- 151 --- --- 142 | 271 --- 425 --- --- 339
------+------------------------------------+--------------------------------
RMS | 1521 20 23 22 23 29 |T 62 53 73 56 49 64
WRMS | 1521 11 15 11 15 29 |NE 67 50 76 54 47 70
MEDI | 1135 11 15 13 14 20 |MD 47 41 44 50 39 45
Table 3.2280.5 GPS week: 2280 Day: 5 MJD: 60209
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 763 18 26 23 19 48 12 | 52 46 51 60 48 52
R02 | 1302 8 19 17 7 16 7 | 27 44 22 34 38 30
R03 | 737 10 11 16 8 24 6 | 33 46 46 41 28 39
R04 | 943 14 10 20 9 20 8 | 39 37 43 46 40 40
R05 | 1055 8 11 9 9 21 5 | 40 30 36 39 42 36
R07 | 1348 7 13 16 9 16 6 | 40 28 44 36 29 36
R08 | 2447 8 13 18 6 17 6 | 41 30 49 37 34 39
R09 | 1975 9 13 16 16 20 8 | 30 43 37 32 30 32
R11 | 1449 11 14 19 16 13 8 | 19 24 21 17 20 16
R12 | 1478 7 12 11 15 19 6 | 48 42 55 59 48 51
R13 | 1592 20 43 19 28 55 16 | 81 51 80 76 57 72
R14 | 707 7 8 9 11 11 5 | 61 61 65 66 58 63
R15 | 1089 7 14 13 9 14 6 | 68 62 74 65 64 66
R16 | 1426 15 18 19 30 15 12 | 60 67 67 42 50 55
R17E | 1253 7 15 18 15 --- 8 | 79 78 81 75 --- 77
R18E | 968 14 17 10 12 16 8 | 56 51 51 59 56 53
R19E | 1263 34 44 55 50 68 26 | 63 70 97 58 66 62
R20E | 2089 36 86 83 26 80 34 | 77 111 120 75 83 81
R21E | 1978 11 15 10 13 20 7 | 33 34 39 38 30 34
R22E | 3162 12 10 15 14 12 7 | 35 38 38 40 42 36
R24E | 977 16 19 19 20 15 10 | 166 163 147 177 155 163
XR25E |12848 9 16 --- --- --- 12 | 42 30 --- --- --- 41
XR26 |11859 112 --- 172 --- --- 139 | 266 --- 403 --- --- 310
------+------------------------------------+--------------------------------
RMS | 1549 16 27 27 19 32 |T 63 53 75 55 50 64
WRMS | 1549 10 16 16 13 32 |NE 60 43 72 46 41 62
MEDI | 1348 11 14 17 14 17 |MD 48 44 51 46 42 51
Table 3.2280.6 GPS week: 2280 Day: 6 MJD: 60210
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1069 30 30 19 13 51 14 | 92 70 81 83 71 81
R02 | 1622 12 8 15 7 19 6 | 50 52 48 55 46 51
R03 | 1782 11 9 11 10 23 6 | 56 64 65 68 49 62
R04 | 1547 10 8 23 14 31 8 | 66 67 74 72 60 68
R05 | 951 3 12 15 18 14 7 | 64 64 72 67 57 66
R07 | 1323 11 10 5 9 20 5 | 67 58 65 62 50 63
R08 | 1239 10 18 20 10 22 8 | 61 56 76 66 52 64
R09 | 2594 17 12 17 23 30 10 | 56 57 56 50 52 53
R11 | 1604 17 12 16 20 16 9 | 48 48 46 48 46 45
R12 | 1416 15 15 18 13 14 9 | 78 76 68 83 72 75
R13 | 1092 23 27 20 30 43 15 | 105 71 94 99 87 92
R14 | 645 8 12 7 11 11 6 | 83 88 83 87 74 85
R15 | 707 9 22 11 18 16 9 | 101 81 101 111 86 98
R16 | 1976 15 17 15 16 15 9 | 92 75 91 74 72 82
R17 | 1342 11 17 11 14 --- 8 | 58 57 57 59 --- 57
R18E | 1050 17 24 14 16 16 10 | 89 96 92 96 86 92
R19E | 1114 40 27 74 55 39 29 | 51 50 100 59 48 48
R20E | 1799 35 67 78 33 71 32 | 74 87 99 79 89 71
R21E | 1796 9 15 16 11 15 7 | 53 51 56 60 49 54
R22E | 3890 15 6 10 12 12 6 | 22 28 28 32 31 26
R24E | 1746 13 16 18 19 15 9 | 147 144 145 157 149 148
XR25 |12593 10 12 --- --- --- 11 | 28 23 --- --- --- 28
XR26 |15307 78 --- 103 --- --- 90 | 476 --- 584 --- --- 517
------+------------------------------------+--------------------------------
RMS | 1685 18 22 27 21 29 |T 87 66 99 74 66 88
WRMS | 1685 15 15 17 15 29 |NE 99 66 106 73 62 100
MEDI | 1547 13 15 16 14 16 |MD 66 64 74 68 57 66
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