[IGSREPORT-29450] Wk 2272 IGLOS Final Orbits
acc
acc at igs.org
Mon Aug 14 04:00:17 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2272 (Jul 23, 2023 - Jul 29, 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 2.2272.
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:
igl2272[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2272 in the SP3 format.
igl22727.sum Combination Report for GPS Week 2272.
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 | 0.6 ns
1 | -2.0 ns
2 | -14.8 ns
3 | 0.9 ns
4 | 0.4 ns
5 | 0.3 ns
6 | -1.7 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 1.2272, 1a.2272).
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 2.2272.0-6)
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 3.2272.0-6).
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 2272 summary. (Jul 23, 2023 - Jul 29, 2023)
Table 1.2272.a GPS week : 2272 MJD: 60148.0-60154.0
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 0 0 -25 20 -.00 18 15 | 34456 -643 2911 8894
| 0 0 0 12 15 23 .02 | 7164 2194
esa n/a| 0 0 1 -4 3 24 -.24 33 24 | -3393 240 2897 7081
| 0 1 1 8 10 14 .07 | 8155 2236
gfz n/a| 0 0 -1 7 6 36 -.15 21 15 | 0 -482 2875 8348
| 0 0 0 10 7 15 .05 | 0 2411
grg n/a| 2 0 0 -6 15 -76 .32 21 17 | -2366 -193 2863 7846
| 1 1 1 10 11 35 .03 | 5737 2565
iac n/a| 0 0 -3 -14 -11 25 -.23 25 21 | 365 -1033 2897 8979
| 2 1 2 17 25 94 .06 | 5721 599
jgx n/a| -1 0 2 40 9 -30 -.23 31 31 | 35294 -387 2828 8444
| 1 1 1 21 17 40 .08 | 7178 2824
Table 1.2272.b GPS week : 2272 MJD: 60148.0-60154.0
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 | 19 20 20 18 21 20 15 |
R02 | 8 8 10 8 7 6 7 |
R03 | 7 8 9 8 7 8 8 |
R04 | 9 8 9 9 9 7 8 |
R05 | 8 11 8 7 9 9 7 |
R07 | 7 9 10 8 8 8 8 |
R08 | 10 8 8 10 9 8 10 |
R09 | 7 6 7 7 6 9 8 |
R11 | 11 6 7 9 7 8 8 |
R12 | 10 8 8 7 9 8 8 |
R13 | 19 22 13 21 21 15 16 |
R14 | 6 6 6 6 7 6 8 |
R15 | 9 7 12 11 10 7 7 |
R16 | 8 11 11 9 9 9 9 |
R17 | 9 9 7 7 8 8 9 |
R18 | 9 9 12 10 12 11 12 |
R19 | 28 27 24 29 29 32 25 |
R20 | 31 35 30 33 35 32 38 |
R21 | 9 9 8 9 10 10 7 |
R22 | 7 7 8 8 11 8 7 |
R24 | 11 9 9 11 11 10 12 |
R25 | 13 13 14 11 15 0 16 |
Table 1.2272.c GPS week : 2272 MJD: 60148.0-60154.0
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 2272 0 | 39 -14 81 -12 -643 6035 80.7 1570 1570 | 627 0
brd 2272 1 | -33 -8 62 1201 -534 9878 82.1 1518 1518 | -1996 0
brd 2272 2 | -12 -94 64 -860 193 7268 81.1 1594 1594 | -14778 0
brd 2272 3 | -12 -78 101 -598 -1152 6134 82.8 1454 1454 | 902 0
brd 2272 4 | 48 -86 203 753 -1128 6069 80.9 1367 1367 | 370 0
brd 2272 5 | 0 -81 156 -231 123 5601 81.8 1405 1405 | 320 0
brd 2272 6 | 18 -1 280 375 1485 5122 81.4 1461 1461 | -1741 0
-------------+------------------------------------------------------------+----------------
brd 2272 mean| 6 -52 135 89 -236 6586 81.5 1481 1481 | -2328 0
brd 2272 sdev| 29 41 81 735 927 1591 .8 83 83 | 5611 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 2.2272.0 GPS week: 2272 Day: 0 MJD: 60148
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 0 11 -34 -1 .02 16 13 | 34711 1296 3102 9996
esa n/a| 0 -1 0 0 8 43 -.25 34 27 | 8393 1951 3099 6746
gfz n/a| -1 -1 -2 2 0 40 -.08 19 15 | 0 1225 3159 9185
grg n/a| 3 2 0 -16 38 -87 .30 23 17 | -679 2782 3129 8973
iac n/a| 2 0 -2 4 -7 213 -.26 27 24 | 2788 -226 3089 9990
jgx n/a| 0 1 0 34 14 32 -.26 30 30 | 35714 2427 3015 9477
Table 2.2272.1 GPS week: 2272 Day: 1 MJD: 60149
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 1 13 -20 20 .00 18 16 | 34427 -4204 3272 8710
esa n/a| 0 0 0 -12 -10 19 -.13 31 22 | 743 -2587 3298 7410
gfz n/a| 0 0 0 -12 8 20 -.16 21 14 | 0 -3783 3304 8340
grg n/a| 3 0 -2 -14 16 -55 .34 25 17 | -266 -3709 3278 7831
iac n/a| -4 1 -5 -6 37 11 -.15 24 20 | 893 -1434 3266 8763
jgx n/a| 0 -1 2 14 -25 9 -.38 32 32 | 36553 -4898 3281 8431
Table 2.2272.2 GPS week: 2272 Day: 2 MJD: 60150
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 0 -6 35 -.01 19 15 | 18851 290 3020 9074
esa n/a| 0 0 3 -8 -4 26 -.21 28 24 | -15930 208 3034 7078
gfz n/a| 0 2 -1 7 15 18 -.19 23 19 | 0 733 2697 8686
grg n/a| 1 0 -1 -17 11 -64 .31 17 13 | -15363 854 2679 8203
iac n/a| 0 -1 -3 -20 -28 -89 -.17 24 22 | -12449 -1263 3024 9244
jgx n/a| 0 0 2 20 13 -82 -.21 31 31 | 19383 1636 2613 8786
Table 2.2272.3 GPS week: 2272 Day: 3 MJD: 60151
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 0 -21 -18 40 -.03 18 13 | 36624 662 2883 7866
esa n/a| -1 1 3 3 2 32 -.21 33 26 | -1684 1632 2860 6173
gfz n/a| 0 1 0 12 2 27 -.14 22 16 | 0 1455 2894 6808
grg n/a| 1 -1 -1 1 7 -94 .36 22 18 | 32 1701 2900 6224
iac n/a| 0 1 0 5 -22 6 -.30 26 23 | 3270 -668 2875 7640
jgx n/a| -4 1 4 37 9 -43 -.14 30 30 | 37391 1503 2876 6878
Table 2.2272.4 GPS week: 2272 Day: 4 MJD: 60152
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 0 -8 -33 47 -.01 21 15 | 37872 717 2962 8860
esa n/a| 0 0 2 -15 17 -1 -.23 34 24 | -1419 2544 2922 8299
gfz n/a| 1 1 -2 17 0 61 -.11 19 16 | 0 1057 2969 8499
grg n/a| 2 0 -1 -1 16 -140 .32 24 20 | -325 1043 2961 7691
iac n/a| 2 0 -2 -31 -25 8 -.24 24 20 | 2841 -408 2940 9078
jgx n/a| -3 1 5 56 24 -54 -.20 32 32 | 38730 484 2998 8203
Table 2.2272.5 GPS week: 2272 Day: 5 MJD: 60153
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 -8 -12 -17 -.02 19 16 | 39517 112 2575 9770
esa n/a| -1 0 1 6 -1 16 -.35 36 25 | -12127 1039 2557 7088
gfz n/a| -1 1 -3 16 2 43 -.15 21 13 | 0 50 2566 9318
grg n/a| 4 0 0 9 3 -28 .28 19 15 | 151 -362 2552 8756
iac n/a| -3 -1 -2 -12 2 -29 -.19 25 21 | 3447 -1413 2542 9921
jgx n/a| 0 0 0 42 5 -59 -.19 33 33 | 39952 -147 2504 9505
Table 2.2272.6 GPS week: 2272 Day: 6 MJD: 60154
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 0 6 -51 20 .03 17 15 | 39190 -3376 2564 7982
esa n/a| -1 0 4 -5 15 31 -.27 33 19 | -1729 -3106 2515 6774
gfz n/a| 0 1 -2 7 18 46 -.23 21 15 | 0 -4115 2541 7601
grg n/a| 2 0 0 -8 16 -62 .36 21 18 | -114 -3663 2548 7247
iac n/a| 0 1 -6 -42 -37 53 -.32 23 21 | 1770 -1824 2547 8222
jgx n/a| 0 -1 0 77 25 -18 -.25 32 32 | 39341 -3720 2512 7834
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 3.2272.0 GPS week: 2272 Day: 0 MJD: 60148
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 672 28 51 27 29 35 48 19 | 98 120 107 101 92 105 101
R02 | 832 11 12 10 17 23 --- 7 | 82 81 79 84 75 --- 80
R03E | 1001 7 13 13 14 27 14 7 | 102 97 102 104 87 96 101
R04E | 1246 9 16 15 19 25 20 8 | 93 92 89 96 89 88 91
R05E | 1518 8 11 15 19 20 16 8 | 77 80 79 82 76 77 78
R07E | 821 11 12 11 11 19 11 6 | 61 65 64 69 51 62 64
R08E | 2755 12 18 17 19 32 12 9 | 58 62 57 71 51 57 60
R09 | 833 12 10 16 9 34 14 7 | 18 15 19 14 31 15 14
R11 | 1439 12 18 20 23 18 9 10 | 29 26 26 33 33 27 25
R12 | 1254 14 12 21 16 26 9 9 | 35 42 42 41 39 39 37
R13 | 756 15 37 30 45 25 81 18 | 56 47 51 44 50 50 47
R14 | 1251 10 8 10 13 17 11 6 | 40 48 45 51 36 41 44
R15 | 1184 18 17 13 14 13 10 9 | 48 41 43 50 42 39 44
R16 | 1799 10 21 14 12 17 11 8 | 55 57 48 44 55 57 49
R17 | 788 13 21 9 19 17 --- 9 | 64 54 56 55 54 --- 56
R18 | 1342 7 24 11 16 18 20 8 | 48 66 44 49 47 40 49
R19 | 1437 27 85 38 44 48 49 27 | 106 40 108 92 77 58 88
R20 | 3569 36 99 38 41 48 54 31 | 113 44 116 99 75 60 92
R21 | 768 13 11 16 16 35 24 8 | 78 65 71 69 63 55 71
R22 | 2291 12 13 9 11 12 12 6 | 43 42 49 46 45 47 44
R24 | 1815 17 19 16 20 20 12 10 | 55 62 60 66 58 51 58
XR25 |14014 8 18 --- --- 37 --- 12 | 22 34 --- --- 31 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 1570 16 34 19 23 27 30 |T 62 58 64 64 57 56 59
WRMS | 1570 13 27 15 17 24 30 |NE 55 47 57 55 50 44 51
MEDI | 1251 12 17 15 17 23 14 |MD 56 54 57 66 51 55 56
Table 3.2272.1 GPS week: 2272 Day: 1 MJD: 60149
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 747 24 45 42 20 41 26 19 | 80 90 100 86 78 76 85
R02 | 1108 12 14 15 14 21 --- 8 | 93 91 94 92 89 --- 91
R03E | 799 8 17 17 12 16 18 8 | 95 98 94 101 93 97 96
R04E | 1421 11 13 10 17 17 20 7 | 76 76 74 79 82 74 75
R05E | 1479 7 18 16 29 19 12 10 | 75 73 72 86 79 71 75
R07E | 1105 12 20 12 15 21 15 8 | 61 62 66 60 66 60 61
R08E | 2472 11 18 11 11 23 14 7 | 58 62 65 64 54 52 61
R09 | 890 10 7 14 7 23 10 6 | 18 22 25 24 31 23 21
R11 | 2049 8 9 13 10 14 --- 6 | 30 31 42 32 34 --- 32
R12 | 1163 7 10 13 22 16 16 8 | 29 38 41 47 34 44 36
R13 | 776 31 37 31 50 12 53 21 | 40 49 45 45 38 37 37
R14 | 764 7 10 12 13 24 8 6 | 36 38 31 39 42 31 35
R15 | 1445 13 12 13 9 24 26 7 | 38 41 52 42 45 33 42
R16 | 1370 17 20 19 20 11 14 11 | 41 59 55 42 47 47 46
R17 | 856 15 19 10 18 19 --- 9 | 40 42 32 36 32 --- 35
R18 | 1371 10 22 13 12 16 16 8 | 35 44 36 34 34 32 35
R19 | 1143 23 77 43 33 29 49 26 | 57 32 70 53 55 29 50
R20 | 2827 46 83 40 70 57 95 34 | 62 45 35 67 52 34 43
R21 | 1187 14 14 18 14 17 19 8 | 42 43 48 48 39 37 44
R22 | 2804 12 9 12 14 18 10 7 | 31 34 33 38 37 30 32
R24 | 1324 21 14 9 15 19 7 9 | 33 40 40 48 42 42 37
XR25 |10383 9 16 --- --- 26 --- 12 | 21 31 --- --- 38 --- 23
------+-----------------------------------------+-------------------------------------
RMS | 1518 18 31 21 25 24 32 |T 49 51 54 55 51 47 49
WRMS | 1518 16 22 14 17 20 32 |NE 40 42 45 45 43 34 39
MEDI | 1187 12 16 13 15 19 16 |MD 40 43 48 48 42 37 42
Table 3.2272.2 GPS week: 2272 Day: 2 MJD: 60150
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 769 31 43 39 21 48 36 19 | 49 79 76 56 43 39 57
R02 | 1894 12 21 23 14 20 --- 10 | 36 39 39 44 35 --- 36
R03E | 1217 17 13 14 18 10 12 9 | 57 53 55 59 49 52 54
R04E | 861 15 17 14 14 25 18 8 | 47 47 43 51 58 49 46
R05E | 1687 10 12 14 16 23 22 7 | 32 31 33 31 38 32 29
R07E | 942 16 19 18 14 19 17 9 | 32 39 36 38 35 33 33
R08E | 2797 15 12 14 14 15 13 8 | 33 32 37 42 32 29 34
R09 | 1336 7 8 14 12 12 16 6 | 16 16 20 22 16 21 16
R11 | 1903 13 9 8 12 27 10 6 | 29 38 39 31 20 31 32
R12 | 1732 14 12 17 9 20 19 7 | 26 24 34 22 28 33 23
R13 | 1307 26 24 23 13 30 62 12 | 41 38 43 45 56 51 35
R14 | 913 5 9 11 14 14 13 6 | 27 27 25 39 25 26 29
R15 | 1639 13 19 28 18 38 19 11 | 33 39 30 43 19 25 34
R16 | 875 20 14 20 17 18 13 10 | 39 42 52 28 39 33 37
R17 | 1086 13 13 14 7 17 --- 7 | 46 39 35 50 35 --- 42
R18 | 1224 7 26 32 9 16 15 11 | 35 39 21 41 26 27 32
R19 | 1214 39 72 30 18 30 35 24 | 84 48 79 64 64 53 66
R20 | 1970 40 75 49 43 31 87 29 | 78 50 102 63 69 64 70
R21 | 1589 9 14 16 13 14 19 7 | 55 52 61 52 52 44 53
R22 | 3092 14 11 15 16 23 15 8 | 40 42 46 48 39 52 42
R24 | 937 17 18 18 10 18 26 9 | 50 48 35 51 33 31 44
XR25 |11262 10 17 --- --- 32 --- 13 | 24 29 --- --- 47 --- 24
------+-----------------------------------------+-------------------------------------
RMS | 1594 19 28 23 17 24 31 |T 41 40 44 43 39 38 39
WRMS | 1594 15 24 19 13 22 31 |NE 41 38 44 42 37 37 38
MEDI | 1307 14 14 17 14 20 18 |MD 36 39 39 44 35 33 35
Table 3.2272.3 GPS week: 2272 Day: 3 MJD: 60151
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 923 21 37 40 21 50 37 17 | 47 50 80 59 48 42 54
R02 | 1338 10 18 13 10 16 --- 7 | 44 43 42 48 39 --- 43
R03E | 1101 12 14 14 16 21 14 8 | 84 81 80 82 76 78 81
R04E | 1025 12 19 15 15 22 23 8 | 46 39 47 45 45 37 43
R05E | 1636 9 12 14 11 21 19 6 | 41 41 44 45 49 42 42
R07E | 855 7 18 14 17 21 14 8 | 44 44 49 50 49 47 44
R08E | 1641 11 16 23 16 20 19 10 | 58 50 59 61 49 50 55
R09 | 1870 13 10 11 13 20 17 7 | 28 28 35 25 30 29 26
R11 | 1590 15 16 18 12 21 11 9 | 37 30 26 34 30 30 30
R12 | 1521 9 13 12 12 21 12 6 | 36 37 39 37 42 35 35
R13 | 1425 25 25 42 44 32 53 20 | 57 37 52 46 67 52 46
R14 | 847 9 9 10 11 19 13 5 | 36 37 30 33 44 33 32
R15 | 1567 11 19 18 23 30 15 10 | 43 44 43 55 35 47 44
R16 | 601 15 17 14 12 30 10 8 | 48 53 51 40 60 47 46
R17 | 827 11 13 13 9 25 --- 6 | 63 61 55 66 51 --- 61
R18 | 945 6 30 21 10 17 19 10 | 45 62 39 47 40 47 46
R19 | 1210 34 86 36 40 26 45 28 | 93 45 94 81 83 61 77
R20 | 1587 49 93 37 47 38 73 33 | 93 49 79 65 49 52 67
R21 | 1793 13 17 11 19 17 27 9 | 64 53 64 53 52 43 58
R22 | 3158 12 18 11 17 11 15 8 | 44 44 44 54 38 46 44
R24 | 849 14 23 18 20 30 37 10 | 62 59 62 69 48 42 61
XR25 |12030 6 15 --- --- 32 --- 11 | 35 44 --- --- 40 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1454 18 33 22 22 26 30 |T 52 46 53 52 48 45 48
WRMS | 1454 13 26 16 18 23 30 |NE 51 45 50 50 46 43 47
MEDI | 1338 12 17 14 16 21 19 |MD 45 44 49 50 48 46 44
Table 3.2272.4 GPS week: 2272 Day: 4 MJD: 60152
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 879 25 30 44 40 58 47 20 | 51 50 74 55 47 51 50
R02 | 1018 9 13 10 15 14 --- 7 | 40 41 36 44 34 --- 39
R03E | 1663 10 15 11 9 18 19 6 | 44 52 46 54 37 44 47
R04E | 1102 16 14 14 16 18 18 8 | 50 46 46 48 54 45 46
R05E | 1341 13 17 11 18 19 28 8 | 38 36 37 45 39 36 37
R07E | 912 13 14 11 12 11 13 7 | 36 35 35 38 33 35 34
R08E | 1385 11 15 15 18 18 19 8 | 43 49 46 52 37 45 45
R09 | 1555 8 8 11 10 32 24 5 | 23 25 30 27 28 24 25
R11 | 1153 10 13 12 11 20 12 7 | 31 31 25 34 29 30 28
R12 | 914 11 21 14 13 16 18 8 | 28 31 15 32 28 27 23
R13 | 1334 28 33 29 52 21 62 21 | 46 38 37 24 31 43 33
R14 | 694 9 12 12 13 14 22 6 | 32 26 37 27 37 36 30
R15 | 1594 15 15 18 17 14 32 9 | 34 28 23 34 33 51 28
R16 | 804 19 12 15 12 23 31 9 | 40 41 40 38 42 55 37
R17 | 845 14 16 12 13 19 --- 8 | 54 45 55 51 41 --- 51
R18 | 878 8 29 27 13 26 23 12 | 36 50 25 47 26 26 36
R19 | 1859 33 90 29 36 25 45 28 | 85 32 77 80 62 61 67
R20 | 1263 59 99 25 53 43 66 35 | 87 44 64 56 51 46 57
R21 | 1246 11 23 15 16 19 25 9 | 51 42 59 47 38 35 49
R22 | 3076 14 13 20 24 13 14 10 | 29 35 51 40 36 39 36
R24 | 1146 22 15 15 23 23 26 11 | 61 41 45 46 37 33 46
XR25 |15734 10 20 --- --- 27 --- 15 | 31 37 --- --- 20 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1367 21 34 19 24 24 32 |T 44 38 43 43 37 40 39
WRMS | 1367 15 24 16 20 19 32 |NE 44 36 41 41 35 38 38
MEDI | 1153 13 15 15 16 19 24 |MD 40 38 40 45 37 39 37
Table 3.2272.5 GPS week: 2272 Day: 5 MJD: 60153
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 869 19 40 43 33 53 37 20 | 85 86 111 85 86 88 88
R02 | 1586 10 12 9 12 19 --- 6 | 56 56 57 64 52 --- 58
R03E | 1473 15 19 11 12 19 18 8 | 52 48 50 54 50 50 50
R04E | 822 12 15 11 12 18 14 7 | 70 69 66 79 67 69 71
R05E | 855 11 14 16 17 20 16 8 | 54 60 62 57 64 62 56
R07E | 694 13 17 12 14 25 16 8 | 44 48 48 49 40 45 45
R08E | 1236 15 17 11 15 16 23 8 | 41 42 39 47 39 41 40
R09 | 1853 19 15 17 7 16 11 8 | 21 18 16 18 18 13 12
R11 | 1176 8 20 13 12 15 16 7 | 24 33 24 26 23 23 24
R12 | 645 19 9 15 8 20 16 8 | 22 28 33 24 22 20 24
R13 | 1386 23 36 17 29 36 62 15 | 38 41 34 23 24 43 30
R14 | 948 9 9 10 14 22 10 6 | 26 33 31 24 32 29 27
R15 | 2001 12 17 10 8 16 14 6 | 27 26 34 23 35 25 26
R16 | 1405 19 19 13 9 23 23 9 | 30 39 28 32 36 38 27
R17 | 1141 9 23 13 12 11 --- 8 | 46 33 52 49 44 --- 45
R18 | 966 6 27 23 13 21 19 10 | 32 39 30 38 26 27 32
R19 | 1000 41 94 49 41 29 70 31 | 73 27 76 55 51 38 56
R20 | 1947 42 104 42 33 43 83 32 | 82 64 90 80 67 84 73
R21 | 890 15 23 15 13 18 29 9 | 43 44 36 47 44 30 40
R22 | 3055 12 8 14 15 24 9 7 | 28 29 33 31 33 29 28
R24 | 1175 22 13 11 16 11 11 9 | 48 38 32 35 34 35 36
XR25 |16303 1 --- --- --- 34 --- 0 | 31 --- --- --- 21 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1404 19 36 21 19 25 33 |T 44 42 46 44 41 41 41
WRMS | 1404 16 25 13 15 21 33 |NE 39 36 40 37 35 33 35
MEDI | 1175 13 17 13 13 20 16 |MD 41 39 36 47 36 38 36
Table 3.2272.6 GPS week: 2272 Day: 6 MJD: 60154
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 911 19 35 26 22 45 52 14 | 100 101 109 106 93 94 101
R02 | 1237 9 11 11 16 22 --- 7 | 65 69 70 69 63 --- 67
R03E | 1999 16 17 9 9 14 13 7 | 49 54 53 58 49 53 52
R04E | 2012 12 12 13 15 23 17 7 | 90 90 93 100 89 98 92
R05E | 1305 8 14 14 13 17 20 7 | 71 74 69 74 73 78 70
R07E | 1210 12 13 12 17 11 16 8 | 56 49 57 58 49 55 54
R08E | 1299 14 14 20 16 14 15 9 | 47 45 45 49 41 46 45
R09 | 935 16 17 10 10 18 20 8 | 27 23 23 24 19 28 22
R11 | 1146 16 17 12 7 17 18 7 | 34 29 25 32 26 26 28
R12 | 614 16 10 19 9 27 25 8 | 35 42 49 40 32 35 39
R13 | 1174 16 32 21 38 31 52 16 | 59 56 51 48 48 46 51
R14 | 488 7 13 21 10 16 19 7 | 41 46 40 43 42 48 40
R15 | 1510 10 15 12 8 29 12 6 | 47 54 44 50 41 46 47
R16 | 1199 16 13 17 11 12 13 8 | 51 60 60 49 55 56 53
R17 | 1323 19 11 13 17 14 --- 9 | 73 58 58 63 61 --- 62
R18 | 1028 7 33 23 17 23 14 11 | 50 69 41 56 43 44 50
R19 | 922 20 75 44 30 32 54 25 | 110 49 118 89 86 68 92
R20 | 2145 45 105 55 55 39 77 37 | 109 68 110 93 81 67 88
R21 | 1450 13 15 9 8 19 27 6 | 76 67 75 72 71 51 72
R22 | 3001 13 10 10 12 19 13 6 | 45 48 51 47 52 46 46
R24 | 1503 16 25 15 24 14 23 11 | 65 64 57 63 61 51 60
XR25 |17788 10 21 --- --- 15 --- 15 | 35 40 --- --- 32 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1460 17 33 21 21 23 32 |T 60 57 61 61 54 54 57
WRMS | 1460 15 19 15 18 21 32 |NE 57 52 58 55 50 47 53
MEDI | 1237 14 15 14 15 18 19 |MD 51 54 57 58 49 51 52
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