[IGSREPORT-29333] Wk 2261 IGLOS Final Orbits
acc
acc at igs.org
Mon May 29 09:23:50 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2261 (May 07, 2023 - May 13, 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 2.2261.
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:
igl2261[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2261 in the SP3 format.
igl22617.sum Combination Report for GPS Week 2261.
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. 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.
3. 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).
4. 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
5. 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 | -0.4 ns
2 | 0.4 ns
3 | 0.4 ns
4 | -0.6 ns
5 | -1.8 ns
6 | 1.7 ns
6. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESA | R20 R22
1 | ESA | R20 R22
2 | ESA | R20 R22
3 | ESA | R20 R22
4 | ESA | R20 R22
5 | ESA | R20 R22
6 | ESA | R20 R22
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 1.2261, 1a.2261).
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 2.2261.0-6)
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 3.2261.0-6).
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 2261 summary. (May 07, 2023 - May 13, 2023)
Table 1.2261.a GPS week : 2261 MJD: 60071.0-60077.0
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 1 0 -8 7 .03 19 16 | 43783 604 3366 9114
| 0 1 1 15 15 16 .02 | 1184 2123
esa n/a| 0 0 2 11 -7 -19 -.09 47 25 | -99 1018 3439 7863
| 0 0 2 13 17 31 .04 | 4349 2064
gfz n/a| 0 0 -3 32 -8 -35 -.07 23 15 | 0 479 3417 8797
| 0 1 1 12 14 29 .05 | 0 2211
grg n/a| 1 0 0 -51 25 31 .14 23 19 | -307 480 3420 8119
| 1 1 2 21 16 56 .03 | 277 1970
iac n/a| -1 -1 -2 8 39 -40 -.20 25 22 | 2055 139 3347 9304
| 2 2 1 19 41 88 .08 | 667 1052
Table 1.2261.b GPS week : 2261 MJD: 60071.0-60077.0
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 17 16 18 20 19 18 |
R02 | 6 7 5 7 6 7 6 |
R03 | 8 7 8 6 10 6 7 |
R04 | 12 8 8 5 9 7 7 |
R05 | 7 8 7 6 6 9 10 |
R07 | 8 8 12 7 7 6 8 |
R08 | 9 10 7 5 7 10 8 |
R09 | 9 9 9 9 9 9 11 |
R11 | 9 8 8 8 8 6 9 |
R12 | 8 12 11 11 12 9 10 |
R13 | 24 16 21 24 21 16 17 |
R14 | 10 8 9 8 7 10 8 |
R15 | 9 8 10 9 11 9 7 |
R16 | 17 20 17 19 20 22 23 |
R17 | 9 9 7 8 10 10 8 |
R18 | 8 8 9 7 8 10 9 |
R19 | 25 24 23 21 23 24 27 |
R20 | 24 19 25 25 28 24 24 |
R21 | 11 13 10 8 10 12 13 |
R22 | 12 16 17 11 19 15 9 |
R24 | 11 11 12 9 10 9 12 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2261.c GPS week : 2261 MJD: 60071.0-60077.0
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 2261 0 | 7 -44 270 -28 -443 -3549 79.9 1710 1710 | 1140 0
brd 2261 1 | -39 49 279 -446 273 -3803 82.8 1520 1520 | -354 0
brd 2261 2 | 0 57 286 -63 577 2886 82.2 1539 1539 | 436 0
brd 2261 3 | 15 -46 177 969 -500 2309 83.2 1824 1824 | 388 0
brd 2261 4 | -59 -47 179 -551 915 2744 78.9 2152 2152 | -577 0
brd 2261 5 | -17 -58 106 384 365 2432 80.5 2045 2045 | -1848 0
brd 2261 6 | 58 -25 167 -725 373 740 79.9 1918 1918 | 1670 0
-------------+------------------------------------------------------------+----------------
brd 2261 mean| -5 -16 209 -65 222 537 81.1 1815 1815 | 122 0
brd 2261 sdev| 38 48 69 590 519 2963 1.7 242 242 | 1168 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 2.2261.0 GPS week: 2261 Day: 0 MJD: 60071
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 2 0 8 -21 22 .04 19 15 | 43085 1578 3740 9100
esa n/a| 0 -1 1 -4 3 -44 -.04 53 31 | 3340 2564 3706 8356
gfz n/a| 0 0 -6 23 -3 1 -.02 24 18 | 0 2146 3589 8673
grg n/a| 0 -1 4 -43 35 -4 .08 22 18 | -88 1878 3718 8288
iac n/a| -2 0 -2 -20 60 1 -.13 23 21 | 2448 1314 3414 9124
Table 2.2261.1 GPS week: 2261 Day: 1 MJD: 60072
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 0 27 -1 -23 .03 20 16 | 42332 800 2929 8952
esa n/a| 0 0 4 33 -19 -43 -.07 53 28 | -6341 716 3141 8679
gfz n/a| 0 1 -3 33 -14 -31 -.05 21 17 | 0 -36 3189 8541
grg n/a| 0 -1 0 -77 40 72 .14 21 18 | -730 419 3160 7644
iac n/a| -5 2 -1 32 18 -132 -.19 26 23 | 1548 520 3107 9044
Table 2.2261.2 GPS week: 2261 Day: 2 MJD: 60073
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 3 1 -10 20 .02 19 16 | 43637 735 2989 8658
esa n/a| 0 0 3 19 10 -43 -.10 46 25 | 1299 1193 3042 7959
gfz n/a| 0 0 -4 36 1 -59 -.11 22 16 | 0 1281 3013 8215
grg n/a| 1 -1 -4 -76 16 78 .18 24 20 | -100 795 2995 7499
iac n/a| -1 0 -2 5 16 15 -.14 25 23 | 2055 -425 2985 8786
Table 2.2261.3 GPS week: 2261 Day: 3 MJD: 60074
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 3 -2 -4 8 .05 18 13 | 45060 1286 3546 8276
esa n/a| 0 0 2 -4 -25 -5 -.09 47 25 | -5844 1188 3693 7014
gfz n/a| -1 -1 -4 52 -23 -36 -.14 26 14 | 0 755 3671 8234
grg n/a| 2 1 -1 -53 40 16 .17 20 15 | -57 496 3653 7754
iac n/a| 1 -3 -1 3 45 -172 -.22 25 23 | 2535 -482 3621 8612
Table 2.2261.4 GPS week: 2261 Day: 4 MJD: 60075
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 0 0 -26 -5 .00 20 16 | 45710 -800 3667 9090
esa n/a| 0 0 0 19 16 -43 -.09 45 19 | 599 382 3681 5722
gfz n/a| 0 0 -2 40 -24 -80 -.08 24 14 | 0 -354 3665 9073
grg n/a| 2 1 0 -55 36 108 .14 25 20 | -462 -336 3669 8328
iac n/a| 0 -4 0 0 32 76 -.32 29 25 | 2049 545 3629 9635
Table 2.2261.5 GPS week: 2261 Day: 5 MJD: 60076
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 -23 -12 10 .05 19 17 | 43167 -3109 3442 9975
esa n/a| -1 0 5 4 -7 21 -.09 44 27 | 1323 -2787 3473 9723
gfz n/a| 0 -1 -1 30 15 -1 -.10 20 11 | 0 -3678 3479 9771
grg n/a| 0 1 -1 -25 2 -51 .13 25 22 | -583 -3124 3470 9004
iac n/a| 0 -3 -4 1 -13 -2 -.13 22 23 | 885 -1654 3444 10165
Table 2.2261.6 GPS week: 2261 Day: 6 MJD: 60077
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 -3 21 21 .01 20 20 | 43493 3738 3255 9750
esa n/a| 0 0 0 11 -26 20 -.17 42 24 | 4925 3872 3339 7593
gfz n/a| 0 -1 -2 11 -13 -43 -.01 24 15 | 0 3239 3315 9075
grg n/a| 0 1 -1 -26 4 5 .16 23 21 | -131 3235 3278 8320
iac n/a| -3 0 -4 36 118 -68 -.29 22 20 | 2869 1159 3235 9767
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 3.2261.0 GPS week: 2261 Day: 0 MJD: 60071
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 621 25 37 27 38 25 18 | 72 39 56 67 63 57
R02 | 541 9 12 11 10 24 6 | 49 48 45 49 52 47
R03 | 627 11 11 9 19 24 7 | 46 52 49 57 47 50
R04 | 686 27 29 8 9 18 12 | 47 47 39 37 31 39
R05 | 915 10 16 10 7 16 6 | 34 36 35 33 30 33
R07 | 2723 8 10 17 17 28 8 | 55 54 63 62 63 56
R08 | 682 15 9 18 18 22 9 | 47 64 66 64 63 59
R09E | 3827 13 13 14 20 17 9 | 69 79 76 74 77 73
R11E | 2433 15 15 14 18 18 9 | 46 49 49 50 51 46
R12E | 861 9 14 11 19 12 8 | 202 198 201 201 199 200
R13E | 1066 25 39 63 28 40 23 | 64 51 115 65 64 70
R14E | 1211 15 17 12 21 17 9 | 78 79 78 83 77 78
R15E | 932 9 14 13 21 22 8 | 71 68 71 71 73 69
R16E | 876 21 18 43 24 23 16 | 64 67 76 78 62 66
R17 | 878 9 24 17 10 22 9 | 93 86 100 91 105 92
R18 | 602 10 17 12 13 24 7 | 77 93 88 85 89 85
R19 | 812 44 57 29 42 36 25 | 128 76 113 104 103 105
R20 | 3186 37 215 34 29 29 24 | 160 62 172 174 155 166
R21 | 685 7 25 20 18 18 10 | 88 68 100 88 90 85
XR22 | 3287 --- 334 11 11 15 11 | --- 145 59 56 52 56
R24 | 3204 10 28 22 11 18 11 | 103 90 113 106 113 102
XR25 |17156 2 --- --- --- 31 0 | 52 --- --- --- 54 52
------+------------------------------------+--------------------------------
RMS | 1710 19 53 24 22 23 |T 78 73 84 80 77 76
WRMS | 1710 15 31 18 18 21 |NE 75 68 78 76 74 72
MEDI | 878 11 17 14 18 22 |MD 69 67 76 71 63 66
Table 3.2261.1 GPS week: 2261 Day: 1 MJD: 60072
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 918 27 27 23 37 16 17 | 59 50 56 60 51 54
R02 | 582 8 12 12 15 19 7 | 41 51 48 39 43 43
R03 | 613 16 14 9 8 12 7 | 39 51 51 46 42 46
R04 | 757 14 11 16 12 24 8 | 44 44 40 49 36 42
R05 | 980 14 16 12 7 18 7 | 36 33 39 40 38 35
R07 | 1991 16 14 9 17 35 8 | 50 62 63 64 68 59
R08 | 815 24 13 18 10 27 10 | 44 62 67 52 52 55
R09E | 3310 16 13 12 17 15 8 | 41 45 47 38 46 40
R11E | 2762 13 13 14 14 20 8 | 27 30 29 30 33 26
R12E | 661 14 19 17 28 21 11 | 161 169 167 161 157 164
R13E | 1113 30 26 31 24 35 16 | 62 57 64 57 52 57
R14E | 953 12 11 9 18 21 7 | 50 56 52 64 48 54
R15E | 1035 11 11 12 20 21 8 | 66 61 66 65 61 63
R16E | 891 24 27 55 21 26 20 | 46 48 59 54 41 46
R17 | 875 7 19 19 14 26 9 | 49 50 64 59 62 54
R18 | 736 10 10 16 14 11 7 | 47 50 56 49 49 50
R19 | 755 46 43 22 51 25 24 | 74 52 63 57 48 60
R20 | 3124 30 220 27 22 54 19 | 82 38 96 97 64 89
R21 | 982 8 32 26 14 27 12 | 49 40 55 50 56 47
XR22 | 3215 --- 332 15 15 31 15 | --- 103 44 59 29 48
R24 | 1678 10 25 18 16 32 10 | 50 50 60 63 56 54
XR25 |18295 2 --- --- --- 27 0 | 41 --- --- --- 44 42
------+------------------------------------+--------------------------------
RMS | 1519 20 53 21 21 26 |T 55 57 61 59 53 55
WRMS | 1519 16 28 17 18 23 |NE 50 52 57 56 49 51
MEDI | 953 14 16 16 16 24 |MD 49 50 56 57 48 50
Table 3.2261.2 GPS week: 2261 Day: 2 MJD: 60073
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1141 27 29 19 32 20 15 | 64 46 67 44 61 54
R02 | 527 6 9 8 7 11 4 | 39 42 42 41 38 40
R03 | 1074 16 6 8 19 20 7 | 34 40 47 55 51 43
R04 | 614 12 8 20 13 17 8 | 29 38 44 30 36 33
R05 | 906 14 12 11 11 19 7 | 23 34 24 25 16 24
R07 | 937 12 14 24 31 23 12 | 37 30 33 50 35 33
R08 | 958 13 12 8 13 23 7 | 30 39 29 34 42 32
R09E | 3941 15 14 11 21 15 9 | 54 61 56 47 56 53
R11E | 2489 13 10 16 17 11 8 | 34 41 48 36 35 38
R12E | 667 12 12 24 25 27 11 | 117 114 115 108 113 113
R13E | 2863 29 35 42 40 41 21 | 56 64 73 69 58 60
R14E | 974 17 14 14 16 16 9 | 58 59 61 65 57 59
R15E | 806 12 12 19 26 18 10 | 89 93 98 92 87 91
R16E | 992 20 22 47 19 22 17 | 58 57 66 63 52 59
R17 | 1317 11 15 10 13 24 7 | 66 67 63 73 73 66
R18 | 664 19 11 10 19 12 9 | 59 72 73 82 66 69
R19 | 1214 37 47 15 50 30 23 | 89 72 80 80 69 78
R20 | 1165 30 190 39 33 54 24 | 104 66 133 130 102 119
R21 | 1120 13 20 18 12 17 9 | 62 52 66 58 62 58
XR22 | 2770 --- 331 15 17 15 16 | --- 133 44 34 37 35
R24 | 1546 16 20 25 21 33 12 | 62 63 85 81 85 70
XR25 |14856 2 --- --- --- 33 0 | 49 --- --- --- 56 50
------+------------------------------------+--------------------------------
RMS | 1538 19 46 22 24 25 |T 57 61 64 61 58 58
WRMS | 1538 16 25 16 20 23 |NE 53 56 59 58 55 53
MEDI | 1074 14 14 16 19 20 |MD 58 59 63 58 56 54
Table 3.2261.3 GPS week: 2261 Day: 3 MJD: 60074
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1057 29 34 28 32 22 18 | 70 40 62 48 51 54
R02 | 573 10 10 13 11 23 6 | 50 56 60 48 59 52
R03 | 963 11 12 8 8 21 6 | 51 48 45 50 58 48
R04 | 739 8 6 8 10 11 5 | 42 39 39 37 35 38
R05 | 836 12 8 9 6 17 5 | 38 41 38 37 31 38
R07 | 1177 8 13 8 17 18 7 | 43 38 38 51 35 42
R08 | 1149 9 6 10 10 18 5 | 40 42 39 42 41 40
R09E | 5361 15 13 21 11 16 9 | 58 59 67 54 52 57
R11E | 2478 12 14 14 16 16 8 | 43 49 47 38 43 42
R12E | 824 13 20 14 25 25 11 | 79 81 79 87 80 79
R13E | 1346 29 30 67 32 51 23 | 70 76 100 78 66 69
R14E | 1639 12 12 11 17 23 7 | 65 68 65 68 64 65
R15E | 1538 14 13 11 19 22 8 | 101 102 105 114 101 105
R16E | 971 26 21 58 16 26 19 | 70 69 81 76 64 71
R17 | 1652 9 17 13 10 27 7 | 80 76 86 86 93 81
R18 | 739 15 12 10 10 23 7 | 72 83 82 85 80 79
R19 | 1143 38 37 18 42 17 20 | 107 81 97 94 85 94
R20 | 2314 27 195 44 35 45 25 | 142 65 148 137 128 138
R21 | 906 10 19 16 7 21 8 | 82 73 89 82 90 80
XR22 | 2990 --- 324 12 9 20 11 | --- 156 58 68 48 61
R24 | 2461 10 22 15 13 25 9 | 84 77 89 91 94 84
XR25 |14430 2 --- --- --- 37 0 | 40 --- --- --- 54 40
------+------------------------------------+--------------------------------
RMS | 1823 18 47 26 20 25 |T 67 67 72 70 66 66
WRMS | 1823 13 25 14 15 23 |NE 67 65 69 68 65 64
MEDI | 1149 12 14 13 13 22 |MD 70 68 67 68 59 61
Table 3.2261.4 GPS week: 2261 Day: 4 MJD: 60075
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1051 45 39 16 23 50 19 | 58 25 32 41 62 33
R02 | 871 12 10 8 11 27 6 | 39 35 40 42 55 38
R03 | 1182 22 14 15 12 15 9 | 40 62 63 49 60 53
R04 | 634 12 13 16 20 24 9 | 35 41 48 30 37 36
R05 | 649 13 7 11 9 37 6 | 33 32 29 33 39 30
R07 | 2428 12 7 11 18 24 7 | 33 36 42 44 39 36
R08 | 1470 11 9 14 14 33 7 | 28 28 39 40 49 32
R09E | 6315 14 10 19 17 19 9 | 47 58 62 54 64 54
R11E | 2590 10 11 13 19 12 7 | 36 39 47 48 45 41
R12E | 880 14 13 17 33 26 11 | 133 136 136 114 125 129
R13E | 1083 28 28 51 27 37 20 | 45 52 96 49 49 56
R14E | 918 9 12 13 15 19 7 | 58 57 53 69 61 58
R15E | 816 10 15 16 29 15 10 | 78 79 87 71 76 77
R16E | 1180 28 23 53 21 31 20 | 57 59 71 72 57 62
R17 | 2079 13 17 15 22 24 10 | 64 62 63 60 71 61
R18 | 681 12 15 12 11 26 7 | 55 65 61 64 71 60
R19 | 991 41 39 15 57 21 23 | 93 63 79 84 78 77
R20 | 949 21 184 48 44 46 28 | 110 75 118 126 105 114
R21 | 1270 13 22 13 19 20 10 | 70 64 71 77 74 69
XR22 | 3683 --- 325 17 20 17 19 | --- 122 47 46 47 45
R24 | 4549 15 16 16 19 41 9 | 67 60 71 59 79 63
XR25 |11008 2 --- --- --- 31 0 | 31 --- --- --- 49 31
------+------------------------------------+--------------------------------
RMS | 2151 20 45 24 25 29 |T 57 59 64 60 63 57
WRMS | 2151 16 19 14 20 25 |NE 54 55 57 56 61 51
MEDI | 1083 13 15 15 19 24 |MD 55 59 62 54 60 54
Table 3.2261.5 GPS week: 2261 Day: 5 MJD: 60076
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1115 31 48 24 24 12 19 | 59 50 63 67 53 58
R02 | 820 10 10 13 10 23 6 | 45 44 46 51 45 45
R03 | 1330 10 13 8 10 9 6 | 46 49 42 45 43 44
R04 | 579 11 13 7 18 11 7 | 45 43 42 41 43 41
R05 | 860 12 15 11 19 13 8 | 50 49 41 40 43 44
R07 | 2485 9 9 8 15 10 6 | 44 50 46 55 44 47
R08 | 2327 23 12 16 10 17 9 | 47 57 60 58 51 55
R09E | 5894 18 15 13 10 17 8 | 35 42 40 32 42 36
R11E | 2894 11 7 12 10 17 6 | 28 30 33 29 31 30
R12E | 1602 13 16 10 25 22 9 | 154 156 151 163 161 155
R13E | 677 22 28 32 22 27 15 | 55 72 76 62 64 63
R14E | 988 15 13 10 26 21 9 | 50 51 46 67 49 51
R15E | 1034 12 14 10 26 25 9 | 70 65 72 77 71 70
R16E | 818 24 33 54 29 30 22 | 49 45 78 60 51 55
R17 | 1758 17 13 9 27 26 9 | 53 52 50 65 47 53
R18 | 642 9 21 7 26 23 9 | 43 45 39 50 41 41
R19 | 1088 43 36 16 63 36 23 | 50 57 55 60 64 52
R20 | 1172 21 174 40 38 32 24 | 78 56 61 75 69 67
R21 | 1099 12 29 19 22 16 12 | 60 53 60 76 64 61
XR22 | 4201 --- 343 13 17 22 15 | --- 87 31 45 37 34
R24 | 3348 18 16 12 15 29 9 | 62 62 55 75 65 62
XR25 |11496 1 --- --- --- 39 0 | 37 --- --- --- 55 37
------+------------------------------------+--------------------------------
RMS | 2045 19 44 20 25 22 |T 55 57 56 61 56 54
WRMS | 2045 17 27 11 22 23 |NE 51 53 49 57 50 49
MEDI | 1115 13 15 12 22 22 |MD 50 51 50 60 49 51
Table 3.2261.6 GPS week: 2261 Day: 6 MJD: 60077
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 953 28 38 23 33 24 18 | 77 43 60 69 66 61
R02 | 936 11 10 10 12 21 6 | 53 50 49 55 60 51
R03 | 755 9 12 10 15 12 7 | 58 59 61 63 59 59
R04 | 603 14 12 13 10 24 7 | 53 45 52 47 45 49
R05 | 1623 17 21 14 19 18 10 | 51 53 50 40 45 47
R07 | 1505 11 8 20 13 35 8 | 55 55 56 64 63 56
R08 | 2245 16 12 14 13 17 8 | 52 63 69 63 67 61
R09E | 5583 14 12 21 23 13 10 | 54 65 66 61 62 59
R11E | 3160 15 11 18 17 15 9 | 35 41 46 33 36 38
R12E | 1277 13 16 11 27 28 10 | 217 214 215 227 215 218
R13E | 1596 26 24 40 17 32 16 | 56 60 86 64 68 62
R14E | 1359 11 18 12 15 11 8 | 59 60 60 68 57 60
R15E | 854 11 12 8 13 19 6 | 70 68 74 82 76 73
R16E | 1192 25 24 63 28 20 22 | 63 59 96 69 59 69
R17 | 2066 12 15 7 17 12 7 | 94 89 92 86 99 90
R18 | 833 11 18 12 18 18 8 | 78 92 90 90 89 86
R19 | 912 49 49 26 57 19 27 | 120 75 107 110 102 102
R20 | 1825 26 163 42 29 36 23 | 160 58 166 176 156 165
R21 | 765 10 29 14 28 16 12 | 98 79 103 109 106 96
XR22 | 4063 --- 327 8 8 14 8 | --- 106 58 58 59 57
R24 | 1356 25 24 14 11 24 11 | 102 89 97 104 110 97
XR25 |12346 2 --- --- --- 26 0 | 50 --- --- --- 67 51
------+------------------------------------+--------------------------------
RMS | 1917 20 42 24 23 22 |T 78 72 83 82 80 77
WRMS | 1917 20 24 15 21 20 |NE 78 68 79 81 79 75
MEDI | 1356 14 18 14 17 19 |MD 59 60 69 68 66 61
More information about the IGSREPORT
mailing list