[IGSREPORT-29237] Wk 2252 IGLOS Final Orbits
acc
acc at igs.org
Fri Mar 24 07:58:51 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2252 (Mar 05, 2023 - Mar 11, 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 2.2252.
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:
igl2252[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2252 in the SP3 format.
igl22527.sum Combination Report for GPS Week 2252.
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 | 0.1 ns
1 | -19.3 ns
2 | -14.2 ns
3 | -0.9 ns
4 | 0.3 ns
5 | -14.0 ns
6 | 0.7 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 | R22
1 | ESA | R22
2 | ESA | R22
3 | ESA | R22
4 | ESA | R22
5 | ESA | R22
6 | ESA | 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 1.2252, 1a.2252).
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 2.2252.0-6)
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 3.2252.0-6).
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 2252 summary. (Mar 05, 2023 - Mar 11, 2023)
Table 1.2252.a GPS week : 2252 MJD: 60008.0-60014.0
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 3 -4 -8 40 .05 18 13 | 28931 -1193 3075 8580
| 0 0 2 19 8 22 .05 | 8707 2048
esa n/a| 0 0 -3 -6 -11 -52 -.22 29 22 | -7979 -598 3044 7964
| 1 1 1 8 12 16 .05 | 7653 2573
gfz n/a| -1 1 1 32 -3 -24 -.14 28 21 | 0 -1203 3046 8400
| 1 0 1 18 23 19 .08 | 0 2427
grg n/a| 1 -1 -3 -19 20 19 .26 23 17 | -6191 -1279 3042 7850
| 1 0 2 21 18 37 .05 | 8037 2049
iac n/a| -1 2 -3 24 23 8 -.16 40 28 | 5356 -180 3044 9066
| 2 1 2 14 25 84 .07 | 8357 569
Table 1.2252.b GPS week : 2252 MJD: 60008.0-60014.0
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 | 24 21 17 17 17 15 20 |
R02 | 7 8 7 8 6 9 10 |
R03 | 7 8 10 7 7 7 5 |
R04 | 17 8 7 9 8 8 6 |
R05 | 6 8 7 8 11 6 8 |
R07 | 8 7 8 10 9 8 9 |
R08 | 7 7 8 9 9 9 7 |
R09 | 11 8 10 9 8 10 8 |
R11 | 11 9 8 7 8 8 7 |
R12 | 9 8 11 16 14 9 11 |
R13 | 16 19 14 19 13 16 16 |
R14 | 9 9 8 8 7 8 9 |
R15 | 8 7 8 10 6 8 9 |
R16 | 22 20 19 21 22 25 22 |
R17 | 11 10 8 8 7 8 9 |
R18 | 11 9 9 8 7 8 9 |
R19 | 29 20 24 23 20 22 16 |
R20 | 33 31 31 34 41 35 33 |
R21 | 7 7 8 8 6 9 9 |
R22 | 10 13 13 10 15 13 12 |
R24 | 13 14 11 11 12 12 9 |
Table 1.2252.c GPS week : 2252 MJD: 60008.0-60014.0
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 2252 0 | 16 24 108 -1288 -1541 4305 81.6 1436 1436 | 68 0
brd 2252 1 | 21 44 84 -1693 -1782 2776 80.1 1738 1738 | -19262 0
brd 2252 2 | 4 -41 124 -1436 -2029 -3918 81.4 1447 1447 | -14210 0
brd 2252 3 | -33 66 121 -1253 -660 4739 80.9 1795 1795 | -868 0
brd 2252 4 | 129 -6 84 -897 597 3503 79.1 1733 1733 | 252 0
brd 2252 5 | -51 71 105 -316 -568 6377 80.5 1380 1380 | -13967 0
brd 2252 6 | 74 41 80 642 204 3445 81.5 1335 1335 | 730 0
-------------+------------------------------------------------------------+----------------
brd 2252 mean| 23 28 101 -891 -825 3032 80.7 1552 1552 | -6751 0
brd 2252 sdev| 62 40 18 807 1004 3278 .9 194 194 | 8663 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 2.2252.0 GPS week: 2252 Day: 0 MJD: 60008
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 5 -1 -7 69 -.01 18 13 | 40470 -434 3496 9096
esa n/a| 0 -2 -2 -4 -12 -46 -.24 30 24 | 226 957 3357 8143
gfz n/a| -1 0 2 40 -6 -27 -.04 36 22 | 0 -521 3361 8879
grg n/a| 0 -1 -6 -41 6 -22 .20 22 16 | 10 -91 3337 8320
iac n/a| 0 3 -1 19 46 174 -.27 36 25 | 14392 -103 3323 9564
Table 2.2252.1 GPS week: 2252 Day: 1 MJD: 60009
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 2 -6 1 .08 16 11 | 20563 -4751 2760 8802
esa n/a| 1 0 -4 -6 4 -50 -.22 33 27 | -17496 -5609 2725 7985
gfz n/a| 0 0 3 0 15 -56 -.19 24 18 | 0 -5826 2726 8831
grg n/a| 0 -1 -6 4 5 94 .26 24 19 | -16773 -5264 2716 7926
iac n/a| -2 0 0 41 0 -76 -.05 36 27 | -5495 -1046 2734 9291
Table 2.2252.2 GPS week: 2252 Day: 2 MJD: 60010
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 5 -45 -10 58 -.00 17 12 | 21114 617 2910 8198
esa n/a| 2 0 -5 -9 -16 -50 -.24 29 24 | -17202 1888 2880 7244
gfz n/a| -2 2 0 47 25 -29 -.07 26 18 | 0 938 2884 7887
grg n/a| 0 -2 -2 15 11 2 .30 19 16 | -14264 274 2891 7671
iac n/a| 0 1 -3 24 37 4 -.16 36 26 | -1025 574 2901 8676
Table 2.2252.3 GPS week: 2252 Day: 3 MJD: 60011
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 1 -1 -13 34 .03 19 14 | 35726 -2626 2746 8276
esa n/a| 2 0 -2 -15 -17 -43 -.16 28 19 | -4499 -1923 2686 7146
gfz n/a| 0 2 3 45 13 6 -.10 27 20 | 0 -2149 2711 8123
grg n/a| 0 -1 -3 -28 10 24 .26 25 18 | 215 -2212 2687 7553
iac n/a| 2 2 -5 8 43 -22 -.15 39 36 | 13575 -303 2691 8907
Table 2.2252.4 GPS week: 2252 Day: 4 MJD: 60012
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 9 4 55 .05 21 16 | 34489 -119 2945 8677
esa n/a| 0 1 -2 -3 -12 -54 -.16 28 16 | 1194 969 2932 7282
gfz n/a| -1 0 1 46 -41 -32 -.15 24 17 | 0 218 2927 8579
grg n/a| 2 0 -3 -40 15 23 .26 26 17 | 316 -363 2930 7988
iac n/a| -1 1 -1 32 14 -37 -.16 41 25 | 13770 453 2916 9218
Table 2.2252.5 GPS week: 2252 Day: 5 MJD: 60013
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 -7 -22 36 .09 15 11 | 18604 -2030 2952 8145
esa n/a| -1 1 -3 8 3 -87 -.23 30 21 | -11273 -1117 3015 11136
gfz n/a| -2 2 2 28 -16 -20 -.28 29 29 | 0 -2145 3034 7898
grg n/a| 2 0 -3 -29 44 19 .31 25 16 | -13074 -1875 3022 7438
iac n/a| -2 3 -5 39 -16 -42 -.21 41 26 | -455 -636 3021 8641
Table 2.2252.6 GPS week: 2252 Day: 6 MJD: 60014
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 14 0 29 .14 18 13 | 31557 989 3722 8869
esa n/a| 0 1 -2 -15 -30 -37 -.28 24 20 | -6808 647 3719 6812
gfz n/a| 0 1 -1 15 -13 -15 -.16 29 20 | 0 1060 3685 8608
grg n/a| 2 0 1 -19 50 -7 .20 21 15 | 228 574 3715 8058
iac n/a| -3 2 -5 3 43 61 -.15 47 28 | 2730 -205 3725 9170
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 3.2252.0 GPS week: 2252 Day: 0 MJD: 60008
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 699 37 60 35 27 27 23 | 128 83 94 109 88 104
R02 | 1250 7 15 17 10 21 7 | 78 91 70 74 70 78
R03 | 723 7 17 8 14 14 7 | 95 86 91 102 95 94
R04 | 751 20 21 31 42 49 17 | 102 102 107 107 129 101
R05 | 2004 9 8 14 7 17 5 | 79 77 76 75 76 77
R07 | 1479 10 22 10 10 17 7 | 84 70 78 78 86 77
R08 | 1348 11 14 11 5 15 6 | 79 74 72 75 74 75
R09 | 1622 14 23 19 19 21 10 | 21 21 21 24 22 18
R11 | 754 9 21 26 17 14 10 | 24 22 42 37 38 28
R12 | 936 11 19 11 17 16 8 | 61 71 61 57 55 61
R13 | 886 9 28 30 40 25 16 | 69 69 71 70 82 68
R14 | 863 10 19 18 11 14 8 | 44 61 40 43 48 45
R15 | 1466 15 12 11 14 26 8 | 71 85 79 86 64 78
R16 | 1394 22 36 67 16 17 21 | 76 72 85 72 70 74
R17E | 1074 15 19 21 18 21 10 | 56 49 52 53 50 51
R18E | 759 10 16 22 23 14 10 | 29 27 26 40 30 27
R19E | 2731 32 50 80 35 50 28 | 51 51 97 50 80 52
R20E | 2775 40 68 88 24 123 32 | 93 98 112 88 140 89
R21E | 1153 8 14 10 13 18 6 | 28 26 30 38 35 29
XR22E | 3136 --- 317 11 8 16 9 | --- 128 41 37 37 37
R24E | 1473 11 21 20 31 20 12 | 28 37 36 41 35 29
------+------------------------------------+--------------------------------
RMS | 1436 18 30 36 22 36 |T 64 66 65 64 66 61
WRMS | 1436 13 24 22 16 25 |NE 72 70 70 72 71 69
MEDI | 1250 11 21 19 17 18 |MD 69 71 71 70 70 68
Table 3.2252.1 GPS week: 2252 Day: 1 MJD: 60009
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 542 31 61 21 31 27 20 | 95 64 87 69 73 80
R02 | 1910 9 14 19 15 20 8 | 70 79 68 69 80 70
R03 | 1052 9 16 13 16 15 7 | 75 64 60 74 78 69
R04 | 1192 11 14 14 13 25 7 | 84 82 79 87 86 82
R05 | 1449 13 18 12 15 16 8 | 66 77 74 56 74 66
R07 | 1044 8 16 12 9 24 6 | 66 56 68 59 78 63
R08 | 899 7 17 12 14 13 7 | 57 55 62 61 60 57
R09 | 2325 9 14 16 13 49 7 | 25 32 29 25 51 25
R11 | 750 11 17 12 22 14 9 | 28 24 26 41 29 27
R12 | 869 10 17 11 20 19 8 | 52 57 51 46 50 50
R13 | 993 16 50 24 48 26 19 | 59 56 58 81 62 60
R14 | 1009 7 26 14 14 13 8 | 37 48 33 33 35 35
R15 | 1516 9 16 13 10 21 6 | 56 65 50 57 50 55
R16 | 2540 20 32 54 24 28 20 | 60 64 63 60 61 61
R17E | 1149 9 19 11 27 23 9 | 29 33 30 39 37 28
R18E | 2133 7 17 16 19 17 8 | 26 26 30 26 27 24
R19E | 2383 25 56 35 27 53 20 | 40 55 41 50 42 38
R20E | 4091 37 81 59 43 119 31 | 49 65 88 63 70 55
R21E | 1538 8 12 15 16 19 7 | 26 25 28 31 29 24
XR22E | 3743 --- 299 12 14 23 13 | --- 120 46 41 47 43
R24E | 1342 15 31 21 34 21 14 | 31 39 34 45 36 29
------+------------------------------------+--------------------------------
RMS | 1738 16 33 24 24 36 |T 51 56 52 53 55 49
WRMS | 1738 11 27 18 19 27 |NE 59 58 57 58 61 57
MEDI | 1342 9 17 14 16 21 |MD 52 56 51 56 51 55
Table 3.2252.2 GPS week: 2252 Day: 2 MJD: 60010
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 608 29 48 15 13 31 16 | 89 52 81 71 70 74
R02 | 1935 9 11 15 9 16 6 | 61 55 54 63 64 58
R03 | 975 8 16 23 21 13 10 | 74 63 53 82 66 68
R04 | 1055 10 19 9 10 16 7 | 80 71 78 84 82 78
R05 | 1202 8 11 15 11 14 6 | 68 63 66 72 67 66
R07 | 1013 11 13 15 12 14 7 | 70 58 59 63 67 62
R08 | 715 8 13 19 13 19 8 | 67 54 49 69 69 60
R09 | 1176 13 25 13 15 16 9 | 21 28 20 23 26 18
R11 | 771 12 17 8 13 13 7 | 22 38 29 17 31 23
R12 | 987 10 18 16 26 14 10 | 54 57 65 44 49 53
R13 | 730 12 29 25 28 31 13 | 69 52 77 62 67 64
R14 | 1116 10 16 10 18 12 8 | 35 41 32 25 31 31
R15 | 1354 12 11 21 8 12 8 | 46 44 37 45 37 42
R16 | 1597 19 23 58 23 35 19 | 74 70 77 75 79 73
R17E | 777 7 13 15 18 11 8 | 42 48 56 44 41 45
R18E | 1234 12 15 12 20 15 9 | 24 22 24 30 21 21
R19E | 1274 40 50 39 34 84 23 | 39 61 53 38 64 37
R20E | 2631 39 82 63 26 112 31 | 64 67 87 58 90 56
R21E | 1240 7 15 11 20 19 8 | 21 23 24 28 25 21
XR22E | 3144 --- 305 14 11 23 13 | --- 112 37 31 39 30
R24E | 3368 14 19 23 21 18 11 | 26 38 41 30 26 26
------+------------------------------------+--------------------------------
RMS | 1446 17 29 26 19 36 |T 52 53 52 50 52 47
WRMS | 1446 12 24 18 16 26 |NE 59 53 55 56 57 55
MEDI | 1176 11 17 15 18 16 |MD 54 54 53 45 64 53
Table 3.2252.3 GPS week: 2252 Day: 3 MJD: 60011
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 769 34 36 24 15 23 16 | 100 56 82 73 72 79
R02 | 1281 10 16 19 10 12 8 | 64 72 62 61 63 63
R03 | 560 6 20 12 9 14 7 | 73 60 81 77 67 73
R04 | 849 13 23 10 11 12 8 | 75 58 71 73 72 70
R05 | 1108 12 14 17 7 16 7 | 66 61 67 67 62 65
R07 | 1320 9 25 15 16 11 9 | 72 73 65 75 68 70
R08 | 680 9 18 20 12 17 8 | 73 76 58 69 65 68
R09 | 1761 14 16 17 12 13 8 | 24 36 35 21 31 26
R11 | 651 8 13 14 11 20 7 | 18 22 23 18 23 15
R12 | 1072 14 36 11 40 13 15 | 35 48 20 31 29 26
R13 | 713 23 35 35 36 20 18 | 68 35 45 63 55 52
R14 | 1318 6 14 11 22 17 8 | 38 45 46 28 39 38
R15 | 1115 20 17 19 11 10 10 | 47 43 35 38 36 38
R16 | 1672 21 36 56 27 21 21 | 92 104 94 93 81 93
R17E | 579 12 17 11 17 19 8 | 40 50 43 32 38 39
R18E | 1302 8 16 19 13 21 8 | 18 20 21 27 23 16
R19E | 1126 38 37 35 44 107 22 | 41 59 66 55 77 43
R20E | 2901 39 70 68 61 122 34 | 54 70 82 66 108 51
R21E | 1075 10 13 10 18 16 7 | 26 27 26 26 21 25
XR22E | 3643 --- 292 9 10 17 9 | --- 135 58 59 64 58
R24E | 5820 9 22 16 27 14 11 | 24 33 25 37 23 21
------+------------------------------------+--------------------------------
RMS | 1794 19 28 27 25 39 |T 52 56 52 51 53 49
WRMS | 1794 14 19 20 18 36 |NE 60 56 56 56 54 55
MEDI | 1115 12 20 17 15 17 |MD 47 56 58 59 62 51
Table 3.2252.4 GPS week: 2252 Day: 4 MJD: 60012
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1034 40 36 16 18 21 17 | 100 64 77 74 71 77
R02 | 961 8 10 10 8 18 5 | 70 73 67 69 61 69
R03 | 730 11 14 12 12 22 7 | 84 84 77 84 73 81
R04 | 733 14 14 9 16 16 8 | 85 77 85 99 91 86
R05 | 1557 18 10 27 14 18 11 | 74 69 62 78 70 69
R07 | 1000 10 17 8 22 18 8 | 74 66 77 84 73 74
R08 | 637 16 14 15 12 13 8 | 68 65 71 58 59 65
R09 | 1963 11 16 17 11 12 8 | 29 31 31 29 29 27
R11 | 622 16 10 17 8 15 8 | 23 30 37 28 27 27
R12 | 1035 16 25 9 35 18 13 | 56 58 58 52 52 53
R13 | 726 25 24 13 26 23 13 | 58 37 43 35 61 42
R14 | 1706 8 15 10 13 13 7 | 40 48 44 37 46 41
R15 | 997 12 10 9 10 23 6 | 60 62 55 55 44 57
R16 | 1929 27 30 58 22 25 21 | 82 93 85 88 79 86
R17E | 929 9 14 13 13 21 7 | 36 36 39 41 34 36
R18E | 999 9 11 9 16 27 6 | 29 28 30 35 34 29
R19E | 1817 30 40 36 34 70 20 | 33 51 58 41 67 38
R20E | 2467 49 90 58 82 151 40 | 61 107 77 56 101 51
R21E | 794 7 13 8 10 17 5 | 25 28 22 26 24 23
XR22E | 4424 --- 290 15 15 21 15 | --- 123 47 43 42 44
R24E | 5270 12 14 29 20 15 11 | 33 33 46 32 35 32
------+------------------------------------+--------------------------------
RMS | 1732 21 28 24 26 41 |T 56 60 56 54 55 52
WRMS | 1732 16 16 17 17 25 |NE 64 61 62 62 59 61
MEDI | 1000 12 14 13 15 18 |MD 58 62 58 52 59 51
Table 3.2252.5 GPS week: 2252 Day: 5 MJD: 60013
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1398 25 35 18 21 25 14 | 79 60 64 64 69 68
R02 | 844 3 27 18 12 27 9 | 52 71 44 48 37 52
R03 | 670 6 19 9 11 13 6 | 74 68 79 72 68 73
R04 | 778 9 23 13 7 24 7 | 80 79 87 80 94 80
R05 | 1713 9 13 10 10 22 6 | 62 56 60 61 61 59
R07 | 964 6 21 9 20 20 8 | 63 52 67 77 58 64
R08 | 1614 14 24 12 13 25 9 | 54 63 58 64 66 58
R09 | 1443 11 20 18 21 18 9 | 23 31 27 32 37 24
R11 | 1095 7 17 11 17 28 7 | 15 27 18 17 26 15
R12 | 817 12 19 14 17 13 8 | 44 56 45 45 48 45
R13 | 561 13 32 34 36 26 16 | 45 40 65 27 49 41
R14 | 1943 4 22 14 15 15 8 | 32 41 24 24 37 29
R15 | 1627 9 10 20 15 18 8 | 48 48 54 46 44 47
R16 | 1101 22 28 79 29 26 24 | 80 72 96 73 80 79
R17E | 974 6 17 15 16 14 7 | 30 33 35 41 32 32
R18E | 555 5 16 22 13 24 8 | 21 25 31 22 26 21
R19E | 2321 28 39 51 35 74 21 | 39 50 66 46 54 37
R20E | 2073 36 90 52 70 145 34 | 61 108 76 64 108 56
R21E | 704 9 11 20 18 15 8 | 26 31 32 32 30 25
XR22E | 4345 --- 324 13 12 20 13 | --- 162 70 76 66 72
R24E | 2135 8 13 21 34 23 11 | 28 28 32 46 36 28
------+------------------------------------+--------------------------------
RMS | 1380 15 30 29 25 41 |T 47 57 53 50 53 47
WRMS | 1380 11 21 29 16 26 |NE 53 54 56 52 55 52
MEDI | 1101 9 21 18 17 23 |MD 45 52 58 46 49 47
Table 3.2252.6 GPS week: 2252 Day: 6 MJD: 60014
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 813 33 41 34 26 21 19 | 122 83 88 109 100 101
R02 | 507 11 28 16 14 20 10 | 73 99 72 75 71 78
R03 | 667 6 8 7 8 15 4 | 102 100 100 106 94 102
R04 | 865 6 16 8 11 16 6 | 113 111 112 115 117 112
R05 | 1450 7 20 15 11 24 8 | 92 87 91 98 97 91
R07 | 573 13 17 19 14 16 9 | 88 71 74 91 82 81
R08 | 2062 12 17 10 8 18 7 | 77 86 77 81 87 79
R09 | 1198 12 15 14 11 21 7 | 29 29 34 31 42 28
R11 | 1536 8 18 9 8 26 6 | 19 26 23 24 29 19
R12 | 1103 15 20 11 22 23 10 | 58 70 56 56 53 59
R13 | 673 20 28 27 36 32 16 | 67 61 79 64 73 66
R14 | 974 9 19 7 19 17 8 | 44 58 46 34 42 44
R15 | 1423 14 15 16 17 18 9 | 63 67 57 56 61 59
R16 | 782 19 22 71 25 24 22 | 89 77 98 91 93 88
R17E | 1100 12 16 19 16 19 9 | 43 41 43 53 50 43
R18E | 593 11 17 19 15 26 9 | 23 22 28 33 24 23
R19E | 797 29 25 36 15 81 15 | 44 63 64 53 75 49
R20E | 2767 49 60 67 54 169 33 | 83 100 96 78 125 74
R21E | 1139 12 14 23 11 22 9 | 30 30 43 31 41 31
XR22E | 3671 --- 325 13 10 18 11 | --- 205 64 62 68 63
R24E | 2577 9 16 25 12 23 9 | 29 28 37 35 34 29
------+------------------------------------+--------------------------------
RMS | 1335 18 24 29 21 47 |T 64 72 65 65 69 62
WRMS | 1335 13 20 20 15 28 |NE 74 73 71 73 74 71
MEDI | 1100 12 18 16 14 21 |MD 63 70 64 62 71 63
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