[IGSREPORT-29199] Wk 2248 IGLOS Final Orbits
acc
acc at igs.org
Sun Feb 26 23:36:29 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2248 (Feb 05, 2023 - Feb 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 2.2248.
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:
igl2248[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2248 in the SP3 format.
igl22487.sum Combination Report for GPS Week 2248.
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 | 1.3 ns
1 | -2.6 ns
2 | -1.0 ns
3 | 0.7 ns
4 | -0.6 ns
5 | -0.8 ns
6 | -13.4 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 | R20 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 1.2248, 1a.2248).
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 2.2248.0-6)
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 3.2248.0-6).
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 2248 summary. (Feb 05, 2023 - Feb 11, 2023)
Table 1.2248.a GPS week : 2248 MJD: 59980.0-59986.0
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 1 5 -9 2 34 .10 22 18 | 34011 -629 3031 8704
| 1 1 1 27 14 19 .09 | 5724 2418
esa n/a| 0 0 -4 -17 -1 -33 -.25 41 28 | 1538 -932 3009 8521
| 1 2 3 21 10 17 .04 | 6344 2226
gfz n/a| 0 2 2 23 -3 -38 -.17 25 16 | 0 -847 3008 8540
| 1 0 1 19 14 31 .06 | 0 2210
grg n/a| 2 -4 -6 -5 0 40 .27 29 22 | -1950 -925 3005 8025
| 2 2 2 22 28 31 .05 | 4937 2114
iac n/a| -1 2 -1 19 31 -34 -.27 27 25 | -300 -417 3004 9094
| 1 2 1 27 45 112 .11 | 4758 1117
Table 1.2248.b GPS week : 2248 MJD: 59980.0-59986.0
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 | 22 21 24 23 21 24 22 |
R02 | 7 10 11 8 7 7 7 |
R03 | 22 17 11 9 8 7 8 |
R04 | 10 17 10 7 9 9 7 |
R05 | 10 24 7 7 8 8 9 |
R07 | 24 19 12 10 8 9 8 |
R08 | 14 21 8 10 9 9 8 |
R09 | 10 8 8 7 7 8 10 |
R11 | 9 9 7 7 8 10 8 |
R12 | 10 14 7 7 11 7 10 |
R13 | 22 20 18 20 20 24 16 |
R14 | 8 8 5 8 9 8 7 |
R15 | 8 9 8 9 12 9 8 |
R16 | 26 25 22 26 24 22 22 |
R17 | 7 12 11 9 10 11 8 |
R18 | 5 7 9 10 13 9 8 |
R19 | 20 21 23 19 26 26 26 |
R20 | 46 45 27 39 38 44 48 |
R21 | 9 8 8 7 10 12 11 |
R22 | 11 14 11 15 6 14 12 |
R24 | 14 11 10 15 10 13 15 |
Table 1.2248.c GPS week : 2248 MJD: 59980.0-59986.0
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 2248 0 | 2 23 115 2102 1422 -3457 78.6 1451 1451 | 1255 0
brd 2248 1 | -22 -54 52 1084 1862 -1740 79.6 1496 1496 | -2592 0
brd 2248 2 | 5 -3 41 -56 468 -1206 78.4 1672 1672 | -1003 0
brd 2248 3 | 18 11 14 -644 1062 -763 79.4 1929 1929 | 683 0
brd 2248 4 | -17 -42 38 670 231 -4828 80.1 1865 1865 | -599 0
brd 2248 5 | 2 54 71 -381 -917 -6970 79.6 1941 1941 | -794 0
brd 2248 6 | 62 -89 58 -573 -191 -11730 81.1 1800 1800 | -13431 0
-------------+------------------------------------------------------------+----------------
brd 2248 mean| 7 -14 55 314 562 -4384 79.5 1736 1736 | -2354 0
brd 2248 sdev| 27 50 31 1020 962 3913 .9 201 201 | 5038 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 2.2248.0 GPS week: 2248 Day: 0 MJD: 59980
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 6 -44 -6 54 .15 25 19 | 37887 3007 2830 8808
esa n/a| -1 0 0 19 5 -53 -.25 36 26 | -2722 2485 2887 8532
gfz n/a| 0 1 0 38 -7 -3 -.22 25 16 | 0 2693 2848 8707
grg n/a| 4 -4 -8 -20 24 17 .34 40 25 | -144 2396 2814 8182
iac n/a| 0 0 -1 23 56 16 -.38 30 30 | 2401 1465 2862 9160
Table 2.2248.1 GPS week: 2248 Day: 1 MJD: 59981
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 3 3 0 -19 24 .26 24 21 | 37848 -4469 3036 9270
esa n/a| 1 4 -9 -49 -18 -18 -.24 37 26 | 10482 -4864 2992 12028
gfz n/a| 2 2 2 4 5 -12 -.22 24 16 | 0 -4138 3000 9152
grg n/a| -2 -9 -3 3 39 40 .31 49 30 | -405 -4382 3025 8698
iac n/a| 0 4 -2 -8 -20 54 -.27 31 33 | 446 -1817 3019 9708
Table 2.2248.2 GPS week: 2248 Day: 2 MJD: 59982
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 1 3 26 16 44 .12 19 15 | 35320 -1531 2891 8087
esa n/a| -2 0 -5 -12 0 -10 -.18 44 27 | 5992 -1259 2847 7217
gfz n/a| 0 3 1 12 -33 -14 -.17 22 15 | 0 -1851 2871 7873
grg n/a| 4 -6 -4 -48 17 -15 .22 25 23 | -242 -1115 2868 7424
iac n/a| -1 2 -2 -10 -25 38 -.22 25 22 | 1020 -754 2862 8444
Table 2.2248.3 GPS week: 2248 Day: 3 MJD: 59983
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 5 -33 21 17 -.00 19 17 | 35794 1613 3259 7218
esa n/a| -1 0 -3 -9 14 -32 -.25 40 26 | 2223 409 3244 9324
gfz n/a| -2 2 2 35 -3 -42 -.10 25 16 | 0 1137 3258 7049
grg n/a| 3 -1 -5 1 -40 46 .21 23 19 | 178 682 3249 6540
iac n/a| 0 1 -2 6 84 -236 -.08 25 22 | 1939 642 3226 7640
Table 2.2248.4 GPS week: 2248 Day: 4 MJD: 59984
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 7 16 7 16 .04 23 19 | 35660 -773 3360 9230
esa n/a| -2 -3 -4 -29 -5 -46 -.23 43 31 | 4705 -578 3317 6769
gfz n/a| 0 2 2 -5 3 -54 -.15 24 15 | 0 -1676 3302 8996
grg n/a| 2 -2 -6 17 -9 82 .28 20 18 | 190 -1670 3285 8282
iac n/a| 0 0 -2 66 83 -146 -.20 23 23 | 1814 -440 3301 9677
Table 2.2248.5 GPS week: 2248 Day: 5 MJD: 59985
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 1 -2 19 .08 23 18 | 34177 -1750 3320 9497
esa n/a| 0 0 0 -19 1 -20 -.28 43 30 | -1168 -1690 3288 8802
gfz n/a| -4 1 3 37 7 -45 -.25 30 19 | 0 -1401 3285 9394
grg n/a| 4 -2 -8 0 -25 53 .26 21 20 | -92 -1714 3281 8841
iac n/a| -2 5 -3 43 22 -13 -.43 27 22 | 1268 -1181 3267 9847
Table 2.2248.6 GPS week: 2248 Day: 6 MJD: 59986
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 -29 1 61 .04 25 18 | 21392 -503 2522 8818
esa n/a| 1 0 -6 -22 -7 -53 -.31 41 28 | -8745 -1029 2488 6979
gfz n/a| -1 1 3 43 3 -93 -.10 27 17 | 0 -695 2495 8615
grg n/a| 0 -3 -7 9 -9 56 .26 22 19 | -13136 -678 2514 8211
iac n/a| -3 4 1 17 21 45 -.28 26 24 | -10992 -835 2492 9182
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 3.2248.0 GPS week: 2248 Day: 0 MJD: 59980
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 2535 29 52 31 44 40 22 | 61 52 63 74 46 51
R02E | 1010 12 15 10 13 26 7 | 79 83 77 83 85 79
R03E | 1502 24 15 21 79 49 22 | 54 49 57 86 69 49
R04E | 962 16 16 9 30 27 10 | 81 67 71 75 82 72
R05E | 2322 12 14 8 33 23 10 | 107 101 106 115 117 106
R07E | 821 24 20 23 82 47 23 | 95 90 93 127 105 91
R08E | 2292 24 24 18 32 56 14 | 56 55 45 63 56 49
R09 | 913 21 13 17 13 10 10 | 31 28 34 34 33 30
R11 | 482 11 15 16 15 17 8 | 30 33 36 32 32 30
R12 | 913 17 12 12 24 16 9 | 31 29 30 25 30 28
R13 | 802 32 35 27 58 19 21 | 44 46 39 45 39 41
R14 | 1249 11 18 9 16 29 7 | 36 43 40 35 30 38
R15 | 552 13 15 10 17 25 8 | 39 38 37 37 40 37
R16 | 507 31 40 60 30 32 25 | 44 51 51 42 41 43
R17 | 586 14 16 8 10 14 7 | 92 75 87 93 86 87
R18 | 801 8 8 6 11 19 5 | 95 102 94 109 110 99
R19 | 2737 22 45 26 44 24 19 | 113 64 103 109 107 96
R20 | 1869 70 122 58 61 32 46 | 163 52 146 96 118 115
R21 | 1419 11 19 11 19 23 8 | 97 78 91 88 90 89
XR22 | 1777 --- 357 7 14 18 10 | --- 230 53 56 53 53
R24 | 1217 17 29 12 36 19 13 | 113 97 113 128 111 111
------+------------------------------------+--------------------------------
RMS | 1450 25 36 25 40 30 |T 73 69 69 73 70 66
WRMS | 1450 19 26 16 25 30 |NE 70 67 67 66 64 63
MEDI | 1010 17 18 12 30 24 |MD 61 55 63 75 69 53
Table 3.2248.1 GPS week: 2248 Day: 1 MJD: 59981
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 2272 39 55 24 20 41 21 | 51 38 35 46 32 33
R02E | 1120 8 17 13 30 26 9 | 129 128 121 150 131 129
R03E | 1973 11 20 18 67 64 17 | 46 47 45 80 81 42
R04E | 1718 15 19 17 67 25 17 | 36 39 42 83 50 38
R05E | 2739 24 20 17 96 38 23 | 73 67 70 113 69 67
R07E | 598 19 32 15 69 32 19 | 74 75 87 123 83 81
R08E | 3181 18 27 19 81 35 21 | 47 43 52 117 68 53
R09 | 641 16 15 12 12 17 8 | 16 18 18 21 17 15
R11 | 468 10 22 13 21 27 9 | 13 38 24 21 25 17
R12 | 598 18 21 19 41 14 13 | 28 48 52 17 33 35
R13 | 814 31 42 15 53 29 19 | 36 45 25 30 42 28
R14 | 695 9 14 15 11 12 7 | 27 25 28 22 20 24
R15 | 787 17 12 17 12 15 9 | 22 24 33 18 17 21
R16 | 440 26 40 59 31 45 24 | 19 28 22 25 20 20
R17 | 840 10 29 23 20 14 12 | 55 52 78 66 53 62
R18 | 519 13 13 10 12 19 7 | 83 88 91 93 93 88
R19 | 1355 29 46 24 52 22 20 | 87 84 92 85 93 84
R20 | 835 66 112 57 84 42 45 | 90 79 97 50 82 70
R21 | 1071 11 17 7 19 16 7 | 54 45 50 46 45 49
XR22 | 1701 --- 371 8 20 31 13 | --- 112 31 30 38 29
R24 | 2426 13 24 17 26 24 11 | 69 75 90 87 88 78
------+------------------------------------+--------------------------------
RMS | 1495 24 37 24 49 31 |T 52 57 56 63 56 50
WRMS | 1495 21 26 16 30 33 |NE 46 53 51 43 46 43
MEDI | 840 16 22 17 30 26 |MD 47 47 50 50 50 42
Table 3.2248.2 GPS week: 2248 Day: 2 MJD: 59982
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 2229 32 67 36 23 40 23 | 62 38 61 48 33 46
R02E | 2152 21 15 12 28 13 11 | 49 56 68 78 54 60
R03E | 1651 11 18 18 28 17 11 | 41 36 34 53 37 36
R04E | 2029 9 22 9 28 18 10 | 37 34 41 64 44 41
R05E | 1684 11 13 10 14 15 6 | 43 45 47 49 51 44
R07E | 749 12 14 20 31 17 11 | 50 47 43 64 48 47
R08E | 3430 13 17 9 14 18 7 | 43 41 41 41 34 39
R09 | 897 14 16 10 13 18 7 | 22 24 28 26 24 23
R11 | 497 6 17 7 16 20 6 | 19 27 27 23 26 22
R12 | 542 14 12 9 13 20 7 | 18 24 20 21 23 17
R13 | 962 29 37 19 43 23 18 | 29 34 29 24 33 24
R14 | 938 5 10 7 12 14 5 | 20 18 18 31 15 19
R15 | 798 14 12 11 14 7 7 | 22 27 29 17 21 21
R16 | 513 26 32 54 28 48 22 | 29 28 34 26 37 27
R17 | 1833 12 28 15 21 14 10 | 105 91 104 105 92 101
R18 | 581 17 15 8 20 32 8 | 57 73 70 72 76 66
R19 | 2366 37 49 30 41 23 22 | 75 47 57 74 53 57
R20 | 1868 28 161 46 35 53 26 | 88 87 114 112 85 105
R21 | 935 17 15 8 14 14 8 | 76 66 62 66 65 67
XR22 | 2059 --- 376 8 13 20 10 | --- 142 32 38 36 33
R24 | 2556 8 24 10 23 19 9 | 82 79 82 95 87 84
------+------------------------------------+--------------------------------
RMS | 1671 19 44 22 25 25 |T 48 50 49 53 46 46
WRMS | 1671 15 27 15 23 22 |NE 50 53 51 51 47 47
MEDI | 1651 14 17 10 21 18 |MD 43 41 41 49 37 41
Table 3.2248.3 GPS week: 2248 Day: 3 MJD: 59983
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 2212 40 71 23 24 41 23 | 84 40 57 53 41 54
R02E | 3147 7 14 14 16 24 7 | 55 58 48 65 48 55
R03E | 2311 13 20 12 17 30 9 | 46 31 45 37 35 38
R04E | 2345 9 10 12 17 29 7 | 52 52 54 64 55 54
R05E | 1584 10 16 12 9 20 6 | 46 40 45 48 46 43
R07E | 1372 11 27 14 19 20 10 | 56 57 58 66 60 57
R08E | 3170 13 22 13 17 17 9 | 47 49 51 60 54 51
R09 | 919 13 13 9 7 14 6 | 22 28 20 26 32 22
R11 | 508 10 20 11 9 23 7 | 20 26 25 26 36 22
R12 | 486 11 15 9 9 17 6 | 22 29 22 24 27 20
R13 | 2284 35 35 27 41 27 20 | 30 29 39 39 38 31
R14 | 754 7 14 14 18 11 8 | 24 34 35 23 33 27
R15 | 894 12 17 18 14 21 9 | 27 28 30 28 30 24
R16 | 587 25 36 65 38 24 25 | 32 41 34 30 33 30
R17 | 1557 10 27 11 15 20 9 | 102 90 95 105 93 98
R18 | 619 18 14 8 24 28 10 | 94 94 96 107 115 96
R19 | 3496 32 48 28 21 37 18 | 104 80 107 79 113 93
R20 | 1100 26 128 65 47 26 39 | 106 62 136 109 98 99
R21 | 526 10 17 9 11 27 6 | 73 60 69 71 73 68
XR22 | 2439 --- 379 14 15 18 15 | --- 159 40 50 53 43
R24 | 3086 20 26 22 36 21 15 | 59 39 43 74 65 52
------+------------------------------------+--------------------------------
RMS | 1928 19 40 25 23 25 |T 55 53 54 56 56 51
WRMS | 1928 17 26 16 19 22 |NE 57 55 56 56 58 51
MEDI | 1557 12 20 14 17 23 |MD 47 41 45 53 48 51
Table 3.2248.4 GPS week: 2248 Day: 4 MJD: 59984
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1068 42 66 15 17 27 20 | 82 43 61 55 42 55
R02E | 2490 10 14 12 11 19 6 | 55 59 49 61 54 54
R03E | 3056 10 26 10 12 23 8 | 62 44 62 58 47 56
R04E | 2633 17 16 11 18 26 9 | 59 56 56 55 41 54
R05E | 1958 11 14 12 14 18 7 | 65 60 58 62 63 60
R07E | 1846 11 22 9 16 12 8 | 59 50 57 57 58 55
R08E | 2144 14 21 13 11 16 8 | 49 48 61 63 57 55
R09 | 860 8 18 11 9 20 6 | 16 22 22 18 21 14
R11 | 663 12 19 11 12 15 7 | 17 28 26 25 25 21
R12 | 903 26 16 8 21 16 11 | 19 31 29 25 26 24
R13 | 2769 27 31 35 38 38 19 | 29 37 26 24 32 25
R14 | 607 14 11 12 18 13 8 | 21 27 29 27 22 24
R15 | 1505 16 23 23 18 13 11 | 19 34 38 17 17 20
R16 | 736 32 39 57 25 20 23 | 28 41 33 26 21 27
R17 | 948 18 23 14 14 30 9 | 96 72 81 85 85 84
R18 | 556 12 21 25 23 28 12 | 61 56 48 76 64 59
R19 | 3585 50 74 24 32 34 25 | 97 45 73 74 63 71
R20 | 1243 38 132 56 38 33 38 | 91 47 101 78 58 73
R21 | 667 12 30 10 14 13 9 | 50 35 48 55 46 47
XR22 | 1927 --- 384 5 7 28 6 | --- 133 53 51 47 51
R24 | 2274 12 32 14 12 29 10 | 84 76 89 96 75 86
------+------------------------------------+--------------------------------
RMS | 1864 23 43 24 20 23 |T 52 49 52 51 45 48
WRMS | 1864 19 31 15 18 23 |NE 50 48 50 48 42 45
MEDI | 1505 14 23 12 16 20 |MD 55 45 53 55 47 54
Table 3.2248.5 GPS week: 2248 Day: 5 MJD: 59985
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1574 44 67 27 26 29 23 | 70 35 53 36 32 41
R02E | 2091 6 9 16 13 18 6 | 48 48 44 53 38 47
R03E | 3330 5 21 9 14 16 7 | 47 39 44 54 43 46
R04E | 3268 10 29 15 11 29 9 | 59 54 68 65 45 60
R05E | 2218 12 14 9 15 23 7 | 42 43 44 45 36 42
R07E | 1820 8 27 12 12 18 8 | 49 43 52 53 48 48
R08E | 2048 13 20 14 16 24 9 | 42 44 38 46 43 40
R09 | 1348 13 16 14 12 22 8 | 26 19 18 20 29 17
R11 | 641 12 21 22 16 16 10 | 15 24 32 18 21 18
R12 | 739 14 15 7 12 23 7 | 18 31 24 21 29 20
R13 | 2406 26 52 44 44 46 24 | 24 34 23 48 22 25
R14 | 645 8 11 17 16 19 8 | 21 28 32 16 29 21
R15 | 799 12 15 18 17 10 9 | 21 33 31 15 24 21
R16 | 1578 25 26 63 22 21 21 | 17 34 26 17 28 18
R17 | 1012 16 22 14 21 18 10 | 132 142 140 128 136 133
R18 | 785 15 21 11 14 21 8 | 87 77 81 77 83 80
R19 | 2974 51 74 28 25 49 25 | 99 79 90 84 77 85
R20 | 1941 47 136 86 41 50 44 | 89 79 126 51 75 74
R21 | 575 12 24 27 16 17 11 | 49 42 67 53 59 51
XR22 | 2142 --- 402 15 12 23 14 | --- 165 95 102 104 97
R24 | 2753 24 25 15 21 27 12 | 67 65 62 65 54 62
------+------------------------------------+--------------------------------
RMS | 1941 23 43 30 21 27 |T 51 55 56 50 50 49
WRMS | 1941 18 30 19 20 22 |NE 52 59 60 50 53 50
MEDI | 1820 13 22 15 16 22 |MD 47 43 44 51 43 46
Table 3.2248.6 GPS week: 2248 Day: 6 MJD: 59986
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 2064 42 61 21 27 27 22 | 104 39 81 61 53 69
R02E | 2326 7 15 13 9 19 6 | 66 70 62 67 58 65
R03E | 3239 8 22 14 13 15 8 | 69 53 65 68 61 64
R04E | 2332 7 15 10 14 25 6 | 81 74 79 82 66 79
R05E | 2929 15 17 18 14 22 9 | 68 67 69 68 53 66
R07E | 1628 8 19 14 12 15 7 | 78 68 83 83 73 78
R08E | 1609 9 21 12 13 20 8 | 70 68 68 78 71 70
R09 | 1934 19 23 10 14 20 9 | 26 22 28 29 28 24
R11 | 727 8 22 13 14 14 8 | 23 23 29 29 28 25
R12 | 937 17 14 11 23 19 10 | 25 29 25 23 26 24
R13 | 1912 9 40 21 37 38 16 | 42 41 42 67 28 45
R14 | 786 6 17 11 13 13 7 | 28 33 33 26 29 27
R15 | 682 16 12 13 10 11 7 | 28 32 36 27 25 29
R16 | 1425 26 35 57 22 30 21 | 36 46 39 34 33 35
R17 | 1073 13 16 10 12 17 7 | 122 119 124 120 114 121
R18 | 709 8 22 12 9 20 7 | 65 75 68 70 73 68
R19 | 1732 50 70 31 30 51 26 | 94 52 93 78 62 77
R20 | 2432 65 128 84 59 48 47 | 124 49 123 80 97 87
R21 | 656 14 24 16 18 27 10 | 69 48 74 64 77 64
XR22 | 1621 --- 391 12 11 13 11 | --- 227 66 74 70 69
R24 | 1558 34 22 22 18 16 14 | 111 103 102 95 103 100
------+------------------------------------+--------------------------------
RMS | 1799 25 41 27 22 26 |T 66 63 66 63 58 61
WRMS | 1799 18 28 17 19 24 |NE 64 62 64 58 56 57
MEDI | 1621 13 22 13 14 20 |MD 68 52 68 68 61 66
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