[IGSREPORT-29208] Wk 2249 IGLOS Final Orbits
acc
acc at igs.org
Fri Mar 3 21:31:54 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2249 (Feb 12, 2023 - Feb 18, 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 2.2249.
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:
igl2249[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2249 in the SP3 format.
igl22497.sum Combination Report for GPS Week 2249.
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 | 0.7 ns
2 | 0.3 ns
3 | -15.1 ns
4 | -0.5 ns
5 | 1.3 ns
6 | -15.1 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 1.2249, 1a.2249).
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 2.2249.0-6)
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 3.2249.0-6).
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 2249 summary. (Feb 12, 2023 - Feb 18, 2023)
Table 1.2249.a GPS week : 2249 MJD: 59987.0-59993.0
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 5 -12 11 33 .10 22 17 | 32029 767 3497 9063
| 1 0 1 20 10 31 .04 | 6841 1997
esa n/a| -1 0 -3 -4 -9 -31 -.30 34 25 | 2641 412 3457 8793
| 1 1 2 11 17 12 .07 | 6896 1908
gfz n/a| 0 2 3 13 0 -21 -.15 28 21 | 0 618 3463 8889
| 0 1 1 15 13 14 .02 | 0 1939
grg n/a| 2 -3 -7 7 -8 25 .28 25 20 | -4390 714 3451 8250
| 1 1 1 17 20 34 .06 | 6986 1919
iac n/a| -1 1 0 12 15 -51 -.28 23 21 | -2338 720 3459 9427
| 1 1 1 21 30 25 .08 | 7394 804
Table 1.2249.b GPS week : 2249 MJD: 59987.0-59993.0
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 | 20 20 22 20 23 24 26 |
R02 | 8 7 9 11 8 7 10 |
R03 | 8 10 9 8 7 12 11 |
R04 | 9 9 11 10 11 11 8 |
R05 | 7 7 9 9 11 8 10 |
R07 | 9 10 10 10 8 10 10 |
R08 | 12 11 12 7 9 9 11 |
R09 | 12 9 10 13 11 7 11 |
R11 | 8 8 10 9 9 11 8 |
R12 | 10 10 10 7 7 8 10 |
R13 | 16 23 18 17 16 19 20 |
R14 | 6 8 5 5 9 7 7 |
R15 | 10 8 10 6 10 13 10 |
R16 | 22 24 26 23 21 24 24 |
R17 | 8 9 8 11 10 13 9 |
R18 | 7 7 8 11 12 11 13 |
R19 | 22 21 20 19 20 23 22 |
R20 | 44 46 45 38 37 47 43 |
R21 | 10 9 9 9 8 8 10 |
R22 | 20 11 11 11 16 10 10 |
R24 | 12 11 10 8 11 10 16 |
Table 1.2249.c GPS week : 2249 MJD: 59987.0-59993.0
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 2249 0 | 78 4 124 -775 2232 -12570 80.4 1479 1479 | 1059 0
brd 2249 1 | -3 -24 102 -937 2739 -6503 80.0 1198 1198 | 725 0
brd 2249 2 | -64 18 47 1175 2236 2054 80.3 1191 1191 | 258 0
brd 2249 3 | 42 26 178 403 1912 -2972 80.2 1441 1441 | -15125 0
brd 2249 4 | -63 -40 104 1496 684 -5917 78.9 1520 1520 | -505 0
brd 2249 5 | 54 27 74 -908 953 -5684 79.5 1524 1524 | 1257 0
brd 2249 6 | 51 -24 68 2140 -79 -9417 79.6 1541 1541 | -15059 0
-------------+------------------------------------------------------------+----------------
brd 2249 mean| 13 -1 99 370 1525 -5858 79.8 1413 1413 | -3912 0
brd 2249 sdev| 58 27 43 1271 1019 4638 .6 153 153 | 7658 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 2.2249.0 GPS week: 2249 Day: 0 MJD: 59987
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 6 7 -2 25 .10 24 19 | 35518 2725 3071 8605
esa n/a| 1 0 0 -3 -19 -38 -.38 36 24 | -761 2513 3063 6969
gfz n/a| 0 1 3 11 11 -13 -.12 26 16 | 0 2779 3085 8440
grg n/a| 1 -3 -6 -23 -16 37 .25 20 16 | -423 2895 3047 7779
iac n/a| -3 3 0 37 -11 -67 -.29 23 21 | 2095 1431 3078 9033
Table 2.2249.1 GPS week: 2249 Day: 1 MJD: 59988
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 6 3 20 98 .12 23 17 | 37433 1281 2705 9005
esa n/a| -1 2 0 -4 -31 -39 -.33 34 23 | 8620 538 2725 7251
gfz n/a| -1 2 2 8 -22 -7 -.17 29 13 | 0 1561 2705 8832
grg n/a| 1 -4 -8 6 7 -44 .31 25 19 | 108 956 2699 8153
iac n/a| 0 2 1 -6 9 -50 -.32 19 19 | 2554 548 2710 9418
Table 2.2249.2 GPS week: 2249 Day: 2 MJD: 59989
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 -22 5 12 .10 22 16 | 37155 -25 3570 8322
esa n/a| -2 1 -4 2 -20 -14 -.29 32 22 | 2972 -31 3523 7270
gfz n/a| 0 3 5 23 5 -9 -.17 27 14 | 0 -50 3532 8149
grg n/a| 3 -5 -6 11 9 25 .33 30 20 | 166 -123 3523 7621
iac n/a| 0 2 -3 25 -35 -25 -.41 24 22 | 1542 727 3534 8672
Table 2.2249.3 GPS week: 2249 Day: 3 MJD: 59990
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 5 -12 29 43 .13 21 17 | 22354 -1806 3463 8507
esa n/a| -2 3 -4 -7 2 -14 -.27 33 21 | -10461 -2170 3416 6834
gfz n/a| 0 2 1 11 -6 -21 -.14 25 30 | 0 -2015 3412 8319
grg n/a| 3 -3 -3 -3 -25 18 .25 22 20 | -14267 -1870 3420 7591
iac n/a| 0 1 1 -9 16 -49 -.18 22 19 | -13328 40 3415 8850
Table 2.2249.4 GPS week: 2249 Day: 4 MJD: 59991
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 7 -39 8 38 .04 22 18 | 34623 -435 3668 8887
esa n/a| -1 2 -3 8 21 -32 -.34 33 25 | 5675 -242 3623 7773
gfz n/a| -1 0 1 19 11 -48 -.14 24 14 | 0 -347 3624 8633
grg n/a| 3 0 -7 25 -28 29 .35 23 20 | -550 -21 3622 8154
iac n/a| 1 0 0 -12 42 -33 -.29 20 18 | 1286 -46 3620 9102
Table 2.2249.5 GPS week: 2249 Day: 5 MJD: 59992
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 12 11 10 .06 22 17 | 35227 3930 3937 9450
esa n/a| -2 -1 -5 -27 -9 -33 -.30 35 28 | 2262 3269 3889 11959
gfz n/a| -1 3 5 -15 -15 -28 -.16 33 29 | 0 3204 3878 9248
grg n/a| 3 -4 -9 28 20 50 .33 26 22 | -834 3566 3868 8658
iac n/a| -4 1 -1 18 39 -33 -.19 24 21 | 2437 2143 3876 9864
Table 2.2249.6 GPS week: 2249 Day: 6 MJD: 59993
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 -34 5 7 .13 22 18 | 21898 -299 4066 10671
esa n/a| -1 -1 -4 0 -7 -45 -.18 37 30 | 10186 -991 3960 13500
gfz n/a| 0 1 4 35 10 -21 -.16 30 33 | 0 -803 4005 10605
grg n/a| 1 0 -8 10 -24 63 .17 26 23 | -14933 -403 3984 9798
iac n/a| -2 2 0 34 48 -98 -.28 28 26 | -12954 200 3984 11055
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 3.2249.0 GPS week: 2249 Day: 0 MJD: 59987
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 2069 41 56 21 18 24 20 | 95 43 76 55 56 63
R02 | 2275 16 14 11 14 15 8 | 55 64 68 75 59 65
R03 | 1806 7 22 10 13 13 7 | 75 59 74 76 70 71
R04 | 1284 10 20 15 14 20 8 | 73 72 65 71 76 68
R05 | 2256 12 13 10 14 16 7 | 62 63 61 65 65 61
R07 | 1264 10 18 13 17 12 8 | 63 55 66 66 62 62
R08 | 1130 11 18 25 21 24 11 | 65 63 63 63 58 61
R09 | 2080 31 12 17 16 17 12 | 45 38 46 33 40 38
R11 | 711 10 20 14 9 18 7 | 42 45 58 49 53 48
R12 | 724 21 16 11 16 16 9 | 38 39 39 34 37 34
R13 | 2133 13 31 23 37 33 16 | 55 49 50 59 39 52
R14 | 900 8 9 9 10 19 5 | 46 51 49 47 44 47
R15 | 726 25 17 17 6 15 10 | 109 111 112 110 109 109
R16 | 1043 28 38 57 16 23 21 | 59 63 58 56 51 56
R17 | 1002 11 17 13 13 11 7 | 58 40 52 48 48 49
R18 | 1033 12 13 10 11 23 6 | 68 76 74 80 82 74
R19 | 608 47 41 19 37 25 21 | 83 42 72 68 67 64
R20 | 1983 56 121 82 46 50 44 | 125 45 136 61 80 85
R21 | 941 11 30 14 11 17 9 | 85 61 80 73 75 75
XR22 | 2064 --- 370 22 18 19 20 | --- 238 55 58 43 53
R24 | 1345 27 15 16 19 26 11 | 73 59 63 77 66 66
------+------------------------------------+--------------------------------
RMS | 1479 24 36 26 20 23 |T 68 65 67 63 60 61
WRMS | 1479 18 24 16 16 21 |NE 68 65 67 63 60 61
MEDI | 1264 12 18 15 16 19 |MD 63 59 63 63 59 62
Table 3.2249.1 GPS week: 2249 Day: 1 MJD: 59988
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1282 43 45 19 26 19 19 | 70 34 54 41 43 46
R02 | 2056 10 17 7 14 10 7 | 44 50 42 43 43 43
R03 | 891 9 26 16 11 12 9 | 56 45 63 57 52 55
R04 | 966 12 17 15 17 17 9 | 59 53 52 56 57 53
R05 | 1798 12 12 9 11 13 6 | 59 48 48 53 48 51
R07 | 1283 9 27 15 18 14 10 | 51 47 60 66 56 55
R08 | 1074 13 26 14 20 17 10 | 51 56 52 53 55 49
R09 | 984 20 20 13 9 17 9 | 39 28 36 29 33 31
R11 | 690 15 11 15 12 17 8 | 34 40 45 36 40 38
R12 | 636 17 20 13 19 14 10 | 25 40 35 20 20 25
R13 | 1749 29 36 29 54 15 22 | 25 37 27 23 19 21
R14 | 875 13 10 15 15 17 8 | 33 26 34 26 19 28
R15 | 1040 16 16 7 15 12 8 | 55 68 71 75 61 67
R16 | 972 34 43 58 23 28 24 | 39 57 34 32 24 34
R17 | 866 18 14 9 20 17 9 | 35 28 27 40 32 30
R18 | 1277 11 11 12 10 11 6 | 48 43 58 48 52 49
R19 | 1246 37 41 34 32 29 21 | 38 35 47 39 46 31
R20 | 1062 45 107 94 66 44 46 | 66 59 106 35 51 56
R21 | 787 13 20 11 18 13 9 | 47 35 36 56 45 43
XR22 | 1765 --- 365 10 11 18 10 | --- 133 24 38 28 29
R24 | 1300 21 20 15 18 14 10 | 45 44 50 57 44 46
------+------------------------------------+--------------------------------
RMS | 1198 23 34 29 25 19 |T 45 47 47 43 41 41
WRMS | 1198 17 23 13 19 19 |NE 45 47 47 43 41 41
MEDI | 1062 15 20 15 18 17 |MD 45 44 47 41 44 43
Table 3.2249.2 GPS week: 2249 Day: 2 MJD: 59989
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1584 45 44 22 35 31 21 | 68 32 34 37 30 35
R02 | 1354 11 18 12 19 16 8 | 43 46 40 53 49 43
R03 | 491 8 25 13 15 19 9 | 57 43 60 61 59 54
R04 | 665 13 26 20 13 21 10 | 53 45 70 54 52 54
R05 | 1056 7 22 15 13 21 8 | 54 47 63 61 38 55
R07 | 2248 9 25 14 17 26 9 | 55 37 51 63 55 51
R08 | 1222 14 29 13 25 10 12 | 51 50 54 73 55 55
R09 | 1093 18 19 15 17 36 10 | 39 40 38 37 48 35
R11 | 845 13 20 19 13 22 9 | 37 48 48 36 43 40
R12 | 818 13 17 15 21 16 9 | 37 46 43 32 39 37
R13 | 734 19 28 24 45 25 17 | 36 37 43 33 38 34
R14 | 862 7 9 8 9 14 5 | 32 35 28 35 37 31
R15 | 755 14 21 11 20 23 9 | 123 115 118 120 127 119
R16 | 598 26 40 68 28 29 25 | 45 37 47 48 38 42
R17 | 847 15 16 9 17 21 8 | 56 42 49 51 47 48
R18 | 842 9 14 12 15 18 7 | 59 59 50 61 62 56
R19 | 2214 28 30 33 46 23 20 | 44 44 61 52 47 43
R20 | 1093 60 94 73 88 42 45 | 91 87 134 42 69 76
R21 | 591 14 18 12 17 14 9 | 63 47 57 51 54 54
XR22 | 1340 --- 383 10 11 22 10 | --- 174 30 33 30 28
R24 | 1731 20 15 17 16 33 10 | 52 48 62 57 60 53
------+------------------------------------+--------------------------------
RMS | 1190 22 32 27 30 24 |T 54 55 56 51 51 49
WRMS | 1190 16 22 14 20 22 |NE 54 55 56 51 51 49
MEDI | 862 14 22 15 17 22 |MD 52 46 50 51 48 48
Table 3.2249.3 GPS week: 2249 Day: 3 MJD: 59990
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 878 27 63 22 19 35 20 | 86 49 79 68 59 68
R02 | 1216 14 26 13 22 16 11 | 47 65 61 49 53 52
R03 | 682 10 17 12 17 20 8 | 73 56 58 76 75 65
R04 | 794 9 24 9 21 11 9 | 66 53 58 80 63 63
R05 | 698 11 19 14 18 16 9 | 58 50 52 68 62 56
R07 | 1544 15 16 20 13 19 9 | 68 55 51 66 57 59
R08 | 2124 10 17 7 11 13 6 | 60 52 56 67 58 59
R09 | 744 15 14 22 31 17 12 | 40 31 46 33 37 34
R11 | 1177 12 21 13 15 26 9 | 28 43 37 33 35 32
R12 | 841 13 14 8 13 11 7 | 34 33 30 28 31 30
R13 | 1764 19 18 31 42 23 17 | 51 41 57 27 38 43
R14 | 1817 6 8 10 11 10 5 | 40 42 43 36 34 40
R15 | 1103 11 12 11 9 14 6 | 102 94 92 101 98 97
R16 | 977 29 25 63 26 27 23 | 57 48 55 47 48 51
R17 | 699 11 24 16 25 14 11 | 48 40 47 52 50 44
R18 | 622 19 19 19 18 21 11 | 56 66 81 75 65 67
R19 | 1223 32 39 29 34 28 19 | 57 33 50 53 50 43
R20 | 2356 62 106 53 35 47 38 | 90 80 101 73 71 68
R21 | 804 16 11 20 12 13 9 | 65 56 53 63 56 58
XR22 | 1333 --- 387 10 11 18 10 | --- 182 34 43 34 37
R24 | 3312 13 13 13 12 26 7 | 45 44 48 52 56 46
------+------------------------------------+--------------------------------
RMS | 1440 21 33 25 22 22 |T 58 57 56 56 53 52
WRMS | 1440 17 21 30 20 19 |NE 58 57 56 56 53 52
MEDI | 1103 13 19 14 18 18 |MD 57 50 53 53 56 52
Table 3.2249.4 GPS week: 2249 Day: 4 MJD: 59991
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 642 41 69 18 24 20 23 | 101 37 74 82 71 72
R02 | 1349 13 18 11 15 18 8 | 53 63 51 60 47 55
R03 | 737 9 16 9 15 15 7 | 68 61 63 70 58 65
R04 | 1175 10 25 17 20 17 10 | 71 62 82 79 68 73
R05 | 680 14 22 20 18 13 10 | 65 57 78 78 73 68
R07 | 2158 15 22 7 10 17 8 | 70 50 58 60 64 59
R08 | 1967 11 17 16 14 22 8 | 63 57 51 68 54 59
R09 | 841 13 10 20 23 18 10 | 36 40 40 32 36 34
R11 | 1118 9 19 16 16 20 8 | 27 35 40 31 37 31
R12 | 774 10 20 10 9 17 7 | 26 28 31 33 26 27
R13 | 1918 26 30 22 31 25 16 | 46 56 50 33 46 43
R14 | 3025 15 15 17 15 15 9 | 32 47 52 35 32 40
R15 | 835 16 18 17 14 13 9 | 123 106 117 121 124 117
R16 | 664 24 33 53 25 21 20 | 40 43 43 33 39 36
R17 | 630 11 28 12 18 13 10 | 68 65 63 67 66 64
R18 | 682 22 13 11 27 17 11 | 39 45 48 61 42 47
R19 | 1190 36 38 32 32 36 20 | 50 34 55 33 59 38
R20 | 2805 53 95 59 52 35 37 | 74 52 65 40 29 45
R21 | 843 14 15 9 12 19 7 | 49 35 33 43 35 39
XR22 | 2166 --- 393 16 15 18 15 | --- 155 25 31 27 25
R24 | 2381 15 16 21 19 16 10 | 33 37 41 44 33 35
------+------------------------------------+--------------------------------
RMS | 1520 22 33 24 23 20 |T 56 55 55 54 50 51
WRMS | 1520 18 25 14 20 18 |NE 56 55 55 54 50 51
MEDI | 1118 14 20 17 18 18 |MD 50 50 51 44 46 45
Table 3.2249.5 GPS week: 2249 Day: 5 MJD: 59992
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 664 45 64 19 21 28 23 | 88 44 61 62 53 61
R02 | 1144 6 14 12 12 33 6 | 55 57 58 54 61 55
R03 | 1086 10 26 25 17 14 11 | 73 62 72 62 57 65
R04 | 1586 13 20 24 20 27 11 | 68 70 85 61 75 69
R05 | 840 11 16 13 13 18 7 | 60 61 63 70 68 62
R07 | 1858 14 28 10 14 26 10 | 65 54 57 67 69 59
R08 | 656 12 24 10 15 19 9 | 59 54 53 52 50 53
R09 | 915 8 13 13 13 28 7 | 30 26 40 21 28 26
R11 | 874 16 16 23 21 11 11 | 33 36 48 44 32 38
R12 | 911 14 14 7 15 19 7 | 21 35 27 22 27 23
R13 | 2501 26 35 32 34 34 18 | 31 39 24 21 43 23
R14 | 3512 10 14 10 13 11 7 | 25 32 28 30 29 27
R15 | 1835 19 18 17 30 24 12 | 223 232 223 237 227 228
R16 | 781 23 37 69 28 22 24 | 33 50 29 26 28 30
R17 | 688 16 17 24 30 21 13 | 92 93 94 92 91 91
R18 | 1010 13 17 21 24 18 11 | 35 41 30 48 30 36
R19 | 1288 37 56 36 28 30 23 | 60 28 60 37 37 42
R20 | 1426 52 98 102 72 35 46 | 60 48 99 34 35 41
R21 | 1506 14 17 9 14 12 8 | 44 37 38 39 34 38
XR22 | 2337 --- 399 10 9 14 9 | --- 143 28 32 26 28
R24 | 1990 19 17 15 17 18 10 | 44 40 41 58 45 44
------+------------------------------------+--------------------------------
RMS | 1524 22 35 33 26 24 |T 59 61 59 55 54 54
WRMS | 1524 17 28 29 22 21 |NE 59 61 59 55 54 54
MEDI | 1144 14 18 17 17 21 |MD 55 48 53 48 43 42
Table 3.2249.6 GPS week: 2249 Day: 6 MJD: 59993
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 733 44 68 26 35 34 25 | 117 50 96 63 61 80
R02 | 1280 7 17 22 17 17 9 | 80 86 79 77 84 79
R03 | 1611 13 28 19 12 16 10 | 99 73 105 94 99 93
R04 | 1841 9 17 12 13 20 7 | 93 91 100 87 93 92
R05 | 1401 15 15 12 21 19 9 | 86 79 82 80 82 81
R07 | 1389 6 28 13 16 15 9 | 92 76 93 91 92 88
R08 | 815 13 29 18 14 24 10 | 82 81 91 90 83 84
R09 | 1584 13 15 22 23 24 11 | 36 34 42 25 37 30
R11 | 805 11 16 18 8 36 8 | 45 48 65 49 61 50
R12 | 838 10 22 17 19 13 10 | 36 55 45 29 32 37
R13 | 2146 24 39 38 38 32 20 | 58 52 47 45 49 49
R14 | 2864 8 14 16 12 20 7 | 34 42 39 35 40 35
R15 | 2684 19 21 14 12 17 10 | 189 202 197 202 194 196
R16 | 776 27 25 69 27 25 24 | 56 61 68 54 48 57
R17 | 913 9 21 9 19 31 8 | 56 63 62 64 62 59
R18 | 905 12 21 28 27 20 13 | 41 50 39 62 52 45
R19 | 911 39 56 27 23 51 21 | 68 32 58 45 37 46
R20 | 1285 51 106 76 64 61 42 | 91 62 112 45 49 59
R21 | 1033 13 17 11 24 10 9 | 60 43 49 56 48 51
XR22 | 2370 --- 410 9 10 21 9 | --- 234 25 32 22 28
R24 | 2247 23 31 13 39 25 16 | 74 58 69 72 59 65
------+------------------------------------+--------------------------------
RMS | 1540 22 37 30 26 28 |T 74 74 74 66 65 66
WRMS | 1540 18 30 33 23 26 |NE 74 74 74 66 65 66
MEDI | 1285 13 22 18 19 21 |MD 68 61 68 62 59 59
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