[IGSREPORT-29221] Wk 2250 IGLOS Final Orbits
acc
acc at igs.org
Tue Mar 14 08:56:54 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2250 (Feb 19, 2023 - Feb 25, 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 2.2250.
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:
igl2250[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2250 in the SP3 format.
igl22507.sum Combination Report for GPS Week 2250.
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 | -14.9 ns
1 | 0.8 ns
2 | -0.3 ns
3 | -13.5 ns
4 | -13.7 ns
5 | 0.3 ns
6 | -2.2 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 1.2250, 1a.2250).
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 2.2250.0-6)
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 3.2250.0-6).
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 2250 summary. (Feb 19, 2023 - Feb 25, 2023)
Table 1.2250.a GPS week : 2250 MJD: 59994.0-60000.0
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 4 -6 -8 31 .09 22 16 | 27492 -980 3301 8517
| 0 0 1 14 5 14 .06 | 7724 2532
esa n/a| 0 0 -2 0 -11 -33 -.20 30 23 | 1547 -873 3273 8653
| 1 1 1 16 15 18 .02 | 9854 2219
gfz n/a| 0 1 3 17 0 -33 -.13 27 20 | 0 -1100 3254 8430
| 1 1 2 7 19 20 .04 | 0 2545
grg n/a| 2 -2 -7 -8 7 41 .25 30 20 | -5768 -1078 3273 7879
| 2 2 3 24 27 31 .06 | 7198 2334
iac n/a| 0 2 0 28 21 -3 -.29 30 24 | -888 -356 3267 8909
| 2 1 2 16 32 129 .08 | 11390 1227
Table 1.2250.b GPS week : 2250 MJD: 59994.0-60000.0
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 | 21 22 19 21 22 24 23 |
R02 | 7 7 10 7 10 7 7 |
R03 | 11 11 8 11 9 9 7 |
R04 | 9 10 9 10 11 7 8 |
R05 | 7 7 7 7 10 9 8 |
R07 | 10 9 8 11 7 9 10 |
R08 | 10 11 9 13 8 13 7 |
R09 | 12 13 13 10 9 8 11 |
R11 | 8 8 11 9 7 5 6 |
R12 | 7 9 14 14 7 8 10 |
R13 | 14 16 17 17 13 16 18 |
R14 | 6 8 7 6 6 6 6 |
R15 | 6 10 7 10 9 7 8 |
R16 | 20 21 22 22 25 24 22 |
R17 | 23 11 11 8 11 7 9 |
R18 | 12 20 9 8 8 11 9 |
R19 | 25 23 24 26 17 18 23 |
R20 | 42 45 47 52 40 35 32 |
R21 | 10 15 11 7 9 9 8 |
R22 | 16 16 23 36 16 12 8 |
R24 | 20 15 11 10 11 10 12 |
Table 1.2250.c GPS week : 2250 MJD: 59994.0-60000.0
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 2250 0 | -99 49 136 411 274 -8982 80.7 1601 1601 | -14855 0
brd 2250 1 | -24 -62 106 -918 -1960 -12400 81.7 1471 1471 | 781 0
brd 2250 2 | 30 -71 137 -1147 -1943 -10500 79.7 1289 1289 | -330 0
brd 2250 3 | 51 -23 155 -1067 -653 -3167 80.1 1160 1160 | -13458 0
brd 2250 4 | 42 1 136 -3360 -671 -918 79.6 1366 1366 | -13712 0
brd 2250 5 | 23 46 108 -3189 -887 -2519 79.1 1622 1622 | 257 0
brd 2250 6 | 62 0 99 -304 1477 -2730 80.6 1753 1753 | -2240 0
-------------+------------------------------------------------------------+----------------
brd 2250 mean| 12 -8 125 -1367 -623 -5888 80.2 1466 1466 | -6222 0
brd 2250 sdev| 56 48 20 1409 1212 4594 .8 208 208 | 7355 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 2.2250.0 GPS week: 2250 Day: 0 MJD: 59994
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 8 -15 -9 26 .16 24 20 | 22010 -2902 3197 8838
esa n/a| 1 0 -5 -20 -11 -6 -.20 31 24 | -7284 -2175 3169 11412
gfz n/a| 0 3 2 26 35 -23 -.10 26 20 | 0 -2770 3091 8742
grg n/a| 2 -4 -9 11 -25 35 .19 35 24 | -13285 -3043 3169 8073
iac n/a| 0 2 -3 12 18 -84 -.25 33 28 | -12632 -1341 3160 9143
Table 2.2250.1 GPS week: 2250 Day: 1 MJD: 59995
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 4 -32 -4 52 .06 23 17 | 34492 996 3497 8338
esa n/a| -1 0 -2 -23 -24 -32 -.22 33 31 | 6785 791 3461 7674
gfz n/a| -1 2 7 16 4 -47 -.13 28 22 | 0 1632 3461 8227
grg n/a| 6 -3 -12 13 -6 35 .18 31 21 | 77 1288 3466 7896
iac n/a| 0 3 2 24 27 -26 -.32 27 27 | 2024 1459 3455 8656
Table 2.2250.2 GPS week: 2250 Day: 2 MJD: 59996
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 0 -8 22 .16 24 15 | 34362 -319 3161 8361
esa n/a| -2 0 -1 14 -32 -38 -.20 32 21 | 5278 -285 3132 7419
gfz n/a| -1 0 3 26 -20 -49 -.23 29 17 | 0 -801 3118 8240
grg n/a| 1 0 -9 -17 16 59 .28 28 18 | 2 -916 3136 8000
iac n/a| 0 0 -3 48 60 65 -.22 20 19 | 1291 522 3122 8805
Table 2.2250.3 GPS week: 2250 Day: 3 MJD: 59997
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 -18 25 .14 23 18 | 19256 -2295 3163 8088
esa n/a| 0 2 -2 5 -20 -23 -.16 29 20 | -8174 -2138 3109 7000
gfz n/a| 0 0 7 6 2 -18 -.12 27 16 | 0 -2524 3103 8055
grg n/a| 0 1 -10 -48 42 38 .31 41 22 | -12331 -2244 3130 7518
iac n/a| -3 2 1 46 51 -108 -.19 35 24 | -10971 -1570 3113 8500
Table 2.2250.4 GPS week: 2250 Day: 4 MJD: 59998
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 8 -13 12 .07 19 13 | 17085 2143 3711 8565
esa n/a| 0 0 -2 4 6 -46 -.21 28 20 | -10016 1507 3704 7535
gfz n/a| 0 2 2 18 -17 -39 -.13 28 37 | 0 1640 3705 8652
grg n/a| 2 -2 -4 -28 34 74 .24 26 17 | -14672 1607 3689 7760
iac n/a| -2 2 0 30 11 -171 -.39 35 28 | -12213 6 3703 8988
Table 2.2250.5 GPS week: 2250 Day: 5 MJD: 59999
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 3 -7 -5 51 .06 20 14 | 33846 566 3187 8696
esa n/a| 0 0 -2 17 8 -62 -.19 29 21 | 14515 863 3161 11748
gfz n/a| 0 0 2 15 3 -54 -.10 25 18 | 0 336 3147 8544
grg n/a| 1 -2 -2 -7 -27 64 .24 24 20 | -110 375 3168 7939
iac n/a| 2 0 -1 35 18 113 -.38 28 20 | 14491 224 3159 9244
Table 2.2250.6 GPS week: 2250 Day: 6 MJD: 60000
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 -4 -2 31 .01 22 16 | 31394 -5050 3193 8737
esa n/a| 0 0 -3 9 -6 -23 -.21 29 26 | 9730 -4677 3178 7786
gfz n/a| 1 2 1 10 -13 0 -.13 25 13 | 0 -5217 3153 8550
grg n/a| 0 -3 -3 16 19 -19 .35 21 18 | -63 -4619 3154 7973
iac n/a| 0 4 0 4 -39 188 -.27 29 24 | 11794 -1794 3161 9027
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 3.2250.0 GPS week: 2250 Day: 0 MJD: 59994
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 676 35 55 23 23 33 21 | 91 44 86 68 59 68
R02 | 1142 11 12 11 11 15 6 | 72 82 79 78 77 76
R03 | 1367 10 21 18 28 19 11 | 86 69 78 95 84 80
R04 | 655 11 16 14 23 11 9 | 82 85 88 87 81 83
R05 | 1338 10 14 12 14 22 7 | 70 71 73 69 66 70
R07 | 1006 12 20 15 19 12 9 | 74 57 66 66 62 64
R08 | 595 9 15 19 25 24 10 | 60 70 59 70 70 63
R09 | 1232 14 15 12 37 15 12 | 57 62 60 66 60 58
R11 | 1412 9 15 15 16 22 8 | 45 40 47 44 50 43
R12 | 1104 10 13 9 15 12 6 | 52 59 52 49 53 52
R13 | 1936 15 30 18 35 36 14 | 71 72 77 67 60 70
R14 | 1769 10 12 8 8 23 5 | 41 47 46 41 49 43
R15 | 3155 10 13 9 11 22 6 | 45 44 42 48 40 43
R16 | 1372 21 30 54 23 22 20 | 113 127 115 117 115 117
R17E | 2100 19 13 32 76 21 22 | 54 55 59 89 53 54
R18E | 743 13 11 19 36 34 12 | 53 53 52 62 54 50
R19E | 624 41 45 34 54 57 25 | 86 84 95 85 76 83
R20E | 1895 71 94 65 52 87 42 | 150 113 146 119 119 125
R21E | 817 14 19 9 27 31 10 | 61 63 62 68 71 61
XR22E | 2356 --- 392 13 18 19 16 | --- 206 70 72 72 69
R24E | 3316 28 25 26 60 36 20 | 101 82 99 115 78 94
------+------------------------------------+--------------------------------
RMS | 1601 24 31 26 35 33 |T 73 75 73 75 69 69
WRMS | 1601 20 24 20 24 28 |NE 68 66 69 68 66 66
MEDI | 1338 12 16 15 23 22 |MD 70 69 70 69 66 68
Table 3.2250.1 GPS week: 2250 Day: 1 MJD: 59995
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 837 30 63 35 14 38 22 | 62 35 74 51 36 51
R02 | 1260 11 15 6 11 9 6 | 41 52 46 47 41 45
R03 | 810 7 29 18 14 14 10 | 54 38 71 62 55 55
R04 | 617 9 21 24 11 17 10 | 60 66 81 64 56 66
R05 | 1192 10 12 11 10 23 6 | 52 50 51 50 54 50
R07 | 764 11 20 10 16 15 8 | 46 45 47 38 41 42
R08 | 756 17 15 22 17 23 10 | 42 45 52 41 43 43
R09 | 2085 20 19 17 30 23 12 | 61 61 66 57 60 59
R11 | 1482 6 18 10 15 20 7 | 40 46 38 41 40 39
R12 | 1258 14 16 13 20 33 9 | 38 46 36 31 51 35
R13 | 2053 17 25 30 38 21 16 | 49 41 47 40 31 43
R14 | 991 10 19 16 11 14 8 | 31 43 47 38 29 38
R15 | 2004 14 26 13 12 14 10 | 29 30 31 33 30 26
R16 | 1756 21 38 56 22 30 21 | 84 96 87 90 86 87
R17E | 1534 19 11 19 24 13 11 | 54 49 55 50 49 50
R18E | 708 12 19 27 61 55 19 | 37 36 41 75 58 37
R19E | 767 37 33 29 53 43 22 | 56 50 54 41 53 45
R20E | 3120 67 100 75 66 35 44 | 108 89 120 74 77 90
R21E | 1050 23 15 12 41 33 14 | 43 35 39 62 48 40
XR22E | 2278 --- 377 14 16 17 15 | --- 154 63 66 60 63
R24E | 1634 21 16 17 41 19 14 | 68 70 66 79 71 67
------+------------------------------------+--------------------------------
RMS | 1471 23 33 28 31 27 |T 52 56 57 53 50 51
WRMS | 1471 17 31 22 21 27 |NE 49 49 55 48 46 48
MEDI | 1258 14 19 17 17 21 |MD 49 46 52 50 51 45
Table 3.2250.2 GPS week: 2250 Day: 2 MJD: 59996
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1183 40 47 13 14 16 19 | 73 31 47 45 50 46
R02 | 1499 7 19 21 17 12 9 | 59 56 52 67 52 57
R03 | 1334 6 19 11 16 13 8 | 54 44 59 59 46 53
R04 | 1213 12 20 10 18 15 9 | 58 50 58 58 53 55
R05 | 682 10 12 16 11 17 7 | 54 59 55 56 55 54
R07 | 804 7 22 9 13 14 8 | 58 51 58 61 47 55
R08 | 946 13 22 13 12 15 9 | 48 51 34 44 36 42
R09 | 1909 20 19 19 27 23 12 | 55 63 58 37 58 50
R11 | 931 15 12 26 19 18 11 | 24 32 37 28 30 27
R12 | 804 12 17 23 38 17 14 | 53 59 53 60 55 52
R13 | 2329 17 31 24 42 16 17 | 68 60 69 49 48 60
R14 | 1042 7 10 15 13 15 6 | 46 49 45 43 45 44
R15 | 757 12 14 8 11 13 6 | 45 58 53 49 43 49
R16 | 1431 30 37 56 23 34 22 | 116 120 109 120 103 114
R17E | 1338 18 16 19 22 17 11 | 42 37 40 47 30 39
R18E | 682 13 13 14 18 19 8 | 36 36 34 40 38 34
R19E | 809 45 31 42 42 34 23 | 85 101 110 109 83 96
R20E | 1488 62 102 85 77 37 47 | 182 155 197 141 149 161
R21E | 1075 19 18 13 24 16 11 | 36 31 33 41 32 32
XR22E | 2392 --- 383 21 24 20 23 | --- 176 83 101 73 89
R24E | 1927 17 15 15 23 22 10 | 79 74 75 76 67 74
------+------------------------------------+--------------------------------
RMS | 1288 24 32 29 28 20 |T 63 66 64 63 56 61
WRMS | 1288 15 21 17 18 19 |NE 57 55 56 55 51 54
MEDI | 1183 13 19 16 19 17 |MD 54 56 55 56 50 53
Table 3.2250.3 GPS week: 2250 Day: 3 MJD: 59997
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 785 37 54 15 16 24 20 | 72 33 55 46 58 47
R02 | 910 8 13 11 14 27 6 | 52 54 57 61 60 55
R03 | 1492 6 21 12 30 12 10 | 56 40 56 81 57 56
R04 | 1341 14 21 17 11 15 9 | 54 39 65 56 60 52
R05 | 790 11 15 10 10 18 7 | 43 40 47 43 42 42
R07 | 658 8 24 24 12 11 10 | 59 42 76 66 63 60
R08 | 856 19 31 21 17 23 13 | 51 52 33 48 39 44
R09 | 1020 17 13 15 22 22 9 | 41 46 44 29 42 38
R11 | 624 12 20 14 16 16 9 | 28 47 37 26 31 33
R12 | 827 14 13 20 43 14 13 | 32 39 39 22 32 30
R13 | 1839 23 23 24 49 37 17 | 54 41 54 39 66 44
R14 | 734 9 8 9 11 12 5 | 38 39 33 34 41 35
R15 | 919 15 12 17 20 17 9 | 49 38 36 54 48 42
R16 | 643 26 25 58 30 28 22 | 73 56 68 59 54 64
R17E | 1031 13 17 9 19 21 8 | 42 43 45 54 45 44
R18E | 495 10 15 9 18 26 7 | 31 35 33 39 35 32
R19E | 786 44 25 26 79 90 26 | 94 100 102 123 99 96
R20E | 1109 61 84 80 137 91 51 | 147 144 170 187 159 145
R21E | 651 13 15 7 11 15 7 | 38 31 35 41 34 34
XR22E | 2399 --- 399 28 45 53 36 | --- 178 65 80 66 64
R24E | 2962 18 13 16 21 30 10 | 70 66 67 75 72 67
------+------------------------------------+--------------------------------
RMS | 1160 23 29 27 41 35 |T 56 57 57 60 57 53
WRMS | 1160 18 20 16 22 24 |NE 50 43 50 47 49 45
MEDI | 856 14 20 16 19 22 |MD 51 42 54 54 54 44
Table 3.2250.4 GPS week: 2250 Day: 4 MJD: 59998
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 946 28 64 25 26 27 22 | 77 32 75 70 50 62
R02 | 952 11 17 16 22 23 9 | 74 69 64 73 57 69
R03 | 1321 7 20 12 22 15 9 | 56 47 52 76 53 57
R04 | 1829 10 26 22 17 22 11 | 64 61 79 78 74 68
R05 | 567 12 22 20 10 15 9 | 56 60 77 65 57 62
R07 | 691 8 19 9 13 20 7 | 56 42 48 64 59 52
R08 | 712 14 16 10 9 16 7 | 49 52 47 49 47 49
R09 | 859 11 13 14 20 19 8 | 39 40 46 35 42 38
R11 | 624 6 15 15 6 23 6 | 33 33 31 32 39 30
R12 | 947 12 11 7 15 13 6 | 57 65 58 60 55 59
R13 | 1486 13 14 27 29 35 12 | 65 65 71 48 60 62
R14 | 1202 6 9 10 13 25 5 | 44 45 44 40 32 42
R15 | 808 17 19 11 11 17 8 | 50 45 40 46 46 44
R16 | 806 27 25 74 31 22 24 | 109 109 97 105 98 106
R17E | 1904 9 19 21 26 22 11 | 54 59 60 56 49 55
R18E | 644 9 18 9 16 16 7 | 37 43 33 47 35 38
R19E | 1075 26 19 33 39 44 17 | 74 80 90 83 78 78
R20E | 1967 56 74 71 78 117 39 | 164 163 178 144 153 155
R21E | 801 8 20 18 16 20 9 | 38 43 47 46 35 41
XR22E | 1956 --- 382 15 15 22 15 | --- 185 76 76 72 75
R24E | 3527 16 24 18 16 38 10 | 85 79 79 96 69 83
------+------------------------------------+--------------------------------
RMS | 1366 19 28 28 26 35 |T 64 67 66 66 60 63
WRMS | 1366 13 20 37 17 28 |NE 59 54 59 60 54 57
MEDI | 947 11 19 16 16 22 |MD 56 59 60 64 55 59
Table 3.2250.5 GPS week: 2250 Day: 5 MJD: 59999
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1611 35 73 14 30 26 24 | 74 41 54 79 52 55
R02 | 760 9 16 8 15 16 7 | 67 69 69 77 72 69
R03 | 1171 14 17 15 12 23 8 | 53 59 62 53 43 55
R04 | 1541 8 17 11 11 23 7 | 63 57 69 71 64 64
R05 | 1005 11 23 8 19 15 9 | 55 48 45 67 52 52
R07 | 872 13 20 11 15 18 8 | 58 45 41 64 51 51
R08 | 1070 15 21 24 29 29 13 | 39 39 31 60 60 40
R09 | 768 10 13 12 20 12 8 | 42 46 56 40 50 45
R11 | 859 10 10 6 7 18 5 | 40 41 45 45 40 41
R12 | 1047 12 10 14 15 16 7 | 42 44 47 46 51 43
R13 | 1348 20 31 29 30 31 16 | 64 49 62 57 63 57
R14 | 2114 8 7 14 12 17 6 | 33 34 39 32 27 33
R15 | 774 11 15 8 12 13 6 | 38 33 28 30 36 31
R16 | 883 24 30 66 31 19 24 | 79 88 77 80 80 79
R17E | 2306 9 14 12 14 16 7 | 40 35 41 43 27 38
R18E | 660 15 11 23 21 15 10 | 30 27 38 38 28 30
R19E | 2502 34 21 24 40 38 17 | 57 49 51 55 53 48
R20E | 2017 50 73 62 52 88 34 | 98 117 121 74 111 94
R21E | 1485 11 15 16 19 16 9 | 32 29 32 37 30 30
XR22E | 1479 --- 378 11 12 32 11 | --- 122 50 53 52 50
R24E | 3793 13 20 16 22 19 10 | 73 73 73 73 74 71
------+------------------------------------+--------------------------------
RMS | 1622 20 29 25 24 28 |T 53 54 53 55 53 51
WRMS | 1622 14 21 18 20 20 |NE 53 49 51 57 52 51
MEDI | 1171 12 17 14 19 18 |MD 53 46 50 55 52 50
Table 3.2250.6 GPS week: 2250 Day: 6 MJD: 60000
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1926 42 66 19 23 18 23 | 95 46 67 86 70 69
R02 | 673 7 17 12 10 28 6 | 82 83 81 87 92 82
R03 | 816 8 14 13 12 19 7 | 76 68 72 84 63 74
R04 | 973 9 19 9 14 22 7 | 90 93 94 91 79 90
R05 | 1982 12 13 17 11 11 8 | 77 77 80 78 76 77
R07 | 614 12 28 19 9 23 10 | 80 66 84 83 72 77
R08 | 1675 14 13 12 10 21 7 | 66 61 53 72 62 62
R09 | 829 17 14 14 24 22 10 | 68 59 67 54 66 60
R11 | 1050 10 11 11 6 21 5 | 58 55 58 61 57 57
R12 | 1355 16 16 13 20 16 9 | 55 63 55 50 62 54
R13 | 1309 17 28 34 39 24 17 | 76 76 79 72 75 73
R14 | 1603 6 12 7 11 14 5 | 45 51 48 45 39 47
R15 | 1084 13 10 14 18 16 8 | 57 51 54 48 52 51
R16 | 1346 26 33 55 27 23 21 | 121 136 117 119 120 122
R17E | 1281 13 19 12 16 34 8 | 56 63 60 59 69 57
R18E | 699 15 15 15 12 15 8 | 45 48 45 53 46 46
R19E | 3449 37 45 41 35 37 22 | 68 68 86 76 65 67
R20E | 2057 56 69 59 33 89 31 | 106 115 124 108 112 101
R21E | 1667 10 18 10 17 14 8 | 47 36 46 53 37 44
XR22E | 1685 --- 374 8 6 26 7 | --- 192 61 66 62 62
R24E | 4076 10 25 12 27 23 11 | 74 68 68 83 69 71
------+------------------------------------+--------------------------------
RMS | 1752 22 29 25 21 29 |T 72 75 71 72 68 68
WRMS | 1752 16 26 13 18 24 |NE 74 70 72 73 70 71
MEDI | 1346 13 18 13 16 22 |MD 68 66 67 72 66 67
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