[IGSREPORT-29226] Wk 2251 IGLOS Final Orbits
acc
acc at igs.org
Fri Mar 17 04:33:37 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2251 (Feb 26, 2023 - Mar 04, 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 2.2251.
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:
igl2251[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2251 in the SP3 format.
igl22517.sum Combination Report for GPS Week 2251.
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 | 0.6 ns
1 | 0.6 ns
2 | 1.8 ns
3 | -14.4 ns
4 | -12.0 ns
5 | -0.9 ns
6 | -15.3 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
2 | GFZ | R19 R20
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 1.2251, 1a.2251).
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 2.2251.0-6)
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 3.2251.0-6).
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 2251 summary. (Feb 26, 2023 - Mar 04, 2023)
Table 1.2251.a GPS week : 2251 MJD: 60001.0-60007.0
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 13 -3 33 .06 19 15 | 29767 -2756 3253 8963
| 1 0 0 14 18 17 .02 | 7860 10540
esa n/a| 0 1 -2 -16 -15 -53 -.24 30 25 | -5732 1569 3215 8838
| 1 0 1 12 10 21 .02 | 8501 1992
gfz n/a| 0 0 2 11 5 -34 -.11 40 30 | 0 1063 3213 8818
| 1 1 3 17 27 26 .03 | 0 2139
grg n/a| 2 -2 -4 -10 6 14 .25 23 18 | -6306 1045 3219 8296
| 1 0 2 23 14 30 .02 | 8169 2072
iac n/a| -2 0 -2 8 31 -55 -.22 30 25 | 7798 -225 3216 9534
| 1 1 3 33 41 126 .12 | 8155 1272
Table 1.2251.b GPS week : 2251 MJD: 60001.0-60007.0
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 30 23 23 19 21 |
R02 | 8 9 18 6 8 11 8 |
R03 | 7 7 11 9 9 6 7 |
R04 | 8 10 11 9 12 9 8 |
R05 | 11 9 10 8 8 9 10 |
R07 | 8 6 20 7 8 9 10 |
R08 | 9 6 10 10 9 7 10 |
R09 | 11 14 10 9 11 11 6 |
R11 | 7 8 8 10 9 7 7 |
R12 | 9 7 14 10 12 7 7 |
R13 | 19 10 26 20 20 15 13 |
R14 | 7 6 12 7 7 7 9 |
R15 | 9 5 9 8 9 7 8 |
R16 | 24 19 19 22 25 22 23 |
R17 | 10 9 13 8 10 12 9 |
R18 | 7 9 10 8 8 9 13 |
R19 | 22 28 28 22 24 18 19 |
R20 | 31 30 32 36 37 35 31 |
R21 | 7 11 15 8 8 8 8 |
R22 | 12 12 12 9 9 11 10 |
R24 | 11 13 22 11 13 9 11 |
Table 1.2251.c GPS week : 2251 MJD: 60001.0-60007.0
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 2251 0 | -23 9 58 11 688 -2272 82.0 1860 1860 | 577 0
brd 2251 1 | 25 -19 148 2176 2489 1816 81.5 1765 1765 | 563 0
brd 2251 2 | -24 -18 114 -520 1014 2751 77.8 2101 2101 | 1779 0
brd 2251 3 | 29 -12 11 -103 344 -4983 81.3 1859 1859 | -14372 0
brd 2251 4 | -15 37 -71 -1194 -188 -4989 81.2 1446 1446 | -12039 0
brd 2251 5 | -36 -88 41 950 -899 -5007 80.6 1482 1482 | -891 0
brd 2251 6 | 51 48 136 91 -567 199 79.7 1436 1436 | -15306 0
-------------+------------------------------------------------------------+----------------
brd 2251 mean| 0 -6 62 201 411 -1783 80.6 1707 1707 | -5669 0
brd 2251 sdev| 33 45 77 1085 1140 3381 1.5 257 257 | 7803 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 2.2251.0 GPS week: 2251 Day: 0 MJD: 60001
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 4 -8 -4 7 .04 19 14 | 37812 -26221 3025 10346
esa n/a| 0 2 -1 -1 -23 -27 -.27 31 26 | -10403 1332 2994 8492
gfz n/a| 0 -1 3 24 -1 -27 -.12 25 15 | 0 525 2999 10160
grg n/a| 1 -1 -9 -6 12 20 .27 23 20 | 183 488 3007 9589
iac n/a| -3 1 4 -21 5 -35 -.19 30 25 | 13688 -54 2992 10734
Table 2.2251.1 GPS week: 2251 Day: 1 MJD: 60002
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 3 36 28 45 .06 21 15 | 32902 -87 2916 9701
esa n/a| 1 2 -4 -28 -8 -83 -.25 30 33 | 3488 889 2880 7673
gfz n/a| 3 2 4 -13 -27 -30 -.10 25 17 | 0 612 2872 9485
grg n/a| 1 -3 -5 -2 -14 29 .23 19 18 | 240 526 2871 8800
iac n/a| -2 -1 -1 48 84 -130 -.23 28 25 | 14783 -1531 2876 10150
Table 2.2251.2 GPS week: 2251 Day: 2 MJD: 60003
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 3 -13 18 .07 20 16 | 34829 2530 3270 8090
esa n/a| 0 0 -1 -36 -1 -41 -.26 28 24 | 6704 2641 3241 10955
gfz n/a| 1 0 8 8 18 -82 -.13 123 70 | 0 3347 3193 7965
grg n/a| 2 -3 -3 25 0 50 .23 19 15 | 382 2642 3251 7789
iac n/a| -1 1 -5 35 -44 -147 -.38 31 30 | 14821 1340 3233 8730
Table 2.2251.3 GPS week: 2251 Day: 3 MJD: 60004
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 10 4 37 .04 20 17 | 20074 -401 3935 8656
esa n/a| -1 1 0 -14 -12 -67 -.21 31 28 | -9356 -314 3887 7230
gfz n/a| 0 2 2 38 -32 -58 -.15 27 15 | 0 -356 3923 8461
grg n/a| 2 -2 -6 -17 25 27 .26 22 17 | -14120 -580 3886 8078
iac n/a| 0 0 -7 -36 29 91 -.34 30 27 | -932 -1029 3914 9189
Table 2.2251.4 GPS week: 2251 Day: 4 MJD: 60005
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 26 -32 34 .09 22 17 | 23107 4224 3432 8009
esa n/a| 0 0 -4 -13 -34 -67 -.22 30 22 | -16404 4555 3389 6919
gfz n/a| 0 0 -1 8 44 -12 -.06 25 33 | 0 3645 3392 8080
grg n/a| 3 -2 -4 -53 11 -6 .29 30 20 | -14322 4128 3407 7356
iac n/a| -2 2 -3 29 45 132 -.19 28 23 | 1015 1202 3393 8770
Table 2.2251.5 GPS week: 2251 Day: 5 MJD: 60006
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 11 -10 31 .07 16 10 | 37956 -1624 3025 9183
esa n/a| 0 1 -3 -5 -10 -27 -.24 28 20 | -2521 -1167 2998 12370
gfz n/a| -2 0 0 -4 11 -7 -.11 28 23 | 0 -2407 2996 8993
grg n/a| 3 -2 -2 -2 17 -44 .25 25 19 | 51 -2011 2998 8485
iac n/a| -4 1 -3 24 43 -90 -.02 29 24 | 13804 -1823 2994 9904
Table 2.2251.6 GPS week: 2251 Day: 6 MJD: 60007
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 3 15 1 60 .04 16 12 | 21694 2287 3172 8759
esa n/a| -1 1 -3 -13 -20 -61 -.26 30 21 | -11632 3053 3117 8229
gfz n/a| -1 0 0 17 25 -24 -.11 28 36 | 0 2078 3118 8585
grg n/a| 2 -2 -1 -20 -8 23 .23 19 16 | -16556 2126 3114 7981
iac n/a| 0 0 -2 -17 55 -209 -.17 31 24 | -2591 316 3110 9263
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 3.2251.0 GPS week: 2251 Day: 0 MJD: 60001
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1728 31 66 14 19 27 20 | 134 66 113 109 99 108
R02 | 695 8 15 16 16 14 8 | 120 121 118 119 115 118
R03 | 1278 7 17 13 9 21 6 | 108 98 109 110 122 106
R04 | 1133 7 19 13 13 23 7 | 111 110 115 115 118 112
R05 | 2424 12 24 16 20 16 10 | 114 118 109 108 114 111
R07 | 603 13 20 14 9 22 8 | 97 85 101 97 95 95
R08 | 1542 7 21 16 16 26 8 | 95 95 102 106 89 99
R09 | 954 19 11 18 22 20 10 | 53 39 49 40 40 43
R11 | 1163 12 15 14 10 26 7 | 29 39 44 36 44 35
R12 | 904 8 15 13 23 13 9 | 30 37 35 23 30 28
R13 | 1071 9 31 29 51 28 19 | 55 53 52 56 50 50
R14 | 1240 14 9 9 11 13 6 | 37 40 36 29 39 34
R15 | 759 13 25 10 9 17 8 | 48 47 49 47 45 46
R16 | 1621 26 34 65 29 30 23 | 76 88 84 69 79 78
R17E | 2747 7 19 18 23 28 10 | 134 133 136 138 137 134
R18E | 571 5 15 14 13 13 7 | 34 33 34 40 32 34
R19E | 3473 38 50 39 24 37 22 | 105 113 134 111 109 109
R20E | 2095 47 74 55 43 92 31 | 113 132 128 109 130 117
R21E | 1583 9 13 14 14 15 7 | 37 38 40 45 39 38
XR22E | 1747 --- 353 11 12 36 12 | --- 133 66 70 68 66
R24E | 4286 13 23 12 23 22 10 | 124 132 130 143 128 130
------+------------------------------------+--------------------------------
RMS | 1860 19 31 25 23 30 |T 82 83 84 81 82 80
WRMS | 1860 14 26 15 20 25 |NE 79 74 79 76 77 75
MEDI | 1278 12 20 14 16 22 |MD 95 88 101 97 89 95
Table 3.2251.1 GPS week: 2251 Day: 1 MJD: 60002
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 492 36 64 26 17 31 21 | 100 52 97 79 67 81
R02 | 603 11 14 17 15 10 8 | 109 105 126 104 105 109
R03 | 968 9 16 7 13 9 6 | 91 87 89 94 89 90
R04 | 1452 12 15 21 16 25 9 | 94 87 82 96 94 89
R05 | 1964 12 18 17 11 29 8 | 104 114 99 106 88 105
R07 | 933 6 12 11 8 15 5 | 75 73 77 74 71 74
R08 | 1184 9 11 11 5 17 5 | 76 69 78 75 70 75
R09 | 764 25 16 24 29 18 14 | 57 41 50 47 49 45
R11 | 1005 12 17 15 9 29 7 | 40 50 57 51 51 47
R12 | 730 13 10 7 15 23 7 | 35 35 33 32 33 32
R13 | 1296 10 21 14 22 15 10 | 44 43 56 41 39 42
R14 | 884 6 12 10 14 18 6 | 37 42 43 42 35 39
R15 | 801 9 9 8 9 24 5 | 44 41 42 44 44 42
R16 | 1955 19 28 54 21 33 19 | 53 51 57 45 47 49
R17E | 3644 7 22 9 21 15 9 | 116 109 113 123 110 115
R18E | 556 9 19 18 12 20 8 | 49 48 49 45 43 46
R19E | 2084 45 56 53 39 46 27 | 74 90 117 73 80 73
R20E | 1104 53 70 48 30 70 29 | 109 107 105 107 118 99
R21E | 1155 14 22 15 21 20 10 | 49 53 58 49 46 48
XR22E | 1635 --- 341 12 10 31 11 | --- 133 76 76 71 75
R24E | 4792 18 30 17 26 15 13 | 104 118 107 116 106 110
------+------------------------------------+--------------------------------
RMS | 1765 21 30 25 19 28 |T 73 73 76 72 69 70
WRMS | 1765 15 33 17 18 25 |NE 68 63 70 66 63 65
MEDI | 1104 12 18 15 15 20 |MD 74 69 77 74 70 74
Table 3.2251.2 GPS week: 2251 Day: 2 MJD: 60003
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 546 36 63 106 12 29 29 | 111 53 138 97 95 88
R02 | 895 14 19 83 16 25 17 | 86 99 133 81 87 89
R03 | 1155 12 25 35 9 45 11 | 86 71 104 86 116 82
R04 | 1520 10 24 26 16 23 10 | 98 87 100 102 101 95
R05 | 2088 12 14 34 16 19 9 | 111 103 120 109 112 109
R07 | 766 17 19 98 16 30 20 | 78 67 127 76 80 74
R08 | 808 12 15 39 14 21 10 | 79 74 93 88 87 80
R09 | 1118 17 13 23 17 15 10 | 29 30 24 29 21 23
R11 | 745 13 8 25 11 20 7 | 22 24 31 25 28 21
R12 | 677 16 24 24 29 20 13 | 32 39 34 30 42 27
R13 | 1199 22 30 116 32 21 26 | 52 30 107 52 48 43
R14 | 833 10 13 55 11 23 11 | 31 36 63 31 45 32
R15 | 770 14 17 20 9 21 8 | 33 27 25 29 42 27
R16 | 2123 22 24 88 11 22 19 | 38 33 47 44 41 36
R17E | 4386 13 18 48 17 14 12 | 72 77 104 72 66 74
R18E | 565 12 12 32 16 18 9 | 25 24 43 32 26 24
R19E | 1466 45 37 313 35 58 28 | 106 128 324 113 118 113
R20E | 781 35 63 358 35 74 31 | 73 103 292 75 89 76
R21E | 905 12 20 69 14 24 15 | 21 25 73 28 27 22
XR22E | 1507 --- 333 20 7 23 11 | --- 128 35 33 32 30
R24E | 6732 21 25 104 19 23 22 | 56 56 130 60 54 57
------+------------------------------------+--------------------------------
RMS | 2101 20 28 123 19 31 |T 61 62 102 61 64 58
WRMS | 2101 16 24 70 15 30 |NE 63 55 81 62 67 59
MEDI | 905 14 20 48 16 23 |MD 56 56 100 60 54 57
Table 3.2251.3 GPS week: 2251 Day: 3 MJD: 60004
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 679 48 55 19 22 30 22 | 122 52 96 85 92 89
R02 | 1037 10 11 11 9 24 6 | 83 82 68 82 90 79
R03 | 1457 8 22 19 10 27 8 | 95 86 113 95 111 97
R04 | 1216 9 19 11 19 21 8 | 84 69 78 92 93 81
R05 | 1148 10 18 15 11 24 7 | 84 77 95 92 93 86
R07 | 621 9 16 12 10 21 7 | 87 75 94 87 80 85
R08 | 740 18 20 14 16 19 10 | 80 86 92 75 79 82
R09 | 845 11 14 11 20 25 8 | 17 18 22 23 27 17
R11 | 809 11 12 27 15 27 10 | 20 29 39 19 30 23
R12 | 685 12 18 15 24 19 10 | 26 28 29 20 30 20
R13 | 738 28 38 34 36 36 19 | 45 32 46 32 47 34
R14 | 685 14 11 7 14 30 7 | 30 25 29 20 39 23
R15 | 863 11 17 9 15 36 7 | 35 34 32 28 48 30
R16 | 1708 26 34 60 24 21 22 | 39 40 38 37 43 34
R17E | 3688 11 17 12 16 23 8 | 43 46 35 42 49 38
R18E | 1086 10 16 14 13 18 7 | 26 27 25 29 26 24
R19E | 903 40 36 41 29 53 21 | 74 87 106 89 109 82
R20E | 1351 31 91 69 55 64 36 | 127 157 185 111 136 128
R21E | 547 9 18 14 15 16 8 | 21 26 30 26 29 21
XR22E | 1995 --- 311 9 7 20 8 | --- 92 23 26 20 23
R24E | 6122 16 23 20 17 19 11 | 27 35 23 36 33 25
------+------------------------------------+--------------------------------
RMS | 1859 20 31 27 22 30 |T 58 57 61 54 62 53
WRMS | 1859 17 28 15 17 27 |NE 60 52 62 56 64 55
MEDI | 903 11 18 14 16 24 |MD 43 46 39 37 48 34
Table 3.2251.4 GPS week: 2251 Day: 4 MJD: 60005
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1427 50 48 20 26 25 22 | 113 62 76 75 82 80
R02 | 1167 10 16 9 18 15 7 | 99 102 90 93 88 96
R03 | 1711 9 23 12 18 15 9 | 98 80 92 107 91 94
R04 | 1350 18 23 24 12 28 11 | 96 91 115 97 92 99
R05 | 938 8 12 18 13 18 7 | 101 95 105 102 104 100
R07 | 826 7 16 13 17 19 7 | 85 77 94 98 95 87
R08 | 1012 16 18 11 18 23 9 | 81 85 86 90 74 85
R09 | 733 20 14 19 17 22 10 | 54 56 63 58 45 55
R11 | 1004 18 14 15 14 19 9 | 37 43 47 52 40 42
R12 | 946 10 17 22 29 18 11 | 41 47 52 38 36 41
R13 | 849 22 23 22 64 28 20 | 57 48 57 44 44 47
R14 | 1058 7 13 10 16 20 6 | 44 51 51 43 49 46
R15 | 1714 16 24 8 14 24 9 | 55 51 55 57 58 52
R16 | 1298 26 27 66 38 28 24 | 57 56 64 61 49 58
R17E | 3248 14 21 15 16 17 9 | 101 102 102 98 92 99
R18E | 813 10 15 13 15 19 7 | 51 54 54 56 42 51
R19E | 678 33 38 43 50 47 23 | 97 128 169 110 117 114
R20E | 946 45 95 45 65 74 36 | 90 87 88 119 105 79
R21E | 569 9 14 13 21 11 8 | 49 53 50 56 47 50
XR22E | 2899 --- 339 9 8 28 9 | --- 107 58 61 50 58
R24E | 3045 16 18 19 32 31 12 | 85 90 85 97 88 85
------+------------------------------------+--------------------------------
RMS | 1446 22 30 25 30 28 |T 74 74 78 76 70 72
WRMS | 1446 17 22 33 20 23 |NE 72 67 74 72 67 70
MEDI | 1012 16 18 15 18 22 |MD 81 77 76 75 74 79
Table 3.2251.5 GPS week: 2251 Day: 5 MJD: 60006
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1332 27 48 27 32 22 19 | 98 78 75 108 92 90
R02 | 1296 11 26 15 24 19 11 | 68 80 63 62 65 66
R03 | 2019 3 12 7 16 20 5 | 86 82 83 96 87 86
R04 | 1055 9 23 13 16 17 9 | 96 92 101 102 90 96
R05 | 1674 10 18 23 13 24 9 | 94 96 106 94 99 96
R07 | 903 8 13 19 19 24 8 | 79 71 60 84 86 74
R08 | 1325 7 14 11 13 15 6 | 71 75 70 79 76 73
R09 | 1168 14 18 26 21 23 11 | 35 29 41 30 33 31
R11 | 870 8 15 13 10 30 6 | 17 29 26 22 29 21
R12 | 1624 7 11 10 18 26 6 | 39 45 48 37 46 41
R13 | 916 17 17 25 41 18 14 | 43 50 67 34 52 44
R14 | 836 7 14 15 13 20 7 | 32 36 24 26 38 29
R15 | 2083 9 16 12 12 15 7 | 38 52 51 39 39 42
R16 | 1634 24 26 66 19 20 21 | 47 49 54 43 41 46
R17E | 1920 8 19 24 30 19 11 | 107 103 107 121 108 107
R18E | 590 8 20 16 20 24 9 | 40 40 35 48 31 39
R19E | 2734 24 26 41 32 47 17 | 75 83 93 78 79 77
R20E | 1043 40 84 62 60 76 34 | 156 184 171 154 162 158
R21E | 972 6 16 16 16 17 7 | 29 30 26 31 35 26
XR22E | 3053 --- 338 10 11 19 11 | --- 106 44 49 48 45
R24E | 1734 9 17 11 23 29 8 | 90 92 99 100 95 93
------+------------------------------------+--------------------------------
RMS | 1481 16 28 28 25 29 |T 67 71 68 68 68 65
WRMS | 1481 10 20 23 19 24 |NE 60 61 62 61 62 59
MEDI | 1325 9 18 16 19 20 |MD 68 75 63 62 65 66
Table 3.2251.6 GPS week: 2251 Day: 6 MJD: 60007
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 916 32 58 22 26 20 20 | 136 73 94 115 111 107
R02 | 1183 9 22 11 10 20 7 | 86 98 82 88 81 88
R03 | 1198 5 20 9 14 19 7 | 111 99 112 117 110 110
R04 | 863 13 17 9 13 53 7 | 117 116 119 117 115 117
R05 | 2266 17 21 15 14 18 9 | 118 116 127 119 125 119
R07 | 1516 13 30 8 12 15 9 | 98 81 95 97 95 93
R08 | 1124 8 16 23 20 18 10 | 92 87 86 97 88 90
R09 | 1266 8 14 10 11 26 6 | 33 31 31 31 35 30
R11 | 690 9 14 14 9 12 6 | 21 24 30 24 26 22
R12 | 1859 8 14 10 13 14 6 | 39 54 50 41 42 44
R13 | 1188 14 28 22 23 38 12 | 62 61 71 56 74 60
R14 | 805 7 10 18 21 16 8 | 40 49 54 32 46 41
R15 | 1477 14 16 6 14 12 7 | 47 48 47 43 51 44
R16 | 1367 19 29 70 27 23 23 | 54 46 59 44 59 49
R17E | 1216 7 18 13 20 18 8 | 123 123 122 126 127 123
R18E | 741 15 17 27 27 16 12 | 83 78 86 60 71 75
R19E | 2576 32 23 49 22 54 19 | 109 120 139 118 125 115
R20E | 2180 27 84 68 30 84 30 | 145 179 150 137 149 143
R21E | 592 11 14 12 14 17 7 | 27 28 28 27 27 26
XR22E | 3453 --- 330 10 8 23 9 | --- 137 42 47 49 44
R24E | 1640 12 19 18 26 26 11 | 109 114 119 118 117 113
------+------------------------------------+--------------------------------
RMS | 1436 16 30 28 19 31 |T 82 83 83 78 82 78
WRMS | 1436 12 21 36 16 24 |NE 75 70 75 72 75 72
MEDI | 1216 12 19 14 14 19 |MD 86 81 86 88 81 88
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