[IGSREPORT-29165] Wk 2245 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 3 07:58:33 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2245 (Jan 15, 2023 - Jan 21, 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 2.2245.
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:
igl2245[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2245 in the SP3 format.
igl22457.sum Combination Report for GPS Week 2245.
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 | -0.4 ns
1 | -0.9 ns
2 | -0.3 ns
3 | -0.0 ns
4 | 0.5 ns
5 | -15.3 ns
6 | 0.2 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
----+--------+---------------
5 | ESA | R20 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 1.2245, 1a.2245).
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 2.2245.0-6)
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 3.2245.0-6).
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 2245 summary. (Jan 15, 2023 - Jan 21, 2023)
Table 1.2245.a GPS week : 2245 MJD: 59959.0-59965.0
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 0 -16 -12 53 .03 19 18 | 33457 -362 3196 8825
| 0 0 0 14 11 19 .04 | 6054 1355
esa n/a| 0 0 -1 -20 30 -28 -.24 43 29 | 2353 -578 3187 7562
| 1 1 1 10 10 35 .06 | 12106 1481
gfz n/a| 0 1 2 17 4 -30 -.08 24 18 | 0 -192 3192 8702
| 0 0 2 14 10 26 .07 | 0 1472
grg n/a| 1 -3 0 7 -16 -17 .22 28 23 | -2306 -258 3167 8076
| 0 2 2 25 17 53 .03 | 6295 1582
iac n/a| -2 1 -2 -15 -6 5 -.20 28 24 | -508 -21 3175 9121
| 2 2 2 22 30 176 .09 | 5712 637
Table 1.2245.b GPS week : 2245 MJD: 59959.0-59965.0
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 | 17 18 19 20 20 18 34 |
R02 | 7 8 7 8 5 6 10 |
R03 | 6 7 7 9 8 9 9 |
R04 | 7 9 7 7 7 6 10 |
R05 | 7 7 6 8 8 7 9 |
R07 | 7 9 8 9 10 8 8 |
R08 | 8 11 11 7 11 11 9 |
R09 | 13 10 9 11 10 12 10 |
R11 | 8 7 11 11 9 8 9 |
R12 | 9 9 6 10 9 9 17 |
R13 | 19 17 22 21 17 19 16 |
R14 | 9 8 7 10 7 8 8 |
R15 | 11 9 7 11 9 7 11 |
R16 | 24 24 26 23 23 24 22 |
R17 | 8 10 10 11 7 8 11 |
R18 | 11 9 8 9 9 6 6 |
R19 | 23 27 26 33 26 29 30 |
R20 | 39 36 39 46 43 33 46 |
R21 | 8 7 9 12 9 11 11 |
R22 | 159 155 156 165 168 12 14 |
R24 | 13 13 14 16 13 12 14 |
Table 1.2245.c GPS week : 2245 MJD: 59959.0-59965.0
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 2245 0 | 17 -24 8 -1583 315 -3727 80.7 1450 1450 | -422 0
brd 2245 1 | -25 -88 -13 -223 90 -5770 80.3 1259 1259 | -928 0
brd 2245 2 | 14 0 -9 -1254 360 -9419 81.7 1142 1142 | -257 0
brd 2245 3 | 24 -34 30 -698 485 -8336 81.1 1272 1272 | -1 0
brd 2245 4 | 3 66 74 89 1594 -7862 82.4 1153 1153 | 487 0
brd 2245 5 | 53 18 32 1379 1487 -5855 81.8 956 956 | -15271 0
brd 2245 6 | -6 90 -11 656 946 -8824 78.8 1434 1434 | 205 0
-------------+------------------------------------------------------------+----------------
brd 2245 mean| 11 3 15 -233 754 -7113 81.0 1238 1238 | -2312 0
brd 2245 sdev| 25 61 32 1046 597 2047 1.2 173 173 | 5732 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 2.2245.0 GPS week: 2245 Day: 0 MJD: 59959
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 1 -37 -10 68 -.04 21 20 | 36857 -1325 3217 8183
esa n/a| 0 1 -1 -18 23 -84 -.28 40 25 | 813 -1849 3247 7023
gfz n/a| 0 1 0 -7 3 -67 -.01 17 11 | 0 -1409 3217 8121
grg n/a| 2 -6 4 51 -15 63 .21 30 25 | 363 -1954 3244 7544
iac n/a| -2 0 -5 -10 6 -16 -.33 24 20 | 1054 -250 3234 8482
Table 2.2245.1 GPS week: 2245 Day: 1 MJD: 59960
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 0 -7 -11 48 .04 17 16 | 35881 -1832 3685 8795
esa n/a| -2 0 0 -29 22 -28 -.30 42 29 | 6430 -1536 3651 6576
gfz n/a| -1 2 1 3 -1 -11 -.08 21 14 | 0 -2121 3677 8784
grg n/a| 2 -6 0 13 -8 -46 .23 26 22 | 23 -2108 3647 8050
iac n/a| -2 -2 -7 18 7 75 -.27 24 19 | 1517 -1091 3652 9254
Table 2.2245.2 GPS week: 2245 Day: 2 MJD: 59961
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 1 -24 1 48 .07 15 14 | 35130 -979 3045 9228
esa n/a| 1 0 -1 -11 29 -24 -.29 45 30 | 7944 -921 3043 7460
gfz n/a| 0 2 1 20 -12 -49 -.15 26 30 | 0 -762 3060 9082
grg n/a| 1 -4 -4 -8 -3 -1 .26 27 19 | -128 -627 3011 8322
iac n/a| -2 2 -2 -23 -8 -17 -.21 26 23 | 1417 -345 3026 9403
Table 2.2245.3 GPS week: 2245 Day: 3 MJD: 59962
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 0 1 -8 38 .02 21 20 | 35129 -812 2915 9277
esa n/a| -1 2 0 -24 38 -34 -.28 40 31 | 11189 -1309 2891 8716
gfz n/a| 0 1 2 29 12 -27 .03 29 16 | 0 -675 2915 9284
grg n/a| 2 -4 0 -10 -45 18 .20 30 24 | 300 -695 2871 8529
iac n/a| -2 0 -1 -46 19 -234 -.21 29 20 | 2060 -101 2871 9578
Table 2.2245.4 GPS week: 2245 Day: 4 MJD: 59963
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 0 0 -12 79 .02 19 14 | 34811 857 2994 8881
esa n/a| 0 0 -3 -35 50 -56 -.24 45 32 | 562 674 3015 7783
gfz n/a| 0 1 2 25 14 -52 -.10 23 21 | 0 460 3019 8796
grg n/a| 2 -1 -2 -3 -39 -15 .23 24 21 | -210 1171 2994 8046
iac n/a| -2 4 -3 0 26 282 -.25 34 31 | 2252 278 3019 9193
Table 2.2245.5 GPS week: 2245 Day: 5 MJD: 59964
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 0 -22 -37 21 .07 20 21 | 19839 2057 2990 8059
esa n/a| 0 0 0 -19 27 10 -.18 46 30 | -23019 2223 2952 7103
gfz n/a| 0 1 2 18 14 0 -.13 22 12 | 0 2100 2966 7691
grg n/a| 0 -2 0 31 -2 -37 .22 27 25 | -16576 2227 2950 7519
iac n/a| -7 3 1 -9 -49 126 -.05 30 29 | -13431 848 2963 8339
Table 2.2245.6 GPS week: 2245 Day: 6 MJD: 59965
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 0 -22 -7 68 .04 21 20 | 36556 -501 3529 9357
esa n/a| 1 2 -5 -6 20 16 -.14 41 27 | 12557 -1328 3510 8275
gfz n/a| 0 0 6 35 0 -3 -.15 32 22 | 0 1062 3491 9156
grg n/a| 1 -2 -2 -19 -4 -106 .17 33 24 | 81 174 3456 8525
iac n/a| 2 0 -2 -35 -46 -175 -.12 31 24 | 1575 511 3463 9600
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 3.2245.0 GPS week: 2245 Day: 0 MJD: 59959
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 879 19 41 30 26 35 16 | 76 60 87 73 100 74
R02E | 1289 11 11 9 15 11 6 | 111 105 105 117 102 108
R03E | 1157 8 13 7 16 22 6 | 38 35 36 52 36 38
R04E | 791 10 12 10 14 16 6 | 122 120 121 132 121 123
R05E | 2262 11 14 11 12 10 6 | 73 76 78 80 73 76
R07E | 1115 12 14 12 13 18 7 | 66 64 70 74 63 68
R08E | 611 10 16 9 23 20 8 | 194 190 194 200 190 194
R09 | 1921 16 21 12 40 26 12 | 47 45 40 37 41 38
R11 | 508 12 13 14 14 24 7 | 26 26 41 35 30 31
R12 | 1055 12 15 8 24 19 8 | 45 34 43 39 45 39
R13 | 2114 36 42 11 40 18 18 | 52 30 38 32 36 35
R14 | 1219 11 14 14 21 17 8 | 40 52 56 44 50 47
R15 | 728 24 17 10 21 16 10 | 59 46 49 44 51 49
R16 | 1600 33 39 49 36 34 23 | 133 123 127 126 129 128
R17 | 860 11 21 8 17 15 7 | 62 51 55 68 61 58
R18 | 743 26 14 8 25 11 11 | 50 67 66 79 57 62
R19 | 2586 34 72 10 46 42 23 | 117 56 96 116 104 97
R20 | 993 44 131 31 71 43 39 | 137 70 137 138 132 116
R21 | 997 11 24 7 15 22 8 | 78 63 84 85 90 78
XR22 | 1419 --- 170 --- 148 140 159 | --- 112 --- 50 51 80
R24 | 2614 10 38 10 30 24 12 | 89 64 87 96 89 85
------+------------------------------------+--------------------------------
RMS | 1450 21 40 17 30 24 |T 80 70 80 81 78 77
WRMS | 1450 20 25 11 25 20 |NE 71 59 70 70 69 67
MEDI | 1115 12 17 10 23 20 |MD 66 63 70 74 63 74
Table 3.2245.1 GPS week: 2245 Day: 1 MJD: 59960
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 893 16 38 37 31 48 17 | 57 53 75 54 66 56
R02E | 1122 8 14 15 16 15 7 | 54 53 54 56 53 53
R03E | 1305 6 11 12 17 21 6 | 36 35 33 43 39 34
R04E | 654 10 15 15 20 20 8 | 68 67 68 67 68 66
R05E | 1205 12 11 12 12 12 7 | 52 49 47 51 52 49
R07E | 1650 11 14 9 24 13 8 | 50 49 52 56 56 49
R08E | 1284 11 23 16 29 15 11 | 125 111 119 129 124 121
R09 | 1000 11 21 14 26 11 10 | 41 46 42 33 35 38
R11 | 736 12 14 11 12 16 7 | 24 19 33 28 23 25
R12 | 1223 13 15 10 26 21 9 | 30 20 31 26 41 26
R13 | 1390 30 34 20 36 13 17 | 37 33 39 30 29 33
R14 | 1313 12 9 13 19 21 8 | 28 33 33 24 36 28
R15 | 829 17 14 14 17 25 9 | 40 39 25 29 44 32
R16 | 2127 27 33 61 27 24 23 | 104 101 99 95 103 101
R17 | 865 5 22 13 29 13 10 | 34 31 27 45 31 32
R18 | 883 13 21 9 20 20 9 | 28 35 28 44 32 31
R19 | 1049 30 86 18 54 47 27 | 67 34 65 61 78 59
R20 | 2109 33 134 31 37 32 35 | 74 61 70 96 59 68
R21 | 739 6 17 11 10 30 6 | 41 39 40 46 58 41
XR22 | 1938 --- 176 --- 135 129 154 | --- 40 --- 27 29 37
R24 | 1460 10 42 13 23 21 12 | 41 30 45 51 43 42
------+------------------------------------+--------------------------------
RMS | 1258 17 42 21 26 24 |T 51 46 51 51 52 48
WRMS | 1258 16 29 14 22 19 |NE 45 40 44 45 45 42
MEDI | 1205 12 21 13 24 21 |MD 41 39 42 46 44 41
Table 3.2245.2 GPS week: 2245 Day: 2 MJD: 59961
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 845 17 46 35 37 65 18 | 56 63 74 61 82 56
R02E | 1250 10 14 13 12 22 7 | 56 62 62 62 48 59
R03E | 1388 10 15 9 13 13 6 | 51 60 55 62 58 55
R04E | 756 8 17 11 13 18 6 | 59 62 55 59 54 57
R05E | 1604 8 13 8 13 20 6 | 34 34 36 42 38 35
R07E | 1172 10 18 13 13 18 7 | 43 49 43 47 41 43
R08E | 1876 9 20 14 31 15 10 | 97 108 100 112 102 101
R09 | 735 10 17 14 20 16 8 | 28 34 44 21 40 30
R11 | 1004 11 25 17 23 18 10 | 25 38 35 30 34 27
R12 | 1426 6 15 10 10 26 5 | 34 32 37 34 22 33
R13 | 1030 21 40 31 60 29 21 | 36 30 47 34 15 34
R14 | 631 9 12 11 13 12 6 | 27 34 33 28 28 29
R15 | 1319 8 12 14 17 20 7 | 43 56 59 38 57 47
R16 | 1067 25 23 69 43 35 25 | 87 96 97 83 102 90
R17 | 786 9 27 16 17 15 9 | 45 38 51 49 34 45
R18 | 741 15 17 11 11 20 8 | 36 43 41 42 45 38
R19 | 734 27 98 14 44 18 26 | 89 37 80 90 68 79
R20 | 1664 26 144 63 40 37 39 | 93 42 116 87 98 87
R21 | 734 11 21 17 12 16 8 | 54 53 68 67 66 59
XR22 | 2306 --- 191 --- 126 118 155 | --- 79 --- 33 29 49
R24 | 938 18 50 11 11 23 13 | 66 50 61 63 60 60
------+------------------------------------+--------------------------------
RMS | 1141 15 45 26 27 26 |T 52 52 59 54 53 53
WRMS | 1141 14 30 30 19 23 |NE 51 47 59 49 49 50
MEDI | 1030 10 20 14 17 20 |MD 45 49 55 49 48 49
Table 3.2245.3 GPS week: 2245 Day: 3 MJD: 59962
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 804 31 36 46 21 66 20 | 88 76 90 78 93 81
R02E | 1088 8 12 11 19 17 7 | 42 44 45 52 37 44
R03E | 1354 11 11 17 21 12 9 | 58 63 60 75 49 61
R04E | 811 9 10 9 16 11 6 | 46 49 51 50 44 48
R05E | 1217 12 11 14 17 13 8 | 43 45 45 42 47 42
R07E | 756 9 13 19 21 15 9 | 51 55 60 46 61 52
R08E | 2385 6 12 12 17 16 6 | 44 44 40 49 41 43
R09 | 748 13 16 14 30 26 11 | 41 49 41 31 33 36
R11 | 836 16 16 16 27 15 11 | 20 28 29 35 15 22
R12 | 1849 17 14 11 25 20 10 | 36 25 33 37 31 30
R13 | 1258 23 35 34 51 41 20 | 55 41 48 65 21 48
R14 | 641 12 11 9 28 19 9 | 38 47 44 55 37 43
R15 | 1563 19 13 14 24 23 10 | 43 37 35 55 45 39
R16 | 1017 27 17 61 35 17 22 | 56 56 62 55 56 55
R17 | 787 19 15 9 26 23 10 | 69 64 66 67 70 64
R18 | 554 14 9 17 18 17 8 | 41 49 59 59 43 49
R19 | 772 50 94 21 47 33 33 | 104 40 77 95 66 76
R20 | 1773 40 126 82 62 65 46 | 107 36 120 103 116 88
R21 | 592 11 25 23 25 24 12 | 52 51 69 61 61 56
XR22 | 2632 --- 162 --- 166 157 164 | --- 90 --- 39 26 88
R24 | 2262 23 41 15 26 15 15 | 74 46 59 82 59 64
------+------------------------------------+--------------------------------
RMS | 1272 21 40 29 30 29 |T 55 49 56 58 50 53
WRMS | 1272 20 31 16 24 20 |NE 56 47 57 59 48 54
MEDI | 1017 14 15 15 25 19 |MD 46 47 51 55 45 49
Table 3.2245.4 GPS week: 2245 Day: 4 MJD: 59963
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1165 28 38 39 31 98 19 | 71 76 83 67 116 70
R02E | 587 7 11 8 11 22 5 | 56 59 58 64 39 58
R03E | 1772 10 13 11 21 27 8 | 55 59 61 60 60 56
R04E | 544 9 10 10 18 25 7 | 47 54 53 48 40 49
R05E | 1499 13 10 14 13 19 7 | 38 40 49 51 39 43
R07E | 1303 9 15 18 24 31 9 | 60 60 56 78 47 61
R08E | 1619 9 22 19 25 26 11 | 79 82 75 82 68 77
R09 | 1117 13 15 20 19 21 9 | 39 44 46 28 45 37
R11 | 665 7 14 16 20 24 8 | 25 26 29 30 34 25
R12 | 1605 17 21 7 15 18 8 | 38 27 35 28 25 32
R13 | 880 27 35 23 35 33 17 | 48 30 33 29 29 34
R14 | 1175 7 14 12 15 20 7 | 37 49 44 34 34 39
R15 | 1309 14 12 12 20 29 8 | 47 48 56 39 42 46
R16 | 744 26 29 61 29 31 23 | 75 68 78 65 65 73
R17 | 576 9 18 8 11 30 6 | 39 37 41 41 47 39
R18 | 743 9 18 14 19 15 8 | 33 44 33 37 36 33
R19 | 690 37 80 16 45 28 25 | 69 32 48 62 57 54
R20 | 791 42 159 48 38 48 42 | 95 54 90 83 82 74
R21 | 516 7 27 14 13 19 8 | 40 34 53 49 44 44
XR22 | 2924 --- 207 --- 136 121 168 | --- 105 --- 30 22 65
R24 | 1985 14 47 8 16 25 12 | 64 41 55 63 51 56
------+------------------------------------+--------------------------------
RMS | 1153 19 45 23 24 34 |T 52 50 53 50 48 50
WRMS | 1153 14 32 21 21 31 |NE 49 45 49 44 43 46
MEDI | 1117 10 18 14 20 26 |MD 47 48 53 49 44 49
Table 3.2245.5 GPS week: 2245 Day: 5 MJD: 59964
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 862 29 23 35 30 83 17 | 84 87 94 91 91 84
R02E | 698 6 12 9 14 17 6 | 91 86 85 87 81 87
R03E | 1164 13 14 12 18 23 8 | 72 74 66 74 62 70
R04E | 806 7 14 8 11 25 6 | 103 104 98 102 92 101
R05E | 587 7 10 10 17 22 6 | 54 52 49 58 52 52
R07E | 1050 10 11 12 22 21 8 | 64 68 66 74 63 66
R08E | 1155 13 22 15 25 21 10 | 173 177 180 173 170 176
R09 | 603 18 13 21 25 28 11 | 28 41 43 40 34 35
R11 | 898 14 11 13 18 24 8 | 28 38 39 41 27 34
R12 | 1219 21 11 9 16 23 8 | 53 36 44 51 48 45
R13 | 664 37 34 20 42 23 19 | 58 48 55 52 42 53
R14 | 1389 17 12 11 14 20 8 | 49 51 53 49 49 50
R15 | 1043 11 13 9 14 17 7 | 57 56 51 54 45 53
R16 | 666 26 41 55 27 29 23 | 129 122 127 123 120 127
R17 | 696 11 16 11 13 34 7 | 69 72 74 65 65 69
R18 | 800 10 8 7 13 17 5 | 52 46 45 53 48 48
R19 | 1305 45 77 22 49 32 28 | 59 63 47 63 51 52
R20 | 1331 28 171 47 61 27 32 | 68 81 73 53 57 67
R21 | 577 9 29 8 26 12 11 | 53 45 47 62 42 50
XR22 | 2775 --- 305 8 15 31 11 | --- 89 28 45 41 74
R24 | 874 12 33 8 24 27 11 | 56 52 51 57 55 52
------+------------------------------------+--------------------------------
RMS | 956 20 46 22 27 30 |T 70 70 67 69 63 68
WRMS | 956 21 30 12 25 29 |NE 58 60 55 57 51 57
MEDI | 874 13 14 11 18 23 |MD 58 63 53 58 52 53
Table 3.2245.6 GPS week: 2245 Day: 6 MJD: 59965
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 2157 17 32 83 81 75 34 | 53 55 114 63 83 53
R02E | 1053 12 12 16 23 25 9 | 80 79 79 88 88 81
R03E | 867 13 16 14 19 26 9 | 48 52 53 59 41 50
R04E | 1039 13 19 16 18 15 9 | 96 97 92 95 97 94
R05E | 1034 10 16 7 24 17 8 | 43 45 44 58 51 45
R07E | 1288 8 12 17 18 14 8 | 61 64 64 55 55 60
R08E | 1723 9 23 10 19 13 8 | 182 181 184 192 182 184
R09 | 488 13 19 12 24 27 10 | 45 56 49 44 51 45
R11 | 839 9 11 18 19 18 8 | 40 43 40 43 39 39
R12 | 701 23 50 19 25 15 17 | 54 35 45 44 42 44
R13 | 1260 28 37 15 31 26 16 | 58 36 42 36 40 43
R14 | 1927 14 11 7 18 21 7 | 53 53 52 44 49 50
R15 | 1052 21 19 19 11 24 10 | 66 57 56 55 53 57
R16 | 1010 20 34 58 28 37 21 | 161 146 155 158 153 157
R17 | 706 11 28 18 16 18 10 | 54 48 60 61 53 54
R18 | 545 7 12 12 11 24 6 | 41 47 42 48 50 42
R19 | 2834 45 76 18 64 39 30 | 97 50 75 84 85 74
R20 | 2904 48 132 77 57 58 45 | 112 68 142 106 121 101
R21 | 595 9 25 20 18 17 10 | 55 41 65 60 52 55
XR22 | 2580 --- 326 14 13 17 14 | --- 103 29 34 27 59
R24 | 1145 20 32 20 22 33 13 | 70 48 71 76 69 65
------+------------------------------------+--------------------------------
RMS | 1433 21 41 32 33 31 |T 73 66 73 71 70 69
WRMS | 1433 20 27 22 24 24 |NE 69 59 65 63 63 63
MEDI | 1052 13 23 17 19 24 |MD 55 53 60 59 53 55
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