[IGSREPORT-28953] Wk 2228 IGLOS Final Orbits
acc
acc at igs.org
Mon Oct 10 04:55:21 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2228 (Sep 18, 2022 - Sep 24, 2022)
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 2.2228.
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:
igl2228[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2228 in the SP3 format.
igl22287.sum Combination Report for GPS Week 2228.
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.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. 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).
3. 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
4. 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 | -6.8 ns
1 | -5.1 ns
2 | -6.6 ns
3 | 0.1 ns
4 | 1.4 ns
5 | 0.0 ns
6 | -0.2 ns
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 1.2228, 1a.2228).
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 2.2228.0-6)
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 3.2228.0-6).
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 2228 summary. (Sep 18, 2022 - Sep 24, 2022)
Table 1.2228.a GPS week : 2228 MJD: 59840.0-59846.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 1 -21 -23 55 .12 20 14 | 30864 129 3059 8171
| 1 1 1 15 9 28 .04 | 5485 1351
emx n/a| -1 0 3 -12 -51 -4 -.12 34 25 | 2332 -29 3059 8036
| 1 1 2 17 17 43 .06 | 8053 1015
esx n/a| 0 2 1 1 16 22 -.11 25 20 | 9555 194 3060 11159
| 1 1 1 13 15 30 .03 | 7532 1144
gfz n/a| 0 0 -2 7 -10 47 .10 29 16 | 0 3 3117 8022
| 0 1 2 24 14 29 .03 | 0 1243
grg n/a| 1 -1 1 24 95 -236 .20 31 22 | -2708 49 3060 7614
| 1 1 3 18 24 43 .04 | 3787 1230
iac n/a| 0 0 -7 -8 -24 45 -.25 28 24 | 794 -432 3110 9892
| 3 2 2 30 29 82 .07 | 3963 714
Table 1.2228.b GPS week : 2228 MJD: 59840.0-59846.0
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 15 18 18 16 16 14 |
R02 | 8 7 9 8 7 7 7 |
R03 | 7 7 6 6 7 7 6 |
R04 | 8 6 9 9 8 7 8 |
R05 | 10 8 7 9 11 9 7 |
R07 | 7 6 8 7 7 7 6 |
R08 | 7 7 8 10 8 8 7 |
R09 | 11 9 9 8 9 9 10 |
R11 | 8 8 12 12 14 9 8 |
R12 | 9 7 6 6 8 8 7 |
R13 | 14 13 13 15 14 14 15 |
R14 | 8 7 8 7 6 8 7 |
R15 | 7 7 7 6 7 7 9 |
R17 | 7 7 7 7 7 8 7 |
R18 | 9 7 7 7 7 11 7 |
R19 | 20 23 22 23 27 22 26 |
R20 | 30 28 26 27 24 36 30 |
R21 | 8 8 7 8 9 8 8 |
R24 | 8 10 10 9 11 8 9 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2228.c GPS week : 2228 MJD: 59840.0-59846.0
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 2228 0 | 67 2 89 -584 1143 6069 84.1 1396 1396 | -6822 0
brd 2228 1 | 17 26 58 -421 -31 6519 82.0 1170 1170 | -5140 0
brd 2228 2 | 54 -19 -26 868 -1168 5988 82.4 1127 1127 | -6638 0
brd 2228 3 | 3 -22 127 763 -1337 4886 81.0 1212 1212 | 103 0
brd 2228 4 | 20 -27 175 964 -485 969 81.1 1225 1225 | 1392 0
brd 2228 5 | 22 52 146 649 319 -1026 80.6 1215 1215 | 18 0
brd 2228 6 | -43 28 110 285 256 2219 81.2 1288 1288 | -172 0
-------------+------------------------------------------------------------+----------------
brd 2228 mean| 20 5 97 360 -186 3660 81.8 1233 1233 | -2465 0
brd 2228 sdev| 36 30 66 629 877 2948 1.2 87 87 | 3569 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 2.2228.0 GPS week: 2228 Day: 0 MJD: 59840
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -3 -1 -16 -23 89 .18 21 14 | 24183 309 2792 8432
emx n/a| 0 1 4 15 -60 29 -.06 32 27 | -15252 -620 2826 8326
esx n/a| -2 3 1 4 45 66 -.15 27 26 | -3147 -693 2829 11771
gfz n/a| 0 4 1 -6 -12 70 .14 33 18 | 0 -870 2881 8159
grg n/a| 3 0 5 -2 72 -273 .17 26 21 | -6630 -743 2800 7683
iac n/a| -2 -1 -8 28 -43 -48 -.32 27 23 | -3922 251 2890 10206
Table 2.2228.1 GPS week: 2228 Day: 1 MJD: 59841
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 0 -4 -34 35 .08 14 11 | 25031 2114 3954 8722
emx n/a| 0 -1 4 -11 -28 -74 -.04 33 26 | 788 1352 3957 8686
esx n/a| 0 4 0 -14 18 0 -.10 30 23 | 2685 1285 3944 10184
gfz n/a| 0 0 -4 -14 -27 70 .09 36 17 | 0 1917 4042 8831
grg n/a| 3 -3 1 48 56 -258 .17 25 19 | -6369 2046 3968 8094
iac n/a| 0 -2 -7 -5 37 169 -.30 25 20 | -3540 801 3940 9228
Table 2.2228.2 GPS week: 2228 Day: 2 MJD: 59842
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 -15 -20 73 .06 18 13 | 26121 514 3305 8389
emx n/a| 0 1 5 -18 -32 3 -.19 30 24 | 7468 -586 3313 8079
esx n/a| 0 2 3 -9 24 25 -.09 26 18 | 16961 909 3304 11732
gfz n/a| 0 0 -4 12 -9 32 .11 30 15 | 0 378 3336 8242
grg n/a| 1 -2 0 38 94 -260 .20 30 24 | -7211 731 3292 7713
iac n/a| 2 0 -10 7 -37 0 -.13 27 25 | -2766 -502 3320 10273
Table 2.2228.3 GPS week: 2228 Day: 3 MJD: 59843
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 2 -47 -10 84 .12 21 17 | 33469 -210 2891 9028
emx n/a| -1 2 3 -1 -54 49 -.17 39 25 | 4614 -517 2905 8903
esx n/a| -1 0 1 4 16 35 -.10 24 19 | 15591 955 2894 12359
gfz n/a| 1 -1 -2 54 -22 64 .07 25 18 | 0 -624 2930 8791
grg n/a| 0 0 0 36 103 -265 .15 30 25 | -113 -11 2892 8560
iac n/a| 3 0 -5 -39 -50 -41 -.26 28 27 | 3906 -843 2933 10873
Table 2.2228.4 GPS week: 2228 Day: 4 MJD: 59844
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 -2 3 -37 -33 40 .14 24 18 | 34967 999 2667 7463
emx n/a| -1 -1 3 -41 -52 -35 -.17 28 27 | 6084 1397 2659 7387
esx n/a| 0 1 3 28 1 0 -.06 19 14 | 9886 1017 2667 10439
gfz n/a| 0 0 1 -14 6 13 .14 24 15 | 0 1392 2711 7159
grg n/a| 0 -2 -2 30 113 -208 .28 32 22 | 833 711 2656 7185
iac n/a| 1 3 -11 -35 -17 126 -.27 22 22 | 4671 -881 2754 9712
Table 2.2228.5 GPS week: 2228 Day: 5 MJD: 59845
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 2 -14 -31 12 .13 21 16 | 36307 -629 3030 7546
emx n/a| -3 0 3 -19 -48 22 -.10 37 24 | 6630 -44 2966 7436
esx n/a| 2 3 0 1 9 51 -.08 23 17 | 9020 -353 3001 10668
gfz n/a| 0 -1 -3 20 12 76 .08 27 16 | 0 -959 3088 7395
grg n/a| 2 -2 2 16 95 -239 .18 35 21 | 89 -704 3049 7148
iac n/a| -5 1 -7 -42 -39 67 -.28 37 27 | 3743 -601 3112 9147
Table 2.2228.6 GPS week: 2228 Day: 6 MJD: 59846
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 1 -15 -13 52 .11 20 12 | 35974 -2193 2780 7618
emx n/a| 0 1 -2 -12 -80 -23 -.08 36 25 | 5998 -1188 2788 7440
esx n/a| 0 3 0 -7 1 -17 -.15 25 21 | 15895 -1758 2787 10965
gfz n/a| 0 0 -2 2 -21 7 .10 26 14 | 0 -1209 2832 7578
grg n/a| 3 -1 6 6 131 -151 .23 38 22 | 442 -1682 2768 6917
iac n/a| -1 -1 -3 26 -17 43 -.20 27 22 | 3469 -1250 2824 9805
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 3.2228.0 GPS week: 2228 Day: 0 MJD: 59840
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 594 32 40 57 39 17 16 16 | 119 79 51 111 101 94 91
R02 | 776 7 29 11 15 17 24 7 | 68 44 62 61 76 82 65
R03 | 560 9 21 13 18 18 17 7 | 70 53 65 62 81 72 67
XR04 | 846 8 22 12 --- 14 22 7 | 84 72 82 --- 92 91 84
R05 | 1082 16 28 23 25 15 22 9 | 79 60 73 69 78 76 72
R07 | 686 8 25 16 15 10 19 7 | 70 52 59 70 70 79 65
R08 | 1935 7 22 11 13 20 21 7 | 68 53 73 76 73 85 71
R09 | 1788 15 10 16 20 40 26 10 | 72 61 72 71 60 72 66
R11 | 2368 16 17 14 17 18 18 7 | 40 45 44 38 39 39 38
R12 | 999 15 34 13 18 11 26 8 | 78 67 76 84 82 88 78
R13 | 883 22 39 34 29 33 35 14 | 95 65 65 92 76 99 80
R14 | 715 11 24 13 20 16 23 7 | 50 40 58 63 50 64 53
R15 | 730 6 18 9 15 22 17 6 | 74 68 69 79 91 76 75
R17E | 1503 9 26 10 19 16 14 7 | 65 65 65 63 67 66 64
R18E | 895 15 24 15 18 24 25 9 | 44 36 36 40 43 47 39
R19E | 1043 45 44 36 64 27 47 19 | 57 59 81 120 78 62 66
R20E | 782 49 72 70 95 70 54 30 | 98 107 106 120 111 89 95
R21E | 802 10 24 15 19 10 23 7 | 46 51 52 44 46 52 46
R24E | 3370 10 30 14 24 14 15 7 | 57 51 55 49 59 53 53
XR25 |10504 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1395 21 32 27 33 26 27 |T 70 59 65 72 72 72 66
WRMS | 1395 14 27 26 18 21 23 |NE 74 58 65 73 74 78 69
MEDI | 883 11 25 14 19 17 22 |MD 70 59 65 69 76 76 66
Table 3.2228.1 GPS week: 2228 Day: 1 MJD: 59841
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 511 30 38 57 18 22 16 14 | 82 38 33 64 65 67 62
R02 | 1231 6 34 8 16 15 14 7 | 50 30 51 53 54 52 48
R03 | 1011 7 23 13 15 23 14 7 | 51 36 46 41 66 52 49
XR04 | 564 8 13 15 --- 11 14 6 | 55 47 49 --- 58 66 54
R05 | 801 7 23 17 24 20 18 7 | 51 39 48 38 65 60 49
R07 | 525 7 25 17 10 10 12 6 | 44 27 38 42 41 47 40
R08 | 1077 9 25 13 15 15 17 6 | 42 30 48 47 41 53 42
R09 | 1413 15 12 20 19 34 19 9 | 64 64 64 62 45 50 56
R11 | 1631 13 11 17 26 21 20 8 | 21 24 33 25 37 31 24
R12 | 805 8 25 13 17 11 24 7 | 59 51 58 67 57 73 59
R13 | 783 19 26 52 27 22 25 13 | 71 53 58 70 71 75 66
R14 | 1243 13 16 10 9 12 25 6 | 37 40 47 44 51 61 44
R15 | 758 9 17 14 15 20 18 6 | 56 53 53 63 71 74 60
R17E | 1234 7 25 12 15 14 18 6 | 38 40 38 33 42 43 37
R18E | 729 9 25 17 14 19 12 7 | 42 44 53 58 53 52 48
R19E | 1150 24 63 40 92 48 41 22 | 64 63 74 105 89 56 66
R20E | 988 27 75 72 92 62 64 28 | 68 76 86 87 77 80 62
R21E | 869 8 26 13 30 13 20 8 | 41 40 36 38 44 35 37
R24E | 2565 10 39 16 35 14 13 9 | 38 47 35 35 44 41 37
XR25 |12726 --- --- --- --- --- 11 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1169 14 33 30 36 25 25 |T 51 44 49 54 56 56 49
WRMS | 1169 11 26 23 17 19 20 |NE 52 40 48 51 55 58 50
MEDI | 988 9 25 16 17 19 18 |MD 51 40 48 47 54 53 49
Table 3.2228.2 GPS week: 2228 Day: 2 MJD: 59842
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 467 28 42 66 29 30 33 18 | 90 60 46 94 85 95 75
R02 | 1200 8 28 14 11 17 31 8 | 51 38 61 56 53 76 54
R03 | 594 10 16 12 7 12 22 6 | 59 46 59 62 59 68 58
XR04 | 555 13 14 8 --- 24 30 9 | 64 55 59 --- 54 64 58
R05 | 1156 13 19 18 14 19 15 7 | 55 47 60 61 70 56 56
R07 | 561 10 17 15 22 17 20 7 | 54 39 45 41 59 63 49
R08 | 477 10 29 9 16 16 20 7 | 49 33 49 58 64 64 51
R09 | 1078 14 13 13 25 35 15 9 | 65 61 71 82 60 71 66
R11 | 1488 21 21 21 18 45 32 12 | 43 45 30 46 24 43 31
R12 | 1577 8 12 13 7 16 18 5 | 53 56 59 52 51 53 53
R13 | 1023 24 21 40 18 37 26 12 | 82 58 46 72 65 78 67
R14 | 1219 13 19 25 14 16 24 8 | 42 40 68 57 42 62 50
R15 | 677 10 19 8 12 25 17 6 | 56 52 63 65 76 65 61
R17E | 1110 7 24 12 20 12 15 7 | 38 39 39 34 41 38 36
R18E | 733 13 14 18 16 16 16 7 | 46 51 58 61 61 51 52
R19E | 1069 31 54 33 76 51 48 22 | 48 50 62 98 62 57 53
R20E | 916 43 66 43 69 67 59 25 | 41 59 70 72 54 75 51
R21E | 957 9 20 10 23 12 18 7 | 38 38 35 36 43 39 36
R24E | 2331 13 35 11 31 21 18 10 | 40 45 34 38 44 36 35
XR25 |13699 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1126 18 30 26 30 30 27 |T 53 48 53 60 56 60 52
WRMS | 1126 13 24 18 15 24 25 |NE 58 48 55 62 58 66 56
MEDI | 1023 13 20 14 18 19 20 |MD 51 47 59 58 59 63 53
Table 3.2228.3 GPS week: 2228 Day: 3 MJD: 59843
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 733 43 40 56 21 20 41 18 | 107 74 67 79 95 96 82
R02 | 887 12 26 13 8 14 33 8 | 60 51 59 58 68 77 60
R03 | 820 10 21 8 8 17 13 5 | 64 57 63 60 71 62 62
XR04 | 565 11 20 11 --- 19 27 8 | 68 57 67 --- 62 52 62
R05 | 1254 21 21 20 17 13 29 9 | 67 55 70 58 63 48 59
R07 | 708 8 20 16 12 20 22 7 | 71 60 70 73 81 75 71
R08 | 622 19 34 8 28 8 29 10 | 67 57 77 90 80 88 76
R09 | 1259 15 15 13 11 30 18 7 | 64 61 56 64 39 67 57
R11 | 716 25 24 15 19 47 21 11 | 30 36 37 36 59 37 27
R12 | 1874 11 14 18 9 14 15 6 | 52 50 53 57 61 53 52
R13 | 1147 24 38 39 24 42 34 15 | 82 74 53 60 84 71 67
R14 | 751 11 14 14 16 18 23 7 | 57 48 59 49 49 61 52
R15 | 931 8 17 9 11 20 19 6 | 71 62 70 71 78 64 69
R17E | 1095 11 20 14 16 17 18 7 | 58 62 56 53 65 56 56
R18E | 996 11 22 9 13 29 13 7 | 33 37 40 42 48 36 36
R19E | 1612 32 76 30 59 60 48 22 | 71 61 65 85 77 52 64
R20E | 2037 42 109 46 54 64 51 26 | 56 75 70 63 62 60 51
R21E | 1114 9 22 13 27 15 17 8 | 65 62 62 55 65 58 60
R24E | 1851 12 23 13 27 16 25 8 | 50 46 42 46 51 47 44
XR25 |15492 --- --- --- --- --- 7 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1211 21 39 24 25 30 28 |T 62 57 59 61 66 61 58
WRMS | 1211 17 25 19 18 25 27 |NE 66 57 61 62 68 65 61
MEDI | 996 12 22 14 16 19 22 |MD 64 57 62 58 65 60 60
Table 3.2228.4 GPS week: 2228 Day: 4 MJD: 59844
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1064 45 36 46 21 35 21 16 | 92 62 60 63 88 64 66
R02 | 537 10 27 13 6 11 15 6 | 50 37 50 42 47 46 45
R03 | 506 8 17 10 11 10 25 6 | 56 43 52 49 60 69 54
XR04 | 464 12 17 12 --- 24 17 8 | 63 59 65 --- 61 48 58
R05 | 1178 20 22 16 29 21 31 10 | 56 48 69 82 58 47 59
R07 | 756 12 15 12 15 21 10 6 | 60 49 55 52 72 61 57
R08 | 1341 15 24 12 28 11 17 8 | 46 48 51 76 58 69 57
R09 | 1955 20 21 9 14 35 19 9 | 63 60 60 62 51 71 58
R11 | 941 26 18 27 21 57 29 14 | 25 30 52 29 85 41 39
R12 | 2194 12 21 15 13 11 26 7 | 53 56 62 63 68 63 59
R13 | 1066 29 49 20 21 45 23 13 | 56 39 54 45 49 43 43
R14 | 781 13 16 11 11 11 12 5 | 42 30 37 38 39 37 36
R15 | 954 12 19 18 8 19 19 7 | 64 53 52 63 73 63 59
R17E | 751 8 24 10 15 14 23 7 | 45 55 45 40 47 41 43
R18E | 706 9 29 8 21 13 14 7 | 29 33 30 34 31 27 27
XR19E | 2995 28 --- 38 65 70 66 27 | 36 --- 67 83 69 59 48
R20E | 1208 60 52 28 59 79 36 23 | 68 95 81 66 82 85 67
R21E | 982 11 29 13 18 32 16 8 | 54 60 53 42 61 45 50
R24E | 2096 21 26 12 37 9 26 10 | 39 43 33 35 39 51 35
XR25 |15128 --- --- --- --- --- 11 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1224 24 28 19 24 32 22 |T 52 50 54 53 59 54 50
WRMS | 1224 18 27 14 15 22 22 |NE 55 47 55 55 62 55 53
MEDI | 982 13 22 13 18 21 19 |MD 54 48 53 49 60 51 54
Table 3.2228.5 GPS week: 2228 Day: 5 MJD: 59845
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1043 25 38 57 15 31 18 15 | 75 67 52 65 85 65 65
R02 | 523 8 23 15 12 11 18 6 | 49 37 40 55 52 55 47
R03 | 606 8 21 14 11 12 22 6 | 59 44 51 57 60 67 55
XR04 | 594 8 18 13 --- 15 20 7 | 66 57 60 --- 65 75 64
R05 | 764 16 25 23 18 15 19 8 | 66 56 70 61 56 56 60
R07 | 946 16 20 13 14 9 16 6 | 62 56 44 48 54 53 52
R08 | 1005 6 19 17 26 16 22 8 | 53 50 45 60 55 62 52
R09 | 1765 18 19 11 14 35 12 8 | 46 47 45 43 37 39 39
R11 | 941 19 20 16 15 18 25 8 | 28 35 38 35 37 36 29
R12 | 1604 8 22 15 8 20 34 8 | 63 61 53 59 56 71 58
R13 | 974 34 27 20 28 32 41 13 | 53 45 44 34 43 39 39
R14 | 873 13 11 15 18 21 27 7 | 37 35 43 43 48 37 37
R15 | 663 11 16 19 10 11 19 6 | 58 50 44 51 59 63 53
R17E | 1162 13 20 12 17 16 23 7 | 60 63 61 61 69 59 61
R18E | 1093 11 36 12 41 14 27 11 | 33 33 40 57 37 32 34
R19E | 2063 32 47 40 57 75 32 21 | 46 62 69 87 96 67 59
R20E | 1557 52 112 33 62 100 121 35 | 87 71 89 75 107 146 79
R21E | 674 13 30 12 19 18 15 8 | 44 43 42 37 43 44 40
R24E | 1983 12 27 12 25 17 15 8 | 35 35 34 35 40 33 33
XR25 |13762 --- --- --- --- --- 8 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1215 21 37 23 27 35 37 |T 53 49 50 53 57 57 50
WRMS | 1215 16 24 17 16 21 27 |NE 55 49 48 50 54 55 50
MEDI | 974 13 22 15 17 17 20 |MD 53 50 45 55 55 56 52
Table 3.2228.6 GPS week: 2228 Day: 6 MJD: 59846
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 986 16 37 44 24 37 25 13 | 111 89 65 94 114 105 94
R02 | 625 8 23 8 10 13 27 6 | 66 51 65 69 68 86 67
R03 | 915 6 16 16 6 15 21 6 | 75 57 68 70 76 82 71
XR04 | 649 14 16 18 --- 22 15 8 | 80 63 73 --- 74 77 74
R05 | 1262 15 25 16 12 8 14 7 | 78 60 74 76 72 67 72
R07 | 786 10 14 11 9 9 21 5 | 82 71 78 75 81 75 77
R08 | 1645 10 20 13 16 18 19 7 | 76 66 81 84 88 88 79
R09 | 1089 18 22 14 13 41 22 9 | 64 64 64 63 59 66 60
R11 | 1614 11 14 18 15 27 19 7 | 46 51 58 54 36 38 46
R12 | 627 9 22 18 14 17 14 6 | 75 74 72 77 74 81 74
R13 | 1068 33 37 40 18 47 30 15 | 83 55 62 65 79 66 66
R14 | 619 9 23 13 16 19 19 7 | 58 49 62 58 60 49 55
R15 | 780 12 16 21 13 28 25 8 | 79 64 66 75 93 67 72
R17E | 1513 8 21 12 15 19 21 7 | 65 69 66 64 66 72 66
R18E | 1081 11 19 12 15 20 20 7 | 32 37 34 35 31 35 30
R19E | 1792 24 64 50 60 115 31 25 | 64 36 48 84 134 64 59
R20E | 2216 62 99 48 69 55 71 30 | 147 100 107 113 102 160 114
R21E | 723 8 36 13 22 17 11 8 | 59 59 67 62 66 63 61
R24E | 2076 12 32 11 15 25 22 8 | 45 45 38 40 42 49 40
XR25 |17894 --- --- --- --- --- 4 0 | --- --- --- --- --- --- 0
------+-----------------------------------------+-------------------------------------
RMS | 1288 20 36 25 26 38 27 |T 72 61 65 69 74 73 67
WRMS | 1288 12 25 21 14 22 22 |NE 74 62 68 71 74 72 69
MEDI | 1068 11 22 16 15 20 21 |MD 75 60 66 69 74 67 67
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