[IGSREPORT-28856] Wk 2221 IGLOS Final Orbits
acc
acc at igs.org
Sun Aug 21 04:23:31 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2221 (Jul 31, 2022 - Aug 06, 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 2.2221.
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:
igl2221[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2221 in the SP3 format.
igl22217.sum Combination Report for GPS Week 2221.
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 | -1.5 ns
1 | -7.0 ns
2 | 1.2 ns
3 | 0.4 ns
4 | -0.1 ns
5 | -1.2 ns
6 | -8.0 ns
5. 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
----+--------+---------------
3 | EMX | R19
4 | EMX | R19
5 | EMX | R19
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 1.2221, 1a.2221).
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 2.2221.0-6)
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 3.2221.0-6).
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 2221 summary. (Jul 31, 2022 - Aug 06, 2022)
Table 1.2221.a GPS week : 2221 MJD: 59791.0-59797.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 0 -19 -39 -1 .08 23 18 | 33047 -1549 2937 8509
| 0 1 1 6 14 22 .02 | 4297 2175
emx n/a| -2 0 3 12 36 -20 -.20 44 27 | -10808 -1221 2954 8356
| 2 1 2 24 15 24 .05 | 5827 1115
esx n/a| 0 0 1 8 22 27 -.08 27 23 | -16667 -337 2930 11534
| 1 1 2 15 17 23 .05 | 8800 2173
gfz n/a| 1 0 1 -9 2 19 -.01 24 15 | 0 -1158 2952 8288
| 0 1 0 22 18 16 .07 | 0 1898
grg n/a| 2 0 -2 17 26 -23 .33 23 19 | -1851 -1314 2940 8035
| 0 1 3 9 13 25 .06 | 3485 2037
iac n/a| -1 -2 0 -9 -48 2 -.22 23 22 | 230 -463 2923 9141
| 2 1 2 13 40 33 .10 | 3959 838
Table 1.2221.b GPS week : 2221 MJD: 59791.0-59797.0
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 16 18 19 17 16 17 |
R02 | 8 7 6 6 6 7 6 |
R03 | 6 7 8 8 8 7 7 |
R04 | 9 9 8 8 7 8 7 |
R05 | 9 6 7 9 7 7 7 |
R07 | 8 8 7 6 7 10 7 |
R08 | 7 7 8 7 6 6 7 |
R09 | 5 7 8 6 8 8 7 |
R11 | 6 6 7 7 8 8 8 |
R12 | 8 8 7 7 9 7 9 |
R13 | 10 13 16 13 11 13 16 |
R14 | 7 8 5 6 5 8 7 |
R15 | 8 9 6 7 6 7 8 |
R17 | 8 8 9 8 7 9 8 |
R18 | 8 9 10 10 10 7 8 |
R19 | 21 28 28 26 26 25 27 |
R20 | 23 22 23 23 23 23 21 |
R21 | 8 9 8 8 7 8 8 |
R24 | 12 11 10 10 8 9 8 |
Table 1.2221.c GPS week : 2221 MJD: 59791.0-59797.0
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 2221 0 | 46 -21 144 1022 -495 -47 82.3 1538 1538 | -1453 0
brd 2221 1 | -5 -49 153 80 571 -3391 80.5 1729 1729 | -7048 0
brd 2221 2 | 79 9 127 -169 2372 6140 84.0 1537 1537 | 1236 0
brd 2221 3 | -66 -44 63 -845 921 2816 82.8 1468 1468 | 438 0
brd 2221 4 | 52 -39 89 1422 1696 -2588 81.6 1451 1451 | -103 0
brd 2221 5 | 26 -5 97 1419 -954 3476 79.9 1452 1452 | -1191 0
brd 2221 6 | -57 8 161 -127 -2434 1022 81.0 1714 1714 | -7986 0
-------------+------------------------------------------------------------+----------------
brd 2221 mean| 10 -20 119 400 239 1061 81.7 1555 1555 | -2301 0
brd 2221 sdev| 56 24 36 887 1651 3392 1.4 119 119 | 3688 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 2.2221.0 GPS week: 2221 Day: 0 MJD: 59791
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 0 -7 -29 9 .08 20 15 | 35421 -3741 3539 7650
emx n/a| 0 1 4 15 51 -12 -.25 36 23 | -12863 -1998 3535 7396
esx n/a| 0 2 -1 -2 20 -20 -.13 26 22 | -7288 -1767 3525 10858
gfz n/a| 1 0 0 -13 -5 36 -.14 20 16 | 0 -2705 3582 7253
grg n/a| 1 0 1 9 30 -32 .24 24 19 | 61 -3244 3531 6955
iac n/a| -4 -1 -2 8 -71 -14 .00 29 25 | 569 -694 3517 8285
Table 2.2221.1 GPS week: 2221 Day: 1 MJD: 59792
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 2 -29 -40 -22 .09 24 20 | 26862 247 3399 8009
emx n/a| -1 2 5 41 55 -51 -.25 44 29 | -8577 291 3410 7717
esx n/a| -2 2 5 17 42 54 -.04 24 22 | -9405 1500 3395 11323
gfz n/a| 0 0 2 -38 -12 -10 -.04 26 14 | 0 424 3405 7905
grg n/a| 2 0 -5 12 8 -17 .32 22 18 | -7461 276 3430 7532
iac n/a| -1 -3 -1 -5 -89 0 -.22 25 24 | -5040 457 3395 8646
Table 2.2221.2 GPS week: 2221 Day: 2 MJD: 59793
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 0 -20 -30 -17 .08 28 20 | 35926 1029 2505 9318
emx n/a| -2 -1 6 43 16 -38 -.17 39 23 | -10407 348 2526 9083
esx n/a| -1 1 1 -2 -7 28 -.04 25 22 | -13729 2491 2507 12188
gfz n/a| 1 1 1 -33 -1 27 .05 25 14 | 0 1301 2520 9065
grg n/a| 1 -2 0 23 19 -21 .28 26 22 | 356 1297 2517 8811
iac n/a| 3 0 -5 -12 2 25 -.25 24 23 | 4093 -297 2503 9947
Table 2.2221.3 GPS week: 2221 Day: 3 MJD: 59794
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 0 -17 -49 -13 .10 23 18 | 36324 -628 2865 8506
emx n/a| -1 0 0 19 15 -43 -.17 46 22 | -13625 -1692 2866 8382
esx n/a| 0 0 0 -1 11 28 -.10 29 32 | -29537 1109 2839 11447
gfz n/a| 2 1 2 -5 -17 25 .07 28 15 | 0 205 2886 8267
grg n/a| 3 -1 -2 10 14 -34 .36 21 17 | 424 -630 2843 8052
iac n/a| -3 -2 0 -31 11 50 -.31 23 22 | 3048 165 2857 9057
Table 2.2221.4 GPS week: 2221 Day: 4 MJD: 59795
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 0 -15 -66 43 .07 22 16 | 34152 -68 2910 8859
emx n/a| -5 1 1 -20 39 14 -.23 49 29 | -10792 -1147 2940 8880
esx n/a| 0 -1 5 -5 40 26 -.06 27 22 | -21750 18 2903 12234
gfz n/a| 0 0 1 -12 33 16 .03 25 14 | 0 -870 2882 8847
grg n/a| 2 -2 -7 34 30 -18 .34 22 18 | -367 56 2899 8474
iac n/a| 1 0 0 0 -68 -57 -.23 19 19 | 1875 -494 2893 9493
Table 2.2221.5 GPS week: 2221 Day: 5 MJD: 59796
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 -1 -19 -37 -5 .08 24 20 | 35834 -3546 2671 8441
emx n/a| -1 0 1 2 40 -16 -.16 49 29 | -19290 -1991 2703 8337
esx n/a| 0 -2 0 31 24 47 -.02 29 20 | -9652 -2776 2653 11418
gfz n/a| 0 1 1 24 18 32 -.02 21 17 | 0 -2966 2692 8225
grg n/a| 3 -1 -1 22 37 -62 .38 23 20 | 400 -3228 2663 8129
iac n/a| -1 -5 1 -21 -80 7 -.30 20 19 | 2706 -2148 2639 9124
Table 2.2221.6 GPS week: 2221 Day: 6 MJD: 59797
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 -23 -24 -7 .05 21 16 | 26810 -4137 2676 8780
emx n/a| -6 2 2 -14 39 0 -.15 46 33 | -106 -2361 2703 8699
esx n/a| 2 1 1 24 27 25 -.15 27 21 | -25310 -2937 2692 11275
gfz n/a| 2 0 1 10 1 11 -.05 21 16 | 0 -3500 2703 8456
grg n/a| 2 1 0 6 45 22 .42 26 19 | -6375 -3729 2699 8297
iac n/a| 0 -1 2 -4 -45 7 -.20 22 19 | -5640 -230 2663 9439
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 3.2221.0 GPS week: 2221 Day: 0 MJD: 59791
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 642 46 29 51 43 34 67 20 | 58 74 97 93 71 65 68
R02E | 2061 8 19 21 13 16 23 7 | 37 48 45 45 45 46 41
R03E | 985 8 22 11 10 13 18 6 | 81 78 85 81 84 89 82
XR04E | 1341 12 26 17 --- 10 30 9 | 73 63 70 --- 77 78 71
R05E | 766 13 21 21 22 13 31 9 | 52 51 58 58 55 60 53
R07E | 1046 9 18 13 20 16 26 7 | 47 46 50 48 56 53 48
R08E | 1594 10 23 19 15 13 19 7 | 52 54 55 56 51 48 51
R09 | 2323 10 12 10 12 12 8 5 | 33 34 36 37 32 40 33
R11 | 2176 11 15 13 9 11 24 6 | 41 43 34 40 33 33 35
R12 | 903 15 15 14 12 11 30 7 | 37 38 39 44 36 36 37
R13 | 865 21 16 32 19 25 20 10 | 57 51 50 57 51 56 51
R14 | 1076 11 9 16 14 17 18 6 | 41 42 45 43 46 42 41
R15 | 1241 21 22 22 9 13 23 8 | 48 51 46 52 38 47 45
R17 | 765 15 25 11 13 20 19 7 | 58 42 50 52 49 44 49
R18 | 1171 4 14 33 17 19 13 8 | 35 38 57 37 41 39 39
R19 | 2362 30 91 49 29 25 53 20 | 93 60 38 93 78 92 69
R20 | 2938 34 86 44 34 67 26 22 | 83 39 55 73 58 59 56
R21 | 874 16 25 16 16 19 21 8 | 66 48 59 62 58 59 58
R24 | 1175 24 50 12 19 15 31 11 | 71 45 61 67 67 54 61
------+-----------------------------------------+-------------------------------------
RMS | 1537 20 36 26 20 24 29 |T 55 49 54 57 54 54 52
WRMS | 1537 15 23 22 16 19 25 |NE 55 44 47 54 48 50 47
MEDI | 1171 13 22 17 15 16 23 |MD 52 48 50 52 51 53 51
Table 3.2221.1 GPS week: 2221 Day: 1 MJD: 59792
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 988 25 54 26 49 31 35 16 | 35 45 45 53 49 51 38
R02E | 3041 9 23 12 15 16 16 6 | 31 32 36 32 37 40 33
R03E | 1392 12 28 12 18 13 15 7 | 46 53 50 49 51 50 48
XR04E | 705 10 27 13 --- 15 24 8 | 43 39 43 --- 47 47 42
R05E | 891 9 24 13 12 10 18 6 | 35 33 35 39 38 39 35
R07E | 786 13 27 13 21 15 23 8 | 39 39 44 37 38 46 38
R08E | 2592 14 20 15 15 13 20 7 | 27 36 34 34 33 27 29
R09 | 2294 11 17 12 18 20 17 7 | 47 48 43 40 47 56 44
R11 | 2225 12 10 9 14 11 21 6 | 45 46 45 46 41 43 42
R12 | 601 15 18 11 23 8 23 7 | 39 38 45 49 43 40 40
R13 | 1456 23 26 29 36 37 19 13 | 49 43 46 61 39 44 44
R14 | 703 12 14 15 11 20 25 7 | 40 44 40 38 46 36 38
R15 | 2131 15 19 11 14 10 36 8 | 41 46 44 43 41 47 39
R17 | 797 20 27 12 12 10 29 8 | 49 43 49 49 51 43 46
R18 | 1000 12 20 29 15 11 23 8 | 41 42 50 40 45 40 41
R19 | 2973 49 114 64 69 50 39 28 | 63 50 56 98 59 71 57
R20 | 1907 61 100 40 25 34 24 21 | 66 55 51 55 44 44 45
R21 | 881 23 23 12 10 22 21 8 | 59 56 62 54 62 62 58
R24 | 930 23 51 16 14 16 29 11 | 53 46 51 48 59 42 48
------+-----------------------------------------+-------------------------------------
RMS | 1728 24 44 24 26 22 25 |T 44 43 45 48 45 45 42
WRMS | 1728 20 29 22 14 18 24 |NE 49 46 48 51 48 47 45
MEDI | 1000 14 24 13 15 15 23 |MD 43 44 45 46 45 44 42
Table 3.2221.2 GPS week: 2221 Day: 2 MJD: 59793
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1315 39 51 21 54 24 45 18 | 35 57 44 82 46 42 40
R02E | 1410 8 20 13 9 11 12 5 | 40 42 46 43 43 43 42
R03E | 1355 10 29 10 15 14 22 7 | 46 51 45 51 52 47 46
XR04E | 861 13 27 9 --- 15 15 8 | 43 43 43 --- 52 45 44
R05E | 1045 11 21 14 16 14 17 7 | 37 35 40 39 41 44 37
R07E | 713 13 29 10 13 10 17 7 | 39 42 45 40 43 45 40
R08E | 2544 11 24 12 16 21 23 8 | 34 31 33 36 39 37 32
R09 | 1428 14 21 20 15 19 17 8 | 16 24 31 30 24 31 21
R11 | 2391 15 15 10 13 16 20 6 | 29 39 32 35 20 25 26
R12 | 659 13 13 10 15 12 24 6 | 32 29 32 38 36 30 30
R13 | 1603 23 25 40 26 59 18 16 | 50 45 46 54 47 33 43
R14 | 559 11 19 8 8 10 14 5 | 36 35 38 40 35 38 35
R15 | 1127 15 15 13 10 15 14 6 | 37 40 33 36 30 41 34
R17 | 833 26 19 13 10 15 34 9 | 49 33 39 37 40 32 35
R18 | 889 9 15 37 16 14 20 9 | 31 24 41 24 36 29 28
R19 | 3029 64 122 64 40 52 26 28 | 91 46 35 72 79 71 58
R20 | 2003 65 49 43 58 43 39 22 | 73 57 34 63 45 40 41
R21 | 1042 22 27 15 9 23 13 8 | 47 32 49 43 39 34 39
R24 | 875 32 33 12 19 19 23 10 | 58 41 45 45 58 40 45
------+-----------------------------------------+-------------------------------------
RMS | 1537 28 39 25 25 26 24 |T 43 39 39 44 42 39 37
WRMS | 1537 20 23 22 14 22 23 |NE 45 37 37 43 40 37 36
MEDI | 1127 14 24 13 15 15 20 |MD 39 40 40 40 41 40 39
Table 3.2221.3 GPS week: 2221 Day: 3 MJD: 59794
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 859 27 58 29 71 28 35 19 | 42 60 44 79 45 40 42
R02E | 1518 9 17 14 14 11 16 6 | 32 35 41 36 40 38 35
R03E | 1207 13 23 14 16 10 28 8 | 63 63 69 67 66 55 63
XR04E | 1510 9 24 17 --- 11 15 7 | 46 42 49 --- 52 47 46
R05E | 1807 12 21 18 26 11 27 8 | 42 38 44 45 48 52 41
R07E | 1882 12 21 12 14 10 15 6 | 39 35 40 40 42 36 37
R08E | 2318 9 27 14 14 11 17 7 | 32 32 34 31 37 40 32
R09 | 835 11 11 11 14 14 14 5 | 13 25 25 29 27 18 20
R11 | 2096 12 18 15 10 11 21 6 | 23 33 40 29 25 28 27
R12 | 725 10 18 14 13 19 11 6 | 29 37 28 31 20 31 26
R13 | 1826 33 15 21 19 36 32 12 | 59 37 37 49 38 46 42
R14 | 627 10 14 15 12 12 17 6 | 39 36 33 43 39 36 36
R15 | 800 8 9 10 19 18 17 6 | 40 36 39 54 35 45 40
R17 | 895 18 23 10 15 16 23 8 | 51 34 47 51 48 34 43
R18 | 994 9 18 39 10 12 29 10 | 28 28 50 34 36 30 30
R19 | 1599 53 157 81 39 43 20 26 | 105 52 33 89 73 76 75
R20 | 2315 52 56 60 60 39 24 22 | 76 27 36 67 54 59 47
R21 | 791 13 34 11 14 14 13 7 | 43 28 34 45 44 43 37
R24 | 1325 20 30 14 15 22 27 9 | 54 39 43 34 46 62 43
------+-----------------------------------------+-------------------------------------
RMS | 1467 23 46 29 28 21 23 |T 45 37 40 47 42 42 40
WRMS | 1467 18 22 32 15 17 22 |NE 46 34 37 46 40 42 38
MEDI | 1325 12 21 14 14 14 20 |MD 42 36 40 43 42 40 40
Table 3.2221.4 GPS week: 2221 Day: 4 MJD: 59795
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1496 23 61 35 47 25 36 16 | 37 39 43 58 39 40 34
R02E | 1329 9 23 11 12 13 14 6 | 42 41 44 52 46 50 45
R03E | 1165 12 26 7 11 16 28 7 | 48 42 43 50 55 39 44
XR04E | 1902 9 29 13 --- 11 11 7 | 44 46 41 --- 47 42 43
R05E | 1977 12 27 13 15 12 11 6 | 43 40 44 47 51 45 43
R07E | 1181 20 21 12 15 11 19 7 | 44 25 33 37 36 32 32
R08E | 1383 10 18 14 10 14 11 5 | 34 29 34 38 45 41 36
R09 | 968 17 18 12 13 15 22 7 | 40 41 49 41 43 53 43
R11 | 1194 16 26 20 15 11 15 7 | 45 46 47 49 35 44 42
R12 | 726 17 23 14 19 24 22 9 | 37 37 46 41 35 38 36
R13 | 1196 12 27 23 19 41 18 11 | 44 70 51 50 45 48 48
R14 | 666 8 15 14 13 8 11 5 | 41 36 48 40 41 48 42
R15 | 1018 12 17 8 15 12 14 5 | 42 40 51 58 42 54 47
R17 | 748 15 25 12 14 15 16 7 | 50 45 43 43 65 52 48
R18 | 808 13 21 28 15 20 26 9 | 42 37 48 46 58 42 43
R19 | 1412 56 156 78 39 46 19 26 | 82 49 42 91 91 62 71
R20 | 3531 46 86 49 65 32 21 22 | 60 47 35 76 61 64 51
R21 | 881 11 32 15 11 12 11 6 | 53 44 53 54 56 56 52
R24 | 1749 22 28 15 13 16 12 8 | 53 41 48 42 53 47 46
------+-----------------------------------------+-------------------------------------
RMS | 1451 22 49 27 25 22 19 |T 46 41 44 50 49 47 44
WRMS | 1451 16 29 22 14 18 19 |NE 49 44 46 52 52 50 47
MEDI | 1194 13 26 14 15 15 16 |MD 44 41 44 47 46 47 43
Table 3.2221.5 GPS week: 2221 Day: 5 MJD: 59796
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 770 29 50 47 37 24 28 16 | 46 51 80 72 45 49 52
R02E | 3296 10 27 14 13 11 20 7 | 35 47 36 40 40 34 37
R03E | 1247 10 23 16 12 12 23 7 | 95 93 91 84 90 84 88
XR04E | 1895 10 23 14 --- 14 14 7 | 67 70 58 --- 70 61 64
R05E | 838 13 24 10 13 13 21 7 | 41 39 48 47 47 46 43
R07E | 1099 32 28 21 15 11 18 9 | 59 44 48 49 52 51 47
R08E | 1276 9 27 12 10 10 17 6 | 52 54 53 48 54 61 52
R09 | 823 20 12 14 19 23 12 8 | 21 24 24 31 17 24 19
R11 | 1151 11 13 26 12 15 19 7 | 20 23 19 19 27 34 19
R12 | 661 13 19 16 15 10 18 6 | 30 29 29 35 33 29 28
R13 | 899 21 50 24 15 34 25 12 | 35 56 31 30 32 44 31
R14 | 915 7 14 16 17 26 11 7 | 31 32 47 49 27 40 35
R15 | 1025 10 12 9 18 17 20 7 | 37 31 42 43 30 53 38
R17 | 692 27 18 13 17 20 16 8 | 45 38 41 39 46 32 38
R18 | 988 7 20 25 13 11 16 7 | 32 32 33 32 39 30 30
R19 | 1139 56 153 78 21 49 31 25 | 53 54 49 47 62 37 46
R20 | 3135 51 82 54 55 43 27 23 | 57 55 38 53 46 29 36
R21 | 644 19 29 15 11 9 19 7 | 35 22 32 28 39 39 31
R24 | 1800 16 43 9 21 12 14 9 | 52 50 57 55 55 49 51
------+-----------------------------------------+-------------------------------------
RMS | 1451 24 49 29 21 23 20 |T 44 44 45 44 44 43 41
WRMS | 1451 20 29 20 17 20 19 |NE 37 37 36 38 37 36 33
MEDI | 1025 13 24 16 15 14 19 |MD 41 44 42 43 45 40 38
Table 3.2221.6 GPS week: 2221 Day: 6 MJD: 59797
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 937 36 58 46 38 22 23 16 | 46 41 63 72 49 44 46
R02E | 4291 8 22 13 13 14 15 6 | 32 29 35 36 37 30 32
R03E | 2010 14 27 12 20 9 15 7 | 84 72 85 80 84 87 82
XR04E | 1590 9 26 11 --- 13 14 7 | 66 57 61 --- 69 59 62
R05E | 1369 12 24 18 16 13 14 7 | 54 52 55 60 59 51 54
R07E | 1624 12 31 15 12 10 12 6 | 50 40 59 56 59 52 52
R08E | 1831 13 28 13 12 10 16 6 | 48 44 54 53 57 59 52
R09 | 753 13 20 11 14 11 19 6 | 38 42 41 48 38 55 43
R11 | 1061 12 16 21 25 17 15 8 | 39 41 37 38 36 37 35
R12 | 989 10 22 27 16 11 24 8 | 49 51 48 49 46 48 46
R13 | 1937 18 68 27 24 52 25 15 | 61 58 51 54 52 62 54
R14 | 1016 9 12 11 18 10 21 6 | 54 55 58 65 54 58 57
R15 | 973 13 9 30 11 15 22 8 | 61 62 57 69 55 72 62
R17 | 861 19 26 14 21 11 20 8 | 70 55 63 66 64 54 62
R18 | 1170 10 14 28 14 23 16 8 | 50 48 61 56 60 45 51
R19 | 967 42 127 64 30 58 52 26 | 105 71 76 111 96 79 89
R20 | 2104 49 81 45 30 56 30 21 | 102 66 69 93 79 71 75
R21 | 1030 16 26 13 20 19 14 8 | 71 47 60 67 62 66 63
R24 | 2167 8 42 15 13 18 18 8 | 77 64 76 71 76 69 72
------+-----------------------------------------+-------------------------------------
RMS | 1713 21 46 27 21 26 22 |T 60 52 58 63 59 57 57
WRMS | 1713 16 33 21 16 19 19 |NE 64 55 58 65 59 59 59
MEDI | 1170 13 26 15 16 14 18 |MD 54 52 59 60 59 58 54
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