[IGSREPORT-28582] Wk 2201 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 4 01:57:25 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2201 (Mar 13, 2022 - Mar 19, 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 2.2201.
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:
igl2201[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2201 in the SP3 format.
igl22017.sum Combination Report for GPS Week 2201.
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 | -6.5 ns
2 | -6.5 ns
3 | -6.4 ns
4 | -6.9 ns
5 | -6.1 ns
6 | 0.8 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
----+--------+---------------
0 | COD | R11
0 | GFZ | R11
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 1.2201, 1a.2201).
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 2.2201.0-6)
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 3.2201.0-6).
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 2201 summary. (Mar 13, 2022 - Mar 19, 2022)
Table 1.2201.a GPS week : 2201 MJD: 59651.0-59657.0
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 2 16 -20 26 .13 23 16 | 28778 -571 3186 8973
| 1 0 1 18 15 31 .02 | 4218 1962
emx n/a| 0 1 -9 23 6 15 -.00 36 30 | -8414 76 3181 8842
| 1 1 4 24 28 32 .09 | 11109 1159
esx n/a| 0 1 0 -9 -24 -40 -.08 27 19 | -1974 -861 3188 12104
| 1 1 1 19 14 19 .05 | 9428 1486
gfz n/a| 0 0 6 -28 5 -17 -.08 31 16 | 0 -542 3172 8507
| 1 0 2 18 13 24 .05 | 0 1691
grg n/a| 0 -1 -7 -11 2 43 .28 25 19 | -4606 -310 3271 8580
| 1 1 3 13 17 46 .04 | 3206 1033
iac n/a| 0 0 2 7 38 -48 -.28 29 27 | -1774 -274 3200 10289
| 3 3 3 21 35 42 .04 | 3286 1429
Table 1.2201.b GPS week : 2201 MJD: 59651.0-59657.0
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 | 16 16 17 17 17 18 18 |
R02 | 7 8 7 7 8 8 7 |
R03 | 10 11 11 7 8 8 10 |
R04 | 10 12 10 8 9 9 11 |
R05 | 12 10 7 7 9 9 8 |
R07 | 9 10 8 7 7 7 7 |
R08 | 7 8 9 11 8 7 9 |
R09 | 9 8 8 6 7 7 9 |
R11 | 65 0 --- 0 0 0 --- |
R12 | 7 7 8 7 6 8 7 |
R13 | 12 14 14 16 14 13 16 |
R14 | 7 7 7 9 6 7 7 |
R15 | 6 7 7 6 6 8 7 |
R17 | 8 7 10 8 7 9 7 |
R18 | 7 8 7 7 8 9 8 |
R19 | 21 18 17 18 20 20 26 |
R20 | 22 26 28 22 21 25 27 |
R21 | 9 8 7 8 7 8 9 |
R22 | 23 25 22 22 20 25 24 |
R24 | 8 9 8 10 8 9 8 |
Table 1.2201.c GPS week : 2201 MJD: 59651.0-59657.0
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 2201 0 | -47 13 110 -937 648 -2923 81.9 1531 1531 | -1545 0
brd 2201 1 | 61 10 154 594 1289 -3488 83.1 1578 1578 | -6453 0
brd 2201 2 | 7 39 111 -65 1664 -2365 81.5 1519 1519 | -6476 0
brd 2201 3 | 29 64 52 -639 2268 -1030 79.4 1352 1352 | -6427 0
brd 2201 4 | 16 -6 88 -1359 854 -1292 80.4 1405 1405 | -6910 0
brd 2201 5 | -69 -31 22 226 1597 -7525 83.2 1393 1393 | -6083 0
brd 2201 6 | -15 -43 -156 1037 -270 -4338 83.5 1384 1384 | 813 0
-------------+------------------------------------------------------------+----------------
brd 2201 mean| -2 6 54 -163 1150 -3280 81.9 1451 1451 | -4725 0
brd 2201 sdev| 45 37 102 859 825 2204 1.5 88 88 | 3064 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 2.2201.0 GPS week: 2201 Day: 0 MJD: 59651
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 -5 -26 -7 .12 27 21 | 35855 -4446 3153 8304
emx n/a| 0 1 -16 25 53 10 .17 37 33 | -9560 -2232 3186 8363
esx n/a| 1 2 -2 -45 -16 -45 -.15 25 19 | 14765 -3163 3203 10988
gfz n/a| 1 0 7 0 -13 -40 -.10 27 16 | 0 -3882 3141 7937
grg n/a| 0 -5 -2 6 2 69 .35 24 20 | -47 -1969 3754 8212
iac n/a| -5 4 5 9 51 -8 -.22 26 25 | 1718 -1739 3164 8762
Table 2.2201.1 GPS week: 2201 Day: 1 MJD: 59652
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 52 -44 3 .15 25 16 | 25845 228 2988 8908
emx n/a| -2 2 -11 47 -31 -10 -.03 39 35 | -1905 495 2976 8775
esx n/a| -1 -1 0 -1 -43 -45 -.12 23 18 | -2583 -681 2987 12028
gfz n/a| 0 0 4 -57 5 25 -.07 30 16 | 0 182 2971 8390
grg n/a| 1 0 -4 -13 -2 106 .29 28 22 | -6514 2 3007 8586
iac n/a| 1 -1 5 -23 110 -83 -.24 29 29 | -6027 2057 3003 9481
Table 2.2201.2 GPS week: 2201 Day: 2 MJD: 59653
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 10 -23 8 .11 20 13 | 25254 -251 3012 9777
emx n/a| -1 2 -10 -20 6 63 -.00 33 30 | -28682 -22 3003 9582
esx n/a| 0 0 1 -4 -16 -10 -.11 27 22 | -1617 -456 2998 12863
gfz n/a| 3 0 7 -28 10 -3 -.06 34 15 | 0 -93 2917 9563
grg n/a| 1 -1 -12 -28 1 -5 .29 27 20 | -6631 83 3000 9580
iac n/a| 1 -2 3 4 14 -80 -.34 30 29 | -4803 1148 3003 10314
Table 2.2201.3 GPS week: 2201 Day: 3 MJD: 59654
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 23 4 31 .16 21 16 | 26604 293 3433 9137
emx n/a| -1 -1 -11 5 11 7 -.05 31 28 | -1294 172 3432 8944
esx n/a| 1 1 2 -8 -26 -18 -.03 27 18 | -8153 -459 3421 12918
gfz n/a| 0 0 7 -10 -1 -31 -.06 26 14 | 0 9 3472 8496
grg n/a| 0 -1 -8 -30 -8 -16 .29 27 18 | -6567 -10 3419 8637
iac n/a| -1 1 5 47 7 -11 -.29 30 26 | -559 -1430 3432 12259
Table 2.2201.4 GPS week: 2201 Day: 4 MJD: 59655
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 8 -10 32 .11 20 13 | 26365 -359 3583 8709
emx n/a| 1 1 -5 21 -16 27 -.10 35 31 | -8743 578 3572 8633
esx n/a| 0 2 0 9 -45 -36 -.07 27 17 | -5201 -315 3590 11414
gfz n/a| 0 0 2 -32 29 -20 -.04 27 16 | 0 250 3559 8220
grg n/a| 0 0 -9 -5 -18 22 .26 23 17 | -7042 -190 3592 8227
iac n/a| 3 0 3 -4 18 -9 -.27 26 25 | -1712 -1191 3660 12173
Table 2.2201.5 GPS week: 2201 Day: 5 MJD: 59656
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 -1 3 18 -22 88 .15 24 16 | 27827 -1340 3214 9101
emx n/a| -2 3 -5 46 27 40 .03 36 28 | -14415 -41 3214 8885
esx n/a| -1 2 0 6 -9 -63 -.03 27 16 | -14977 -2350 3222 12651
gfz n/a| 2 0 5 -36 1 -9 -.19 32 16 | 0 -1550 3216 8799
grg n/a| 0 -1 -5 -10 9 37 .28 24 18 | -5573 -1301 3214 8586
iac n/a| 0 -5 -1 7 27 -109 -.30 31 27 | -3737 -860 3206 9633
Table 2.2201.6 GPS week: 2201 Day: 6 MJD: 59657
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 7 -20 31 .12 22 15 | 33697 1873 2920 8879
emx n/a| 0 -1 -5 39 -4 -32 -.03 38 27 | 5701 1587 2887 8716
esx n/a| 1 0 3 -23 -11 -61 -.08 33 20 | 3946 1396 2901 11868
gfz n/a| -1 -1 11 -35 4 -44 -.04 39 17 | 0 1286 2929 8148
grg n/a| 2 -1 -9 0 37 86 .23 24 18 | 131 1213 2913 8232
iac n/a| -2 1 -2 6 38 -33 -.33 31 26 | 2702 97 2934 9402
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 3.2201.0 GPS week: 2201 Day: 0 MJD: 59651
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 894 48 49 43 18 21 17 15 | 107 54 57 83 85 74 75
R02 | 3772 7 25 12 18 13 18 7 | 63 45 72 64 56 70 62
R03 | 509 15 37 15 14 17 29 9 | 85 66 86 101 104 119 94
XR04 | 734 12 38 15 --- 15 18 9 | 84 60 89 --- 91 93 85
R05 | 1713 24 38 27 32 24 20 12 | 74 70 100 96 73 89 82
R07 | 656 10 30 13 17 17 30 8 | 90 63 77 84 77 91 80
R08 | 2558 9 29 10 9 19 20 7 | 67 48 72 70 68 74 66
R09 | 1038 17 18 11 20 18 29 8 | 43 43 37 40 38 51 38
XR11 | 1131 536 --- --- 807 59 71 65 | 317 --- --- 12 9 53 52
R12 | 1263 14 17 13 13 16 18 6 | 81 76 81 73 71 80 76
R13 | 562 23 32 10 19 38 29 11 | 86 68 74 77 58 87 74
R14 | 751 16 16 10 19 13 13 6 | 53 48 48 39 38 49 44
R15 | 713 10 19 12 14 8 18 6 | 58 60 63 55 55 50 56
R17E | 917 10 29 14 17 16 22 8 | 65 64 65 67 66 63 64
R18E | 755 10 22 18 15 15 15 7 | 27 18 31 23 35 27 25
R19E | 781 48 73 41 41 32 52 21 | 34 39 48 54 40 37 30
R20E | 1266 48 63 49 59 39 30 21 | 74 75 84 89 79 65 71
R21E | 796 12 36 19 12 18 17 8 | 38 24 29 37 42 39 32
R22E | 2454 54 49 49 57 51 38 22 | 38 41 65 65 72 54 43
R24E | 1618 12 35 13 13 14 20 8 | 34 31 36 39 39 42 34
------+-----------------------------------------+-------------------------------------
RMS | 1530 27 37 25 27 24 26 |T 75 52 63 61 59 65 59
WRMS | 1530 21 33 19 16 20 25 |NE 92 58 71 66 63 75 68
MEDI | 894 14 32 14 18 17 20 |MD 65 54 65 65 58 63 62
Table 3.2201.1 GPS week: 2201 Day: 1 MJD: 59652
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 601 40 45 39 24 29 27 15 | 77 47 46 60 76 55 57
R02 | 4146 15 24 13 14 14 22 7 | 41 24 41 42 34 42 37
R03 | 812 7 31 18 13 19 47 10 | 62 49 62 64 72 98 66
XR04 | 1071 6 37 18 --- 29 31 12 | 63 44 56 --- 82 89 65
R05 | 865 9 37 20 18 20 24 9 | 57 40 75 78 49 71 62
R07 | 603 17 29 25 13 19 24 9 | 64 48 68 55 47 54 55
R08 | 2083 16 27 14 16 21 18 8 | 46 37 45 47 47 56 45
R09 | 1260 15 18 8 18 22 25 8 | 42 33 37 43 45 29 35
XR11 | 8879 --- --- --- --- --- 9 0 | --- --- --- --- --- 94 113
R12 | 970 10 15 12 8 19 20 6 | 56 60 58 52 45 61 53
R13 | 854 34 27 25 30 41 20 13 | 58 49 44 56 42 47 47
R14 | 750 15 15 9 13 21 16 6 | 41 33 36 29 24 36 32
R15 | 763 11 25 8 15 12 20 6 | 38 45 40 31 32 31 34
R17E | 838 14 23 14 15 19 15 7 | 71 73 66 72 73 85 71
R18E | 1019 12 23 16 16 14 27 8 | 24 21 26 23 30 27 22
R19E | 1191 39 63 27 37 33 49 18 | 32 33 54 49 43 24 31
R20E | 887 46 69 37 83 60 42 25 | 75 74 71 86 83 68 69
R21E | 672 9 33 16 13 15 21 8 | 31 23 26 30 39 34 28
R22E | 1547 51 78 52 60 55 47 25 | 45 75 74 66 72 42 50
R24E | 3154 11 35 13 19 17 27 9 | 28 25 28 31 32 33 25
------+-----------------------------------------+-------------------------------------
RMS | 1577 25 39 23 30 28 29 |T 50 43 50 50 50 53 49
WRMS | 1577 16 35 18 16 22 29 |NE 53 42 50 50 49 58 53
MEDI | 887 15 29 16 16 20 24 |MD 46 44 46 49 45 47 47
Table 3.2201.2 GPS week: 2201 Day: 2 MJD: 59653
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 658 44 40 46 25 28 20 16 | 95 65 43 65 56 61 63
R02 | 3809 5 24 16 15 15 18 6 | 61 44 65 69 63 59 60
R03 | 660 8 29 27 10 12 55 11 | 73 61 60 72 79 115 74
XR04 | 1433 11 23 22 --- 16 29 9 | 78 70 70 --- 85 86 76
R05 | 749 8 25 14 12 13 18 6 | 72 54 77 68 67 76 69
R07 | 1008 14 32 14 17 13 23 8 | 77 54 69 81 76 76 72
R08 | 1765 8 27 17 18 21 24 8 | 54 48 56 57 42 67 51
R09 | 833 10 23 12 26 16 25 8 | 34 26 35 38 28 37 29
R12 | 721 11 15 21 11 21 25 7 | 71 71 74 67 68 85 71
R13 | 1124 19 32 33 29 38 34 13 | 72 66 52 56 62 72 60
R14 | 980 10 14 13 9 24 13 6 | 47 41 49 45 33 46 42
R15 | 1182 8 13 7 14 22 21 6 | 58 51 50 49 50 67 52
R17E | 1508 16 32 14 17 16 40 10 | 77 72 81 85 83 57 75
R18E | 1243 8 21 17 12 11 20 6 | 28 23 31 30 32 34 27
R19E | 699 39 50 34 41 29 40 17 | 27 31 48 62 50 29 34
R20E | 777 33 62 50 103 67 44 27 | 56 41 72 116 51 51 53
R21E | 726 12 29 14 9 13 21 7 | 34 30 31 34 42 41 33
R22E | 907 36 46 57 67 46 45 22 | 44 48 74 71 56 43 42
R24E | 3216 11 37 13 18 13 20 8 | 27 19 24 28 34 28 24
------+-----------------------------------------+-------------------------------------
RMS | 1519 20 33 27 34 27 30 |T 57 48 55 60 55 59 53
WRMS | 1519 13 30 22 15 20 29 |NE 66 54 58 60 59 70 59
MEDI | 980 11 29 17 17 16 24 |MD 58 48 56 62 56 59 53
Table 3.2201.3 GPS week: 2201 Day: 3 MJD: 59654
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 1078 41 37 47 26 37 26 16 | 79 40 53 68 45 56 52
R02 | 2558 6 22 15 12 22 21 7 | 52 39 61 59 42 66 51
R03 | 736 5 28 11 16 17 13 7 | 75 49 70 87 87 71 74
XR04 | 821 16 23 7 --- 15 15 8 | 72 48 67 --- 78 67 67
R05 | 891 9 18 10 9 7 30 6 | 55 46 60 56 57 83 57
R07 | 903 8 25 13 15 12 19 6 | 71 43 61 72 70 65 64
R08 | 955 14 30 28 21 18 31 10 | 59 36 65 72 52 82 59
R09 | 1200 12 17 12 12 16 15 6 | 24 24 33 25 24 22 23
XR11 | 9569 --- --- --- --- --- 6 0 | --- --- --- --- --- 64 64
R12 | 643 11 14 13 17 13 24 6 | 48 43 46 43 44 56 44
R13 | 544 33 26 31 13 52 52 16 | 79 61 49 59 46 93 60
R14 | 1847 9 15 11 19 15 40 8 | 39 35 40 33 37 65 38
R15 | 1373 12 12 7 11 12 19 5 | 55 49 49 47 46 39 47
R17E | 1859 7 31 13 16 16 17 7 | 90 88 90 93 91 94 90
R18E | 1163 12 21 15 16 12 16 6 | 30 20 31 27 33 30 27
R19E | 779 34 54 29 37 40 52 18 | 31 46 48 60 42 42 34
R20E | 866 30 56 54 60 56 34 22 | 87 83 109 92 83 75 84
R21E | 1246 10 29 15 12 12 26 7 | 29 22 30 33 34 39 28
R22E | 1048 39 47 60 62 36 43 22 | 32 36 76 75 67 48 45
R24E | 2416 18 36 16 15 16 26 9 | 30 26 27 32 36 42 27
------+-----------------------------------------+-------------------------------------
RMS | 1351 21 31 27 26 27 30 |T 54 43 56 57 53 59 51
WRMS | 1351 16 28 18 14 18 26 |NE 59 42 54 56 52 63 53
MEDI | 1048 12 26 15 16 16 24 |MD 55 43 53 59 46 64 51
Table 3.2201.4 GPS week: 2201 Day: 4 MJD: 59655
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 860 31 52 52 36 33 20 17 | 88 54 64 93 84 83 76
R02 | 1884 6 26 26 17 16 20 8 | 57 39 64 48 47 67 53
R03 | 945 10 23 15 14 19 20 7 | 75 61 70 70 81 60 69
XR04 | 740 10 26 14 --- 18 20 8 | 82 58 82 --- 90 73 78
R05 | 1366 14 25 18 13 10 36 8 | 70 60 76 82 78 100 76
R07 | 545 11 22 10 6 15 22 6 | 78 59 69 71 79 57 70
R08 | 858 11 31 11 13 15 26 7 | 64 44 71 70 64 84 66
R09 | 1213 14 16 13 20 14 14 7 | 34 33 38 37 34 35 33
XR11 | 8889 --- --- --- --- --- 5 0 | --- --- --- --- --- 35 33
R12 | 891 11 14 13 15 9 11 5 | 74 78 83 69 86 75 76
R13 | 753 23 34 25 25 32 48 14 | 78 83 66 83 61 76 72
R14 | 2261 6 14 12 10 13 21 5 | 44 43 48 43 41 53 44
R15 | 1526 10 17 11 14 16 15 6 | 57 49 58 58 65 63 57
R17E | 3031 6 27 14 15 14 18 6 | 86 82 86 85 81 82 83
R18E | 824 17 21 16 12 17 22 7 | 51 48 52 43 53 64 49
R19E | 1117 40 69 34 55 25 33 19 | 43 54 44 64 38 35 34
R20E | 953 25 55 51 59 55 38 21 | 70 65 65 86 93 67 66
R21E | 984 10 27 13 14 11 25 7 | 41 37 37 44 50 49 41
R22E | 758 43 54 57 45 34 36 20 | 36 39 88 69 57 67 48
R24E | 1894 10 38 16 16 16 19 8 | 32 24 32 36 39 37 31
------+-----------------------------------------+-------------------------------------
RMS | 1404 20 35 27 27 23 26 |T 61 53 62 63 64 63 57
WRMS | 1404 13 31 17 16 17 25 |NE 66 55 65 65 67 66 61
MEDI | 953 11 26 15 15 16 20 |MD 64 54 65 69 64 64 57
Table 3.2201.5 GPS week: 2201 Day: 5 MJD: 59656
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 530 35 51 50 22 33 40 17 | 79 43 57 73 72 76 62
R02 | 1085 10 29 19 13 12 28 8 | 51 40 60 49 55 71 53
R03 | 858 10 22 14 19 14 33 8 | 64 49 59 61 61 50 56
XR04 | 629 12 19 15 --- 14 31 9 | 70 62 68 --- 64 56 63
R05 | 1914 18 33 18 15 16 22 9 | 62 56 78 77 76 74 70
R07 | 1334 11 18 8 20 8 27 7 | 73 65 64 74 71 60 67
R08 | 1001 12 21 13 17 11 16 6 | 52 42 56 47 46 48 48
R09 | 1683 16 10 12 15 14 20 6 | 27 26 28 39 29 32 27
XR11 | 1037 --- --- --- --- --- 7 0 | --- --- --- --- --- 63 60
R12 | 1367 16 15 14 16 14 27 7 | 60 59 71 70 61 65 63
R13 | 1053 18 28 26 26 31 44 13 | 69 62 74 85 69 76 69
R14 | 1296 11 19 11 10 12 24 6 | 38 33 41 40 34 43 36
R15 | 1040 16 15 8 17 17 26 7 | 52 37 38 39 31 40 38
R17E | 3339 7 36 11 11 14 30 8 | 83 80 90 86 91 92 86
R18E | 1469 14 22 12 22 22 25 8 | 45 38 41 40 42 57 40
R19E | 714 44 70 39 50 33 41 20 | 42 35 52 75 37 35 31
R20E | 789 42 62 44 82 57 39 24 | 130 125 137 150 114 110 122
R21E | 1050 11 29 16 18 17 22 8 | 32 28 32 37 35 34 30
R22E | 1117 51 60 66 65 33 50 24 | 36 29 112 108 60 73 60
R24E | 966 13 36 16 16 13 19 8 | 28 26 29 31 30 34 26
------+-----------------------------------------+-------------------------------------
RMS | 1393 24 36 27 32 24 31 |T 57 49 62 65 56 59 55
WRMS | 1393 16 28 16 16 18 27 |NE 58 47 57 59 55 58 54
MEDI | 1050 14 28 15 17 14 27 |MD 52 42 59 61 60 57 56
Table 3.2201.6 GPS week: 2201 Day: 6 MJD: 59657
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01 | 852 46 36 61 21 30 30 18 | 112 57 59 81 87 71 77
R02 | 1651 10 23 22 13 10 17 7 | 66 50 76 71 59 77 65
R03 | 1287 10 34 15 17 11 42 10 | 84 66 80 92 92 101 85
XR04 | 885 8 23 16 --- 14 38 10 | 100 84 98 --- 102 108 98
R05 | 1704 12 21 18 20 12 20 7 | 84 79 99 107 87 90 89
R07 | 942 12 18 10 11 9 26 6 | 94 72 89 88 89 76 85
R08 | 1128 13 19 23 22 16 27 8 | 75 50 74 72 60 64 65
R09 | 2037 12 22 16 24 16 29 8 | 39 39 39 40 43 51 39
R12 | 1661 16 14 17 20 13 16 7 | 85 80 91 79 81 87 83
R13 | 651 15 31 37 35 44 49 16 | 87 74 82 88 72 103 82
R14 | 591 8 20 19 13 8 19 6 | 49 41 58 45 46 48 47
R15 | 948 11 14 14 13 18 19 7 | 61 54 61 54 51 57 55
R17E | 2405 10 28 14 9 13 16 6 | 92 93 92 95 93 92 92
R18E | 1130 12 20 18 24 19 19 8 | 43 42 45 47 50 59 45
R19E | 1463 39 96 45 87 31 48 26 | 50 89 44 116 49 55 50
R20E | 939 30 72 63 102 51 35 27 | 147 148 120 139 161 138 138
R21E | 1424 13 30 19 15 17 26 9 | 34 27 46 48 38 42 35
R22E | 1595 50 45 68 61 42 53 24 | 26 39 111 95 68 74 57
R24E | 1016 12 31 15 18 16 19 8 | 56 49 48 46 53 56 50
------+-----------------------------------------+-------------------------------------
RMS | 1383 22 38 33 39 24 31 |T 72 64 74 77 72 76 70
WRMS | 1383 15 27 20 17 18 26 |NE 78 62 75 74 72 77 72
MEDI | 1130 12 23 18 20 16 26 |MD 75 57 76 79 68 74 65
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