[IGSREPORT-28828] Wk 2219 IGLOS Final Orbits
acc
acc at igs.org
Mon Aug 8 01:53:46 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2219 (Jul 17, 2022 - Jul 23, 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 2.2219.
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:
igl2219[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2219 in the SP3 format.
igl22197.sum Combination Report for GPS Week 2219.
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 | 0.6 ns
1 | 1.6 ns
2 | -0.8 ns
3 | -0.5 ns
4 | -1.2 ns
5 | 0.5 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
----+--------+---------------
2 | EMX | R19
3 | EMX | R19
4 | 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 1.2219, 1a.2219).
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 2.2219.0-6)
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 3.2219.0-6).
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 2219 summary. (Jul 17, 2022 - Jul 23, 2022)
Table 1.2219.a GPS week : 2219 MJD: 59777.0-59783.0
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 2 -2 -24 14 .11 20 16 | 35439 -1213 3215 9129
| 0 1 1 11 17 12 .02 | 3885 2279
emx n/a| -1 0 -2 17 -7 -21 -.12 45 29 | -11847 -933 3220 8867
| 1 2 3 24 31 25 .03 | 5692 1469
esx n/a| 0 0 0 -3 -4 0 -.09 27 21 | -3840 -121 3183 11878
| 1 0 1 13 12 16 .03 | 11633 2268
gfz n/a| 0 0 0 -3 -2 35 -.08 23 14 | 0 -1153 3242 8735
| 0 1 2 27 17 25 .04 | 0 2157
grg n/a| 2 0 -2 7 38 -48 .38 26 19 | -784 -1073 3188 8557
| 1 0 2 15 9 44 .03 | 2604 2126
iac n/a| 0 0 0 4 12 6 -.27 23 22 | 1290 -773 3178 9549
| 2 1 1 23 10 34 .06 | 3153 1312
Table 1.2219.b GPS week : 2219 MJD: 59777.0-59783.0
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 16 18 18 18 16 |
R02 | 7 6 6 8 8 6 7 |
R03 | 7 8 7 8 7 9 8 |
R04 | 9 9 10 8 8 9 10 |
R05 | 7 8 8 8 8 7 8 |
R07 | 9 10 8 8 9 7 7 |
R08 | 10 8 8 8 8 7 7 |
R09 | 6 8 6 8 6 7 7 |
R11 | 14 11 12 11 11 9 9 |
R12 | 7 8 10 8 8 8 7 |
R13 | 16 15 11 11 14 14 14 |
R14 | 7 7 5 8 7 7 6 |
R15 | 7 7 7 6 6 9 6 |
R17 | 7 7 8 8 7 8 6 |
R18 | 10 12 9 7 9 9 9 |
R19 | 32 28 25 25 24 24 22 |
R20 | 21 21 21 23 22 21 21 |
R21 | 7 8 8 8 8 7 7 |
R24 | 9 10 8 8 8 10 9 |
Table 1.2219.c GPS week : 2219 MJD: 59777.0-59783.0
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 2219 0 | -8 105 185 -442 -2321 4746 82.0 1504 1504 | 582 0
brd 2219 1 | -7 -34 130 -759 -117 13360 81.3 1732 1732 | 1568 0
brd 2219 2 | -32 -27 130 1210 -823 6569 83.1 1686 1686 | -815 0
brd 2219 3 | -7 -22 133 416 -183 6104 84.2 1667 1667 | -464 0
brd 2219 4 | 14 -18 287 12 560 5453 81.5 1715 1715 | -1235 0
brd 2219 5 | 104 49 339 -1848 985 8341 82.4 1764 1764 | 480 0
brd 2219 6 | 58 39 265 -857 544 3611 82.0 1639 1639 | -7991 0
-------------+------------------------------------------------------------+----------------
brd 2219 mean| 17 13 210 -323 -193 6883 82.4 1672 1672 | -1125 0
brd 2219 sdev| 47 53 86 985 1112 3217 1.0 85 85 | 3173 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 2.2219.0 GPS week: 2219 Day: 0 MJD: 59777
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 18 -6 -1 .07 20 15 | 35749 716 3324 8274
emx n/a| 0 -1 0 58 -69 -24 -.11 33 31 | -13576 339 3362 8075
esx n/a| 1 0 -2 0 -4 1 -.11 21 17 | -14740 1226 3267 11313
gfz n/a| 0 0 0 -52 -18 26 -.12 17 14 | 0 529 3346 7980
grg n/a| 3 0 4 15 42 -9 .34 21 18 | 17 769 3264 7636
iac n/a| 0 2 -2 -5 23 -51 -.19 29 28 | 2481 -217 3253 8823
Table 2.2219.1 GPS week: 2219 Day: 1 MJD: 59778
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 -1 -28 1 .12 22 14 | 38680 2146 2601 10484
emx n/a| -3 -2 0 0 0 -60 -.09 44 32 | -18984 1101 2666 10158
esx n/a| 1 0 1 15 1 -10 -.05 28 21 | -16766 3164 2634 13383
gfz n/a| 0 -1 -1 -3 19 61 -.05 24 15 | 0 1978 2689 10136
grg n/a| 1 0 -3 24 30 -59 .39 32 20 | 383 1898 2653 9906
iac n/a| -1 0 -1 -24 -2 13 -.29 25 25 | 4022 276 2626 10799
Table 2.2219.2 GPS week: 2219 Day: 2 MJD: 59779
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 0 0 27 .13 21 15 | 38592 -4141 3294 8725
emx n/a| -2 2 -2 24 11 -4 -.15 49 27 | -15822 -2759 3317 8483
esx n/a| -2 1 1 2 -19 17 -.13 29 22 | 121 -2568 3320 11078
gfz n/a| 0 1 1 -26 -9 76 -.08 22 12 | 0 -3082 3407 8253
grg n/a| 2 0 -3 26 21 -117 .40 22 17 | 506 -3347 3329 8195
iac n/a| 2 0 0 -7 10 12 -.32 21 21 | 2159 -2208 3313 9065
Table 2.2219.3 GPS week: 2219 Day: 3 MJD: 59780
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 -2 -13 9 .08 20 16 | 36428 -1407 3486 8026
emx n/a| -3 -1 0 10 -9 3 -.12 53 29 | -9245 -1360 3468 7846
esx n/a| 0 0 2 -7 -22 24 -.07 31 25 | -8766 -451 3410 10870
gfz n/a| -1 2 5 20 -27 41 -.09 22 15 | 0 -1308 3438 7931
grg n/a| 4 0 -4 0 50 -92 .40 25 19 | 80 -1353 3407 7386
iac n/a| 0 -1 -2 -1 17 31 -.25 23 22 | 2010 32 3396 8528
Table 2.2219.4 GPS week: 2219 Day: 4 MJD: 59781
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 4 -18 -39 14 .12 19 16 | 34721 -2515 2791 9224
emx n/a| 0 1 -6 -13 -9 -24 -.09 48 28 | -9466 -1830 2811 8850
esx n/a| 0 0 -1 -20 8 -15 -.10 29 23 | 15425 -2073 2770 12815
gfz n/a| 0 0 3 3 -8 9 .01 25 12 | 0 -3087 2792 9093
grg n/a| 1 0 -2 -15 42 -49 .32 29 18 | 89 -2790 2773 8615
iac n/a| 0 0 -1 50 8 41 -.31 21 19 | 1328 -1940 2780 9735
Table 2.2219.5 GPS week: 2219 Day: 5 MJD: 59782
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 -2 -38 14 .13 17 16 | 36655 10 3200 9000
emx n/a| -2 -3 -8 4 34 -46 -.16 45 32 | -14299 186 3182 8734
esx n/a| 0 -1 0 -19 5 -18 -.04 26 19 | -8143 1970 3159 11310
gfz n/a| 1 0 0 7 12 8 -.10 25 16 | 0 385 3199 8464
grg n/a| 1 1 -2 10 42 -18 .41 29 22 | 108 463 3138 8364
iac n/a| -2 1 0 9 3 25 -.33 23 20 | 2649 878 3156 9305
Table 2.2219.6 GPS week: 2219 Day: 6 MJD: 59783
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 -10 -44 32 .12 21 18 | 27249 -3305 3813 10173
emx n/a| 0 0 -1 38 -10 5 -.13 40 27 | -1538 -2209 3735 9927
esx n/a| 0 0 -1 5 2 2 -.10 24 19 | 5984 -2116 3721 12383
gfz n/a| 1 0 -1 24 12 25 -.09 22 16 | 0 -3486 3826 9290
grg n/a| 2 0 -1 -8 37 3 .39 24 17 | -6676 -3157 3753 9801
iac n/a| -3 -1 1 10 26 -30 -.18 19 17 | -5613 -2235 3727 10594
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 3.2219.0 GPS week: 2219 Day: 0 MJD: 59777
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1175 39 56 30 34 41 33 17 | 82 78 78 88 83 74 78
R02E | 2451 10 21 13 12 13 24 6 | 38 41 40 42 47 49 40
R03E | 1200 10 33 11 12 14 11 6 | 73 70 72 76 78 74 73
XR04E | 2213 14 31 15 --- 17 19 9 | 33 30 31 --- 41 29 30
R05E | 845 16 26 10 10 14 16 6 | 61 60 58 56 64 55 58
R07E | 830 17 35 12 13 20 30 9 | 115 117 113 112 115 113 113
R08E | 1522 12 38 11 13 18 48 10 | 114 121 117 116 111 125 115
R09 | 1121 13 15 11 12 15 18 6 | 39 43 42 46 44 52 43
XR11 | 2585 --- 28 13 27 33 36 13 | --- 30 32 35 30 38 29
R12 | 719 12 16 14 14 13 28 7 | 53 50 58 56 53 64 55
XR13 | 890 28 --- 30 30 40 32 16 | 69 --- 55 70 59 47 60
R14 | 634 11 19 11 7 20 23 6 | 43 40 47 43 50 41 43
R15 | 1507 10 14 9 10 15 29 6 | 62 61 61 61 64 67 61
R17 | 1765 13 20 10 11 14 29 7 | 53 46 47 51 52 45 48
R18 | 1625 10 23 26 9 11 49 9 | 36 32 48 37 43 38 36
XR19 |>>>>> 42 --- 78 --- 39 44 32 | 80 --- 60 --- 80 82 63
R20 | 2560 47 61 60 37 39 21 20 | 80 56 50 81 82 67 67
R21 | 1315 11 26 9 7 21 19 6 | 52 41 47 50 51 49 47
R24 | 1699 16 42 8 10 14 30 8 | 52 43 51 53 59 61 52
------+-----------------------------------------+-------------------------------------
RMS | 1504 20 33 21 17 21 29 |T 63 56 58 63 63 61 58
WRMS | 1504 15 31 17 14 18 28 |NE 56 44 49 53 55 54 50
MEDI | 1507 13 26 12 12 17 29 |MD 53 46 51 56 59 55 55
Table 3.2219.1 GPS week: 2219 Day: 1 MJD: 59778
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1393 38 48 38 52 25 28 17 | 62 61 61 69 59 65 57
R02E | 4116 8 22 13 8 15 20 6 | 38 30 35 39 43 40 37
R03E | 1529 11 31 14 17 16 16 7 | 86 83 80 90 87 80 83
XR04E | 1495 9 38 13 --- 19 19 9 | 31 32 32 --- 38 31 29
R05E | 1283 16 37 17 14 17 14 8 | 57 58 67 62 71 67 62
R07E | 932 14 36 22 17 26 25 10 | 107 106 104 107 108 117 107
R08E | 1984 8 43 15 13 12 18 8 | 78 86 74 77 82 78 77
R09 | 841 16 18 14 12 13 23 7 | 38 51 44 48 41 57 44
XR11 | 2628 --- 12 21 12 16 32 10 | --- 32 38 37 32 44 32
R12 | 974 11 9 17 20 16 21 7 | 36 35 49 48 39 47 40
R13 | 794 14 30 27 34 63 17 14 | 51 70 45 60 32 39 45
R14 | 721 5 14 16 9 12 27 6 | 37 36 42 40 41 31 36
R15 | 1282 15 18 12 11 18 14 6 | 47 50 47 47 43 47 44
R17 | 1156 13 24 10 16 20 17 7 | 39 39 38 43 39 39 37
R18 | 1838 8 18 32 18 15 51 12 | 30 27 30 32 33 40 25
R19 | 1194 45 125 64 41 84 21 28 | 55 48 45 67 75 31 41
R20 | 3173 52 47 61 45 36 28 21 | 57 58 56 56 58 44 50
R21 | 866 10 28 8 14 24 24 8 | 42 39 41 40 49 43 39
R24 | 1369 9 52 11 10 17 28 9 | 44 40 36 41 50 52 41
------+-----------------------------------------+-------------------------------------
RMS | 1731 22 44 28 24 32 25 |T 51 51 50 55 53 52 48
WRMS | 1731 14 32 21 15 20 25 |NE 43 43 42 46 44 42 39
MEDI | 1283 11 30 16 14 17 21 |MD 44 48 45 48 43 44 41
Table 3.2219.2 GPS week: 2219 Day: 2 MJD: 59779
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1488 34 44 42 43 20 31 16 | 44 46 57 52 47 46 42
R02E | 1906 8 23 10 11 17 15 6 | 28 27 28 23 35 25 25
R03E | 1231 15 25 16 9 14 19 7 | 97 89 103 92 97 88 94
XR04E | 1208 12 32 18 --- 14 26 10 | 24 18 24 --- 28 25 20
R05E | 901 11 33 12 14 12 20 7 | 41 41 48 44 52 48 44
R07E | 1658 15 28 16 13 16 16 7 | 68 73 71 74 78 72 71
R08E | 2692 8 30 14 16 13 21 7 | 48 49 49 53 49 50 47
R09 | 2069 12 19 11 15 16 12 6 | 25 25 26 37 24 32 26
XR11 | 3193 --- 24 19 24 24 25 11 | --- 21 30 17 36 39 21
R12 | 781 14 18 17 20 22 31 9 | 44 46 47 57 52 39 45
R13 | 764 9 31 11 24 36 23 10 | 43 54 56 48 36 40 45
R14 | 1052 5 14 7 9 13 17 4 | 36 31 40 39 30 40 35
R15 | 1001 14 12 13 14 13 17 6 | 50 45 46 47 44 45 45
R17 | 1339 12 26 18 10 22 22 8 | 40 28 33 30 51 44 35
R18 | 2494 11 28 27 15 15 22 8 | 33 28 33 38 43 45 34
R19 | 2193 44 165 76 37 48 21 24 | 52 39 27 48 53 39 45
R20 | 2145 47 48 62 48 33 31 21 | 57 45 42 59 52 47 46
R21 | 687 10 31 16 17 17 15 7 | 52 48 48 61 60 51 52
R24 | 2160 13 30 11 9 18 18 7 | 38 41 34 32 35 39 34
------+-----------------------------------------+-------------------------------------
RMS | 1686 21 49 29 22 22 21 |T 45 41 44 47 47 44 42
WRMS | 1686 15 27 22 12 17 21 |NE 42 37 38 42 43 41 38
MEDI | 1488 12 28 16 15 17 21 |MD 43 41 42 47 47 44 44
Table 3.2219.3 GPS week: 2219 Day: 3 MJD: 59780
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1515 32 51 36 45 20 50 17 | 58 65 55 73 55 49 52
R02E | 1410 14 37 14 11 17 16 8 | 46 32 47 44 51 44 43
R03E | 1881 13 30 12 13 17 16 7 | 132 137 145 140 140 130 136
XR04E | 901 12 21 19 --- 15 12 7 | 32 27 31 --- 32 28 27
R05E | 1119 13 31 15 13 13 18 7 | 72 70 71 73 76 72 71
R07E | 692 10 29 13 18 15 18 7 | 131 134 131 133 140 141 134
R08E | 1579 8 30 20 18 14 21 8 | 44 42 41 48 49 38 41
R09 | 3173 12 19 13 16 24 17 7 | 19 21 19 24 35 31 19
XR11 | 3508 --- 19 27 18 20 23 11 | --- 27 33 27 26 22 17
R12 | 593 16 16 17 14 17 22 7 | 30 22 21 21 22 30 20
R13 | 674 12 23 22 20 33 28 10 | 44 47 49 53 31 49 42
R14 | 1576 9 18 17 16 22 17 7 | 29 29 43 45 24 42 32
R15 | 923 12 12 15 9 12 14 5 | 46 37 47 48 40 46 43
R17 | 1508 13 24 15 18 12 18 7 | 36 25 29 28 39 35 30
R18 | 1380 12 16 26 11 15 11 7 | 27 25 31 25 36 30 26
R19 | 963 51 182 77 18 57 19 25 | 74 49 35 52 74 54 56
R20 | 3203 36 58 73 54 50 30 22 | 58 52 34 66 60 53 49
R21 | 1123 7 35 13 18 13 19 7 | 47 46 42 49 53 46 46
R24 | 2085 11 32 9 13 19 22 8 | 32 31 34 24 31 43 29
------+-----------------------------------------+-------------------------------------
RMS | 1667 20 53 31 22 25 23 |T 53 48 49 54 53 51 48
WRMS | 1667 16 29 25 15 19 22 |NE 40 34 34 38 39 40 34
MEDI | 1410 12 29 17 16 17 18 |MD 44 37 41 48 40 44 42
Table 3.2219.4 GPS week: 2219 Day: 4 MJD: 59781
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 2582 25 43 36 65 31 36 18 | 50 55 63 89 60 67 54
R02E | 2239 8 28 18 14 19 16 7 | 37 38 47 44 38 31 37
R03E | 2605 10 26 11 14 13 12 6 | 83 67 74 83 73 80 77
XR04E | 937 10 23 14 --- 17 14 7 | 33 30 35 --- 37 39 32
R05E | 795 15 29 13 14 16 18 7 | 49 51 48 48 53 36 45
R07E | 1005 19 33 14 19 13 21 9 | 93 94 89 83 89 76 85
R08E | 1343 9 28 17 13 22 16 7 | 59 60 67 65 62 57 60
R09 | 2750 10 15 13 14 11 19 6 | 37 30 26 39 39 39 33
XR11 | 3790 --- 16 26 16 22 27 11 | --- 26 31 27 33 40 26
R12 | 621 13 14 20 12 16 25 7 | 48 45 46 45 55 49 46
R13 | 622 16 26 33 33 51 25 14 | 44 41 35 39 32 47 36
R14 | 1327 8 12 16 14 15 19 6 | 30 26 38 37 23 25 27
R15 | 739 15 14 16 8 9 14 6 | 48 45 39 43 44 39 42
R17 | 1708 13 31 9 14 16 13 7 | 33 29 34 34 33 28 30
R18 | 1352 12 21 27 8 25 19 8 | 30 23 33 28 33 30 28
R19 | 1010 36 159 76 26 50 31 23 | 49 34 52 58 56 47 47
R20 | 3019 39 62 51 47 70 26 22 | 70 39 39 59 60 47 49
R21 | 825 20 27 9 7 16 15 7 | 48 34 48 47 42 43 43
R24 | 1369 12 35 16 10 14 17 7 | 38 28 36 32 40 37 33
------+-----------------------------------------+-------------------------------------
RMS | 1715 19 48 29 25 29 21 |T 48 41 46 50 47 45 43
WRMS | 1715 16 28 23 12 18 19 |NE 43 33 38 40 40 39 36
MEDI | 1343 13 27 16 14 16 19 |MD 48 38 39 44 42 40 42
Table 3.2219.5 GPS week: 2219 Day: 5 MJD: 59782
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 2780 35 49 45 43 39 38 18 | 87 92 113 103 83 99 91
R02E | 1326 10 29 11 18 10 10 6 | 41 39 40 46 45 44 41
R03E | 3379 10 33 20 24 20 13 8 | 109 101 99 112 106 106 105
XR04E | 688 11 34 12 --- 17 22 9 | 45 45 48 --- 46 40 43
R05E | 886 10 33 13 21 18 9 7 | 60 69 64 70 67 65 64
R07E | 1602 14 29 16 12 11 16 7 | 139 144 140 139 143 151 142
R08E | 1429 12 29 16 11 14 13 6 | 84 85 74 79 88 77 80
R09 | 2478 11 14 11 11 13 28 7 | 32 35 32 37 30 43 33
XR11 | 2741 --- 24 15 13 17 21 9 | --- 40 29 30 27 41 30
R12 | 801 17 28 15 18 18 8 7 | 48 52 56 57 43 47 49
R13 | 784 23 24 33 29 49 26 14 | 43 32 45 50 40 49 41
R14 | 1245 11 17 13 18 22 9 6 | 38 41 42 40 44 35 37
R15 | 784 11 17 14 22 14 31 8 | 44 47 51 55 43 45 44
R17 | 1407 13 21 13 22 12 26 8 | 33 30 39 37 38 39 34
R18 | 1215 9 30 27 15 17 17 8 | 33 31 34 32 35 36 31
R19 | 1214 26 126 52 39 53 37 23 | 34 32 37 36 32 37 32
R20 | 3013 26 70 48 53 69 22 20 | 40 59 54 51 44 37 44
R21 | 1092 10 31 12 12 17 19 7 | 38 33 35 36 41 47 37
R24 | 1346 21 51 8 10 19 28 10 | 41 51 35 35 36 43 35
------+-----------------------------------------+-------------------------------------
RMS | 1763 17 45 25 25 29 23 |T 54 55 56 58 54 56 53
WRMS | 1763 16 32 19 16 22 20 |NE 38 40 40 41 37 41 37
MEDI | 1326 11 29 15 18 17 21 |MD 41 45 45 46 43 44 41
Table 3.2219.6 GPS week: 2219 Day: 6 MJD: 59783
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac IGL | cod emx esx gfz grg iac IGL
------+-----------------------------------------+-------------------------------------
R01E | 1825 34 48 35 39 27 34 16 | 96 92 95 101 100 92 93
R02E | 2118 12 29 15 10 12 18 7 | 37 28 38 38 44 34 35
R03E | 3507 11 30 21 17 15 14 8 | 109 109 118 115 108 117 112
XR04E | 616 11 36 12 --- 20 20 9 | 71 64 64 --- 77 63 67
R05E | 921 18 33 16 14 15 14 8 | 49 50 60 58 59 58 54
R07E | 2464 9 25 12 13 14 18 6 | 122 116 119 117 116 111 116
R08E | 878 9 28 9 14 17 17 7 | 95 94 92 97 92 90 93
R09 | 1773 13 8 8 18 23 15 7 | 31 37 35 45 35 46 36
XR11 | 2512 --- 23 17 14 19 19 9 | --- 32 29 27 33 41 29
R12 | 631 19 18 9 11 19 11 6 | 55 54 54 59 51 55 54
R13 | 813 30 19 42 28 33 24 14 | 50 38 48 55 45 50 45
R14 | 866 16 11 12 16 12 15 6 | 39 32 40 37 39 30 34
R15 | 849 12 18 12 17 10 13 6 | 52 52 52 52 53 54 51
R17 | 1357 8 24 14 15 11 9 6 | 56 43 51 55 60 50 52
R18 | 1012 14 19 28 20 14 18 8 | 43 42 54 46 45 41 43
R19 | 1143 37 101 56 27 42 30 21 | 76 47 33 58 75 71 60
R20 | 2443 43 76 36 47 55 28 20 | 88 62 57 87 78 64 69
R21 | 932 15 21 11 10 17 16 6 | 64 52 58 60 64 52 58
R24 | 1089 17 46 10 25 8 15 9 | 54 47 50 58 54 56 50
------+-----------------------------------------+-------------------------------------
RMS | 1639 21 40 24 22 24 19 |T 65 57 60 64 64 61 60
WRMS | 1639 18 27 19 16 17 17 |NE 55 44 46 53 52 50 48
MEDI | 1089 14 25 14 16 17 17 |MD 55 50 54 58 59 55 54
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