[IGSREPORT-28139] Wk 2170 IGLOS Final Orbits
acc
acc at igs.org
Fri Aug 27 00:35:06 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2170 (Aug 08, 2021 - Aug 14, 2021)
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 2.2170.
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:
igl2170[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2170 in the SP3 format.
igl21707.sum Combination Report for GPS Week 2170.
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 | 2.6 ns
2 | -2.3 ns
3 | -3.3 ns
4 | -5.0 ns
5 | 0.4 ns
6 | -3.5 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 1.2170, 1a.2170).
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 2.2170.0-6)
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 3.2170.0-6).
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 2170 summary. (Aug 08, 2021 - Aug 14, 2021)
Table 1.2170.a GPS week : 2170 MJD: 59434.0-59440.0
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 -1 0 -28 -45 .11 26 23 | 16332 -644 3361 8558
| 0 0 2 12 16 33 .02 | 1371 4107
emx n/a| -1 1 4 -12 7 -33 -.20 38 28 | -11515 -556 3418 9158
| 1 1 1 14 13 37 .07 | 9152 2287
esx n/a| 0 0 -1 21 12 19 -.02 32 26 | -874 371 3352 8885
| 1 0 1 28 12 37 .04 | 10068 3822
gfz n/a| 1 0 0 -10 -7 9 -.06 22 15 | 0 -782 3415 8357
| 0 1 2 15 21 21 .04 | 0 4087
grg n/a| 3 0 2 16 25 -133 .38 33 24 | -1608 -528 3404 8333
| 1 1 2 18 16 46 .03 | 1213 3930
iac n/a| -2 -4 -2 -20 -10 218 -.14 30 27 | 891 -1325 3363 9031
| 2 0 3 23 36 80 .09 | 2566 1906
mcc n/a| 0 5 0 -37 166 393 -.76 166 166 | --- --- --- ---
| 8 9 5 102 355 226 .15 | --- ---
Table 1.2170.b GPS week : 2170 MJD: 59434.0-59440.0
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 21 17 17 19 21 20 |
R02 | 7 9 9 9 7 9 8 |
R03 | 6 8 8 8 7 7 7 |
R04 | 9 10 12 11 9 8 7 |
R05 | 8 10 12 9 8 8 7 |
R07 | 8 9 10 7 7 7 7 |
R08 | 8 8 6 8 8 8 6 |
R09 | 10 11 11 14 11 9 7 |
R11 | 11 10 10 16 11 12 12 |
R12 | 7 8 6 10 11 9 9 |
R13 | 16 13 16 12 16 17 12 |
R14 | 7 8 7 6 9 8 7 |
R15 | 7 7 6 9 9 8 7 |
R16 | 15 13 13 16 14 13 16 |
R17 | 8 7 9 8 8 8 7 |
R18 | 9 10 9 10 9 9 9 |
R19 | 30 30 27 25 23 23 23 |
R20 | 23 24 23 20 19 20 19 |
R21 | 8 9 9 8 10 9 8 |
R22 | 17 19 20 24 29 22 21 |
R24 | 12 12 8 11 9 8 8 |
Table 1.2170.c GPS week : 2170 MJD: 59434.0-59440.0
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 2170 0 | 22 48 137 -2069 919 7866 84.0 1628 1628 | -567 0
brd 2170 1 | -37 -88 59 192 1950 4409 82.9 1805 1805 | 2573 0
brd 2170 2 | -4 -96 75 2341 2356 7908 82.4 1433 1433 | -2297 0
brd 2170 3 | -36 -77 94 2304 1471 6545 84.6 7852 7852 | -3274 0
brd 2170 4 | -62 -25 34 2113 -1366 -651 84.1 1134 1134 | -4970 0
brd 2170 5 | 59 28 87 -1209 -1133 -970 84.7 1189 1189 | 350 0
brd 2170 6 | -19 -80 -21 -463 -731 -3667 83.6 1614 1614 | -3543 0
-------------+------------------------------------------------------------+----------------
brd 2170 mean| -11 -41 66 458 495 3062 83.8 2379 2379 | -1675 0
brd 2170 sdev| 41 59 50 1815 1545 4758 .8 2425 2425 | 2603 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 2.2170.0 GPS week: 2170 Day: 0 MJD: 59434
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 -6 -22 5 .08 28 23 | 14106 -1847 3083 8561
emx n/a| 0 0 5 1 19 -15 -.20 41 27 | -14608 -1814 3169 9220
esx n/a| 0 1 0 31 4 8 -.06 30 24 | -4039 -514 3081 11368
gfz n/a| 1 1 0 12 17 18 -.06 24 14 | 0 -1798 3122 8391
grg n/a| 3 -1 0 14 30 -171 .40 32 21 | 175 -1696 3113 8219
iac n/a| -3 -3 -6 -39 -76 180 -.17 30 27 | 2197 -1417 3095 9040
mcc n/a| -8 8 -3 141 -123 648 -.62 166 166 | --- --- --- ---
Table 2.2170.1 GPS week: 2170 Day: 1 MJD: 59435
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 2 -26 -41 .10 27 22 | 16601 4899 3393 8912
emx n/a| 0 0 6 4 15 -96 -.10 38 24 | -11868 2560 3447 9582
esx n/a| 0 0 -2 1 10 44 -.03 33 29 | 9192 5431 3383 8387
gfz n/a| 0 0 0 -35 6 20 -.12 26 18 | 0 4651 3456 8785
grg n/a| 3 1 4 30 15 -85 .39 29 20 | -75 4873 3443 8556
iac n/a| -6 -4 -4 -10 -3 275 -.21 35 32 | 4900 -205 3368 9473
mcc n/a| -9 7 2 -78 24 507 -.88 200 200 | --- --- --- ---
Table 2.2170.2 GPS week: 2170 Day: 2 MJD: 59436
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 9 -44 -104 .13 28 23 | 17785 463 3351 7981
emx n/a| 0 4 4 -21 -4 -7 -.21 37 25 | -3407 -632 3420 8528
esx n/a| -1 0 0 -25 8 11 -.03 32 28 | -4857 785 3358 6809
gfz n/a| 0 1 -3 -1 -37 -10 -.06 21 16 | 0 -84 3435 7846
grg n/a| 6 1 4 8 13 -166 .34 34 25 | -2523 153 3408 7692
iac n/a| -2 -5 0 25 47 296 -.08 27 24 | 1350 -2647 3361 8357
mcc n/a| 13 4 9 56 123 544 -.74 128 128 | --- --- --- ---
Table 2.2170.3 GPS week: 2170 Day: 3 MJD: 59437
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 -4 15 -6 -24 .11 24 24 | 17522 -983 3551 8469
emx n/a| -3 0 5 -37 2 16 -.32 38 30 | -23706 -357 3621 9167
esx n/a| -1 1 -3 53 14 37 .00 36 35 | 4980 -46 3530 8133
gfz n/a| 1 1 3 -10 -16 14 -.10 23 18 | 0 -1389 3609 8244
grg n/a| 3 -2 0 35 13 -195 .35 33 24 | -3082 -679 3616 8253
iac n/a| 1 -4 1 -44 -3 135 -.03 28 28 | -1466 -640 3534 8959
mcc n/a| 6 -6 -6 -113 -6 355 -.87 111 111 | --- --- --- ---
Table 2.2170.4 GPS week: 2170 Day: 4 MJD: 59438
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 -4 -19 -10 -46 .13 24 23 | 15607 -7133 3180 9833
emx n/a| -3 2 6 -2 -13 -19 -.18 41 36 | 3314 -4164 3274 10445
esx n/a| 1 1 0 54 39 59 .04 33 29 | -20400 -5503 3174 12026
gfz n/a| 2 0 0 -23 -29 11 -.03 22 16 | 0 -7358 3207 9648
grg n/a| 2 -1 4 -18 38 -114 .41 34 27 | -1882 -6651 3206 9506
iac n/a| -3 -5 -5 -27 -8 220 -.20 31 29 | -3080 -1992 3201 10412
mcc n/a| -1 -3 3 -39 -55 -13 -.57 119 119 | --- --- --- ---
Table 2.2170.5 GPS week: 2170 Day: 5 MJD: 59439
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 8 -47 -55 .10 23 20 | 15300 3555 3927 9137
emx n/a| -2 0 3 -16 25 -55 -.22 37 29 | -11171 1949 3923 9682
esx n/a| 0 0 0 8 5 31 .01 31 21 | 6473 4759 3918 8969
gfz n/a| 0 0 -4 -3 -10 37 -.00 22 13 | 0 3676 3992 8878
grg n/a| 3 -1 0 18 54 -72 .42 33 24 | -1901 3559 3954 9071
iac n/a| -1 -4 0 -21 -8 106 -.24 30 25 | 1314 1800 3938 9633
mcc n/a| 4 20 0 -73 286 497 -.65 192 192 | --- --- --- ---
Table 2.2170.6 GPS week: 2170 Day: 6 MJD: 59440
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 -10 -39 -49 .11 26 23 | 17403 -3466 3043 7015
emx n/a| 0 0 1 -16 8 -53 -.17 37 28 | -19163 -1436 3075 7488
esx n/a| 0 0 0 29 3 -54 -.08 27 20 | 2530 -2311 3025 6508
gfz n/a| 0 0 -1 -12 13 -27 -.06 17 10 | 0 -3172 3087 6712
grg n/a| 0 0 0 26 10 -131 .37 34 27 | -1973 -3259 3094 7036
iac n/a| -3 -4 -3 -26 -23 312 -.04 28 22 | 1026 -4175 3049 7344
mcc n/a| -1 9 -5 -152 914 218 -.98 248 248 | --- --- --- ---
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 3.2170.0 GPS week: 2170 Day: 0 MJD: 59434
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1133 53 40 33 48 62 26 --- 20 | 27 38 34 64 81 41 --- 38
R02E | 1032 10 17 15 17 13 16 177 6 | 39 45 44 37 44 41 44 39
R03E | 1713 8 26 11 9 10 13 163 6 | 29 30 27 26 36 27 42 27
XR04E | 2270 11 27 12 --- 12 25 --- 9 | 42 45 44 --- 51 41 --- 43
R05E | 2230 11 30 14 14 12 27 126 8 | 60 60 63 57 63 54 83 58
R07E | 857 11 26 12 16 14 21 203 7 | 29 36 28 33 30 31 97 28
R08E | 2298 10 26 15 14 15 21 --- 7 | 50 51 52 57 50 51 --- 51
R09 | 2126 11 25 12 10 30 38 --- 9 | 50 47 48 49 29 66 --- 46
XR11 | 909 11 --- 16 15 --- 31 --- 10 | 24 --- 24 21 --- 37 --- 20
R12 | 562 11 14 16 8 18 28 --- 7 | 84 81 75 76 79 78 --- 78
R13 | 2555 33 27 30 35 54 32 --- 16 | 67 60 52 65 48 44 --- 53
R14 | 562 10 14 15 13 13 24 --- 6 | 40 38 39 41 41 44 --- 38
R15 | 774 18 19 15 9 17 14 206 7 | 52 53 40 49 43 46 69 46
R16 | 1397 35 24 17 32 51 38 --- 15 | 42 48 42 50 47 45 --- 41
R17 | 799 12 24 14 15 19 18 --- 7 | 72 60 63 69 57 62 --- 63
R18 | 2239 8 21 27 12 12 28 --- 8 | 49 40 63 49 46 45 --- 48
R19 | 2802 51 117 76 54 57 43 --- 30 | 112 47 49 115 90 114 --- 86
R20 | 1302 62 76 50 29 45 44 --- 22 | 105 52 54 92 72 80 --- 74
R21 | 1123 13 27 9 12 22 17 89 7 | 64 43 51 58 58 62 97 56
R22 | 1698 34 17 57 23 42 39 --- 17 | 53 51 90 55 67 61 --- 56
R24 | 686 21 55 14 7 11 42 --- 12 | 70 42 65 59 62 61 --- 59
------+----------------------------------------------+------------------------------------------
RMS | 1627 28 41 30 24 32 30 166 |T 55 48 49 56 54 53 72 49
WRMS | 1627 23 27 24 14 21 27 166 |NE 63 50 53 60 56 60 83 54
MEDI | 1302 11 26 15 14 17 27 163 |MD 50 47 49 55 50 46 69 48
Table 3.2170.1 GPS week: 2170 Day: 1 MJD: 59435
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1161 45 27 54 59 31 45 --- 20 | 37 45 53 96 53 65 --- 50
R02E | 1096 14 17 22 24 17 17 294 8 | 37 34 42 38 43 39 68 36
R03E | 1541 14 26 13 13 14 18 165 7 | 27 27 29 30 35 33 53 27
XR04E | 2277 12 25 18 --- 13 33 --- 10 | 25 28 31 --- 36 27 --- 25
R05E | 3264 19 27 22 19 15 31 108 9 | 34 36 43 37 39 38 79 34
R07E | 540 9 29 10 14 9 37 233 8 | 28 28 28 29 32 40 152 27
R08E | 1649 13 26 14 14 11 21 --- 7 | 32 36 27 29 32 39 --- 29
R09 | 1842 14 24 13 8 32 45 --- 10 | 56 56 49 55 30 71 --- 48
XR11 | 1139 11 --- 20 12 --- 26 --- 10 | 26 --- 30 28 --- 32 --- 24
R12 | 1175 15 12 21 19 15 26 --- 8 | 71 68 69 75 58 71 --- 67
R13 | 4583 29 22 27 22 41 27 --- 13 | 46 39 29 40 35 40 --- 31
R14 | 791 12 14 9 18 10 35 --- 7 | 31 29 41 42 37 35 --- 33
R15 | 896 9 13 19 15 18 17 231 7 | 33 31 29 36 35 31 115 30
R16 | 849 20 26 22 14 42 46 --- 13 | 26 48 28 32 29 28 --- 25
R17 | 678 15 20 10 13 12 27 --- 7 | 41 37 44 39 39 34 --- 37
R18 | 1382 8 22 29 18 17 34 --- 9 | 31 27 35 36 34 28 --- 28
R19 | 2988 63 117 63 41 52 57 --- 30 | 67 35 32 56 50 81 --- 47
R20 | 848 50 65 62 53 53 36 --- 24 | 66 50 44 75 52 72 --- 53
R21 | 569 12 29 13 13 14 32 87 8 | 37 32 35 38 38 53 60 35
R22 | 1521 35 15 68 23 50 46 --- 19 | 37 28 47 51 52 56 --- 36
R24 | 858 26 40 20 12 20 40 --- 11 | 47 32 39 34 39 54 --- 37
------+----------------------------------------------+------------------------------------------
RMS | 1805 27 38 33 26 29 35 200 |T 39 37 38 44 39 46 87 36
WRMS | 1805 22 24 29 18 20 32 200 |NE 43 39 39 45 40 49 87 37
MEDI | 1161 14 25 20 15 17 33 165 |MD 37 34 35 38 37 39 68 34
Table 3.2170.2 GPS week: 2170 Day: 2 MJD: 59436
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 811 47 38 22 30 49 37 --- 17 | 29 51 42 56 71 37 --- 40
R02E | 775 13 15 24 23 26 16 191 9 | 41 42 43 46 53 44 114 41
R03E | 840 15 25 25 13 14 17 118 8 | 23 26 31 23 29 25 43 22
XR04E | 1680 18 28 11 --- 16 35 --- 11 | 36 39 31 --- 33 40 --- 30
R05E | 2448 12 24 36 22 26 30 102 11 | 48 53 65 54 53 50 68 50
R07E | 1709 17 24 14 18 21 33 68 9 | 26 30 30 36 38 31 80 29
R08E | 1772 14 14 16 11 11 17 --- 6 | 35 34 37 39 39 44 --- 36
R09 | 935 16 30 13 12 39 30 --- 10 | 45 43 43 46 24 50 --- 38
XR11 | 910 20 --- 13 13 --- 19 --- 9 | 14 --- 31 27 --- 25 --- 21
R12 | 1156 16 17 12 12 11 15 --- 6 | 92 89 96 96 95 86 --- 92
R13 | 3221 34 35 22 33 61 18 --- 16 | 54 63 41 35 41 47 --- 41
R14 | 1174 12 13 8 15 16 24 --- 6 | 36 32 39 33 37 50 --- 34
R15 | 1331 11 12 13 10 11 17 89 5 | 41 38 36 38 41 37 100 37
R16 | 1384 32 11 19 18 48 37 --- 13 | 34 55 36 31 45 36 --- 33
R17 | 582 18 25 12 9 21 28 --- 8 | 60 46 46 46 52 49 --- 47
R18 | 874 11 20 23 7 16 31 --- 8 | 40 33 46 39 37 45 --- 38
R19 | 1027 60 108 65 34 60 30 --- 27 | 73 34 35 69 72 64 --- 56
R20 | 1204 57 59 49 40 59 37 --- 22 | 59 61 40 53 48 57 --- 45
R21 | 755 10 30 17 11 14 34 159 9 | 47 37 42 46 54 65 128 46
R22 | 1374 36 28 81 31 38 28 --- 19 | 38 47 76 42 43 35 --- 38
R24 | 1127 25 36 11 8 9 11 --- 8 | 46 48 40 42 40 38 --- 40
------+----------------------------------------------+------------------------------------------
RMS | 1433 28 37 32 21 34 27 128 |T 43 45 44 44 47 45 88 40
WRMS | 1433 23 25 28 16 25 24 128 |NE 48 48 46 45 48 48 114 43
MEDI | 1156 17 25 17 13 21 28 102 |MD 41 42 40 42 41 44 80 38
Table 3.2170.3 GPS week: 2170 Day: 3 MJD: 59437
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 958 32 44 34 37 36 40 --- 16 | 29 38 57 58 47 54 --- 37
R02E | 1094 15 26 24 19 15 26 141 9 | 60 54 54 61 64 63 107 57
R03E | 665 10 28 14 10 16 20 101 7 | 27 34 29 28 34 34 61 27
XR04E | 2189 14 27 16 --- 20 31 --- 11 | 25 29 30 --- 28 38 --- 25
R05E | 1956 13 20 21 22 17 25 112 9 | 74 75 89 85 83 63 52 77
R07E | 1355 11 19 16 13 23 16 88 7 | 37 39 42 39 39 38 87 37
R08E | 1623 9 17 16 17 16 25 --- 7 | 34 36 37 40 36 45 --- 35
R09 | 1630 18 34 9 21 40 48 --- 13 | 37 46 28 34 31 46 --- 29
XR11 | 1790 31 --- 20 12 --- 37 --- 15 | 20 --- 33 21 --- 38 --- 20
R12 | 1159 15 35 26 14 15 28 --- 10 | 54 64 42 47 45 61 --- 49
R13 | 2139 23 31 18 19 40 32 --- 12 | 48 59 49 58 50 46 --- 48
R14 | 938 6 13 11 14 19 15 --- 6 | 29 31 26 38 24 33 --- 28
R15 | 1303 12 11 38 10 14 26 88 9 | 46 43 29 48 41 60 46 42
R16 | 1125 37 49 21 26 52 20 --- 15 | 32 37 27 36 44 46 --- 31
R17 | 623 14 28 17 20 18 13 --- 8 | 57 38 44 55 52 45 --- 48
R18 | 1283 15 22 25 17 21 27 --- 9 | 44 28 48 36 44 40 --- 37
R19 | 786 55 99 53 19 74 26 --- 25 | 78 38 40 58 74 73 --- 56
R20 | 1103 41 51 50 32 41 47 --- 19 | 77 67 41 76 62 59 --- 59
R21 | 917 17 23 12 20 15 18 126 8 | 52 39 40 38 50 56 104 43
R22 |33774 29 31 107 50 44 30 --- 24 | 35 36 75 56 45 44 --- 33
R24 | 1630 14 49 14 19 28 14 --- 10 | 46 29 48 51 59 43 --- 43
------+----------------------------------------------+------------------------------------------
RMS | 7851 24 38 36 23 33 28 111 |T 44 43 43 48 47 48 76 41
WRMS | 7851 24 30 35 18 24 28 111 |NE 46 42 40 46 47 49 75 40
MEDI | 1283 15 28 20 19 20 26 101 |MD 44 38 41 47 45 46 61 37
Table 3.2170.4 GPS week: 2170 Day: 4 MJD: 59438
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 976 45 50 37 44 29 34 --- 18 | 43 50 77 76 65 48 --- 54
R02E | 1230 12 20 16 13 14 17 112 6 | 74 80 84 86 76 74 85 79
R03E | 770 11 26 15 15 14 16 108 7 | 30 38 35 38 32 39 37 32
XR04E | 1826 10 25 14 --- 18 26 --- 9 | 47 50 44 --- 50 41 --- 44
R05E | 1026 12 26 16 9 18 31 99 8 | 62 64 58 61 62 63 63 59
R07E | 986 12 27 13 11 12 15 86 6 | 38 35 39 39 38 43 106 36
R08E | 682 12 25 15 19 12 24 --- 8 | 34 35 39 43 40 39 --- 36
R09 | 1949 16 16 14 20 38 34 --- 10 | 36 37 38 41 34 46 --- 33
XR11 | 3176 23 --- 14 13 --- 20 --- 10 | 29 --- 43 37 --- 39 --- 33
R12 | 1219 12 25 14 20 36 33 --- 10 | 81 94 88 85 91 93 --- 84
R13 | 1658 39 17 31 31 48 33 --- 15 | 47 52 47 55 45 53 --- 46
R14 | 737 9 15 12 26 14 36 --- 9 | 36 46 43 44 40 62 --- 41
R15 | 878 9 15 18 11 24 35 139 8 | 47 53 46 52 44 61 46 48
R16 | 720 25 51 16 14 49 26 --- 13 | 40 59 40 48 67 38 --- 43
R17 | 667 14 26 12 12 14 24 --- 7 | 66 53 64 59 59 40 --- 56
R18 | 1556 9 18 24 11 18 35 --- 8 | 52 39 56 46 50 39 --- 45
R19 | 836 44 90 51 26 62 27 --- 22 | 64 37 48 59 52 61 --- 48
R20 | 926 40 45 47 33 58 29 --- 19 | 75 45 57 65 55 53 --- 56
R21 | 683 10 27 17 23 14 34 156 9 | 58 46 52 59 53 66 93 53
R22 | 853 43 91 100 29 57 58 --- 28 | 52 85 76 47 47 54 --- 43
R24 | 1835 9 40 13 13 13 25 --- 8 | 50 45 54 56 57 61 --- 51
------+----------------------------------------------+------------------------------------------
RMS | 1133 24 41 33 22 34 31 119 |T 50 52 53 54 52 53 71 48
WRMS | 1133 23 36 29 16 27 29 119 |NE 52 53 53 53 53 54 69 48
MEDI | 976 12 26 16 15 18 29 108 |MD 47 46 48 52 50 53 63 46
Table 3.2170.5 GPS week: 2170 Day: 5 MJD: 59439
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1216 47 49 55 48 28 46 --- 21 | 33 37 76 74 45 35 --- 41
R02E | 1406 24 17 15 15 16 22 128 8 | 92 83 89 84 92 73 180 84
R03E | 1329 10 25 14 11 10 15 98 6 | 26 25 22 26 31 32 50 24
XR04E | 837 9 19 17 --- 16 18 --- 8 | 25 28 36 --- 35 30 --- 28
R05E | 1258 15 28 13 13 12 25 92 8 | 84 82 86 88 85 95 77 85
R07E | 782 11 20 15 12 15 16 265 6 | 26 23 27 25 30 19 195 22
R08E | 925 11 25 20 7 13 23 --- 7 | 43 53 44 46 51 43 --- 44
R09 | 1886 23 13 14 10 21 30 --- 8 | 41 41 46 43 30 62 --- 40
XR11 | 4084 15 --- 21 12 --- 34 --- 12 | 30 --- 45 32 --- 40 --- 32
R12 | 866 15 21 29 14 19 21 --- 8 | 37 38 42 52 45 52 --- 41
R13 | 1439 29 30 32 25 62 44 --- 16 | 32 39 35 36 35 48 --- 31
R14 | 811 11 15 13 9 17 38 --- 8 | 26 28 30 29 33 32 --- 24
R15 | 794 13 21 10 16 22 26 190 8 | 35 41 40 40 31 39 95 35
R16 | 785 18 35 30 11 53 21 --- 12 | 35 43 47 34 37 42 --- 34
R17 | 980 8 28 20 17 13 11 --- 7 | 40 30 36 48 41 38 --- 38
R18 | 1405 15 26 22 10 29 20 --- 8 | 37 25 36 32 41 34 --- 30
R19 | 958 38 95 53 38 51 36 --- 23 | 29 27 35 45 36 47 --- 31
R20 | 871 42 56 35 49 60 22 --- 20 | 40 39 51 50 49 41 --- 38
R21 | 642 14 25 8 13 14 33 282 8 | 38 33 36 34 39 37 306 32
R22 | 1650 31 51 79 22 60 54 --- 22 | 34 41 43 45 46 42 --- 30
R24 | 1597 11 31 12 13 15 19 --- 7 | 32 28 33 36 35 40 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1189 23 37 31 22 33 30 192 |T 38 39 44 44 43 43 150 37
WRMS | 1189 20 29 21 13 24 25 192 |NE 34 34 39 39 38 42 200 33
MEDI | 980 15 25 20 13 17 23 128 |MD 35 37 40 40 37 40 95 32
Table 3.2170.6 GPS week: 2170 Day: 6 MJD: 59440
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01E | 1161 52 55 48 41 28 41 --- 20 | 39 32 71 68 42 34 --- 40
R02E | 1433 25 22 23 9 16 14 217 8 | 84 95 108 98 88 93 194 94
R03E | 1200 12 27 13 13 15 17 125 7 | 28 22 31 33 38 28 87 28
XR04E | 838 11 17 14 --- 12 14 --- 7 | 32 31 37 --- 35 36 --- 32
R05E | 1418 14 21 15 12 18 20 151 7 | 85 85 98 94 100 87 102 91
R07E | 895 12 26 10 9 13 18 293 6 | 43 35 40 45 48 33 223 40
R08E | 2403 9 23 14 7 12 19 --- 6 | 55 55 52 57 57 54 --- 54
R09 | 1532 11 12 10 11 28 18 --- 6 | 44 47 45 51 40 57 --- 45
XR11 | 4346 16 --- 16 16 --- 32 --- 11 | 38 --- 35 37 --- 43 --- 33
R12 | 901 14 26 14 13 24 26 --- 8 | 66 69 63 65 69 55 --- 63
R13 | 3725 24 15 27 18 46 30 --- 12 | 53 60 55 63 45 63 --- 54
R14 | 664 9 15 13 7 20 26 --- 6 | 44 48 52 45 54 45 --- 45
R15 | 742 14 18 11 15 15 21 169 7 | 56 61 52 50 54 51 233 52
R16 | 1231 16 19 17 15 65 66 --- 16 | 50 62 62 53 62 44 --- 51
R17 | 860 18 22 7 8 19 17 --- 6 | 75 53 63 73 66 58 --- 65
R18 | 1054 21 17 28 11 17 18 --- 8 | 54 42 68 55 53 42 --- 51
R19 | 1971 49 97 53 28 46 25 --- 22 | 93 37 48 87 79 86 --- 69
R20 | 900 44 65 39 27 52 37 --- 19 | 95 59 66 88 80 81 --- 76
R21 | 690 13 24 13 10 18 25 412 7 | 71 56 61 70 68 70 271 65
R22 | 2758 48 51 60 17 72 29 --- 20 | 54 73 99 62 52 74 --- 59
R24 | 1370 18 31 12 13 18 16 --- 7 | 65 46 63 64 64 63 --- 60
------+----------------------------------------------+------------------------------------------
RMS | 1614 26 37 27 17 34 28 248 |T 58 53 60 62 59 57 185 55
WRMS | 1614 23 28 20 10 27 22 248 |NE 61 54 59 61 60 59 252 56
MEDI | 1200 16 22 14 13 18 21 169 |MD 54 53 61 62 54 55 194 54
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