[IGSREPORT-28166] Wk 2172 IGLOS Final Orbits
acc
acc at igs.org
Fri Sep 10 04:32:05 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2172 (Aug 22, 2021 - Aug 28, 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 2.2172.
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:
igl2172[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2172 in the SP3 format.
igl21727.sum Combination Report for GPS Week 2172.
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 | -0.5 ns
1 | -2.4 ns
2 | 1.3 ns
3 | -0.1 ns
4 | -0.8 ns
5 | 1.6 ns
6 | -1.3 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 1.2172, 1a.2172).
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 2.2172.0-6)
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 3.2172.0-6).
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 2172 summary. (Aug 22, 2021 - Aug 28, 2021)
Table 1.2172.a GPS week : 2172 MJD: 59448.0-59454.0
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 -4 -12 -7 -41 .10 31 24 | 14248 -464 3329 8131
| 1 1 2 15 18 10 .05 | 833 2293
emx n/a| 0 1 15 -1 -22 -11 -.04 41 30 | -3115 -634 3407 8689
| 1 1 3 19 39 45 .10 | 4364 1601
esx n/a| 0 1 0 19 14 11 -.11 30 23 | -3925 476 3325 7307
| 1 1 1 23 12 29 .03 | 2601 2522
gfz n/a| 0 1 -2 -12 -8 -4 -.11 23 15 | 0 -221 3353 7972
| 0 1 1 11 13 22 .04 | 0 2434
grg n/a| 3 -1 0 -4 21 -112 .40 29 24 | -580 -97 3419 7770
| 1 1 3 29 13 37 .09 | 642 2639
iac n/a| -1 -1 -2 -2 -6 220 -.27 29 27 | 1695 -694 3330 8585
| 1 2 3 29 38 69 .05 | 1573 1431
mcc n/a| 0 -3 -1 19 -22 -441 -.93 204 204 | --- --- --- ---
| 8 16 15 138 66 803 .50 | --- ---
Table 1.2172.b GPS week : 2172 MJD: 59448.0-59454.0
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 | 26 17 19 17 18 21 21 |
R02 | 9 11 10 9 9 9 9 |
R03 | 8 11 9 13 9 9 8 |
R04 | 11 12 12 10 10 10 10 |
R05 | 11 8 9 10 9 12 10 |
R07 | 10 9 8 9 10 10 9 |
R08 | 8 9 11 9 9 8 10 |
R09 | 6 9 11 11 8 8 8 |
R11 | 12 9 13 14 14 10 12 |
R12 | 9 7 7 8 9 9 10 |
R13 | 14 15 15 13 11 18 17 |
R14 | 8 6 7 6 9 8 7 |
R15 | 9 8 8 7 7 6 7 |
R16 | 14 16 18 15 13 19 16 |
R17 | 9 6 9 8 10 8 7 |
R18 | 9 7 9 10 11 8 9 |
R19 | 23 28 28 27 24 26 20 |
R20 | 23 22 24 24 23 20 23 |
R21 | 9 9 9 8 7 8 10 |
R22 | 22 19 22 21 23 25 22 |
R24 | 10 14 10 9 8 9 10 |
Table 1.2172.c GPS week : 2172 MJD: 59448.0-59454.0
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 2172 0 | -62 -83 86 195 724 3323 82.2 1257 1257 | -492 0
brd 2172 1 | -53 -106 127 2143 304 714 82.5 1484 1484 | -2427 0
brd 2172 2 | 20 -26 191 1186 -410 -3767 81.2 1304 1304 | 1322 0
brd 2172 3 | -26 -32 73 2932 -1130 -5028 83.0 1222 1222 | -51 0
brd 2172 4 | -26 2 156 988 256 -5028 83.7 1200 1200 | -814 0
brd 2172 5 | -20 -12 82 -80 239 -253 82.9 1266 1266 | 1575 0
brd 2172 6 | -93 2 138 -830 -1171 1320 81.5 1487 1487 | -1311 0
-------------+------------------------------------------------------------+----------------
brd 2172 mean| -37 -36 122 933 -169 -1245 82.4 1317 1317 | -314 0
brd 2172 sdev| 36 42 43 1304 747 3347 .9 119 119 | 1417 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 2.2172.0 GPS week: 2172 Day: 0 MJD: 59448
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 -6 -6 -33 -49 .11 28 22 | 13712 -436 3122 7197
emx n/a| 1 2 10 -39 -19 40 -.18 39 27 | -9035 -433 3188 7643
esx n/a| 0 0 0 27 37 -27 -.12 30 21 | -7447 807 3111 6803
gfz n/a| -1 1 -3 -24 7 7 -.14 22 16 | 0 773 3064 7009
grg n/a| 3 -3 1 35 6 -135 .43 25 18 | -829 396 3313 6929
iac n/a| -2 2 2 -57 -73 277 -.33 33 25 | 2135 -595 3102 7580
mcc n/a| -4 -37 16 -45 25 -1731 -.77 241 241 | --- --- --- ---
Table 2.2172.1 GPS week: 2172 Day: 1 MJD: 59449
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 -3 -9 -33 -48 .03 32 25 | 13743 -4007 3362 7492
emx n/a| 0 0 13 3 23 -31 -.14 44 32 | -9643 -2319 3460 8002
esx n/a| 0 1 0 -7 9 0 -.14 27 23 | -4029 -3807 3360 6786
gfz n/a| 1 1 -3 -3 -18 -50 -.12 22 13 | 0 -4585 3350 7119
grg n/a| 3 -1 5 14 24 -56 .52 32 23 | -877 -4033 3483 7109
iac n/a| -3 -3 -2 -25 35 288 -.21 32 30 | 532 -2763 3351 7894
mcc n/a| 8 -14 -10 21 -98 183 -1.80 142 142 | --- --- --- ---
Table 2.2172.2 GPS week: 2172 Day: 2 MJD: 59450
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| -3 -1 -5 -15 9 -20 .06 35 25 | 13227 1549 3229 8355
emx n/a| 0 1 13 21 -22 -94 .02 41 31 | 398 741 3328 9002
esx n/a| 0 0 0 3 0 3 -.13 27 22 | -4314 2598 3238 6210
gfz n/a| 0 2 -4 -21 6 10 -.12 27 17 | 0 2450 3331 7962
grg n/a| 2 -2 1 9 15 -69 .38 30 24 | -200 2427 3287 7756
iac n/a| 0 -1 0 4 -21 207 -.28 30 30 | 1808 1537 3266 8957
mcc n/a| -6 2 -13 -50 19 -1041 -1.46 221 221 | --- --- --- ---
Table 2.2172.3 GPS week: 2172 Day: 3 MJD: 59451
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 -7 -24 3 -45 .18 33 25 | 15601 -328 3410 8355
emx n/a| 1 0 15 7 6 9 .01 39 27 | -745 -1292 3479 8932
esx n/a| 1 2 -1 -8 8 30 -.07 30 24 | -1293 86 3402 8037
gfz n/a| 0 -2 0 -3 -6 0 -.08 23 14 | 0 -774 3477 8209
grg n/a| 1 0 0 -31 27 -140 .23 27 24 | 148 -727 3486 7883
iac n/a| -1 0 -5 24 -35 212 -.27 29 29 | 3177 -2204 3389 8835
mcc n/a| 14 7 -12 302 -77 -1004 -.49 200 200 | --- --- --- ---
Table 2.2172.4 GPS week: 2172 Day: 4 MJD: 59452
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| -3 0 -1 -22 -4 -42 .16 26 21 | 13888 -2233 3170 8956
emx n/a| 0 1 19 -2 5 34 -.09 42 31 | -1359 -2635 3247 9490
esx n/a| -1 1 1 24 15 61 -.10 32 25 | -501 -969 3150 7597
gfz n/a| 0 1 -2 3 -24 15 -.12 26 15 | 0 -1058 3162 8868
grg n/a| 7 -4 -4 11 3 -130 .38 30 29 | 3 -1957 3198 8286
iac n/a| 0 -1 -3 8 13 105 -.20 23 25 | 399 108 3161 9353
mcc n/a| 0 5 4 -34 -102 309 -.47 364 364 | --- --- --- ---
Table 2.2172.5 GPS week: 2172 Day: 5 MJD: 59453
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 -3 -28 2 -34 .09 29 25 | 14632 2959 3202 7837
emx n/a| -2 0 19 8 -79 -18 .01 43 34 | -2127 1834 3227 8355
esx n/a| -1 0 -1 44 23 -10 -.09 36 25 | -6858 4078 3193 8791
gfz n/a| 0 1 -2 -25 -4 -19 -.14 22 14 | 0 2437 3217 7994
grg n/a| 4 0 -3 -20 39 -154 .46 31 26 | -583 3847 3270 7645
iac n/a| -1 -3 -2 20 13 285 -.29 30 23 | 4067 -455 3215 8271
mcc n/a| -1 8 -18 67 45 121 -.79 108 108 | --- --- --- ---
Table 2.2172.6 GPS week: 2172 Day: 6 MJD: 59454
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 -2 18 5 -50 .09 34 26 | 14936 -754 3813 8728
emx n/a| 1 1 18 -7 -71 -18 .10 39 31 | 706 -334 3926 9403
esx n/a| -1 3 1 48 2 24 -.14 31 23 | -3037 539 3826 6927
gfz n/a| 0 1 -2 -11 -21 1 -.02 22 14 | 0 -792 3874 8643
grg n/a| 2 0 -3 -48 31 -97 .37 28 21 | -1726 -633 3898 8786
iac n/a| 0 -5 -7 7 20 165 -.34 27 27 | -252 -489 3830 9209
mcc n/a| -7 0 20 -125 30 73 -.76 151 151 | --- --- --- ---
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 3.2172.0 GPS week: 2172 Day: 0 MJD: 59448
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
XR01E | 1041 58 58 54 43 --- 52 --- 26 | 129 139 136 130 --- 131 --- 130
R02E | 2879 9 29 18 21 17 24 152 9 | 108 111 105 108 111 120 153 109
R03E | 1167 12 31 13 14 12 19 --- 7 | 109 110 106 108 111 121 --- 109
XR04E | 1203 15 27 19 --- 17 28 --- 10 | 94 92 96 --- 96 94 --- 93
XR05E | 2478 23 31 14 14 --- 30 222 11 | 80 76 66 65 --- 71 161 70
R07E | 656 15 27 20 22 17 34 371 10 | 100 102 86 93 99 97 321 94
R08E | 1422 16 27 16 20 16 11 --- 8 | 132 128 136 136 136 139 --- 134
R09 | 1089 13 12 13 13 9 21 --- 6 | 24 24 26 28 28 25 --- 24
XR11 | 1270 19 --- 21 11 --- 31 --- 11 | 14 --- 42 30 --- 34 --- 22
R12 | 620 19 16 17 24 16 18 --- 8 | 27 23 46 41 35 21 --- 29
R13 | 899 28 25 38 26 31 37 --- 14 | 26 39 33 17 21 25 --- 19
XR14 | 574 11 28 11 15 --- 16 --- 8 | 19 17 24 34 --- 24 --- 20
R15 | 940 16 26 14 13 19 26 164 8 | 15 21 19 24 24 27 102 16
R16 | 1224 21 24 10 17 45 50 --- 13 | 24 38 31 38 21 28 --- 23
R17 | 1384 13 23 13 10 17 36 --- 8 | 69 50 58 58 56 68 --- 58
R18 | 792 17 23 28 18 13 24 --- 9 | 42 37 66 36 54 57 --- 47
R19 | 703 54 99 52 29 28 39 --- 23 | 106 34 32 82 69 79 --- 61
R20 | 914 61 68 39 47 44 49 --- 22 | 85 32 44 84 51 62 --- 56
R21 | 1084 23 20 13 14 17 28 211 8 | 69 45 55 56 64 54 167 56
R22 | 1395 49 34 74 28 44 50 --- 21 | 59 78 129 79 59 68 --- 75
R24 | 1188 19 42 18 16 15 30 --- 10 | 68 41 63 62 62 35 --- 55
------+----------------------------------------------+------------------------------------------
RMS | 1257 28 39 30 22 25 33 241 |T 66 61 66 65 64 65 180 61
WRMS | 1257 22 27 21 16 18 25 241 |NE 46 36 47 47 45 43 134 40
MEDI | 1089 19 27 18 17 17 30 211 |MD 69 41 58 58 59 62 161 56
Table 3.2172.1 GPS week: 2172 Day: 1 MJD: 59449
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 | 888 47 52 33 32 25 38 --- 16 | 191 178 158 177 167 161 --- 172
R02E | 3810 18 25 10 15 23 44 152 10 | 79 81 86 91 82 84 114 84
R03E | 1015 18 33 20 21 18 31 --- 10 | 108 103 113 114 105 92 --- 106
XR04E | 1368 14 27 10 --- 21 42 --- 12 | 89 90 85 --- 96 94 --- 90
R05E | 2166 22 27 15 12 20 12 148 8 | 79 72 82 75 85 76 79 76
R07E | 1339 19 32 12 16 18 19 --- 8 | 64 60 60 70 68 65 --- 63
R08E | 911 12 34 11 18 19 18 --- 8 | 103 104 102 105 108 104 --- 103
R09 | 1428 15 23 14 21 17 26 --- 8 | 30 32 34 42 27 26 --- 31
XR11 | 2184 18 --- 12 7 --- 25 --- 9 | 20 --- 37 27 --- 41 --- 29
R12 | 743 15 16 10 6 18 22 --- 6 | 34 38 46 44 37 37 --- 38
R13 | 1602 41 21 28 24 49 31 --- 15 | 32 22 30 24 27 37 --- 24
XR14 | 568 12 13 12 7 --- 19 --- 6 | 22 21 30 34 --- 36 --- 28
R15 | 678 21 20 22 7 13 27 113 8 | 21 27 30 30 26 29 76 25
R16 | 1124 29 51 12 27 67 13 --- 16 | 22 27 28 32 38 48 --- 27
R17 | 917 16 24 9 8 11 19 --- 6 | 46 34 38 41 41 36 --- 38
R18 | 902 12 25 20 9 11 16 --- 7 | 35 34 43 37 43 40 --- 37
R19 | 1479 61 118 58 48 42 50 --- 27 | 76 30 41 80 44 86 --- 53
R20 | 806 67 72 46 33 47 35 --- 22 | 69 29 34 57 40 52 --- 42
R21 | 624 25 22 11 10 13 36 151 9 | 44 41 37 33 49 40 28 36
R22 | 1436 37 44 56 23 53 41 --- 19 | 57 43 84 58 52 65 --- 55
R24 | 1456 31 35 18 8 33 55 --- 13 | 45 36 36 29 51 35 --- 30
------+----------------------------------------------+------------------------------------------
RMS | 1483 32 44 27 22 32 32 142 |T 60 55 58 60 62 61 74 56
WRMS | 1483 25 32 23 13 23 30 142 |NE 39 31 39 40 39 43 52 35
MEDI | 1124 19 27 14 15 20 27 148 |MD 46 36 41 42 49 48 76 38
Table 3.2172.2 GPS week: 2172 Day: 2 MJD: 59450
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 | 556 62 59 33 45 27 25 --- 19 | 250 244 255 250 222 264 --- 252
R02E | 2703 15 25 13 25 19 26 165 9 | 138 139 132 135 141 141 122 136
R03E | 825 14 32 14 22 18 20 365 9 | 114 109 111 113 114 122 187 112
XR04E | 1382 19 28 16 --- 18 34 --- 11 | 100 99 102 --- 105 96 --- 99
R05E | 1185 20 31 15 14 21 12 239 8 | 91 91 98 96 83 95 101 92
R07E | 927 14 28 9 17 18 16 --- 7 | 63 56 54 59 60 65 --- 57
R08E | 1033 22 27 16 17 25 37 --- 11 | 138 139 140 146 149 161 --- 145
R09 | 1103 17 28 11 10 20 49 --- 11 | 13 22 24 20 28 43 --- 18
XR11 | 2510 17 --- 24 13 --- 33 --- 13 | 20 --- 39 33 --- 32 --- 26
R12 | 1005 10 13 9 17 11 23 --- 6 | 30 29 28 38 34 28 --- 28
R13 | 1654 39 21 23 30 54 21 --- 15 | 26 25 34 30 14 16 --- 18
R14 | 894 13 15 9 13 12 22 --- 6 | 15 20 27 27 18 24 --- 17
R15 | 1106 17 13 24 11 12 23 115 8 | 16 18 19 15 17 27 47 15
R16 | 1230 49 46 13 33 54 37 --- 17 | 23 31 18 32 20 27 --- 20
R17 | 947 24 20 13 9 16 37 --- 9 | 52 34 47 42 52 39 --- 40
R18 | 821 13 31 29 14 10 11 --- 9 | 36 27 51 36 44 35 --- 37
R19 | 2306 74 110 60 47 45 24 --- 27 | 97 30 26 73 64 50 --- 48
R20 | 894 60 66 48 56 50 34 --- 23 | 73 44 26 76 38 58 --- 43
R21 | 983 20 29 11 20 12 22 118 8 | 59 46 50 63 55 41 25 51
R22 | 1686 46 34 59 40 49 57 --- 22 | 52 43 85 64 61 94 --- 63
R24 | 804 18 26 17 10 18 37 --- 9 | 51 42 50 48 54 27 --- 43
------+----------------------------------------------+------------------------------------------
RMS | 1303 35 41 27 27 30 30 221 |T 69 64 67 69 68 70 96 64
WRMS | 1303 25 31 22 17 24 30 221 |NE 40 31 37 42 38 38 36 33
MEDI | 1033 19 28 16 17 18 25 165 |MD 52 42 50 48 54 43 101 43
Table 3.2172.3 GPS week: 2172 Day: 3 MJD: 59451
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 | 1198 54 51 42 34 22 21 --- 17 | 103 95 75 97 85 90 --- 87
R02E | 1389 11 34 11 14 14 28 224 8 | 98 106 102 100 102 108 130 101
R03E | 719 26 34 20 16 22 47 283 12 | 122 108 121 113 124 94 221 111
XR04E | 1296 18 29 13 --- 14 18 --- 9 | 111 118 118 --- 120 118 --- 116
R05E | 1130 19 33 22 12 21 20 202 9 | 133 119 126 132 128 125 177 127
R07E | 1974 18 32 17 17 13 20 --- 8 | 56 52 44 52 52 51 --- 48
R08E | 1053 11 25 11 13 20 31 --- 8 | 132 136 133 134 143 120 --- 133
R09 | 1243 19 34 7 15 18 39 --- 10 | 21 32 22 28 18 34 --- 21
XR11 | 2404 28 --- 18 18 --- 35 --- 14 | 17 --- 38 35 --- 40 --- 28
R12 | 1065 15 12 18 17 11 26 --- 7 | 53 63 67 67 55 49 --- 58
R13 | 1157 37 20 16 14 39 36 --- 12 | 22 20 25 16 17 23 --- 16
R14 | 1096 16 18 11 14 9 16 --- 6 | 16 16 26 26 19 29 --- 20
R15 | 1416 11 12 19 13 15 24 119 7 | 18 19 21 22 23 23 64 18
R16 | 797 37 30 25 19 41 39 --- 14 | 20 43 28 26 25 40 --- 23
R17 | 804 19 24 9 11 16 29 --- 8 | 58 38 48 46 51 44 --- 45
R18 | 831 12 18 30 12 22 32 --- 10 | 46 27 56 41 45 30 --- 38
R19 | 2358 70 105 64 40 43 22 --- 26 | 100 36 29 76 74 61 --- 56
R20 | 862 55 64 43 55 64 22 --- 23 | 75 36 36 76 47 62 --- 51
R21 | 596 14 25 17 13 20 21 119 8 | 62 42 51 58 54 67 45 54
R22 | 1131 60 27 72 38 25 32 --- 20 | 42 49 107 51 61 77 --- 59
R24 | 1030 20 28 15 18 15 26 --- 9 | 54 36 48 32 51 63 --- 43
------+----------------------------------------------+------------------------------------------
RMS | 1222 33 39 30 23 27 29 200 |T 64 59 62 61 64 64 127 59
WRMS | 1222 25 27 24 14 24 29 200 |NE 43 35 43 42 41 45 54 37
MEDI | 1130 19 28 18 15 20 26 202 |MD 56 42 48 51 52 61 130 51
Table 3.2172.4 GPS week: 2172 Day: 4 MJD: 59452
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 | 1570 41 66 50 34 22 22 --- 17 | 138 129 136 142 99 134 --- 133
R02E | 1250 13 32 14 8 38 16 172 9 | 99 104 106 107 107 107 130 103
R03E | 1212 17 32 15 18 25 17 137 9 | 97 87 94 100 106 89 125 95
XR04E | 1706 13 28 15 --- 26 17 --- 9 | 101 103 94 --- 103 101 --- 98
R05E | 1326 16 28 12 13 30 18 186 9 | 83 82 90 87 105 86 140 87
R07E | 1843 17 41 15 16 16 22 828 9 | 66 54 52 63 66 54 809 57
R08E | 991 13 28 17 15 24 20 --- 8 | 125 127 130 125 127 130 --- 126
R09 | 1337 12 21 15 20 19 20 --- 8 | 18 22 24 26 25 28 --- 21
XR11 | 2695 21 --- 26 19 --- 27 --- 13 | 18 --- 32 25 --- 22 --- 18
R12 | 1057 14 19 12 17 28 22 --- 8 | 54 65 64 68 42 51 --- 56
R13 | 1259 22 20 20 21 39 25 --- 11 | 26 33 35 34 27 22 --- 26
R14 | 862 11 16 10 17 14 37 --- 9 | 19 19 24 30 15 48 --- 22
R15 | 1109 12 7 10 18 16 19 61 6 | 19 19 23 24 20 21 45 17
R16 | 763 27 29 20 24 49 17 --- 12 | 24 26 20 21 21 16 --- 16
R17 | 771 14 33 14 9 23 31 --- 9 | 53 44 45 46 50 64 --- 49
R18 | 1267 12 25 35 8 15 33 --- 10 | 47 40 55 39 45 28 --- 38
R19 | 1076 50 104 54 46 48 19 --- 24 | 82 43 44 83 73 55 --- 58
R20 | 966 44 84 47 54 50 26 --- 22 | 57 45 34 75 44 47 --- 45
R21 | 794 12 29 15 15 16 12 147 7 | 54 45 44 53 55 58 40 51
R22 | 1132 52 23 84 49 35 25 --- 22 | 31 47 85 49 50 46 --- 42
R24 | 1562 17 30 19 16 15 14 --- 8 | 48 39 50 34 49 44 --- 40
------+----------------------------------------------+------------------------------------------
RMS | 1199 26 42 32 26 30 23 364 |T 59 58 61 61 61 59 214 57
WRMS | 1199 21 31 25 15 29 25 364 |NE 39 37 41 43 39 39 42 35
MEDI | 1212 16 28 15 17 24 20 147 |MD 54 45 50 49 50 51 125 49
Table 3.2172.5 GPS week: 2172 Day: 5 MJD: 59453
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 | 1845 60 59 48 45 19 37 --- 20 | 123 109 96 110 83 107 --- 104
R02E | 962 21 26 11 19 24 22 129 9 | 86 78 78 77 80 83 106 78
R03E | 1907 22 26 14 16 22 21 100 9 | 53 50 41 44 55 46 120 45
XR04E | 1203 19 26 17 --- 24 18 --- 10 | 111 116 115 --- 122 112 --- 114
R05E | 1135 22 36 14 26 19 35 103 11 | 99 87 103 99 98 107 105 98
R07E | 1650 24 34 21 14 19 23 97 9 | 54 44 51 51 56 48 114 48
R08E | 1757 11 29 14 9 17 23 --- 7 | 137 145 144 141 141 125 --- 138
R09 | 1376 12 16 14 17 24 17 --- 7 | 14 19 17 25 27 25 --- 17
XR11 | 1374 24 --- 13 15 --- 16 --- 10 | 20 --- 30 28 --- 24 --- 22
R12 | 745 19 30 15 13 16 22 --- 8 | 52 57 46 49 48 39 --- 46
R13 | 1127 37 47 44 8 53 43 --- 17 | 33 41 32 26 21 30 --- 19
R14 | 807 10 15 19 17 20 20 --- 7 | 20 22 27 28 13 30 --- 19
R15 | 1435 13 10 11 13 13 19 72 6 | 17 18 18 22 17 32 79 18
R16 | 927 43 36 26 25 62 47 --- 18 | 29 39 32 32 24 44 --- 25
R17 | 798 12 32 15 10 15 25 --- 8 | 43 42 39 41 45 53 --- 42
R18 | 1016 15 20 22 15 17 19 --- 8 | 35 30 36 27 46 42 --- 33
R19 | 1014 46 100 62 30 69 38 --- 25 | 43 29 56 54 71 39 --- 41
R20 | 1003 39 68 51 40 40 24 --- 19 | 51 46 28 51 48 33 --- 35
R21 | 990 14 33 11 12 11 21 136 7 | 40 27 34 40 44 42 37 37
R22 | 937 43 58 102 30 32 51 --- 25 | 28 52 62 41 34 47 --- 23
R24 | 1578 24 27 14 11 17 23 --- 8 | 34 40 41 35 36 49 --- 36
------+----------------------------------------------+------------------------------------------
RMS | 1265 29 42 36 22 31 30 108 |T 53 54 53 51 55 55 93 49
WRMS | 1265 25 34 25 14 26 23 108 |NE 32 35 35 35 36 37 58 29
MEDI | 1127 22 30 15 15 19 23 100 |MD 43 42 41 41 46 44 105 37
Table 3.2172.6 GPS week: 2172 Day: 6 MJD: 59454
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 | 1710 67 55 51 39 26 36 --- 20 | 131 114 101 112 89 118 --- 110
R02E | 2831 12 33 10 10 16 26 110 8 | 104 103 104 108 110 110 134 106
R03E | 2537 18 29 12 12 16 18 74 7 | 84 72 73 76 80 76 123 75
XR04E | 705 24 25 18 --- 22 14 --- 10 | 107 116 110 --- 117 109 --- 110
R05E | 1819 21 32 14 17 20 23 183 9 | 125 108 127 125 114 122 119 122
R07E | 901 26 35 14 10 15 22 183 9 | 68 54 53 58 65 63 118 58
R08E | 1229 18 34 13 19 14 32 --- 10 | 133 145 137 138 142 142 --- 138
R09 | 1105 16 14 9 15 13 30 --- 8 | 23 30 26 34 29 24 --- 26
XR11 | 1779 20 --- 15 16 --- 28 --- 11 | 25 --- 34 33 --- 32 --- 29
R12 | 1421 15 24 24 16 26 18 --- 9 | 50 48 46 50 42 40 --- 42
R13 | 1952 54 23 31 33 53 26 --- 17 | 35 27 37 49 30 34 --- 31
R14 | 673 13 8 12 16 13 23 --- 7 | 28 28 30 34 19 40 --- 28
R15 | 1428 12 14 21 17 12 15 110 7 | 26 31 24 32 24 34 109 26
R16 | 720 35 31 31 13 55 33 --- 15 | 33 31 30 40 40 37 --- 30
R17 | 675 15 29 11 9 15 15 --- 7 | 74 51 63 66 64 68 --- 64
R18 | 1010 22 22 29 16 19 17 --- 9 | 48 47 73 50 66 56 --- 55
R19 | 1526 41 77 45 24 43 35 --- 19 | 104 47 59 84 80 74 --- 67
R20 | 1687 51 79 42 44 53 37 --- 22 | 90 53 57 90 67 68 --- 66
R21 | 817 15 35 21 14 23 22 201 9 | 75 52 57 70 72 74 59 66
R22 | 853 74 31 78 27 19 43 --- 22 | 56 69 121 74 65 69 --- 70
R24 | 927 21 44 17 16 16 21 --- 10 | 75 61 74 76 70 66 --- 69
------+----------------------------------------------+------------------------------------------
RMS | 1486 34 39 31 22 28 27 151 |T 71 64 68 69 69 69 110 66
WRMS | 1486 26 31 23 14 21 27 151 |NE 53 44 52 55 51 51 84 47
MEDI | 1229 21 31 18 16 19 23 110 |MD 74 52 59 66 66 68 118 66
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