[IGSREPORT-27859] Wk 2150 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 9 01:26:44 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2150 (Mar 21, 2021 - Mar 27, 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 2.2150.
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:
igl2150[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2150 in the SP3 format.
igl21507.sum Combination Report for GPS Week 2150.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://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 | -1.1 ns
2 | 1.8 ns
3 | -1.0 ns
4 | -0.3 ns
5 | 1.7 ns
6 | -0.1 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 1.2150, 1a.2150).
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 2.2150.0-6)
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 3.2150.0-6).
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 2150 summary. (Mar 21, 2021 - Mar 27, 2021)
Table 1.2150.a GPS week : 2150 MJD: 59294.0-59300.0
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 9 6 -1 7 -.01 28 21 | 11998 -79 3397 8196
| 0 1 1 23 15 28 .04 | 1020 1980
emx n/a| 0 0 -10 -16 16 -47 -.01 33 29 | -5295 365 3347 8638
| 2 1 3 18 19 46 .07 | 10416 1124
esx n/a| 0 0 -5 4 -17 -46 -.00 32 27 | 1172 574 3347 7499
| 1 1 2 17 15 33 .06 | 4647 2405
gfz n/a| 0 0 7 -7 -13 -65 -.07 30 17 | 0 -237 3364 7969
| 2 1 2 13 18 28 .06 | 0 2200
grg n/a| 1 -1 -6 8 12 26 .32 31 26 | 306 -332 3358 7838
| 0 2 5 28 10 45 .07 | 518 1389
iac n/a| -1 0 2 3 12 125 -.18 28 26 | 1880 45 3392 8590
| 3 2 4 28 42 50 .05 | 1295 1656
mcc n/a| 1 -2 -5 41 -37 84 -.39 184 184 | --- --- --- ---
| 3 4 18 80 71 265 .34 | --- ---
Table 1.2150.b GPS week : 2150 MJD: 59294.0-59300.0
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 17 20 21 19 18 18 |
R02 | 7 6 6 9 9 8 8 |
R03 | 8 10 10 10 10 9 10 |
R04 | 11 10 12 11 10 11 12 |
R05 | 11 10 9 12 10 10 12 |
R07 | 9 11 10 9 10 11 12 |
R08 | 9 11 9 11 10 9 8 |
R09 | 6 8 9 8 10 11 12 |
R11 | 8 37 10 11 9 11 9 |
R12 | 7 7 7 10 7 8 7 |
R13 | 16 13 14 16 18 21 14 |
R14 | 6 7 8 8 7 8 7 |
R15 | 8 7 7 6 7 8 7 |
R16 | 18 12 12 17 14 14 13 |
R17 | 11 9 8 10 9 9 10 |
R18 | 8 9 9 10 9 7 9 |
R19 | 16 15 15 15 25 25 20 |
R20 | 31 27 26 29 26 28 23 |
R21 | 10 10 9 10 9 9 10 |
R22 | 22 23 23 25 28 23 21 |
R24 | 9 10 9 15 10 11 11 |
Table 1.2150.c GPS week : 2150 MJD: 59294.0-59300.0
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 2150 0 | -26 15 315 -968 528 3089 82.7 1679 1679 | 516 0
brd 2150 1 | -12 41 338 -230 -1251 -2087 81.6 1430 1430 | -1094 0
brd 2150 2 | 4 -41 261 -1780 -369 -425 81.8 1393 1393 | 1770 0
brd 2150 3 | 58 8 270 -418 104 7465 82.1 1302 1302 | -951 0
brd 2150 4 | 4 72 171 -799 -751 9712 80.7 1135 1135 | -273 0
brd 2150 5 | -93 44 216 -354 -221 5481 82.8 1337 1337 | 1679 0
brd 2150 6 | 16 -5 185 1359 787 -1692 83.8 1652 1652 | -128 0
-------------+------------------------------------------------------------+----------------
brd 2150 mean| -6 19 251 -456 -167 3077 82.2 1418 1418 | 217 0
brd 2150 sdev| 46 37 63 956 710 4667 1.0 193 193 | 1160 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 2.2150.0 GPS week: 2150 Day: 0 MJD: 59294
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 8 -8 -28 -38 -.03 29 23 | 13044 233 3185 8070
emx n/a| -2 1 -11 -3 14 -91 -.08 29 26 | -12733 544 3239 8613
esx n/a| 0 0 -3 27 0 -64 -.01 31 25 | -3852 928 3170 6031
gfz n/a| 3 0 8 -15 7 -104 -.07 35 15 | 0 0 3232 7820
grg n/a| 1 1 -4 -33 16 105 .27 34 25 | 567 -353 3255 7708
iac n/a| -1 -3 0 34 -12 142 -.06 22 22 | 154 2511 3182 8509
mcc n/a| 5 -4 -20 156 -55 208 -.51 120 120 | --- --- --- ---
Table 2.2150.1 GPS week: 2150 Day: 1 MJD: 59295
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 6 5 -13 3 .03 28 24 | 10791 -2405 3749 8538
emx n/a| -2 0 -15 9 43 -28 -.07 32 28 | 3641 -791 3537 8900
esx n/a| 0 0 -6 24 -9 -42 .06 29 24 | 3704 -2379 3495 7640
gfz n/a| 0 2 7 4 -28 -39 .04 26 13 | 0 -2627 3497 8113
grg n/a| 1 0 0 40 22 5 .24 30 24 | -341 -1758 3537 8271
iac n/a| 0 -1 2 -21 -27 106 -.19 25 25 | 1592 -1277 3713 8936
mcc n/a| -2 -4 -35 -15 51 84 -.13 189 189 | --- --- --- ---
Table 2.2150.2 GPS week: 2150 Day: 2 MJD: 59296
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 10 47 10 -2 .04 30 21 | 11588 2968 3513 7113
emx n/a| 2 -1 -6 -38 6 -129 .07 36 31 | -15555 1210 3369 7486
esx n/a| -1 0 -2 2 -49 -46 .06 27 22 | -2029 2987 3520 6432
gfz n/a| 0 0 2 -21 6 -93 -.07 28 19 | 0 2659 3521 6869
grg n/a| 2 -1 0 -5 9 64 .24 27 25 | 857 1636 3367 6796
iac n/a| -1 0 -1 15 29 117 -.18 22 19 | 3424 654 3527 7410
mcc n/a| 2 -7 19 8 -36 327 .20 277 277 | --- --- --- ---
Table 2.2150.3 GPS week: 2150 Day: 3 MJD: 59297
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 9 -5 7 -3 .03 26 21 | 12340 -1812 3273 7750
emx n/a| -1 -1 -6 -13 14 -35 -.02 35 31 | -5526 -472 3229 8240
esx n/a| -2 -1 -5 -23 -17 -29 .04 35 29 | 2338 -1283 3263 7427
gfz n/a| -2 -1 8 -14 -1 -42 -.12 36 17 | 0 -1940 3289 7551
grg n/a| 0 -1 -11 -21 9 -13 .32 33 28 | -477 -1042 3252 7646
iac n/a| 4 0 0 39 -28 164 -.19 28 26 | 2283 -2460 3263 8078
mcc n/a| 7 -5 5 78 -146 428 -.42 194 194 | --- --- --- ---
Table 2.2150.4 GPS week: 2150 Day: 4 MJD: 59298
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 2 11 14 15 40 -.03 26 17 | 10818 -355 3218 8049
emx n/a| 1 0 -10 -42 6 -15 -.02 38 31 | 4740 -102 3226 8591
esx n/a| 1 0 -4 3 -16 -89 -.09 39 31 | -482 786 3191 8164
gfz n/a| 2 0 5 -19 -22 -46 -.11 31 14 | 0 -1684 3173 7693
grg n/a| 0 -2 -12 19 18 36 .36 29 24 | 391 -1520 3232 7619
iac n/a| -2 1 6 0 -9 163 -.22 32 32 | 199 851 3215 8495
mcc n/a| 1 -3 1 107 -101 47 -.55 161 161 | --- --- --- ---
Table 2.2150.5 GPS week: 2150 Day: 5 MJD: 59299
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 9 -26 3 43 -.07 29 19 | 11991 2019 3349 9410
emx n/a| 1 1 -12 -7 -9 -29 -.03 32 25 | 6617 2416 3333 9802
esx n/a| 0 2 -8 -9 -20 -65 -.05 33 28 | 9941 4216 3324 8986
gfz n/a| 2 0 8 9 -19 -88 -.07 29 20 | 0 2837 3346 9292
grg n/a| 1 -2 -8 28 19 -22 .43 34 27 | 746 1542 3324 8712
iac n/a| -5 1 10 -9 68 160 -.21 36 26 | 2981 840 3354 9807
mcc n/a| -2 5 4 -84 36 -222 -.50 203 203 | --- --- --- ---
Table 2.2150.6 GPS week: 2150 Day: 6 MJD: 59300
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 -1 6 17 -5 8 -.05 29 18 | 13420 -1207 3495 8448
emx n/a| 0 1 -8 -20 41 0 .10 32 28 | -18252 -247 3499 8835
esx n/a| 0 1 -7 6 -10 15 -.01 32 28 | -1415 -1237 3468 7814
gfz n/a| -1 3 11 7 -40 -46 -.12 25 17 | 0 -907 3491 8449
grg n/a| 0 -6 -8 30 -7 10 .40 28 27 | 404 -830 3540 8116
iac n/a| -1 2 3 -36 67 24 -.19 29 29 | 2528 -798 3496 8899
mcc n/a| -1 0 -11 39 -11 -284 -.84 141 141 | --- --- --- ---
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 3.2150.0 GPS week: 2150 Day: 0 MJD: 59294
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1604 58 31 52 18 21 12 --- 16 | 111 55 50 70 82 70 --- 68
R02 | 580 17 17 7 14 16 13 55 6 | 58 43 47 54 59 47 48 50
R03 | 529 13 20 26 17 21 8 94 8 | 82 59 55 82 90 73 35 73
XR04 | 490 25 23 23 --- 18 15 --- 10 | 86 64 63 --- 79 78 --- 73
R05 | 595 14 30 32 16 17 25 98 10 | 69 50 65 72 72 80 52 66
R07 | 1069 14 29 21 17 16 14 108 8 | 85 58 60 88 88 91 73 78
R08 | 855 18 27 13 18 26 21 --- 9 | 77 57 64 72 86 83 --- 73
R09 | 2024 10 10 10 12 19 11 --- 5 | 51 57 57 53 54 56 --- 53
XR11 | 1458 13 --- 13 18 --- 11 --- 8 | 29 --- 57 32 --- 31 --- 29
R12 | 956 15 19 15 14 15 15 --- 7 | 64 69 68 66 60 57 --- 62
R13 | 5314 33 31 38 35 45 32 --- 16 | 78 68 48 67 83 92 --- 71
R14 | 893 12 13 12 10 12 15 --- 5 | 52 41 48 48 46 49 --- 46
R15 | 773 14 12 28 17 19 14 205 8 | 65 64 57 68 70 68 85 64
R16 | 767 31 35 41 23 62 43 --- 18 | 42 39 38 51 78 83 --- 53
R17E | 1362 20 31 24 20 34 18 --- 11 | 191 191 188 190 194 187 --- 189
R18E | 1873 13 27 10 11 18 18 --- 7 | 92 94 94 99 103 100 --- 96
R19E | 810 32 27 21 51 37 30 --- 15 | 53 48 43 53 53 58 --- 43
R20E | 585 54 64 66 113 78 20 --- 31 | 73 51 58 121 56 64 --- 59
R21E | 652 18 30 24 20 18 15 108 9 | 149 150 151 149 154 150 305 149
R22E | 1456 60 38 49 54 61 37 --- 22 | 80 76 110 94 124 107 --- 92
R24E | 1998 16 25 15 19 21 15 --- 8 | 154 154 153 157 153 154 --- 154
------+----------------------------------------------+------------------------------------------
RMS | 1679 29 29 31 35 34 22 120 |T 82 74 74 84 89 84 99 78
WRMS | 1679 23 26 25 15 25 22 120 |NE 67 55 55 63 72 68 58 61
MEDI | 893 17 27 23 18 19 15 98 |MD 77 58 58 70 79 78 52 68
Table 3.2150.1 GPS week: 2150 Day: 1 MJD: 59295
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1186 58 31 55 18 24 26 --- 17 | 74 43 59 53 50 68 --- 51
R02 | 787 11 16 13 11 16 13 57 6 | 43 41 35 41 45 37 56 39
R03 | 805 11 32 30 16 23 15 103 9 | 59 45 49 69 76 68 35 60
XR04 | 900 25 23 20 --- 13 14 --- 10 | 61 50 52 --- 66 54 --- 55
R05 | 652 19 23 26 16 20 24 114 9 | 51 38 48 53 58 48 85 47
R07 | 1307 13 29 33 17 24 20 99 10 | 66 47 55 64 73 70 47 61
R08 | 909 24 26 19 17 21 31 --- 10 | 59 44 54 63 70 54 --- 55
R09 | 842 13 14 13 9 29 18 --- 7 | 55 51 59 52 46 65 --- 53
XR11 | 2385 35 --- 119 29 --- 43 --- 36 | 29 --- 110 33 --- 34 --- 36
R12 | 1453 16 19 18 9 15 13 --- 6 | 48 52 48 47 52 43 --- 46
R13 | 2748 39 24 33 18 30 22 --- 12 | 59 50 48 56 49 53 --- 50
R14 | 969 12 16 14 8 17 26 --- 7 | 38 28 34 37 29 52 --- 35
R15 | 588 9 17 20 10 19 18 396 7 | 45 46 42 47 52 51 195 45
R16 | 1215 23 20 19 26 42 20 --- 11 | 28 41 45 35 51 37 --- 33
R17E | 1131 15 31 13 13 10 30 --- 9 | 207 204 208 212 207 215 --- 209
R18E | 3687 22 27 13 9 16 23 --- 8 | 94 91 94 97 98 96 --- 94
R19E | 713 31 37 28 38 34 29 --- 15 | 44 58 59 63 41 49 --- 44
R20E | 678 50 71 63 71 64 26 --- 26 | 50 37 58 83 48 46 --- 45
R21E | 469 15 37 21 20 18 14 142 9 | 161 157 158 164 168 160 461 161
R22E | 1599 59 54 36 45 57 56 --- 23 | 47 51 73 68 94 91 --- 62
R24E | 1197 14 28 20 22 32 21 --- 10 | 140 138 137 137 148 142 --- 139
------+----------------------------------------------+------------------------------------------
RMS | 1429 28 32 29 26 30 25 189 |T 69 65 72 73 76 73 146 67
WRMS | 1429 24 28 24 13 24 25 189 |NE 51 44 52 50 55 52 83 47
MEDI | 969 19 26 20 17 21 22 103 |MD 55 47 55 56 52 54 56 51
Table 3.2150.2 GPS week: 2150 Day: 2 MJD: 59296
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1661 45 52 55 34 50 18 --- 19 | 96 62 71 94 95 76 --- 75
R02 | 685 10 15 6 11 17 17 148 6 | 42 38 44 51 37 48 123 42
R03 | 1417 17 20 37 10 20 18 99 10 | 70 55 35 53 73 69 30 57
XR04 | 1771 28 23 27 --- 18 15 --- 11 | 74 54 47 --- 64 63 --- 58
R05 | 752 21 24 23 13 20 20 172 9 | 64 53 50 56 61 52 96 53
R07 | 920 11 25 32 17 27 8 111 9 | 71 54 53 76 85 68 86 66
R08 | 1324 14 30 15 11 34 16 --- 9 | 67 47 61 60 80 59 --- 61
R09 | 1101 12 16 10 24 37 13 --- 9 | 58 55 59 60 47 59 --- 54
XR11 | 2696 9 --- 22 14 --- 19 --- 10 | 20 --- 41 24 --- 26 --- 21
R12 | 1912 16 16 14 20 16 12 --- 7 | 53 37 46 57 41 48 --- 46
R13 | 1927 33 30 35 35 19 26 --- 13 | 61 61 47 93 63 73 --- 63
R14 | 1198 11 17 12 24 18 17 --- 7 | 39 33 48 58 39 45 --- 41
R15 | 594 6 12 13 21 18 18 121 7 | 51 56 52 46 61 67 117 54
R16 | 1292 21 24 20 30 42 14 --- 11 | 28 44 41 41 43 34 --- 35
R17E | 1046 25 28 10 11 16 16 --- 8 | 144 151 154 148 157 145 --- 149
R18E | 3516 17 26 9 14 22 29 --- 9 | 60 61 63 64 73 72 --- 64
R19E | 945 44 48 22 31 23 23 --- 14 | 50 46 29 52 45 49 --- 38
R20E | 684 58 78 61 81 27 28 --- 25 | 55 41 45 92 65 50 --- 46
R21E | 473 23 29 13 16 22 17 611 9 | 132 138 136 137 132 136 270 134
R22E | 927 72 72 24 31 41 54 --- 22 | 149 132 150 163 169 165 --- 152
R24E | 722 17 35 14 14 14 21 --- 8 | 154 145 153 157 160 148 --- 151
------+----------------------------------------------+------------------------------------------
RMS | 1393 30 36 27 28 27 22 277 |T 73 68 67 79 79 73 120 69
WRMS | 1393 21 31 22 19 25 19 277 |NE 56 49 49 59 60 56 90 51
MEDI | 1101 17 25 20 17 20 18 121 |MD 61 54 50 60 64 63 96 57
Table 3.2150.3 GPS week: 2150 Day: 3 MJD: 59297
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 750 45 55 72 23 52 20 --- 21 | 86 36 29 62 89 51 --- 53
R02 | 566 10 26 10 32 23 18 110 9 | 54 32 46 65 58 42 67 48
R03 | 1210 17 20 28 12 18 29 107 9 | 68 46 43 60 59 76 29 58
XR04 | 1462 23 20 31 --- 11 17 --- 10 | 73 46 34 --- 61 67 --- 57
R05 | 1589 10 36 30 22 24 29 131 11 | 57 33 40 68 70 81 62 57
R07 | 970 16 19 32 11 14 21 85 9 | 67 48 39 57 62 65 33 56
R08 | 1063 16 17 28 27 15 32 --- 10 | 58 43 38 43 60 79 --- 53
R09 | 907 14 16 14 15 26 16 --- 7 | 38 42 43 45 30 45 --- 38
XR11 | 2148 16 --- 18 15 --- 26 --- 11 | 20 --- 30 21 --- 30 --- 20
R12 | 1209 15 15 25 19 23 32 --- 10 | 50 38 40 39 39 63 --- 42
R13 | 1919 26 24 53 38 39 31 --- 16 | 69 60 51 66 92 87 --- 69
R14 | 1443 15 15 26 11 9 23 --- 8 | 42 28 31 31 41 52 --- 36
R15 | 1144 9 10 8 14 13 19 101 6 | 49 50 48 41 54 50 50 47
R16 | 1325 32 44 27 42 54 23 --- 17 | 34 45 49 48 66 55 --- 43
R17E | 1044 18 34 22 18 21 21 --- 10 | 193 188 186 190 189 199 --- 190
R18E | 2772 13 29 17 31 24 21 --- 10 | 63 65 68 69 70 63 --- 63
R19E | 828 35 40 26 37 30 34 --- 15 | 83 73 62 78 64 80 --- 69
R20E | 837 48 73 65 95 59 35 --- 28 | 78 68 61 114 69 66 --- 68
R21E | 713 29 24 15 15 22 13 411 9 | 147 143 150 148 147 140 263 144
R22E | 1485 51 52 51 68 59 45 --- 24 | 110 100 143 163 145 127 --- 123
R24E | 1127 15 38 25 31 34 45 --- 14 | 133 135 135 141 137 140 --- 135
------+----------------------------------------------+------------------------------------------
RMS | 1302 26 35 35 36 33 28 194 |T 74 65 65 77 80 78 84 69
WRMS | 1302 21 31 29 17 28 26 194 |NE 54 42 40 49 60 60 48 48
MEDI | 1144 16 24 26 22 23 23 107 |MD 67 46 46 62 64 66 50 57
Table 3.2150.4 GPS week: 2150 Day: 4 MJD: 59298
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 528 35 41 89 15 25 34 --- 19 | 81 70 59 71 73 89 --- 68
R02 | 759 14 26 11 18 18 23 81 8 | 50 27 38 37 50 37 57 39
R03 | 888 10 28 34 12 24 23 94 9 | 64 39 40 63 72 70 36 59
XR04 | 682 19 22 26 --- 14 22 --- 10 | 66 49 43 --- 56 64 --- 55
R05 | 1297 11 24 32 17 14 34 80 10 | 61 52 50 70 57 80 40 60
R07 | 1170 11 23 35 12 10 32 78 9 | 69 49 45 69 67 77 63 63
R08 | 1202 9 24 29 19 18 29 --- 9 | 57 44 43 67 58 77 --- 57
R09 | 1041 18 14 19 15 37 14 --- 9 | 46 47 54 47 52 46 --- 45
XR11 | 1468 11 --- 16 19 --- 14 --- 9 | 24 --- 26 34 --- 34 --- 27
R12 | 662 14 15 23 9 11 22 --- 7 | 54 54 48 54 53 47 --- 51
R13 | 1401 27 38 53 51 34 31 --- 17 | 62 60 45 60 70 65 --- 58
R14 | 1555 21 15 17 11 12 15 --- 7 | 43 32 33 29 38 43 --- 35
R15 | 1191 8 16 29 14 11 17 107 7 | 53 48 45 58 66 59 23 54
R16 | 1918 25 38 33 23 35 28 --- 13 | 38 26 44 47 50 52 --- 39
R17E | 680 12 31 18 13 18 23 --- 8 | 105 101 103 107 99 100 --- 102
R18E | 1442 13 22 13 16 28 17 --- 8 | 39 37 41 39 49 36 --- 38
R19E | 1365 45 76 43 52 50 64 --- 24 | 93 107 91 92 79 97 --- 84
R20E | 757 42 71 67 58 46 65 --- 25 | 70 66 83 89 57 100 --- 67
R21E | 960 20 26 17 12 18 29 341 9 | 116 117 110 116 112 123 167 115
R22E | 898 61 67 53 79 57 32 --- 27 | 64 65 86 105 97 80 --- 70
R24E | 781 18 34 21 20 21 21 --- 10 | 154 150 150 150 153 155 --- 151
------+----------------------------------------------+------------------------------------------
RMS | 1135 26 38 39 31 29 32 161 |T 67 62 60 70 70 72 64 63
WRMS | 1135 17 31 31 14 24 32 161 |NE 54 45 43 54 58 60 43 50
MEDI | 1041 18 26 29 16 18 23 81 |MD 62 49 45 63 58 70 40 58
Table 3.2150.5 GPS week: 2150 Day: 5 MJD: 59299
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 649 48 35 66 18 30 23 --- 17 | 87 63 59 65 72 78 --- 66
R02 | 1558 12 19 19 13 18 27 75 8 | 50 40 38 42 55 62 101 45
R03 | 1003 18 21 26 19 20 18 82 9 | 62 44 42 60 62 45 47 51
XR04 | 516 18 18 26 --- 18 29 --- 11 | 68 54 52 --- 62 79 --- 61
R05 | 951 19 17 32 17 19 33 51 10 | 55 57 60 67 52 72 39 57
R07 | 1341 8 25 36 26 14 23 84 10 | 70 61 54 87 71 89 85 71
R08 | 823 11 23 16 26 21 18 --- 9 | 57 44 48 62 66 67 --- 55
R09 | 2166 17 12 18 24 38 30 --- 10 | 50 55 61 56 42 53 --- 49
XR11 | 1169 15 --- 11 21 --- 22 --- 10 | 25 --- 22 27 --- 23 --- 22
R12 | 1019 16 11 19 17 17 19 --- 7 | 47 39 44 53 40 45 --- 42
R13 | 2704 23 29 45 38 89 32 --- 21 | 61 41 41 58 108 59 --- 58
R14 | 1006 21 12 11 18 17 24 --- 8 | 37 26 34 31 32 26 --- 29
R15 | 1729 11 17 22 19 22 15 125 8 | 49 46 46 57 44 47 29 46
R16 | 1725 35 41 25 22 23 25 --- 13 | 39 29 38 53 37 46 --- 33
R17E | 725 11 31 17 17 9 26 --- 9 | 131 126 131 133 128 130 --- 129
R18E | 869 9 20 11 12 22 20 --- 7 | 47 41 43 44 54 45 --- 44
R19E | 1507 52 63 43 56 34 77 --- 24 | 90 64 62 95 71 98 --- 73
R20E | 733 49 69 68 54 57 78 --- 28 | 85 74 76 91 75 97 --- 72
R21E | 1049 15 26 15 19 15 19 457 8 | 109 109 108 113 107 115 242 109
R22E | 752 64 29 45 58 49 58 --- 23 | 32 44 74 70 68 48 --- 48
R24E | 964 21 32 17 18 21 30 --- 10 | 110 102 108 110 107 108 --- 106
------+----------------------------------------------+------------------------------------------
RMS | 1336 29 32 33 29 34 36 203 |T 64 57 59 68 67 68 90 60
WRMS | 1336 19 25 28 20 27 26 203 |NE 54 46 45 55 57 56 60 48
MEDI | 1006 18 23 22 19 21 25 82 |MD 57 46 52 60 62 62 47 55
Table 3.2150.6 GPS week: 2150 Day: 6 MJD: 59300
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod emx esx gfz grg iac mcc IGL | cod emx esx gfz grg iac mcc IGL
------+----------------------------------------------+------------------------------------------
R01 | 1028 51 35 58 17 41 34 --- 18 | 112 70 65 88 102 79 --- 82
R02 | 1576 10 23 19 10 9 28 137 7 | 63 46 48 57 57 82 81 58
R03 | 1028 19 16 36 18 14 31 103 10 | 82 54 48 71 77 76 72 67
XR04 | 452 11 20 34 --- 19 29 --- 12 | 89 74 68 --- 87 98 --- 81
R05 | 858 14 31 28 21 25 33 74 11 | 76 68 71 91 85 87 52 78
R07 | 1178 12 29 42 28 12 34 119 12 | 96 77 71 119 92 123 73 96
R08 | 753 14 22 18 25 16 10 --- 8 | 80 65 67 87 85 83 --- 78
R09 | 3052 26 18 13 24 42 24 --- 12 | 75 72 72 76 50 70 --- 66
XR11 | 1252 13 --- 12 11 --- 24 --- 9 | 27 --- 38 35 --- 45 --- 33
R12 | 663 15 20 16 14 14 14 --- 7 | 69 61 62 70 64 67 --- 64
R13 | 4604 24 43 33 15 44 17 --- 13 | 89 59 59 83 113 93 --- 81
R14 | 889 17 10 15 15 11 24 --- 7 | 58 45 47 45 55 48 --- 48
R15 | 1035 13 13 12 10 13 27 125 7 | 71 64 65 69 68 79 57 69
R16 | 1573 18 32 38 22 42 17 --- 13 | 52 49 56 66 74 55 --- 55
R17E | 1461 10 28 25 14 19 31 --- 9 | 110 112 101 107 112 115 --- 108
R18E | 1002 9 27 10 15 25 20 --- 8 | 54 55 53 52 63 59 --- 54
R19E | 892 42 62 45 42 30 48 --- 20 | 76 75 65 80 77 84 --- 70
R20E | 611 55 50 53 57 50 34 --- 22 | 74 78 74 82 79 81 --- 68
R21E | 1397 16 32 21 18 14 23 235 9 | 100 103 101 109 108 115 370 104
R22E | 841 66 32 50 39 37 51 --- 21 | 33 55 72 58 67 60 --- 44
R24E | 1504 17 39 16 17 22 29 --- 10 | 118 119 113 118 119 127 --- 117
------+----------------------------------------------+------------------------------------------
RMS | 1651 29 32 32 25 28 29 141 |T 76 70 67 78 81 82 117 72
WRMS | 1651 18 28 28 17 27 29 141 |NE 74 61 59 73 77 77 67 68
MEDI | 1028 16 28 25 17 19 28 119 |MD 76 65 65 76 77 81 72 69
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