[IGSREPORT-27846] Wk 2149 IGLOS Final Orbits
acc
acc at igs.org
Sat Apr 3 12:38:04 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2149 (Mar 14, 2021 - Mar 20, 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 2.2149.
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:
igl2149[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2149 in the SP3 format.
igl21497.sum Combination Report for GPS Week 2149.
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 | 1.1 ns
1 | -1.2 ns
2 | -0.6 ns
3 | 0.0 ns
4 | -1.5 ns
5 | 0.5 ns
6 | -1.0 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 1.2149, 1a.2149).
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 2.2149.0-6)
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 3.2149.0-6).
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 2149 summary. (Mar 14, 2021 - Mar 20, 2021)
Table 1.2149.a GPS week : 2149 MJD: 59287.0-59293.0
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 1 8 13 -3 23 -.03 29 21 | 17860 -516 3134 7669
| 1 0 2 8 13 22 .02 | 2621 1865
emx n/a| 0 1 -12 -31 -5 -52 -.02 36 30 | -3695 398 3147 8239
| 2 1 1 21 32 43 .04 | 8487 1045
esx n/a| -1 0 -5 12 -16 -55 -.00 33 27 | 2313 -807 3118 7661
| 1 1 1 12 22 38 .05 | 4887 2253
gfz n/a| 0 1 8 -13 4 -95 -.06 30 18 | 0 -1054 3130 7461
| 0 1 1 27 18 22 .06 | 0 1856
grg n/a| 3 -2 -7 -5 15 31 .34 27 23 | -12 -813 3164 7352
| 2 1 1 15 11 41 .02 | 320 1722
iac n/a| -3 -1 5 11 0 129 -.18 28 27 | 1461 84 3127 8090
| 1 1 1 36 27 70 .05 | 1205 792
mcc n/a| 0 3 -6 64 -19 -431 -.43 131 131 | --- --- --- ---
| 8 6 9 66 101 246 .37 | --- ---
Table 1.2149.b GPS week : 2149 MJD: 59287.0-59293.0
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 19 20 20 19 17 16 |
R02 | 7 10 9 7 7 7 6 |
R03 | 11 11 9 12 9 10 9 |
R04 | 11 12 13 10 11 9 12 |
R05 | 11 9 11 10 11 13 11 |
R07 | 11 9 10 10 10 10 9 |
R08 | 10 11 11 8 8 9 9 |
R09 | 10 11 8 10 10 10 7 |
R11 | 9 11 13 10 11 10 11 |
R12 | 9 8 9 10 8 8 7 |
R13 | 15 13 13 12 21 15 14 |
R14 | 6 7 8 7 8 5 6 |
R15 | 7 8 8 8 6 8 5 |
R16 | 13 14 15 15 12 16 17 |
R17 | 10 11 10 9 9 8 9 |
R18 | 11 9 11 11 8 8 9 |
R19 | 15 15 17 20 23 18 12 |
R20 | 27 30 27 28 29 28 29 |
R21 | 9 11 11 11 11 10 12 |
R22 | 23 22 24 26 26 22 19 |
R24 | 12 9 10 10 9 9 11 |
Table 1.2149.c GPS week : 2149 MJD: 59287.0-59293.0
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 2149 0 | 49 -64 304 -216 -789 2238 80.3 1715 1715 | 1099 0
brd 2149 1 | 74 -25 290 489 -438 10650 81.5 1789 1789 | -1159 0
brd 2149 2 | 106 -22 298 1490 2373 15910 80.4 1970 1970 | -550 0
brd 2149 3 | -8 86 388 -1079 980 13480 80.4 1676 1676 | 46 0
brd 2149 4 | 61 77 338 -49 2889 8773 81.7 1496 1496 | -1531 0
brd 2149 5 | -3 -66 258 458 -342 4053 83.8 1527 1527 | 547 0
brd 2149 6 | -38 -45 358 296 -1901 2218 83.6 1895 1895 | -958 0
-------------+------------------------------------------------------------+----------------
brd 2149 mean| 34 -8 319 198 395 8188 81.7 1724 1724 | -358 0
brd 2149 sdev| 52 64 44 784 1750 5510 1.5 176 176 | 959 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 2.2149.0 GPS week: 2149 Day: 0 MJD: 59287
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 4 10 -3 38 -.02 27 20 | 21726 2323 3175 6370
emx n/a| 0 1 -14 -23 -6 -62 -.04 34 31 | 6457 1820 3185 6964
esx n/a| 0 2 -6 15 -28 -97 .04 31 26 | 8785 1581 3149 6283
gfz n/a| 1 0 10 -5 14 -112 -.01 27 18 | 0 1354 3159 6178
grg n/a| 5 -2 -5 -3 35 -21 .36 29 27 | -1 2026 3222 6573
iac n/a| -2 -1 4 -40 17 220 -.16 27 25 | 3191 76 3146 6799
mcc n/a| 12 11 -15 180 90 -381 .03 238 238 | --- --- --- ---
Table 2.2149.1 GPS week: 2149 Day: 1 MJD: 59288
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 7 24 13 27 -.01 26 19 | 19985 -1355 2945 7333
emx n/a| -2 1 -9 -23 0 -37 -.05 36 30 | -4897 -988 2997 7882
esx n/a| -1 1 -5 10 -27 -36 -.06 34 28 | -5718 -1143 2929 5835
gfz n/a| 0 -1 6 -42 34 -98 -.08 30 19 | 0 -2321 2887 7173
grg n/a| 5 -2 -7 -15 14 22 .35 28 25 | -254 -2078 2988 6987
iac n/a| -3 0 4 71 -47 122 -.09 27 27 | 344 -61 2946 7745
mcc n/a| 11 9 1 72 -155 -450 .08 112 112 | --- --- --- ---
Table 2.2149.2 GPS week: 2149 Day: 2 MJD: 59289
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 5 25 6 32 -.05 28 20 | 18230 -498 2954 8236
emx n/a| -1 -1 -13 -11 -45 -15 -.03 37 34 | -10931 252 2997 8740
esx n/a| -3 -1 -8 -11 14 -30 .01 35 28 | 1427 -854 2938 7589
gfz n/a| 0 2 9 -18 7 -109 -.06 30 19 | 0 -1134 2914 7923
grg n/a| 6 -3 -7 4 5 4 .36 27 23 | -263 -807 3020 7566
iac n/a| 0 -2 7 9 -12 102 -.19 28 28 | 184 1088 2960 8694
mcc n/a| -6 6 2 -1 -140 -510 -.33 97 97 | --- --- --- ---
Table 2.2149.3 GPS week: 2149 Day: 3 MJD: 59290
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 10 3 6 42 -.03 28 19 | 19113 -345 3350 7862
emx n/a| 3 0 -10 -17 -36 -67 -.06 37 29 | 8582 437 3386 8410
esx n/a| -1 0 -4 26 -47 -41 -.03 36 29 | 5415 860 3355 7100
gfz n/a| 0 1 10 -25 3 -114 -.18 33 16 | 0 -264 3420 7684
grg n/a| 3 -3 -6 11 10 6 .34 21 21 | 214 -664 3378 7618
iac n/a| -5 0 4 -10 -7 174 -.23 36 36 | 2208 1054 3347 8293
mcc n/a| -2 0 1 42 21 -403 -.57 106 106 | --- --- --- ---
Table 2.2149.4 GPS week: 2149 Day: 4 MJD: 59291
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 9 11 -4 28 -.05 33 24 | 16019 -3112 3031 7613
emx n/a| 3 1 -12 -21 18 -117 -.04 39 34 | -2255 -83 2922 8169
esx n/a| 0 0 -4 17 2 -63 .02 31 27 | 2045 -2882 2992 9195
gfz n/a| 1 2 6 -43 7 -108 -.05 33 23 | 0 -3408 3017 7295
grg n/a| 2 -4 -8 10 1 51 .31 29 24 | -418 -2288 3001 7099
iac n/a| -4 -2 4 36 -3 158 -.17 29 29 | 593 -760 3028 8073
mcc n/a| 0 1 -5 -10 4 -851 -.70 129 129 | --- --- --- ---
Table 2.2149.5 GPS week: 2149 Day: 5 MJD: 59292
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 4 -24 17 -.02 31 22 | 15108 1307 3396 8149
emx n/a| -2 4 -12 -56 50 13 .01 35 28 | -12736 1726 3473 8756
esx n/a| 0 0 -2 10 -1 -3 -.07 32 30 | -1514 1246 3402 7709
gfz n/a| 1 2 8 8 -22 -58 -.01 24 16 | 0 1064 3433 7951
grg n/a| 0 -3 -10 -16 21 48 .34 29 21 | 145 776 3422 7711
iac n/a| -3 -2 4 -12 24 -5 -.17 28 24 | 2636 149 3392 8561
mcc n/a| -11 2 -20 55 -52 -410 -.86 114 114 | --- --- --- ---
Table 2.2149.6 GPS week: 2149 Day: 6 MJD: 59293
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 14 -14 -23 -.03 30 22 | 14841 -1935 3092 8124
emx n/a| 1 0 -14 -66 -21 -78 .05 30 26 | -10087 -374 3072 8757
esx n/a| -2 2 -3 20 -28 -113 .06 29 23 | 5752 -4462 3064 9917
gfz n/a| 0 0 8 31 -12 -68 -.04 32 13 | 0 -2675 3085 8026
grg n/a| 1 0 -7 -29 19 104 .32 29 24 | 493 -2660 3118 7914
iac n/a| -2 0 6 22 33 131 -.22 21 21 | 1075 -958 3073 8466
mcc n/a| 0 -8 -13 112 96 -10 -.68 121 121 | --- --- --- ---
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 3.2149.0 GPS week: 2149 Day: 0 MJD: 59287
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 | 703 52 40 52 27 25 14 --- 17 | 106 47 52 85 62 78 --- 67
R02 | 3192 6 21 11 15 17 15 272 6 | 58 42 44 56 52 58 101 51
R03 | 807 14 29 32 24 19 29 199 11 | 75 49 44 78 72 73 81 65
XR04 | 591 26 21 21 --- 23 18 --- 11 | 76 55 52 --- 83 67 --- 65
R05 | 1066 9 35 30 10 14 35 141 10 | 60 39 49 67 64 75 121 57
R07 | 1588 12 37 33 27 20 15 119 11 | 84 52 54 100 93 86 84 78
R08 | 1670 14 34 25 22 25 14 --- 10 | 75 50 59 88 84 86 --- 73
R09 | 670 17 21 16 16 36 19 --- 9 | 40 41 42 48 37 40 --- 37
XR11 | 1836 11 --- 15 18 --- 17 --- 9 | 17 --- 23 25 --- 29 --- 20
R12 | 2420 15 12 20 22 25 24 --- 9 | 57 51 64 66 44 58 --- 55
R13 | 3675 38 26 17 26 47 31 --- 14 | 73 65 63 68 61 62 --- 64
R14 | 1123 7 9 8 11 14 22 --- 5 | 48 43 48 42 40 54 --- 45
R15 | 590 7 13 12 11 14 28 422 7 | 55 60 54 51 52 59 179 54
R16 | 802 27 33 21 18 44 16 --- 12 | 75 86 88 86 92 74 --- 82
R17 | 1922 12 30 23 23 21 16 --- 9 | 61 41 40 68 61 57 --- 53
R18 | 1064 20 29 10 16 19 39 --- 10 | 94 89 96 94 107 119 --- 99
R19 | 2187 41 40 20 30 30 32 --- 14 | 43 40 37 61 40 47 --- 34
R20 | 1242 48 70 62 75 60 35 --- 26 | 86 33 55 111 57 74 --- 60
R21 | 476 14 31 25 19 13 15 122 9 | 65 44 41 67 63 66 73 57
R22 | 1439 54 51 69 36 32 51 --- 22 | 58 79 111 88 123 135 --- 91
R24 | 1600 17 38 22 17 27 33 --- 11 | 53 26 34 48 47 55 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1714 27 34 31 27 29 27 238 |T 64 51 54 69 66 69 106 59
WRMS | 1714 20 31 26 18 27 25 238 |NE 64 51 54 69 66 69 106 59
MEDI | 1242 15 30 21 19 23 22 141 |MD 61 47 52 67 61 66 84 57
Table 3.2149.1 GPS week: 2149 Day: 1 MJD: 59288
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 | 885 40 54 65 43 29 20 --- 19 | 78 35 57 96 65 54 --- 61
R02 | 3196 8 20 17 19 25 32 87 9 | 40 35 46 42 28 57 123 37
R03 | 615 8 30 33 14 17 31 113 10 | 56 38 33 55 58 73 66 52
XR04 | 914 17 28 31 --- 24 15 --- 11 | 56 41 39 --- 65 50 --- 49
R05 | 1237 14 24 28 14 17 12 137 8 | 41 29 33 42 44 35 83 35
R07 | 1483 13 25 31 12 22 20 102 9 | 61 41 41 50 65 66 50 53
R08 | 1491 10 30 24 21 14 39 --- 11 | 55 37 48 51 54 66 --- 50
R09 | 1442 18 18 13 27 37 26 --- 11 | 34 44 44 56 27 46 --- 37
XR11 | 1314 15 --- 19 15 --- 26 --- 11 | 19 --- 38 34 --- 34 --- 25
R12 | 2238 17 19 15 15 15 24 --- 8 | 39 30 47 51 36 50 --- 41
R13 | 4010 33 15 28 31 29 29 --- 13 | 43 45 39 54 40 28 --- 38
R14 | 1562 12 15 13 11 17 20 --- 6 | 34 29 43 31 40 38 --- 34
R15 | 996 14 19 17 21 11 19 146 7 | 38 39 32 21 39 39 134 32
R16 | 1312 21 25 27 33 47 17 --- 13 | 49 40 55 57 47 45 --- 47
R17 | 2385 12 34 27 13 32 20 --- 10 | 42 35 28 41 58 50 --- 40
R18 | 1794 15 24 13 11 31 12 --- 8 | 74 68 76 72 87 77 --- 74
R19 | 1434 33 37 36 39 26 23 --- 14 | 27 28 33 32 37 28 --- 22
R20 | 1390 34 89 77 90 53 39 --- 29 | 49 25 50 93 55 64 --- 48
R21 | 686 17 35 29 18 14 26 62 10 | 41 35 30 42 37 53 52 38
R22 | 877 68 50 53 22 30 50 --- 21 | 39 46 85 57 68 76 --- 56
R24 | 984 16 38 18 17 14 16 --- 9 | 37 23 26 34 42 41 --- 32
------+----------------------------------------------+------------------------------------------
RMS | 1788 26 36 34 30 28 27 112 |T 45 37 43 50 49 50 84 42
WRMS | 1788 19 30 27 19 25 27 112 |NE 45 37 43 50 49 50 84 42
MEDI | 1390 16 25 27 18 24 23 102 |MD 41 35 41 50 44 50 66 40
Table 3.2149.2 GPS week: 2149 Day: 2 MJD: 59289
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 | 964 42 58 75 30 32 23 --- 20 | 95 46 47 94 79 80 --- 70
R02 | 2868 6 26 19 21 20 20 104 8 | 50 40 47 60 54 47 52 48
R03 | 652 14 26 26 14 23 16 98 9 | 59 38 35 51 60 58 59 49
XR04 | 878 10 29 29 --- 16 35 --- 12 | 60 41 37 --- 65 84 --- 57
R05 | 1087 12 32 30 20 23 22 90 10 | 51 27 43 56 63 59 58 49
R07 | 1902 17 24 33 8 18 24 120 9 | 62 39 39 59 69 63 48 55
R08 | 707 10 32 28 17 29 25 --- 10 | 58 35 43 62 75 74 --- 58
R09 | 938 16 12 12 10 23 19 --- 7 | 37 41 44 41 34 36 --- 36
XR11 | 1143 9 --- 19 18 --- 35 --- 12 | 14 --- 25 20 --- 38 --- 17
R12 | 2217 19 14 17 15 14 32 --- 8 | 44 36 42 42 41 68 --- 43
R13 | 6141 20 26 40 31 24 21 --- 12 | 52 59 44 60 57 65 --- 53
R14 | 1703 14 12 15 18 10 25 --- 7 | 41 36 37 37 33 36 --- 34
R15 | 1257 13 17 20 16 19 19 106 7 | 41 45 36 32 51 38 75 38
R16 | 915 27 28 24 34 49 22 --- 14 | 47 43 46 51 41 45 --- 41
R17 | 1231 16 36 26 10 15 28 --- 10 | 51 33 32 45 50 58 --- 43
R18 | 1322 13 28 13 17 32 30 --- 10 | 59 60 56 61 72 78 --- 62
R19 | 1185 34 45 30 50 31 34 --- 17 | 39 25 26 52 34 46 --- 26
R20 | 700 55 73 72 79 39 29 --- 27 | 85 59 56 107 46 62 --- 64
R21 | 1415 17 33 30 19 15 29 49 10 | 56 36 31 54 48 68 29 47
R22 | 1525 68 66 40 42 39 60 --- 24 | 48 49 93 118 105 121 --- 85
R24 | 745 18 35 24 19 13 20 --- 9 | 44 29 23 45 47 32 --- 34
------+----------------------------------------------+------------------------------------------
RMS | 1970 28 37 35 30 27 28 97 |T 52 40 42 57 56 59 53 48
WRMS | 1970 20 34 28 19 23 28 97 |NE 52 40 42 57 56 59 53 48
MEDI | 1185 16 28 26 18 23 25 98 |MD 51 39 42 52 51 59 52 48
Table 3.2149.3 GPS week: 2149 Day: 3 MJD: 59290
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 | 801 45 49 85 21 23 28 --- 20 | 86 31 40 69 69 71 --- 54
R02 | 1120 7 27 16 12 11 19 127 7 | 50 28 44 52 55 54 60 46
R03 | 774 14 29 28 43 15 20 126 11 | 71 42 43 96 59 51 55 59
XR04 | 865 21 24 20 --- 16 15 --- 9 | 65 42 40 --- 52 55 --- 49
R05 | 1024 15 26 26 19 17 24 59 9 | 54 35 42 56 59 71 46 51
R07 | 1700 13 28 35 9 18 24 151 10 | 70 42 42 67 77 78 98 62
R08 | 869 9 24 23 16 16 20 --- 8 | 59 36 43 59 64 69 --- 54
R09 | 1680 19 11 8 24 20 37 --- 9 | 41 32 36 40 25 56 --- 31
XR11 | 1825 21 --- 13 12 --- 21 --- 10 | 18 --- 21 25 --- 31 --- 17
R12 | 870 26 14 21 22 13 34 --- 10 | 39 31 40 40 30 48 --- 32
R13 | 4933 25 20 25 39 27 19 --- 12 | 59 59 59 56 64 67 --- 58
R14 | 2494 17 13 22 10 9 17 --- 6 | 41 31 34 29 34 34 --- 32
R15 | 1371 16 11 15 14 12 36 85 8 | 42 37 32 41 38 37 38 35
R16 | 1543 23 52 21 26 42 17 --- 14 | 32 28 28 22 38 40 --- 27
R17 | 801 18 27 20 13 16 24 --- 8 | 45 26 28 38 38 49 --- 35
R18 | 1007 13 30 12 30 24 27 --- 10 | 70 53 59 50 74 70 --- 61
R19 | 1362 45 64 47 53 23 30 --- 19 | 67 34 32 77 51 43 --- 41
R20 | 928 53 72 79 88 33 32 --- 27 | 76 52 39 90 56 49 --- 49
R21 | 1119 19 29 27 17 15 43 52 11 | 53 34 36 53 44 67 35 44
R22 | 1180 56 64 44 36 27 108 --- 25 | 61 60 114 102 103 177 --- 95
R24 | 874 18 30 22 20 17 20 --- 9 | 53 30 34 50 45 49 --- 41
------+----------------------------------------------+------------------------------------------
RMS | 1676 28 37 36 33 21 36 106 |T 54 38 42 55 53 60 55 46
WRMS | 1676 19 29 29 16 21 36 106 |NE 54 38 42 55 53 60 55 46
MEDI | 1119 19 27 22 20 17 24 85 |MD 54 34 40 52 52 54 46 46
Table 3.2149.4 GPS week: 2149 Day: 4 MJD: 59291
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 | 1149 51 43 64 21 27 22 --- 18 | 85 44 40 68 64 58 --- 53
R02 | 1291 8 21 14 11 22 10 117 7 | 47 34 43 45 62 47 102 46
R03 | 716 16 26 23 8 23 15 192 8 | 64 40 41 55 73 55 74 54
XR04 | 695 22 20 21 --- 23 18 --- 10 | 64 44 50 --- 65 41 --- 51
R05 | 584 25 24 22 30 22 19 59 10 | 56 40 48 72 40 61 65 50
R07 | 998 11 30 30 25 16 19 175 10 | 72 48 49 92 75 82 169 70
R08 | 1215 13 27 16 21 12 12 --- 7 | 63 39 46 71 57 62 --- 56
R09 | 2174 14 19 7 16 36 27 --- 10 | 48 59 49 53 46 56 --- 49
XR11 | 1959 11 --- 12 21 --- 23 --- 10 | 29 --- 29 38 --- 30 --- 28
R12 | 1187 20 24 17 17 11 21 --- 8 | 47 38 41 53 44 44 --- 42
R13 | 3307 34 67 35 42 62 32 --- 20 | 58 68 39 56 55 65 --- 49
R14 | 2301 19 16 8 13 20 20 --- 7 | 40 34 37 35 34 47 --- 36
R15 | 1500 9 10 17 11 15 15 105 6 | 44 42 38 47 46 50 39 43
R16 | 1632 31 42 18 23 19 18 --- 11 | 51 41 54 68 41 43 --- 45
R17 | 579 21 25 16 19 25 13 --- 9 | 56 42 45 55 49 49 --- 47
R18 | 1691 9 28 11 12 18 20 --- 7 | 70 59 63 63 75 70 --- 66
R19 | 1005 55 61 42 73 21 37 --- 22 | 60 32 29 90 38 46 --- 38
R20 | 912 57 76 72 78 56 53 --- 29 | 84 67 51 93 55 92 --- 62
R21 | 1181 16 34 28 22 24 16 67 10 | 59 43 45 63 64 50 46 52
R22 | 879 83 57 35 44 33 78 --- 26 | 50 66 112 109 94 148 --- 97
R24 | 1317 22 29 19 17 20 13 --- 9 | 59 44 50 55 46 48 --- 48
------+----------------------------------------------+------------------------------------------
RMS | 1496 33 39 31 33 29 29 129 |T 57 46 47 64 56 59 82 51
WRMS | 1496 24 34 27 23 24 29 129 |NE 57 46 47 64 56 59 82 51
MEDI | 1187 20 27 19 21 22 19 105 |MD 58 42 45 56 55 50 65 49
Table 3.2149.5 GPS week: 2149 Day: 5 MJD: 59292
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 | 2525 52 40 61 17 21 22 --- 17 | 77 34 35 51 55 59 --- 48
R02 | 1193 10 23 15 11 15 15 93 6 | 64 52 60 64 60 58 75 59
R03 | 1054 7 31 33 11 19 27 160 10 | 63 46 48 65 68 74 59 60
XR04 | 548 19 20 21 --- 15 14 --- 9 | 55 41 46 --- 49 43 --- 45
R05 | 462 22 31 30 31 19 30 56 12 | 46 31 55 67 48 35 27 44
R07 | 1136 12 23 31 15 14 30 149 9 | 64 49 40 67 58 70 148 57
R08 | 1931 18 25 16 10 11 34 --- 9 | 58 44 49 56 54 71 --- 54
R09 | 2162 21 27 18 15 30 14 --- 9 | 25 37 34 34 28 30 --- 26
XR11 | 1439 12 --- 15 13 --- 26 --- 10 | 18 --- 21 23 --- 33 --- 19
R12 | 1313 16 19 10 16 11 30 --- 8 | 45 56 52 52 42 39 --- 45
R13 | 2031 31 34 32 22 51 24 --- 14 | 52 40 38 57 62 33 --- 45
R14 | 1096 14 9 11 11 10 14 --- 5 | 37 34 36 41 38 31 --- 35
R15 | 1325 10 13 17 18 17 24 126 7 | 43 48 42 59 44 58 55 47
R16 | 1824 24 31 45 26 50 35 --- 16 | 53 82 46 61 72 76 --- 58
R17 | 564 20 27 16 14 18 14 --- 8 | 43 31 38 41 45 33 --- 37
R18 | 1442 10 30 8 12 17 17 --- 7 | 48 50 46 38 52 37 --- 43
R19 | 1794 41 62 35 29 33 32 --- 17 | 42 60 34 36 43 34 --- 30
R20 | 1004 59 80 66 58 57 53 --- 27 | 57 55 39 65 42 75 --- 45
R21 | 1662 11 32 26 19 28 11 52 10 | 52 39 44 54 60 44 21 48
R22 | 1525 75 26 37 46 48 48 --- 22 | 51 76 87 65 96 87 --- 72
R24 | 1262 17 39 21 13 16 14 --- 9 | 34 26 33 35 41 31 --- 30
------+----------------------------------------------+------------------------------------------
RMS | 1526 31 35 32 24 29 28 114 |T 48 46 43 51 52 50 64 45
WRMS | 1526 22 28 30 16 21 24 114 |NE 48 46 43 51 52 50 64 45
MEDI | 1325 18 27 21 15 18 24 93 |MD 51 44 42 54 49 43 55 45
Table 3.2149.6 GPS week: 2149 Day: 6 MJD: 59293
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 | 2367 56 30 57 18 16 20 --- 16 | 110 50 41 74 73 72 --- 66
R02 | 2244 17 20 8 10 10 16 70 6 | 75 54 63 65 66 73 53 65
R03 | 1060 13 24 30 11 16 17 196 8 | 81 51 51 80 76 85 70 71
XR04 | 455 19 26 29 --- 20 23 --- 12 | 72 44 48 --- 69 73 --- 60
R05 | 468 12 28 33 22 28 20 80 11 | 63 37 53 74 66 65 72 58
R07 | 816 24 23 18 16 17 16 112 8 | 87 56 56 80 75 81 90 71
R08 | 1416 22 22 16 12 31 17 --- 9 | 78 53 62 74 80 71 --- 68
R09 | 2790 11 18 9 12 22 12 --- 6 | 32 33 34 35 40 39 --- 33
XR11 | 986 17 --- 15 22 --- 20 --- 11 | 31 --- 35 47 --- 41 --- 37
R12 | 881 15 14 14 12 19 17 --- 7 | 63 61 57 57 49 57 --- 55
R13 | 5759 40 32 30 32 39 8 --- 14 | 72 65 47 59 79 62 --- 62
R14 | 716 18 14 13 11 14 14 --- 6 | 53 43 45 41 53 43 --- 45
R15 | 678 11 10 12 11 10 14 137 5 | 61 63 56 58 65 50 67 58
R16 | 1347 31 31 22 48 56 31 --- 17 | 61 70 57 65 65 66 --- 59
R17 | 914 20 28 18 11 17 19 --- 8 | 63 39 42 57 50 58 --- 50
R18 | 897 14 31 12 14 19 17 --- 8 | 51 36 50 64 72 68 --- 56
R19 | 1456 30 39 17 28 26 22 --- 12 | 42 33 31 48 45 30 --- 30
R20 | 638 48 66 67 103 59 26 --- 29 | 90 55 41 111 53 80 --- 61
R21 | 861 17 36 34 12 25 23 78 11 | 80 56 51 73 77 79 46 68
R22 | 1409 67 21 37 43 42 35 --- 19 | 70 97 135 120 121 143 --- 111
R24 | 1469 15 35 15 13 20 33 --- 10 | 61 35 37 53 46 60 --- 47
------+----------------------------------------------+------------------------------------------
RMS | 1895 30 30 29 32 29 21 120 |T 66 51 52 66 66 66 66 58
WRMS | 1895 22 26 23 13 24 21 120 |NE 66 51 52 66 66 66 66 58
MEDI | 986 18 26 18 13 20 19 80 |MD 63 51 50 64 66 66 67 59
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