[IGSREPORT-27885] Wk 2152 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 23 06:28:02 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2152 (Apr 04, 2021 - Apr 10, 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 2.2152.
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:
igl2152[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2152 in the SP3 format.
igl21527.sum Combination Report for GPS Week 2152.
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 | -1.0 ns
1 | -9.9 ns
2 | -7.6 ns
3 | -7.6 ns
4 | -7.9 ns
5 | -9.4 ns
6 | -8.3 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 1.2152, 1a.2152).
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 2.2152.0-6)
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 3.2152.0-6).
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 2152 summary. (Apr 04, 2021 - Apr 10, 2021)
Table 1.2152.a GPS week : 2152 MJD: 59308.0-59314.0
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 3 19 -3 17 -.49 24 18 | 998 80 3494 8351
| 1 0 1 10 9 20 .04 | 3962 2079
emx n/a| 0 0 -1 -47 -34 -52 .07 32 27 | -10166 379 3527 8956
| 0 1 3 11 25 27 .03 | 10495 1436
esx n/a| 0 0 -1 8 -16 -48 .12 31 23 | -4156 122 3490 8281
| 1 0 2 28 19 18 .04 | 9461 1942
gfz n/a| 0 0 0 -5 1 -69 .13 30 16 | 0 12 3523 8129
| 1 1 2 17 17 36 .04 | 0 2170
grg n/a| 0 0 -2 -20 19 7 .49 30 23 | -7489 -45 3538 7973
| 1 1 3 9 21 65 .05 | 3339 2115
iac n/a| -1 0 1 39 15 141 -.07 29 23 | -5323 -124 3493 8814
| 1 1 2 30 35 55 .03 | 3528 1032
mcc n/a| 1 0 -23 45 -54 -271 -.27 127 127 | --- --- --- ---
| 5 6 14 22 56 307 .30 | --- ---
Table 1.2152.b GPS week : 2152 MJD: 59308.0-59314.0
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 | 15 17 17 18 15 17 18 |
R02 | 7 6 7 8 8 7 10 |
R03 | 9 9 8 8 7 6 8 |
R04 | 8 10 12 9 7 9 12 |
R05 | 9 10 12 9 10 8 9 |
R07 | 10 7 6 8 9 8 10 |
R08 | 8 9 9 9 7 9 8 |
R09 | 12 11 11 11 9 9 13 |
R11 | 14 10 8 12 14 11 10 |
R12 | 10 9 9 10 10 11 11 |
R13 | 18 20 19 16 17 19 25 |
R14 | 8 8 7 6 7 8 10 |
R15 | 10 9 9 9 9 7 10 |
R16 | 13 18 15 11 13 14 14 |
R17 | 7 8 8 7 7 8 9 |
R18 | 7 8 8 6 7 7 9 |
R19 | 22 18 18 18 22 20 18 |
R20 | 24 25 28 23 22 24 25 |
R21 | 10 10 8 8 8 8 7 |
R22 | 25 22 24 24 24 32 23 |
R24 | 8 9 8 8 8 9 9 |
Table 1.2152.c GPS week : 2152 MJD: 59308.0-59314.0
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 2152 0 | -66 14 284 662 -544 4281 82.1 1803 1803 | -1038 0
brd 2152 1 | -75 3 345 668 -1081 6952 85.2 1579 1579 | -9929 0
brd 2152 2 | -5 64 218 -722 -812 8668 82.2 1404 1404 | -7615 0
brd 2152 3 | 58 58 166 -1223 849 5924 81.4 1498 1498 | -7591 0
brd 2152 4 | 10 -96 39 -1095 1111 6536 83.5 1423 1423 | -7858 0
brd 2152 5 | 17 87 124 -713 2529 6157 84.6 1454 1454 | -9446 0
brd 2152 6 | -30 0 127 623 2475 4245 81.7 1585 1585 | -8340 0
-------------+------------------------------------------------------------+----------------
brd 2152 mean| -13 18 186 -257 646 6109 82.9 1535 1535 | -7402 0
brd 2152 sdev| 47 60 104 869 1509 1543 1.5 137 137 | 2950 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 2.2152.0 GPS week: 2152 Day: 0 MJD: 59308
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 -2 2 8 -7 4 -.51 29 20 | 9635 -1715 3390 9130
emx n/a| -2 -2 -4 -59 -9 -50 .11 34 28 | -12492 -832 3449 9675
esx n/a| -1 0 -3 14 -42 -60 .07 28 22 | 10035 -1316 3382 10873
gfz n/a| 0 4 2 -2 -26 -90 .10 27 14 | 0 -1521 3441 8882
grg n/a| 2 -1 4 -32 41 120 .45 28 23 | -31 -2119 3451 8589
iac n/a| 0 -1 0 62 40 107 -.11 33 24 | 2159 -1890 3386 9553
mcc n/a| -5 -9 -11 83 -55 -224 -.37 121 121 | --- --- --- ---
Table 2.2152.1 GPS week: 2152 Day: 1 MJD: 59309
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 9 -10 -14 -.52 26 20 | -971 -3058 3680 7934
emx n/a| 0 1 -2 -49 -7 -85 .03 33 29 | 4024 -1790 3761 8600
esx n/a| 0 0 -4 28 -6 -41 .06 30 24 | -7564 -2818 3671 6013
gfz n/a| 1 0 1 -14 -14 -32 .12 30 15 | 0 -3313 3733 7735
grg n/a| 2 0 -1 -23 44 -2 .55 32 23 | -8606 -2877 3748 7590
iac n/a| -1 0 0 67 1 133 -.11 28 21 | -8725 443 3660 8415
mcc n/a| 6 -7 0 70 -154 -568 -.66 124 124 | --- --- --- ---
Table 2.2152.2 GPS week: 2152 Day: 2 MJD: 59310
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 0 16 5 5 -.50 21 17 | -2305 871 3608 7358
emx n/a| 0 0 -5 -51 -45 -79 .10 30 24 | -14759 681 3603 7946
esx n/a| 0 -1 0 48 -17 -47 .18 30 25 | -5533 529 3618 6765
gfz n/a| 1 1 3 16 1 -73 .18 34 14 | 0 550 3624 6926
grg n/a| 0 1 0 -14 33 -8 .49 34 22 | -8169 973 3626 7040
iac n/a| 1 -1 3 -11 48 252 -.07 32 24 | -6518 833 3611 7823
mcc n/a| 8 4 -20 23 -9 -305 .28 141 141 | --- --- --- ---
Table 2.2152.3 GPS week: 2152 Day: 3 MJD: 59311
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 2 24 -15 25 -.42 22 15 | -624 1473 3405 8228
emx n/a| 0 0 0 -61 -66 -43 .09 32 28 | -3405 902 3494 8871
esx n/a| 0 0 -2 1 -26 -22 .16 30 22 | 1985 485 3396 7952
gfz n/a| 0 0 0 -9 9 -11 .14 31 16 | 0 1003 3456 7952
grg n/a| 0 0 -3 -21 0 -85 .53 30 22 | -8086 683 3468 8106
iac n/a| -2 1 5 40 60 70 -.08 24 24 | -5031 -840 3432 8656
mcc n/a| -3 1 -42 41 -28 -344 -.18 161 161 | --- --- --- ---
Table 2.2152.4 GPS week: 2152 Day: 4 MJD: 59312
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 6 16 10 23 -.47 23 18 | 835 1093 3615 9060
emx n/a| 0 1 3 -39 -37 -4 .08 28 24 | -25394 1537 3694 9778
esx n/a| 0 0 -2 -11 -31 -75 .13 33 23 | -7314 1597 3629 8557
gfz n/a| 0 1 -2 -35 6 -82 .08 32 16 | 0 1879 3593 8957
grg n/a| 2 0 -8 -14 26 -38 .51 29 23 | -8728 1256 3683 8990
iac n/a| 0 1 2 70 -7 141 -.04 26 20 | -5557 -49 3630 9612
mcc n/a| 5 5 -26 26 8 315 -.28 117 117 | --- --- --- ---
Table 2.2152.5 GPS week: 2152 Day: 5 MJD: 59313
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 2 23 -4 39 -.48 21 17 | -468 -1023 3608 7532
emx n/a| -1 -1 -1 -38 -63 -41 .06 28 23 | -775 -250 3543 8275
esx n/a| 3 -1 0 19 15 -32 .09 31 23 | -409 -701 3589 6869
gfz n/a| 2 -1 0 13 7 -75 .12 24 14 | 0 -1380 3627 7166
grg n/a| 0 -1 -3 -29 -8 13 .42 29 24 | -8973 -1302 3673 7021
iac n/a| -3 2 2 20 2 139 -.06 27 22 | -7579 -440 3587 7972
mcc n/a| 0 -2 -34 33 -39 -165 -.48 110 110 | --- --- --- ---
Table 2.2152.6 GPS week: 2152 Day: 6 MJD: 59314
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 37 -3 40 -.53 23 20 | 884 2919 3154 9218
emx n/a| -1 0 1 -29 -8 -62 .04 35 32 | -18366 2408 3151 9547
esx n/a| 2 -1 2 -40 -9 -61 .13 34 25 | -20297 3084 3147 10941
gfz n/a| 1 1 0 -8 28 -120 .19 33 20 | 0 2868 3193 9289
grg n/a| -1 1 -1 -6 0 54 .46 31 24 | -9835 3070 3121 8475
iac n/a| -2 0 -3 25 -37 143 -.01 32 26 | -6014 1071 3145 9667
mcc n/a| 0 6 -28 41 -104 -610 -.20 117 117 | --- --- --- ---
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 3.2152.0 GPS week: 2152 Day: 0 MJD: 59308
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 | 2008 48 28 42 22 20 29 --- 15 | 92 53 29 72 61 58 --- 57
R02 | 1002 11 18 15 20 12 14 149 7 | 50 41 41 58 45 44 54 45
R03 | 794 12 17 30 9 27 17 102 9 | 75 61 56 76 88 77 26 71
XR04 | 991 14 12 23 --- 12 17 --- 8 | 90 81 72 --- 87 90 --- 83
R05 | 1483 22 21 18 18 20 14 85 8 | 65 56 69 68 75 78 48 67
R07 | 928 17 18 25 16 19 28 172 9 | 70 59 61 76 64 83 39 67
R08 | 648 14 19 10 17 23 19 --- 7 | 53 51 50 64 64 57 --- 54
R09 | 1644 25 24 16 19 45 25 --- 12 | 73 70 68 66 57 72 --- 63
XR11 | 1153 15 --- 26 15 --- 36 --- 13 | 27 --- 29 36 --- 45 --- 29
R12 | 1211 26 32 19 20 15 25 --- 10 | 96 71 79 96 86 88 --- 85
R13 | 4750 40 46 43 25 51 21 --- 17 | 108 87 73 109 105 105 --- 95
R14 | 1392 21 10 9 10 10 31 --- 7 | 67 52 55 59 56 43 --- 54
R15 | 1668 12 27 12 20 24 33 107 9 | 77 58 68 82 61 88 58 71
R16 | 1756 28 28 24 25 39 17 --- 12 | 54 61 71 60 81 64 --- 62
R17E | 786 13 21 12 14 14 21 --- 7 | 61 59 63 65 66 57 --- 61
R18E | 923 11 20 11 12 20 14 --- 6 | 39 39 41 43 46 41 --- 40
R19E | 569 42 71 50 44 22 54 --- 21 | 37 55 65 59 50 50 --- 39
R20E | 2040 42 66 53 67 34 48 --- 23 | 83 93 105 107 94 99 --- 89
R21E | 1153 18 25 16 16 25 29 81 9 | 34 40 47 44 49 43 80 40
R22E | 2448 60 56 43 48 40 82 --- 25 | 29 40 61 66 61 53 --- 39
R24E | 2189 13 28 16 15 20 15 --- 8 | 42 52 43 43 54 48 --- 44
------+----------------------------------------------+------------------------------------------
RMS | 1803 29 34 28 27 28 33 121 |T 62 58 59 67 67 65 50 59
WRMS | 1803 20 28 22 14 23 24 121 |NE 71 61 58 70 71 70 45 64
MEDI | 1211 18 24 19 18 20 25 102 |MD 65 56 61 65 61 58 48 61
Table 3.2152.1 GPS week: 2152 Day: 1 MJD: 59309
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 | 2139 53 44 49 20 14 21 --- 16 | 71 38 31 50 43 38 --- 40
R02 | 1098 14 13 21 10 10 10 93 6 | 33 32 32 35 38 36 25 32
R03 | 1291 9 18 31 19 23 10 119 8 | 49 46 41 62 59 52 22 50
XR04 | 1062 16 16 29 --- 11 19 --- 9 | 65 62 55 --- 66 69 --- 62
R05 | 1393 10 24 31 10 31 22 75 10 | 49 45 56 52 69 54 38 51
R07 | 849 14 16 18 14 14 22 223 7 | 47 38 41 48 44 41 28 42
R08 | 649 23 18 17 12 14 26 --- 8 | 35 37 31 38 32 44 --- 34
R09 | 2174 22 13 13 14 44 18 --- 10 | 76 65 63 71 61 71 --- 65
XR11 | 1769 12 --- 22 17 --- 13 --- 9 | 32 --- 40 40 --- 33 --- 34
R12 | 1485 21 26 20 18 12 17 --- 8 | 63 65 69 78 76 66 --- 68
R13 | 1541 42 49 60 33 49 23 --- 19 | 75 62 51 75 82 72 --- 67
R14 | 1173 22 14 15 14 18 18 --- 7 | 48 41 44 36 35 38 --- 38
R15 | 1208 14 20 24 6 15 32 106 8 | 54 46 43 50 48 61 33 49
R16 | 1656 25 35 12 30 73 38 --- 17 | 43 51 45 44 55 65 --- 46
R17E | 951 16 29 9 15 18 19 --- 8 | 64 62 60 54 64 55 --- 58
R18E | 1070 11 25 17 10 16 27 --- 8 | 27 28 35 39 39 38 --- 33
R19E | 1759 31 57 35 42 17 53 --- 18 | 33 42 70 65 47 46 --- 43
R20E | 1211 30 60 48 84 56 40 --- 25 | 61 72 79 85 96 70 --- 69
R21E | 1246 11 32 20 18 20 24 50 9 | 31 41 33 39 40 43 54 35
R22E | 2177 44 46 51 55 43 50 --- 22 | 18 51 60 52 50 38 --- 32
R24E | 3000 14 31 13 14 14 23 --- 8 | 36 39 33 36 39 44 --- 36
------+----------------------------------------------+------------------------------------------
RMS | 1578 25 33 30 30 32 28 124 |T 48 48 48 52 54 51 33 46
WRMS | 1578 20 29 24 15 23 21 124 |NE 52 48 45 52 54 52 29 48
MEDI | 1291 16 25 21 15 17 22 93 |MD 48 45 44 50 48 46 28 43
Table 3.2152.2 GPS week: 2152 Day: 2 MJD: 59310
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 | 1056 39 28 54 24 45 24 --- 16 | 67 46 35 59 29 55 --- 44
R02 | 1366 12 12 19 10 13 21 71 6 | 43 38 37 48 46 51 45 41
R03 | 628 15 14 26 8 17 16 99 7 | 57 42 43 53 60 47 22 49
XR04 | 1010 22 12 34 --- 20 28 --- 12 | 69 55 52 --- 57 75 --- 60
R05 | 993 13 21 44 14 15 38 71 11 | 49 35 43 52 52 73 48 45
R07 | 651 10 22 9 8 20 12 268 6 | 59 43 62 64 74 58 68 58
R08 | 735 21 22 19 14 19 25 --- 9 | 39 35 50 52 51 50 --- 44
R09 | 1700 11 21 12 14 50 24 --- 10 | 80 75 76 71 53 86 --- 71
XR11 | 1681 8 --- 17 13 --- 15 --- 7 | 25 --- 30 33 --- 32 --- 29
R12 | 1409 20 21 16 16 24 20 --- 8 | 73 63 62 65 53 76 --- 65
R13 | 1621 30 50 56 23 53 41 --- 19 | 90 77 62 78 90 97 --- 78
R14 | 1184 8 17 12 23 18 17 --- 7 | 47 44 44 64 50 52 --- 48
R15 | 1371 19 16 29 11 16 14 138 8 | 65 58 41 58 52 54 68 54
R16 | 549 20 28 16 25 57 52 --- 15 | 35 33 40 31 56 68 --- 39
R17E | 1326 15 24 14 17 17 21 --- 8 | 74 68 65 84 75 64 --- 72
R18E | 1316 12 17 11 16 15 27 --- 7 | 23 35 29 30 31 36 --- 26
R19E | 1249 32 40 27 41 39 54 --- 17 | 24 31 38 53 40 51 --- 26
R20E | 2153 33 65 49 99 62 41 --- 27 | 62 57 75 101 83 71 --- 63
R21E | 1100 10 28 16 13 20 22 89 8 | 18 23 29 27 33 38 75 23
R22E | 1133 34 48 51 80 44 58 --- 24 | 27 48 62 57 51 44 --- 28
R24E | 2974 11 24 17 17 19 19 --- 8 | 26 23 22 24 39 38 --- 25
------+----------------------------------------------+------------------------------------------
RMS | 1404 21 30 30 34 34 32 141 |T 50 46 47 55 53 57 54 47
WRMS | 1404 17 24 25 14 22 24 141 |NE 57 49 48 56 55 62 50 51
MEDI | 1249 15 22 19 16 20 24 89 |MD 49 43 43 53 52 54 48 45
Table 3.2152.3 GPS week: 2152 Day: 3 MJD: 59311
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 | 592 42 38 51 34 48 22 --- 18 | 69 64 41 57 40 64 --- 48
R02 | 2025 14 15 12 15 28 16 84 7 | 39 44 34 38 32 38 91 34
R03 | 615 7 15 18 15 27 19 106 7 | 62 55 53 74 81 54 28 61
XR04 | 1384 15 16 19 --- 16 17 --- 8 | 62 53 60 --- 52 68 --- 59
R05 | 1380 10 17 34 16 17 21 71 9 | 48 45 28 49 51 57 33 44
R07 | 1026 9 22 23 12 21 16 284 7 | 59 42 45 60 73 57 125 55
R08 | 834 16 26 25 22 11 10 --- 8 | 44 35 42 59 50 50 --- 45
R09 | 1523 11 11 23 14 49 19 --- 10 | 68 58 73 63 33 66 --- 57
XR11 | 1882 9 --- 23 11 --- 31 --- 11 | 26 --- 26 31 --- 45 --- 28
R12 | 921 20 32 19 31 14 18 --- 10 | 58 30 38 68 54 47 --- 48
R13 | 3052 37 46 43 33 28 20 --- 15 | 86 54 41 85 88 83 --- 71
R14 | 891 10 16 12 14 13 16 --- 6 | 48 39 39 51 49 45 --- 44
R15 | 1246 10 26 26 8 12 26 190 8 | 63 43 44 64 63 76 89 59
R16 | 591 13 29 17 22 45 18 --- 11 | 48 27 54 42 64 53 --- 46
R17E | 1368 8 23 9 15 17 19 --- 7 | 48 41 38 37 46 42 --- 40
R18E | 1011 15 13 12 12 14 16 --- 6 | 22 24 25 23 26 27 --- 21
R19E | 788 38 52 40 44 27 42 --- 18 | 38 63 57 64 45 52 --- 45
R20E | 3115 29 58 56 61 55 46 --- 22 | 34 33 70 77 52 44 --- 38
R21E | 839 13 24 15 13 15 19 121 7 | 24 30 29 33 39 48 148 31
R22E | 1049 40 55 50 78 45 41 --- 23 | 28 42 60 67 57 38 --- 33
R24E | 1987 10 28 15 15 16 22 --- 8 | 22 33 32 27 37 28 --- 23
------+----------------------------------------------+------------------------------------------
RMS | 1498 22 32 30 31 30 24 160 |T 47 42 44 53 51 51 85 44
WRMS | 1498 15 28 22 16 22 24 160 |NE 55 45 44 57 56 57 73 49
MEDI | 1049 13 24 23 15 17 19 106 |MD 48 42 41 57 50 50 89 45
Table 3.2152.4 GPS week: 2152 Day: 4 MJD: 59312
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 | 928 37 18 51 37 25 16 --- 14 | 67 52 46 54 64 54 --- 52
R02 | 2071 18 16 10 17 16 21 139 7 | 35 37 28 24 24 29 84 26
R03 | 584 12 11 26 16 13 13 88 7 | 52 55 36 63 56 49 33 51
XR04 | 1324 14 10 17 --- 11 16 --- 7 | 75 66 64 --- 65 58 --- 65
R05 | 907 16 25 33 18 14 24 99 10 | 56 49 51 52 58 69 54 54
R07 | 748 8 21 32 10 16 29 91 9 | 58 48 41 57 66 73 130 56
R08 | 1267 13 12 19 13 21 13 --- 7 | 40 35 36 35 39 39 --- 36
R09 | 2509 9 13 14 16 42 16 --- 9 | 58 55 64 61 58 66 --- 56
XR11 | 1748 12 --- 24 26 --- 29 --- 13 | 23 --- 30 33 --- 47 --- 29
R12 | 846 24 23 25 22 15 18 --- 9 | 70 65 61 85 75 79 --- 71
R13 | 965 30 37 63 33 42 22 --- 17 | 90 97 60 87 101 97 --- 86
R14 | 748 17 18 14 16 16 16 --- 7 | 43 37 39 39 40 29 --- 36
R15 | 1458 13 22 18 20 22 17 95 8 | 56 50 49 67 71 44 132 54
R16 | 770 25 28 18 36 39 25 --- 13 | 49 54 51 50 71 71 --- 54
R17E | 2093 13 22 11 16 15 14 --- 7 | 44 46 45 47 50 41 --- 44
R18E | 1033 11 16 17 15 17 16 --- 7 | 30 24 35 33 31 38 --- 29
R19E | 1335 42 57 48 58 28 51 --- 21 | 32 48 66 72 46 43 --- 38
R20E | 2727 32 49 47 68 51 45 --- 22 | 52 56 71 75 80 47 --- 53
R21E | 1038 12 24 14 19 15 18 166 7 | 19 27 32 30 25 27 74 22
R22E | 855 45 43 57 67 58 47 --- 23 | 35 48 96 103 69 59 --- 52
R24E | 1505 15 27 14 13 13 20 --- 8 | 33 35 38 35 40 41 --- 34
------+----------------------------------------------+------------------------------------------
RMS | 1422 23 28 33 32 29 26 117 |T 48 49 49 55 56 52 84 47
WRMS | 1422 18 24 23 16 22 20 117 |NE 55 53 46 54 60 57 86 51
MEDI | 1038 15 22 19 18 16 18 95 |MD 49 48 46 52 58 47 74 52
Table 3.2152.5 GPS week: 2152 Day: 5 MJD: 59313
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 | 914 35 21 67 20 36 25 --- 16 | 60 35 44 41 68 59 --- 45
R02 | 2360 15 9 13 12 17 19 106 6 | 36 36 34 28 37 25 38 31
R03 | 517 10 12 11 16 11 16 85 6 | 51 43 51 54 51 53 30 49
XR04 | 1075 20 15 17 --- 15 19 --- 8 | 68 64 59 --- 61 50 --- 60
R05 | 764 15 19 24 20 16 12 72 8 | 49 45 68 60 53 55 36 53
R07 | 1095 8 14 24 12 8 28 112 7 | 53 47 44 59 55 67 64 53
R08 | 1904 11 14 22 15 24 27 --- 8 | 39 36 34 48 39 55 --- 40
R09 | 1578 10 12 14 17 37 14 --- 8 | 74 69 77 85 55 68 --- 70
XR11 | 1301 17 --- 18 9 --- 26 --- 10 | 24 --- 34 29 --- 42 --- 30
R12 | 911 22 25 25 10 29 37 --- 11 | 69 59 72 68 60 83 --- 66
R13 | 1624 29 50 66 24 36 37 --- 18 | 76 96 63 97 85 92 --- 79
R14 | 783 17 21 11 13 14 18 --- 7 | 42 38 41 43 47 37 --- 40
R15 | 1351 18 18 16 11 11 16 103 7 | 49 41 41 41 50 38 77 42
R16 | 1191 23 29 22 31 50 24 --- 13 | 40 39 41 37 58 52 --- 40
R17E | 3354 9 25 14 14 18 17 --- 7 | 41 37 46 48 46 38 --- 40
R18E | 1280 8 16 15 14 23 18 --- 7 | 25 34 28 30 35 34 --- 28
R19E | 800 39 54 39 42 30 53 --- 19 | 40 54 65 79 60 64 --- 50
R20E | 985 42 54 47 67 58 46 --- 23 | 57 70 93 88 108 64 --- 74
R21E | 663 15 22 11 11 20 24 159 7 | 23 26 26 28 35 29 47 25
XR22E | 1088 61 --- 57 79 66 39 --- 31 | 28 --- 82 101 73 57 --- 48
R24E | 1105 11 31 15 18 18 15 --- 8 | 29 40 29 33 36 35 --- 31
------+----------------------------------------------+------------------------------------------
RMS | 1454 21 28 31 24 29 27 110 |T 46 47 51 54 55 52 48 47
WRMS | 1454 17 23 23 14 24 22 110 |NE 52 49 50 53 55 55 49 49
MEDI | 1095 17 21 18 15 20 24 103 |MD 42 41 44 48 53 53 38 45
Table 3.2152.6 GPS week: 2152 Day: 6 MJD: 59314
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 | 490 38 26 66 22 30 37 --- 17 | 85 50 47 72 54 84 --- 61
R02 | 2140 12 14 13 16 13 45 78 9 | 52 43 45 50 49 30 36 42
R03 | 727 10 16 15 17 19 23 87 7 | 72 62 60 77 78 61 34 68
XR04 | 693 23 15 33 --- 21 23 --- 12 | 89 80 77 --- 78 78 --- 80
R05 | 719 17 13 21 24 15 18 58 8 | 62 60 71 79 61 64 40 64
R07 | 1258 14 13 32 17 11 40 145 10 | 73 62 59 72 70 93 37 70
R08 | 1706 10 14 20 16 16 26 --- 7 | 53 44 44 52 49 63 --- 49
R09 | 1679 23 17 19 17 50 25 --- 12 | 83 67 78 72 55 78 --- 68
XR11 | 1468 14 --- 17 15 --- 25 --- 10 | 23 --- 30 40 --- 45 --- 31
R12 | 1327 17 38 28 13 12 31 --- 10 | 90 70 84 92 85 95 --- 84
R13 | 3668 27 78 65 45 59 54 --- 24 | 111 108 79 123 114 137 --- 106
R14 | 930 18 23 23 25 15 20 --- 9 | 62 48 65 69 57 56 --- 58
R15 | 1008 15 25 22 26 19 19 111 9 | 69 52 54 76 64 68 89 62
R16 | 2037 23 51 21 20 39 25 --- 14 | 65 54 55 65 72 69 --- 59
R17E | 2860 9 31 14 23 14 24 --- 8 | 61 65 62 63 68 58 --- 61
R18E | 1311 9 19 11 28 27 16 --- 8 | 31 44 42 48 43 49 --- 39
R19E | 793 27 55 34 52 33 40 --- 18 | 48 67 66 79 50 56 --- 54
R20E | 981 37 50 61 81 57 39 --- 25 | 85 105 133 137 95 96 --- 100
R21E | 708 16 18 11 13 17 13 177 6 | 25 31 32 36 40 33 40 30
R22E | 871 54 36 56 56 49 48 --- 22 | 37 42 95 87 91 70 --- 56
R24E | 749 13 35 12 21 18 13 --- 9 | 39 49 41 39 51 48 --- 42
------+----------------------------------------------+------------------------------------------
RMS | 1585 23 35 34 33 31 32 117 |T 62 60 62 71 66 68 46 61
WRMS | 1585 20 32 25 20 24 26 117 |NE 70 61 60 72 68 72 47 64
MEDI | 1008 17 23 21 21 19 25 87 |MD 62 54 60 72 61 64 37 61
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