[IGSREPORT-28261] Wk 2179 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 29 04:32:53 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2179 (Oct 10, 2021 - Oct 16, 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 2.2179.
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:
igl2179[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2179 in the SP3 format.
igl21797.sum Combination Report for GPS Week 2179.
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 | -3.3 ns
1 | -3.7 ns
2 | -4.2 ns
3 | -2.1 ns
4 | 0.2 ns
5 | -2.0 ns
6 | 0.5 ns
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2179, 1a.2179).
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 2.2179.0-6)
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 3.2179.0-6).
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 2179 summary. (Oct 10, 2021 - Oct 16, 2021)
Table 1.2179.a GPS week : 2179 MJD: 59497.0-59503.0
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 0 -10 7 29 .13 21 16 | 16652 -463 3501 8442
| 1 0 1 8 20 34 .03 | 1620 1929
emx n/a| 0 0 2 4 3 -13 -.11 33 28 | -6459 -553 3505 8771
| 1 1 2 16 23 37 .02 | 8202 1437
esx n/a| 0 1 1 6 -30 22 -.09 25 18 | -5702 -29 3491 8499
| 0 1 1 18 27 25 .05 | 8002 2018
gfz n/a| -1 1 1 12 -2 27 .04 32 18 | 0 -621 3529 8331
| 0 0 1 22 15 30 .06 | 0 1956
grg n/a| 0 -3 2 -3 14 -76 .22 30 22 | -1985 -430 3493 8022
| 0 2 2 14 14 49 .05 | 1167 1864
iac n/a| 0 -1 -6 -7 10 28 -.18 29 29 | 143 -321 3505 8903
| 3 3 3 43 44 91 .07 | 1054 1539
mcc n/a| 0 -1 14 63 -3 980 -.49 117 117 | --- --- --- ---
| 8 6 25 101 138 463 .32 | --- ---
Table 1.2179.b GPS week : 2179 MJD: 59497.0-59503.0
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 | 11 12 13 17 16 14 11 |
R02 | 8 6 8 6 6 8 5 |
R03 | 8 8 8 6 5 7 5 |
R04 | 7 8 13 9 8 8 10 |
R05 | 11 7 9 9 9 9 9 |
R07 | 7 9 8 7 7 6 7 |
R08 | 9 8 7 9 8 7 8 |
R09 | 8 9 8 7 9 8 7 |
R11 | 8 9 9 11 8 9 7 |
R12 | 10 11 11 9 9 9 11 |
R13 | 21 18 17 17 14 15 17 |
R14 | 8 9 8 8 9 7 8 |
R15 | 10 10 10 10 10 7 9 |
R16 | 19 16 15 16 15 16 15 |
R17 | 7 8 8 8 8 7 7 |
R18 | 9 8 10 9 10 7 8 |
R19 | 20 18 23 24 19 21 21 |
R20 | 24 26 21 20 19 20 20 |
R21 | 8 9 7 8 9 8 7 |
R22 | 24 28 25 25 20 22 22 |
R24 | 11 12 11 8 9 8 8 |
Table 1.2179.c GPS week : 2179 MJD: 59497.0-59503.0
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 2179 0 | 72 -36 57 591 -157 -8332 80.7 1650 1650 | -3294 0
brd 2179 1 | 41 17 -31 -769 -2443 -4865 80.9 14220 14220 | -3696 0
brd 2179 2 | -13 -25 -102 -2734 -1100 -8112 81.9 1515 1515 | -4231 0
brd 2179 3 | -114 -72 -67 -982 1718 -2961 81.2 1657 1657 | -2112 0
brd 2179 4 | 14 -12 0 364 1573 -1859 81.7 1430 1430 | 233 0
brd 2179 5 | -22 16 5 31 -490 1517 83.0 1389 1389 | -1952 0
brd 2179 6 | -21 -53 64 -702 -1200 2252 81.9 1643 1643 | 549 0
-------------+------------------------------------------------------------+----------------
brd 2179 mean| -6 -23 -10 -600 -299 -3194 81.6 3357 3357 | -2071 0
brd 2179 sdev| 59 33 61 1117 1509 4224 .8 4791 4791 | 1870 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 2.2179.0 GPS week: 2179 Day: 0 MJD: 59497
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -7 1 -42 .14 22 15 | 18765 -70 3552 8642
emx n/a| 0 -1 4 16 -2 35 -.10 33 33 | -11532 -782 3565 9025
esx n/a| 0 2 0 -16 -19 8 -.10 23 17 | -18465 656 3546 8507
gfz n/a| -2 0 4 -19 27 19 .07 32 23 | 0 -1170 3614 8683
grg n/a| 1 -1 2 15 10 -55 .15 37 25 | -3259 -411 3530 8022
iac n/a| -4 -9 -7 9 -6 111 -.11 38 38 | 123 -325 3554 9005
mcc n/a| -4 5 50 -23 247 727 -.27 103 103 | --- --- --- ---
Table 2.2179.1 GPS week: 2179 Day: 1 MJD: 59498
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 1 0 0 -8 2 31 .14 22 14 | 18514 -2720 3716 9250
emx n/a| 0 0 3 1 17 -18 -.08 30 29 | -1513 -2324 3702 9762
esx n/a| 0 0 1 27 -28 -4 -.10 29 21 | -6149 -1982 3712 9235
gfz n/a| -1 1 1 -8 -3 -23 .02 34 20 | 0 -1978 3675 9389
grg n/a| 0 -2 0 5 8 -76 .16 32 22 | -2455 -2490 3709 8799
iac n/a| 0 -2 -2 34 -4 159 -.23 32 32 | -656 -2267 3734 9709
mcc n/a| -10 -11 39 66 -23 1475 -.14 107 107 | --- --- --- ---
Table 2.2179.2 GPS week: 2179 Day: 2 MJD: 59499
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -12 -25 28 .11 27 16 | 17469 -3142 4152 7867
emx n/a| 0 0 3 -7 -6 -41 -.14 33 27 | -3899 -2312 4231 8154
esx n/a| 0 2 1 17 -30 46 -.17 26 19 | -11392 -2244 4134 7680
gfz n/a| -1 0 0 9 -24 44 .10 28 17 | 0 -3347 4153 7773
grg n/a| 0 -2 4 3 26 -91 .21 30 23 | -3198 -2705 4133 7502
iac n/a| -1 -2 -9 -42 38 26 -.08 32 32 | -673 -1905 4150 8278
mcc n/a| 1 5 2 177 -128 1547 -.40 131 131 | --- --- --- ---
Table 2.2179.3 GPS week: 2179 Day: 3 MJD: 59500
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 1 -1 40 66 .15 21 15 | 15416 995 3274 8249
emx n/a| 1 0 0 22 -15 -49 -.11 34 28 | -8095 122 3254 8584
esx n/a| 1 0 3 0 -55 -14 -.07 26 18 | -5144 671 3276 7321
gfz n/a| -1 3 0 22 2 -2 -.09 37 17 | 0 56 3351 8179
grg n/a| -1 -1 1 0 -5 -80 .27 30 23 | -2312 293 3277 7811
iac n/a| -2 0 -10 -64 2 56 -.15 30 30 | -1212 1815 3267 8769
mcc n/a| 11 1 -13 -87 42 240 -.96 127 127 | --- --- --- ---
Table 2.2179.4 GPS week: 2179 Day: 4 MJD: 59501
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 0 -23 17 32 .12 19 15 | 16208 256 3250 7737
emx n/a| -2 -2 4 -26 33 36 -.11 32 25 | -21579 -85 3235 8023
esx n/a| 0 1 3 28 19 34 -.09 23 17 | 6464 1082 3233 9820
gfz n/a| -1 1 4 40 -9 57 .03 33 18 | 0 683 3276 7442
grg n/a| 0 -5 0 -2 41 -171 .28 27 24 | -31 487 3249 7429
iac n/a| 2 2 -10 -47 -69 5 -.21 27 27 | 1197 1472 3253 8226
mcc n/a| 0 0 -15 145 -171 759 -.33 108 108 | --- --- --- ---
Table 2.2179.5 GPS week: 2179 Day: 5 MJD: 59502
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 -1 -18 22 56 .15 21 19 | 14546 -779 2695 8018
emx n/a| -2 1 2 13 -29 -7 -.10 34 28 | -1862 -251 2682 8317
esx n/a| 1 0 1 -7 -67 37 -.00 24 16 | 657 -1660 2680 6527
gfz n/a| 0 0 0 39 -3 42 .01 29 17 | 0 -1260 2722 8063
grg n/a| 0 -6 3 -21 9 -46 .23 27 19 | -1494 -894 2694 7684
iac n/a| 3 1 -1 15 63 -92 -.28 24 24 | 587 -709 2697 8443
mcc n/a| -9 -4 17 8 53 1217 -.44 108 108 | --- --- --- ---
Table 2.2179.6 GPS week: 2179 Day: 6 MJD: 59503
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 2 -1 -3 30 .08 18 15 | 15651 2215 3869 9336
emx n/a| -1 0 -2 11 29 -49 -.11 33 29 | 3264 1759 3868 9533
esx n/a| 0 3 0 -4 -34 46 -.08 26 19 | -5886 3269 3859 10408
gfz n/a| -1 1 0 4 -6 52 .10 33 13 | 0 2668 3912 8791
grg n/a| 1 -4 5 -25 13 -12 .24 26 17 | -1152 2710 3861 8912
iac n/a| 2 1 -5 44 47 -70 -.20 24 24 | 1635 -334 3881 9893
mcc n/a| 7 -8 19 158 -45 899 -.91 133 133 | --- --- --- ---
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 3.2179.0 GPS week: 2179 Day: 0 MJD: 59497
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 | 695 26 25 30 19 19 21 --- 11 | 102 85 62 87 85 81 --- 83
R02 | 835 6 13 7 19 13 40 105 7 | 57 51 56 46 59 72 56 56
R03 | 534 5 11 14 10 10 45 89 7 | 69 59 64 67 70 90 43 68
XR04 | 1539 15 13 17 --- 10 12 --- 7 | 72 68 56 --- 62 68 --- 64
R05 | 2165 27 16 27 19 17 37 60 11 | 67 60 58 56 55 60 61 56
R07 | 758 6 20 10 15 14 31 126 7 | 70 63 65 67 67 88 63 68
R08 | 763 15 19 18 12 21 31 --- 8 | 62 60 78 72 73 86 --- 70
R09 | 1974 14 15 17 17 23 22 --- 8 | 57 63 60 60 58 69 --- 59
R11 | 1803 15 16 8 16 29 17 --- 7 | 60 53 55 55 60 63 --- 56
R12 | 797 16 38 16 12 34 21 --- 10 | 84 54 72 80 105 84 --- 78
R13 | 2985 27 80 33 37 58 54 --- 21 | 93 58 59 92 99 96 --- 76
R14 | 743 11 30 15 16 18 23 --- 8 | 62 45 74 77 79 67 --- 66
R15 | 1844 7 30 20 17 22 36 113 9 | 83 62 68 88 97 103 43 81
R16 | 3253 20 51 13 59 68 32 --- 18 | 72 47 73 84 73 92 --- 70
R17E | 1615 8 26 9 10 17 25 --- 7 | 43 37 42 42 45 44 --- 41
R18E | 1038 10 25 9 15 23 43 --- 9 | 58 50 59 59 68 57 --- 57
R19E | 1663 40 36 27 64 28 66 --- 19 | 218 213 200 201 202 222 --- 206
R20E | 1036 43 36 38 52 95 51 --- 23 | 53 53 57 68 117 85 --- 57
R21E | 1054 9 29 10 20 19 25 115 8 | 65 60 63 69 70 74 77 65
R22E | 1554 46 35 53 64 52 69 --- 23 | 62 78 107 82 88 83 --- 75
R24E | 2193 15 37 14 39 23 21 --- 11 | 34 35 35 42 35 37 --- 31
------+----------------------------------------------+------------------------------------------
RMS | 1649 22 33 23 32 37 38 103 |T 73 64 69 74 79 81 57 70
WRMS | 1649 15 33 17 23 25 38 103 |NE 72 59 64 71 74 79 53 67
MEDI | 1539 15 26 16 17 22 31 105 |MD 65 59 62 68 70 81 56 66
Table 3.2179.1 GPS week: 2179 Day: 1 MJD: 59498
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 | 725 26 29 30 20 20 26 --- 11 | 73 61 50 73 56 52 --- 60
R02 | 1044 10 19 9 9 11 24 92 6 | 42 30 41 38 39 48 39 38
R03 | 808 5 12 16 11 14 40 105 8 | 52 42 45 50 57 62 38 50
XR04 | 880 13 10 18 --- 15 17 --- 7 | 46 44 33 --- 42 57 --- 43
R05 | 1542 13 15 19 15 10 18 72 7 | 45 37 44 43 44 42 58 40
R07 | 603 13 11 22 15 11 35 159 8 | 46 38 37 39 43 51 109 40
R08 | 1168 12 16 10 20 8 37 --- 8 | 42 40 39 53 45 62 --- 44
R09 | 2199 18 20 18 17 15 33 --- 9 | 43 51 44 47 50 45 --- 43
R11 | 940 15 13 9 17 24 32 --- 8 | 45 43 42 38 53 61 --- 44
R12 | 1298 10 39 22 14 33 17 --- 10 | 56 41 48 59 74 62 --- 54
R13 | 2284 17 48 46 31 56 33 --- 17 | 73 48 57 87 95 78 --- 70
R14 | 1042 11 28 18 22 25 22 --- 9 | 52 52 60 71 67 44 --- 55
R15 | 1563 7 28 27 13 30 21 105 9 | 64 48 50 70 84 75 44 64
R16 | 2628 20 42 34 38 51 29 --- 16 | 53 42 58 65 72 70 --- 56
R17E | 2189 9 33 13 15 17 20 --- 8 | 38 36 39 33 41 32 --- 35
R18E | 1545 10 17 12 21 23 25 --- 8 | 44 41 43 42 53 36 --- 41
R19E | 1845 33 46 38 47 40 38 --- 18 | 210 208 198 226 211 225 --- 210
R20E |63205 59 28 49 55 85 44 --- 25 | 36 53 62 109 124 85 --- 62
R21E | 1247 8 29 13 23 12 27 90 8 | 37 38 38 46 42 41 65 37
R22E | 1799 48 42 75 100 31 59 --- 28 | 41 54 95 83 46 49 --- 48
R24E | 1323 15 43 15 41 14 24 --- 12 | 24 33 35 47 36 32 --- 29
------+----------------------------------------------+------------------------------------------
RMS |14215 22 30 29 34 32 32 107 |T 55 51 55 65 65 62 58 55
WRMS |14215 14 29 21 20 22 32 107 |NE 52 44 46 56 58 57 57 50
MEDI | 1323 13 28 18 20 20 27 92 |MD 45 42 44 50 53 52 44 44
Table 3.2179.2 GPS week: 2179 Day: 2 MJD: 59499
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 | 525 38 25 31 21 28 29 --- 13 | 80 62 53 75 52 64 --- 63
R02 | 765 13 19 10 13 20 25 133 7 | 40 42 54 47 58 61 82 48
R03 | 518 10 13 12 11 11 40 141 8 | 55 42 46 54 52 72 47 52
XR04 | 644 19 18 21 --- 20 47 --- 13 | 56 50 45 --- 39 49 --- 45
R05 | 752 11 19 16 19 22 27 97 8 | 52 50 50 54 40 69 49 49
R07 | 871 15 12 20 15 15 26 200 8 | 55 44 43 45 42 57 154 46
R08 | 1631 13 18 10 22 9 22 --- 7 | 47 42 47 63 49 64 --- 51
R09 | 2414 15 9 18 21 22 19 --- 8 | 47 57 51 61 48 55 --- 51
R11 | 1434 18 24 16 17 22 17 --- 8 | 41 41 44 38 41 46 --- 39
R12 | 1730 9 29 24 11 42 23 --- 11 | 61 52 61 65 93 65 --- 64
R13 | 2183 31 41 49 25 34 39 --- 16 | 81 47 37 70 85 89 --- 64
XR14 | 1073 19 --- 13 13 16 20 --- 8 | 47 --- 57 65 69 64 --- 58
R15 | 1065 9 32 21 18 26 22 88 9 | 65 47 52 70 80 63 29 61
R16 | 1807 26 37 26 26 46 38 --- 14 | 46 32 54 63 77 76 --- 54
R17E | 2035 10 31 10 14 13 17 --- 7 | 40 41 40 38 45 59 --- 41
R18E | 1051 18 27 21 19 19 24 --- 9 | 45 44 50 40 53 45 --- 43
R19E | 1953 45 76 33 42 55 58 --- 23 | 132 123 134 146 149 131 --- 132
R20E | 2404 42 59 30 64 37 45 --- 21 | 43 46 56 64 62 42 --- 43
R21E | 784 10 24 14 16 11 22 93 7 | 43 38 45 50 52 49 70 45
R22E | 804 69 27 60 55 50 58 --- 25 | 52 50 98 110 78 69 --- 66
R24E | 1521 17 37 12 32 19 20 --- 10 | 42 32 36 44 43 39 --- 36
------+----------------------------------------------+------------------------------------------
RMS | 1514 27 33 26 28 30 32 131 |T 55 49 54 63 62 63 71 54
WRMS | 1514 16 27 19 17 23 32 131 |NE 55 46 49 59 58 63 72 53
MEDI | 1073 17 25 20 19 22 25 97 |MD 47 44 50 61 52 63 49 51
Table 3.2179.3 GPS week: 2179 Day: 3 MJD: 59500
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 | 514 45 29 42 27 18 41 --- 16 | 92 68 60 55 63 47 --- 62
R02 | 570 6 11 12 14 20 18 116 6 | 43 43 44 44 51 50 123 43
R03 | 971 5 9 12 15 13 25 135 6 | 52 46 55 46 53 55 40 50
XR04 | 680 13 14 11 --- 17 29 --- 8 | 47 50 52 --- 43 50 --- 46
R05 | 892 13 20 20 14 23 29 85 9 | 53 56 43 42 35 66 41 46
R07 | 1317 11 12 14 8 11 30 211 7 | 59 54 58 59 64 79 171 61
R08 | 1049 12 19 8 17 18 35 --- 8 | 52 50 52 61 55 78 --- 56
R09 | 2999 11 9 17 19 20 19 --- 7 | 35 38 43 46 30 49 --- 37
R11 | 1456 18 25 23 14 37 23 --- 10 | 24 26 39 24 38 32 --- 23
R12 | 1769 8 25 20 25 25 17 --- 9 | 53 36 44 68 73 51 --- 52
R13 | 1868 29 46 40 29 60 15 --- 17 | 83 46 48 61 95 63 --- 64
R14 | 897 10 29 17 19 19 14 --- 8 | 47 32 59 64 57 40 --- 49
R15 | 1059 12 31 20 11 28 24 60 9 | 69 52 57 68 88 71 35 67
R16 | 942 22 37 28 34 45 45 --- 15 | 47 40 59 62 51 85 --- 52
R17E | 2107 7 30 9 19 10 29 --- 8 | 45 42 43 45 50 39 --- 43
R18E | 1800 11 24 16 14 26 24 --- 8 | 50 48 60 54 52 61 --- 51
R19E | 1673 39 73 41 76 55 46 --- 24 | 147 144 141 170 144 165 --- 144
R20E | 3618 24 63 38 73 36 39 --- 20 | 44 37 54 77 65 46 --- 43
R21E | 940 12 27 15 13 18 24 98 8 | 87 88 90 86 98 74 70 86
R22E | 1206 39 53 57 96 34 41 --- 24 | 44 67 56 68 49 57 --- 39
R24E | 1805 13 24 13 22 12 18 --- 7 | 39 34 38 39 41 37 --- 36
------+----------------------------------------------+------------------------------------------
RMS | 1656 21 34 26 36 30 30 127 |T 57 52 56 61 61 61 80 54
WRMS | 1656 15 28 18 17 23 30 127 |NE 54 45 50 53 56 58 82 50
MEDI | 1206 12 25 17 19 20 25 98 |MD 50 46 54 59 53 55 41 50
Table 3.2179.4 GPS week: 2179 Day: 4 MJD: 59501
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 | 606 38 29 42 35 29 19 --- 15 | 74 61 64 58 62 73 --- 61
R02 | 630 8 11 14 20 12 13 67 5 | 39 36 32 28 35 39 58 34
R03 | 1089 7 15 9 11 15 13 153 5 | 48 39 43 49 53 49 24 46
XR04 | 552 10 14 12 --- 23 23 --- 8 | 51 51 64 --- 46 59 --- 52
R05 | 652 13 22 21 25 19 20 99 8 | 44 38 55 59 38 43 42 44
R07 | 895 10 13 9 19 16 22 159 6 | 63 49 53 45 61 71 108 56
R08 | 1267 15 17 12 23 14 25 --- 8 | 52 47 50 64 67 72 --- 56
R09 | 2560 14 12 9 20 29 28 --- 8 | 50 58 49 54 48 65 --- 51
R11 | 1599 15 20 22 7 23 12 --- 8 | 42 49 41 33 43 40 --- 37
R12 | 1338 10 36 18 19 12 17 --- 8 | 61 38 62 64 60 71 --- 58
R13 | 1202 36 29 23 34 28 38 --- 14 | 73 40 53 51 60 45 --- 50
R14 | 1328 12 25 21 13 27 17 --- 8 | 41 29 55 39 57 31 --- 40
R15 | 1012 12 32 20 18 26 21 60 9 | 67 49 55 75 87 66 32 65
R16 | 1383 23 40 30 44 44 29 --- 15 | 59 41 63 63 82 75 --- 61
R17E | 982 7 28 15 27 13 21 --- 8 | 55 51 53 61 56 50 --- 52
R18E | 1511 17 27 15 21 25 29 --- 9 | 40 36 42 45 62 36 --- 40
R19E | 917 21 76 31 56 37 39 --- 19 | 131 145 131 160 146 138 --- 137
R20E | 1894 24 64 32 61 38 41 --- 19 | 34 37 49 56 63 38 --- 35
R21E | 1126 14 28 17 18 18 29 63 9 | 58 56 55 50 68 50 60 54
R22E | 2469 27 22 43 75 49 41 --- 19 | 72 72 74 81 60 61 --- 63
R24E | 2001 7 24 16 21 19 28 --- 8 | 25 22 27 33 34 25 --- 23
------+----------------------------------------------+------------------------------------------
RMS | 1430 19 32 23 33 27 27 108 |T 56 49 55 58 61 57 54 53
WRMS | 1430 15 25 17 18 24 27 108 |NE 54 44 52 52 57 57 52 50
MEDI | 1202 14 25 18 21 23 23 67 |MD 52 47 53 54 60 50 42 52
Table 3.2179.5 GPS week: 2179 Day: 5 MJD: 59502
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 | 1712 35 18 43 23 25 24 --- 13 | 64 53 53 51 52 65 --- 51
R02 | 1047 11 16 14 29 12 20 100 8 | 35 38 32 25 31 39 36 30
R03 | 1052 6 12 11 13 14 31 150 7 | 43 40 50 40 39 50 38 42
XR04 | 567 11 14 12 --- 22 14 --- 7 | 46 45 38 --- 29 45 --- 39
R05 | 626 18 19 22 19 15 25 110 8 | 44 31 59 53 37 36 37 42
R07 | 628 12 11 11 15 12 20 97 6 | 53 50 48 41 50 50 60 47
R08 | 1289 11 11 9 23 13 16 --- 6 | 50 48 52 57 43 65 --- 51
R09 | 2326 19 15 12 20 17 21 --- 8 | 41 43 41 48 41 48 --- 41
XR11 | 2840 16 --- 19 12 19 17 --- 8 | 32 --- 40 36 38 36 --- 33
R12 | 1047 10 40 15 13 17 12 --- 8 | 52 29 48 48 52 53 --- 46
R13 | 1549 36 49 31 27 32 20 --- 15 | 55 29 40 46 41 44 --- 37
R14 | 1375 13 18 22 16 13 13 --- 7 | 31 23 43 27 35 35 --- 29
R15 | 1143 13 30 10 11 8 15 90 6 | 50 39 49 50 47 52 27 47
R16 | 1313 32 40 26 42 45 20 --- 15 | 52 35 56 77 84 46 --- 56
R17E | 972 9 20 12 17 11 18 --- 6 | 36 39 37 32 39 36 --- 35
R18E | 1805 11 22 19 16 11 17 --- 7 | 32 33 39 38 26 31 --- 30
R19E | 900 29 79 33 46 51 33 --- 20 | 139 123 141 151 154 140 --- 138
R20E | 999 35 49 38 54 41 47 --- 19 | 33 40 54 57 61 36 --- 34
R21E | 2147 13 29 14 12 19 16 85 7 | 66 71 72 67 69 75 39 68
R22E | 1886 32 51 51 64 57 30 --- 21 | 44 69 68 68 40 61 --- 50
R24E | 1030 15 26 11 22 14 23 --- 8 | 31 26 29 30 31 35 --- 26
------+----------------------------------------------+------------------------------------------
RMS | 1389 21 34 24 29 27 24 108 |T 49 45 51 52 49 51 39 46
WRMS | 1389 19 28 16 17 19 24 108 |NE 46 38 46 46 44 47 39 42
MEDI | 1143 13 20 15 19 17 20 97 |MD 44 39 48 48 41 46 37 42
Table 3.2179.6 GPS week: 2179 Day: 6 MJD: 59503
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 | 968 23 27 19 31 20 22 --- 10 | 101 89 76 78 81 84 --- 84
R02 | 779 9 13 11 8 12 16 166 5 | 57 52 49 50 51 60 88 52
R03 | 909 6 10 13 12 9 18 157 5 | 62 57 61 57 59 72 38 61
XR04 | 924 22 19 12 --- 16 25 --- 10 | 63 57 50 --- 47 49 --- 52
R05 | 986 20 22 17 16 13 29 128 9 | 59 51 55 56 43 40 52 49
R07 | 896 10 10 12 27 11 16 111 6 | 73 68 67 75 67 67 61 68
R08 | 933 12 9 10 17 18 28 --- 7 | 67 68 68 71 75 89 --- 71
R09 | 2379 15 16 11 13 18 15 --- 6 | 58 59 58 60 57 67 --- 58
R11 | 3726 14 15 9 12 19 20 --- 7 | 48 45 51 53 53 52 --- 49
R12 | 989 12 42 21 30 28 15 --- 11 | 78 49 66 89 95 86 --- 76
R13 | 2109 33 59 44 18 31 27 --- 16 | 90 42 55 74 87 77 --- 69
R14 | 634 11 26 17 18 14 16 --- 7 | 52 37 61 62 54 55 --- 52
R15 | 638 10 30 21 12 13 27 123 8 | 76 51 60 80 86 90 32 73
R16 | 955 24 31 36 45 39 23 --- 14 | 68 47 83 74 79 87 --- 72
R17E | 1781 10 21 13 17 13 18 --- 6 | 48 45 48 49 48 41 --- 45
R18E | 1164 12 28 21 18 11 15 --- 8 | 44 47 47 44 50 50 --- 44
R19E | 756 23 72 42 58 50 38 --- 20 | 159 153 155 175 164 154 --- 157
R20E | 924 22 53 39 75 38 42 --- 20 | 51 36 50 78 61 38 --- 42
R21E | 1548 9 29 12 16 12 19 99 7 | 61 60 63 65 68 71 80 63
R22E | 3596 38 34 57 69 63 31 --- 22 | 62 78 87 95 76 70 --- 68
R24E | 997 13 31 13 15 18 15 --- 7 | 33 33 35 39 38 30 --- 30
------+----------------------------------------------+------------------------------------------
RMS | 1643 18 33 26 33 26 24 133 |T 67 58 64 71 68 68 58 63
WRMS | 1643 15 29 19 13 17 24 133 |NE 68 55 61 67 66 69 54 63
MEDI | 968 13 27 17 17 18 20 123 |MD 62 51 60 65 61 67 52 61
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