[IGSREPORT-28318] Wk 2183 IGLOS Final Orbits
acc
acc at igs.org
Fri Nov 26 06:26:05 UTC 2021
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2183 (Nov 07, 2021 - Nov 13, 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 2.2183.
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:
igl2183[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2183 in the SP3 format.
igl21837.sum Combination Report for GPS Week 2183.
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 | -1.7 ns
1 | -1.3 ns
2 | -1.6 ns
3 | -1.3 ns
4 | -1.7 ns
5 | -0.4 ns
6 | -0.7 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 1.2183, 1a.2183).
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 2.2183.0-6)
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 3.2183.0-6).
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 2183 summary. (Nov 07, 2021 - Nov 13, 2021)
Table 1.2183.a GPS week : 2183 MJD: 59525.0-59531.0
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 2 -4 4 32 .10 25 20 | 13976 -302 3170 8314
| 1 1 0 12 17 20 .04 | 801 1219
emx n/a| 0 0 -10 -10 12 -13 .08 37 28 | 2179 -334 3176 8611
| 1 2 2 24 23 29 .02 | 8766 543
esx n/a| 0 2 0 -7 -33 27 -.10 32 22 | 463 -254 3167 8994
| 1 1 2 10 15 32 .05 | 10021 1551
gfz n/a| 0 1 0 -12 -10 -13 -.12 36 16 | 0 -64 3219 8150
| 1 1 3 21 18 29 .04 | 0 1172
grg n/a| 0 -5 3 17 3 -46 .18 30 21 | -1311 24 3170 7816
| 1 1 2 15 19 45 .10 | 845 1233
iac n/a| 1 -2 2 18 69 3 -.27 49 44 | 740 33 3180 8824
| 3 5 8 43 64 120 .12 | 602 551
mcc n/a| 6 0 -13 114 94 480 -.60 196 196 | --- --- --- ---
| 11 5 22 157 78 170 .36 | --- ---
Table 1.2183.b GPS week : 2183 MJD: 59525.0-59531.0
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 13 16 14 17 16 18 |
R02 | 7 8 8 8 8 8 7 |
R03 | 9 8 7 7 10 8 8 |
R04 | 11 10 8 8 10 9 8 |
R05 | 9 9 9 11 9 9 9 |
R07 | 8 7 10 8 7 7 9 |
R08 | 10 11 11 9 8 8 10 |
R09 | 9 10 7 8 10 8 8 |
R11 | 8 14 9 10 8 8 9 |
R12 | 12 10 10 10 8 9 8 |
R13 | 15 17 14 15 16 16 16 |
R14 | 10 12 10 10 10 11 8 |
R15 | 8 10 10 12 8 10 8 |
R16 | 16 14 16 16 17 14 15 |
R17 | 9 12 10 10 9 10 8 |
R18 | 12 10 10 10 10 10 9 |
R19 | 28 30 33 29 30 29 32 |
R20 | 20 23 28 27 28 24 23 |
R21 | 9 9 9 10 10 11 8 |
R22 | 31 27 27 35 33 34 31 |
R24 | 11 11 9 10 9 9 10 |
Table 1.2183.c GPS week : 2183 MJD: 59525.0-59531.0
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 2183 0 | 27 7 65 298 2139 4555 83.2 1853 1853 | -1689 0
brd 2183 1 | 9 -51 72 -468 1904 -5733 82.8 1646 1646 | -1300 0
brd 2183 2 | -26 -50 125 816 -1730 -8684 82.2 1731 1731 | -1612 0
brd 2183 3 | 5 72 -23 -568 -910 -3803 83.7 1761 1761 | -1320 0
brd 2183 4 | 33 -51 -53 284 -1109 -1271 84.2 1734 1734 | -1725 0
brd 2183 5 | 10 26 6 -1078 -786 -1038 82.3 1578 1578 | -394 0
brd 2183 6 | -55 8 99 -706 -2266 1871 82.8 1587 1587 | -724 0
-------------+------------------------------------------------------------+----------------
brd 2183 mean| 0 -5 41 -203 -394 -2014 83.0 1698 1698 | -1252 0
brd 2183 sdev| 31 47 66 677 1728 4495 .7 99 99 | 510 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 2.2183.0 GPS week: 2183 Day: 0 MJD: 59525
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 3 1 7 -13 54 .12 26 19 | 13697 -1105 3330 7445
emx n/a| 1 0 -9 -39 23 29 .08 34 29 | -4676 -650 3310 7682
esx n/a| 0 1 -2 -4 -22 51 -.02 27 20 | -5817 -723 3333 5704
gfz n/a| 0 0 -4 1 8 -1 -.09 35 15 | 0 -1308 3371 7071
grg n/a| -1 -5 5 24 -37 -90 .05 28 23 | -1227 -984 3329 7256
iac n/a| -2 1 18 42 174 -146 -.42 53 51 | -179 -1 3347 7947
mcc n/a| 5 -1 -31 76 165 356 -.16 214 214 | --- --- --- ---
Table 2.2183.1 GPS week: 2183 Day: 1 MJD: 59526
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 4 0 21 7 .15 26 19 | 12945 1843 3074 8114
emx n/a| -1 1 -9 -37 36 -21 .09 36 29 | -13594 744 3134 8627
esx n/a| 0 3 1 -28 -53 66 -.09 30 21 | -17436 2074 3059 10522
gfz n/a| 0 1 0 -2 13 15 -.09 32 15 | 0 1418 3131 7864
grg n/a| 0 -6 0 13 2 -31 .05 28 21 | -2335 1911 3040 7711
iac n/a| 0 -9 1 57 -32 -46 -.27 54 50 | 506 1136 3038 8744
mcc n/a| 13 -7 -29 311 73 503 -.48 233 233 | --- --- --- ---
Table 2.2183.2 GPS week: 2183 Day: 2 MJD: 59527
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 2 2 -2 23 .02 24 20 | 13146 262 2749 8891
emx n/a| 0 -2 -11 -13 19 -6 .09 33 24 | 11041 -110 2746 9169
esx n/a| 1 2 3 -6 -42 15 -.15 34 21 | -3288 -447 2752 9610
gfz n/a| -3 0 2 -30 -33 -20 -.16 35 18 | 0 108 2784 8791
grg n/a| 0 -4 0 44 10 19 .26 29 20 | -1660 -187 2759 7966
iac n/a| -3 -4 0 -32 116 -63 -.18 62 52 | 169 -135 2776 9462
mcc n/a| 0 -1 -30 194 88 309 -.51 258 258 | --- --- --- ---
Table 2.2183.3 GPS week: 2183 Day: 3 MJD: 59528
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 3 2 -6 37 .06 24 24 | 15177 101 3161 8164
emx n/a| 0 1 -13 -14 14 6 .08 37 29 | 7539 -607 3162 8479
esx n/a| -1 3 0 4 -40 24 -.09 30 20 | 3870 1363 3181 6850
gfz n/a| -1 -1 5 16 -32 1 -.15 39 16 | 0 1213 3251 8214
grg n/a| 1 -3 4 13 6 -46 .16 34 24 | -1896 1006 3200 7696
iac n/a| 5 -7 5 -40 57 47 -.08 48 42 | 1181 176 3184 8699
mcc n/a| 5 8 -16 140 139 601 -.65 159 159 | --- --- --- ---
Table 2.2183.4 GPS week: 2183 Day: 4 MJD: 59529
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 -6 22 60 .08 26 20 | 14565 -747 3468 7707
emx n/a| 0 -2 -12 -11 23 -8 .05 37 25 | 608 -833 3469 7905
esx n/a| 0 2 -1 -10 -21 39 -.13 35 26 | 7554 -948 3437 9316
gfz n/a| -2 3 1 -31 -13 3 -.18 38 18 | 0 -556 3502 7577
grg n/a| 0 -6 4 3 0 -2 .29 29 20 | -1420 -664 3426 7416
iac n/a| 6 4 4 74 56 -46 -.23 48 40 | 816 41 3487 8164
mcc n/a| -11 5 -16 0 -67 316 -.43 171 171 | --- --- --- ---
Table 2.2183.5 GPS week: 2183 Day: 5 MJD: 59530
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 1 -11 -14 34 .11 25 22 | 14445 -2028 3501 9738
emx n/a| 0 3 -12 27 8 -60 .09 39 30 | 8877 -679 3497 9951
esx n/a| -2 3 1 -6 -46 33 -.18 33 21 | 6464 -2626 3500 11146
gfz n/a| 0 2 -1 -41 -2 -18 -.07 38 14 | 0 -1634 3576 9506
grg n/a| 0 -6 6 21 23 -63 .27 27 19 | 309 -1599 3508 8911
iac n/a| 0 -3 -6 20 80 53 -.39 41 38 | 1254 -534 3508 10111
mcc n/a| 10 2 2 235 110 498 -.61 143 143 | --- --- --- ---
Table 2.2183.6 GPS week: 2183 Day: 6 MJD: 59531
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 2 -28 24 9 .13 25 20 | 13858 -446 2910 8140
emx n/a| -1 -1 -7 15 -37 -36 .12 44 29 | 5459 -209 2914 8469
esx n/a| 0 0 -2 -2 -11 -35 -.06 32 25 | 11899 -474 2908 9816
gfz n/a| 2 1 3 0 -16 -75 -.09 33 18 | 0 308 2923 8032
grg n/a| 0 -4 1 0 16 -109 .23 32 21 | -950 685 2928 7756
iac n/a| 0 0 -4 6 35 229 -.29 35 35 | 1438 -452 2923 8643
mcc n/a| 24 -6 29 -157 149 775 -1.32 191 191 | --- --- --- ---
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 3.2183.0 GPS week: 2183 Day: 0 MJD: 59525
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 | 822 45 24 34 27 29 65 --- 16 | 50 53 47 48 33 73 --- 39
R02 | 2791 9 9 12 10 10 43 233 6 | 24 24 23 24 24 46 86 20
R03 | 477 9 18 12 14 20 57 191 9 | 28 32 29 31 31 63 69 28
XR04 | 1167 12 13 15 --- 19 58 --- 11 | 27 27 24 --- 32 49 --- 24
R05 | 953 17 15 19 16 12 42 51 8 | 19 27 42 34 23 44 62 24
R07 | 545 11 8 16 18 12 48 123 8 | 34 36 44 38 33 38 150 35
R08 | 1099 15 19 25 16 21 47 --- 10 | 27 30 39 32 28 39 --- 28
R09E | 3862 13 20 10 15 19 56 --- 9 | 84 85 92 92 86 97 --- 87
R11E | 2890 15 19 12 17 17 36 --- 8 | 24 30 31 35 34 57 --- 28
R12E | 1197 16 36 16 12 35 50 --- 12 | 154 154 162 155 167 152 --- 157
R13E | 3114 23 44 23 36 30 64 --- 15 | 63 74 81 73 72 67 --- 67
R14E | 2407 10 29 18 17 29 37 --- 10 | 73 73 75 71 85 73 --- 73
R15E | 637 12 29 10 9 16 39 334 8 | 90 93 87 91 85 92 87 88
R16E | 826 28 32 30 45 32 62 --- 16 | 53 63 63 75 71 79 --- 59
R17 | 2226 13 35 10 12 20 39 --- 9 | 63 35 48 58 64 62 --- 53
R18 | 667 14 36 17 25 23 58 --- 12 | 55 34 63 47 68 88 --- 54
R19 | 652 41 66 43 96 50 81 --- 27 | 65 40 50 120 51 87 --- 55
R20 | 1162 56 65 38 32 28 37 --- 20 | 89 42 46 71 61 78 --- 57
R21 | 1241 17 27 18 10 17 34 234 8 | 69 43 61 57 60 84 67 59
R22 | 2597 52 44 76 88 64 77 --- 30 | 47 72 108 54 81 83 --- 57
R24 | 906 10 39 17 16 21 54 --- 11 | 67 43 53 57 64 92 --- 57
------+----------------------------------------------+------------------------------------------
RMS | 1853 26 34 27 35 28 53 214 |T 57 52 60 63 59 73 86 54
WRMS | 1853 19 29 20 15 23 51 214 |NE 47 38 48 51 46 66 86 42
MEDI | 1162 15 29 17 16 21 50 191 |MD 55 42 50 57 61 73 69 55
Table 3.2183.1 GPS week: 2183 Day: 1 MJD: 59526
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 | 829 31 22 26 18 30 55 --- 13 | 25 24 40 30 26 47 --- 21
R02 | 2033 8 11 11 13 8 58 366 7 | 17 23 23 29 23 46 172 18
R03 | 525 8 15 11 11 10 54 167 7 | 18 21 23 21 20 57 71 17
XR04 | 1413 7 12 17 --- 14 56 --- 10 | 13 15 19 --- 13 68 --- 12
R05 | 600 13 15 19 26 12 34 115 8 | 12 11 33 28 26 36 117 17
R07 | 789 10 14 8 13 19 32 111 6 | 21 25 30 30 23 43 86 24
R08 | 963 11 12 21 15 22 67 --- 10 | 17 18 30 22 19 59 --- 19
R09E | 4038 13 13 14 16 24 61 --- 10 | 55 58 62 62 64 62 --- 58
XR11E | 3159 17 --- 19 15 33 58 --- 13 | 27 --- 31 35 43 66 --- 29
R12E | 720 20 30 13 20 18 31 --- 9 | 152 148 147 145 153 140 --- 148
R13E | 1143 33 31 26 34 38 75 --- 16 | 37 36 44 65 60 44 --- 38
R14E | 1091 11 23 35 12 19 58 --- 11 | 72 78 77 74 77 101 --- 74
R15E | 506 16 26 19 19 20 45 333 10 | 98 98 99 99 105 94 117 98
R16E | 1341 25 21 31 35 26 50 --- 13 | 60 55 60 55 53 69 --- 52
R17 | 2097 12 34 17 19 14 67 --- 11 | 45 32 36 38 47 94 --- 41
R18 | 1154 14 27 33 19 12 27 --- 10 | 42 30 54 33 43 51 --- 38
R19 | 831 35 82 53 94 55 67 --- 29 | 46 30 58 89 64 66 --- 47
R20 | 1245 59 62 53 39 35 69 --- 23 | 47 36 34 39 43 69 --- 30
R21 | 625 18 32 15 11 14 24 171 8 | 46 33 38 39 43 51 57 38
R22 | 3392 53 70 63 57 59 63 --- 27 | 40 58 57 64 48 78 --- 41
R24 | 1790 14 34 13 18 24 45 --- 10 | 44 35 39 46 44 64 --- 40
------+----------------------------------------------+------------------------------------------
RMS | 1646 26 36 30 32 28 54 233 |T 44 43 49 52 49 66 103 42
WRMS | 1646 19 29 21 15 21 50 233 |NE 30 27 36 39 34 59 100 28
MEDI | 1143 14 23 19 18 20 56 167 |MD 42 32 39 39 43 64 86 38
Table 3.2183.2 GPS week: 2183 Day: 2 MJD: 59527
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 | 587 29 20 37 40 33 64 --- 15 | 36 37 24 23 27 78 --- 27
R02 | 2196 9 13 9 15 22 38 --- 7 | 21 24 22 21 18 43 --- 18
R03 | 642 5 7 11 17 15 35 132 6 | 19 21 24 24 23 26 77 18
XR04 | 1153 12 9 16 --- 12 43 --- 8 | 18 19 20 --- 18 49 --- 18
R05 | 632 19 8 23 21 9 51 188 9 | 19 23 36 27 18 39 186 18
R07 | 715 18 22 14 17 25 36 151 9 | 23 32 29 27 32 55 49 25
R08 | 1946 11 11 15 15 21 82 --- 11 | 26 30 29 22 36 85 --- 29
R09E | 4141 12 16 13 18 14 34 --- 7 | 27 34 30 33 29 53 --- 29
R11E | 2921 17 17 20 17 20 31 --- 8 | 22 30 37 29 35 30 --- 24
R12E | 758 15 29 18 20 14 39 --- 9 | 90 89 88 86 95 84 --- 88
R13E | 1283 26 33 33 30 31 34 --- 13 | 36 43 39 47 55 44 --- 36
R14E | 1365 7 27 23 20 19 53 --- 10 | 57 61 68 65 67 64 --- 60
R15E | 551 10 30 18 14 14 51 488 9 | 41 43 38 48 52 67 214 42
R16E | 1961 20 22 43 54 27 47 --- 15 | 39 41 64 70 48 45 --- 42
R17 | 2395 15 27 17 14 17 50 --- 9 | 46 28 39 48 40 79 --- 40
R18 | 754 10 24 28 17 19 38 --- 9 | 33 23 48 38 46 47 --- 35
R19 | 1024 44 78 61 86 70 140 --- 33 | 46 35 58 85 34 131 --- 38
R20 | 920 39 73 82 38 39 130 --- 27 | 79 33 54 78 82 140 --- 62
R21 | 1692 17 30 10 12 11 42 135 9 | 55 38 50 46 46 49 90 46
R22 | 1292 56 36 69 76 62 49 --- 27 | 29 61 89 36 91 53 --- 48
R24 | 1718 18 29 10 14 13 36 --- 8 | 50 30 40 39 41 49 --- 39
------+----------------------------------------------+------------------------------------------
RMS | 1730 24 33 34 35 29 62 258 |T 38 36 44 44 44 62 123 37
WRMS | 1730 20 24 21 18 20 52 258 |NE 35 31 40 39 39 65 100 32
MEDI | 1283 17 24 18 17 19 43 151 |MD 36 33 39 38 40 53 90 36
Table 3.2183.3 GPS week: 2183 Day: 3 MJD: 59528
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 | 662 29 41 19 22 27 57 --- 14 | 38 51 31 29 31 64 --- 29
R02 | 1220 9 14 11 26 16 35 117 8 | 24 29 25 20 25 42 274 21
R03 | 520 11 9 11 13 22 31 119 7 | 33 35 40 40 35 52 72 35
XR04 | 1176 13 11 13 --- 14 33 --- 8 | 29 28 28 --- 29 47 --- 28
R05 | 784 20 12 22 25 9 56 204 11 | 20 20 36 28 19 45 194 19
R07 | 1085 10 13 11 25 15 29 179 7 | 25 24 27 32 29 35 93 24
R08 | 1074 20 16 19 19 16 35 --- 9 | 25 26 36 41 29 50 --- 28
R09E | 3969 15 15 14 17 13 37 --- 8 | 26 31 34 34 29 39 --- 28
R11E | 3288 21 21 15 27 23 36 --- 10 | 22 26 36 32 37 40 --- 25
R12E | 1305 19 36 11 14 18 28 --- 9 | 85 79 76 83 86 79 --- 80
R13E | 1047 22 46 26 33 34 53 --- 15 | 37 37 42 48 44 56 --- 33
R14E | 970 11 33 14 21 21 34 --- 9 | 94 100 98 98 99 107 --- 96
R15E | 1093 7 35 15 30 21 50 217 11 | 67 68 67 77 65 102 291 68
R16E | 2740 26 32 26 25 43 73 --- 16 | 44 48 41 56 52 94 --- 45
R17 | 2343 16 25 15 15 13 49 --- 9 | 58 42 43 51 54 69 --- 49
R18 | 633 15 24 29 10 15 29 --- 9 | 36 25 53 34 46 50 --- 37
R19 | 1117 38 81 51 78 78 79 --- 29 | 47 36 45 87 51 104 --- 44
R20 | 811 50 77 75 58 37 47 --- 26 | 90 38 51 98 78 74 --- 64
R21 | 2321 15 30 9 11 20 48 50 9 | 63 38 53 54 69 46 95 54
R22 | 1015 51 40 71 116 91 78 --- 34 | 31 71 101 73 71 97 --- 52
R24 | 1901 18 32 17 14 18 29 --- 9 | 64 41 44 50 70 60 --- 53
------+----------------------------------------------+------------------------------------------
RMS | 1760 24 37 30 39 34 48 159 |T 45 42 47 53 49 64 169 43
WRMS | 1760 24 29 20 16 24 42 159 |NE 41 36 43 49 45 59 145 38
MEDI | 1093 18 30 15 22 20 37 119 |MD 37 37 42 48 46 56 95 37
Table 3.2183.4 GPS week: 2183 Day: 4 MJD: 59529
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 | 555 38 34 24 26 50 47 --- 16 | 35 53 42 42 37 54 --- 34
R02 | 2302 15 8 12 18 20 37 121 8 | 27 23 27 19 28 50 127 21
R03 | 1261 5 6 30 18 14 56 95 10 | 31 28 48 27 29 41 50 28
XR04 | 973 13 15 16 --- 17 41 --- 9 | 32 26 36 --- 25 35 --- 26
R05 | 1165 18 16 21 27 14 31 132 9 | 27 25 31 37 25 38 120 24
R07 | 1052 11 12 9 18 10 40 326 7 | 30 33 35 30 29 50 161 30
R08 | 1073 18 12 12 21 14 28 --- 7 | 28 30 33 37 42 53 --- 32
R09E | 3165 14 15 19 18 15 54 --- 9 | 24 27 38 30 30 53 --- 27
R11E | 3123 17 17 15 19 13 26 --- 7 | 25 33 32 29 32 34 --- 25
R12E | 1742 12 29 13 14 14 24 --- 7 | 53 41 53 51 49 56 --- 48
R13E | 2240 23 49 31 54 24 33 --- 16 | 55 56 50 86 60 42 --- 51
R14E | 1007 15 34 21 22 18 26 --- 10 | 73 71 66 73 81 66 --- 70
R15E | 2349 12 30 12 21 13 14 163 7 | 51 49 50 52 48 54 124 47
R16E | 2096 12 22 42 42 41 65 --- 16 | 37 41 38 40 46 82 --- 35
R17 | 1509 12 30 21 14 11 32 --- 8 | 53 35 44 50 54 66 --- 47
R18 | 545 22 21 26 15 18 30 --- 9 | 31 20 47 34 41 49 --- 33
R19 | 1093 41 88 50 73 66 99 --- 30 | 53 56 37 72 38 102 --- 40
R20 | 852 58 86 75 45 27 88 --- 28 | 87 38 56 67 61 113 --- 56
R21 | 1528 16 31 15 16 16 43 41 10 | 61 45 51 48 59 72 54 53
R22 | 1615 55 38 90 104 66 68 --- 32 | 36 56 112 75 53 81 --- 53
R24 | 1045 19 32 12 15 12 24 --- 8 | 55 31 44 37 49 46 --- 42
------+----------------------------------------------+------------------------------------------
RMS | 1733 26 37 35 38 29 48 171 |T 43 38 46 46 43 58 106 39
WRMS | 1733 20 25 26 18 20 40 171 |NE 41 35 45 44 40 60 102 37
MEDI | 1261 16 29 21 19 16 37 121 |MD 36 35 44 40 42 53 120 35
Table 3.2183.5 GPS week: 2183 Day: 5 MJD: 59530
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 | 656 35 32 36 30 32 44 --- 15 | 34 35 53 41 44 56 --- 37
R02 | 1586 17 19 14 14 17 32 262 8 | 24 34 31 25 29 29 89 23
R03 | 1379 12 20 14 14 10 42 90 8 | 27 28 33 26 25 42 40 25
XR04 | 1159 10 19 9 --- 18 30 --- 8 | 28 33 34 --- 24 42 --- 27
R05 | 1381 18 23 14 16 14 40 83 9 | 25 29 39 41 22 40 53 24
R07 | 1009 13 11 12 13 19 24 --- 7 | 36 34 40 42 34 37 --- 36
R08 | 1185 16 13 20 19 11 26 --- 7 | 41 40 46 47 40 59 --- 41
R09E | 3260 16 15 16 15 20 31 --- 8 | 33 41 40 43 42 42 --- 36
R11E | 1993 20 14 13 17 19 23 --- 8 | 19 23 29 31 36 32 --- 23
R12E | 891 11 31 15 11 14 34 --- 8 | 63 56 65 62 65 71 --- 62
R13E | 2486 24 47 36 44 24 44 --- 16 | 40 39 50 63 53 61 --- 42
R14E | 1402 16 37 18 22 15 39 --- 10 | 100 93 104 108 104 112 --- 102
R15E | 2978 13 32 11 15 15 42 112 9 | 63 55 56 59 60 57 142 57
R16E | 1447 17 25 32 28 37 52 --- 14 | 32 35 47 50 35 57 --- 34
R17 | 744 13 34 20 11 16 41 --- 10 | 46 28 32 36 51 64 --- 40
R18 | 574 19 30 21 12 15 38 --- 10 | 35 31 47 40 45 55 --- 38
R19 | 584 35 101 54 83 58 47 --- 28 | 60 58 42 80 64 54 --- 47
R20 | 1231 64 74 60 32 23 52 --- 23 | 72 28 46 49 40 78 --- 44
R21 | 681 12 40 17 13 17 44 80 10 | 52 38 44 48 55 65 63 48
R22 | 1575 38 42 92 122 62 70 --- 34 | 34 35 94 83 37 83 --- 44
R24 | 616 17 32 16 15 19 22 --- 9 | 50 38 52 40 42 47 --- 42
------+----------------------------------------------+------------------------------------------
RMS | 1577 25 39 33 38 27 41 143 |T 43 39 48 50 45 56 77 41
WRMS | 1577 22 30 21 14 19 38 143 |NE 40 34 45 46 39 53 61 36
MEDI | 1231 17 31 17 15 18 40 90 |MD 36 35 46 43 42 56 63 40
Table 3.2183.6 GPS week: 2183 Day: 6 MJD: 59531
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 | 1108 40 32 37 43 40 50 --- 18 | 63 58 62 60 50 67 --- 53
R02 | 2060 12 15 12 14 7 31 359 7 | 33 38 32 31 27 40 217 28
R03 | 822 13 16 10 12 12 33 102 7 | 41 37 42 36 35 54 56 38
XR04 | 1075 9 18 18 --- 19 15 --- 8 | 39 38 33 --- 30 31 --- 32
R05 | 958 18 17 14 20 28 23 119 9 | 36 37 37 35 34 30 70 30
R07 | 816 19 14 11 19 21 28 --- 8 | 51 53 49 45 50 54 --- 49
R08 | 841 17 15 18 31 19 33 --- 10 | 47 47 52 54 50 60 --- 48
R09E | 3276 14 13 12 17 17 29 --- 7 | 86 89 90 92 86 82 --- 86
R11E | 2209 18 20 24 11 17 28 --- 9 | 52 53 52 55 66 41 --- 51
R12E | 1607 11 27 17 13 15 25 --- 8 | 92 86 82 84 96 83 --- 86
R13E | 1905 19 50 34 51 24 39 --- 16 | 49 48 51 76 47 51 --- 46
R14E | 2312 14 25 21 8 15 20 --- 7 | 68 70 73 67 75 74 --- 70
R15E | 2693 9 32 13 15 16 26 136 8 | 64 50 63 66 63 64 137 59
R16E | 1524 15 36 30 52 21 38 --- 14 | 76 83 90 96 74 76 --- 77
R17 | 624 15 28 15 18 11 20 --- 8 | 79 58 63 76 77 73 --- 70
R18 | 613 8 30 22 19 27 15 --- 9 | 69 55 82 70 74 67 --- 69
R19 | 928 37 140 52 66 67 70 --- 32 | 95 52 60 114 79 119 --- 72
R20 | 580 54 72 64 37 16 51 --- 23 | 115 52 52 96 87 96 --- 78
R21 | 479 13 32 15 12 17 23 99 8 | 87 58 76 76 80 85 56 76
R22 | 1545 58 40 79 72 91 36 --- 30 | 68 84 139 71 94 75 --- 79
R24 | 755 9 39 18 18 20 33 --- 10 | 85 65 80 88 94 88 --- 82
------+----------------------------------------------+------------------------------------------
RMS | 1586 25 44 32 33 32 35 191 |T 66 57 64 69 65 67 107 60
WRMS | 1586 20 29 25 18 21 35 191 |NE 64 52 61 65 61 67 99 57
MEDI | 1075 15 28 18 18 19 29 119 |MD 68 53 62 70 74 67 70 69
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