[IGSREPORT-29925] Wk 2316 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 17 06:47:16 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2316 (May 26, 2024 - Jun 01, 2024)
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 2.2316.
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:
igl2316[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2316 in the SP3 format.
igl23167.sum Combination Report for GPS Week 2316.
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.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
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 | 5.7 ns
1 | 5.0 ns
2 | 3.1 ns
3 | 5.7 ns
4 | 5.5 ns
5 | 4.1 ns
6 | 7.9 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
2 | ALL | R25
3 | ALL | R25
4 | ALL | R25
5 | ALL | R25
6 | ALL | R25
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 1.2316, 1a.2316).
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 2.2316.0-6)
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 3.2316.0-6).
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 2316 summary. (May 26, 2024 - Jun 01, 2024)
Table 1.2316.a GPS week : 2316 MJD: 60456.0-60462.0
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| -2 0 3 -8 -10 13 .14 22 17 | 7380 -730 3499 19762
| 1 0 1 13 8 28 .03 | 1251 1170
esa n/a| -1 0 2 -4 -3 -4 -.10 33 23 | 3110 66 3229 7483
| 1 1 1 12 9 41 .03 | 3667 1373
gfz n/a| 0 0 3 9 0 0 -.06 18 14 | 0 -1095 3210 7103
| 1 0 2 17 11 44 .04 | 0 1482
grg n/a| 3 0 0 -28 5 -17 .40 29 24 | 9134 -1014 3501 19500
| 1 1 1 18 9 30 .06 | 2009 1369
iac n/a| 0 0 -4 8 -15 25 -.09 20 18 | 10853 -402 3501 21324
| 1 1 2 25 27 92 .07 | 1256 866
jgx n/a| 0 0 -7 26 28 -18 -.19 28 28 | 5387 -1032 3277 7432
| 1 1 2 24 9 37 .03 | 1197 1438
Table 1.2316.b GPS week : 2316 MJD: 60456.0-60462.0
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 18 17 16 18 16 20 |
R02 | 6 7 6 8 6 4 6 |
R03 | 7 6 7 8 8 7 8 |
R04 | 8 8 7 7 8 6 10 |
R05 | 6 7 8 6 8 7 8 |
R07 | 8 6 7 7 7 7 10 |
R08 | 9 7 9 6 7 7 9 |
R09 | 9 7 7 8 7 7 7 |
R11 | 7 8 6 6 6 5 7 |
R12 | 9 7 7 7 9 7 7 |
R13 | 20 16 11 15 14 14 20 |
R14 | 8 7 8 8 8 5 6 |
R15 | 6 6 7 7 8 9 7 |
R16 | 8 7 8 5 9 8 11 |
R17 | 6 6 8 7 7 9 7 |
R18 | 8 6 8 8 9 7 9 |
R19 | 22 20 17 19 19 17 25 |
R20 | 24 24 21 30 32 29 29 |
R21 | 8 7 8 7 8 6 8 |
R22 | 8 7 7 8 7 8 7 |
R24 | 9 10 8 8 10 8 7 |
R25 | 19 19 --- --- --- --- --- |
R26 | 31 36 33 28 33 36 15 |
Table 1.2316.c GPS week : 2316 MJD: 60456.0-60462.0
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 2316 0 | -4 -83 180 465 3440 2368 80.3 1821 1821 | 5731 0
brd 2316 1 | 32 45 143 303 -129 2925 81.4 1590 1590 | 4988 0
brd 2316 2 | 31 95 112 -1721 -219 1395 81.3 2013 2013 | 3127 0
brd 2316 3 | -143 35 258 -2253 -1747 3312 81.8 1954 1954 | 5665 0
brd 2316 4 | -43 -84 316 -345 541 -4426 80.3 1787 1787 | 5519 0
brd 2316 5 | 136 -10 308 262 2556 488 78.4 1507 1507 | 4114 0
brd 2316 6 | 4 88 326 516 2352 3549 79.6 1936 1936 | 7923 0
-------------+------------------------------------------------------------+----------------
brd 2316 mean| 1 12 235 -395 970 1373 80.4 1801 1801 | 5295 0
brd 2316 sdev| 84 74 88 1133 1858 2778 1.2 190 190 | 1498 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 2.2316.0 GPS week: 2316 Day: 0 MJD: 60456
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 4 3 -13 3 .14 22 17 | 6662 -648 3243 18777
esa n/a| 1 0 2 8 4 -1 -.08 34 27 | -2463 557 3070 7926
gfz n/a| 1 -1 4 0 16 0 -.09 18 14 | 0 -263 3020 6574
grg n/a| 3 -2 -1 -46 3 -38 .38 28 23 | 9050 -509 3196 18749
iac n/a| 0 2 -1 10 -64 80 -.17 28 27 | 10493 -1396 3273 20451
jgx n/a| 0 1 -8 19 37 -16 -.14 27 27 | 5637 -281 3088 6843
Table 2.2316.1 GPS week: 2316 Day: 1 MJD: 60457
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| -4 0 2 -31 -4 -45 .18 24 19 | 8184 1241 2938 18707
esa n/a| 0 0 4 -16 0 -75 -.10 35 27 | 365 2328 2748 6906
gfz n/a| 2 0 4 8 -13 -63 -.11 17 13 | 0 948 2731 7087
grg n/a| 4 2 0 -24 19 -1 .51 28 24 | 7678 1187 3031 18454
iac n/a| -2 0 -5 40 -10 174 -.04 19 18 | 11359 -8 3015 20516
jgx n/a| 0 0 -5 0 13 -7 -.19 22 22 | 6374 1231 2842 7571
Table 2.2316.2 GPS week: 2316 Day: 2 MJD: 60458
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 -6 -24 27 .12 20 17 | 6333 154 3943 19742
esa n/a| -2 1 0 14 0 -10 -.09 32 21 | 5212 1028 3780 8838
gfz n/a| 0 0 3 13 -11 -2 -.07 15 11 | 0 253 3734 8218
grg n/a| 3 1 0 0 0 -5 .42 27 31 | 6232 148 3930 19373
iac n/a| 0 0 -2 8 18 -38 -.01 18 17 | 8650 1020 3977 21506
jgx n/a| -1 0 -2 6 32 40 -.19 22 22 | 4710 117 3864 8564
Table 2.2316.3 GPS week: 2316 Day: 3 MJD: 60459
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 3 0 -4 40 .14 21 16 | 9501 -1757 3614 19909
esa n/a| -1 0 2 -6 -8 29 -.12 33 22 | 1129 -831 3332 7729
gfz n/a| 0 0 0 -15 -11 6 -.08 18 13 | 0 -2292 3337 7623
grg n/a| 3 -1 0 -28 8 -58 .41 25 16 | 9995 -1754 3575 19558
iac n/a| 0 0 -1 27 1 -17 -.08 20 17 | 12195 -1111 3646 21730
jgx n/a| 0 1 -7 19 23 -27 -.25 35 35 | 7097 -1820 3367 7826
Table 2.2316.4 GPS week: 2316 Day: 4 MJD: 60460
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 3 -13 -17 15 .16 22 18 | 8129 -459 3172 19673
esa n/a| -1 0 2 1 7 -36 -.09 37 23 | 8580 156 2967 7972
gfz n/a| -1 0 3 14 5 -42 -.05 20 16 | 0 -1064 2945 7213
grg n/a| 3 1 3 -13 -7 -42 .33 35 30 | 9440 -1253 3208 19261
iac n/a| 0 0 -6 -33 -18 33 -.08 18 17 | 11761 -665 3236 21501
jgx n/a| 1 1 -6 69 39 5 -.19 32 32 | 5859 -1368 2999 7493
Table 2.2316.5 GPS week: 2316 Day: 5 MJD: 60461
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 4 3 -7 31 .15 19 16 | 6067 -1689 3784 20428
esa n/a| -1 -2 2 -10 -10 50 -.05 34 21 | 4716 -1422 3360 7407
gfz n/a| 0 0 6 1 5 63 -.01 20 16 | 0 -3066 3358 7189
grg n/a| 4 -1 1 -51 13 32 .36 30 23 | 8837 -2529 3751 20110
iac n/a| 2 1 -6 -4 -17 -83 -.16 15 13 | 10665 -257 3864 22242
jgx n/a| 1 0 -9 50 31 -53 -.15 31 31 | 3694 -2398 3395 7613
Table 2.2316.6 GPS week: 2316 Day: 6 MJD: 60462
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 -16 -2 21 .09 24 17 | 6789 -1957 3804 21099
esa n/a| -2 0 1 -19 -20 12 -.14 29 21 | 4234 -1352 3351 5606
gfz n/a| 2 0 4 40 2 43 -.01 20 15 | 0 -2182 3345 5821
grg n/a| 1 -1 -1 -37 -2 -9 .41 27 18 | 12707 -2393 3818 21000
jgx n/a| 1 -2 -10 18 21 -74 -.21 26 26 | 4343 -2711 3390 6117
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 3.2316.0 GPS week: 2316 Day: 0 MJD: 60456
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 821 47 47 25 42 22 33 16 | 117 48 94 68 76 60 80
R02 | 1665 13 16 9 13 15 16 6 | 90 76 91 80 77 76 84
R03 | 755 8 15 17 11 20 16 6 | 90 74 93 85 83 73 85
R04 | 1117 16 16 9 12 32 13 7 | 82 75 71 68 67 60 71
R05 | 2218 15 9 10 15 17 16 6 | 77 68 69 62 63 57 67
R07 | 2416 15 17 18 16 33 9 8 | 86 69 69 87 81 71 77
R08 | 1918 15 17 13 13 36 15 8 | 83 78 95 98 97 79 89
R09 | 3173 21 27 17 12 28 10 8 | 31 44 45 35 41 34 36
R11 | 3007 14 20 15 12 17 11 6 | 37 41 41 37 29 37 35
R12 | 798 20 22 11 24 28 11 8 | 58 60 45 45 34 46 46
R13 | 1297 36 46 28 54 37 61 19 | 102 66 95 70 78 59 80
R14 | 1343 10 18 14 14 29 14 7 | 67 73 66 71 62 56 65
R15 | 2499 10 12 11 13 19 12 5 | 81 81 81 75 65 71 77
R16 | 978 7 28 13 11 34 15 8 | 77 73 82 71 75 65 73
XR17 | 905 8 18 8 8 19 --- 6 | 27 27 32 33 25 --- 28
R18 | 737 13 20 17 16 13 26 8 | 26 28 29 29 21 21 22
R19 | 1431 43 49 21 65 36 64 21 | 34 44 30 31 33 23 23
R20 | 1691 32 104 36 55 35 49 24 | 50 67 52 57 31 56 46
R21 | 845 10 18 14 22 23 18 7 | 29 29 36 33 24 26 29
R22 | 3055 20 12 24 14 18 8 8 | 57 57 54 58 31 54 55
R24 | 799 8 19 16 10 39 24 9 | 37 30 41 34 34 25 32
XR25 |14950 26 27 --- --- 24 --- 18 | 57 13 --- --- 52 --- 55
XR26 |17937 32 --- --- 24 72 --- 31 | 148 --- --- 141 79 --- 146
------+-----------------------------------------+-------------------------------------
RMS | 1820 22 34 18 28 28 27 |T 67 55 62 62 54 52 60
WRMS | 1820 17 27 14 23 27 27 |NE 67 55 62 62 54 52 60
MEDI | 1431 15 18 15 14 28 15 |MD 67 60 66 62 62 56 65
Table 3.2316.1 GPS week: 2316 Day: 1 MJD: 60457
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 803 51 60 25 39 25 42 17 | 84 42 72 54 63 48 60
R02 | 969 11 14 17 18 10 16 6 | 67 59 77 58 56 59 64
R03 | 1381 15 8 13 15 15 10 6 | 66 57 62 61 46 53 56
R04 | 1346 24 14 15 19 15 15 7 | 68 62 64 50 40 44 53
R05 | 1095 23 11 13 27 13 9 7 | 63 55 53 39 33 44 47
R07 | 1734 9 21 13 16 14 10 6 | 60 48 56 65 46 61 56
R08 | 1576 19 13 11 21 17 15 7 | 56 57 53 71 57 51 57
R09 | 3357 15 21 14 17 18 9 7 | 32 41 38 39 33 32 34
XR11 | 4190 13 16 12 20 16 --- 7 | 40 56 44 38 32 --- 40
R12 | 1107 12 32 15 17 8 11 7 | 45 61 40 39 28 45 40
XR13 | 935 19 45 29 43 25 --- 16 | 74 69 94 52 63 --- 74
R14 | 1210 7 17 16 13 18 11 6 | 63 61 60 59 51 53 57
R15 | 1889 14 15 10 10 10 16 5 | 60 56 55 57 43 51 53
R16 | 1213 20 17 10 11 13 20 7 | 60 56 56 57 43 43 51
XR17 | 996 11 17 8 11 10 --- 5 | 31 30 35 32 25 --- 29
R18 | 690 21 13 9 17 10 11 6 | 32 39 32 30 23 35 29
R19 | 2253 45 47 27 70 35 44 19 | 30 24 31 25 37 34 23
R20 | 1039 41 108 35 59 26 44 23 | 39 76 56 39 37 54 42
R21 | 775 17 15 10 17 20 13 7 | 29 36 31 40 27 36 31
R22 | 2621 15 12 18 13 20 13 7 | 59 61 54 63 36 57 55
R24 | 612 26 19 11 25 31 21 10 | 41 31 35 42 27 29 29
XR25 |12841 20 --- --- --- 17 --- 18 | 70 --- --- --- 52 --- 61
XR26 |17949 53 --- --- 34 58 --- 36 | 118 --- --- 120 79 --- 123
------+-----------------------------------------+-------------------------------------
RMS | 1589 24 35 17 28 19 22 |T 55 51 52 51 42 46 50
WRMS | 1589 19 27 13 24 18 22 |NE 55 51 52 51 42 46 50
MEDI | 1213 19 17 13 17 17 13 |MD 60 56 54 50 40 45 53
Table 3.2316.2 GPS week: 2316 Day: 2 MJD: 60458
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1409 47 62 22 33 19 39 16 | 88 28 66 71 66 60 64
R02 | 1342 9 13 7 17 11 16 5 | 75 74 78 84 71 72 76
R03 | 2075 10 14 15 17 17 19 7 | 73 70 79 72 72 61 72
R04 | 1059 16 9 7 24 15 17 6 | 76 64 71 67 62 59 68
R05 | 1468 15 8 17 24 20 13 7 | 57 54 62 44 37 56 51
R07 | 856 10 18 6 14 18 20 6 | 65 54 67 63 66 54 62
R08 | 927 17 25 6 28 14 24 8 | 64 56 71 92 63 80 70
R09 | 2600 16 22 12 11 17 13 6 | 30 37 35 33 27 33 31
R11 | 6572 11 14 10 15 16 13 6 | 18 25 24 29 27 25 21
R12 | 1205 8 24 10 9 20 19 7 | 34 47 37 38 21 29 32
R13 | 805 25 29 20 24 15 30 10 | 67 48 62 54 55 72 56
R14 | 675 13 20 17 21 17 10 7 | 54 61 47 47 51 50 51
R15 | 1007 12 10 7 30 11 15 6 | 66 64 65 61 56 58 62
R16 | 1474 23 21 10 15 21 12 7 | 65 59 53 55 41 59 54
XR17 | 922 8 15 14 15 21 --- 7 | 20 19 24 26 25 --- 20
R18 | 955 15 16 17 18 19 17 7 | 18 19 23 23 23 22 18
R19 | 1910 35 36 23 69 25 36 16 | 35 30 33 30 22 47 25
R20 | 1003 30 102 31 47 31 35 21 | 27 58 51 32 24 49 32
R21 | 760 9 17 10 21 23 19 7 | 23 24 25 26 23 24 22
R22 | 2260 13 11 8 24 16 17 6 | 66 68 65 63 42 67 66
R24 | 1100 18 17 13 11 13 27 7 | 30 23 23 25 20 23 21
XR26 |15091 35 --- --- 37 58 --- 32 | 139 --- --- 125 81 --- 137
------+-----------------------------------------+-------------------------------------
RMS | 2014 20 32 15 27 18 22 |T 53 46 50 52 43 50 49
WRMS | 2014 17 21 11 31 17 22 |NE 53 46 50 52 43 50 49
MEDI | 1100 15 17 12 21 17 17 |MD 57 54 53 47 41 54 51
Table 3.2316.3 GPS week: 2316 Day: 3 MJD: 60459
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2515 53 46 18 20 16 42 15 | 97 47 61 59 42 63 61
R02 | 1443 17 14 16 9 14 29 7 | 76 61 62 67 61 53 65
R03 | 1398 10 19 9 17 23 24 7 | 75 64 75 70 78 61 73
R04 | 917 10 8 12 14 16 27 6 | 66 63 71 64 56 53 63
R05 | 1437 13 12 9 11 10 19 5 | 57 48 51 53 41 44 50
R07 | 925 11 20 16 16 16 10 7 | 68 58 58 72 57 60 63
R08 | 1284 11 12 12 18 12 19 6 | 63 63 58 78 58 69 65
R09 | 1769 17 23 11 16 19 12 7 | 25 41 28 32 25 29 26
R11 | 5592 16 12 9 11 12 15 5 | 31 43 36 35 26 32 33
R12 | 822 8 22 18 12 14 18 7 | 49 57 49 49 38 41 46
R13 | 903 22 34 26 41 22 61 15 | 81 49 76 54 68 36 63
R14 | 1060 17 17 19 13 17 13 7 | 45 51 64 53 35 44 49
R15 | 1293 10 13 10 25 17 16 7 | 62 64 54 52 63 62 59
R16 | 1322 11 13 10 15 7 15 5 | 73 65 70 71 63 65 69
XR17 | 1069 6 17 12 14 13 --- 6 | 22 21 25 29 22 --- 19
R18 | 1376 14 23 9 20 15 24 7 | 20 23 23 28 20 25 18
R19 | 1602 41 40 28 63 32 54 19 | 44 34 31 39 32 45 31
R20 | 2453 33 116 49 54 47 98 29 | 38 42 47 34 37 44 31
R21 | 911 9 12 7 6 15 34 6 | 24 28 25 24 21 25 22
R22 | 2575 17 15 11 20 23 20 8 | 29 26 35 39 36 35 31
R24 | 1484 22 19 12 20 12 22 8 | 27 21 20 32 21 24 20
XR26 |14561 30 --- --- 30 51 --- 27 | 64 --- --- 81 76 --- 78
------+-----------------------------------------+-------------------------------------
RMS | 1954 21 33 18 25 20 35 |T 50 46 48 50 43 45 46
WRMS | 1954 16 22 13 16 17 35 |NE 50 46 48 50 43 45 46
MEDI | 1376 14 17 12 16 16 20 |MD 49 48 51 52 38 44 49
Table 3.2316.4 GPS week: 2316 Day: 4 MJD: 60460
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2799 42 51 31 42 20 52 17 | 81 45 80 51 31 58 58
R02 | 1534 7 14 13 16 14 16 6 | 60 56 55 57 45 67 58
R03 | 745 12 21 15 16 20 19 7 | 66 49 60 59 54 54 59
R04 | 744 23 11 14 14 15 26 8 | 71 65 58 57 52 56 60
R05 | 891 19 10 14 21 13 22 7 | 55 64 73 82 54 54 65
R07 | 1007 8 18 15 18 20 16 7 | 63 52 57 66 51 55 61
R08 | 1604 12 15 15 18 14 22 7 | 61 60 72 75 49 52 65
R09 | 1089 22 18 12 17 8 16 7 | 28 42 41 45 31 37 35
R11 | 3899 16 12 13 10 15 12 6 | 32 25 34 26 26 24 26
R12 | 1329 15 26 21 19 16 14 8 | 45 55 31 53 28 34 38
R13 | 837 33 27 31 33 21 46 14 | 77 55 49 65 45 51 58
R14 | 1143 12 20 13 29 21 15 8 | 51 58 52 70 30 42 48
R15 | 1507 9 20 16 20 23 10 7 | 61 65 66 72 35 58 58
R16 | 1084 11 24 18 30 16 13 8 | 65 59 71 49 47 61 60
XR17 | 707 8 12 17 11 15 --- 6 | 18 16 24 21 16 --- 16
R18 | 885 18 19 15 17 22 27 9 | 19 20 21 31 20 24 16
R19 | 3672 45 55 20 59 23 52 18 | 33 47 40 39 26 46 32
R20 | 1298 28 126 42 109 29 81 31 | 46 57 46 39 33 58 38
R21 | 809 10 17 21 10 15 33 8 | 19 18 28 24 16 26 17
R22 | 2606 13 13 15 20 12 17 6 | 56 62 49 60 50 58 57
R24 | 1085 31 23 19 22 9 26 9 | 28 24 32 35 16 19 20
XR26 |10459 41 --- --- 46 51 --- 33 | 120 --- --- 105 75 --- 121
------+-----------------------------------------+-------------------------------------
RMS | 1787 22 37 20 35 18 32 |T 51 47 49 53 37 46 47
WRMS | 1787 18 23 16 30 17 32 |NE 51 47 49 53 37 46 47
MEDI | 1089 15 19 15 19 16 19 |MD 55 55 49 53 34 52 57
Table 3.2316.5 GPS week: 2316 Day: 5 MJD: 60461
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1299 35 58 38 26 20 35 15 | 67 34 84 54 52 41 53
R02 | 1698 8 7 12 11 7 9 4 | 56 58 62 64 62 55 57
R03 | 606 5 14 22 13 10 20 6 | 52 50 65 54 66 48 51
R04 | 699 15 14 10 16 11 16 6 | 59 59 59 53 61 44 55
R05 | 600 10 15 14 16 18 22 7 | 52 47 56 51 67 40 52
R07 | 878 8 20 13 20 14 18 7 | 59 50 66 55 70 44 56
R08 | 2513 11 20 18 17 10 20 7 | 56 48 72 70 74 45 59
R09 | 1298 14 28 16 16 9 14 7 | 25 39 34 27 32 33 29
R11 | 2966 11 8 6 11 10 12 4 | 30 30 33 35 33 29 30
R12 | 1252 11 18 21 16 10 12 6 | 41 44 26 44 41 32 34
R13 | 1234 25 35 24 46 19 47 14 | 79 48 64 65 78 60 61
R14 | 719 9 19 7 7 12 11 5 | 52 59 54 55 43 49 49
R15 | 1360 19 19 13 24 19 25 9 | 64 63 66 73 56 51 57
R16 | 1578 14 30 18 26 12 14 8 | 65 72 77 61 69 56 65
XR17 | 793 12 17 16 16 22 --- 8 | 23 22 22 32 23 --- 21
R18 | 718 13 12 16 12 14 20 6 | 22 19 22 28 16 19 18
R19 | 1876 33 62 15 51 21 48 16 | 40 22 28 30 21 26 24
R20 | 2030 46 100 41 91 25 96 29 | 58 65 77 35 40 64 48
R21 | 986 8 11 13 9 13 22 6 | 23 16 21 23 26 16 18
R22 | 2036 15 8 21 23 12 16 7 | 67 61 63 69 43 64 62
R24 | 911 15 20 21 17 18 17 8 | 29 43 46 36 24 24 28
XR26 |10431 41 --- --- 53 56 --- 36 | 183 --- --- 190 108 --- 187
------+-----------------------------------------+-------------------------------------
RMS | 1507 19 34 20 30 15 31 |T 53 45 52 54 49 42 49
WRMS | 1507 16 21 16 23 13 31 |NE 53 45 52 54 49 42 49
MEDI | 1252 13 19 16 16 13 18 |MD 52 48 59 53 43 44 51
Table 3.2316.6 GPS week: 2316 Day: 6 MJD: 60462
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 738 48 51 28 31 33 19 | 102 33 83 59 48 63
R02 | 1908 7 13 14 12 12 6 | 81 74 81 82 70 77
R03 | 745 11 10 22 16 16 8 | 79 74 88 73 73 76
R04 | 768 21 19 26 11 15 9 | 77 71 59 69 60 65
R05 | 793 15 8 22 20 12 8 | 68 66 75 59 57 65
R07 | 1552 11 32 18 16 12 9 | 84 61 86 82 63 76
R08 | 1616 7 14 27 16 17 9 | 80 69 94 83 66 78
R09 | 2172 19 17 9 13 13 7 | 28 41 37 32 36 32
R11 | 1785 15 12 11 12 15 6 | 36 35 40 40 30 35
R12 | 1127 12 15 11 14 18 7 | 59 66 52 60 48 55
R13 | 1590 37 34 20 53 47 19 | 101 64 81 83 71 78
R14 | 1470 8 15 13 11 7 5 | 66 72 65 66 62 65
R15 | 1209 15 15 13 12 10 6 | 88 85 78 83 71 80
R16 | 1420 20 21 27 18 17 10 | 83 75 97 72 72 79
XR17 | 822 8 12 6 17 --- 6 | 30 31 31 36 --- 29
R18 | 638 17 18 21 17 17 9 | 24 22 28 28 21 22
R19 | 2437 37 62 26 63 50 24 | 38 48 49 55 37 36
R20 | 5918 54 75 28 61 64 29 | 61 51 71 55 60 53
R21 | 860 14 14 15 14 20 8 | 31 30 36 35 30 31
R22 | 1500 10 7 18 16 11 6 | 74 73 74 71 76 73
R24 | 1504 12 11 15 11 19 7 | 41 43 43 40 34 38
XR26 | 8361 14 --- --- 15 --- 14 | 207 --- --- 210 --- 210
------+------------------------------------+--------------------------------
RMS | 1936 24 29 20 27 26 |T 68 56 64 66 54 62
WRMS | 1936 17 21 15 18 26 |NE 68 56 64 66 54 62
MEDI | 1470 14 15 18 16 16 |MD 68 64 71 60 60 65
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