[IGSREPORT-30824] Wk 2406 IGLOS Final Orbits
acc
acc at igs.org
Fri Mar 6 02:17:27 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2406 (Feb 15, 2026 - Feb 21, 2026)
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 2.2406.
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:
igl2406[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2406 in the SP3 format.
igl24067.sum Combination Report for GPS Week 2406.
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.
Starting 02-Feb-2025 (GPS week 2352) the IGS Analysis Centers started using
the IGS realization of the updated ITRF2020-u2023, called IGb20. The combined
GLONASS orbits from this date are therefore in IGb20 frame.
Starting 11-Jan-2026 (GPS Week 2401, day 0, MJD 61051), all IGS products
are based on the IGS realization of the second yearly update of ITRF2020
called ITRF2020-u2024. This IGS realization is called IGc20.
For more information see IGSMAIL #8634.
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
Starting 28-Nov-2022, the absolute antenna model file has been updated to
igs20.atx to be consistent with IGS20.
See IGSMAIL #8238 and #8256 for more information
https://files.igs.org/pub/station/general/igs20.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 | 6.6 ns
1 | 5.2 ns
2 | 6.1 ns
3 | 6.3 ns
4 | 5.6 ns
5 | 6.7 ns
6 | 6.7 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
----+--------+---------------
0 | ESA | R06
1 | ESA | R06
2 | ESA | R06
3 | ESA | R06
4 | ESA | R06
5 | ESA | R06
6 | ESA | R06
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 1.2406, 1a.2406).
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 2.2406.0-6)
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 3.2406.0-6).
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 2406 summary. (Feb 15, 2026 - Feb 21, 2026)
Table 1.2406.a GPS week : 2406 MJD: 61086.0-61092.0
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| -1 0 -2 15 -10 -16 .13 16 15 | 2714 -1230 3558 9185
| 0 0 1 25 10 20 .03 | 1323 1420
esa n/a| -3 -1 0 -29 19 2 -.06 36 34 | 3760 -699 3605 9981
| 1 1 3 25 25 45 .04 | 630 1275
gfz n/a| -1 0 -2 12 11 8 -.17 17 16 | 0 -1249 3563 9188
| 1 0 1 26 14 20 .06 | 0 1663
grg n/a| 2 0 1 -13 -1 22 .26 17 15 | 6604 -1355 3615 9332
| 0 0 2 18 18 39 .04 | 823 1567
iac n/a| 0 0 -1 16 -4 -21 -.17 19 19 | 7974 -481 3745 10248
| 1 1 2 21 33 20 .03 | 460 1319
jgx n/a| 0 0 5 -18 -9 6 -.06 15 15 | 4758 -1571 3665 9761
| 0 1 2 15 24 28 .07 | 1217 1657
Table 1.2406.b GPS week : 2406 MJD: 61086.0-61092.0
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
------+------------------------------------+------------------------------------------
R02 | 7 6 8 7 9 7 8 |
R03 | 7 6 9 7 7 6 9 |
R04 | 6 7 7 7 6 6 7 |
R05 | 7 8 8 8 9 6 8 |
R06 | 30 30 35 41 41 34 34 |
R07 | 6 9 8 7 8 7 7 |
R08 | 10 9 9 8 9 10 10 |
R09 | 8 8 8 10 8 7 7 |
R11 | 6 6 7 6 9 6 6 |
R12 | 6 9 7 8 7 11 8 |
R14 | 7 6 9 6 7 7 7 |
R15 | 8 7 7 8 6 7 9 |
R16 | 8 11 9 9 10 9 10 |
R17 | 8 6 8 8 12 9 10 |
R18 | 9 7 6 7 10 8 9 |
R19 | 11 8 8 8 9 9 8 |
R20 | 11 11 10 10 13 12 13 |
R21 | 10 11 10 11 10 9 9 |
R22 | 12 10 8 11 9 8 7 |
R24 | 8 9 9 9 9 9 10 |
R26 | 27 27 27 29 27 34 47 |
R28 | 52 47 99 83 55 72 74 |
Table 1.2406.c GPS week : 2406 MJD: 61086.0-61092.0
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 2406 0 | 8 -4 14 -159 880 10280 79.9 1905 1905 | 6626 0
brd 2406 1 | 61 75 101 -349 1016 6731 77.9 1614 1614 | 5189 0
brd 2406 2 | -188 140 153 26 1244 4389 79.8 1572 1572 | 6137 0
brd 2406 3 | -55 -16 109 234 -1393 3867 78.9 1338 1338 | 6345 0
brd 2406 4 | -25 -58 16 1518 438 3464 81.0 1584 1584 | 5590 0
brd 2406 5 | -46 154 87 286 -680 3299 82.3 1782 1782 | 6673 0
brd 2406 6 | -96 13 88 -212 -1295 3690 79.5 1675 1675 | 6698 0
-------------+------------------------------------------------------------+----------------
brd 2406 mean| -48 43 81 191 30 5102 79.9 1638 1638 | 6179 0
brd 2406 sdev| 79 81 50 629 1127 2563 1.4 178 178 | 587 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 2.2406.0 GPS week: 2406 Day: 0 MJD: 61086
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 -3 37 -15 -46 .17 16 15 | 4173 635 3270 9885
esa n/a| -1 -3 0 -46 6 49 -.06 36 34 | 2998 556 3302 10905
gfz n/a| 1 0 -2 4 5 24 -.26 14 14 | 0 767 3265 9781
grg n/a| 1 0 2 -13 -19 52 .28 19 14 | 6402 69 3422 9995
iac n/a| -1 1 2 0 32 -45 -.19 20 21 | 7481 1977 3587 10480
jgx n/a| 0 1 2 4 -12 -15 .03 14 14 | 6110 352 3450 10604
Table 2.2406.1 GPS week: 2406 Day: 1 MJD: 61087
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 -1 20 0 -32 .12 15 14 | 4478 -2117 4636 10928
esa n/a| -3 0 4 -23 -29 -70 -.09 36 29 | 4385 -1410 4660 11745
gfz n/a| 0 0 0 15 25 16 -.17 17 16 | 0 -2057 4645 11035
grg n/a| 1 0 -1 -43 -24 45 .25 18 15 | 5770 -1713 4666 11270
iac n/a| 2 1 -3 51 0 -13 -.20 16 17 | 7997 -1174 4848 11464
jgx n/a| 0 2 6 -24 -12 28 -.01 16 16 | 6310 -2901 4878 11745
Table 2.2406.2 GPS week: 2406 Day: 2 MJD: 61088
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 6 -15 -5 .16 15 15 | 3228 -1350 3640 7678
esa n/a| -2 -3 0 -43 34 -38 -.05 39 36 | 3610 -520 3681 8111
gfz n/a| 0 0 0 13 -6 -12 -.13 16 15 | 0 -795 3637 7855
grg n/a| 1 0 2 7 2 67 .30 21 20 | 6110 -466 3635 7783
iac n/a| -1 0 -2 5 -19 -34 -.13 16 17 | 7931 -150 3667 8979
jgx n/a| 0 -1 3 -12 8 -3 -.01 13 13 | 4620 -538 3644 8222
Table 2.2406.3 GPS week: 2406 Day: 3 MJD: 61089
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 -4 -29 -8 0 .11 17 15 | 2606 646 3640 9069
esa n/a| -5 0 -1 6 35 -1 -.03 34 33 | 3352 1297 3693 9968
gfz n/a| -1 0 -2 67 -4 29 -.09 16 15 | 0 950 3651 8923
grg n/a| 3 0 4 -3 -8 -24 .22 15 15 | 6095 203 3449 8935
iac n/a| 0 -1 0 -11 40 12 -.19 17 19 | 8029 281 3717 10110
jgx n/a| 1 2 2 -3 1 1 -.08 15 15 | 5270 -12 3578 9735
Table 2.2406.4 GPS week: 2406 Day: 4 MJD: 61090
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 34 -28 -32 .16 16 16 | 2111 -2738 3214 9145
esa n/a| -3 -1 -2 -19 9 17 -.10 42 41 | 3242 -1923 3267 10151
gfz n/a| 0 1 -5 -10 10 25 -.17 19 17 | 0 -3146 3229 9176
grg n/a| 3 -1 0 -11 3 50 .28 16 14 | 6931 -3288 3362 9443
iac n/a| 0 0 0 30 2 -38 -.21 21 23 | 7359 -988 3296 10279
jgx n/a| 0 1 7 -22 13 -30 -.07 16 16 | 3752 -3584 3376 9777
Table 2.2406.5 GPS week: 2406 Day: 5 MJD: 61091
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 0 -1 -13 -12 .09 16 16 | 1042 -1042 3311 8464
esa n/a| -6 0 -4 -8 34 58 .01 33 33 | 4036 -728 3337 9720
gfz n/a| -4 0 -2 8 26 -4 -.22 18 18 | 0 -1428 3316 8440
grg n/a| 2 0 0 3 0 -24 .28 13 12 | 6667 -664 3449 8680
iac n/a| 0 2 -3 27 -52 -6 -.15 22 20 | 8688 -1977 3447 9748
jgx n/a| 1 0 7 -39 -9 11 -.13 14 14 | 2994 -980 3429 8893
Table 2.2406.6 GPS week: 2406 Day: 6 MJD: 61092
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 40 4 12 .08 15 15 | 1361 -2646 3199 9131
esa n/a| -2 0 -2 -68 44 3 -.11 34 34 | 4697 -2170 3295 9273
gfz n/a| -2 1 -3 -9 23 -19 -.13 18 15 | 0 -3040 3200 9110
grg n/a| 2 0 3 -32 33 -7 .20 14 13 | 8253 -3627 3327 9219
iac n/a| -2 0 -4 12 -34 -27 -.15 20 17 | 8339 -1341 3655 10682
jgx n/a| 0 0 7 -30 -59 55 -.14 19 19 | 4251 -3336 3306 9354
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 3.2406.0 GPS week: 2406 Day: 0 MJD: 61086
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 928 14 21 10 12 20 18 7 | 70 55 61 64 68 53 61
R03M | 4487 13 17 19 13 16 9 6 | 83 93 74 80 84 69 78
R04 | 2121 14 20 10 13 17 14 6 | 94 106 93 90 94 90 93
R05M | 3217 17 33 12 11 16 8 6 | 76 80 69 73 66 66 70
XR06M | 1037 36 694 20 --- 67 --- 30 | 31 231 46 --- 91 --- 48
R07 | 2364 8 34 14 7 10 10 6 | 76 80 69 75 73 72 73
R08 | 1479 19 51 21 16 19 19 10 | 49 85 56 63 65 54 57
R09 | 813 11 56 11 14 16 8 8 | 42 47 40 46 46 44 41
R11M | 2049 8 20 7 11 24 12 6 | 30 31 31 30 40 27 29
R12M | 1497 17 26 14 8 10 12 6 | 62 51 62 52 59 51 56
R14M | 1049 8 33 12 8 23 10 6 | 57 69 61 50 50 51 54
R15M | 612 18 23 18 19 13 9 7 | 73 81 63 65 61 59 64
R16 | 1663 17 55 11 11 16 11 8 | 80 66 77 75 65 71 72
XR17 | 1805 9 21 13 18 16 --- 7 | 82 69 85 72 80 --- 78
R18 | 1451 12 25 13 31 16 21 9 | 69 88 64 77 79 68 70
XR19E | 2124 15 26 25 --- 30 18 11 | 108 123 127 --- 105 110 113
R20E | 719 8 36 13 34 41 17 11 | 64 65 62 76 76 66 64
R21M | 981 29 40 13 17 14 20 9 | 130 108 116 119 123 115 119
R22 | 795 13 54 21 38 26 12 11 | 63 94 61 61 74 61 63
R24 | 1569 22 22 10 16 23 18 8 | 97 74 90 83 98 77 87
XR26 |14240 36 67 29 --- 64 --- 26 | 24 64 39 --- 75 --- 36
XR28E |16153 44 --- --- --- 62 --- 52 | 88 --- --- --- 92 --- 82
------+-----------------------------------------+-------------------------------------
RMS | 1904 16 36 14 19 20 14 |T 70 83 68 69 75 66 68
WRMS | 1904 15 34 14 14 21 14 |NE 67 77 67 71 74 67 67
MEDI | 1497 14 33 13 13 17 12 |MD 70 80 63 72 74 66 64
Table 3.2406.1 GPS week: 2406 Day: 1 MJD: 61087
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 681 16 14 13 11 13 15 6 | 39 45 33 40 43 33 37
R03M | 3008 12 18 8 13 11 15 5 | 54 61 53 57 47 46 51
R04 | 1204 11 26 9 15 21 5 6 | 69 76 70 63 68 65 67
R05M | 3437 17 35 14 9 14 18 7 | 47 49 40 44 36 35 39
XR06M | 1029 39 702 24 --- 56 --- 29 | 45 157 61 --- 60 --- 51
R07 | 1517 11 46 26 12 14 10 8 | 45 58 39 39 43 46 42
R08 | 1606 13 55 18 8 16 20 9 | 36 57 34 37 34 40 35
R09 | 1648 12 47 16 14 12 12 7 | 30 35 32 40 32 33 31
R11M | 1158 9 19 12 17 11 11 5 | 25 32 24 32 26 27 24
R12M | 1655 15 27 21 24 18 14 8 | 50 43 50 40 57 36 44
R14M | 1103 8 18 12 12 17 14 6 | 44 47 50 40 49 37 43
R15M | 746 13 23 27 10 8 11 7 | 56 64 43 62 55 51 52
R16 | 1537 28 55 24 14 9 17 10 | 53 52 41 42 44 39 41
XR17 | 1636 11 20 12 14 10 --- 6 | 47 43 49 49 47 --- 46
R18 | 1253 8 29 19 20 11 13 7 | 45 54 37 59 47 40 45
XR19E | 2103 12 23 21 --- 12 17 8 | 44 45 44 --- 40 36 39
R20E | 644 12 33 13 27 34 20 10 | 66 78 70 85 58 67 65
R21M | 662 22 53 9 24 18 23 10 | 82 83 70 61 83 56 70
R22 | 1446 11 44 25 26 16 14 9 | 38 61 35 56 48 47 41
R24 | 1068 15 20 15 23 19 22 8 | 58 52 60 58 63 49 56
XR26 |15201 42 56 29 --- 59 --- 27 | 51 43 48 --- 46 --- 40
XR28E |21834 44 --- --- --- 49 --- 47 | 81 --- --- --- 106 --- 87
------+-----------------------------------------+-------------------------------------
RMS | 1613 15 36 17 18 16 16 |T 50 58 46 50 51 43 47
WRMS | 1613 14 29 16 15 17 16 |NE 47 53 44 49 47 44 44
MEDI | 1446 12 29 16 14 14 14 |MD 47 52 44 44 47 40 43
Table 3.2406.2 GPS week: 2406 Day: 2 MJD: 61088
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1090 11 34 12 17 17 17 7 | 52 37 55 61 60 43 51
R03M | 2424 18 41 15 14 15 26 9 | 60 74 52 54 55 39 51
R04 | 1007 10 29 9 22 15 11 6 | 65 75 64 76 62 62 64
R05M | 2343 11 29 14 28 13 11 7 | 60 58 55 72 54 51 56
XR06M | 1103 38 684 37 --- 68 --- 35 | 54 110 42 --- 80 --- 54
R07 | 967 15 53 20 11 13 8 8 | 58 64 44 54 51 49 51
R08 | 1474 22 38 22 15 14 13 8 | 45 71 53 60 58 64 55
R09 | 1678 9 64 10 10 10 8 7 | 49 57 45 48 49 51 47
R11M | 1748 13 15 15 26 9 9 6 | 25 34 23 48 28 26 27
R12M | 1361 16 23 8 27 15 9 7 | 49 48 45 34 54 35 42
R14M | 1056 6 42 23 32 7 10 8 | 49 71 66 40 50 48 50
R15M | 919 17 34 15 9 8 16 7 | 50 50 40 50 46 39 43
R16 | 2669 21 46 19 12 16 9 8 | 53 35 41 44 39 41 40
XR17 | 1272 14 25 17 18 14 --- 8 | 71 49 64 58 69 --- 63
R18 | 807 8 29 12 13 13 10 5 | 57 70 49 56 61 51 54
XR19E | 2548 13 25 19 --- 9 15 7 | 47 52 58 --- 53 46 49
R20E | 708 12 27 20 22 35 15 10 | 53 54 45 50 67 56 52
R21M | 1421 14 46 19 28 20 14 9 | 86 88 80 92 92 91 86
R22 | 2036 10 49 19 18 13 8 7 | 46 69 42 52 51 54 48
R24 | 1085 21 29 14 32 14 15 9 | 87 74 89 78 81 77 81
XR26 |15040 35 81 34 --- 55 --- 27 | 24 51 28 --- 37 --- 20
XR28E |16205 96 --- --- --- 101 --- 99 | 62 --- --- --- 103 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1572 15 39 16 21 16 13 |T 54 61 51 57 59 51 51
WRMS | 1572 15 36 15 20 17 13 |NE 55 61 51 58 55 56 52
MEDI | 1361 14 34 17 18 14 11 |MD 53 58 49 54 54 49 51
Table 3.2406.3 GPS week: 2406 Day: 3 MJD: 61089
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1092 15 15 21 16 17 8 7 | 61 60 46 66 47 53 54
R03M | 1234 18 24 12 16 17 14 7 | 68 76 57 71 56 54 61
R04 | 1459 9 31 11 9 22 12 6 | 62 74 64 63 75 60 64
R05M | 1554 8 38 19 21 12 11 7 | 65 69 51 76 62 57 62
XR06M | 1170 35 658 42 --- 85 --- 40 | 118 149 114 --- 143 --- 120
R07 | 1113 12 43 8 14 13 11 7 | 63 59 70 76 69 57 65
R08 | 1868 18 26 19 14 14 16 7 | 43 61 46 55 56 58 51
R09 | 1378 10 61 23 12 12 16 9 | 18 28 37 33 29 26 24
R11M | 866 9 18 13 16 10 11 5 | 14 28 18 31 19 20 17
R12M | 1064 18 40 12 16 18 9 8 | 48 41 35 41 46 37 39
R14M | 1357 9 33 10 9 13 13 6 | 54 69 51 49 53 43 49
R15M | 852 14 27 19 12 21 13 7 | 55 61 54 49 36 40 46
R16 | 2415 21 55 14 11 14 13 9 | 59 26 48 50 41 40 44
XR17 | 936 13 21 11 19 9 --- 7 | 74 64 75 63 66 --- 68
R18 | 873 9 25 13 17 19 13 7 | 64 74 64 60 78 64 65
XR19E | 2192 15 32 11 --- 13 10 7 | 38 51 48 --- 50 46 45
R20E | 673 20 23 19 14 29 22 9 | 48 52 63 57 55 58 53
R21M | 1400 31 31 19 15 19 26 10 | 115 109 96 117 115 109 109
XR22 | 2045 11 40 21 20 19 --- 10 | 35 60 35 39 42 --- 37
R24 | 1133 25 25 11 24 19 16 9 | 73 58 64 58 68 53 60
XR26 |11532 41 87 33 --- 56 --- 29 | 47 69 70 --- 76 --- 58
XR28E |18936 78 --- --- --- 87 --- 82 | 77 --- --- --- 160 --- 104
------+-----------------------------------------+-------------------------------------
RMS | 1338 17 34 16 15 17 15 |T 59 63 57 58 65 51 58
WRMS | 1338 15 33 15 15 19 15 |NE 53 57 57 55 60 51 53
MEDI | 1234 15 31 14 15 17 13 |MD 59 61 54 57 56 53 54
Table 3.2406.4 GPS week: 2406 Day: 4 MJD: 61090
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 779 24 35 13 17 20 18 9 | 48 39 30 41 31 43 36
R03M | 910 9 42 18 14 10 11 7 | 63 88 70 67 64 60 65
R04 | 1773 14 22 15 6 8 11 5 | 67 82 73 66 67 64 67
R05M | 1301 8 40 28 13 20 12 8 | 51 52 76 62 42 52 55
XR06M | 1016 42 621 38 --- 81 --- 40 | 72 118 85 --- 92 --- 75
R07 | 2256 13 37 31 12 10 13 8 | 51 59 29 50 50 40 43
R08 | 2878 8 50 20 15 25 16 9 | 34 60 31 30 50 30 33
R09 | 1959 15 53 12 9 16 10 7 | 38 41 39 40 42 39 38
R11M | 860 9 43 17 22 17 20 9 | 17 42 23 25 22 27 15
R12M | 1763 17 25 8 18 13 10 6 | 45 39 37 36 39 38 37
R14M | 1166 9 43 11 12 9 14 6 | 49 71 52 51 47 43 48
R15M | 763 15 23 11 10 12 13 6 | 57 60 60 62 50 48 55
R16 | 1089 18 74 22 12 9 11 9 | 63 41 69 52 51 47 53
XR17 | 1490 18 28 20 28 24 --- 11 | 65 48 41 53 69 --- 53
R18 | 712 15 29 26 20 29 13 9 | 56 71 50 74 84 55 62
XR19E | 1407 13 35 15 --- 24 10 8 | 36 45 29 --- 53 34 36
R20E | 679 14 43 20 17 56 17 13 | 38 57 33 41 78 36 43
R21M | 708 20 38 16 16 10 31 9 | 202 209 211 204 201 202 204
R22 | 1857 18 53 16 15 16 16 8 | 36 72 45 53 44 47 44
R24 | 2693 25 34 11 24 17 14 9 | 80 64 76 79 80 70 74
XR26 |10709 34 46 36 --- 64 --- 26 | 35 42 41 --- 68 --- 41
XR28E |23677 51 --- --- --- 59 --- 55 | 104 --- --- --- 144 --- 114
------+-----------------------------------------+-------------------------------------
RMS | 1583 16 42 19 16 21 16 |T 59 66 57 60 66 54 58
WRMS | 1583 16 41 17 14 23 16 |NE 52 58 49 55 60 49 50
MEDI | 1301 15 40 17 15 17 13 |MD 51 59 45 52 51 43 48
Table 3.2406.5 GPS week: 2406 Day: 5 MJD: 61091
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 849 22 23 16 13 11 9 7 | 44 42 38 35 38 33 36
R03M | 1062 8 19 22 6 12 12 6 | 67 60 51 63 61 71 63
R04 | 1550 7 24 19 6 20 10 6 | 57 66 51 55 49 62 55
R05M | 1955 12 27 11 10 19 12 6 | 50 45 42 41 50 40 42
XR06M | 936 33 636 31 --- 76 --- 34 | 128 132 135 --- 132 --- 129
R07 | 1041 11 16 14 14 21 11 6 | 43 34 33 45 25 36 36
R08 | 4253 18 47 24 11 18 21 9 | 32 50 48 31 31 25 31
R09 | 1075 8 36 15 9 17 10 6 | 39 42 39 40 42 47 40
R11M | 785 15 19 14 13 10 12 6 | 18 25 23 27 23 19 18
R12M | 2249 29 42 22 23 20 11 10 | 48 63 50 51 44 41 45
R14M | 1581 13 35 12 11 21 11 7 | 44 54 45 45 33 38 40
R15M | 1347 17 30 14 14 15 11 7 | 50 58 50 39 35 40 42
R16 | 907 15 49 26 15 10 12 9 | 58 46 73 47 61 49 54
XR17 | 711 18 29 10 19 14 --- 9 | 60 43 51 54 60 --- 53
R18 | 686 10 34 15 20 25 11 8 | 52 61 51 52 64 50 51
XR19E | 886 12 26 21 --- 25 12 9 | 59 64 55 --- 68 67 61
R20E | 1139 9 37 23 6 59 16 12 | 46 57 34 48 67 35 42
R21M | 1087 23 35 19 18 24 13 9 | 266 264 262 256 259 259 260
R22 | 2131 15 39 16 14 11 17 8 | 41 62 57 53 47 40 46
R24 | 2688 25 26 20 11 15 25 9 | 67 46 62 57 49 51 55
XR26 |10275 35 66 52 --- 83 --- 34 | 38 75 44 --- 88 --- 51
XR28E |22059 59 --- --- --- 87 --- 72 | 88 --- --- --- 59 --- 62
------+-----------------------------------------+-------------------------------------
RMS | 1781 16 33 18 13 22 14 |T 63 66 61 57 62 55 59
WRMS | 1781 16 33 18 12 20 14 |NE 48 52 50 48 51 45 47
MEDI | 1087 15 34 19 13 19 12 |MD 50 57 50 47 49 40 46
Table 3.2406.6 GPS week: 2406 Day: 6 MJD: 61092
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 1707 23 26 26 10 10 12 8 | 67 58 52 55 54 53 55
R03M | 1339 10 27 17 15 18 29 8 | 87 93 81 87 91 71 83
R04 | 1538 12 26 22 8 19 11 7 | 86 101 78 81 76 80 81
R05M | 2938 12 35 23 11 15 17 8 | 81 91 80 72 76 68 75
XR06M | 906 32 639 34 --- 71 --- 33 | 147 226 139 --- 168 --- 147
R07 | 812 10 24 13 8 13 22 6 | 68 72 70 66 60 55 63
R08 | 2452 15 46 23 10 22 25 9 | 45 73 59 53 47 37 48
R09 | 1219 9 36 17 9 13 12 6 | 49 55 49 48 50 51 48
R11M | 957 8 26 16 9 8 12 5 | 25 30 30 31 30 29 27
R12M | 2190 19 20 11 17 20 13 7 | 57 60 53 46 49 50 50
R14M | 1120 6 31 17 13 10 19 7 | 54 70 62 51 56 42 53
R15M | 2144 20 41 11 12 14 27 9 | 71 81 63 60 57 55 61
R16 | 1034 28 41 18 23 18 9 10 | 77 58 75 57 65 60 63
XR17 | 831 10 38 30 16 13 --- 10 | 82 58 92 66 73 --- 74
R18 | 744 17 34 21 23 12 16 9 | 70 83 66 67 71 60 66
XR19E | 989 11 29 18 --- 16 11 8 | 81 87 80 --- 90 85 83
R20E | 1396 12 36 15 20 55 16 12 | 70 72 74 66 94 72 72
R21M | 2100 16 42 11 13 21 20 8 | 325 320 319 326 326 320 322
R22 | 941 11 38 12 13 11 12 6 | 55 88 62 61 63 55 60
R24 | 1842 18 33 26 14 9 32 9 | 88 65 88 74 77 66 77
XR26 | 8386 33 --- 59 --- 96 --- 46 | 37 --- 31 --- 119 --- 49
XR28E |13138 65 --- --- --- 83 --- 74 | 108 --- --- --- 90 --- 90
------+-----------------------------------------+-------------------------------------
RMS | 1675 15 34 18 14 20 19 |T 83 92 81 75 85 72 79
WRMS | 1675 15 34 15 13 17 19 |NE 65 72 67 63 70 58 62
MEDI | 1339 12 34 18 13 15 16 |MD 70 72 70 61 71 55 63
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