[IGSREPORT-30915] Wk 2414 IGLOS Final Orbits
acc
acc at igs.org
Fri May 1 03:04:16 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2414 (Apr 12, 2026 - Apr 18, 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 2.2414.
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:
igl2414[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2414 in the SP3 format.
igl24147.sum Combination Report for GPS Week 2414.
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 | 6.4 ns
1 | 8.9 ns
2 | 7.2 ns
3 | 6.9 ns
4 | 10.8 ns
5 | 5.9 ns
6 | 8.0 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 | IAC | 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 1.2414, 1a.2414).
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 2.2414.0-6)
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 3.2414.0-6).
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 2414 summary. (Apr 12, 2026 - Apr 18, 2026)
Table 1.2414.a GPS week : 2414 MJD: 61142.0-61148.0
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 3 2 2 7 .12 13 13 | 99 -519 3239 9445
| 0 1 2 14 15 18 .03 | 922 2279
esa n/a| -2 -2 7 -17 -37 33 -.05 33 31 | 5511 -714 3270 9720
| 1 2 2 28 29 36 .08 | 1838 2591
gfz n/a| 0 0 1 19 7 -5 -.11 15 15 | 0 -650 3235 9212
| 1 0 1 11 14 28 .04 | 0 2440
grg n/a| 1 0 2 -34 5 -21 .29 23 15 | 7893 -700 3367 9064
| 0 1 4 16 17 30 .05 | 436 2709
iac n/a| 1 0 -4 14 21 -8 -.12 18 18 | 8554 -429 3239 9867
| 1 1 2 25 21 56 .03 | 995 1518
jgx n/a| 0 0 -5 -1 -5 -2 -.13 13 13 | 2841 -681 3356 9370
| 1 0 1 9 12 16 .05 | 792 2832
Table 1.2414.b GPS week : 2414 MJD: 61142.0-61148.0
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 | 6 5 8 6 7 5 6 |
R03 | 5 4 6 6 8 5 6 |
R04 | 7 7 6 7 9 7 7 |
R05 | 7 6 6 6 6 6 8 |
R06 | 20 31 30 32 33 29 30 |
R07 | 7 7 5 6 6 7 7 |
R08 | 11 11 12 12 13 13 12 |
R09 | 7 7 6 15 9 7 7 |
R11 | 6 7 6 7 6 8 9 |
R12 | 5 7 6 6 8 12 12 |
R14 | 5 7 6 7 17 12 7 |
R15 | 7 6 8 7 6 14 11 |
R16 | 7 7 7 9 9 11 11 |
R17 | 7 7 7 7 7 7 6 |
R18 | 6 5 6 7 7 7 6 |
R19 | 7 8 8 7 8 7 7 |
R20 | 7 8 9 6 7 7 8 |
R21 | 7 10 9 11 10 9 9 |
R22 | 5 8 5 7 6 8 7 |
R24 | 7 6 6 8 8 7 8 |
R26 | 29 29 27 28 27 33 32 |
Table 1.2414.c GPS week : 2414 MJD: 61142.0-61148.0
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 2414 0 | 77 156 165 -125 2995 6411 77.9 1857 1857 | 6370 0
brd 2414 1 | 171 58 47 39 2379 4870 78.2 1641 1641 | 8865 0
brd 2414 2 | 15 43 87 -69 -5 7969 78.1 1900 1900 | 7151 0
brd 2414 3 | -27 56 43 78 -969 11800 77.6 1846 1846 | 6931 0
brd 2414 4 | -42 49 95 -779 223 8458 76.7 2222 2222 | 10824 0
brd 2414 5 | -48 -46 -30 -812 -652 6623 80.6 2062 2062 | 5894 0
brd 2414 6 | 37 -85 30 1234 1600 4387 80.5 1844 1844 | 8043 0
-------------+------------------------------------------------------------+----------------
brd 2414 mean| 26 33 62 -62 795 7216 78.5 1910 1910 | 7725 0
brd 2414 sdev| 78 78 61 682 1537 2504 1.5 184 184 | 1690 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 2.2414.0 GPS week: 2414 Day: 0 MJD: 61142
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 2 4 25 31 10 .10 14 15 | 721 -2714 2974 9204
esa n/a| -4 -3 3 -18 -66 15 -.02 20 19 | 2891 -1317 3029 9464
gfz n/a| 2 0 2 28 7 12 -.07 14 13 | 0 -2285 2975 8843
grg n/a| 1 -1 1 -21 -15 -69 .27 15 15 | 7349 -2235 3085 8798
iac n/a| 2 -1 -2 -10 22 76 -.14 17 15 | 6945 -306 2979 9599
jgx n/a| 0 1 -4 0 0 -11 -.13 10 10 | 3257 -2488 3135 9213
Table 2.2414.1 GPS week: 2414 Day: 1 MJD: 61143
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 2 16 -11 3 .09 11 11 | -168 544 3080 9145
esa n/a| -2 -6 10 -32 -60 10 -.15 38 35 | 3805 1519 3119 8489
gfz n/a| 0 0 1 12 -6 11 -.09 15 16 | 0 501 3076 8964
grg n/a| 1 0 2 -45 -2 -15 .24 15 12 | 8618 359 3264 8805
iac n/a| 1 1 -8 -5 40 7 -.07 15 15 | 8633 842 3072 9530
jgx n/a| 0 0 -4 17 -12 -23 -.21 12 12 | 2507 1169 3227 9107
Table 2.2414.2 GPS week: 2414 Day: 2 MJD: 61144
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 -9 0 -18 .09 12 12 | -759 -1023 3007 9020
esa n/a| -2 -3 6 -4 -58 85 -.03 36 31 | 5352 -529 3030 9566
gfz n/a| 0 0 2 34 20 26 -.19 16 13 | 0 -1315 3007 8880
grg n/a| 1 0 3 -17 2 21 .22 12 13 | 7779 -1803 3118 9019
iac n/a| 4 1 -5 46 1 -90 -.10 18 19 | 8403 -118 3008 9560
jgx n/a| 0 0 -6 -5 -4 16 -.17 13 13 | 3108 -2139 3121 9290
Table 2.2414.3 GPS week: 2414 Day: 3 MJD: 61145
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 -6 5 2 .16 12 12 | -1372 -2405 3130 9741
esa n/a| 0 -3 10 14 -12 2 -.15 33 33 | 6117 -2394 3167 10368
gfz n/a| 1 0 3 22 15 -54 -.10 18 17 | 0 -2924 3125 9520
grg n/a| 0 0 2 -32 13 -20 .35 24 15 | 7849 -2410 3302 9630
iac n/a| 3 0 0 -7 0 38 -.16 16 17 | 8753 -2655 3134 10266
jgx n/a| -1 0 -7 3 -1 6 -.11 15 15 | 1920 -2610 3295 9903
Table 2.2414.4 GPS week: 2414 Day: 4 MJD: 61146
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 6 -9 -2 -5 .10 14 15 | 773 3770 3607 9598
esa n/a| 0 2 8 -27 -59 46 .03 35 36 | 7556 3851 3617 10217
gfz n/a| -1 0 -2 24 1 5 -.08 16 16 | 0 4191 3601 9325
grg n/a| 2 -2 0 -22 -10 -40 .34 33 21 | 8251 4740 3752 8862
iac n/a| 0 2 -4 4 59 -14 -.15 24 25 | 10298 1637 3608 9865
jgx n/a| 1 0 -5 -5 4 2 -.11 12 12 | 2808 4787 3723 9131
Table 2.2414.5 GPS week: 2414 Day: 5 MJD: 61147
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 7 -10 -15 23 .16 14 15 | 1221 -2070 3385 10790
esa n/a| -2 -1 9 12 0 79 -.05 33 32 | 7886 -3372 3424 11342
gfz n/a| 0 -1 2 11 28 -30 -.06 14 13 | 0 -2279 3377 10490
grg n/a| 2 0 -3 -34 35 8 .27 40 17 | 7473 -3281 3451 10096
iac n/a| 0 0 -5 47 12 -61 -.08 19 20 | 8755 -2121 3380 11119
jgx n/a| 0 0 -4 -8 3 12 -.06 12 12 | 4234 -3059 3393 10377
Table 2.2414.6 GPS week: 2414 Day: 6 MJD: 61148
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 8 11 36 .12 12 13 | 277 261 3494 8619
esa n/a| -4 -2 4 -67 -5 -2 .03 37 34 | 4970 -2759 3507 8595
gfz n/a| -1 0 0 0 -13 -12 -.14 15 14 | 0 -441 3486 8463
grg n/a| 1 -2 10 -65 12 -33 .31 25 15 | 7933 -274 3597 8244
iac n/a| 1 0 -6 24 13 -17 -.11 15 14 | 8093 -287 3497 9132
jgx n/a| 1 0 -8 -13 -30 -22 -.10 18 18 | 2053 -432 3604 8574
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 3.2414.0 GPS week: 2414 Day: 0 MJD: 61142
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 944 10 13 14 14 19 8 5 | 57 58 67 66 68 57 61
R03M | 1339 6 15 9 12 16 10 5 | 68 67 65 72 75 61 66
R04 | 740 22 18 7 9 16 14 6 | 66 73 58 60 54 48 57
R05 | 2644 14 22 19 11 13 11 6 | 61 59 51 57 56 49 54
XR06 | 1021 18 --- 21 --- 101 --- 20 | 27 --- 55 --- 98 --- 44
R07 | 911 13 29 11 17 19 7 7 | 68 88 67 69 76 65 69
R08 | 1691 28 37 17 28 20 13 10 | 47 93 65 63 61 55 58
R09E | 2216 11 16 19 15 18 10 6 | 47 55 54 43 54 46 47
R11E | 2315 10 17 13 13 15 9 5 | 46 51 50 53 48 51 49
R12E | 1137 7 16 11 17 8 8 5 | 71 71 73 78 68 72 71
R14E | 1460 10 13 9 14 9 10 5 | 73 78 79 86 76 72 76
R15E | 1551 11 18 16 16 16 10 6 | 38 43 40 51 42 38 39
R16E | 2898 15 19 17 17 13 11 6 | 63 82 71 76 66 68 69
XR17 | 1507 8 20 15 12 13 --- 7 | 51 42 49 52 45 --- 47
R18 | 1345 12 12 14 8 19 8 5 | 33 41 36 35 32 33 33
XR19 | 954 11 16 15 --- 17 9 6 | 23 26 27 --- 22 24 22
R20 | 1112 18 15 22 8 14 10 6 | 28 36 40 30 31 31 28
R21 | 3023 8 23 12 10 27 9 6 | 37 60 35 42 46 39 38
R22 | 978 6 19 12 13 10 8 5 | 21 31 25 33 28 25 24
R24 | 2652 14 16 14 13 19 12 6 | 44 46 45 40 48 47 44
XR26 | 7396 44 66 33 --- 57 --- 28 | 24 87 34 --- 83 --- 46
------+-----------------------------------------+-------------------------------------
RMS | 1856 14 20 14 15 17 10 |T 47 59 51 55 56 48 49
WRMS | 1856 15 19 13 15 15 10 |NE 40 56 45 48 52 41 43
MEDI | 1460 11 17 14 13 16 10 |MD 47 58 51 53 54 48 47
Table 3.2414.1 GPS week: 2414 Day: 1 MJD: 61143
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 818 8 25 12 12 14 6 5 | 39 39 42 42 42 40 39
R03M | 942 6 15 9 11 13 6 4 | 45 44 41 50 48 43 45
R04 | 925 16 28 11 6 22 16 7 | 48 53 44 47 40 35 42
R05 | 1094 11 29 18 6 10 11 6 | 39 40 53 43 37 38 40
XR06 | 928 30 571 24 --- 69 --- 30 | 24 112 27 --- 54 --- 32
R07 | 1059 9 37 17 18 8 5 6 | 46 47 36 57 43 47 45
R08 | 1133 18 76 17 23 18 12 10 | 36 73 37 49 32 43 38
R09E | 2618 12 36 15 13 14 14 6 | 50 56 50 48 52 46 48
R11E | 2400 8 23 20 19 16 12 7 | 52 54 56 52 55 58 53
R12E | 1741 9 33 12 16 18 9 6 | 78 83 80 81 78 81 78
R14E | 932 8 19 22 20 12 11 7 | 91 86 90 99 86 85 89
R15E | 1458 8 23 15 15 13 13 6 | 48 56 50 54 49 47 48
R16E | 3127 17 32 12 18 9 9 7 | 71 76 71 74 67 69 70
XR17 | 2278 10 23 9 12 15 --- 6 | 34 37 36 39 43 --- 35
R18 | 1749 10 17 10 7 13 11 4 | 30 38 36 36 34 31 32
XR19 | 876 11 16 22 --- 16 10 7 | 32 37 31 --- 33 34 30
R20 | 771 9 46 19 12 21 14 8 | 36 49 27 29 39 38 32
R21 | 2177 8 79 15 20 21 14 10 | 31 51 35 33 31 32 31
R22 | 883 13 32 18 16 19 13 7 | 30 37 33 34 35 33 30
R24 | 1467 7 23 10 11 8 17 5 | 34 40 34 36 39 33 33
XR26 |10754 40 84 29 --- 68 --- 29 | 32 49 46 --- 61 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 1640 11 38 15 15 15 12 |T 44 55 45 50 47 46 44
WRMS | 1640 11 35 16 12 15 12 |NE 34 51 36 40 40 36 35
MEDI | 1133 10 29 15 13 15 11 |MD 39 49 41 47 43 40 40
Table 3.2414.2 GPS week: 2414 Day: 2 MJD: 61144
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 873 12 25 17 13 18 19 7 | 45 53 63 63 58 39 51
R03M | 1782 6 25 19 9 12 11 5 | 52 45 63 58 52 49 53
R04 | 1047 12 26 11 9 13 17 6 | 56 65 61 60 51 47 54
R05 | 3341 9 23 16 9 12 16 6 | 48 56 52 54 51 41 48
XR06 | 919 32 579 21 --- 69 --- 29 | 25 152 44 --- 67 --- 38
R07 | 1145 10 32 7 7 11 11 5 | 52 61 51 53 50 48 51
R08 | 1238 27 77 13 18 22 20 12 | 36 92 47 57 31 46 44
R09E | 1656 9 38 12 10 19 7 6 | 30 37 31 27 32 28 28
R11E | 2904 13 19 14 11 19 11 6 | 32 35 32 37 38 36 33
R12E | 1647 8 22 15 9 18 10 5 | 35 29 41 39 44 27 33
R14E | 864 9 20 13 13 17 11 5 | 34 32 31 40 40 26 31
R15E | 2589 8 24 18 15 23 16 7 | 40 36 46 51 35 41 41
R16E | 2947 13 28 18 18 18 10 7 | 80 85 81 88 77 81 80
XR17 | 1892 13 23 16 10 10 --- 6 | 48 41 42 40 37 --- 40
R18 | 1893 12 15 18 9 16 4 5 | 29 35 40 35 26 27 29
XR19 | 1127 13 16 21 --- 9 14 7 | 13 25 22 --- 20 22 16
R20 | 812 14 54 26 8 17 10 8 | 20 53 43 25 26 27 25
R21 | 1632 6 71 12 13 23 9 9 | 32 33 37 37 26 33 31
R22 | 2107 6 22 16 8 15 10 5 | 21 31 28 24 25 28 23
R24 | 959 10 21 16 11 20 11 6 | 35 40 45 39 35 41 37
XR26 | 9556 35 55 30 --- 74 --- 27 | 31 56 30 --- 73 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1899 12 36 16 12 18 13 |T 37 52 44 45 42 38 39
WRMS | 1899 12 31 13 13 19 13 |NE 34 56 41 42 39 36 36
MEDI | 1647 12 25 16 10 18 11 |MD 35 41 43 40 38 36 37
Table 3.2414.3 GPS week: 2414 Day: 3 MJD: 61145
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 829 9 20 13 14 13 10 5 | 57 63 53 66 64 48 56
R03M | 3203 7 21 9 25 11 14 6 | 61 67 66 83 70 57 65
R04 | 1092 9 25 16 23 10 18 7 | 56 68 61 48 61 44 53
R05 | 3166 6 22 16 15 12 13 6 | 53 60 63 56 62 48 55
XR06 | 1109 35 581 23 --- 66 --- 32 | 26 137 41 --- 76 --- 43
R07 | 1317 7 25 13 11 12 12 5 | 57 68 63 57 63 50 57
R08 | 1193 27 55 11 21 12 32 12 | 39 85 52 58 55 55 51
R09E | 1250 10 34 43 69 21 16 14 | 31 45 51 68 33 32 29
R11E | 2600 12 22 19 10 12 14 6 | 26 33 31 30 33 34 28
R12E | 1891 7 21 17 15 15 9 6 | 54 50 62 55 63 53 55
R14E | 1418 15 33 16 16 14 9 7 | 98 84 82 95 101 92 92
R15E | 2212 9 18 9 18 18 17 6 | 35 33 34 44 40 34 34
R16E | 1169 14 26 21 21 22 15 8 | 59 57 62 61 63 59 58
XR17 | 1287 8 23 13 24 9 --- 7 | 29 33 35 30 23 --- 27
R18 | 1954 10 21 19 19 14 11 6 | 29 27 33 26 24 28 25
XR19 | 1160 13 20 12 --- 12 10 6 | 13 24 21 --- 21 22 17
R20 | 1477 11 30 16 11 9 11 6 | 15 30 23 21 20 19 16
R21 | 1751 6 78 17 26 11 14 11 | 23 32 28 35 21 21 21
R22 | 1369 8 26 13 7 22 12 6 | 12 35 20 22 28 20 18
R24 | 1220 13 21 11 16 29 9 8 | 31 36 31 28 32 30 28
XR26 |10722 38 59 31 --- 68 --- 28 | 13 60 21 --- 68 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 1846 12 33 18 24 16 15 |T 38 53 44 49 48 41 40
WRMS | 1846 12 33 17 15 17 15 |NE 30 53 37 38 42 33 34
MEDI | 1369 10 25 16 16 13 12 |MD 31 50 41 48 55 34 34
Table 3.2414.4 GPS week: 2414 Day: 4 MJD: 61146
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 720 10 16 20 10 15 12 6 | 47 38 35 42 45 38 39
R03M | 3862 10 36 20 33 14 10 8 | 59 78 48 76 47 49 53
R04 | 954 18 38 17 19 14 16 8 | 57 69 52 46 56 38 49
R05 | 2316 8 26 10 13 12 11 5 | 58 65 59 52 53 51 55
XR06 | 1003 27 620 26 --- 87 --- 33 | 22 166 43 --- 70 --- 35
R07 | 1092 7 27 11 9 13 12 5 | 56 63 55 55 59 53 55
R08 | 1067 37 53 20 19 37 12 13 | 38 79 65 53 76 52 53
R09E | 1248 11 36 11 49 15 16 9 | 28 27 26 65 26 29 26
R11E | 5412 11 22 17 18 12 11 6 | 33 39 34 41 37 39 34
R12E | 2348 9 21 23 25 11 14 7 | 56 60 60 69 59 61 58
R14E | 2040 12 24 20 100 60 10 17 | 81 97 93 153 78 84 86
R15E | 2199 10 25 11 19 9 11 6 | 39 46 40 48 42 40 39
R16E | 1049 15 37 17 17 28 15 9 | 62 66 70 69 63 68 64
XR17 | 1192 9 25 12 15 9 --- 6 | 46 55 37 50 37 --- 41
R18 | 1697 13 27 13 20 23 10 7 | 23 36 31 24 22 25 23
XR19 | 1085 14 19 23 --- 16 10 8 | 22 25 37 --- 22 18 18
R20 | 2439 7 34 13 20 16 8 6 | 15 27 18 29 26 24 18
R21 | 1426 6 75 13 27 15 10 10 | 24 36 26 32 18 18 20
R22 | 840 11 26 11 13 21 10 6 | 10 30 18 20 22 19 14
R24 | 1366 9 31 9 18 29 13 7 | 24 42 25 29 31 26 25
XR26 |11505 25 70 29 --- 76 --- 26 | 15 55 22 --- 61 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 2222 14 35 16 33 24 12 |T 38 57 42 52 45 40 39
WRMS | 2222 15 36 16 21 25 12 |NE 31 57 37 39 42 32 33
MEDI | 1366 11 27 17 19 15 11 |MD 38 55 37 48 45 38 39
Table 3.2414.5 GPS week: 2414 Day: 5 MJD: 61147
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 798 6 13 6 11 16 9 4 | 33 33 29 35 37 27 30
R03M | 3144 9 16 14 14 10 6 4 | 38 37 26 44 32 33 32
R04 | 2024 12 31 11 22 16 9 6 | 55 66 49 55 53 53 53
R05 | 1127 15 25 11 15 12 9 6 | 49 45 42 38 46 41 42
XR06 | 891 34 587 21 --- 65 --- 29 | 17 187 40 --- 48 --- 32
R07 | 1142 5 31 13 12 16 14 6 | 43 46 49 35 40 32 39
R08 | 1132 35 64 14 19 25 12 12 | 27 69 48 43 48 35 39
R09E | 968 11 33 17 20 15 11 7 | 35 44 36 42 37 35 34
R11E | 3499 10 28 13 42 15 15 8 | 47 49 50 58 49 51 47
R12E | 2071 14 27 14 82 21 16 12 | 74 73 77 106 70 78 73
R14E | 4627 15 25 15 64 35 14 11 | 116 121 119 128 112 112 114
R15E | 1245 11 30 25 90 31 16 14 | 54 57 52 107 70 53 54
R16E | 1757 10 35 17 71 18 10 11 | 70 65 70 96 74 66 67
R17 | 1164 12 25 12 12 8 17 6 | 25 21 25 27 21 14 22
R18 | 1320 20 19 15 13 11 10 6 | 23 19 27 26 23 19 19
XR19 | 1337 11 24 15 --- 15 13 7 | 14 23 21 --- 25 21 17
R20 | 2476 10 43 10 15 11 8 6 | 12 30 10 12 13 19 11
R21 | 1413 7 59 11 15 14 14 8 | 18 25 20 24 21 24 18
R22 | 1302 17 33 11 14 22 11 7 | 15 35 29 26 23 24 20
R24 | 1269 10 14 14 22 24 12 7 | 24 25 25 25 29 28 23
XR26 |11849 45 47 31 --- 96 --- 33 | 13 33 28 --- 69 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2062 14 33 14 40 19 12 |T 38 52 41 51 44 40 38
WRMS | 2062 15 32 13 17 20 12 |NE 25 48 31 31 35 28 27
MEDI | 1320 11 30 14 15 16 12 |MD 33 44 36 38 40 33 32
Table 3.2414.6 GPS week: 2414 Day: 6 MJD: 61148
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02M | 816 7 20 10 10 13 17 5 | 64 61 60 64 66 52 60
R03M | 1758 5 20 17 10 10 16 5 | 70 77 76 81 71 62 71
R04 | 1701 11 30 12 16 14 15 6 | 80 97 74 74 71 69 74
R05 | 1995 16 31 17 16 15 14 7 | 75 75 69 67 75 65 70
XR06 | 824 35 529 25 --- 61 --- 30 | 29 170 30 --- 83 --- 39
R07 | 958 7 48 11 16 7 11 6 | 79 83 81 76 76 74 77
R08 | 1087 32 69 17 11 23 12 12 | 52 119 77 75 69 66 68
R09E | 1419 8 36 12 17 17 12 6 | 44 50 48 44 51 45 45
R11E | 2249 11 29 16 29 12 25 8 | 47 48 54 50 50 57 49
R12E | 2054 12 27 25 57 13 21 11 | 93 88 93 118 97 97 94
R14E | 4429 13 22 9 28 16 14 7 | 156 145 151 160 157 148 154
R15E | 716 13 28 17 48 15 25 10 | 63 55 57 92 66 61 61
R16E | 2503 9 42 18 46 16 28 11 | 62 63 63 80 64 64 61
R17 | 820 8 12 14 15 16 11 5 | 39 37 36 37 34 14 34
R18 | 1089 10 33 12 11 9 17 6 | 30 37 29 27 24 25 26
XR19 | 1340 11 25 13 --- 17 12 7 | 22 29 25 --- 26 22 21
R20 | 1635 6 51 12 12 14 13 7 | 19 34 18 19 25 22 19
R21 | 1209 7 67 20 13 12 8 9 | 31 29 32 41 34 29 30
R22 | 1248 11 29 10 16 14 17 6 | 18 40 19 22 23 23 19
R24 | 1793 11 17 15 14 19 25 7 | 34 38 36 32 38 32 33
XR26 | 8458 43 49 32 --- 79 --- 31 | 15 59 28 --- 93 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1843 12 37 15 25 15 18 |T 53 68 55 64 61 54 54
WRMS | 1843 13 34 14 15 14 18 |NE 40 65 42 47 51 40 42
MEDI | 1419 11 30 15 16 15 15 |MD 47 59 54 64 66 57 49
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