[IGSREPORT-30890] Wk 2412 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 17 03:18:57 UTC 2026
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2412 (Mar 29, 2026 - Apr 04, 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 2.2412.
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:
igl2412[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2412 in the SP3 format.
igl24127.sum Combination Report for GPS Week 2412.
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 | 5.1 ns
1 | 4.7 ns
2 | 4.8 ns
3 | 5.5 ns
4 | 5.6 ns
5 | 5.2 ns
6 | 6.4 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
3 | GRG | R16
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 1.2412, 1a.2412).
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 2.2412.0-6)
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 3.2412.0-6).
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 2412 summary. (Mar 29, 2026 - Apr 04, 2026)
Table 1.2412.a GPS week : 2412 MJD: 61128.0-61134.0
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 -8 9 18 .06 14 13 | 2620 -782 3341 10808
| 1 1 0 18 14 11 .02 | 765 1223
esa n/a| -1 -2 7 -13 -4 43 .02 34 32 | 5245 -841 3384 11594
| 2 1 3 32 10 51 .06 | 762 1020
gfz n/a| 0 0 0 23 4 9 -.14 16 14 | 0 -1056 3338 10490
| 0 1 1 15 14 48 .05 | 0 1119
grg n/a| 1 0 3 -13 -4 -29 .27 23 14 | 5628 -1081 3357 9725
| 0 1 1 14 14 55 .04 | 416 1640
iac n/a| 0 0 -5 -10 4 -20 -.03 21 20 | 6032 -520 3340 11089
| 1 2 1 35 43 118 .06 | 818 1409
jgx n/a| 0 0 -7 4 0 0 -.11 17 17 | 5958 -1184 3360 10163
| 0 0 2 8 14 21 .04 | 1602 1443
Table 1.2412.b GPS week : 2412 MJD: 61128.0-61134.0
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 6 5 6 6 8 7 |
R03 | 6 7 6 5 7 7 9 |
R04 | 7 5 7 7 7 8 7 |
R05 | 8 7 10 6 8 6 7 |
R06 | 36 35 32 29 29 32 32 |
R07 | 6 7 7 7 7 7 7 |
R08 | 13 11 11 34 10 11 11 |
R09 | 6 7 9 7 7 7 7 |
R11 | 7 6 5 6 7 8 8 |
R12 | 8 7 9 7 7 8 7 |
R14 | 7 8 6 8 8 5 7 |
R15 | 8 7 7 8 7 11 8 |
R16 | 10 10 9 39 10 10 8 |
R17 | 7 8 8 9 9 9 9 |
R18 | 6 10 9 7 9 8 7 |
R19 | 9 7 6 7 7 7 6 |
R20 | 6 7 8 7 6 7 8 |
R21 | 9 10 11 9 8 10 10 |
R22 | 6 8 7 7 7 6 6 |
R24 | 5 8 9 11 9 9 7 |
R26 | 25 27 25 26 24 24 22 |
Table 1.2412.c GPS week : 2412 MJD: 61128.0-61134.0
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 2412 0 | -134 -11 -62 1010 -3191 6286 79.8 2818 2818 | 5123 0
brd 2412 1 | 223 216 -38 1418 779 9354 76.5 2663 2663 | 4651 0
brd 2412 2 | 17 -10 199 -2009 3200 15230 80.8 2181 2181 | 4772 0
brd 2412 3 | -150 116 188 2319 2316 13900 80.0 1974 1974 | 5481 0
brd 2412 4 | -57 -11 283 -1602 -440 12890 82.9 2057 2057 | 5560 0
brd 2412 5 | 136 53 163 -2947 2457 15680 78.1 3491 3491 | 5149 0
brd 2412 6 | -11 61 -44 -3170 2471 13780 76.2 4677 4677 | 6426 0
-------------+------------------------------------------------------------+----------------
brd 2412 mean| 3 59 98 -711 1084 12445 79.2 2837 2837 | 5308 0
brd 2412 sdev| 137 84 142 2243 2254 3410 2.4 968 968 | 594 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 2.2412.0 GPS week: 2412 Day: 0 MJD: 61128
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 -11 -5 13 .05 12 12 | 2908 -395 3018 14035
esa n/a| -3 0 2 -12 -6 -20 -.06 30 30 | 4757 -1329 3081 14018
gfz n/a| 0 0 1 25 20 -36 -.10 14 13 | 0 -935 3015 13478
grg n/a| 1 0 4 -6 18 -35 .28 17 12 | 5160 -416 3143 9638
iac n/a| 1 2 -3 -26 -59 128 -.05 16 16 | 6063 -2701 3033 14033
jgx n/a| 1 0 -7 15 8 -22 -.12 12 12 | 7708 -286 3092 10187
Table 2.2412.1 GPS week: 2412 Day: 1 MJD: 61129
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| -3 0 3 -3 6 30 .05 14 15 | 3797 -1507 3932 11304
esa n/a| -3 -3 10 -13 7 57 -.02 31 31 | 5625 -720 3961 12462
gfz n/a| 0 0 0 52 -9 5 -.11 18 17 | 0 -1597 3934 10751
grg n/a| 1 2 3 -5 0 -73 .20 15 12 | 5893 -3200 3291 9459
iac n/a| 1 -2 -6 -24 25 38 .04 19 19 | 4705 94 3929 11387
jgx n/a| 1 1 -7 13 -11 5 -.20 13 13 | 8673 -3584 3278 9689
Table 2.2412.2 GPS week: 2412 Day: 2 MJD: 61130
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 2 3 -11 0 18 .04 12 11 | 2789 -1108 3354 8918
esa n/a| 0 -2 9 -52 -4 99 .01 38 38 | 5340 -1103 3389 10294
gfz n/a| 0 -2 0 15 0 62 -.09 15 16 | 0 -1571 3357 8742
grg n/a| 0 0 6 10 -14 7 .23 21 19 | 5289 -1760 3513 8894
iac n/a| 0 -1 -4 14 28 -214 .01 21 21 | 5146 -429 3349 9293
jgx n/a| 1 0 -4 2 11 19 -.10 13 13 | 5426 -1699 3534 9041
Table 2.2412.3 GPS week: 2412 Day: 3 MJD: 61131
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 2 3 -44 38 34 .10 23 13 | 3215 -1821 3187 9011
esa n/a| 0 -2 6 -53 12 67 .06 39 29 | 6550 -1401 3209 9572
gfz n/a| 0 0 0 16 18 -72 -.12 22 12 | 0 -1707 3182 8820
grg n/a| 1 2 4 -26 -21 40 .31 57 16 | 5957 -1122 3335 8319
iac n/a| 0 -3 -5 38 -37 24 -.11 31 31 | 6413 -481 3171 9359
jgx n/a| 0 2 -5 -2 22 -33 -.10 36 36 | 5644 -895 3305 8805
Table 2.2412.4 GPS week: 2412 Day: 4 MJD: 61132
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 -1 7 19 .07 13 12 | 1979 -180 3337 10965
esa n/a| -4 0 11 24 -10 63 .05 30 25 | 5266 -569 3386 12185
gfz n/a| 0 -1 0 6 16 28 -.24 15 14 | 0 -806 3335 10703
grg n/a| 0 0 3 -18 3 -13 .29 16 14 | 5720 -658 3461 10782
iac n/a| 0 -1 -4 -33 -20 -80 .01 17 16 | 6523 -693 3336 11334
jgx n/a| 0 0 -10 9 4 6 -.12 16 16 | 4996 -1193 3446 11102
Table 2.2412.5 GPS week: 2412 Day: 5 MJD: 61133
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 1 4 16 .07 14 13 | 1817 -1989 3169 10292
esa n/a| 3 -5 9 29 -13 76 .14 37 36 | 5107 -1985 3220 10852
gfz n/a| 0 0 2 31 -13 28 -.13 17 15 | 0 -2058 3165 9966
grg n/a| 1 0 2 -22 -2 -5 .25 18 13 | 6197 -2334 3261 9830
iac n/a| -2 2 -2 -59 52 -106 -.02 18 18 | 6356 -1371 3178 10645
jgx n/a| 0 1 -10 -7 -15 -1 -.07 14 14 | 4364 -1747 3239 10340
Table 2.2412.6 GPS week: 2412 Day: 6 MJD: 61134
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| -3 0 4 13 14 0 .06 13 14 | 1838 1522 3394 11133
esa n/a| -2 -2 4 -12 -14 -38 .01 34 34 | 4074 1215 3447 11777
gfz n/a| 0 0 -1 15 -3 52 -.20 13 12 | 0 1280 3381 10971
grg n/a| 1 -1 3 -29 -19 -128 .31 15 14 | 5185 1919 3496 11153
iac n/a| 2 0 -8 21 43 66 -.13 21 21 | 7024 1935 3384 11575
jgx n/a| 1 0 -9 2 -13 28 -.09 17 17 | 4897 1112 3627 11977
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 3.2412.0 GPS week: 2412 Day: 0 MJD: 61128
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 958 10 21 9 11 24 6 6 | 38 39 40 40 42 38 37
R03 | 3621 11 23 13 12 20 10 6 | 41 50 50 46 52 43 44
R04 | 1949 14 30 10 9 16 17 7 | 47 50 39 37 41 32 39
R05 | 1890 19 15 28 19 16 6 8 | 45 62 45 44 41 37 40
XR06 | 955 39 658 20 --- 83 --- 36 | 41 275 40 --- 77 --- 45
R07 | 1949 9 35 11 10 9 11 6 | 53 51 55 54 55 45 51
XR08 | 7671 23 65 20 13 19 --- 13 | 744 702 731 724 737 --- 733
R09E | 2717 9 35 10 7 18 11 6 | 86 92 83 83 83 79 82
R11E | 990 10 26 12 12 17 14 6 | 26 34 24 28 27 28 25
R12E | 2532 14 30 12 15 13 23 8 | 206 214 205 204 199 197 202
R14E | 1411 6 28 17 18 18 10 6 | 45 42 52 51 47 39 44
R15E | 1749 11 24 14 30 17 9 7 | 87 85 84 96 84 75 86
R16E | 7145 16 25 23 38 19 13 10 | 9999 9999 9999 9999 9999 9999 9999
XR17 | 2091 11 27 11 11 9 --- 6 | 58 38 59 58 62 --- 57
R18 | 2268 15 17 14 15 11 10 6 | 48 59 55 56 67 50 53
XR19 | 1615 16 24 20 --- 22 11 9 | 27 31 34 --- 39 29 28
R20 | 1831 11 27 10 10 19 10 6 | 38 44 43 42 52 39 41
R21 | 1301 8 61 13 17 14 9 8 | 61 38 67 71 59 60 60
R22 | 1394 9 32 12 13 10 10 6 | 31 39 29 40 32 32 31
R24 | 4334 8 30 9 11 11 8 5 | 58 45 66 56 67 49 57
XR26 |10086 36 63 19 --- 60 --- 25 | 18 53 28 --- 61 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2817 12 30 14 17 16 12 |T 89 102 91 101 96 54 89
WRMS | 2817 12 30 13 12 16 12 |NE 89 105 92 105 98 41 89
MEDI | 1949 11 28 13 12 17 10 |MD 45 50 50 54 55 39 44
Table 3.2412.1 GPS week: 2412 Day: 1 MJD: 61129
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1123 14 11 13 14 18 10 6 | 31 37 36 42 37 30 32
R03 | 2721 11 17 13 13 22 13 6 | 33 38 33 34 32 29 30
R04 | 2356 11 21 6 8 13 10 5 | 35 38 34 35 31 30 32
R05 | 2585 8 39 11 12 16 13 7 | 30 46 37 34 28 28 30
XR06 | 1056 31 656 32 --- 79 --- 34 | 47 221 46 --- 61 --- 47
R07 | 1926 11 19 27 13 17 8 7 | 33 45 43 37 37 30 34
R08 | 3988 25 58 12 13 10 26 11 | 417 399 423 410 419 663 415
R09E | 2015 9 31 12 11 18 10 6 | 64 66 63 63 66 63 63
R11E | 941 14 18 12 7 15 12 5 | 29 21 25 24 24 21 23
R12E | 2431 6 21 16 11 29 13 7 | 140 138 146 137 127 141 138
R14E | 1998 11 35 12 20 15 10 7 | 30 43 30 33 31 26 27
R15E | 1974 10 21 19 23 12 13 7 | 62 60 56 57 58 46 57
R16E | 6502 20 29 18 30 15 15 9 | 904 902 897 908 900 894 901
XR17 | 1397 10 31 10 10 22 --- 7 | 39 41 44 42 44 --- 40
R18 | 2366 25 17 24 13 34 9 9 | 40 39 43 37 49 42 37
XR19 | 1323 12 23 16 --- 14 11 7 | 26 32 33 --- 32 26 27
R20 | 1938 10 28 11 15 21 15 7 | 46 47 50 52 57 51 49
R21 | 1057 13 55 23 15 22 9 9 | 42 30 54 54 49 46 45
R22 | 1622 9 22 25 13 22 13 7 | 28 27 37 35 36 34 30
R24 | 2427 13 30 26 10 19 15 8 | 35 35 47 45 38 38 38
XR26 | 8877 32 60 34 --- 66 --- 26 | 22 45 24 --- 43 --- 26
------+-----------------------------------------+-------------------------------------
RMS | 2663 14 31 18 15 19 13 |T 101 111 104 115 104 124 101
WRMS | 2663 15 31 17 12 19 13 |NE 60 74 65 71 66 87 60
MEDI | 1998 11 28 16 13 18 12 |MD 35 43 43 42 43 34 37
Table 3.2412.2 GPS week: 2412 Day: 2 MJD: 61130
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1586 10 17 16 8 13 7 5 | 27 29 28 26 22 20 22
R03 | 1187 8 25 14 10 14 8 5 | 31 41 33 33 32 31 30
R04 | 1996 15 23 10 30 16 6 7 | 34 39 31 30 35 32 30
R05 | 2160 10 73 14 15 14 16 9 | 36 84 51 34 32 38 39
XR06 | 1311 29 657 25 --- 79 --- 31 | 25 218 38 --- 52 --- 32
R07 | 1391 12 40 12 18 17 8 7 | 38 43 41 43 38 34 36
R08 | 2197 25 49 14 14 39 16 11 | 654 641 653 652 631 443 650
R09E | 1296 13 28 21 28 24 15 9 | 38 54 29 52 47 30 36
R11E | 1121 9 21 12 14 12 10 5 | 16 25 26 20 19 21 17
R12E | 1414 11 25 16 17 33 16 8 | 172 176 178 180 156 177 173
R14E | 2722 7 24 12 23 10 8 5 | 36 40 34 36 34 36 33
R15E | 4231 8 27 13 23 18 9 6 | 54 61 54 55 49 36 51
R16E | 2756 13 42 15 30 21 17 9 | 949 943 950 952 963 953 951
XR17 | 2143 6 42 14 11 16 --- 8 | 39 35 44 40 38 --- 38
R18 | 1982 15 31 18 20 30 15 9 | 39 50 50 38 56 33 41
XR19 | 882 9 20 14 --- 13 9 6 | 23 25 32 --- 25 23 24
R20 | 3761 11 51 11 22 18 11 8 | 17 50 23 19 30 20 18
R21 | 1464 9 68 15 31 15 20 10 | 41 30 43 57 40 29 37
R22 | 1303 7 26 20 19 12 10 6 | 22 33 28 30 22 26 23
R24 | 1328 13 28 20 17 25 19 8 | 36 33 38 33 39 32 33
XR26 | 8186 30 61 21 --- 71 --- 24 | 15 49 21 --- 49 --- 22
------+-----------------------------------------+-------------------------------------
RMS | 2181 12 38 15 21 21 13 |T 111 128 115 129 114 111 111
WRMS | 2181 11 38 16 19 21 13 |NE 71 93 76 86 76 63 71
MEDI | 1586 11 28 14 18 17 10 |MD 36 43 38 36 38 32 33
Table 3.2412.3 GPS week: 2412 Day: 3 MJD: 61131
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1470 12 17 16 13 5 17 6 | 34 34 39 37 40 34 34
R03 | 1680 9 18 10 14 13 10 5 | 43 37 41 44 42 41 39
R04 | 1898 15 30 18 14 11 10 7 | 45 50 36 34 42 36 38
R05 | 719 9 27 9 14 14 8 5 | 45 54 45 40 56 47 46
XR06 | 1170 36 627 25 --- 55 --- 28 | 21 236 35 --- 48 --- 31
R07 | 777 9 27 9 18 13 26 7 | 43 56 46 49 53 41 45
R08 | 1537 61 78 44 123 46 109 34 | 840 816 832 759 834 656 814
R09E | 1217 12 31 12 14 15 11 6 | 35 43 35 33 31 35 33
R11E | 1533 10 17 11 19 12 12 5 | 26 24 24 29 27 22 22
R12E | 1550 13 26 12 20 13 15 7 | 68 83 64 67 64 71 66
R14E | 2710 7 32 18 19 16 10 7 | 33 29 37 40 35 34 32
R15E | 4930 8 37 17 21 15 11 7 | 47 60 47 56 55 30 48
R16E | 1169 58 76 64 193 105 84 39 | 9999 9999 9999 9999 9999 9999 9999
XR17 | 1191 8 33 12 11 23 --- 8 | 42 39 39 40 56 --- 42
R18 | 946 14 30 9 16 12 20 7 | 39 53 40 36 40 39 39
XR19 | 653 11 27 11 --- 14 13 7 | 20 26 28 --- 30 24 24
R20 | 3251 15 30 9 11 20 10 7 | 22 30 32 31 46 30 30
R21 | 894 16 57 9 15 13 7 8 | 47 29 41 50 47 43 42
R22 | 1389 14 24 15 19 14 13 7 | 23 38 30 36 27 24 24
R24 | 830 16 38 14 23 30 24 10 | 42 45 47 48 65 33 46
XR26 |11647 34 57 31 --- 61 --- 26 | 20 49 21 --- 56 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 1973 23 39 22 57 31 36 |T 76 91 77 84 84 72 76
WRMS | 1973 13 29 12 16 31 36 |NE 88 106 90 100 98 87 88
MEDI | 1389 13 30 12 16 14 12 |MD 39 43 39 40 46 35 38
Table 3.2412.4 GPS week: 2412 Day: 4 MJD: 61132
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1777 9 20 14 13 16 8 6 | 32 36 38 38 29 33 32
R03 | 1748 9 18 17 12 16 15 6 | 40 46 41 41 26 34 35
R04 | 1344 17 14 15 11 15 16 6 | 40 41 40 35 27 28 33
R05 | 786 15 34 14 9 10 20 7 | 48 57 41 43 42 33 41
XR06 | 1117 33 548 26 --- 59 --- 29 | 26 196 37 --- 45 --- 30
R07 | 799 10 32 14 11 17 12 6 | 37 47 47 39 47 35 40
R08 | 3187 19 54 11 14 19 15 9 | 561 545 556 570 552 410 562
R09E | 1686 9 26 17 17 14 13 6 | 47 55 40 50 47 42 44
R11E | 1159 12 24 19 11 14 16 7 | 26 24 32 26 19 27 22
R12E | 1423 9 24 19 16 8 16 6 | 139 144 141 139 140 135 139
R14E | 2332 11 26 10 25 21 8 7 | 36 37 37 49 40 33 35
R15E | 3785 6 29 17 19 14 11 7 | 59 60 56 56 61 57 56
R16E | 3445 22 44 19 23 18 15 10 | 906 899 903 897 894 900 902
XR17 | 891 5 33 8 16 23 --- 8 | 40 28 38 39 47 --- 39
R18 | 1050 12 22 11 24 26 25 9 | 36 45 39 34 44 33 36
XR19 | 1223 7 24 16 --- 15 11 7 | 27 40 27 --- 31 32 28
R20 | 3073 13 25 8 6 17 15 6 | 26 37 20 22 27 22 21
R21 | 1344 11 42 17 13 15 12 7 | 45 44 51 49 37 43 43
R22 | 1277 13 27 11 22 10 10 6 | 24 41 32 39 26 29 27
R24 | 799 12 18 20 15 25 26 9 | 41 45 53 49 47 40 44
XR26 |10126 34 49 22 --- 59 --- 24 | 17 27 24 --- 34 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 2056 13 30 15 16 17 16 |T 107 118 109 123 107 109 106
WRMS | 2056 12 25 14 14 16 16 |NE 69 85 72 83 70 64 68
MEDI | 1344 12 26 16 14 16 15 |MD 40 45 40 41 42 33 36
Table 3.2412.5 GPS week: 2412 Day: 5 MJD: 61133
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1040 13 26 15 17 23 9 7 | 26 31 31 40 39 29 30
R03 | 2697 9 27 14 14 18 17 7 | 27 31 35 32 28 22 26
R04 | 2094 19 34 12 11 13 17 7 | 25 31 24 26 22 21 21
R05 | 846 14 22 14 12 12 9 6 | 28 32 23 26 27 23 23
XR06 | 1303 37 560 26 --- 68 --- 32 | 36 150 37 --- 36 --- 31
R07 | 1532 8 50 8 8 21 11 7 | 36 42 33 29 43 31 33
R08 | 5646 21 66 24 13 15 22 11 | 443 422 426 436 442 275 437
R09E | 1455 9 21 22 8 16 10 6 | 69 73 69 70 72 69 68
R11E | 2013 15 29 24 13 15 12 7 | 28 27 37 21 27 25 24
R12E | 1900 19 30 18 15 22 12 8 | 126 132 129 131 123 123 126
R14E | 1652 8 22 10 14 10 10 5 | 41 42 40 48 43 41 41
R15E | 2550 21 36 12 45 18 14 11 | 59 62 60 80 64 67 59
R16E |11269 17 43 21 36 14 10 10 | 770 765 772 778 764 768 770
XR17 | 1021 10 44 8 13 26 --- 9 | 36 33 37 45 44 --- 38
R18 | 1025 13 16 14 10 29 19 8 | 33 32 30 35 36 28 29
XR19 | 897 8 15 15 --- 17 13 6 | 23 25 22 --- 27 25 21
R20 | 1159 9 38 13 14 10 15 6 | 22 38 23 34 25 29 24
R21 | 2466 7 67 25 13 22 17 10 | 39 28 43 41 43 31 36
R22 | 1621 10 22 10 14 16 9 5 | 23 31 24 33 30 27 25
R24 | 1531 10 32 22 10 25 18 8 | 33 30 43 41 39 33 34
XR26 | 7935 30 47 23 --- 63 --- 23 | 19 30 25 --- 30 --- 21
------+-----------------------------------------+-------------------------------------
RMS | 3490 14 37 17 18 18 14 |T 92 99 93 108 95 92 91
WRMS | 3490 13 36 15 13 18 14 |NE 56 65 57 68 60 47 55
MEDI | 1621 13 32 15 13 18 12 |MD 33 32 37 40 39 29 31
Table 3.2412.6 GPS week: 2412 Day: 6 MJD: 61134
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1177 13 27 15 11 24 14 7 | 44 46 53 53 49 40 46
R03 | 1533 12 18 9 17 41 21 9 | 49 51 51 58 60 41 49
R04 | 1519 19 26 11 8 14 17 7 | 50 53 42 38 39 37 40
R05 | 1412 17 30 12 11 15 16 7 | 51 57 49 45 42 38 45
XR06 | 1200 33 586 25 --- 81 --- 32 | 40 210 43 --- 73 --- 42
R07 | 2554 8 37 11 18 14 13 7 | 58 58 59 64 65 55 59
R08 | 6348 25 58 16 22 15 26 11 | 700 663 688 689 696 454 692
R09E | 1218 8 31 8 16 15 18 6 | 65 74 62 68 71 64 66
R11E | 2419 14 32 15 19 17 16 8 | 26 31 28 27 28 30 25
R12E | 1214 9 30 14 16 15 12 6 | 214 213 215 215 212 216 213
R14E | 2606 13 16 18 17 19 13 7 | 58 57 62 65 58 58 58
XR15E | 1405 12 23 14 15 15 --- 7 | 103 112 98 108 96 --- 101
R16E |16336 14 35 19 15 11 15 7 | 9999 9999 9999 9999 9999 9999 9999
XR17 | 1114 16 38 9 18 15 --- 8 | 59 45 65 70 71 --- 63
R18 | 891 8 17 12 8 26 19 6 | 48 57 53 44 57 43 49
XR19 | 1523 6 20 6 --- 17 12 5 | 20 26 22 --- 28 26 22
R20 | 1125 14 41 9 16 19 15 7 | 30 42 31 35 38 28 30
R21 | 1867 8 68 11 11 30 12 9 | 61 42 65 64 70 55 59
R22 | 2045 8 23 11 11 17 8 5 | 30 31 26 43 39 32 31
R24 | 1699 8 14 12 7 22 26 7 | 58 56 62 59 64 49 57
XR26 | 8458 22 56 27 --- 61 --- 22 | 27 51 39 --- 59 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 4676 13 34 13 15 21 17 |T 89 98 90 102 95 79 89
WRMS | 4676 14 34 12 14 21 17 |NE 88 99 89 105 96 74 88
MEDI | 1523 13 30 12 15 17 15 |MD 50 53 53 59 59 41 49
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