[IGSREPORT-30722] Wk 2395 IGLOS Final Orbits
acc
acc at igs.org
Fri Dec 19 12:45:18 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2395 (Nov 30, 2025 - Dec 06, 2025)
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 2.2395.
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:
igl2395[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2395 in the SP3 format.
igl23957.sum Combination Report for GPS Week 2395.
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.
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 | 2.3 ns
1 | 4.5 ns
2 | 8.0 ns
3 | 3.0 ns
4 | 7.9 ns
5 | 7.1 ns
6 | 2.7 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 | GFZ | R20
1 | GFZ | R20
2 | GFZ | R20
3 | GFZ | R20
4 | GFZ | R20
5 | GFZ | R20
6 | GFZ | R20
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 1.2395, 1a.2395).
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 2.2395.0-6)
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 3.2395.0-6).
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 2395 summary. (Nov 30, 2025 - Dec 06, 2025)
Table 1.2395.a GPS week : 2395 MJD: 61009.0-61015.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 -2 -14 11 25 .17 15 14 | -195 -581 3363 9053
| 0 1 2 16 13 26 .04 | 1220 2907
esa n/a| -2 0 0 -21 -4 54 -.13 21 20 | 2707 -205 3401 8730
| 2 1 2 15 14 53 .03 | 1597 2791
gfz n/a| 0 0 1 32 -6 16 -.07 19 17 | 0 -419 3406 7939
| 1 1 3 19 17 23 .06 | 0 3182
grg n/a| 0 0 4 -10 -44 -49 .27 21 16 | 4535 -262 3422 8748
| 1 1 4 14 25 45 .06 | 1854 3096
iac n/a| 0 0 -3 -6 21 -34 -.13 16 17 | 6438 -57 3692 9108
| 1 1 3 17 19 29 .05 | 2045 820
jgx n/a| 0 0 2 16 21 -11 -.15 18 18 | 2011 -145 3520 7763
| 1 1 1 14 12 47 .05 | 1458 3441
Table 1.2395.b GPS week : 2395 MJD: 61009.0-61015.0
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 | 5 7 7 11 6 8 12 |
R03 | 6 7 8 11 8 11 15 |
R04 | 8 8 7 9 6 10 9 |
R05 | 8 7 6 6 7 8 12 |
R07 | 8 8 7 10 7 10 17 |
R08 | 7 8 6 13 8 11 13 |
R09 | 7 7 7 5 5 6 8 |
R11 | 7 9 11 7 13 8 8 |
R12 | 7 5 8 9 7 6 7 |
R14 | 5 6 6 6 7 8 8 |
R15 | 5 7 7 7 7 6 9 |
R16 | 7 8 8 8 7 9 9 |
R17 | 9 7 7 8 7 8 8 |
R18 | 7 6 6 7 7 7 8 |
R19 | 10 9 7 7 8 11 12 |
R20 | 12 14 14 30 14 18 18 |
R21 | 8 9 8 9 8 9 8 |
R22 | 6 7 8 8 7 6 6 |
R24 | 9 9 9 9 9 9 9 |
R26 | 29 28 29 28 27 32 38 |
R27 | 22 25 26 24 23 26 30 |
R28 | 45 43 48 39 62 53 38 |
Table 1.2395.c GPS week : 2395 MJD: 61009.0-61015.0
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 2395 0 | 45 20 -85 521 1077 3934 80.7 1306 1306 | 2264 0
brd 2395 1 | -8 27 -50 -803 -247 9440 80.3 1509 1509 | 4543 0
brd 2395 2 | 19 63 -46 70 -323 8581 81.1 1401 1401 | 8035 0
brd 2395 3 | 8 7 -59 1614 338 4218 77.6 1467 1467 | 3011 0
brd 2395 4 | -7 10 -52 758 627 1210 76.8 1424 1424 | 7943 0
brd 2395 5 | -67 35 -126 -626 -1044 1952 79.6 1156 1156 | 7059 0
brd 2395 6 | 0 45 -25 1421 -17 4775 79.7 1162 1162 | 2727 0
-------------+------------------------------------------------------------+----------------
brd 2395 mean| -1 30 -63 422 58 4872 79.4 1346 1346 | 5083 0
brd 2395 sdev| 34 19 32 937 695 3105 1.6 142 142 | 2545 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 2.2395.0 GPS week: 2395 Day: 0 MJD: 61009
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 -5 -21 25 10 .14 14 14 | 980 -2300 2918 9698
esa n/a| -2 0 0 -26 -2 21 -.15 18 18 | 3199 -1780 2927 9181
gfz n/a| 1 0 2 22 0 28 -.08 17 17 | 0 -2045 2960 8823
grg n/a| 1 -1 4 -13 -42 0 .26 13 14 | 2974 -2382 3013 9268
iac n/a| 0 0 -2 13 11 -47 -.18 15 15 | 5384 -966 3035 9150
jgx n/a| 2 0 6 24 24 -18 -.15 18 18 | 3514 -2891 3110 9377
Table 2.2395.1 GPS week: 2395 Day: 1 MJD: 61010
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 -5 7 9 -18 .15 15 16 | -1361 -2218 3201 8382
esa n/a| -7 0 -1 -40 -16 104 -.11 20 19 | -326 -1188 3209 8120
gfz n/a| 1 -3 8 -3 5 37 -.06 19 17 | 0 -2281 3262 7636
grg n/a| 0 -1 1 2 -28 8 .30 15 14 | 4868 -1802 3252 8171
iac n/a| 0 0 -3 -10 19 -62 -.14 13 13 | 4625 178 3319 8902
jgx n/a| 1 1 3 37 31 -26 -.20 18 18 | -168 -1546 3328 8091
Table 2.2395.2 GPS week: 2395 Day: 2 MJD: 61011
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 -2 2 0 38 .20 16 17 | 1691 2969 3702 8491
esa n/a| -2 0 3 -15 -5 68 -.10 23 23 | 5001 4055 3759 7990
gfz n/a| -1 -1 0 55 -34 15 -.19 17 19 | 0 3909 3738 7140
grg n/a| 1 0 3 -4 -53 -80 .35 19 17 | 5438 3721 3817 8209
iac n/a| 0 0 -2 -12 36 -42 -.11 11 11 | 9771 -209 3946 8491
jgx n/a| 0 0 3 -2 24 52 -.13 16 16 | 4026 5092 3979 7103
Table 2.2395.3 GPS week: 2395 Day: 3 MJD: 61012
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 0 -4 -3 6 .15 13 13 | -248 -3522 3231 9517
esa n/a| -2 2 2 -43 -23 128 -.15 22 20 | 3140 -2727 3265 9991
gfz n/a| 2 0 5 29 19 0 -.06 34 21 | 0 -3694 3157 7919
grg n/a| 1 0 5 9 -71 -69 .24 16 13 | 3674 -2753 3252 9101
iac n/a| 0 1 -7 16 43 -23 -.14 17 17 | 4247 1103 3753 10549
jgx n/a| 1 -1 2 12 20 -25 -.18 19 19 | 2354 -3426 3319 7449
Table 2.2395.4 GPS week: 2395 Day: 4 MJD: 61013
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 -27 34 33 .10 12 12 | -664 -999 3461 8636
esa n/a| -2 0 3 0 -11 62 -.14 21 18 | 2846 -1452 3515 8576
gfz n/a| 0 2 0 33 -17 -23 -.02 16 15 | 0 -985 3549 7678
grg n/a| 3 0 4 -13 -78 -21 .29 18 16 | 8151 -1327 3471 7970
iac n/a| -3 -1 -7 0 39 27 -.17 18 17 | 8180 -770 4403 8730
jgx n/a| -1 0 0 29 13 -96 -.21 19 19 | 1821 -1519 3602 7034
Table 2.2395.5 GPS week: 2395 Day: 5 MJD: 61014
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 -34 6 52 .21 16 16 | -1742 4055 3432 9001
esa n/a| 0 0 0 -7 11 -29 -.16 21 21 | 2133 3577 3478 8643
gfz n/a| 2 0 0 47 -12 45 -.01 15 15 | 0 4274 3496 7656
grg n/a| 0 0 0 -21 -6 -110 .30 23 18 | 3822 4689 3472 8723
iac n/a| 0 0 2 -31 -6 -52 -.05 18 18 | 7366 910 3732 8394
jgx n/a| -1 0 1 10 34 29 -.09 18 18 | 803 4389 3589 6873
Table 2.2395.6 GPS week: 2395 Day: 6 MJD: 61015
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 -26 8 54 .20 16 13 | -21 -2058 3602 9650
esa n/a| 0 -2 0 -20 17 29 -.07 23 21 | 2961 -1923 3657 8612
gfz n/a| 0 0 -2 46 -6 16 -.06 18 18 | 0 -2112 3683 8726
grg n/a| -2 0 12 -31 -28 -73 .15 44 20 | 2819 -1980 3677 9794
iac n/a| 1 0 -4 -21 5 -41 -.10 21 24 | 5494 -647 3657 9541
jgx n/a| 3 1 3 1 -1 4 -.08 18 18 | 1733 -1116 3719 8415
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 3.2395.0 GPS week: 2395 Day: 0 MJD: 61009
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1091 7 14 11 9 13 10 5 | 103 106 102 100 112 16 103
R03 | 999 7 16 13 13 8 18 5 | 106 91 111 104 104 89 101
R04 | 1106 15 18 10 16 13 25 7 | 112 95 99 102 101 83 99
R05 | 858 9 14 28 16 12 21 7 | 121 120 135 121 124 113 122
R07E | 1211 15 17 25 11 10 21 7 | 126 119 127 111 114 104 117
R08 | 687 12 20 18 9 17 19 7 | 114 111 126 113 127 105 115
R09 | 881 17 10 14 11 19 17 6 | 22 31 38 35 42 25 31
R11 | 1675 19 17 22 14 13 8 7 | 20 26 41 32 25 29 26
R12 | 1331 18 17 15 17 16 6 7 | 80 71 73 77 79 76 75
R14 | 2430 11 10 10 6 9 17 4 | 49 51 46 45 43 43 45
R15 | 2058 11 9 10 9 9 11 4 | 71 62 55 63 62 54 61
R16 | 942 23 11 16 11 14 14 7 | 62 46 48 47 53 42 48
R17 | 1245 13 22 11 23 25 24 9 | 122 110 125 131 120 107 120
R18 | 1005 10 19 21 7 13 18 6 | 108 125 103 111 112 102 109
XR19 | 3062 18 20 13 --- 13 --- 9 | 61 60 56 --- 55 --- 57
XR20 | 523 12 --- 380 13 24 --- 12 | 931 --- 888 935 929 --- 931
R21 | 653 9 31 11 7 22 19 8 | 129 111 135 132 134 112 126
XR22 | 646 11 15 11 9 12 --- 5 | 62 58 64 67 63 --- 62
R24 | 1356 9 30 18 15 17 25 8 | 128 109 137 136 139 111 128
XR26E | 7030 42 56 44 --- 54 --- 28 | 84 52 39 --- 86 --- 89
XR27E | 6707 40 38 --- 20 51 --- 22 | 36 51 --- 30 33 --- 32
XR28 |15399 44 --- --- --- 45 --- 44 | 184 --- --- --- 162 --- 172
------+-----------------------------------------+-------------------------------------
RMS | 1306 14 18 17 13 15 18 |T 128 80 127 131 128 75 125
WRMS | 1306 14 18 17 14 15 18 |NE 136 81 132 138 136 73 133
MEDI | 1106 12 17 14 11 13 18 |MD 103 71 99 102 101 83 99
Table 3.2395.1 GPS week: 2395 Day: 1 MJD: 61010
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02 | 1517 12 20 22 18 12 14 7 | 69 76 74 69 76 17 69
R03 | 2368 10 20 13 20 12 17 7 | 63 55 55 77 56 52 58
R04 | 1937 19 21 13 12 11 22 7 | 70 61 59 59 57 51 58
R05 | 963 14 18 17 17 15 17 7 | 79 85 88 83 83 70 80
R07E | 2169 20 16 17 15 15 15 7 | 92 92 85 79 75 73 81
R08 | 882 10 27 26 15 15 15 8 | 84 88 97 88 85 79 85
R09 | 1011 13 11 15 16 14 20 6 | 16 24 35 31 31 20 24
R11 | 1034 19 20 13 27 14 17 8 | 17 52 39 51 30 26 33
R12 | 881 14 10 16 11 9 9 5 | 69 66 70 71 62 66 66
R14 | 2222 15 17 10 11 9 12 5 | 38 40 35 31 35 31 34
R15 | 1548 23 11 25 10 8 16 7 | 60 55 45 57 51 49 52
R16 | 1666 21 14 25 14 11 19 8 | 53 46 45 54 43 35 44
R17 | 1053 10 14 14 19 12 26 7 | 67 66 67 78 59 53 65
R18 | 1255 10 23 10 8 15 13 6 | 60 66 71 64 52 60 61
XR19 | 3996 15 14 16 --- 16 --- 9 | 29 35 43 --- 30 --- 32
XR20 | 1064 15 --- 406 15 24 --- 13 | 753 --- 714 763 748 --- 754
R21 | 839 11 36 27 9 11 19 9 | 65 52 78 57 58 58 61
XR22 | 622 14 16 15 11 14 --- 7 | 32 34 32 38 44 --- 35
R24 | 1412 8 28 20 10 19 25 8 | 66 59 80 66 74 58 68
XR26E | 7998 43 47 51 --- 52 --- 28 | 69 40 39 --- 61 --- 69
XR27E | 9433 39 47 --- 33 49 --- 24 | 38 43 --- 37 36 --- 35
XR28 |17896 49 --- --- --- 37 --- 43 | 63 --- --- --- 92 --- 71
------+-----------------------------------------+-------------------------------------
RMS | 1509 15 20 19 15 13 18 |T 88 56 92 97 88 49 87
WRMS | 1509 16 19 17 14 13 18 |NE 92 56 95 102 92 48 92
MEDI | 1412 14 18 16 15 14 17 |MD 63 55 59 64 57 52 61
Table 3.2395.2 GPS week: 2395 Day: 2 MJD: 61011
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02 | 1555 10 14 12 20 11 --- 6 | 87 80 96 80 95 --- 88
R03 | 1841 18 20 24 18 8 16 7 | 95 83 107 86 92 77 89
R04 | 1645 25 14 12 11 6 18 6 | 94 79 80 82 79 73 80
R05 | 992 6 13 14 15 11 14 5 | 92 94 96 97 95 92 93
R07E | 2128 9 15 24 15 11 19 7 | 115 103 123 101 115 102 110
R08 | 1326 10 20 12 16 15 10 6 | 107 115 123 108 116 112 114
R09 | 1448 15 13 26 7 10 8 6 | 21 24 27 21 26 22 20
R11 | 755 22 44 17 42 11 13 11 | 11 63 22 64 21 18 25
R12 | 845 14 15 21 31 8 11 7 | 58 53 60 59 61 58 56
R14 | 1506 13 15 10 15 10 12 5 | 39 39 30 49 32 35 35
R15 | 1997 24 17 13 11 10 12 6 | 53 39 40 44 33 40 39
R16 | 979 24 22 14 23 16 11 8 | 44 45 42 48 35 40 37
R17 | 852 10 19 18 12 9 26 7 | 88 81 96 88 90 76 87
R18 | 1899 10 22 8 12 11 15 6 | 79 85 75 79 77 72 77
XR19 | 3648 16 12 11 --- 11 --- 7 | 44 48 38 --- 42 --- 42
XR20 | 773 20 --- 398 16 20 --- 13 | 900 --- 898 905 896 --- 902
R21 | 836 17 36 16 16 6 18 8 | 94 78 92 88 89 77 86
XR22 | 645 17 14 22 12 11 --- 7 | 47 45 48 50 41 --- 43
R24 | 655 10 32 14 19 17 24 8 | 89 80 100 105 103 82 94
XR26E | 9790 37 48 63 --- 47 --- 28 | 95 34 41 --- 91 --- 92
XR27E | 6497 42 43 --- 43 47 --- 25 | 20 34 --- 23 29 --- 24
XR28 |14899 61 --- --- --- 37 --- 48 | 121 --- --- --- 123 --- 121
------+-----------------------------------------+-------------------------------------
RMS | 1401 16 23 17 19 11 16 |T 108 65 111 114 108 65 107
WRMS | 1401 17 23 19 17 11 16 |NE 113 66 115 120 112 62 112
MEDI | 1448 16 17 14 16 11 14 |MD 87 63 75 80 79 73 80
Table 3.2395.3 GPS week: 2395 Day: 3 MJD: 61012
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02 | 1596 12 22 37 18 22 --- 10 | 93 105 95 89 112 --- 97
R03 | 963 8 23 54 16 20 25 10 | 95 77 124 83 105 80 90
R04 | 1150 19 16 41 20 8 24 9 | 88 73 92 71 74 65 76
R05 | 1232 11 19 24 13 12 8 6 | 94 104 80 101 95 91 95
R07E | 3491 9 20 56 12 25 16 10 | 79 65 75 78 90 64 74
R08 | 1512 10 21 81 20 26 23 13 | 79 64 130 67 93 63 76
R09 | 801 9 18 9 10 8 9 5 | 22 30 27 21 23 21 21
R11 | 960 10 16 9 18 24 14 7 | 14 29 23 27 21 19 17
R12 | 736 11 38 11 27 9 9 8 | 32 63 36 29 33 33 32
R14 | 1191 7 16 15 10 8 19 5 | 35 42 34 26 32 22 30
R15 | 1875 19 12 22 7 13 10 6 | 47 36 32 36 39 33 37
R16 | 785 24 16 20 11 12 22 8 | 37 36 31 30 27 33 29
R17 | 847 7 19 25 12 21 24 8 | 95 87 102 99 104 83 94
R18 | 2351 9 25 20 14 12 22 7 | 80 96 84 79 86 69 81
XR19 | 4315 9 16 16 --- 13 --- 7 | 46 50 52 --- 42 --- 45
XR20 | 843 35 --- 386 35 54 --- 29 | 373 --- 436 358 333 --- 354
R21 | 631 8 26 19 24 12 29 9 | 110 104 116 122 106 98 108
R22 | 633 16 16 18 14 23 9 7 | 53 49 53 58 45 19 49
R24 | 1217 9 30 26 11 24 14 8 | 103 92 105 103 118 100 103
XR26E |11555 29 56 67 --- 52 --- 27 | 72 52 33 --- 74 --- 75
XR27E | 9382 27 55 --- 36 53 --- 24 | 24 48 --- 23 24 --- 17
XR28 |15200 33 --- --- --- 46 --- 39 | 121 --- --- --- 134 --- 122
------+-----------------------------------------+-------------------------------------
RMS | 1467 13 22 34 16 17 19 |T 81 65 88 78 82 55 78
WRMS | 1467 13 20 21 13 17 19 |NE 85 66 91 82 85 55 81
MEDI | 1191 10 19 22 14 20 16 |MD 79 63 75 71 74 63 75
Table 3.2395.4 GPS week: 2395 Day: 4 MJD: 61013
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02 | 1278 9 11 11 12 17 --- 6 | 69 69 77 65 87 --- 72
R03 | 1458 8 22 20 17 12 28 8 | 77 61 82 79 82 67 74
R04 | 1591 13 15 9 18 10 15 6 | 67 55 58 54 66 55 59
R05 | 1379 13 18 19 20 15 10 7 | 86 85 77 69 81 82 79
R07E | 3188 11 20 19 15 13 18 7 | 81 80 87 95 93 84 85
R08 | 1046 10 17 18 14 27 19 7 | 76 77 82 90 101 77 83
R09 | 556 9 12 10 8 10 15 4 | 24 31 30 24 21 17 22
R11 | 1615 12 42 31 40 24 16 12 | 19 47 35 42 20 18 13
R12 | 936 11 19 13 15 19 19 7 | 65 73 64 60 57 72 64
R14 | 897 7 16 17 10 23 13 6 | 44 50 30 39 54 50 42
R15 | 1536 18 14 13 18 10 8 6 | 63 57 60 52 55 58 57
R16 | 642 23 12 9 18 11 11 7 | 51 50 49 45 47 41 46
R17 | 661 8 21 12 15 19 22 7 | 70 62 64 79 77 57 68
R18 | 2108 8 23 10 10 13 24 6 | 62 66 59 66 67 48 60
XR19 | 4429 10 14 14 --- 18 --- 8 | 31 36 37 --- 44 --- 36
XR20 | 1870 11 --- 370 19 30 --- 14 | 913 --- 915 910 914 --- 914
R21 | 873 5 24 13 16 18 33 8 | 80 71 82 86 77 66 77
R22 | 576 17 9 20 11 17 12 7 | 38 35 32 39 29 19 33
R24 | 1128 9 29 14 16 29 21 8 | 76 67 66 75 86 64 72
XR26E | 6569 18 57 50 --- 60 --- 26 | 98 70 48 --- 92 --- 97
XR27E |13272 24 42 --- 36 60 --- 23 | 21 36 --- 33 28 --- 21
XR28 |18038 46 --- --- --- 83 --- 62 | 113 --- --- --- 100 --- 105
------+-----------------------------------------+-------------------------------------
RMS | 1424 12 21 16 18 18 19 |T 101 58 101 105 103 54 99
WRMS | 1424 12 18 15 16 17 19 |NE 106 58 105 110 108 52 104
MEDI | 1379 11 18 14 16 18 16 |MD 67 61 60 65 67 57 64
Table 3.2395.5 GPS week: 2395 Day: 5 MJD: 61014
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02 | 1221 15 20 17 12 13 --- 8 | 78 79 90 82 87 --- 82
R03 | 671 15 19 11 51 15 23 10 | 122 110 122 126 125 122 119
R04 | 1112 16 14 25 21 26 24 10 | 121 109 127 110 104 113 114
R05 | 1061 11 14 19 23 15 19 7 | 123 133 122 136 119 120 124
R07E | 1934 17 20 17 30 30 16 9 | 135 129 137 132 116 127 128
R08 | 1445 22 23 16 46 17 24 11 | 125 122 125 136 125 123 124
R09 | 739 18 18 10 14 11 7 6 | 22 29 32 29 30 28 26
R11 | 1694 21 14 14 15 12 19 7 | 16 25 22 28 20 30 19
R12 | 1060 9 21 15 10 15 9 6 | 58 49 50 62 59 52 53
R14 | 907 8 26 18 17 24 9 8 | 45 64 39 47 56 45 46
R15 | 1602 18 12 8 12 9 12 5 | 59 63 52 53 59 49 55
R16 | 839 28 19 11 19 15 21 8 | 52 43 43 41 40 36 40
R17 | 543 12 24 8 14 21 21 7 | 59 59 60 65 72 54 60
R18 | 1271 12 23 15 11 13 16 7 | 52 64 53 55 56 46 53
XR19 | 3745 12 22 11 --- 28 --- 11 | 37 37 39 --- 54 --- 40
XR20 | 3922 16 --- 360 19 34 --- 17 | 732 --- 689 727 723 --- 728
R21 | 753 10 28 23 16 10 22 8 | 65 55 74 71 62 60 64
R22 | 1069 16 11 12 8 19 11 6 | 37 34 37 38 30 15 32
R24 | 676 13 32 9 18 25 22 9 | 65 57 55 69 71 54 60
XR26E |10528 36 58 60 --- 63 --- 32 | 148 86 70 --- 141 --- 143
XR27E |12820 28 37 --- 56 56 --- 26 | 30 37 --- 40 27 --- 23
XR28 |20908 49 --- --- --- 56 --- 53 | 129 --- --- --- 119 --- 121
------+-----------------------------------------+-------------------------------------
RMS | 1155 16 21 15 23 18 18 |T 105 69 101 107 104 67 102
WRMS | 1155 16 21 15 18 18 18 |NE 105 66 101 110 105 63 103
MEDI | 1112 16 20 15 17 17 19 |MD 59 59 55 65 62 52 60
Table 3.2395.6 GPS week: 2395 Day: 6 MJD: 61015
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02 | 1821 14 13 11 47 32 --- 11 | 84 89 88 101 92 --- 88
R03 | 1323 24 25 24 94 23 19 15 | 90 69 93 105 97 86 84
R04 | 1130 19 17 19 31 19 19 9 | 113 116 121 100 107 107 111
R05 | 897 16 24 30 27 35 24 11 | 119 113 131 128 143 116 123
R07E | 1080 21 18 27 103 31 18 16 | 103 95 108 103 106 92 95
R08 | 1648 12 18 17 80 32 14 13 | 90 93 80 107 106 91 89
R09 | 1206 15 21 19 6 19 14 7 | 23 27 34 29 32 28 26
R11 | 949 14 36 13 12 16 12 8 | 13 25 22 16 18 24 14
R12 | 1602 17 11 9 14 14 19 6 | 77 71 70 69 80 72 73
R14 | 554 5 32 9 10 20 17 7 | 56 64 51 52 63 51 54
R15 | 1018 13 23 18 15 15 23 8 | 78 72 71 66 77 67 70
R16 | 737 16 20 12 33 16 21 8 | 69 65 64 53 67 50 60
R17 | 787 19 20 10 18 12 19 7 | 100 88 92 102 101 81 93
R18 | 698 11 21 23 17 16 15 8 | 81 97 74 81 92 73 81
XR19 | 2955 16 18 22 --- 26 --- 12 | 47 49 47 --- 60 --- 48
XR20 | 6040 16 --- 365 22 34 --- 17 | 910 --- 887 913 910 --- 909
R21 | 587 9 24 18 20 15 14 7 | 105 90 116 116 109 100 105
R22 | 2293 14 17 10 17 13 11 6 | 43 47 44 52 40 17 42
R24 | 603 15 29 11 21 22 18 8 | 110 88 106 115 117 92 104
XR26E |15213 32 --- --- --- 44 --- 38 | 166 --- --- --- 154 --- 160
XR27E |11740 35 34 --- 84 63 --- 30 | 42 55 --- 78 49 --- 39
XR28 |24304 32 --- --- --- 44 --- 38 | 173 --- --- --- 145 --- 159
------+-----------------------------------------+-------------------------------------
RMS | 1162 16 23 18 44 21 18 |T 122 74 121 125 125 71 119
WRMS | 1162 13 21 18 20 24 18 |NE 125 74 121 129 129 70 122
MEDI | 1130 16 21 18 21 20 18 |MD 84 72 80 100 92 73 84
More information about the IGSREPORT
mailing list