[IGSREPORT-30499] Wk 2370 IGLOS Final Orbits
acc
acc at igs.org
Fri Jun 27 06:11:11 UTC 2025
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2370 (Jun 08, 2025 - Jun 14, 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 2.2370.
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:
igl2370[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2370 in the SP3 format.
igl23707.sum Combination Report for GPS Week 2370.
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 | 2.2 ns
1 | 3.9 ns
2 | 2.2 ns
3 | -0.9 ns
4 | 1.8 ns
5 | 0.6 ns
6 | 3.7 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 | ALL | R26
0 | ESA | R19 R20
0 | GFZ | R19
0 | GRG | R19
1 | ESA | R19
1 | GFZ | R19
1 | GRG | R19
2 | ALL | R27
2 | ESA | R19
2 | GFZ | R19 R26
2 | GRG | R19
3 | ESA | R19
3 | GFZ | R19
4 | ESA | R19 R20
4 | GFZ | R19
5 | ESA | R19 R20
5 | GFZ | R19
6 | ESA | R19
6 | GFZ | R19
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 1.2370, 1a.2370).
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 2.2370.0-6)
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 3.2370.0-6).
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 2370 summary. (Jun 08, 2025 - Jun 14, 2025)
Table 1.2370.a GPS week : 2370 MJD: 60834.0-60840.0
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 6 -8 -33 8 .16 16 14 | 4166 237 3617 8400
| 1 0 1 8 11 37 .05 | 1661 1511
esa n/a| -2 -1 0 2 -5 -45 -.10 36 36 | 4882 -739 3607 8495
| 1 1 3 13 12 46 .08 | 1651 2535
gfz n/a| 1 0 0 28 13 29 -.10 18 16 | 0 -386 3642 8371
| 1 1 3 11 20 29 .05 | 0 1709
grg n/a| 2 0 0 -16 4 -36 .38 24 16 | 1903 -303 3683 8174
| 0 1 6 18 8 28 .04 | 1235 1641
iac n/a| 0 0 -1 9 26 -4 -.17 15 15 | 3114 -314 3622 8845
| 1 1 2 22 19 60 .07 | 1135 1381
jgx n/a| 0 0 -5 0 -1 27 -.19 21 21 | 5012 -231 3728 8495
| 1 0 3 12 12 35 .04 | 1582 1446
Table 1.2370.b GPS week : 2370 MJD: 60834.0-60840.0
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 7 8 15 9 8 9 |
R03 | 6 6 9 12 7 5 8 |
R04 | 8 6 8 12 8 8 6 |
R05 | 6 8 9 9 8 6 7 |
R07 | 8 6 9 12 8 6 8 |
R08 | 8 7 11 14 9 7 8 |
R09 | 6 7 8 8 8 9 8 |
R11 | 6 7 6 6 7 8 8 |
R12 | 7 8 6 6 6 8 8 |
R14 | 6 6 5 4 6 6 5 |
R15 | 8 7 8 6 7 8 8 |
R16 | 6 9 8 6 7 7 6 |
R17 | 5 6 6 5 6 8 7 |
R18 | 7 6 7 8 9 8 8 |
R19 | 13 19 21 8 10 10 10 |
R20 | 24 24 23 24 17 21 20 |
R21 | 8 6 6 8 7 6 6 |
R22 | 9 9 8 7 8 8 8 |
R24 | 7 6 6 9 7 6 8 |
R25 | 52 70 67 103 53 75 55 |
R26 | --- 67 44 27 26 27 28 |
R27 | 62 86 --- 46 34 35 31 |
Table 1.2370.c GPS week : 2370 MJD: 60834.0-60840.0
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 2370 0 | -88 -52 209 -1410 -457 5492 81.4 1587 1587 | 2175 0
brd 2370 1 | 58 66 265 -259 756 7809 83.2 1862 1862 | 3881 0
brd 2370 2 | 35 62 34 -2452 -523 14180 83.6 2354 2354 | 2195 0
brd 2370 3 | 33 91 126 -604 1775 14560 81.8 1897 1897 | -869 0
brd 2370 4 | -9 66 147 -558 506 16720 80.1 2079 2079 | 1752 0
brd 2370 5 | 63 -83 239 -365 2764 16250 78.2 2311 2311 | 598 0
brd 2370 6 | -43 173 42 1593 933 19550 80.0 2664 2664 | 3672 0
-------------+------------------------------------------------------------+----------------
brd 2370 mean| 7 46 152 -579 822 13508 81.2 2107 2107 | 1914 0
brd 2370 sdev| 56 87 91 1229 1172 5043 1.9 362 362 | 1663 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 2.2370.0 GPS week: 2370 Day: 0 MJD: 60834
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 7 -12 -19 -36 .14 15 13 | 1636 -54 3480 11021
esa n/a| -4 -2 0 18 2 36 -.20 34 29 | 4006 -631 3476 9018
gfz n/a| 0 0 2 13 -22 -17 -.11 19 14 | 0 -597 3436 9251
grg n/a| 3 -1 0 -44 1 -65 .37 19 12 | 2152 -349 3464 9111
iac n/a| 0 3 -2 33 41 89 -.13 14 13 | 1721 -1314 3412 10493
jgx n/a| 1 0 -9 0 0 8 -.17 22 22 | 2154 -98 3535 9223
Table 2.2370.1 GPS week: 2370 Day: 1 MJD: 60835
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 -2 -43 -11 .10 12 12 | 6686 1302 4090 8404
esa n/a| 0 -2 -1 5 9 -21 -.11 32 27 | 6546 1308 4086 9000
gfz n/a| 2 -2 4 14 5 68 -.11 18 17 | 0 1165 4039 8425
grg n/a| 2 0 2 -13 10 -1 .43 23 18 | 3480 920 4077 8242
iac n/a| -2 1 -4 14 41 -50 -.13 14 15 | 5142 670 4038 8662
jgx n/a| 1 0 -7 14 18 52 -.14 25 25 | 6399 1640 4125 8559
Table 2.2370.2 GPS week: 2370 Day: 2 MJD: 60836
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 -9 -37 46 .22 17 15 | 3530 1705 4297 9143
esa n/a| -1 0 -3 -12 -19 -97 -.02 36 49 | 2302 2236 4239 9718
gfz n/a| 0 -1 -4 27 16 12 -.13 15 13 | 0 1433 4365 9371
grg n/a| 2 3 8 -35 -2 -4 .36 31 22 | 1295 1364 4274 9323
iac n/a| 1 0 -2 13 36 -41 -.10 14 16 | 2482 990 4274 9465
jgx n/a| 0 -2 -8 9 -3 81 -.16 22 22 | 4962 273 4558 9476
Table 2.2370.3 GPS week: 2370 Day: 3 MJD: 60837
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 0 -47 7 .22 18 15 | 4187 -2831 3681 9298
esa n/a| 0 1 1 2 -4 -42 .03 35 35 | 4396 -3230 3710 10668
gfz n/a| 1 1 2 26 12 45 -.01 17 16 | 0 -3799 3745 9916
grg n/a| 1 -2 -7 -14 -3 -55 .32 43 17 | 752 -3683 3824 9697
iac n/a| 0 -1 0 -1 41 -4 -.17 15 15 | 3223 -2735 3710 9996
jgx n/a| 0 0 -1 7 10 8 -.16 21 21 | 3992 -3085 3776 10060
Table 2.2370.4 GPS week: 2370 Day: 4 MJD: 60838
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 5 -2 -18 47 .12 14 13 | 3350 -164 3437 6095
esa n/a| -4 0 5 18 8 -35 -.12 40 48 | 3971 255 3441 6485
gfz n/a| 1 0 -1 35 10 7 -.15 20 19 | 0 -37 3455 6395
grg n/a| 3 1 -8 8 17 -68 .39 19 14 | 1559 327 3548 6120
iac n/a| 0 0 1 -30 14 9 -.14 16 15 | 2689 -769 3418 7121
jgx n/a| 1 -1 -1 -5 -3 -15 -.22 17 17 | 4856 -596 3608 6348
Table 2.2370.5 GPS week: 2370 Day: 5 MJD: 60839
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 7 -3 -37 42 .13 15 14 | 3967 864 3325 7996
esa n/a| -2 -3 1 -13 -21 -97 -.13 40 33 | 6444 -4976 3323 7450
gfz n/a| 1 0 1 46 23 46 -.09 18 14 | 0 -381 3380 7944
grg n/a| 2 1 0 -5 -1 -43 .43 17 14 | 500 -164 3478 7610
iac n/a| -2 2 -2 1 16 -85 -.25 15 15 | 2549 -3 3380 8436
jgx n/a| -1 0 -7 -22 -10 54 -.26 21 21 | 6026 477 3479 8172
Table 2.2370.6 GPS week: 2370 Day: 6 MJD: 60840
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 5 -23 -30 -36 .19 17 14 | 5807 842 3012 6847
esa n/a| -4 -1 -5 -4 -15 -64 -.12 33 28 | 6514 -138 2978 7132
gfz n/a| 2 0 -2 33 46 41 -.07 17 16 | 0 -487 3078 7300
grg n/a| 2 1 4 -7 10 -14 .36 16 13 | 3583 -540 3120 7120
iac n/a| -1 0 0 35 -8 49 -.28 17 18 | 3992 959 3128 7743
jgx n/a| -1 0 -2 -7 -18 1 -.22 18 18 | 6697 -232 3016 7627
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 3.2370.0 GPS week: 2370 Day: 0 MJD: 60834
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 1294 15 14 10 13 23 9 6 | 99 103 104 106 109 21 103
R03E | 885 14 13 11 14 9 13 5 | 113 106 112 120 107 105 110
R04E | 823 15 23 13 17 11 19 7 | 80 72 77 89 80 73 78
R05E | 1591 8 17 13 15 9 19 6 | 77 77 83 87 76 63 77
R07E | 1633 21 14 16 14 13 17 7 | 66 60 62 66 62 53 60
R08E | 890 11 26 15 16 16 16 7 | 119 121 116 120 118 115 117
R09 | 2426 13 14 16 7 9 13 5 | 23 34 37 29 31 31 28
R11 | 2222 13 11 16 9 15 12 5 | 44 41 48 49 47 41 43
R12 | 877 10 26 13 10 10 19 6 | 48 64 42 49 47 39 46
R14 | 944 8 16 16 8 19 7 5 | 42 47 41 36 36 36 38
R15 | 1183 11 20 18 25 20 7 8 | 64 66 64 48 53 52 56
R16 | 1477 9 20 17 12 12 7 5 | 67 76 76 64 66 67 68
R17 | 2349 11 15 10 13 7 11 5 | 73 68 71 66 68 65 68
R18 | 1023 7 31 12 11 12 9 6 | 56 73 53 51 57 49 55
XR19 | 2630 11 319 376 376 15 --- 13 | 28 160 183 203 36 --- 31
R20 | 2691 36 120 43 54 15 72 23 | 102 58 117 102 100 84 97
R21 | 1115 9 17 29 14 11 25 8 | 71 66 81 76 62 56 67
XR22 | 2754 15 19 24 12 14 --- 8 | 27 36 46 39 39 --- 34
R24 | 1594 12 17 22 11 10 14 6 | 72 59 80 80 71 66 71
XR25 |12585 47 --- --- --- 55 --- 51 | 131 --- --- --- 132 --- 123
XR27E | 8251 58 --- --- --- 66 --- 62 | 206 --- --- --- 253 --- 221
------+-----------------------------------------+-------------------------------------
RMS | 1586 15 34 19 19 14 22 |T 80 77 85 77 82 59 79
WRMS | 1586 13 29 14 12 13 22 |NE 60 65 72 68 60 53 58
MEDI | 1591 12 17 16 13 13 13 |MD 71 66 76 66 66 56 68
Table 3.2370.1 GPS week: 2370 Day: 1 MJD: 60835
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R02E | 1425 9 23 21 19 15 15 7 | 98 96 97 91 98 29 95
R03E | 1602 8 16 13 13 12 19 6 | 84 74 86 88 81 71 81
R04E | 1166 9 20 12 14 13 19 6 | 51 47 50 53 51 42 48
R05E | 904 9 29 23 21 20 14 8 | 106 117 119 118 101 106 109
R07E | 1771 12 19 14 14 8 18 6 | 47 42 49 46 42 31 42
R08E | 906 8 26 16 15 14 19 7 | 110 111 111 117 110 110 110
R09 | 1990 8 28 22 12 15 9 7 | 16 31 23 20 26 22 19
R11 | 3533 10 17 17 18 20 12 7 | 25 20 32 33 28 26 24
R12 | 1428 13 11 25 23 10 20 7 | 34 37 27 45 34 26 31
R14 | 1242 8 21 14 9 14 9 5 | 31 44 28 28 34 25 29
R15 | 1055 15 22 14 20 14 8 6 | 47 49 51 32 40 40 42
R16 | 1107 10 28 16 41 13 10 8 | 52 61 59 41 53 55 51
R17 | 1603 7 26 11 15 7 12 5 | 43 47 41 38 43 42 42
R18 | 1165 5 25 10 13 13 19 6 | 34 36 33 34 41 30 34
XR19 | 2519 16 305 395 387 21 --- 19 | 24 123 92 202 39 --- 27
R20 | 4395 31 96 34 58 27 84 23 | 40 28 39 60 48 49 41
R21 | 875 9 26 14 11 10 19 6 | 36 31 39 37 35 35 35
XR22 | 1637 15 32 15 12 15 --- 8 | 18 29 33 36 29 --- 24
R24 | 1342 9 18 11 16 10 14 5 | 43 33 36 56 42 55 43
XR25 |13796 60 --- --- --- 81 --- 70 | 93 --- --- --- 95 --- 70
XR26E |12657 56 --- --- --- 78 --- 66 | 198 --- --- --- 170 --- 184
XR27E |19078 73 --- --- --- 100 --- 86 | 204 --- --- --- 104 --- 158
------+-----------------------------------------+-------------------------------------
RMS | 1861 12 32 18 23 14 25 |T 65 55 55 61 61 46 60
WRMS | 1861 12 27 17 18 15 25 |NE 38 43 41 50 41 36 36
MEDI | 1428 9 25 15 15 14 15 |MD 43 44 41 45 42 40 42
Table 3.2370.2 GPS week: 2370 Day: 2 MJD: 60836
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2328 10 19 13 24 18 --- 8 | 58 52 59 80 54 --- 57
R03E | 1506 14 18 13 36 17 22 8 | 152 147 152 176 141 159 152
R04E | 1324 12 21 10 33 14 15 7 | 89 91 87 114 90 77 89
R05E | 953 19 23 13 32 24 10 9 | 86 73 88 84 70 78 79
R07E | 2080 11 27 13 44 9 17 8 | 66 60 64 101 60 62 65
R08E | 1036 14 20 14 54 20 24 10 | 129 138 132 153 142 122 133
R09 | 2787 20 31 15 14 14 18 8 | 23 27 34 31 33 21 24
R11 | 3356 11 22 15 6 10 11 5 | 59 62 54 59 61 57 57
R12 | 2118 13 26 10 16 12 12 6 | 39 37 29 40 32 28 32
R14 | 3234 7 13 8 9 16 10 5 | 29 32 27 32 39 24 29
R15 | 1656 18 39 13 13 9 20 8 | 48 56 41 49 39 36 42
R16 | 1438 20 25 19 28 12 10 8 | 51 49 49 31 39 38 41
R17 | 914 6 24 10 14 12 11 5 | 53 56 52 61 44 48 50
R18 | 1522 11 35 11 13 9 19 7 | 39 47 33 38 40 37 37
XR19 | 1854 21 320 399 374 20 --- 21 | 24 98 130 198 43 --- 31
R20 | 5762 40 104 37 70 21 64 23 | 82 41 79 83 63 66 67
R21 | 1150 9 30 15 14 6 10 6 | 49 38 53 47 47 45 46
XR22 | 2324 17 19 10 11 16 --- 7 | 20 22 28 25 31 --- 23
R24 | 1365 12 17 11 12 12 13 5 | 59 52 51 54 54 51 52
XR25 |18901 68 --- --- --- 66 --- 67 | 162 --- --- --- 110 --- 132
XR26E |11868 44 --- 598 --- 42 --- 43 | 118 --- 499 --- 137 --- 126
------+-----------------------------------------+-------------------------------------
RMS | 2354 17 36 15 31 14 22 |T 69 62 87 76 66 59 66
WRMS | 2354 15 49 13 22 16 22 |NE 52 47 50 57 48 41 47
MEDI | 1854 14 24 13 16 14 13 |MD 58 52 53 59 54 48 52
Table 3.2370.3 GPS week: 2370 Day: 3 MJD: 60837
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2751 10 20 12 82 20 --- 14 | 71 73 71 109 77 --- 72
R03E | 1161 16 25 12 76 23 17 12 | 110 110 114 138 111 114 111
R04E | 960 18 21 22 69 23 18 12 | 119 127 126 153 119 115 120
R05E | 1656 14 22 15 54 17 9 9 | 94 97 93 123 85 88 92
R07E | 2091 17 18 19 74 15 17 11 | 58 53 62 81 58 56 55
R08E | 1837 19 31 26 85 21 12 13 | 127 135 134 131 126 130 126
R09 | 2455 16 35 17 14 16 10 8 | 13 23 33 34 32 23 23
R11 | 2635 11 21 13 8 14 8 5 | 31 45 28 28 28 31 29
R12 | 1856 10 13 11 12 13 16 5 | 40 39 38 36 40 25 34
R14 | 1969 11 12 11 10 9 5 4 | 31 33 39 34 40 31 34
R15 | 1710 11 20 14 11 12 10 5 | 43 37 39 37 38 37 37
R16 | 1557 13 20 12 12 10 9 5 | 49 46 39 40 39 37 40
R17 | 851 9 10 11 19 11 8 5 | 55 51 58 64 47 48 52
R18 | 1894 13 42 14 16 8 8 7 | 40 51 32 35 33 30 34
XR19 | 1567 13 339 402 13 8 --- 8 | 18 94 165 157 21 --- 18
R20 | 3449 50 99 27 43 20 67 23 | 74 46 77 64 67 51 60
R21 | 994 14 41 10 17 10 18 8 | 52 56 44 54 51 40 46
XR22 | 2906 15 16 12 16 11 --- 6 | 15 25 25 26 23 --- 19
R24 | 1395 15 22 24 13 14 20 8 | 58 45 62 63 57 45 53
XR25 |22419 109 --- --- --- 97 --- 103 | 144 --- --- --- 107 --- 99
XR26E | 8284 34 48 45 --- 57 --- 27 | 139 88 121 --- 122 --- 134
XR27E | 8701 48 --- --- --- 44 --- 46 | 145 --- --- --- 151 --- 148
------+-----------------------------------------+-------------------------------------
RMS | 1896 18 35 17 43 15 21 |T 69 63 70 74 66 56 65
WRMS | 1896 15 35 16 17 15 21 |NE 47 45 52 51 44 36 41
MEDI | 1856 14 21 14 16 14 10 |MD 55 51 58 63 51 40 52
Table 3.2370.4 GPS week: 2370 Day: 4 MJD: 60838
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 2690 10 15 19 32 12 --- 9 | 110 115 111 107 107 --- 108
R03E | 1753 10 39 14 14 10 13 7 | 77 67 71 73 73 69 72
R04E | 1232 10 24 28 26 12 12 8 | 91 88 91 93 92 84 89
R05E | 2495 12 16 18 31 13 13 8 | 54 45 52 68 57 51 51
R07E | 1520 13 16 18 17 19 17 7 | 50 48 50 49 55 42 47
R08E | 1260 9 20 25 18 27 20 9 | 141 142 139 142 140 134 138
R09 | 1640 12 35 20 16 11 13 7 | 31 25 46 47 32 37 34
R11 | 2393 14 20 19 15 13 14 7 | 55 66 52 64 52 55 54
R12 | 1854 11 22 17 13 11 7 5 | 41 46 30 32 43 43 38
R14 | 2173 9 20 19 11 11 8 5 | 34 32 42 29 30 32 31
R15 | 1070 15 24 14 13 21 7 7 | 52 53 44 45 40 42 44
R16 | 1550 12 33 22 9 7 8 6 | 48 63 48 42 50 47 46
R17 | 1337 9 13 15 9 11 21 6 | 49 47 51 50 54 38 47
R18 | 1916 9 55 12 20 10 14 8 | 35 63 34 35 33 27 33
XR19 | 1448 11 345 411 10 17 --- 9 | 24 82 143 116 33 --- 23
R20 | 5071 37 120 32 36 29 36 17 | 60 43 49 72 56 54 55
R21 | 1034 12 31 14 11 7 18 6 | 45 44 44 47 40 31 40
XR22 | 2705 15 19 15 10 20 --- 8 | 21 34 32 33 33 --- 26
R24 | 1440 12 23 19 11 16 20 7 | 51 44 55 56 55 42 49
XR25 |22281 46 --- --- --- 60 --- 53 | 130 --- --- --- 95 --- 102
XR26E | 8032 30 49 54 --- 54 --- 26 | 34 40 79 --- 45 --- 33
XR27E |14847 39 59 --- --- 52 --- 34 | 71 25 --- --- 67 --- 67
------+-----------------------------------------+-------------------------------------
RMS | 2079 14 40 20 19 16 17 |T 59 57 63 63 58 51 55
WRMS | 2079 13 48 19 14 15 17 |NE 48 49 51 51 46 40 44
MEDI | 1753 12 24 19 14 13 13 |MD 50 47 50 50 52 42 47
Table 3.2370.5 GPS week: 2370 Day: 5 MJD: 60839
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 3796 16 14 16 19 16 --- 8 | 79 84 85 79 82 --- 80
R03E | 1664 8 20 14 11 11 9 5 | 56 57 63 58 58 55 57
R04E | 890 11 39 17 18 9 10 7 | 67 64 73 65 68 64 66
R05E | 1736 11 22 15 15 11 12 6 | 55 54 55 62 47 41 53
R07E | 1455 10 21 12 11 14 10 5 | 43 44 44 47 50 40 43
R08E | 1612 12 18 13 17 18 16 7 | 116 122 119 109 113 113 114
R09 | 1613 13 45 16 11 12 20 8 | 20 27 30 21 20 31 19
R11 | 2912 12 24 12 15 24 14 7 | 32 37 38 33 42 31 33
R12 | 1347 15 33 12 20 20 8 8 | 45 50 44 34 45 40 40
R14 | 2859 6 7 12 17 14 11 5 | 32 35 38 30 39 29 32
R15 | 1939 21 22 11 15 12 18 7 | 53 45 46 49 36 37 44
R16 | 1367 12 24 11 12 16 16 6 | 51 53 50 56 46 62 51
R17 | 2095 10 19 28 15 10 24 8 | 45 45 60 38 46 37 44
R18 | 2257 11 39 19 12 10 24 8 | 29 36 41 29 23 18 26
XR19 | 1527 13 339 427 12 14 --- 9 | 36 96 120 96 36 --- 36
R20 | 5851 41 120 40 41 29 55 21 | 58 37 69 41 43 67 53
R21 | 1270 11 18 11 8 6 19 5 | 41 45 42 43 38 36 39
XR22 | 2673 11 29 12 9 18 --- 7 | 16 29 23 28 18 --- 18
R24 | 1462 11 29 12 8 9 16 6 | 36 32 28 37 36 27 31
XR25 |19083 69 --- --- --- 80 --- 74 | 109 --- --- --- 125 --- 86
XR26E | 7855 31 48 44 --- 58 --- 26 | 60 44 66 --- 57 --- 59
XR27E |12822 44 51 --- --- 53 --- 34 | 79 26 --- --- 83 --- 78
------+-----------------------------------------+-------------------------------------
RMS | 2311 15 40 18 17 15 21 |T 52 50 56 50 52 45 50
WRMS | 2311 14 33 14 14 15 21 |NE 43 43 48 41 42 37 39
MEDI | 1736 12 24 13 15 14 16 |MD 45 45 46 43 45 37 44
Table 3.2370.6 GPS week: 2370 Day: 6 MJD: 60840
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR02E | 3442 17 22 14 22 16 --- 9 | 83 77 89 93 75 --- 83
R03E | 2113 16 17 14 21 16 17 7 | 62 46 57 64 56 62 57
R04E | 1331 11 29 13 13 10 11 6 | 61 54 61 73 60 60 60
XR05E | 1955 12 22 15 12 10 --- 7 | 46 43 51 54 45 --- 47
R07E | 1418 14 15 14 13 25 15 7 | 40 38 47 47 43 34 39
R08E | 2941 12 20 18 17 19 17 7 | 133 125 124 131 127 130 129
R09 | 2839 17 26 26 10 13 16 8 | 23 25 43 28 30 26 26
R11 | 2889 15 24 17 16 20 13 7 | 45 45 48 47 54 45 45
R12 | 1094 12 31 12 10 20 17 7 | 51 63 58 47 56 47 51
R14 | 2475 7 16 9 10 13 13 5 | 49 50 45 51 43 55 48
R15 | 3120 10 9 15 18 25 11 7 | 70 65 66 62 70 64 65
R16 | 1718 14 17 16 7 18 11 6 | 69 69 67 65 59 69 65
R17 | 2426 11 19 24 10 11 15 7 | 69 65 77 66 67 60 67
R18 | 2399 9 33 20 13 13 17 7 | 42 68 51 42 46 36 44
XR19 | 1641 14 348 400 7 19 --- 10 | 32 149 195 128 44 --- 37
R20 | 6206 49 97 26 33 23 45 20 | 95 58 80 80 78 65 75
R21 | 1258 12 12 9 12 8 17 5 | 67 60 69 62 64 54 62
XR22 | 3333 13 32 15 9 18 --- 8 | 25 35 34 33 36 --- 29
R24 | 1180 14 34 9 16 15 17 7 | 65 59 57 71 61 53 60
XR25 |14207 49 --- --- --- 59 --- 54 | 164 --- --- --- 171 --- 156
XR26E |13512 34 54 45 --- 60 --- 27 | 62 56 79 --- 64 --- 64
XR27E | 9675 38 40 --- --- 51 --- 31 | 87 21 --- --- 84 --- 86
------+-----------------------------------------+-------------------------------------
RMS | 2664 17 33 17 16 17 18 |T 65 60 69 65 65 57 63
WRMS | 2664 14 28 16 13 18 18 |NE 61 62 68 60 62 52 59
MEDI | 2426 14 24 15 13 18 16 |MD 62 58 58 62 59 55 60
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