[IGSREPORT-29983] Wk 2321 IGLOS Final Orbits
acc
acc at igs.org
Mon Jul 22 03:02:47 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2321 (Jun 30, 2024 - Jul 06, 2024)
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 2.2321.
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:
igl2321[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2321 in the SP3 format.
igl23217.sum Combination Report for GPS Week 2321.
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.
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 | -2.5 ns
1 | 10.4 ns
2 | 14.5 ns
3 | 13.2 ns
4 | 10.7 ns
5 | 12.6 ns
6 | 14.7 ns
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 1.2321, 1a.2321).
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 2.2321.0-6)
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 3.2321.0-6).
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 2321 summary. (Jun 30, 2024 - Jul 06, 2024)
Table 1.2321.a GPS week : 2321 MJD: 60491.0-60497.0
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 4 13 -33 28 .08 19 16 | -86680 -10049 59525 349245
| 1 0 1 11 10 23 .03 | 111044 17023
esa n/a| 0 0 3 -23 -17 16 -.12 33 22 | 12531 401 3182 7410
| 0 1 0 12 12 25 .02 | 7417 1653
gfz n/a| 0 0 0 21 10 31 -.05 23 15 | 0 -490 3198 8583
| 0 1 2 24 15 40 .08 | 0 1623
grg n/a| 1 1 3 -42 31 -51 .44 27 19 | 10081 -551 3183 8970
| 1 1 2 12 22 52 .04 | 7036 1521
iac n/a| -1 1 -4 18 -5 -6 -.10 16 13 | -68840 -9959 59363 348483
| 0 1 2 14 18 43 .04 | 110967 16761
jgx n/a| 0 0 -7 -13 59 -31 -.18 30 30 | 107335 -143281 3164 8581
| 1 0 2 26 15 76 .05 | 293151 377782
Table 1.2321.b GPS week : 2321 MJD: 60491.0-60497.0
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
------+------------------------------------+------------------------------------------
R01 | 19 19 15 15 16 21 16 |
R02 | 7 7 6 8 6 7 8 |
R03 | 8 6 5 7 7 6 7 |
R04 | 7 6 6 8 7 7 6 |
R05 | 7 7 6 7 5 7 8 |
R07 | 7 6 7 6 6 5 6 |
R08 | 6 6 7 7 8 8 7 |
R09 | 6 6 7 5 6 5 5 |
R11 | 8 6 7 7 7 7 8 |
R12 | 7 7 6 8 6 6 8 |
R13 | 17 14 15 15 15 13 11 |
R14 | 6 5 7 5 5 5 6 |
R15 | 8 7 6 7 7 6 8 |
R16 | 8 7 9 6 6 7 7 |
R17 | 6 6 4 6 8 6 7 |
R18 | 9 8 7 8 7 8 8 |
R19 | 20 16 21 20 20 20 23 |
R20 | 30 30 30 26 24 26 32 |
R21 | 9 7 7 7 7 7 7 |
R22 | 7 7 7 6 6 7 6 |
R24 | 7 7 10 8 8 9 8 |
R25 | 13 16 18 11 14 11 10 |
R26 | 33 36 33 34 34 34 50 |
Table 1.2321.c GPS week : 2321 MJD: 60491.0-60497.0
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 2321 0 | 45 6 179 221 348 -389 82.4 1918 1918 | -2501 0
brd 2321 1 | 14 60 152 244 604 7508 84.1 1925 1925 | 10431 0
brd 2321 2 | 7 45 99 279 379 11810 79.1 1964 1964 | 14510 0
brd 2321 3 | -36 89 42 743 342 5675 80.5 1656 1656 | 13201 0
brd 2321 4 | 3 -40 46 487 112 7337 80.7 1781 1781 | 10661 0
brd 2321 5 | 1 -56 80 697 537 8821 82.6 1584 1584 | 12624 0
brd 2321 6 | 0 136 24 -647 1513 12100 81.6 1526 1526 | 14688 0
-------------+------------------------------------------------------------+----------------
brd 2321 mean| 5 34 89 289 548 7551 81.6 1764 1764 | 10516 0
brd 2321 sdev| 24 69 58 464 453 4224 1.7 178 178 | 5978 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 2.2321.0 GPS week: 2321 Day: 0 MJD: 60491
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 -4 -34 20 .01 19 16 | -134357 -4505 77917 487860
esa n/a| 0 -1 3 -22 -20 34 -.14 32 21 | 994 3245 3335 6974
gfz n/a| 0 -2 3 71 8 74 .09 28 16 | 0 1997 3380 9392
grg n/a| 3 0 1 -31 46 -123 .45 30 23 | -4913 1711 3384 11128
iac n/a| -2 2 0 8 -15 44 -.10 19 16 | -116734 -4057 77145 483103
jgx n/a| 1 -1 -11 -17 75 -65 -.10 25 25 | -17722 2699 3247 9451
Table 2.2321.1 GPS week: 2321 Day: 1 MJD: 60492
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 4 15 -29 76 .08 16 14 | -188930 -14363 134263 919419
esa n/a| 0 0 2 -20 -36 -18 -.11 34 22 | 7943 859 3059 7543
gfz n/a| 0 -2 -2 18 -21 -16 -.11 22 13 | 0 389 3059 8189
grg n/a| 3 3 2 -60 28 15 .44 29 21 | 8529 343 3152 11125
iac n/a| -1 0 -2 8 20 -10 -.07 14 12 | -170739 -14559 134100 918631
jgx n/a| 0 0 -6 15 69 -89 -.14 31 31 | -2395 501 3053 8238
Table 2.2321.2 GPS week: 2321 Day: 2 MJD: 60493
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 0 -46 33 .08 18 14 | -269779 -47016 191848 999999
esa n/a| 0 0 3 -26 -30 -5 -.11 30 20 | 24866 736 3120 7412
gfz n/a| 1 0 3 7 19 19 .02 25 15 | 0 -649 3118 8558
grg n/a| 1 0 5 -44 30 -54 .49 31 24 | 14387 -644 3094 7925
iac n/a| -1 1 -5 26 8 21 -.11 17 13 | -251881 -46312 191704 999999
jgx n/a| 0 -1 -9 6 72 -107 -.17 33 33 | 771976 -999999 3082 8709
Table 2.2321.3 GPS week: 2321 Day: 3 MJD: 60494
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 21 -25 19 .09 20 17 | -3687 -817 3204 8731
esa n/a| 0 1 4 -3 -1 -5 -.10 31 21 | 12249 -6 3243 6542
gfz n/a| 0 2 2 30 12 0 -.05 28 17 | 0 -590 3191 8091
grg n/a| 0 3 6 -48 9 -7 .44 25 18 | 13198 -509 3123 7731
iac n/a| 0 0 -8 9 10 45 -.07 14 12 | 15044 -2079 3192 8987
jgx n/a| 1 -1 -5 -16 40 -93 -.21 30 30 | -1094 -326 3196 8362
Table 2.2321.4 GPS week: 2321 Day: 4 MJD: 60495
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 29 -16 29 .07 20 17 | -5219 233 3135 9460
esa n/a| -1 -1 2 -43 -7 47 -.16 35 25 | 13718 978 3166 6645
gfz n/a| 1 0 0 -4 15 94 -.07 20 15 | 0 203 3198 8050
grg n/a| 2 0 5 -23 26 -116 .42 25 16 | 10311 84 3165 7710
iac n/a| 0 2 -4 37 -19 -43 -.11 15 12 | 12280 -847 3136 9370
jgx n/a| 0 0 -5 -66 49 14 -.20 27 27 | -1656 -80 3190 7657
Table 2.2321.5 GPS week: 2321 Day: 5 MJD: 60496
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 12 -37 15 .11 18 16 | -2541 -2383 3321 10479
esa n/a| 0 -1 3 -31 -15 27 -.12 35 22 | 16986 -1864 3362 9938
gfz n/a| 1 -2 0 22 27 11 -.10 19 15 | 0 -3134 3402 9889
grg n/a| 0 1 3 -47 5 -49 .37 26 17 | 13528 -2948 3338 9600
iac n/a| 0 2 -4 4 -14 -50 -.07 14 11 | 14103 -863 3306 10534
jgx n/a| -1 0 -7 -9 41 92 -.20 30 30 | 1781 -3252 3432 9496
Table 2.2321.6 GPS week: 2321 Day: 6 MJD: 60497
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 4 17 -44 2 .10 23 16 | -2250 -1493 2991 8771
esa n/a| -1 -2 3 -14 -12 32 -.10 35 23 | 10967 -1140 2992 6819
gfz n/a| 2 -1 -2 6 8 35 -.12 22 14 | 0 -1652 3040 7916
grg n/a| 2 0 0 -40 73 -22 .45 24 17 | 15527 -1900 3026 7576
iac n/a| 0 4 -2 36 -28 -50 -.18 20 18 | 16041 -1001 2960 8761
jgx n/a| -1 0 -7 -9 68 27 -.26 32 32 | 461 -2512 2952 8155
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 3.2321.0 GPS week: 2321 Day: 0 MJD: 60491
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01E | 1402 28 44 46 48 29 --- 19 | 62 66 90 82 60 --- 63
XR02E | 1078 11 9 16 14 13 --- 6 | 39 40 35 43 39 --- 37
R03E | 1768 11 12 16 21 12 27 7 | 78 79 82 89 80 82 79
R04E | 951 11 12 10 17 16 24 7 | 52 47 51 46 59 52 50
R05E | 4529 12 13 13 13 15 18 6 | 75 74 76 72 70 74 72
R07E | 3733 10 14 14 14 16 20 6 | 64 59 58 70 64 57 61
R08E | 1604 9 12 12 23 13 14 6 | 96 94 96 81 96 90 92
R09 | 1701 9 13 15 19 11 11 5 | 36 35 42 45 33 37 36
R11 | 2662 11 19 22 11 20 19 8 | 49 46 37 47 50 49 44
R12 | 832 15 13 23 20 10 11 7 | 98 107 103 99 98 101 100
R13 | 1142 37 22 21 70 26 42 17 | 59 52 48 53 50 52 48
R14 | 690 12 16 11 11 14 18 6 | 53 67 56 57 49 56 54
R15 | 1201 11 12 13 31 21 16 8 | 57 58 55 50 58 54 53
R16 | 1134 11 15 17 35 12 20 8 | 60 64 63 50 62 60 58
R17 | 1025 8 12 14 13 18 16 6 | 59 53 55 58 61 49 55
R18 | 879 13 27 17 29 11 16 8 | 49 65 42 45 51 47 47
R19 | 983 29 74 37 45 36 49 20 | 112 48 116 111 114 86 99
R20 | 2664 46 101 98 58 34 51 30 | 118 47 162 110 91 86 99
R21 | 929 19 12 22 13 15 27 8 | 69 62 73 62 64 48 62
R22 | 1492 15 10 12 12 19 12 6 | 33 42 40 43 53 42 41
R24 | 817 16 20 12 26 10 13 7 | 48 57 52 64 43 49 48
XR25 |13826 11 --- --- --- 13 --- 12 | 33 --- --- --- 38 --- 33
XR26E | 6565 35 --- --- 41 57 --- 32 | 34 --- --- 21 31 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 1918 19 32 28 30 19 25 |T 62 60 68 63 61 61 59
WRMS | 1918 16 21 16 23 16 25 |NE 62 57 67 63 61 58 58
MEDI | 1201 12 13 16 20 15 18 |MD 59 58 56 57 59 54 54
Table 3.2321.1 GPS week: 2321 Day: 1 MJD: 60492
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01E | 2775 31 42 45 43 28 --- 18 | 84 84 96 78 92 --- 84
XR02E | 867 12 16 14 11 12 --- 6 | 42 43 45 48 37 --- 40
R03E | 1960 7 11 15 16 7 18 5 | 63 64 65 73 59 66 64
R04E | 2062 10 13 13 19 10 21 6 | 42 34 34 47 38 40 37
R05E | 3946 13 13 14 19 16 19 7 | 76 74 73 73 67 69 70
R07E | 2998 9 11 12 14 14 20 6 | 56 56 52 63 53 56 55
R08E | 1028 11 18 15 12 12 14 6 | 95 105 111 104 94 99 100
R09 | 1895 12 18 10 16 13 14 6 | 26 31 25 30 23 29 24
R11 | 3154 13 8 13 10 8 20 5 | 27 24 29 32 31 38 27
R12 | 720 9 10 16 27 11 16 6 | 69 82 76 80 75 75 74
R13 | 1285 21 28 21 54 11 53 13 | 40 36 42 55 28 31 32
R14 | 923 7 11 11 11 10 14 4 | 37 42 29 36 34 41 35
R15 | 929 16 24 16 13 11 11 7 | 38 45 49 33 40 40 39
R16 | 1516 13 20 11 33 9 13 7 | 39 52 40 25 35 48 37
R17 | 784 11 18 17 11 8 15 6 | 40 35 32 43 36 32 35
R18 | 939 15 24 15 14 16 21 7 | 29 37 29 38 43 27 32
R19 | 2330 20 70 25 37 20 43 15 | 55 39 50 65 54 43 49
R20 | 1536 40 110 70 79 34 92 30 | 60 45 78 36 42 60 43
R21 | 960 11 15 11 22 13 22 6 | 42 38 41 42 47 35 41
R22 | 2382 16 15 20 15 13 17 7 | 32 36 47 45 41 35 37
R24 | 1053 17 18 12 18 12 17 6 | 37 44 40 58 37 46 39
XR25 |13063 16 --- --- --- 15 --- 15 | 19 --- --- --- 24 --- 19
XR26E |10617 45 --- --- 47 56 --- 36 | 31 --- --- 25 35 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 1925 16 34 22 28 14 31 |T 46 49 51 51 46 47 45
WRMS | 1925 14 22 13 21 12 31 |NE 39 41 43 44 39 41 37
MEDI | 1536 13 18 15 16 12 18 |MD 40 43 45 45 40 41 39
Table 3.2321.2 GPS week: 2321 Day: 2 MJD: 60493
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 1843 26 38 43 23 24 44 14 | 45 61 74 66 62 61 56
XR02E | 1731 10 16 8 11 13 --- 6 | 31 39 37 41 34 --- 34
R03E | 1603 9 13 12 9 7 17 5 | 57 59 56 60 54 58 56
R04E | 2081 10 17 13 13 11 17 6 | 40 41 38 40 38 42 38
R05E | 3861 12 10 11 14 12 14 5 | 52 49 49 50 48 47 48
R07E | 2617 12 11 10 23 12 18 6 | 50 47 48 51 43 48 46
R08E | 1281 13 15 16 19 11 26 7 | 64 65 71 78 64 73 66
R09 | 1067 14 14 18 23 15 12 7 | 29 25 31 46 30 33 28
R11 | 2149 15 13 14 18 12 20 6 | 35 37 28 39 37 34 33
R12 | 1000 9 15 11 18 11 15 5 | 90 94 85 99 92 98 92
R13 | 881 27 29 12 57 14 53 14 | 52 41 40 54 32 54 41
R14 | 736 15 11 27 9 11 18 7 | 33 28 28 32 26 34 26
R15 | 718 11 12 14 19 8 19 6 | 41 39 41 56 34 39 39
R16 | 1060 12 24 25 24 12 15 8 | 42 58 65 33 39 42 44
R17 | 734 10 9 6 10 8 15 4 | 42 39 38 38 36 35 37
R18 | 817 10 21 15 13 12 28 7 | 32 38 26 44 36 30 32
R19 | 2433 28 84 35 48 33 41 20 | 76 39 76 77 76 54 64
R20 | 3891 47 67 70 93 45 100 30 | 84 65 107 89 66 68 70
R21 | 990 8 19 17 14 13 22 7 | 47 41 61 46 56 40 48
R22 | 3065 13 10 21 19 13 15 6 | 28 29 43 37 36 35 31
R24 | 1030 15 25 29 19 20 21 9 | 37 52 50 51 40 41 39
XR25 |12931 17 --- --- --- 17 --- 17 | 21 --- --- --- 36 --- 26
XR26E |14529 41 --- --- 35 53 --- 32 | 33 --- --- 27 28 --- 29
------+-----------------------------------------+-------------------------------------
RMS | 1963 18 30 25 31 17 33 |T 46 46 52 52 45 48 44
WRMS | 1963 14 20 15 24 13 33 |NE 45 44 51 52 44 45 43
MEDI | 1603 13 15 15 19 12 18 |MD 42 41 48 46 38 42 39
Table 3.2321.3 GPS week: 2321 Day: 3 MJD: 60494
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 918 34 40 45 16 21 46 15 | 70 83 80 68 69 56 68
XR02E | 1312 12 22 13 18 13 --- 7 | 43 54 49 54 41 --- 45
R03E | 2867 8 15 15 26 9 17 6 | 40 37 43 52 40 36 38
R04E | 1735 9 16 8 22 14 30 7 | 38 35 33 41 34 46 33
R05E | 1815 12 9 20 19 8 23 6 | 54 55 61 50 45 56 51
R07E | 981 9 12 15 21 13 13 6 | 46 46 49 46 43 42 43
R08E | 2060 13 17 14 21 13 17 7 | 99 101 100 101 99 99 98
R09 | 1064 11 15 10 12 9 16 5 | 25 31 29 24 27 28 24
R11 | 1671 16 14 25 9 10 18 7 | 28 33 18 27 25 28 22
R12 | 802 18 9 21 14 19 14 7 | 46 39 50 43 37 39 39
R13 | 1129 31 24 31 44 15 53 14 | 51 34 50 37 28 25 34
R14 | 732 6 7 10 8 11 18 4 | 29 30 31 33 23 41 28
R15 | 892 16 17 19 20 9 14 7 | 33 27 24 42 24 35 27
R16 | 863 13 18 18 11 7 14 6 | 42 45 32 46 37 41 38
R17 | 814 12 8 13 15 13 16 5 | 50 48 52 56 41 42 46
R18 | 850 11 29 32 14 9 12 8 | 36 47 28 35 32 29 31
R19 | 2004 27 83 45 52 22 34 20 | 85 54 105 90 84 73 78
R20 | 2212 46 82 73 55 17 87 26 | 99 53 129 84 90 64 82
R21 | 932 10 18 14 22 14 20 7 | 55 47 59 49 59 45 52
R22 | 3784 16 13 8 17 14 12 6 | 22 27 33 33 42 32 30
R24 | 926 19 20 23 14 14 19 8 | 54 52 61 48 46 40 48
XR25 |17552 17 12 --- --- 16 --- 11 | 19 22 --- --- 35 --- 26
XR26E |16849 43 --- --- 45 51 --- 33 | 26 --- --- 23 20 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 1656 20 31 28 25 14 30 |T 47 45 53 49 44 44 43
WRMS | 1656 17 21 17 18 12 30 |NE 44 39 50 46 42 40 40
MEDI | 1129 13 16 18 18 13 17 |MD 43 45 49 46 40 41 38
Table 3.2321.4 GPS week: 2321 Day: 4 MJD: 60495
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 613 39 46 36 19 31 46 16 | 38 65 61 49 46 49 42
XR02E | 1105 12 10 17 13 10 --- 6 | 35 39 44 40 33 --- 36
R03E | 2739 8 12 12 19 15 17 6 | 39 38 39 49 39 31 37
R04E | 2911 8 12 21 19 9 16 6 | 31 27 33 38 28 27 27
R05E | 1885 13 12 10 15 7 14 5 | 43 42 43 54 44 42 43
R07E | 1052 10 12 15 15 14 16 6 | 40 40 45 43 44 37 40
R08E | 2545 8 25 20 24 12 13 7 | 58 73 66 40 55 49 55
R09 | 1250 15 11 15 8 13 12 5 | 25 31 34 31 29 28 27
R11 | 1420 13 14 12 12 16 18 6 | 36 38 29 36 32 37 31
R12 | 796 12 11 18 12 7 14 5 | 96 93 86 82 90 98 90
R13 | 1217 22 20 29 52 17 54 15 | 56 61 68 39 43 58 52
R14 | 720 13 12 9 12 7 16 5 | 43 38 34 38 32 35 35
R15 | 1205 20 20 14 12 13 17 7 | 48 39 35 40 31 48 37
R16 | 1057 13 13 17 11 12 16 6 | 44 41 44 46 35 52 41
R17 | 928 15 15 21 14 12 21 7 | 47 45 52 48 43 31 43
R18 | 859 8 32 11 11 10 13 6 | 36 48 29 36 30 26 32
R19 | 2959 20 92 23 48 29 54 20 | 87 39 84 92 86 74 77
R20 | 1217 48 101 41 59 22 53 24 | 82 45 69 74 65 60 60
R21 | 823 18 13 10 14 11 21 6 | 46 42 37 38 44 31 39
R22 | 3597 16 13 11 15 10 13 5 | 29 42 40 36 38 45 36
R24 | 1302 26 14 17 20 11 15 8 | 60 43 41 44 40 40 42
XR25 |20884 21 21 --- --- 19 --- 14 | 23 19 --- --- 29 --- 22
XR26E |16667 47 --- --- 37 54 --- 34 | 25 --- --- 22 19 --- 18
------+-----------------------------------------+-------------------------------------
RMS | 1781 20 35 20 25 15 27 |T 46 44 48 46 42 44 41
WRMS | 1781 17 25 15 16 12 27 |NE 50 44 48 48 44 47 44
MEDI | 1217 15 13 17 15 12 16 |MD 43 41 43 40 39 40 39
Table 3.2321.5 GPS week: 2321 Day: 5 MJD: 60496
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
XR01E | 1207 42 37 57 34 33 --- 20 | 62 70 92 70 82 --- 66
XR02E | 1193 12 10 16 19 15 --- 7 | 32 35 36 37 38 --- 33
R03E | 1619 10 14 12 10 15 20 6 | 82 86 88 81 82 76 81
R04E | 2376 9 13 16 21 10 18 6 | 41 44 43 45 41 36 40
R05E | 2092 10 11 15 23 8 23 6 | 55 57 55 64 52 52 54
R07E | 1265 12 11 11 12 11 13 5 | 58 59 63 63 61 53 59
R08E | 2280 11 18 27 19 16 17 8 | 117 112 124 110 110 105 113
R09 | 2195 11 11 14 10 9 13 5 | 34 30 36 32 35 19 31
R11 | 1467 12 20 16 14 12 19 6 | 45 54 52 41 55 48 48
R12 | 681 14 16 15 16 8 15 6 | 70 85 88 68 75 73 75
R13 | 1255 21 26 23 41 8 54 12 | 42 39 58 27 33 40 38
R14 | 655 8 12 18 13 8 10 5 | 28 36 39 24 26 26 28
R15 | 1252 17 21 12 7 8 9 5 | 37 28 28 33 30 27 29
R16 | 961 18 21 14 9 11 15 6 | 36 35 33 34 26 32 29
R17 | 787 8 15 18 18 8 18 6 | 41 34 46 38 41 31 38
R18 | 914 8 28 19 19 19 16 8 | 32 38 45 42 26 28 30
R19 | 2182 31 85 35 49 27 54 20 | 67 35 74 64 69 40 61
R20 | 1044 40 104 37 64 25 85 25 | 75 60 69 77 56 68 60
R21 | 1172 18 18 8 11 10 19 6 | 42 38 38 43 37 32 36
R22 | 2360 14 9 14 28 7 16 6 | 31 33 32 35 32 30 29
R24 | 1415 29 14 14 20 14 15 8 | 57 39 46 40 37 33 40
XR25 |13931 16 14 --- --- 14 --- 10 | 25 22 --- --- 25 --- 22
XR26E |17710 46 --- --- 45 48 --- 33 | 45 --- --- 39 35 --- 35
------+-----------------------------------------+-------------------------------------
RMS | 1583 18 35 19 26 14 30 |T 50 48 56 50 48 44 46
WRMS | 1583 16 22 15 17 11 30 |NE 44 40 48 42 40 37 39
MEDI | 1265 14 15 16 19 11 17 |MD 42 38 46 41 38 36 38
Table 3.2321.6 GPS week: 2321 Day: 6 MJD: 60497
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01E | 2596 40 26 39 27 19 50 15 | 59 67 85 72 75 55 67
XR02E | 1379 9 12 18 16 18 --- 7 | 40 39 40 43 43 --- 39
R03E | 1431 12 11 16 19 16 11 6 | 97 97 100 109 100 98 100
R04E | 1551 9 8 14 11 17 17 6 | 46 44 46 51 45 40 44
R05E | 2148 17 15 18 22 11 22 8 | 73 69 69 79 67 65 69
R07E | 1606 8 9 10 14 15 17 5 | 76 74 77 82 71 67 74
R08E | 1760 12 13 15 12 18 16 6 | 106 104 112 104 105 100 105
R09 | 1523 12 12 8 11 9 12 4 | 36 38 36 36 37 32 34
R11 | 1415 9 23 13 10 27 17 8 | 50 45 43 49 66 42 48
R12 | 904 14 17 16 16 17 28 8 | 92 108 112 96 95 96 98
R13 | 1504 18 15 15 39 15 38 11 | 55 52 45 44 46 44 45
R14 | 730 11 9 16 9 14 15 5 | 40 42 33 40 35 41 36
R15 | 1479 17 21 13 12 24 15 8 | 57 50 51 52 43 45 47
R16 | 995 18 15 15 13 19 10 7 | 58 53 57 49 51 58 52
R17 | 965 11 20 21 10 11 22 7 | 66 56 71 59 61 49 60
R18 | 1423 9 24 12 13 15 26 7 | 45 59 47 46 42 38 44
R19 | 1117 47 84 40 45 30 61 23 | 119 47 127 114 114 76 102
R20 | 1265 58 113 51 67 42 89 31 | 114 59 108 103 91 56 84
R21 | 1660 18 13 20 10 18 13 7 | 72 63 69 64 66 58 65
R22 | 1856 12 13 8 20 10 11 5 | 33 39 42 42 42 37 38
R24 | 1395 18 16 12 14 21 23 8 | 66 58 55 60 57 48 56
XR25 |15006 14 13 --- --- 13 --- 9 | 25 23 --- --- 30 --- 27
XR26E |19877 49 --- --- --- 49 --- 49 | 55 --- --- --- 46 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1525 23 35 22 24 20 32 |T 64 58 67 66 62 57 60
WRMS | 1525 16 23 14 17 18 32 |NE 61 52 64 61 58 51 55
MEDI | 1479 14 15 15 14 17 17 |MD 58 53 57 59 57 49 52
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