[IGSREPORT-29794] Wk 2304 IGLOS Final Orbits
acc
acc at igs.org
Tue Mar 26 00:20:01 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2304 (Mar 03, 2024 - Mar 09, 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 2.2304.
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:
igl2304[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2304 in the SP3 format.
igl23047.sum Combination Report for GPS Week 2304.
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 | 3.9 ns
1 | 3.3 ns
2 | 2.1 ns
3 | 6.0 ns
4 | 2.7 ns
5 | 4.4 ns
6 | 4.7 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 | COD | R26
0 | ESA | R26
0 | GFZ | R26
0 | GRG | R26
0 | IAC | R26
0 | JGX | R26
1 | COD | R26
4 | COD | R25
4 | ESA | R25
4 | GFZ | R25
4 | GRG | R25
4 | IAC | R25
4 | JGX | R25
5 | COD | R25
5 | ESA | R25
5 | GFZ | R25
5 | GRG | R25
5 | IAC | R25
5 | JGX | R25
6 | COD | R25
6 | ESA | R25
6 | GFZ | R25
6 | GRG | R25
6 | IAC | R25
6 | JGX | R25
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 1.2304, 1a.2304).
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 2.2304.0-6)
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 3.2304.0-6).
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 2304 summary. (Mar 03, 2024 - Mar 09, 2024)
Table 1.2304.a GPS week : 2304 MJD: 60372.0-60378.0
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 1 -15 -24 31 .13 19 14 | 2977 -1041 3448 7440
| 0 1 2 18 13 13 .04 | 2113 1464
esa n/a| 1 0 1 -39 16 -27 -.09 26 18 | 7648 -1488 3445 7206
| 0 0 2 21 8 36 .05 | 4563 1484
gfz n/a| 0 0 0 25 8 -11 .03 26 15 | 0 -1209 3437 7436
| 0 1 1 8 13 18 .03 | 0 1461
grg n/a| 1 0 1 2 -4 15 .26 21 15 | 4387 -1308 3444 7019
| 1 1 2 12 16 52 .03 | 1302 1386
iac n/a| -1 -1 -3 3 -8 -45 -.24 22 18 | 6318 -579 3447 7810
| 1 1 2 29 7 47 .06 | 1361 880
jgx n/a| 0 0 -1 25 26 30 -.21 30 30 | 4581 -1115 3529 7683
| 2 1 2 13 17 52 .02 | 2266 1567
Table 1.2304.b GPS week : 2304 MJD: 60372.0-60378.0
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 | 13 14 14 13 14 13 10 |
R02 | 9 7 6 7 6 7 7 |
R03 | 6 5 6 7 6 7 6 |
R04 | 7 6 6 6 6 6 6 |
R05 | 5 7 6 6 7 7 7 |
R07 | 6 5 7 7 7 6 7 |
R08 | 8 7 7 7 6 7 8 |
R09 | 7 7 7 7 7 8 8 |
R11 | 7 7 6 10 8 6 6 |
R12 | 7 6 8 8 8 9 9 |
R13 | 12 16 14 15 13 15 15 |
R14 | 6 7 7 7 7 7 7 |
R15 | 7 7 8 9 7 8 7 |
R16 | 7 8 9 9 9 8 7 |
R17 | 10 8 9 7 7 9 9 |
R18 | 7 6 7 8 8 8 7 |
R19 | 16 18 18 16 20 20 18 |
R20 | 28 24 25 37 33 27 28 |
R21 | 8 7 6 7 7 9 8 |
R22 | 8 7 8 6 7 6 6 |
R24 | 9 8 10 9 10 7 8 |
R25 | --- --- --- 0 --- --- --- |
R26 | --- 164 --- --- --- --- --- |
Table 1.2304.c GPS week : 2304 MJD: 60372.0-60378.0
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 2304 0 | 59 1 152 -773 -3142 -4901 79.3 1924 1924 | 3938 0
brd 2304 1 | 86 -25 156 -792 -946 -574 79.7 1869 1869 | 3270 0
brd 2304 2 | 33 -61 99 -591 1769 4565 77.3 2029 2029 | 2067 0
brd 2304 3 | -5 5 203 3033 1878 9758 80.9 1594 1594 | 6007 0
brd 2304 4 | 58 -15 196 2724 -216 5036 79.4 1833 1833 | 2749 0
brd 2304 5 | -17 53 59 -1652 391 1384 80.8 1675 1675 | 4373 0
brd 2304 6 | 47 -75 140 -969 -1516 1365 80.9 1655 1655 | 4714 0
-------------+------------------------------------------------------------+----------------
brd 2304 mean| 37 -16 143 139 -254 2376 79.8 1797 1797 | 3874 0
brd 2304 sdev| 37 43 51 1903 1801 4655 1.3 159 159 | 1316 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 2.2304.0 GPS week: 2304 Day: 0 MJD: 60372
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 3 -2 -33 46 .14 24 15 | 5596 -878 3742 7197
esa n/a| 1 -1 0 -13 21 11 -.15 23 19 | 8454 -1498 3735 7044
gfz n/a| 0 1 0 19 0 -7 .07 28 19 | 0 -998 3725 7193
grg n/a| 1 1 4 10 3 -31 .27 18 13 | 4012 -1047 3743 6894
iac n/a| -2 0 -2 -21 -23 10 -.20 22 15 | 7301 -1139 3749 7544
jgx n/a| 0 -1 -4 12 27 -39 -.21 23 23 | 7072 -370 3803 7323
Table 2.2304.1 GPS week: 2304 Day: 1 MJD: 60373
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 4 6 -39 27 .18 16 12 | 4789 -2670 3437 7869
esa n/a| 2 0 3 -42 26 19 -.14 26 18 | 11570 -2718 3446 7204
gfz n/a| 1 0 0 38 22 4 -.00 25 15 | 0 -2311 3445 7741
grg n/a| 0 1 0 3 -4 -57 .31 20 15 | 4424 -2435 3427 7276
iac n/a| -2 0 -1 -26 -9 -9 -.25 20 14 | 6629 -957 3440 8391
jgx n/a| 1 0 -4 9 22 -27 -.20 23 23 | 6401 -2891 3591 7929
Table 2.2304.2 GPS week: 2304 Day: 2 MJD: 60374
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 -11 -5 31 .13 18 15 | 328 -1836 3488 8950
esa n/a| 0 -1 1 -25 12 -8 -.14 26 18 | -44 -2427 3486 8523
gfz n/a| 1 2 0 17 -14 -8 .03 21 12 | 0 -2314 3480 8891
grg n/a| -1 -1 3 12 -34 -10 .27 22 14 | 2995 -2466 3473 8280
iac n/a| -2 -1 -7 -18 -4 -36 -.21 22 18 | 4412 -1360 3485 9341
jgx n/a| 0 0 -3 29 44 20 -.20 27 27 | 2152 -2298 3620 9359
Table 2.2304.3 GPS week: 2304 Day: 3 MJD: 60375
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 1 -18 -16 42 .16 21 17 | 4066 488 3432 6485
esa n/a| 0 0 4 -40 25 -51 -.02 28 21 | 13009 -17 3421 6452
gfz n/a| 1 1 1 21 7 -49 .02 32 13 | 0 211 3393 6484
grg n/a| 1 0 0 6 8 43 .25 26 15 | 6196 -49 3441 5885
iac n/a| 0 0 -4 -10 -7 -29 -.18 21 18 | 8274 -613 3429 6739
jgx n/a| -3 0 0 14 -4 31 -.21 32 32 | 6224 309 3497 6616
Table 2.2304.4 GPS week: 2304 Day: 4 MJD: 60376
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 1 -23 -17 6 .08 16 12 | 1510 -39 3373 7409
esa n/a| 1 0 0 -55 11 -38 -.07 27 18 | 3815 -156 3365 7454
gfz n/a| 0 -1 0 34 24 6 .06 30 16 | 0 -380 3358 7487
grg n/a| 2 -1 0 -2 -16 14 .22 24 17 | 2777 -338 3374 7049
iac n/a| -2 -2 -4 40 -7 -54 -.22 23 21 | 4931 -240 3384 7726
jgx n/a| 1 0 0 35 18 107 -.26 37 37 | 2642 158 3352 7740
Table 2.2304.5 GPS week: 2304 Day: 5 MJD: 60377
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 0 -50 -18 36 .10 17 14 | 3907 -2936 3501 6962
esa n/a| 2 -1 -2 -22 1 -41 -.07 28 18 | 6740 -3630 3513 6707
gfz n/a| 0 2 0 21 5 -13 .01 22 14 | 0 -3284 3514 6943
grg n/a| 1 -1 1 11 17 84 .24 21 18 | 5884 -3186 3503 6632
iac n/a| -2 -2 0 42 0 -138 -.33 24 20 | 6924 -989 3493 7312
jgx n/a| 0 0 0 32 45 75 -.23 35 35 | 5750 -3073 3584 7197
Table 2.2304.6 GPS week: 2304 Day: 6 MJD: 60378
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 -1 -10 -38 27 .13 19 14 | 647 578 3169 7210
esa n/a| 1 -2 2 -77 20 -81 -.06 26 18 | 9996 27 3153 7063
gfz n/a| 0 0 3 28 14 -12 .05 21 12 | 0 613 3147 7318
grg n/a| 1 0 -2 -23 -5 69 .23 18 14 | 4424 364 3151 7119
iac n/a| 0 0 -2 16 -9 -61 -.30 24 20 | 5755 1239 3153 7623
jgx n/a| -3 2 0 45 33 42 -.19 29 29 | 1827 355 3262 7621
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 3.2304.0 GPS week: 2304 Day: 0 MJD: 60372
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 823 36 30 30 21 19 35 13 | 98 69 72 91 78 81 79
R02 | 708 11 33 25 14 10 18 8 | 72 79 69 64 69 67 68
R03 | 720 10 10 13 11 11 17 5 | 72 63 64 71 64 56 65
R04 | 1122 15 20 15 11 15 13 6 | 88 83 91 94 94 84 89
R05 | 1596 10 13 9 10 10 8 4 | 70 63 69 69 71 64 67
R07 | 2258 7 19 11 11 17 13 6 | 84 87 84 83 85 79 83
R08 | 1351 21 17 14 15 9 21 7 | 71 77 60 71 66 65 67
R09 | 676 17 15 22 12 12 16 7 | 29 27 31 28 31 25 26
R11 | 787 13 14 15 11 17 18 6 | 25 29 38 37 43 30 32
R12 | 928 12 19 20 16 9 11 6 | 71 83 76 64 71 69 71
XR13 | 2356 19 31 20 21 26 --- 12 | 93 74 107 87 110 --- 93
R14 | 1262 15 20 10 15 9 12 6 | 70 78 61 62 65 56 64
R15 | 1029 17 15 11 9 12 28 7 | 103 107 104 102 102 91 101
R16 | 1080 15 18 17 10 16 16 7 | 101 98 112 101 104 97 101
XR17 | 2156 16 18 15 23 20 --- 9 | 103 114 110 96 100 --- 103
R18E | 1787 19 17 18 17 13 13 7 | 64 65 70 67 63 68 65
R19E | 1966 22 39 49 28 29 41 15 | 56 53 73 48 47 49 47
R20E | 5266 73 52 83 46 69 53 28 | 72 115 126 76 115 55 80
R21E | 934 15 17 22 18 20 16 8 | 54 51 56 59 56 52 53
R22E | 3655 21 11 14 18 20 10 7 | 42 42 46 44 42 37 41
R24E | 1763 22 14 14 21 15 25 8 | 182 178 182 187 174 197 183
------+-----------------------------------------+-------------------------------------
RMS | 1924 24 23 28 18 22 23 |T 81 77 81 74 75 69 75
WRMS | 1924 15 19 19 13 15 23 |NE 82 75 76 72 73 66 73
MEDI | 1262 16 18 15 15 15 16 |MD 72 77 72 69 69 65 68
Table 3.2304.1 GPS week: 2304 Day: 1 MJD: 60373
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1124 22 41 14 36 27 45 14 | 68 72 62 93 64 81 69
R02 | 830 8 23 10 19 9 21 6 | 66 67 67 65 67 61 64
R03 | 746 8 13 7 7 9 13 4 | 52 54 51 49 43 46 48
R04 | 741 8 21 11 14 12 16 6 | 72 62 78 79 68 69 71
R05 | 1082 10 15 13 17 15 21 7 | 56 45 47 55 55 37 49
R07 | 2485 7 8 18 8 10 11 5 | 68 72 57 66 68 67 65
R08 | 1239 13 16 9 19 13 14 6 | 57 62 51 65 53 51 55
R09 | 820 14 13 20 18 9 11 6 | 31 33 46 28 34 32 32
R11 | 1164 11 18 13 24 12 14 7 | 16 28 22 23 24 26 19
R12 | 811 14 17 15 7 12 11 5 | 59 61 53 58 49 54 54
XR13 | 1526 18 44 40 27 30 --- 16 | 81 59 110 93 94 --- 86
R14 | 1739 9 16 19 14 9 20 6 | 72 75 67 69 64 58 66
R15 | 1417 19 17 7 15 20 13 7 | 90 89 85 90 72 84 84
R16 | 1050 11 20 29 12 10 14 7 | 82 85 106 90 87 82 87
XR17 | 1795 12 11 14 24 13 --- 7 | 92 91 89 100 85 --- 91
R18E | 1505 8 21 15 18 9 13 6 | 69 68 64 73 67 69 67
R19E | 3481 24 45 62 37 28 38 17 | 60 56 70 49 52 52 49
R20E | 4691 35 65 64 22 60 60 23 | 62 83 91 75 67 53 61
R21E | 852 11 15 15 20 14 10 6 | 66 70 69 66 64 66 65
R22E | 2699 16 13 6 17 19 14 6 | 15 26 23 35 19 23 19
R24E | 1105 17 17 14 26 14 13 7 | 153 152 162 163 152 163 156
XR26 |>>>>> 970 --- --- 176 152 --- 164 | 321 --- --- 56 19 --- 10
------+-----------------------------------------+-------------------------------------
RMS | 1869 16 26 25 20 20 23 |T 77 67 70 70 62 61 62
WRMS | 1869 12 18 15 15 14 23 |NE 80 63 66 67 59 57 59
MEDI | 1164 12 17 14 18 13 14 |MD 66 67 67 66 64 58 64
Table 3.2304.2 GPS week: 2304 Day: 2 MJD: 60374
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2072 29 55 15 33 21 22 13 | 82 47 67 87 60 70 67
R02 | 890 12 20 13 10 14 14 6 | 53 53 49 53 44 51 49
R03 | 547 13 18 13 11 11 15 6 | 52 41 46 47 41 37 43
R04 | 1170 8 18 10 11 12 13 5 | 60 58 63 60 58 56 59
R05 | 631 9 17 11 13 14 9 5 | 51 47 52 56 56 50 51
R07 | 1679 12 15 10 10 19 22 6 | 51 44 46 55 51 41 47
R08 | 1409 14 16 7 17 18 20 7 | 54 55 44 49 39 50 48
R09 | 951 20 12 16 11 12 15 7 | 26 30 38 34 38 39 31
R11 | 845 12 15 9 15 15 11 6 | 24 29 30 35 36 29 28
R12 | 940 11 23 13 22 16 16 7 | 49 56 50 42 50 40 46
XR13 | 1461 25 35 29 31 18 --- 14 | 73 67 84 79 85 --- 76
R14 | 1214 12 20 12 9 16 24 7 | 64 67 68 64 54 49 61
R15 | 1694 24 15 10 17 15 21 8 | 88 83 81 72 71 77 78
R16 | 845 15 20 20 10 22 34 9 | 80 78 96 78 104 63 83
XR17 | 755 21 12 12 25 11 --- 8 | 66 60 61 61 56 --- 59
R18E | 1129 13 13 12 24 13 18 7 | 29 28 33 34 32 23 27
R19E | 2208 20 53 35 47 36 44 17 | 43 73 46 49 38 38 36
R20E | 6512 36 48 66 42 61 75 25 | 43 69 90 51 47 47 47
R21E | 1672 11 15 13 14 12 11 5 | 34 34 39 39 33 35 34
R22E | 2623 15 16 14 12 22 20 7 | 29 39 41 36 33 40 34
R24E | 705 23 15 17 27 20 22 9 | 55 50 57 54 56 55 51
------+-----------------------------------------+-------------------------------------
RMS | 2029 18 26 21 22 22 27 |T 52 52 56 54 51 46 50
WRMS | 2029 15 18 12 14 18 27 |NE 58 54 58 58 56 50 55
MEDI | 1170 14 17 13 15 16 20 |MD 52 53 50 53 50 47 48
Table 3.2304.3 GPS week: 2304 Day: 3 MJD: 60375
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2814 36 51 20 23 14 21 13 | 76 34 53 58 59 58 55
R02 | 861 11 16 13 12 13 25 6 | 44 34 35 51 35 50 40
R03 | 975 7 16 12 13 10 26 6 | 52 49 55 61 54 35 51
R04 | 902 9 15 11 15 8 23 6 | 54 52 52 53 53 44 50
R05 | 739 11 16 10 16 15 15 6 | 46 50 39 40 47 38 42
R07 | 1284 12 15 12 16 18 17 7 | 56 51 62 45 63 50 54
R08 | 1151 13 11 16 19 7 29 7 | 51 49 47 43 48 36 44
R09 | 1067 22 10 15 16 12 11 7 | 24 25 32 19 24 25 21
R11 | 826 21 24 13 10 30 19 9 | 23 22 41 34 58 42 35
R12 | 783 9 28 15 23 14 17 8 | 47 58 51 36 57 36 46
XR13 | 898 16 29 30 48 18 --- 15 | 76 58 65 74 76 --- 68
R14 | 975 10 28 14 11 15 15 7 | 52 73 57 52 54 48 55
R15 | 2396 17 23 14 8 18 30 8 | 71 71 67 64 50 43 60
R16 | 1117 18 24 13 12 19 34 9 | 84 63 71 79 80 53 72
XR17 | 1098 10 15 12 17 13 --- 6 | 44 46 48 49 42 --- 44
R18E | 640 13 16 18 22 13 23 8 | 36 34 35 37 32 31 31
R19E | 584 22 42 36 40 25 53 16 | 36 47 58 43 36 46 30
R20E | 3336 56 66 122 80 61 95 36 | 55 87 159 58 38 62 47
R21E | 1071 10 23 19 13 11 12 6 | 43 35 54 42 43 43 42
R22E | 2574 16 11 10 12 16 15 6 | 20 24 25 25 28 17 21
R24E | 2074 12 17 18 22 21 23 8 | 47 47 52 64 51 54 49
XR25 |12267 4 --- --- --- --- --- 0 | 64 --- --- --- --- --- 9
------+-----------------------------------------+-------------------------------------
RMS | 1594 21 28 32 26 21 32 |T 50 48 55 48 48 42 43
WRMS | 1594 17 21 13 15 18 32 |NE 54 49 51 50 53 42 46
MEDI | 1067 12 17 14 16 15 23 |MD 47 49 52 49 50 43 44
Table 3.2304.4 GPS week: 2304 Day: 4 MJD: 60376
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2481 29 40 33 30 16 32 13 | 77 49 71 73 56 58 64
R02 | 580 9 12 13 13 12 27 6 | 60 64 56 62 57 62 59
R03 | 2204 9 11 12 12 13 20 5 | 54 55 54 55 52 55 53
R04 | 833 7 9 12 13 15 22 5 | 61 60 64 64 64 61 61
R05 | 810 11 19 13 14 19 23 7 | 46 47 36 37 46 37 40
R07 | 1218 9 18 15 9 24 21 7 | 57 48 58 59 63 51 55
R08 | 726 8 12 14 9 11 20 5 | 51 50 55 48 53 45 50
R09 | 1241 16 17 13 16 13 21 7 | 30 35 27 34 29 26 28
R11 | 783 9 12 10 23 30 24 8 | 27 30 30 23 47 40 29
R12 | 629 10 12 22 21 18 24 8 | 52 55 66 43 58 49 52
XR13 | 1103 11 42 27 29 18 --- 13 | 80 57 106 89 82 --- 81
R14 | 1587 9 24 14 19 8 20 7 | 42 55 45 33 47 45 42
R15 | 3161 15 13 17 15 16 22 7 | 74 75 85 88 71 72 76
R16 | 1684 18 16 9 21 21 25 8 | 77 72 71 69 69 61 69
XR17 | 1095 9 13 10 19 14 --- 6 | 39 39 40 46 39 --- 39
R18E | 935 16 21 15 22 16 21 8 | 46 55 47 40 44 34 42
R19E | 898 26 45 46 43 43 74 20 | 28 47 52 47 41 48 31
R20E | 2976 31 80 105 58 56 108 32 | 58 103 131 61 46 45 58
R21E | 1392 10 13 14 16 18 19 6 | 41 46 38 37 41 40 38
R22E | 3249 13 11 18 22 15 15 7 | 41 39 52 36 40 38 40
R24E | 2854 21 16 22 25 17 23 9 | 60 61 69 62 61 75 61
------+-----------------------------------------+-------------------------------------
RMS | 1832 16 27 30 24 23 37 |T 52 54 59 52 52 49 50
WRMS | 1832 12 18 16 17 21 37 |NE 55 52 57 54 55 50 53
MEDI | 1218 11 16 14 19 16 22 |MD 52 55 55 48 52 48 52
Table 3.2304.5 GPS week: 2304 Day: 5 MJD: 60377
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 829 28 34 24 33 19 25 12 | 77 63 61 82 57 72 68
R02 | 1013 6 12 10 13 20 27 6 | 49 54 45 48 56 47 48
R03 | 2273 17 13 11 14 12 28 7 | 52 39 38 47 43 32 41
R04 | 1321 12 14 11 15 13 21 6 | 63 63 70 63 67 71 65
R05 | 929 10 20 10 10 23 16 6 | 48 52 49 46 41 51 46
R07 | 1248 10 10 13 15 19 18 6 | 59 59 60 52 59 73 58
R08 | 807 15 8 15 13 16 17 6 | 51 48 51 53 51 59 51
R09 | 1620 13 18 14 19 16 25 7 | 36 37 41 32 40 34 34
R11 | 1102 9 13 12 6 18 22 6 | 24 22 33 26 33 28 25
R12 | 722 9 19 21 25 16 20 8 | 63 70 70 51 64 60 61
R13 | 877 18 46 38 36 18 35 14 | 82 63 90 78 80 14 75
R14 | 1516 15 16 7 12 16 28 7 | 48 59 53 54 52 57 51
R15 | 3281 16 26 14 15 21 19 8 | 78 92 83 74 66 76 77
R16 | 2064 14 22 13 17 21 19 8 | 79 91 89 85 69 88 82
XR17 | 964 11 14 17 22 19 --- 8 | 67 65 66 68 59 --- 64
R18E | 746 10 17 13 19 23 23 7 | 75 69 71 76 69 81 72
R19E | 784 31 49 48 25 36 71 19 | 79 67 94 69 63 72 70
R20E | 2020 39 77 49 38 65 101 27 | 62 114 101 71 70 71 73
R21E | 1827 12 22 20 23 18 25 9 | 38 45 45 40 34 44 39
R22E | 2894 13 9 9 17 17 17 6 | 19 21 21 27 17 24 18
R24E | 2230 12 12 13 23 17 19 7 | 123 127 127 132 119 139 126
------+-----------------------------------------+-------------------------------------
RMS | 1675 17 28 22 21 24 35 |T 60 62 64 60 55 59 59
WRMS | 1675 14 18 14 18 20 35 |NE 57 58 59 57 53 54 56
MEDI | 1248 13 17 13 17 18 22 |MD 59 63 61 54 57 59 61
Table 3.2304.6 GPS week: 2304 Day: 6 MJD: 60378
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 533 27 25 20 11 20 23 9 | 105 75 82 96 78 99 88
R02 | 561 13 10 17 12 16 22 6 | 63 67 52 57 68 66 60
R03 | 2136 13 9 9 9 11 24 5 | 70 62 64 64 60 60 63
R04 | 1174 14 12 11 17 12 19 6 | 83 83 89 83 82 79 82
R05 | 1614 16 15 11 18 10 18 6 | 63 57 61 52 58 56 57
R07 | 974 8 19 11 8 17 31 7 | 81 90 80 80 87 77 81
R08 | 962 13 15 17 17 14 27 7 | 70 78 66 74 66 67 69
R09 | 1839 12 28 10 13 14 23 7 | 27 37 35 28 34 36 29
R11 | 657 15 12 8 12 13 24 6 | 28 31 39 38 46 34 34
R12 | 1005 15 28 9 26 21 16 9 | 71 84 71 59 66 64 67
XR13 | 520 21 39 29 35 13 --- 14 | 100 70 94 90 95 --- 89
R14 | 1546 8 17 13 16 9 20 6 | 66 80 76 61 69 55 67
R15 | 2791 14 15 18 7 13 22 6 | 100 104 99 98 87 84 95
R16 | 2226 11 21 16 14 12 13 6 | 100 107 102 99 94 93 98
XR17 | 978 10 15 18 22 15 --- 8 | 62 64 64 72 60 --- 63
R18E | 768 9 16 15 16 11 18 6 | 71 67 70 75 73 70 70
R19E | 951 30 39 46 34 34 52 17 | 69 65 79 70 57 57 60
R20E | 1645 51 78 57 36 78 77 27 | 84 125 125 73 95 88 89
R21E | 1593 9 16 11 15 23 25 7 | 45 41 45 44 48 44 43
R22E | 3130 17 8 10 14 13 20 6 | 39 41 40 42 37 39 38
R24E | 2124 18 16 14 21 14 17 7 | 152 154 158 169 158 162 158
------+-----------------------------------------+-------------------------------------
RMS | 1655 19 26 21 18 24 29 |T 72 75 75 72 69 70 71
WRMS | 1655 14 18 12 14 20 29 |NE 70 72 71 70 66 66 69
MEDI | 1174 14 16 14 16 14 22 |MD 70 70 71 72 66 66 67
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