[IGSREPORT-26224] Wk 2024 IGLOS Final Orbits
acc
acc at igs.org
Sat Nov 10 03:39:57 PST 2018
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2024 (Oct 21, 2018 - Oct 27, 2018)
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 2.2024.
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:
igl2024[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2024 in the SP3 format.
igl20247.sum Combination Report for GPS Week 2024.
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.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/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
ftp://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 | 5.2 ns
1 | 5.0 ns
2 | 5.5 ns
3 | 5.5 ns
4 | 8.4 ns
5 | 3.4 ns
6 | 5.2 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 1.2024, 1a.2024).
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 2.2024.0-6)
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 3.2024.0-6).
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 2024 summary. (Oct 21, 2018 - Oct 27, 2018)
Table 1.2024.a GPS week : 2024 MJD: 58412.0-58418.0
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 -8 -6 -29 2 -.00 38 33 | -51 -1461 3539 9499
| 1 1 1 21 27 22 .04 | 1127 3393
cof n/a| -1 0 -12 4 -24 12 .04 40 34 | -56 -1460 3536 9499
| 1 1 2 15 17 19 .07 | 1125 3391
emx n/a| -1 0 3 -13 2 4 .00 20 20 | 2713 -1268 3545 9116
| 1 0 1 16 20 29 .03 | 9350 2215
esx n/a| 0 0 0 9 14 37 .10 19 17 | 3258 -1234 3540 11425
| 1 1 1 20 22 25 .02 | 8336 3642
gfz n/a| -1 0 10 22 11 -12 .09 38 35 | 0 -1337 3528 9364
| 1 1 2 23 34 24 .05 | 0 3459
grg n/a| 0 1 -5 -11 -34 -104 -.38 39 35 | 6225 -1565 3633 9063
| 1 0 2 8 26 79 .03 | 1028 3504
Table 1.2024.b GPS week : 2024 MJD: 58412.0-58418.0
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 | 26 31 28 31 32 29 27 |
R02 | 11 14 13 12 12 11 15 |
R03 | 12 11 13 12 12 11 11 |
R04 | 10 9 7 7 10 9 9 |
R05 | 14 14 12 10 9 9 11 |
R07 | 14 12 12 15 13 11 13 |
R08 | 14 13 11 11 12 9 9 |
R09 | 9 6 10 8 9 11 11 |
R10 | 12 8 7 10 8 7 10 |
R11 | 8 10 10 6 8 10 8 |
R13 | 11 8 11 11 12 9 10 |
R14 | 10 8 8 8 10 11 9 |
R15 | 20 15 17 16 18 18 18 |
R16 | 29 23 19 22 26 20 20 |
R17 | 12 11 11 11 9 10 10 |
R18 | 9 9 8 9 8 9 9 |
R19 | 23 22 23 26 20 19 21 |
R20 | 15 16 14 11 15 15 13 |
R21 | 12 11 11 10 11 11 12 |
R22 | 11 10 11 11 10 11 12 |
R23 | 13 12 10 10 11 13 13 |
R24 | 18 19 17 13 15 19 16 |
R26 | 0 0 0 --- --- --- --- |
Table 1.2024.c GPS week : 2024 MJD: 58412.0-58418.0
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 2024 0 | -77 31 -69 -788 400 -7524 79.5 2791 2791 | 5230 0
brd 2024 1 | -51 -14 -125 710 325 -9269 82.4 2655 2655 | 5023 0
brd 2024 2 | -100 -29 -48 1529 -2756 -5790 81.9 1986 1986 | 5521 0
brd 2024 3 | -43 -37 -70 -1341 -1018 -250 82.6 1268 1268 | 5455 0
brd 2024 4 | 0 -25 -88 -1579 -1084 -867 82.2 1275 1275 | 8392 0
brd 2024 5 | -32 104 -63 -1192 -1599 -126 82.7 1495 1495 | 3371 0
brd 2024 6 | -114 9 -34 -1243 -895 -1627 83.5 1579 1579 | 5201 0
-------------+------------------------------------------------------------+----------------
brd 2024 mean| -59 5 -71 -557 -946 -3636 82.1 1864 1864 | 5456 0
brd 2024 sdev| 40 49 29 1193 1092 3807 1.2 635 635 | 1487 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 2.2024.0 GPS week: 2024 Day: 0 MJD: 58412
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 -9 -28 -10 -35 .06 37 35 | 397 -1167 3286 10347
cof n/a| 0 -1 -11 2 -39 6 .13 39 36 | 397 -1172 3287 10344
emx n/a| -2 0 3 13 14 -48 .03 24 24 | 2267 -1171 3284 9928
esx n/a| 2 -1 2 -29 -6 87 .07 22 20 | -7146 -663 3290 12321
gfz n/a| 0 2 14 32 -29 -28 .12 37 33 | 0 -250 3294 10201
grg n/a| 1 1 -6 -27 0 -58 -.42 40 38 | 5699 -631 3276 9710
Table 2.2024.1 GPS week: 2024 Day: 1 MJD: 58413
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 -8 27 -17 0 .02 38 34 | -121 -1240 3653 9654
cof n/a| -2 0 -17 17 0 -2 .05 39 34 | -132 -1233 3650 9654
emx n/a| -1 0 3 -8 25 6 .01 21 21 | 10429 -1364 3660 9414
esx n/a| 0 1 0 7 -9 2 .09 20 17 | -6560 -1271 3650 11712
gfz n/a| -1 -1 11 -1 11 -35 .08 40 40 | 0 -1288 3671 9626
grg n/a| 2 1 -4 -14 -10 -38 -.39 39 34 | 5858 -1725 3833 9272
Table 2.2024.2 GPS week: 2024 Day: 2 MJD: 58414
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 -10 -31 -40 -1 .02 41 32 | -921 -1172 3428 7610
cof n/a| -2 0 -13 -16 -41 3 .10 44 34 | -932 -1150 3426 7613
emx n/a| 2 1 1 -19 -8 -23 -.03 17 17 | 3704 -1644 3437 7345
esx n/a| -2 0 0 22 42 35 .10 18 16 | 8090 65 3430 9448
gfz n/a| -2 0 8 31 -10 -10 .16 37 43 | 0 -1217 3413 7485
grg n/a| -1 0 -2 -14 -27 20 -.37 40 38 | 6121 -1090 3429 7060
Table 2.2024.3 GPS week: 2024 Day: 3 MJD: 58415
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 -6 11 10 21 -.01 40 30 | -1526 -1493 4207 9555
cof n/a| 0 2 -13 4 -1 55 .09 43 32 | -1529 -1494 4202 9556
emx n/a| -2 0 3 -33 -15 34 .05 20 20 | -6255 -1287 4206 9262
esx n/a| 0 -1 1 35 21 31 .10 18 14 | 12501 -3442 4206 11565
gfz n/a| 0 1 6 -3 40 31 .12 37 31 | 0 -2330 4153 9441
grg n/a| 2 0 -6 -4 -24 -135 -.38 36 30 | 6621 -2757 4518 9023
Table 2.2024.4 GPS week: 2024 Day: 4 MJD: 58416
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 1 -7 4 -75 -15 -.03 40 31 | 723 4934 2972 10264
cof n/a| -3 0 -11 27 -20 12 -.06 38 30 | 723 4923 2967 10264
emx n/a| 0 0 3 -22 -27 22 -.00 21 21 | 15291 3109 2988 9782
esx n/a| 0 -1 0 11 43 46 .12 18 15 | -77 5778 2986 12395
gfz n/a| 1 1 11 1 73 -26 .04 39 30 | 0 5300 2973 10068
grg n/a| 0 1 -8 -8 -44 -196 -.38 43 39 | 5683 5222 2969 9957
Table 2.2024.5 GPS week: 2024 Day: 5 MJD: 58417
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 -7 -17 -32 23 -.06 39 35 | 1806 -3985 3478 9561
cof n/a| -1 -2 -8 3 -37 5 -.03 43 38 | 1791 -3978 3477 9563
emx n/a| -2 0 3 1 2 20 -.02 18 18 | -12020 -2211 3491 8987
esx n/a| 1 0 0 0 10 30 .12 18 16 | 12871 -3691 3475 11066
gfz n/a| -1 0 11 49 0 -26 .01 39 35 | 0 -3845 3505 9430
grg n/a| 1 2 -3 -10 -71 -149 -.33 41 37 | 5248 -4074 3672 9451
Table 2.2024.6 GPS week: 2024 Day: 6 MJD: 58418
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 -13 -40 23 .00 36 33 | -718 -6108 3750 9502
cof n/a| -2 1 -12 -10 -33 3 -.00 36 34 | -712 -6120 3745 9504
emx n/a| 0 0 4 -24 26 17 -.01 20 20 | 5578 -4308 3751 9095
esx n/a| 1 0 0 16 -2 32 .11 20 18 | 3128 -5419 3744 11470
gfz n/a| -2 1 11 50 -4 10 .12 39 32 | 0 -5729 3689 9297
grg n/a| 0 2 -7 -1 -64 -171 -.36 35 33 | 8350 -5901 3740 8972
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 3.2024.0 GPS week: 2024 Day: 0 MJD: 58412
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 1398 86 92 25 46 57 51 26 | 124 129 51 52 55 87 54
R02 | 941 30 33 19 12 28 21 10 | 85 89 54 57 40 80 59
R03 | 1738 31 38 16 16 38 27 12 | 86 91 63 56 42 86 63
R04 | 1268 24 26 9 10 37 29 10 | 78 82 60 63 50 80 64
R05 | 1806 41 45 21 20 42 24 14 | 157 166 134 146 128 150 141
R07 | 1300 37 42 17 15 44 34 13 | 92 90 64 55 47 86 64
R08 | 1216 27 27 17 16 41 46 13 | 88 89 66 70 55 103 72
R09 | 932 12 14 15 14 28 21 8 | 43 42 48 43 46 49 44
R10 | 1255 12 16 10 14 44 41 11 | 42 44 43 44 32 59 42
R11 | 1861 16 16 11 11 30 17 8 | 50 47 39 50 36 41 42
R13 | 4230 15 11 11 20 26 37 10 | 53 49 39 46 31 43 40
R14 | 687 17 12 12 15 36 22 9 | 53 48 44 43 26 56 43
R15 | 9755 31 39 26 40 57 47 19 | 78 81 66 42 42 86 56
R16 | 1148 22 32 71 40 33 91 28 | 48 55 48 63 42 70 52
R17 | 2344 34 34 16 11 40 22 11 | 146 157 137 144 131 149 141
R18 | 1323 13 13 17 16 21 19 8 | 80 86 82 96 77 93 86
R19 | 4692 92 94 24 25 53 30 23 | 109 111 72 68 76 83 70
R20 | 1695 24 26 28 21 29 47 14 | 94 95 79 79 73 113 83
R21 | 487 29 28 15 16 37 33 12 | 92 92 70 74 69 92 75
R22 | 924 37 35 15 8 25 22 10 | 89 91 58 64 56 66 64
R23 | 762 16 18 23 31 14 29 12 | 83 86 80 101 89 90 88
R24 | 1682 21 20 32 19 31 72 18 | 119 130 112 133 115 158 123
XR26 | 3671 6 50 --- --- --- --- 0 | 43 90 --- --- --- --- 43
------+-----------------------------------------+-------------------------------------
RMS | 2790 37 39 24 22 37 40 |T 84 88 68 72 61 87 69
WRMS | 2790 35 36 24 20 33 38 |NE 84 88 68 72 61 87 69
MEDI | 1323 24 28 17 16 36 29 |MD 85 89 63 63 50 86 64
Table 3.2024.1 GPS week: 2024 Day: 1 MJD: 58413
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 1991 102 104 32 55 78 58 30 | 91 92 41 26 43 56 25
R02 | 1835 30 29 16 13 35 51 13 | 61 61 38 37 29 72 42
R03 | 857 31 28 14 15 35 30 11 | 66 63 46 37 30 65 45
R04 | 1309 21 19 15 10 27 26 9 | 49 46 37 41 30 52 39
R05 | 1556 36 40 18 21 49 29 13 | 132 141 119 134 124 134 126
R07 | 1151 41 43 15 12 39 21 11 | 63 67 38 33 23 40 36
R08 | 1509 33 36 11 18 44 39 13 | 61 62 46 34 32 66 43
R09 | 832 11 12 10 5 22 16 5 | 37 37 36 39 42 43 37
R10 | 1105 9 10 12 8 25 28 7 | 27 24 28 37 37 32 31
R11 | 1206 18 26 9 9 42 28 9 | 30 38 32 27 25 40 28
R13 | 3677 18 18 11 11 33 12 7 | 31 31 31 35 34 25 30
R14 | 1443 22 21 9 10 34 15 8 | 33 30 31 30 23 28 29
R15 | 8709 28 23 21 24 49 39 14 | 44 42 40 44 43 46 40
R16 | 2391 23 28 49 15 47 86 22 | 41 38 40 33 25 28 33
R17 | 1045 30 25 16 13 40 19 10 | 115 108 102 103 95 104 103
R18 | 1122 13 13 15 21 23 15 9 | 76 79 72 86 78 73 77
R19 | 5549 88 82 22 25 56 36 21 | 75 73 57 53 54 61 54
R20 | 937 22 26 27 28 27 51 15 | 54 56 56 63 48 73 56
R21 | 771 31 34 18 12 37 23 11 | 49 51 37 36 30 52 38
R22 | 905 37 42 13 12 29 17 10 | 48 51 37 33 31 40 35
R23 | 833 16 14 26 25 19 14 11 | 55 63 48 64 52 56 55
R24 | 1608 19 41 33 12 37 82 19 | 89 104 85 79 83 80 80
XR26 | 2486 5 57 --- --- --- --- 0 | 24 29 --- --- --- --- 24
------+-----------------------------------------+-------------------------------------
RMS | 2655 38 39 21 20 40 39 |T 58 60 49 50 45 57 48
WRMS | 2655 34 34 21 17 40 34 |NE 58 60 49 50 45 57 48
MEDI | 1309 23 28 15 13 35 28 |MD 54 56 40 37 34 52 39
Table 3.2024.2 GPS week: 2024 Day: 2 MJD: 58414
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 1925 116 124 22 43 65 55 28 | 105 113 25 24 39 56 24
R02 | 2088 35 46 15 11 42 40 12 | 64 72 40 34 23 66 40
R03 | 813 30 32 15 19 34 45 13 | 71 74 49 54 39 79 52
R04 | 1200 19 22 11 10 23 16 7 | 66 73 51 56 51 56 54
R05 | 1600 28 26 19 21 37 26 12 | 121 121 113 98 89 110 105
R07 | 874 39 38 16 19 36 13 11 | 74 71 49 32 23 44 41
R08 | 1742 29 29 13 13 38 30 10 | 68 67 42 40 24 67 44
R09 | 783 19 22 13 18 27 25 9 | 44 50 52 44 41 41 44
R10 | 1200 12 12 13 11 17 22 7 | 30 32 31 41 41 37 34
R11 | 1035 18 20 11 9 34 39 10 | 37 35 38 35 33 46 34
R13 | 2154 24 26 14 13 42 27 10 | 39 41 37 28 25 45 31
R14 | 979 17 17 11 10 26 24 8 | 37 38 35 41 38 48 37
R15 | 4916 29 30 12 23 56 61 16 | 53 49 39 34 33 68 39
R16 | 1682 38 39 21 15 34 87 19 | 44 45 61 34 31 40 38
R17 | 788 28 30 18 14 37 17 10 | 111 109 103 105 100 91 102
R18 | 1048 10 13 16 15 23 19 8 | 55 53 52 57 43 58 53
R19 | 5277 89 103 28 25 53 50 22 | 87 97 52 46 63 67 50
R20 | 886 22 22 19 15 44 50 13 | 65 71 69 64 70 70 64
R21 | 867 33 31 16 15 35 14 10 | 54 51 36 31 33 29 32
R22 | 751 43 42 12 12 33 12 10 | 66 63 49 47 45 45 47
R23 | 617 14 18 22 18 14 27 10 | 85 94 82 89 79 87 84
R24 | 1574 36 37 23 19 30 68 16 | 117 119 89 94 102 124 97
XR26 | 1609 6 92 --- --- --- --- 0 | 53 99 --- --- --- --- 53
------+-----------------------------------------+-------------------------------------
RMS | 1986 41 44 17 18 37 40 |T 67 71 54 51 48 62 52
WRMS | 1986 32 34 17 16 43 38 |NE 67 71 54 51 48 62 52
MEDI | 1200 28 30 15 15 34 27 |MD 65 71 49 41 39 56 44
Table 3.2024.3 GPS week: 2024 Day: 3 MJD: 58415
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 930 111 114 36 42 58 73 30 | 112 115 33 50 60 92 41
R02 | 2060 37 39 11 14 33 33 11 | 68 71 37 35 28 64 41
R03 | 1058 28 30 14 13 40 32 11 | 68 68 49 41 25 69 48
R04 | 766 18 17 13 10 15 10 6 | 66 65 55 52 50 61 55
R05 | 1001 24 19 20 16 23 16 9 | 89 89 72 79 75 87 77
R07 | 764 34 33 15 21 58 37 15 | 73 74 55 41 33 81 51
R08 | 1142 19 24 11 13 33 38 10 | 73 75 53 51 33 87 57
R09 | 1069 15 17 9 11 25 24 8 | 27 26 32 26 32 36 28
R10 | 1073 10 12 17 10 33 30 9 | 36 36 37 39 30 51 36
R11 | 598 11 15 9 11 22 10 6 | 37 37 31 41 30 33 34
R13 | 1295 27 32 13 10 54 17 11 | 47 48 40 32 28 37 33
R14 | 865 13 12 8 6 34 23 8 | 43 40 34 41 34 46 38
R15 | 2251 30 30 14 22 45 56 15 | 63 61 50 44 60 81 51
R16 | 1206 22 45 43 13 30 87 21 | 49 53 48 52 46 51 45
R17 | 720 34 39 18 14 31 13 10 | 150 156 144 150 138 147 147
R18 | 766 9 12 19 20 18 11 8 | 99 105 95 112 95 103 102
R19 | 2983 103 105 33 35 60 35 25 | 104 108 79 90 88 77 78
R20 | 989 21 36 15 14 39 35 11 | 74 68 68 68 62 83 69
R21 | 962 30 32 15 12 33 20 10 | 60 61 38 41 29 39 39
R22 | 908 38 43 16 12 29 16 10 | 80 84 57 56 51 68 59
R23 | 765 16 23 24 20 17 17 10 | 81 78 76 86 75 94 81
R24 | 864 22 26 26 19 37 30 13 | 113 123 122 133 117 107 120
------+-----------------------------------------+-------------------------------------
RMS | 1268 40 43 20 18 37 36 |T 73 74 59 61 55 72 60
WRMS | 1268 30 32 20 14 31 30 |NE 73 74 59 61 55 72 60
MEDI | 962 22 30 15 13 33 24 |MD 68 68 50 50 46 69 51
Table 3.2024.4 GPS week: 2024 Day: 4 MJD: 58416
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 698 116 98 26 50 67 89 32 | 95 87 46 62 67 79 42
R02 | 2258 35 36 22 11 30 26 11 | 73 74 45 59 46 62 53
R03 | 1313 28 31 14 16 44 35 12 | 75 77 58 50 38 83 57
R04 | 1261 24 23 16 13 38 20 9 | 67 64 62 52 46 64 55
R05 | 1347 23 31 17 14 24 21 9 | 119 129 111 119 106 113 114
R07 | 879 33 39 14 18 48 38 13 | 72 79 57 46 35 74 52
R08 | 832 21 19 11 8 47 42 11 | 67 65 57 53 32 82 56
R09 | 1374 12 11 10 11 20 37 8 | 55 59 61 62 62 61 60
R10 | 1214 12 11 11 6 38 20 7 | 45 45 40 43 45 39 41
R11 | 507 18 23 13 9 36 12 8 | 43 46 41 46 36 36 41
R13 | 1676 27 29 11 13 32 46 11 | 50 55 43 43 44 49 42
R14 | 741 22 21 9 13 43 30 10 | 47 46 42 39 34 48 40
R15 | 2774 28 26 17 26 54 69 17 | 59 59 58 50 45 78 53
R16 | 539 17 23 57 19 48 103 25 | 44 52 57 40 42 63 42
R17 | 509 32 29 13 7 29 19 9 | 99 97 86 99 98 81 92
R18 | 641 10 11 16 17 16 18 8 | 56 57 52 67 59 62 59
R19 | 798 85 77 24 21 46 26 19 | 74 76 56 66 72 51 57
R20 | 750 41 39 21 17 45 43 14 | 59 50 62 66 68 89 63
R21 | 1177 36 34 15 10 43 25 11 | 62 62 44 42 47 46 43
R22 | 535 41 41 10 9 30 22 10 | 59 61 38 42 29 39 39
R23 | 1184 23 22 23 23 23 12 11 | 81 97 90 96 79 84 88
R24 | 1915 30 39 26 21 28 48 14 | 75 83 83 94 86 93 85
------+-----------------------------------------+-------------------------------------
RMS | 1275 40 38 21 18 39 43 |T 67 69 58 60 55 67 57
WRMS | 1275 31 30 21 15 30 39 |NE 67 69 58 60 55 67 57
MEDI | 879 27 29 15 13 38 26 |MD 62 62 57 52 46 63 53
Table 3.2024.5 GPS week: 2024 Day: 5 MJD: 58417
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 881 95 105 21 47 64 92 29 | 74 90 47 53 58 84 42
R02 | 1711 35 42 15 9 28 36 11 | 72 76 44 49 47 72 51
R03 | 975 30 35 16 12 36 31 11 | 72 79 59 59 41 67 59
R04 | 2008 26 34 11 12 33 17 8 | 71 80 59 60 45 63 59
R05 | 1459 24 24 11 8 38 25 9 | 74 77 64 64 51 70 64
R07 | 765 30 25 10 12 37 32 10 | 72 66 54 53 40 71 56
R08 | 1119 27 36 10 10 32 25 9 | 63 69 48 48 42 58 49
R09 | 1181 10 10 11 10 27 52 11 | 34 35 34 37 43 56 36
R10 | 762 12 14 12 12 24 14 7 | 23 25 22 29 24 22 23
R11 | 940 23 23 12 10 45 19 9 | 27 27 19 25 25 22 19
R13 | 3525 19 21 10 11 36 22 8 | 34 38 31 39 23 37 32
R14 | 801 21 29 12 17 42 26 10 | 33 40 30 27 28 34 26
R15 | 1916 40 43 21 31 65 40 17 | 43 43 36 21 36 34 26
R16 | 732 9 31 38 19 50 80 20 | 51 70 47 52 47 76 47
R17 | 1009 32 32 16 12 37 16 10 | 133 133 129 131 125 130 129
R18 | 573 11 16 18 19 21 18 9 | 89 89 91 89 81 86 88
R19 | 1452 82 83 23 18 41 30 18 | 76 76 76 79 81 66 73
R20 | 986 38 47 21 17 37 52 14 | 74 79 64 64 60 62 62
R21 | 1259 39 37 17 13 33 23 11 | 56 58 44 42 42 49 43
R22 | 614 44 47 13 5 39 20 11 | 66 68 40 50 43 58 47
R23 | 1840 39 36 17 27 19 21 12 | 75 74 76 84 79 77 78
R24 | 2560 37 52 33 20 29 74 19 | 105 108 112 123 114 135 116
------+-----------------------------------------+-------------------------------------
RMS | 1494 39 43 18 18 39 41 |T 64 68 55 58 53 64 55
WRMS | 1494 35 38 18 16 35 37 |NE 64 68 55 58 53 64 55
MEDI | 1009 30 34 15 12 36 25 |MD 71 70 47 52 43 63 49
Table 3.2024.6 GPS week: 2024 Day: 6 MJD: 58418
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg IGL | cod cof emx esx gfz grg IGL
------+-----------------------------------------+-------------------------------------
R01 | 1571 79 61 27 49 73 56 26 | 121 114 74 60 58 106 67
R02 | 1978 36 37 12 23 47 47 15 | 98 97 72 64 58 104 73
R03 | 757 25 27 10 17 31 33 10 | 99 99 79 73 61 107 81
R04 | 2327 23 20 14 14 28 21 9 | 92 91 79 81 68 91 81
R05 | 917 28 28 17 17 39 15 11 | 107 111 95 89 77 96 92
R07 | 1141 21 31 13 14 42 49 13 | 106 111 89 81 66 119 89
R08 | 1597 22 20 12 8 31 29 9 | 100 101 86 84 74 109 88
R09 | 1318 14 15 11 13 26 43 10 | 55 55 53 53 59 66 54
R10 | 798 9 11 19 10 21 36 9 | 50 53 46 54 50 64 50
R11 | 679 13 17 13 9 31 18 7 | 49 51 45 47 39 52 45
R13 | 2813 28 29 13 8 41 13 9 | 61 60 50 46 31 48 46
R14 | 770 21 23 14 16 33 15 9 | 56 58 53 45 37 60 48
R15 | 1687 41 43 20 32 64 44 18 | 78 80 65 52 46 83 60
R16 | 1753 18 27 44 16 52 62 19 | 65 66 40 56 43 71 50
R17 | 1396 26 28 14 12 31 24 9 | 143 137 133 132 128 141 133
R18 | 522 10 15 19 13 19 27 8 | 95 93 95 96 93 102 95
R19 | 2745 87 78 24 23 42 28 20 | 109 108 93 99 113 94 93
R20 | 1450 39 45 19 19 34 25 12 | 102 106 89 91 92 94 90
R21 | 715 35 38 24 19 26 22 12 | 100 102 84 88 81 91 86
R22 | 1029 39 43 19 12 31 24 11 | 91 94 67 68 59 74 69
R23 | 1442 32 39 22 30 12 17 12 | 103 104 109 129 111 111 114
R24 | 2227 27 32 25 19 39 54 15 | 127 127 127 140 137 159 134
------+-----------------------------------------+-------------------------------------
RMS | 1578 36 36 20 20 39 35 |T 91 91 78 78 71 92 79
WRMS | 1578 33 34 20 18 32 33 |NE 91 91 78 78 71 92 79
MEDI | 1396 26 28 17 16 31 27 |MD 98 97 79 73 61 94 81
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