[IGSREPORT-29904] Wk 2314 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 3 06:47:41 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2314 (May 12, 2024 - May 18, 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 2.2314.
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:
igl2314[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2314 in the SP3 format.
igl23147.sum Combination Report for GPS Week 2314.
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 | 2.7 ns
1 | 0.9 ns
2 | -0.5 ns
3 | -1.4 ns
4 | 0.2 ns
5 | 2.0 ns
6 | 2.1 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 | ESA | R20
3 | ESA | R20
4 | GRG | R09
5 | ESA | R20
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2314, 1a.2314).
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 2.2314.0-6)
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 3.2314.0-6).
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 2314 summary. (May 12, 2024 - May 18, 2024)
Table 1.2314.a GPS week : 2314 MJD: 60442.0-60448.0
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 2 -7 -18 25 .18 19 15 | 13712 354 5773 44771
| 0 0 1 16 15 24 .04 | 1541 2372
esa n/a| -2 0 0 0 -6 -10 -.10 39 25 | -3850 343 3741 8051
| 1 1 1 15 12 31 .02 | 4014 1730
gfz n/a| 1 0 6 5 8 -5 -.08 20 14 | 0 -800 3757 7572
| 0 1 2 16 9 24 .05 | 0 1893
grg n/a| 2 0 -2 -21 -12 12 .37 28 25 | 9294 284 5902 45457
| 1 1 2 27 14 41 .04 | 2818 2272
iac n/a| 0 0 -2 16 13 -32 -.13 21 18 | 10859 585 5860 46512
| 1 1 1 19 23 86 .05 | 2476 1697
jgx n/a| 0 0 -8 2 34 15 -.17 28 28 | 6996 -695 3956 7836
| 0 0 1 15 11 42 .03 | 1967 2153
Table 1.2314.b GPS week : 2314 MJD: 60442.0-60448.0
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 | 16 16 16 14 16 16 15 |
R02 | 8 7 6 8 6 6 8 |
R03 | 8 7 7 6 4 4 7 |
R04 | 6 7 6 7 7 7 8 |
R05 | 8 7 6 5 6 6 8 |
R07 | 6 6 6 5 8 6 8 |
R08 | 8 6 6 6 6 10 9 |
R09 | 9 9 11 18 49 11 8 |
R11 | 6 7 7 8 8 7 7 |
R12 | 9 7 7 7 7 7 7 |
R13 | 17 17 16 16 21 20 20 |
R14 | 8 6 7 5 6 7 8 |
R15 | 7 8 6 8 6 6 6 |
R16 | 7 8 9 9 7 8 10 |
R17 | 7 9 9 7 6 8 7 |
R18 | 7 9 7 7 7 7 7 |
R19 | 18 18 17 16 20 19 19 |
R20 | 23 26 27 28 25 22 30 |
R21 | 9 7 8 7 9 8 7 |
R22 | 6 7 7 8 8 8 7 |
R24 | 8 9 8 8 7 9 7 |
R25 | 10 11 10 9 14 16 13 |
R26 | 26 37 33 40 40 26 22 |
Table 1.2314.c GPS week : 2314 MJD: 60442.0-60448.0
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 2314 0 | -106 -66 190 -852 1377 -1539 78.8 2531 2531 | 2698 0
brd 2314 1 | 9 -22 87 611 1222 -6940 78.8 2181 2181 | 941 0
brd 2314 2 | 94 -10 12 1894 2308 -6527 78.0 2116 2116 | -487 0
brd 2314 3 | -44 -20 77 535 -1266 -4325 79.7 1876 1876 | -1372 0
brd 2314 4 | -16 -20 95 1130 -2075 -4033 79.7 1683 1683 | 174 0
brd 2314 5 | -6 -7 237 1339 885 -2242 81.2 2267 2267 | 1983 0
brd 2314 6 | 33 -36 153 -1284 79 1179 80.0 2282 2282 | 2125 0
-------------+------------------------------------------------------------+----------------
brd 2314 mean| -5 -26 122 481 361 -3489 79.5 2133 2133 | 866 0
brd 2314 sdev| 62 20 76 1159 1554 2865 1.0 279 279 | 1500 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 2.2314.0 GPS week: 2314 Day: 0 MJD: 60442
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 5 0 -37 -10 .13 20 18 | 13983 -41 4980 38997
esa n/a| -1 0 0 -7 2 -12 -.10 38 25 | 211 870 3932 9657
gfz n/a| 1 -1 3 14 -8 -2 -.01 23 16 | 0 -661 4035 8686
grg n/a| 3 0 -1 -13 -9 14 .33 24 27 | 10310 -141 5045 39572
iac n/a| -3 -1 -3 26 13 33 -.12 29 23 | 12846 -1684 5050 40805
jgx n/a| 0 1 -7 3 36 -9 -.19 23 23 | 8058 -345 4092 8916
Table 2.2314.1 GPS week: 2314 Day: 1 MJD: 60443
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 -5 -27 21 .15 17 16 | 12216 4636 5358 40194
esa n/a| -3 0 0 -5 6 -43 -.11 37 27 | -8274 3802 3837 9063
gfz n/a| 1 1 4 -7 5 -19 -.12 21 14 | 0 2737 3755 9076
grg n/a| 2 0 -2 -5 -21 -8 .34 29 24 | 6170 4213 5406 40627
iac n/a| 0 -1 0 21 36 0 -.05 22 19 | 9717 1091 5415 41928
jgx n/a| 0 0 -7 12 19 -5 -.16 26 26 | 6715 3643 4218 9189
Table 2.2314.2 GPS week: 2314 Day: 2 MJD: 60444
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 2 -14 -2 22 .23 18 14 | 16536 -1754 5475 40672
esa n/a| -2 0 0 -14 -8 -3 -.09 36 23 | -1909 -913 4703 8954
gfz n/a| 2 2 5 13 21 17 -.06 19 12 | 0 -2280 4675 7709
grg n/a| 3 2 -3 23 0 88 .33 32 32 | 8615 -2046 5582 41161
iac n/a| -2 0 -3 -6 -12 -122 -.16 18 16 | 10631 -1466 5529 42411
jgx n/a| 0 0 -9 25 18 52 -.17 28 28 | 10412 -2692 4980 7658
Table 2.2314.3 GPS week: 2314 Day: 3 MJD: 60445
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 0 -23 -29 60 .26 21 16 | 12647 -1179 5300 40568
esa n/a| -3 -2 -1 7 -14 -43 -.05 43 22 | -6384 146 4199 7534
gfz n/a| 0 0 9 24 14 -18 -.02 18 13 | 0 -1627 4243 7618
grg n/a| 2 0 0 -16 -41 -46 .41 30 27 | 6742 -1292 5460 41179
iac n/a| 0 1 -2 21 41 38 -.10 17 16 | 7386 761 5405 42224
jgx n/a| 1 1 -5 -21 35 -55 -.22 28 28 | 6217 -720 4375 7822
Table 2.2314.4 GPS week: 2314 Day: 4 MJD: 60446
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 0 23 -25 40 .18 20 13 | 12204 -504 5983 38633
esa n/a| -1 1 0 -9 -13 -29 -.10 39 29 | 836 -176 3593 6723
gfz n/a| 2 -1 8 -15 13 -5 -.13 20 14 | 0 -271 3632 7098
grg n/a| 0 1 0 -33 -7 -7 .37 27 22 | 7591 -425 6136 39338
iac n/a| 0 0 -4 1 14 -31 -.17 21 18 | 8882 508 6090 40365
jgx n/a| 0 1 -8 -8 43 72 -.16 31 30 | 5813 -885 3912 7650
Table 2.2314.5 GPS week: 2314 Day: 5 MJD: 60447
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| -3 1 1 -22 -3 3 .17 17 14 | 14399 -1283 6032 49129
esa n/a| 0 -1 2 29 -23 38 -.12 41 22 | -2434 -1613 2971 7363
gfz n/a| 2 0 6 -9 2 -41 -.11 17 14 | 0 -3170 2984 7265
grg n/a| 2 -1 0 -49 -2 26 .42 24 17 | 11775 -940 6188 49885
iac n/a| 1 0 -2 48 -19 30 -.17 20 16 | 11891 1837 6144 50826
jgx n/a| -1 0 -7 6 46 26 -.20 30 30 | 7590 -2878 3067 7885
Table 2.2314.6 GPS week: 2314 Day: 6 MJD: 60448
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 3 -6 -1 42 .17 19 15 | 14004 2609 7285 65208
esa n/a| -1 0 -1 4 8 19 -.09 38 29 | -8998 285 2956 7063
gfz n/a| 0 0 6 22 10 32 -.11 21 14 | 0 -329 2979 5555
grg n/a| 3 -1 -6 -54 -6 17 .39 30 23 | 13858 2619 7502 66443
iac n/a| 0 1 0 0 23 -180 -.16 23 21 | 14663 3048 7387 67026
jgx n/a| 0 0 -11 1 39 27 -.12 32 29 | 4168 -992 3049 5737
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 3.2314.0 GPS week: 2314 Day: 0 MJD: 60442
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1152 41 45 31 33 19 32 16 | 87 41 76 60 53 42 58
R02 | 2540 16 13 8 14 33 17 7 | 74 62 71 68 81 66 69
R03 | 4284 13 10 11 17 40 8 7 | 67 67 74 68 87 67 69
R04 | 976 16 8 13 11 21 14 6 | 94 85 91 90 79 69 86
R05 | 726 24 12 23 8 20 13 8 | 60 52 45 49 45 45 48
R07 | 1971 9 16 9 9 28 8 6 | 69 53 67 68 77 60 65
R08 | 700 12 12 16 13 32 18 7 | 59 57 68 65 53 59 59
R09 | 5000 22 18 22 24 23 10 9 | 694 695 693 709 693 42 695
R11 | 4637 13 11 19 10 20 10 6 | 41 40 54 39 38 31 40
R12 | 3987 10 16 23 20 20 20 8 | 62 68 76 64 65 51 63
R13 | 1051 19 32 55 23 50 45 17 | 83 56 98 56 94 42 68
R14 | 2895 12 18 17 20 27 11 7 | 65 71 64 58 73 60 63
R15 | 1419 14 14 10 16 20 16 6 | 71 69 68 62 66 58 65
R16 | 943 16 19 12 16 16 14 7 | 88 79 86 83 83 76 82
XR17 | 3273 5 14 16 11 15 --- 6 | 35 33 34 29 46 --- 32
R18 | 1012 17 16 12 11 25 11 7 | 27 34 29 28 37 29 27
R19 | 1881 36 26 31 65 41 34 18 | 49 36 52 58 58 55 48
R20 | 1990 28 146 40 48 42 61 22 | 88 99 90 96 85 85 84
R21 | 835 13 16 15 18 31 21 8 | 45 47 48 48 54 40 45
R22 | 2841 15 11 12 10 15 9 5 | 32 34 34 39 39 33 33
R24 | 2001 8 26 19 14 27 13 8 | 54 57 55 54 63 50 54
XR25 |16556 15 10 --- --- 18 --- 10 | 38 40 --- --- 42 --- 38
XR26 |15789 29 --- --- 15 63 --- 25 | 57 --- --- 74 124 --- 78
------+-----------------------------------------+-------------------------------------
RMS | 2530 20 38 23 24 29 23 |T 88 85 93 89 92 53 85
WRMS | 2530 18 25 16 27 23 23 |NE 88 85 93 89 92 53 85
MEDI | 1990 15 16 16 15 25 14 |MD 62 56 68 60 65 51 63
Table 3.2314.1 GPS week: 2314 Day: 1 MJD: 60443
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1184 35 71 19 23 22 32 15 | 62 36 58 69 62 48 53
R02 | 1307 10 17 7 15 21 23 7 | 51 39 51 49 56 50 49
R03 | 2512 12 11 12 25 16 18 7 | 51 51 44 64 53 45 49
R04 | 739 12 8 18 9 20 21 7 | 72 70 79 71 58 50 68
R05 | 866 20 10 14 8 10 13 6 | 54 37 43 47 42 37 43
R07 | 1690 7 16 16 14 15 15 6 | 55 48 63 53 62 51 55
R08 | 664 11 18 12 15 14 15 6 | 48 49 51 54 49 45 48
R09 | 3133 19 18 19 18 19 17 8 | 657 658 649 666 655 32 655
R11 | 4915 12 13 18 22 15 14 7 | 27 32 40 32 36 31 31
R12 | 3282 10 20 18 14 14 15 7 | 40 53 56 44 50 41 45
R13 | 983 16 40 50 33 29 55 17 | 49 55 79 45 66 28 49
R14 | 4083 6 21 10 21 9 10 5 | 51 59 49 39 45 48 47
R15 | 983 13 18 15 24 23 18 8 | 51 51 42 39 59 34 44
R16 | 1213 10 26 11 22 18 16 7 | 54 56 56 41 61 43 51
XR17 | 2550 14 15 13 21 26 --- 9 | 24 27 38 34 34 --- 28
R18 | 876 16 25 14 24 14 23 8 | 25 29 27 29 24 26 22
R19 | 1012 30 27 35 73 35 40 18 | 47 36 40 27 25 37 27
R20 | 2240 28 123 37 63 46 47 26 | 53 52 53 44 41 48 44
R21 | 1042 8 14 11 15 20 22 7 | 28 33 29 34 35 26 28
R22 | 2714 13 15 10 18 15 16 6 | 20 28 22 24 29 26 20
R24 | 1015 14 17 12 20 24 30 9 | 46 50 45 52 43 37 43
XR25 |15288 15 14 --- --- 17 --- 11 | 38 37 --- --- 39 --- 35
XR26 |14357 40 --- --- 27 75 --- 36 | 42 --- --- 50 99 --- 58
------+-----------------------------------------+-------------------------------------
RMS | 2181 17 37 21 29 22 26 |T 71 72 76 73 74 39 69
WRMS | 2181 16 27 14 24 19 26 |NE 71 72 76 73 74 39 69
MEDI | 1307 13 17 14 21 19 18 |MD 49 48 49 44 49 37 45
Table 3.2314.2 GPS week: 2314 Day: 2 MJD: 60444
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1422 40 57 24 41 13 42 16 | 73 47 55 55 56 54 55
R02 | 742 7 19 13 11 15 15 6 | 77 74 78 84 76 83 78
R03 | 876 9 13 11 16 18 23 6 | 59 62 63 72 47 48 57
R04 | 966 18 10 13 13 12 14 6 | 93 98 94 103 85 86 95
R05 | 1448 8 12 15 13 13 15 5 | 59 66 75 65 54 66 63
R07 | 993 12 10 14 15 12 15 6 | 65 63 76 78 70 63 69
R08 | 991 11 10 10 13 20 13 6 | 57 63 62 60 63 57 59
XR09 | 2481 29 18 15 20 21 --- 11 | 694 686 689 706 701 --- 693
R11 | 4686 15 14 13 15 15 15 6 | 36 40 50 36 45 29 40
R12 | 2112 7 15 12 13 17 26 6 | 59 60 65 68 62 41 58
R13 | 1608 19 47 46 31 19 42 15 | 73 57 97 65 73 52 70
R14 | 4419 13 18 13 19 10 16 6 | 48 52 61 62 52 45 52
R15 | 1132 8 16 10 22 15 13 6 | 51 47 47 47 56 41 47
R16 | 1086 12 21 13 24 23 24 8 | 79 72 65 76 75 73 71
XR17 | 2402 6 18 15 8 30 --- 9 | 27 26 28 34 36 --- 27
R18 | 618 11 17 11 18 15 25 7 | 24 28 23 30 26 30 23
R19 | 2486 36 49 27 60 19 42 17 | 35 45 57 41 36 47 37
R20 | 2830 23 116 31 95 37 68 27 | 60 52 60 72 52 69 57
R21 | 1734 9 24 11 20 18 29 8 | 29 32 36 42 27 27 30
R22 | 2344 13 12 11 26 15 11 6 | 24 31 33 35 28 29 26
R24 | 1610 17 17 11 13 20 22 7 | 48 53 52 49 58 52 50
XR25 | 9671 15 11 --- --- 12 --- 9 | 25 29 --- --- 30 --- 24
XR26 |11898 38 --- --- 30 61 --- 33 | 54 --- --- 57 104 --- 70
------+-----------------------------------------+-------------------------------------
RMS | 2115 18 36 19 32 18 28 |T 80 81 88 88 83 52 80
WRMS | 2115 14 23 12 32 16 28 |NE 80 81 88 88 83 52 80
MEDI | 1610 13 17 13 18 17 22 |MD 57 52 61 60 56 52 57
Table 3.2314.3 GPS week: 2314 Day: 3 MJD: 60445
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 808 35 55 19 36 12 29 14 | 78 40 77 68 63 56 62
R02 | 816 13 20 8 10 26 13 7 | 54 51 63 56 69 52 57
R03 | 849 14 12 12 20 15 9 6 | 63 58 64 72 59 64 61
R04 | 935 17 8 8 24 9 16 6 | 60 53 52 61 49 50 52
R05 | 1167 9 10 14 16 10 10 5 | 52 54 59 51 62 51 54
R07 | 1078 7 12 8 18 8 9 4 | 67 60 68 65 70 66 65
R08 | 958 9 8 14 17 11 14 5 | 66 65 78 67 66 66 67
XR09 | 1802 17 30 27 28 55 --- 17 | 512 507 522 512 547 --- 520
XR11 | 3071 16 20 8 19 16 --- 8 | 33 41 39 31 45 --- 36
R12 | 1437 10 11 16 18 9 24 7 | 53 54 63 50 58 46 53
R13 | 3165 21 51 33 35 27 42 15 | 79 43 82 55 83 49 64
R14 | 2987 15 13 9 9 9 7 4 | 49 57 61 59 58 57 56
R15 | 1434 12 17 19 23 16 19 8 | 46 44 68 65 55 38 50
R16 | 1272 11 28 21 19 18 24 9 | 74 78 82 63 70 60 69
XR17 | 1309 10 7 11 19 15 --- 6 | 23 20 22 28 23 --- 20
R18 | 1099 12 22 13 15 14 15 6 | 19 23 23 23 23 19 18
R19 | 3537 45 40 27 55 25 21 16 | 27 25 37 30 40 34 23
R20 | 2425 39 151 26 81 30 87 27 | 61 58 47 41 44 62 40
R21 | 2125 14 22 19 8 14 15 7 | 27 29 34 31 26 28 27
R22 | 2209 20 17 21 24 14 14 8 | 26 24 40 41 26 23 27
R24 | 1813 19 16 11 18 16 24 8 | 38 22 24 29 38 33 28
XR25 | 8755 14 13 --- --- 11 --- 9 | 21 24 --- --- 26 --- 19
XR26 |11422 43 --- --- 55 66 --- 40 | 40 --- --- 40 110 --- 64
------+-----------------------------------------+-------------------------------------
RMS | 1875 21 43 18 30 17 28 |T 68 65 76 69 74 47 66
WRMS | 1875 16 22 13 27 16 28 |NE 68 65 76 69 74 47 66
MEDI | 1437 14 17 14 19 15 15 |MD 52 44 61 51 58 50 53
Table 3.2314.4 GPS week: 2314 Day: 4 MJD: 60446
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 924 31 66 19 29 23 52 16 | 79 38 70 73 72 32 61
R02 | 810 11 15 15 7 18 13 6 | 87 84 94 88 92 81 87
R03 | 1933 8 10 9 11 10 7 4 | 53 56 63 64 49 56 56
XR04 | 1522 12 16 18 12 9 --- 7 | 92 92 90 87 81 --- 87
R05 | 1363 13 8 17 12 11 11 5 | 51 51 49 60 56 45 51
R07 | 1798 10 25 24 14 11 15 7 | 59 54 84 58 67 59 64
R08 | 1195 7 12 19 12 14 18 6 | 61 57 74 60 55 56 60
XR09 | 5675 97 79 66 265 87 --- 48 | 9999 9999 9999 9999 9999 --- 9999
XR11 | 2122 13 18 17 16 13 --- 7 | 34 31 46 37 41 --- 37
R12 | 607 8 18 11 15 16 22 6 | 47 47 50 47 48 29 44
R13 | 2167 31 49 46 67 24 52 20 | 75 36 87 39 57 59 57
R14 | 1397 7 15 12 14 12 16 5 | 46 56 43 57 53 46 48
R15 | 1394 13 10 9 10 11 17 5 | 50 45 53 51 45 43 47
R16 | 1466 10 28 15 13 11 22 7 | 92 91 91 88 92 89 89
XR17 | 737 5 15 11 8 14 --- 5 | 17 18 17 21 18 --- 15
R18 | 924 9 22 11 20 17 18 7 | 18 21 15 25 20 16 14
R19 | 1220 49 41 19 55 36 55 19 | 41 34 41 38 27 38 31
R20 | 3835 34 117 37 50 35 58 24 | 53 37 50 50 30 49 37
R21 | 1355 5 20 8 14 34 20 8 | 18 20 19 27 28 24 17
R22 | 1888 18 15 12 9 22 22 7 | 22 24 34 26 37 26 26
R24 | 1667 13 22 13 9 19 23 7 | 51 53 53 48 49 58 50
XR25 |10969 13 26 --- --- 21 --- 14 | 21 26 --- --- 32 --- 21
XR26 |10880 33 --- --- 48 79 --- 39 | 38 --- --- 43 95 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1682 20 39 20 27 21 31 |T 50 46 56 51 52 47 47
WRMS | 1682 13 29 14 22 18 30 |NE 50 46 56 51 52 47 47
MEDI | 1466 13 18 15 14 17 20 |MD 50 45 50 50 49 46 48
Table 3.2314.5 GPS week: 2314 Day: 5 MJD: 60447
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1355 37 54 24 40 13 28 15 | 65 30 48 48 45 36 44
R02 | 905 9 12 19 10 8 19 6 | 60 45 59 57 48 46 52
R03 | 1886 8 9 8 11 12 10 4 | 42 46 45 43 42 40 42
R04 | 1737 17 16 13 20 8 12 6 | 93 93 87 91 82 115 89
R05 | 1618 10 15 11 10 19 10 5 | 42 40 34 43 27 37 36
R07 | 2549 11 14 14 10 14 9 5 | 61 50 46 51 55 48 51
R08 | 1503 21 20 20 16 27 24 9 | 48 49 69 47 69 52 55
XR09 | 7982 18 24 16 29 21 --- 10 | 492 492 484 494 493 --- 488
R11 | 1900 16 12 18 18 10 15 7 | 24 28 26 19 28 20 20
R12 | 469 8 22 19 19 9 11 7 | 45 47 30 54 43 41 41
XR13 | 804 36 49 32 53 24 --- 19 | 68 30 56 36 58 --- 46
R14 | 2507 12 18 14 13 11 21 6 | 46 47 60 57 52 34 49
R15 | 1098 10 15 14 13 11 14 5 | 48 44 49 47 38 40 43
R16 | 1004 14 26 10 15 14 26 8 | 88 77 83 85 84 66 81
XR17 | 597 10 10 21 11 16 --- 7 | 20 17 25 23 17 --- 16
R18 | 887 7 14 12 21 15 18 6 | 22 21 25 27 26 23 20
R19 | 994 31 49 18 62 24 62 19 | 41 53 44 48 28 49 37
R20 | 7109 27 141 33 38 42 77 22 | 44 33 45 27 44 53 42
R21 | 762 9 22 12 10 20 26 7 | 21 16 21 25 20 23 18
R22 | 2192 12 16 16 11 33 11 8 | 22 40 32 36 36 31 29
R24 | 1371 12 19 9 9 31 34 9 | 34 44 42 39 48 41 39
XR25 | 9406 17 17 --- --- 30 --- 16 | 11 18 --- --- 32 --- 12
XR26 | 8464 29 --- --- 22 51 --- 25 | 69 --- --- 75 87 --- 74
------+-----------------------------------------+-------------------------------------
RMS | 2267 17 41 17 24 20 30 |T 65 61 67 66 65 44 61
WRMS | 2267 14 22 14 17 16 30 |NE 65 61 67 66 65 44 61
MEDI | 1503 12 17 16 15 16 18 |MD 45 44 45 47 44 40 42
Table 3.2314.6 GPS week: 2314 Day: 6 MJD: 60448
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1256 41 50 16 34 17 35 14 | 102 46 83 76 77 52 74
R02 | 862 12 23 20 13 16 15 7 | 89 71 91 82 82 75 81
R03 | 475 10 18 12 11 24 16 7 | 74 70 79 81 85 65 75
R04 | 1375 14 14 15 24 19 15 7 | 121 118 111 112 106 107 113
R05 | 2056 18 18 14 22 23 14 8 | 71 65 59 63 56 58 61
R07 | 2521 14 26 14 21 21 10 8 | 87 71 89 91 101 85 87
R08 | 1209 15 14 10 15 34 13 8 | 77 73 87 73 101 74 81
XR09 | 7736 18 15 15 14 15 --- 8 | 414 409 408 414 416 --- 412
R11 | 2070 14 16 15 23 17 7 7 | 28 29 35 23 24 19 23
R12 | 638 11 20 19 17 16 13 7 | 66 68 56 65 68 53 60
R13 | 1538 38 56 36 45 30 64 20 | 99 47 95 63 96 53 76
R14 | 3447 15 16 11 18 21 20 7 | 62 69 74 73 77 57 67
R15 | 997 9 13 9 13 10 18 5 | 69 62 71 67 69 54 65
R16 | 760 11 30 21 20 23 22 9 | 88 78 93 76 95 67 82
XR17 | 791 9 21 11 16 13 --- 6 | 25 26 24 24 24 --- 21
R18 | 849 8 17 11 17 9 29 7 | 22 23 23 30 27 20 20
R19 | 1394 28 45 18 67 17 68 19 | 41 38 39 46 41 29 34
R20 | 7148 31 118 56 70 52 73 29 | 59 61 75 72 64 60 54
R21 | 638 8 16 13 10 21 18 6 | 27 23 29 30 34 26 26
R22 | 2672 12 13 16 15 16 17 6 | 28 35 36 34 35 30 31
R24 | 780 8 19 13 13 12 24 6 | 44 51 49 48 56 47 48
XR25 | 9702 18 15 --- --- 18 --- 12 | 22 25 --- --- 30 --- 21
XR26 | 6197 24 --- --- 23 43 --- 22 | 81 --- --- 85 111 --- 88
------+-----------------------------------------+-------------------------------------
RMS | 2282 19 38 21 30 23 32 |T 78 70 81 78 81 54 73
WRMS | 2282 15 29 14 23 21 29 |NE 78 70 81 78 81 54 73
MEDI | 1375 14 18 15 17 18 18 |MD 69 61 74 67 69 54 65
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