[IGSREPORT-29827] Wk 2307 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 15 02:20:03 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2307 (Mar 24, 2024 - Mar 30, 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 2.2307.
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:
igl2307[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2307 in the SP3 format.
igl23077.sum Combination Report for GPS Week 2307.
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 | 6.6 ns
1 | 6.9 ns
2 | 4.4 ns
3 | 4.7 ns
4 | 4.0 ns
5 | 3.9 ns
6 | 4.6 ns
5. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ALL | R26
1 | ALL | R26
2 | ALL | R26
3 | ALL | R26
4 | ALL | R26
5 | ALL | R26
6 | ALL | R26
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 1.2307, 1a.2307).
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 2.2307.0-6)
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 3.2307.0-6).
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 2307 summary. (Mar 24, 2024 - Mar 30, 2024)
Table 1.2307.a GPS week : 2307 MJD: 60393.0-60399.0
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 0 -2 -17 45 .11 24 17 | 4123 736 3634 8272
| 0 1 1 19 24 40 .04 | 1780 1756
esa n/a| 0 -1 2 -18 -4 -26 .01 27 19 | 5757 537 3633 8361
| 1 1 0 16 17 34 .05 | 5324 1743
gfz n/a| 1 0 -6 13 8 -18 -.06 30 17 | 0 677 3621 7876
| 1 1 1 19 13 30 .06 | 0 2055
grg n/a| 1 0 3 -9 1 29 .27 23 18 | 4205 590 3644 7578
| 1 0 2 21 20 36 .05 | 1687 2006
iac n/a| -1 0 -2 0 0 13 -.13 19 17 | 6525 -292 3627 8308
| 0 1 2 7 37 78 .11 | 1307 865
jgx n/a| 0 0 1 37 23 -73 -.11 29 27 | 6802 797 3670 8106
| 1 1 2 7 14 50 .07 | 1792 1865
Table 1.2307.b GPS week : 2307 MJD: 60393.0-60399.0
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 | 10 10 12 14 13 13 12 |
R02 | 5 6 7 6 7 6 6 |
R03 | 9 5 6 6 7 7 7 |
R04 | 8 5 6 5 6 7 7 |
R05 | 5 5 7 6 7 6 7 |
R07 | 7 6 7 5 7 6 7 |
R08 | 9 7 6 6 7 7 9 |
R09 | 7 7 8 7 7 7 9 |
R11 | 8 7 6 7 8 6 6 |
R12 | 7 9 7 9 7 9 7 |
R13 | 14 14 12 13 14 16 17 |
R14 | 8 8 7 8 7 7 8 |
R15 | 8 8 8 6 8 8 9 |
R16 | 10 9 9 9 9 9 10 |
R17 | 8 9 10 7 10 9 10 |
R18 | 6 6 7 8 9 9 9 |
R19 | 19 19 22 21 21 19 22 |
R20 | 30 32 25 30 28 32 33 |
R21 | 9 8 9 7 8 9 10 |
R22 | 9 7 6 7 10 7 10 |
R24 | 7 10 8 10 10 10 11 |
R25 | 9 11 9 9 13 11 14 |
Table 1.2307.c GPS week : 2307 MJD: 60393.0-60399.0
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 2307 0 | 44 20 -64 -3119 648 8490 79.5 1723 1723 | 6557 0
brd 2307 1 | 108 22 86 -3704 1953 -877 81.1 1551 1551 | 6928 0
brd 2307 2 | 70 5 124 -632 2033 2193 79.7 1642 1642 | 4417 0
brd 2307 3 | 63 79 0 533 2202 2743 80.2 1987 1987 | 4720 0
brd 2307 4 | -13 -44 54 911 75 5058 82.2 1698 1698 | 3981 0
brd 2307 5 | -87 72 132 450 -1633 6652 82.4 1812 1812 | 3866 0
brd 2307 6 | -45 -54 32 858 -1885 9737 82.0 1943 1943 | 4600 0
-------------+------------------------------------------------------------+----------------
brd 2307 mean| 19 14 52 -671 484 4856 81.0 1765 1765 | 5009 0
brd 2307 sdev| 70 51 70 1947 1722 3757 1.2 158 158 | 1227 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 2.2307.0 GPS week: 2307 Day: 0 MJD: 60393
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 -24 2 39 .10 21 17 | 2457 -1786 3622 8127
esa n/a| 1 -2 1 7 5 -71 .03 25 19 | 11078 -1727 3613 9848
gfz n/a| 1 -1 -8 54 -7 -52 -.08 37 21 | 0 -2787 3441 8254
grg n/a| 0 0 6 -32 2 88 .19 18 17 | 6849 -2776 3468 8194
iac n/a| -2 0 -4 0 -4 -33 -.17 19 17 | 7910 -1027 3603 8319
jgx n/a| 0 -1 -1 33 9 5 -.14 34 33 | 4676 -1909 3218 8432
Table 2.2307.1 GPS week: 2307 Day: 1 MJD: 60394
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 16 -41 34 .05 22 18 | 2084 1156 3808 7370
esa n/a| 1 -1 3 -22 -40 -40 .03 28 18 | -2166 1578 3815 7588
gfz n/a| 1 1 -5 17 17 -32 .06 32 15 | 0 1048 3811 7417
grg n/a| 1 -1 4 -22 -6 45 .24 21 17 | 6112 1272 3839 7251
iac n/a| -2 0 -2 -7 15 5 -.19 16 16 | 8668 -1065 3811 7464
jgx n/a| 0 1 0 46 16 -29 -.03 28 28 | 5265 1083 3964 7606
Table 2.2307.2 GPS week: 2307 Day: 2 MJD: 60395
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 0 17 7 -3 .10 25 17 | 2150 3707 3065 7292
esa n/a| 0 0 2 -16 7 -25 -.02 22 13 | 6944 3513 3057 6819
gfz n/a| 4 0 -6 10 2 -15 -.04 30 15 | 0 3813 3096 6569
grg n/a| 0 0 1 -30 13 34 .27 23 19 | 2206 3712 3093 6193
iac n/a| 0 -1 -1 0 -3 52 -.11 16 14 | 5872 1019 3049 7157
jgx n/a| -3 0 -1 41 23 -87 -.10 25 21 | 4843 3787 3189 6950
Table 2.2307.3 GPS week: 2307 Day: 3 MJD: 60396
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 -10 -27 72 .12 20 14 | 5260 848 3126 8167
esa n/a| -1 0 2 -11 9 14 .02 29 20 | 5056 646 3133 7401
gfz n/a| 0 1 -7 1 22 20 -.12 31 17 | 0 763 3172 7670
grg n/a| 1 1 2 6 32 21 .30 27 19 | 4093 615 3166 7493
iac n/a| 0 -2 0 5 -6 -62 -.16 19 16 | 6585 -12 3137 8281
jgx n/a| 0 0 3 33 8 -121 -.07 26 21 | 7656 1134 3197 7842
Table 2.2307.4 GPS week: 2307 Day: 4 MJD: 60397
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 -19 -36 111 .18 26 17 | 5542 -638 3186 8983
esa n/a| 0 -3 1 -10 -7 6 .08 27 18 | 9886 -963 3172 8741
gfz n/a| 0 0 -4 7 -6 -9 -.06 24 19 | 0 -333 3188 8392
grg n/a| 2 -1 6 22 -34 -17 .32 25 20 | 3910 -432 3209 7767
iac n/a| -1 0 -4 -5 58 -47 -.21 20 16 | 6088 -1095 3182 9054
jgx n/a| 0 1 1 44 21 -67 -.13 29 25 | 7986 -577 3237 8641
Table 2.2307.5 GPS week: 2307 Day: 5 MJD: 60398
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 -2 -16 -39 64 .14 27 18 | 5667 166 4017 8907
esa n/a| -1 -2 1 -40 -6 -3 .03 29 20 | -634 -291 4017 9272
gfz n/a| 0 0 -5 8 23 12 -.05 26 19 | 0 126 3990 8188
grg n/a| 2 0 3 -17 1 -11 .31 21 17 | 2939 33 4057 7653
iac n/a| -1 0 -4 13 2 14 -.22 20 17 | 5209 -509 3974 8765
jgx n/a| -1 1 4 26 33 -74 -.06 28 29 | 8574 -68 4097 8337
Table 2.2307.6 GPS week: 2307 Day: 6 MJD: 60399
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 17 14 1 .07 26 19 | 5704 1699 4618 9062
esa n/a| 0 -1 3 -35 1 -68 -.10 32 25 | 10141 1009 4629 8860
gfz n/a| 2 -2 -8 -5 10 -56 -.12 27 17 | 0 2110 4654 8642
grg n/a| 0 -1 0 7 -2 45 .24 24 19 | 3328 1709 4677 8500
iac n/a| -1 2 1 -3 -68 166 .11 24 22 | 5347 639 4633 9119
jgx n/a| 0 -2 3 36 50 -143 -.23 31 31 | 8618 2132 4788 8936
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 3.2307.0 GPS week: 2307 Day: 0 MJD: 60393
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1608 24 16 19 21 13 32 9 | 87 72 75 79 77 91 78
R02 | 925 9 10 13 11 7 18 5 | 104 101 101 106 96 103 101
R03 | 1438 10 15 27 16 20 29 8 | 73 75 79 80 78 68 74
R04 | 2047 15 11 13 20 20 15 7 | 77 75 71 74 64 65 70
R05 | 703 9 9 14 8 9 10 4 | 72 77 64 70 76 64 71
R07 | 1181 9 20 24 18 12 14 7 | 73 69 64 75 74 72 70
R08 | 796 16 26 20 9 23 22 9 | 69 70 79 72 79 70 72
R09 | 2137 22 10 15 18 16 11 7 | 31 32 34 33 34 25 28
R11 | 1845 16 14 15 16 22 15 7 | 85 88 87 77 92 81 84
R12 | 696 7 16 24 18 12 17 7 | 74 82 83 62 65 71 70
R13 | 1317 36 36 49 21 15 33 14 | 84 39 88 58 52 51 58
R14 | 2150 9 27 9 10 20 18 7 | 85 85 74 79 74 80 78
R15 | 2846 21 23 22 14 10 19 8 | 66 65 58 54 49 54 55
R16 | 1026 28 22 25 23 12 18 9 | 71 71 61 63 59 56 60
XR17 | 1362 16 20 17 16 10 --- 8 | 101 87 101 85 95 --- 93
R18 | 622 10 15 16 13 11 17 6 | 91 102 98 95 97 88 95
R19 | 3607 25 33 66 32 34 70 19 | 114 91 145 105 109 104 107
R20 | 2231 49 71 117 27 38 102 29 | 98 47 129 62 59 77 61
R21 | 825 22 15 21 20 13 22 8 | 104 83 107 85 86 74 88
XR22 | 1029 16 12 25 23 15 --- 9 | 38 47 47 49 49 --- 43
R24 | 1052 12 11 16 12 12 26 6 | 85 77 98 78 86 67 81
XR25 | 8295 13 9 --- --- 13 --- 8 | 49 53 --- --- 52 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 1722 21 25 37 18 19 34 |T 78 72 83 73 72 71 72
WRMS | 1722 17 19 21 17 17 33 |NE 78 72 83 73 72 71 72
MEDI | 1317 16 15 20 18 13 18 |MD 77 75 79 75 74 71 71
Table 3.2307.1 GPS week: 2307 Day: 1 MJD: 60394
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1524 29 17 14 22 22 23 10 | 51 48 49 41 50 55 47
R02 | 1195 12 14 12 14 13 10 5 | 76 81 83 81 69 83 78
R03 | 2197 8 11 20 11 10 8 5 | 40 49 63 43 40 53 46
R04 | 872 17 5 9 8 12 14 5 | 49 51 56 45 43 45 47
R05 | 875 10 11 10 8 12 15 5 | 51 56 54 51 57 49 53
R07 | 967 11 19 14 17 11 7 6 | 39 43 42 46 41 37 40
R08 | 794 17 10 13 17 14 23 7 | 45 45 44 37 44 48 43
R09 | 2406 15 18 19 14 12 10 6 | 28 34 35 33 27 34 28
R11 | 1369 11 27 11 18 14 11 7 | 85 95 80 76 79 80 81
R12 | 1196 12 20 12 36 13 13 9 | 56 69 62 44 63 53 55
XR13 | 1128 31 28 33 21 21 --- 13 | 55 34 62 44 30 --- 41
R14 | 1727 11 31 15 17 16 10 8 | 79 79 68 75 71 73 72
R15 | 2540 21 16 16 9 15 22 7 | 51 45 49 47 38 38 42
R16 | 895 26 25 16 14 16 21 9 | 55 59 41 51 43 39 45
XR17 | 2221 12 21 14 24 14 --- 9 | 54 49 52 45 53 --- 48
R18 | 662 9 13 10 14 15 11 5 | 56 56 57 60 60 59 57
R19 | 2789 36 37 67 45 22 44 19 | 86 70 97 80 74 75 75
R20 | 1592 58 91 105 37 32 89 31 | 57 83 104 57 49 67 55
R21 | 1384 22 15 21 10 14 21 8 | 63 52 59 54 44 48 52
R22 | 1197 13 10 14 20 13 13 6 | 30 37 36 40 36 44 34
R24 | 760 18 12 32 22 20 30 10 | 53 49 66 53 60 34 50
XR25 |15857 18 11 --- --- 16 --- 11 | 43 38 --- --- 35 --- 36
------+-----------------------------------------+-------------------------------------
RMS | 1550 22 28 32 21 16 28 |T 54 55 59 52 50 53 51
WRMS | 1550 18 17 15 17 16 28 |NE 54 55 59 52 50 53 51
MEDI | 1197 15 16 14 17 14 14 |MD 53 49 57 47 44 49 47
Table 3.2307.2 GPS week: 2307 Day: 2 MJD: 60395
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1513 48 24 24 25 17 16 12 | 60 50 44 51 48 48 48
R02 | 905 12 11 14 14 15 20 6 | 95 95 96 92 86 85 90
R03 | 3377 15 12 11 19 9 17 6 | 49 58 49 56 51 43 50
R04 | 642 13 10 18 7 13 16 6 | 48 44 49 43 47 38 44
R05 | 1018 12 11 24 10 18 12 7 | 50 47 37 44 53 39 45
R07 | 2099 13 12 20 23 8 19 7 | 51 47 48 53 46 42 46
R08 | 1193 11 14 15 12 9 11 5 | 47 53 51 44 47 52 48
R09 | 2954 13 13 22 24 14 19 8 | 26 29 37 27 28 33 25
R11 | 1349 11 8 11 17 9 17 5 | 66 61 77 75 65 70 68
R12 | 954 12 21 14 20 11 14 7 | 69 75 63 58 61 56 63
XR13 | 1584 24 28 32 18 12 --- 11 | 58 39 66 44 45 --- 47
R14 | 1358 7 21 13 21 10 10 6 | 89 96 86 80 91 85 88
R15 | 1766 21 15 16 19 13 15 7 | 52 43 52 50 35 39 42
R16 | 984 30 24 19 13 12 22 9 | 62 58 52 51 45 52 50
XR17 | 1993 12 19 15 29 20 --- 10 | 76 70 66 72 85 --- 73
R18 | 760 6 17 17 20 15 14 7 | 73 71 69 67 73 64 69
R19 | 2350 41 24 88 48 30 56 21 | 125 124 147 121 123 118 122
R20 | 1098 66 72 64 43 32 57 25 | 61 79 89 54 38 44 45
R21 | 1373 23 12 23 15 12 31 8 | 80 72 88 80 67 63 73
R22 | 1576 12 8 13 21 9 16 6 | 36 41 49 53 41 36 40
R24 | 596 12 11 22 21 18 24 8 | 66 59 73 59 74 52 63
XR25 |14445 18 9 --- --- 12 --- 9 | 39 51 --- --- 50 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1642 25 22 30 23 16 25 |T 62 61 66 60 59 55 58
WRMS | 1642 17 13 15 19 14 21 |NE 62 61 66 60 59 55 58
MEDI | 1358 13 13 18 20 12 17 |MD 60 58 63 54 50 52 48
Table 3.2307.3 GPS week: 2307 Day: 3 MJD: 60396
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2408 40 25 25 28 15 40 13 | 68 53 47 58 53 67 54
R02 | 782 13 16 19 12 9 14 6 | 57 42 44 50 49 52 48
R03 | 2483 10 14 10 18 12 13 5 | 58 65 60 69 58 61 60
R04 | 1134 6 10 15 11 13 13 5 | 56 55 56 54 57 54 54
R05 | 1144 9 13 16 14 15 8 5 | 43 49 57 45 57 49 49
R07 | 2786 8 13 7 8 11 14 4 | 54 63 55 60 63 50 57
R08 | 1359 10 7 22 16 10 16 6 | 53 50 54 54 51 49 50
R09 | 2292 11 11 14 22 16 13 6 | 31 33 36 36 29 34 30
R11 | 1202 10 17 18 21 15 19 7 | 46 43 49 62 46 47 46
R12 | 818 14 22 17 40 12 14 9 | 76 84 83 59 64 68 70
R13 | 773 23 32 32 19 29 37 13 | 67 63 70 63 45 29 53
R14 | 1117 9 28 10 19 17 11 7 | 85 94 86 80 75 84 82
R15 | 1601 9 16 14 16 14 17 6 | 46 47 50 55 39 33 43
R16 | 930 14 25 19 20 11 26 8 | 55 36 59 54 54 36 47
XR17 | 1092 12 12 13 25 9 --- 7 | 78 69 74 65 72 --- 72
R18 | 1139 8 23 14 27 7 25 8 | 71 82 68 75 69 65 70
R19 | 5254 45 29 71 52 30 46 20 | 83 77 128 90 79 92 87
R20 | 2921 41 100 90 54 45 63 29 | 82 64 101 77 40 58 53
R21 | 1000 15 15 21 15 13 20 7 | 83 71 82 86 71 64 75
R22 | 1688 15 13 16 16 15 11 6 | 60 56 70 64 66 56 62
R24 | 466 8 14 15 41 28 18 10 | 72 67 81 50 89 65 70
XR25 |10914 12 10 --- --- 13 --- 9 | 43 42 --- --- 35 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1986 20 29 31 27 19 26 |T 62 59 67 62 57 55 57
WRMS | 1986 14 20 17 19 16 21 |NE 62 59 67 62 57 55 57
MEDI | 1144 11 15 16 19 13 16 |MD 58 56 60 60 57 54 54
Table 3.2307.4 GPS week: 2307 Day: 4 MJD: 60397
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1805 32 26 24 40 15 38 13 | 59 54 50 65 57 57 54
R02 | 807 16 13 11 10 7 28 6 | 101 97 96 97 95 101 97
R03 | 1408 10 17 14 14 10 19 6 | 50 47 54 52 48 56 49
R04 | 1087 13 8 15 10 14 10 5 | 51 46 50 48 43 49 46
R05 | 1809 17 8 13 14 19 15 6 | 50 53 52 49 57 49 51
R07 | 994 10 16 16 20 14 17 7 | 55 53 54 63 55 44 53
R08 | 773 11 10 15 20 17 19 7 | 55 57 54 68 60 53 57
R09 | 2680 15 14 21 15 12 13 6 | 54 55 43 47 53 44 49
R11 | 1624 18 20 19 11 21 19 8 | 84 88 87 78 86 90 84
R12 | 766 12 19 14 18 12 13 6 | 64 71 59 67 59 52 60
R13 | 956 41 32 26 34 12 32 13 | 65 38 52 51 45 43 45
R14 | 856 10 24 10 17 12 19 7 | 94 106 100 106 97 95 98
R15 | 2031 21 15 7 21 19 17 8 | 48 47 39 36 42 34 38
R16 | 1514 14 23 27 19 9 26 9 | 74 64 77 72 71 58 67
XR17 | 639 11 17 27 27 13 --- 10 | 75 64 86 57 67 --- 69
R18 | 1100 10 22 12 27 15 25 8 | 63 73 66 59 59 56 61
R19 | 4373 60 43 52 60 23 32 20 | 76 67 87 65 81 68 69
R20 | 1263 62 81 52 18 58 80 27 | 89 74 87 71 64 88 69
R21 | 835 13 24 19 16 13 23 8 | 86 71 93 84 87 77 83
R22 | 1992 22 10 28 37 13 20 10 | 52 46 63 45 42 46 44
R24 | 779 17 14 23 29 20 27 10 | 80 63 77 53 76 55 67
XR25 |11070 25 12 --- --- 15 --- 12 | 47 42 --- --- 52 --- 45
------+-----------------------------------------+-------------------------------------
RMS | 1697 26 27 24 25 20 29 |T 66 62 67 63 63 60 61
WRMS | 1697 17 18 19 20 16 25 |NE 66 62 67 63 63 60 61
MEDI | 1100 15 17 19 19 14 19 |MD 63 57 63 63 59 55 57
Table 3.2307.5 GPS week: 2307 Day: 5 MJD: 60398
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 831 30 35 24 41 14 19 13 | 47 42 37 60 34 47 42
R02 | 640 8 11 17 11 14 16 6 | 75 82 82 73 74 78 76
R03 | 835 12 16 14 11 21 13 6 | 39 36 43 37 32 33 35
R04 | 438 17 13 17 14 13 16 6 | 38 45 44 33 40 39 37
R05 | 1908 15 13 10 12 9 12 5 | 39 41 31 29 35 28 32
R07 | 718 6 12 18 6 13 19 6 | 50 46 54 45 49 40 46
R08 | 2421 15 14 17 11 20 17 7 | 44 44 52 43 49 43 44
R09 | 3776 18 11 14 13 14 14 6 | 43 48 49 44 49 44 44
R11 | 2071 13 9 11 15 16 15 6 | 26 29 29 31 25 28 26
R12 | 1194 12 27 11 13 25 24 8 | 73 83 74 70 67 73 70
XR13 | 2693 27 32 40 31 25 --- 15 | 81 84 97 77 78 --- 80
R14 | 989 17 13 17 16 11 22 7 | 56 62 72 67 67 60 63
R15 | 2075 20 14 14 13 15 22 7 | 50 42 49 43 38 38 40
R16 | 2114 21 24 15 13 19 27 9 | 60 72 70 59 53 61 59
XR17 | 1931 13 19 15 20 15 --- 8 | 67 55 62 58 60 --- 59
R18 | 699 12 28 14 26 16 22 9 | 51 67 42 44 49 43 47
R19 | 2909 49 38 48 40 28 49 18 | 89 83 90 92 77 80 81
R20 | 1682 85 91 79 44 46 74 31 | 101 44 80 38 68 62 53
R21 | 1347 14 21 28 11 10 30 9 | 69 62 83 70 66 54 67
R22 | 2541 17 17 8 18 17 15 7 | 37 33 41 44 43 41 38
R24 | 737 19 17 26 17 20 29 9 | 66 54 67 55 54 44 54
XR25 |11087 18 15 --- --- 14 --- 11 | 36 45 --- --- 40 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1811 27 29 26 21 20 28 |T 56 54 59 52 52 49 51
WRMS | 1811 18 20 19 17 17 29 |NE 56 54 59 52 52 49 51
MEDI | 1682 17 16 17 14 15 19 |MD 50 46 54 45 49 44 46
Table 3.2307.6 GPS week: 2307 Day: 6 MJD: 60399
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1755 25 26 29 34 12 23 11 | 85 76 64 82 78 79 76
R02 | 709 7 8 9 10 16 25 6 | 108 102 106 105 109 99 104
R03 | 2140 9 16 19 17 13 12 6 | 73 68 62 75 73 69 69
R04 | 996 9 13 13 18 14 24 7 | 73 70 70 73 73 59 69
R05 | 1894 11 13 17 10 17 15 6 | 66 64 62 61 69 57 63
R07 | 1252 13 12 15 15 16 13 6 | 74 76 67 78 83 73 74
R08 | 1457 12 13 22 26 20 17 8 | 69 79 79 68 81 74 74
R09 | 4475 23 17 17 18 29 12 9 | 46 48 48 33 38 39 38
R11 | 1807 13 11 13 15 14 16 6 | 65 67 76 70 68 72 69
R12 | 1135 13 18 14 12 18 21 7 | 79 91 79 80 88 76 81
R13 | 2694 39 36 31 29 32 60 17 | 99 87 95 83 101 55 84
R14 | 1065 29 19 11 18 15 13 8 | 78 77 68 65 60 60 66
R15 | 1722 28 15 17 25 16 20 9 | 81 73 79 63 61 69 68
R16 | 1382 20 25 14 26 17 25 9 | 93 93 91 91 74 83 85
XR17 | 1365 15 25 20 15 22 --- 10 | 105 80 104 87 98 --- 94
R18 | 889 13 15 9 18 24 31 8 | 92 100 94 86 98 79 91
R19 | 1248 26 47 37 54 34 82 21 | 122 106 136 109 125 122 116
R20 | 2265 79 108 85 33 50 50 32 | 129 98 133 68 68 80 80
R21 | 1723 21 18 16 20 25 27 9 | 114 94 114 104 105 87 102
R22 | 3226 20 14 19 28 30 18 10 | 54 56 54 52 67 51 54
R24 | 596 22 25 33 15 21 18 10 | 94 74 110 89 90 76 88
XR25 |14587 19 14 --- --- 23 --- 14 | 67 72 --- --- 76 --- 70
------+-----------------------------------------+-------------------------------------
RMS | 1943 26 32 27 24 24 31 |T 84 79 85 77 81 72 77
WRMS | 1943 19 25 17 19 22 31 |NE 84 79 85 77 81 72 77
MEDI | 1457 19 16 17 18 18 20 |MD 79 76 79 78 76 73 74
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