[IGSREPORT-29849] Wk 2309 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 29 02:59:59 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2309 (Apr 07, 2024 - Apr 13, 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 2.2309.
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:
igl2309[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2309 in the SP3 format.
igl23097.sum Combination Report for GPS Week 2309.
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 | 3.2 ns
1 | 0.9 ns
2 | 2.6 ns
3 | 3.0 ns
4 | 3.8 ns
5 | -1.8 ns
6 | 2.5 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
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 1.2309, 1a.2309).
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 2.2309.0-6)
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 3.2309.0-6).
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 2309 summary. (Apr 07, 2024 - Apr 13, 2024)
Table 1.2309.a GPS week : 2309 MJD: 60407.0-60413.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 3 -3 -25 65 .13 23 19 | 11489 -32 4618 29432
| 0 0 1 22 17 28 .03 | 5337 1297
esa n/a| 0 -1 5 -27 4 -5 .02 37 22 | 36 625 3262 7579
| 1 1 1 16 12 39 .07 | 4163 1488
gfz n/a| 1 0 -3 9 -10 -16 .03 23 17 | 0 -342 3281 7266
| 1 0 1 15 6 36 .05 | 0 1392
grg n/a| 2 0 3 -4 -11 60 .24 28 21 | 7149 -169 4543 29041
| 1 1 3 27 14 23 .09 | 5973 1317
iac n/a| -2 0 -7 3 -1 14 -.20 21 18 | 9228 -47 4636 30802
| 1 1 2 20 15 77 .07 | 5267 1477
jgx n/a| 0 0 -1 27 54 -102 -.17 28 27 | 8725 -135 3349 7550
| 1 1 3 12 17 59 .06 | 1185 1665
Table 1.2309.b GPS week : 2309 MJD: 60407.0-60413.0
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 11 12 12 14 13 14 |
R02 | 6 5 8 6 6 8 6 |
R03 | 7 6 6 7 6 6 8 |
R04 | 8 9 6 7 7 5 7 |
R05 | 7 8 6 7 8 7 8 |
R07 | 7 7 7 8 8 6 5 |
R08 | 8 6 6 7 8 6 5 |
R09 | 7 10 8 8 7 6 7 |
R11 | 7 6 8 9 6 5 6 |
R12 | 7 7 9 12 12 8 7 |
R13 | 16 16 21 19 12 14 15 |
R14 | 7 10 14 9 8 7 7 |
R15 | 7 13 11 13 8 9 9 |
R16 | 9 10 11 12 11 9 9 |
R17 | 11 8 9 7 7 7 7 |
R18 | 7 7 7 7 9 9 8 |
R19 | 21 25 19 17 18 18 18 |
R20 | 20 29 33 25 31 29 32 |
R21 | 9 9 9 10 8 8 8 |
R22 | 8 7 8 7 9 9 9 |
R24 | 8 8 7 10 9 8 9 |
R25 | 15 12 12 11 15 10 10 |
R26 | 23 26 27 22 32 36 30 |
Table 1.2309.c GPS week : 2309 MJD: 60407.0-60413.0
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 2309 0 | 66 24 70 235 1773 8299 80.7 2248 2248 | 3190 0
brd 2309 1 | -81 59 65 -530 1719 185 80.3 1990 1990 | 875 0
brd 2309 2 | 54 8 220 -151 800 3556 79.2 1643 1643 | 2579 0
brd 2309 3 | -77 7 169 -272 -1027 3930 81.5 1662 1662 | 2996 0
brd 2309 4 | 0 34 179 434 -1169 1983 82.7 1682 1682 | 3750 0
brd 2309 5 | 54 41 77 858 5 2761 79.1 1757 1757 | -1800 0
brd 2309 6 | -41 89 111 1594 -452 5744 79.7 1978 1978 | 2511 0
-------------+------------------------------------------------------------+----------------
brd 2309 mean| -3 37 127 309 235 3779 80.4 1851 1851 | 2014 0
brd 2309 sdev| 64 29 61 733 1223 2631 1.3 227 227 | 1904 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 2.2309.0 GPS week: 2309 Day: 0 MJD: 60407
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 1 2 21 .17 20 16 | 10554 -935 3707 21190
esa n/a| 0 -1 3 -36 -17 -82 .11 39 26 | 5096 -919 3265 8811
gfz n/a| 0 1 -2 8 -13 -73 -.05 20 15 | 0 -306 3279 7856
grg n/a| 0 1 4 -15 3 57 .18 26 21 | 6989 -604 3704 20934
iac n/a| -1 0 -9 12 -13 166 -.28 23 21 | 9478 -1207 3778 22850
jgx n/a| -1 0 0 38 45 -43 -.07 25 25 | 9176 -177 3324 8098
Table 2.2309.1 GPS week: 2309 Day: 1 MJD: 60408
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 4 -21 -17 80 .14 20 17 | 7935 1776 3809 19623
esa n/a| 1 -3 7 -9 7 -9 .06 37 21 | 4655 2125 3321 8321
gfz n/a| 0 0 -4 -4 0 0 .11 24 18 | 0 1342 3289 7106
grg n/a| 1 0 -1 7 -27 88 .21 27 21 | 3728 991 3798 19584
iac n/a| -3 2 -7 9 9 -64 -.26 23 19 | 6486 481 3883 21255
jgx n/a| 0 -1 0 27 41 -69 -.14 31 31 | 7138 2204 3385 7375
Table 2.2309.2 GPS week: 2309 Day: 2 MJD: 60409
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 5 -1 -16 44 .17 21 16 | 11301 -525 3539 18887
esa n/a| 2 -1 4 -23 -3 -28 .02 38 20 | 865 772 3185 7175
gfz n/a| 3 0 -3 21 -2 -6 .05 21 19 | 0 -961 3226 7198
grg n/a| 1 0 0 2 -26 76 .14 40 22 | 6199 -675 3604 18789
iac n/a| -4 0 -4 -26 20 56 -.18 23 20 | 8576 -590 3617 20541
jgx n/a| 0 0 -2 0 24 -170 -.16 29 29 | 10902 -1495 3207 7499
Table 2.2309.3 GPS week: 2309 Day: 3 MJD: 60410
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 1 28 -36 108 .09 24 17 | 10442 -857 3401 19095
esa n/a| 1 0 5 -43 1 2 .04 40 18 | -2470 -532 3050 6081
gfz n/a| 0 0 0 21 -14 18 -.02 22 17 | 0 -707 3112 6309
grg n/a| 5 -2 7 -60 -14 58 .17 34 21 | 6873 -955 3444 19111
iac n/a| -1 2 -9 40 8 -17 -.07 18 17 | 8340 -242 3445 20862
jgx n/a| -1 0 -8 34 66 -162 -.18 30 30 | 8817 0 3198 6609
Table 2.2309.4 GPS week: 2309 Day: 4 MJD: 60411
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 4 -41 -52 83 .11 28 24 | 10480 997 3421 17642
esa n/a| 0 -2 5 -12 9 34 -.01 32 20 | 507 3095 3081 6907
gfz n/a| 1 0 -5 31 -15 -5 .03 27 15 | 0 1716 3113 6127
grg n/a| 2 0 4 0 -7 83 .36 23 20 | 6104 1164 3421 17468
iac n/a| -1 0 -2 0 0 -19 -.18 19 18 | 9017 -1026 3479 19365
jgx n/a| 0 0 -1 29 69 -138 -.26 26 25 | 8904 1893 3140 6309
Table 2.2309.5 GPS week: 2309 Day: 5 MJD: 60412
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 3 7 -26 66 .10 23 20 | 6717 -1727 3575 14531
esa n/a| 0 0 6 -18 9 15 -.00 39 22 | -6847 -392 3322 8303
gfz n/a| 2 0 -2 -11 -17 -63 .05 24 21 | 0 -2005 3311 8675
grg n/a| 1 0 4 20 11 35 .27 22 18 | 509 -2274 3466 11293
iac n/a| -4 0 -7 -7 -15 13 -.19 18 15 | 2733 -803 3540 13210
jgx n/a| 0 1 -2 28 71 -116 -.20 29 25 | 7880 -2114 3381 9083
Table 2.2309.6 GPS week: 2309 Day: 6 MJD: 60413
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 4 0 -31 54 .15 24 22 | 22999 1047 10877 95062
esa n/a| 0 -2 5 -51 22 25 -.12 34 24 | -1553 228 3613 7459
gfz n/a| 1 0 -3 1 -7 11 .04 25 15 | 0 -1474 3643 7594
grg n/a| 2 4 8 14 -17 25 .36 28 22 | 19646 1170 10370 96108
iac n/a| -1 0 -9 -5 -21 -34 -.23 20 15 | 19972 3053 10711 97537
jgx n/a| -1 2 0 33 61 -16 -.17 26 27 | 8264 -1261 3810 7877
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 3.2309.0 GPS week: 2309 Day: 0 MJD: 60407
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1061 32 22 21 47 20 21 12 | 98 96 96 84 80 82 89
R02 | 2493 11 13 12 13 16 10 5 | 34 30 28 30 32 30 28
R03 | 2514 8 19 14 14 21 7 6 | 33 38 36 32 36 32 32
R04 | 1336 21 19 19 22 13 10 8 | 30 41 38 29 29 31 29
R05 | 749 9 15 12 12 27 8 6 | 33 37 29 31 37 31 29
R07 | 906 12 8 18 17 21 7 6 | 24 34 38 26 24 28 25
R08M | 2991 12 6 22 22 16 19 7 | 20 23 32 21 21 21 18
R09E | 3558 15 16 15 18 14 8 6 | 71 79 77 79 73 79 75
R11E | 3662 14 16 11 15 20 9 6 | 39 38 45 41 43 42 39
R12E | 1022 7 15 18 17 13 15 6 | 127 123 123 130 131 129 126
R13E | 764 38 33 39 24 32 42 16 | 127 132 129 130 124 92 124
R14E | 2906 7 19 11 22 20 9 6 | 51 53 52 58 54 52 50
R15E | 1007 13 11 11 21 16 21 7 | 185 181 178 175 181 208 179
R16E | 1199 18 18 13 24 19 26 9 | 101 105 103 104 99 90 99
XR17 | 587 11 25 33 10 21 --- 11 | 58 48 80 63 61 --- 61
R18 | 531 8 15 16 19 19 19 7 | 48 58 59 50 56 42 51
R19M | 2263 29 42 34 65 57 57 21 | 68 71 74 63 76 62 62
R20M | 3397 44 152 32 29 30 52 19 | 104 98 104 91 79 47 77
R21 | 986 23 14 10 19 21 28 9 | 64 45 64 58 66 47 55
R22 | 4298 17 17 15 18 20 11 7 | 36 34 35 34 33 34 31
R24M | 516 12 23 19 17 15 21 8 | 55 49 65 56 54 43 52
XR25 |16137 24 15 --- --- 23 --- 15 | 29 27 --- --- 41 --- 27
XR26 |14672 21 --- --- 29 44 --- 22 | 21 --- --- 21 26 --- 20
------+-----------------------------------------+-------------------------------------
RMS | 2247 20 39 20 26 23 25 |T 63 65 70 63 63 61 59
WRMS | 2247 16 26 15 21 21 25 |NE 37 39 45 37 40 34 35
MEDI | 1336 14 16 16 19 20 15 |MD 51 48 64 56 54 43 51
Table 3.2309.1 GPS week: 2309 Day: 1 MJD: 60408
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 2374 18 22 22 39 11 30 10 | 63 60 67 57 58 44 57
R02 | 961 5 15 7 13 8 10 4 | 18 19 16 18 15 16 13
R03 | 3020 12 17 13 14 14 9 6 | 20 22 19 19 20 23 16
R04 | 622 26 15 19 9 20 13 8 | 19 22 34 27 30 21 21
R05 | 1380 26 18 14 13 18 15 8 | 21 33 26 31 29 27 22
R07 | 961 10 16 13 21 17 11 6 | 18 25 23 15 20 23 16
R08M | 2523 12 9 14 12 14 18 6 | 17 19 22 17 17 19 14
R09E | 3085 14 23 17 46 8 12 9 | 117 121 121 116 118 115 117
R11E | 2667 11 7 13 12 17 16 6 | 30 32 31 33 34 34 30
R12E | 683 11 13 18 19 11 16 6 | 130 130 137 137 132 133 132
R13E | 750 25 38 43 36 20 52 16 | 129 120 127 136 136 95 125
R14E | 2248 12 24 20 39 16 21 10 | 79 73 86 103 73 91 81
XR15E | 561 23 18 20 31 33 --- 13 | 180 176 166 181 177 --- 174
R16E | 1569 23 22 22 30 12 21 9 | 79 79 74 82 69 70 72
XR17 | 739 10 24 16 9 13 --- 7 | 34 31 44 46 46 --- 39
R18 | 693 12 13 10 13 20 16 6 | 37 40 39 49 47 38 40
R19M | 717 30 53 23 49 73 79 24 | 61 57 65 57 83 53 58
R20M | 4109 47 130 62 38 32 64 29 | 62 51 83 57 64 43 48
R21 | 753 10 25 26 16 10 24 8 | 41 28 55 41 41 37 40
R22 | 2449 15 11 12 21 17 15 7 | 27 33 38 52 29 36 32
R24M | 548 13 19 23 25 9 15 8 | 33 38 45 46 40 34 36
XR25 | 8780 17 20 --- --- 13 --- 11 | 26 21 --- --- 24 --- 22
XR26 |12721 21 --- --- 43 43 --- 25 | 29 --- --- 28 28 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1989 20 37 24 27 23 31 |T 55 55 62 61 57 50 53
WRMS | 1989 17 21 18 21 19 31 |NE 26 27 32 32 29 27 26
MEDI | 1380 14 18 18 21 16 16 |MD 34 33 45 46 41 37 39
Table 3.2309.2 GPS week: 2309 Day: 2 MJD: 60409
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 925 25 35 25 28 14 34 12 | 52 43 60 44 47 58 48
R02 | 1408 8 12 18 12 16 29 7 | 23 23 28 25 27 30 22
R03 | 2491 10 10 13 9 12 19 5 | 23 27 28 29 23 29 24
R04 | 557 14 11 9 8 16 20 6 | 17 20 21 19 20 19 16
R05 | 884 13 13 9 8 14 15 5 | 17 28 23 19 18 28 18
R07 | 835 7 12 10 10 18 22 6 | 15 21 20 22 18 19 16
R08M | 1228 13 11 11 13 14 18 6 | 15 17 21 17 13 20 14
R09E | 2770 24 15 16 15 15 21 8 | 39 55 52 52 51 45 46
R11E | 2972 13 10 12 30 18 16 7 | 52 54 61 74 47 58 55
R12E | 860 12 15 9 40 18 20 8 | 119 124 116 136 122 114 119
R13E | 787 42 26 33 104 30 35 21 | 123 130 134 161 105 118 121
R14E | 2477 16 26 11 80 20 20 14 | 63 65 61 94 54 64 60
XR15E | 627 20 20 16 33 18 --- 10 | 176 167 177 188 164 --- 172
R16E | 2478 24 29 15 39 18 27 11 | 138 143 141 139 136 135 137
XR17 | 849 10 25 18 14 15 --- 8 | 37 33 51 44 49 --- 42
R18 | 1000 15 10 18 12 14 19 7 | 29 40 45 51 38 38 37
R19M | 836 30 47 21 53 59 38 18 | 45 33 35 59 75 42 41
R20M | 1613 43 138 61 55 36 78 32 | 72 69 97 90 71 43 57
R21 | 878 11 21 18 18 21 29 9 | 40 35 49 35 53 33 40
R22 | 1702 17 14 13 26 19 15 7 | 58 46 63 53 69 54 57
R24M | 915 12 16 20 16 12 17 7 | 33 34 39 34 38 31 33
XR25 |11302 15 14 --- --- 20 --- 12 | 35 43 --- --- 31 --- 35
XR26 |11540 28 --- --- 37 47 --- 27 | 45 --- --- 46 39 --- 40
------+-----------------------------------------+-------------------------------------
RMS | 1643 21 38 21 40 23 29 |T 55 56 62 65 56 51 54
WRMS | 1643 16 20 19 22 20 29 |NE 30 31 36 34 35 31 31
MEDI | 1000 15 15 16 18 18 20 |MD 40 40 51 46 47 42 41
Table 3.2309.3 GPS week: 2309 Day: 3 MJD: 60410
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 498 43 18 22 33 18 33 12 | 59 48 50 48 46 52 46
R02 | 775 12 7 14 12 12 22 6 | 24 29 28 26 23 28 24
R03 | 2102 9 9 22 10 12 18 6 | 27 32 41 29 25 28 27
R04 | 691 14 7 13 10 14 25 6 | 27 29 29 27 33 27 26
R05 | 852 20 11 20 15 14 13 7 | 26 24 24 27 26 25 22
R07 | 1709 15 16 12 21 17 29 8 | 17 33 27 18 24 36 23
R08M | 1879 11 16 7 8 21 15 6 | 25 30 22 28 27 27 24
R09E | 3331 21 10 13 12 13 30 7 | 33 31 36 40 31 31 30
R11E | 2053 17 11 27 25 18 23 9 | 31 36 47 32 43 41 34
R12E | 837 14 15 17 63 24 24 12 | 112 114 119 147 113 117 115
XR13E | 1041 23 32 58 35 33 --- 19 | 129 129 125 139 135 --- 127
R14E | 1191 9 20 17 29 16 23 8 | 40 48 49 49 45 41 42
R15E | 1003 27 15 17 68 15 23 12 | 231 227 227 215 223 156 224
R16E | 2135 31 22 10 56 12 23 11 | 91 87 89 93 83 83 84
XR17 | 737 10 16 14 17 13 --- 7 | 45 45 55 54 52 --- 48
R18 | 856 13 13 11 21 18 15 6 | 34 42 40 37 50 40 39
R19M | 1244 48 29 32 51 31 32 16 | 68 65 77 75 64 69 63
R20M | 3105 41 161 52 45 26 80 25 | 87 96 115 90 60 32 73
R21 | 712 19 20 20 22 16 33 9 | 46 33 52 45 45 30 39
R22 | 1640 14 10 14 18 16 16 6 | 34 40 37 40 42 43 36
R24M | 1194 17 21 28 18 14 28 9 | 34 33 55 45 47 39 38
XR25 |20688 19 9 --- --- 18 --- 10 | 18 26 --- --- 27 --- 21
XR26 |10843 24 --- --- 32 34 --- 21 | 26 --- --- 30 40 --- 31
------+-----------------------------------------+-------------------------------------
RMS | 1662 24 40 22 34 18 30 |T 54 58 64 60 56 49 53
WRMS | 1662 17 18 17 21 17 30 |NE 29 33 37 33 35 32 30
MEDI | 1194 17 15 17 21 16 23 |MD 34 36 49 40 45 39 38
Table 3.2309.4 GPS week: 2309 Day: 4 MJD: 60411
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 787 47 27 29 20 18 34 13 | 47 45 43 38 42 49 40
R02 | 1096 13 13 12 16 11 17 6 | 26 29 30 22 22 34 23
R03 | 1318 9 11 10 19 7 15 5 | 23 34 31 21 25 27 24
R04 | 638 9 15 12 15 12 24 6 | 21 35 27 25 31 22 24
R05 | 1230 23 17 21 14 11 11 7 | 23 32 38 22 20 25 22
R07 | 1258 14 21 18 22 13 18 8 | 20 31 29 25 20 28 21
R08M | 2914 15 21 12 18 17 20 7 | 27 32 27 21 22 31 21
R09E | 3299 15 16 16 14 12 17 6 | 31 33 40 30 32 34 31
R11E | 2169 14 11 14 12 8 20 6 | 31 36 39 39 32 32 32
R12E | 1245 19 26 30 17 37 24 12 | 130 137 126 133 135 124 129
R13E | 801 19 23 41 20 27 26 12 | 67 71 82 69 63 79 65
R14E | 1627 12 20 28 15 8 19 7 | 49 47 56 47 50 49 46
R15E | 1263 19 20 20 15 14 18 8 | 216 214 217 205 203 151 209
R16E | 1571 26 23 28 22 14 26 10 | 87 88 86 87 83 79 82
XR17 | 458 8 14 11 17 16 --- 7 | 37 34 30 41 40 --- 35
R18 | 592 11 24 12 18 20 22 8 | 35 49 41 43 42 31 38
R19M | 2408 44 23 47 40 32 49 18 | 113 113 116 105 115 107 110
R20M | 1784 85 112 62 64 35 54 31 | 88 79 83 73 36 42 48
R21 | 1249 17 25 10 12 17 15 7 | 49 35 41 49 40 47 41
R22 | 1669 16 21 11 18 22 21 8 | 26 35 31 37 32 29 28
R24M | 1684 19 21 30 13 13 19 8 | 42 33 55 42 32 32 37
XR25 |16719 24 17 --- --- 21 --- 15 | 23 30 --- --- 39 --- 30
XR26 |10579 40 --- --- 36 52 --- 31 | 44 --- --- 35 32 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 1682 28 32 27 23 19 26 |T 54 57 60 54 51 52 50
WRMS | 1682 24 20 15 20 18 25 |NE 29 34 33 32 31 30 29
MEDI | 1318 17 21 18 17 16 20 |MD 37 35 41 39 36 34 35
Table 3.2309.5 GPS week: 2309 Day: 5 MJD: 60412
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1776 38 35 22 25 19 34 13 | 41 56 42 39 38 42 40
R02 | 1592 9 20 13 7 22 20 7 | 21 24 23 18 18 23 16
R03 | 1590 12 15 11 6 13 11 5 | 20 19 22 15 12 22 14
R04 | 1221 18 11 10 11 8 12 5 | 17 26 22 13 24 22 18
R05 | 1747 18 14 15 12 13 20 7 | 16 31 34 22 27 14 21
R07 | 1216 11 12 12 12 12 14 5 | 17 26 19 21 13 17 17
R08M | 1292 10 15 12 13 12 10 5 | 23 32 29 29 21 21 22
R09E | 2320 15 9 12 19 8 13 5 | 39 39 42 37 37 37 36
R11E | 2668 12 11 13 10 7 14 5 | 32 36 38 33 30 35 32
R12E | 1309 21 10 19 17 15 24 8 | 125 117 121 120 109 111 116
XR13E | 2463 23 37 37 21 16 --- 13 | 96 112 100 94 94 --- 96
R14E | 2800 13 16 11 10 15 20 6 | 59 62 60 63 54 62 58
R15E | 837 17 17 29 17 13 18 8 | 195 197 204 187 192 123 194
R16E | 1608 16 22 28 23 8 23 9 | 77 84 84 74 79 73 76
XR17 | 535 9 12 20 19 10 --- 7 | 37 37 45 34 36 --- 36
R18 | 660 9 25 23 24 14 23 9 | 29 38 40 35 33 28 30
R19M | 1974 47 20 46 46 23 53 17 | 134 140 149 134 125 132 135
R20M | 1545 48 152 56 50 46 86 28 | 63 51 53 61 39 48 49
R21 | 1181 20 20 11 14 15 25 8 | 38 33 31 40 26 32 30
R22 | 2652 18 16 28 20 17 14 8 | 28 25 37 37 27 24 26
R24M | 1497 21 12 21 21 16 18 8 | 37 36 45 37 42 33 36
XR25 |13684 17 13 --- --- 11 --- 9 | 20 22 --- --- 20 --- 19
XR26 |10078 42 --- --- 43 60 --- 35 | 60 --- --- 73 68 --- 66
------+-----------------------------------------+-------------------------------------
RMS | 1757 23 39 24 22 18 29 |T 53 56 59 55 50 47 51
WRMS | 1757 20 22 21 18 15 25 |NE 27 28 30 30 27 22 26
MEDI | 1592 17 15 19 17 14 20 |MD 37 36 42 37 36 33 36
Table 3.2309.6 GPS week: 2309 Day: 6 MJD: 60413
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01M | 1083 41 31 19 43 15 26 13 | 58 62 57 55 56 50 54
R02 | 1433 13 22 14 13 12 11 6 | 25 30 32 27 23 20 23
R03 | 1334 12 25 13 27 12 10 7 | 31 33 30 33 33 28 28
R04 | 1299 23 23 11 19 12 7 7 | 30 29 22 29 27 25 23
R05 | 757 22 16 16 15 18 15 7 | 31 36 34 27 40 29 29
R07 | 2332 8 19 11 15 8 9 5 | 25 26 22 24 22 22 21
R08M | 1387 8 8 9 18 12 11 5 | 32 30 29 34 35 35 32
R09E | 1523 16 8 22 21 10 15 7 | 43 47 49 44 40 42 42
R11E | 2863 14 16 9 17 13 15 6 | 36 33 36 37 42 34 36
R12E | 2636 19 18 13 16 13 17 7 | 130 145 134 138 128 135 133
R13E | 2880 22 38 46 30 19 35 14 | 112 93 120 124 111 129 110
R14E | 2939 10 16 20 17 8 18 7 | 82 85 89 75 81 78 81
R15E | 1781 14 12 14 25 22 19 8 | 194 192 196 199 188 118 192
R16E | 2483 11 28 21 21 12 22 8 | 87 76 92 98 94 85 88
XR17 | 705 10 11 13 24 13 --- 7 | 59 53 61 48 59 --- 55
R18 | 1185 15 16 15 24 16 20 8 | 48 64 65 48 63 45 55
R19M | 1312 44 36 40 53 17 48 18 | 180 165 170 172 176 177 171
R20M | 2738 58 114 68 62 61 72 32 | 127 58 117 119 92 59 90
R21 | 987 10 32 13 12 18 16 8 | 64 42 66 61 61 51 57
XR22 | 3665 19 19 18 17 12 --- 8 | 41 34 49 54 46 --- 43
R24M | 2087 25 21 16 13 15 26 9 | 64 43 63 53 57 43 53
XR25 |13303 16 14 --- --- 11 --- 9 | 22 24 --- --- 25 --- 21
XR26 |12460 37 --- --- 38 48 --- 30 | 98 --- --- 94 95 --- 94
------+-----------------------------------------+-------------------------------------
RMS | 1978 24 34 25 28 20 26 |T 70 63 73 72 69 63 66
WRMS | 1978 22 24 15 22 15 27 |NE 43 37 42 44 44 31 40
MEDI | 1781 16 19 15 19 13 17 |MD 58 43 61 53 57 45 54
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