[IGSREPORT-29834] Wk 2308 IGLOS Final Orbits
acc
acc at igs.org
Fri Apr 19 06:23:13 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2308 (Mar 31, 2024 - Apr 06, 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 2.2308.
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:
igl2308[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2308 in the SP3 format.
igl23087.sum Combination Report for GPS Week 2308.
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 | 2.2 ns
1 | -0.5 ns
2 | 3.1 ns
3 | 4.4 ns
4 | 2.0 ns
5 | 0.8 ns
6 | 0.4 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
----+--------+---------------
6 | 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 1.2308, 1a.2308).
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 2.2308.0-6)
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 3.2308.0-6).
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 2308 summary. (Mar 31, 2024 - Apr 06, 2024)
Table 1.2308.a GPS week : 2308 MJD: 60400.0-60406.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 1 -4 -37 45 .14 24 17 | 8297 -150 3767 17755
| 1 1 2 6 17 19 .04 | 1993 2545
esa n/a| 0 -1 3 -21 5 -35 .01 30 18 | 2545 -472 3438 7774
| 1 1 2 13 8 25 .05 | 5193 2287
gfz n/a| 0 0 -3 3 0 -10 -.02 24 15 | 0 -183 3447 7417
| 1 0 1 9 19 33 .03 | 0 2345
grg n/a| 1 0 3 -19 0 7 .24 24 20 | 4630 -331 3766 17356
| 1 0 1 27 19 23 .04 | 2491 2371
iac n/a| 0 0 -6 8 4 -27 -.15 17 15 | 6751 -160 3787 19062
| 1 1 1 21 14 47 .06 | 2698 1533
jgx n/a| 0 0 5 37 42 28 -.12 29 28 | 7638 -48 3520 7694
| 1 1 2 22 17 65 .07 | 1454 2467
Table 1.2308.b GPS week : 2308 MJD: 60400.0-60406.0
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 | 9 10 10 10 12 14 13 |
R02 | 6 6 7 6 6 7 8 |
R03 | 6 5 5 7 6 6 6 |
R04 | 5 4 6 5 7 7 6 |
R05 | 8 7 7 6 6 6 5 |
R07 | 5 8 7 7 6 6 6 |
R08 | 6 6 8 7 7 6 7 |
R09 | 7 8 7 8 9 7 7 |
R11 | 7 8 7 6 8 7 6 |
R12 | 10 7 7 8 6 8 7 |
R13 | 16 16 18 15 14 16 18 |
R14 | 8 6 7 7 7 8 5 |
R15 | 7 9 7 8 7 9 7 |
R16 | 8 8 9 9 9 9 9 |
R17 | 7 8 9 9 7 8 7 |
R18 | 6 6 6 7 8 8 9 |
R19 | 24 18 17 23 21 17 20 |
R20 | 30 31 31 28 30 28 24 |
R21 | 8 8 10 9 10 8 8 |
R22 | 10 6 9 9 8 8 7 |
R24 | 7 7 9 8 9 10 11 |
R25 | 10 10 10 9 7 10 16 |
R26 | 31 35 32 35 38 37 27 |
Table 1.2308.c GPS week : 2308 MJD: 60400.0-60406.0
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 2308 0 | -88 11 162 3166 -2017 11560 80.6 1711 1711 | 2234 0
brd 2308 1 | 69 51 69 925 481 7409 82.3 1626 1626 | -532 0
brd 2308 2 | -99 -85 95 -1024 18 13490 82.6 1609 1609 | 3054 0
brd 2308 3 | -15 78 48 303 -166 12510 80.2 1562 1562 | 4365 0
brd 2308 4 | -132 -42 -64 -635 -3182 5609 80.4 1659 1659 | 1976 0
brd 2308 5 | -58 6 127 -1542 -1648 6307 81.4 1877 1877 | 751 0
brd 2308 6 | 124 -35 83 -2871 1296 9376 80.1 2113 2113 | 352 0
-------------+------------------------------------------------------------+----------------
brd 2308 mean| -28 -2 74 -239 -745 9465 81.1 1736 1736 | 1742 0
brd 2308 sdev| 94 56 71 1942 1579 3134 1.0 194 194 | 1682 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 2.2308.0 GPS week: 2308 Day: 0 MJD: 60400
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 -21 59 .13 24 17 | 8072 -931 3862 10926
esa n/a| 2 -2 2 -36 15 -55 -.05 28 19 | -1489 -517 3263 8666
gfz n/a| 1 0 -5 -6 12 -56 -.00 34 17 | 0 -592 3283 8410
grg n/a| 0 0 3 19 -30 4 .25 23 18 | 3655 -1207 3720 9585
iac n/a| -1 0 -5 3 -15 46 -.17 18 16 | 6041 -1587 3708 11194
jgx n/a| -1 0 6 39 53 -58 -.14 28 28 | 9427 -783 3350 8667
Table 2.2308.1 GPS week: 2308 Day: 1 MJD: 60401
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 2 0 -28 48 .09 20 15 | 4850 -2524 3079 6984
esa n/a| 0 0 2 -16 -7 -9 .00 28 15 | 7996 -2548 3026 7864
gfz n/a| 3 1 -2 8 27 -20 -.04 28 13 | 0 -2075 3087 6796
grg n/a| 0 -2 4 -4 -12 -2 .24 24 20 | 541 -2372 3141 6313
iac n/a| -1 1 -5 2 9 12 -.06 15 13 | 1854 -559 3080 7216
jgx n/a| -1 1 2 13 22 -40 -.21 29 29 | 6486 -2419 3123 7087
Table 2.2308.2 GPS week: 2308 Day: 2 MJD: 60402
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 0 0 -59 56 .09 23 17 | 9150 -629 3754 21702
esa n/a| 1 0 3 -7 10 -2 -.06 30 18 | 5896 -1248 3400 8458
gfz n/a| 2 1 -3 -7 -18 50 -.05 25 17 | 0 -1202 3429 7444
grg n/a| 1 0 1 -54 -6 24 .30 24 24 | 7282 -830 3813 22049
iac n/a| 0 0 -4 28 14 -101 -.07 16 15 | 8070 675 3820 23532
jgx n/a| 0 1 4 40 70 8 -.21 28 27 | 6557 -698 3566 7796
Table 2.2308.3 GPS week: 2308 Day: 3 MJD: 60403
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 -1 -1 -5 -33 38 .16 27 21 | 9549 278 4328 21600
esa n/a| 0 -1 7 -11 0 -38 .02 24 15 | 6218 157 3977 7277
gfz n/a| 2 2 -1 3 -22 -8 -.05 27 15 | 0 933 3931 7101
grg n/a| 1 0 2 -44 24 15 .27 25 20 | 7686 528 4305 21149
iac n/a| -1 0 -8 26 16 -37 -.18 18 16 | 10539 -1413 4379 23263
jgx n/a| 1 -1 7 68 47 36 -.09 27 26 | 7825 1372 4001 7381
Table 2.2308.4 GPS week: 2308 Day: 4 MJD: 60404
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 0 3 -18 52 .18 28 20 | 7459 5123 3718 21388
esa n/a| 0 -1 5 -9 10 -45 .03 33 19 | 5254 4075 3409 7481
gfz n/a| -1 0 -4 1 -17 2 .02 21 16 | 0 4533 3404 8178
grg n/a| 2 0 4 -30 -2 -37 .18 25 20 | 3390 4489 3711 21148
iac n/a| 1 2 -7 11 21 -17 -.16 18 14 | 7240 2315 3787 23125
jgx n/a| 2 -1 9 15 30 119 -.03 29 28 | 6736 4435 3453 8422
Table 2.2308.5 GPS week: 2308 Day: 5 MJD: 60405
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 2 -2 -62 59 .19 23 17 | 11237 -2249 3372 20988
esa n/a| 0 -3 2 -40 10 -73 .05 29 19 | -6317 -2797 3015 6701
gfz n/a| 0 1 -3 6 12 -36 -.04 19 14 | 0 -2327 2977 6879
grg n/a| 0 0 5 -28 22 13 .22 24 18 | 5790 -2469 3334 20795
iac n/a| 0 -1 -7 18 -8 -40 -.20 19 15 | 7957 -1598 3424 22778
jgx n/a| 1 0 6 66 25 92 -.08 32 27 | 9874 -2786 3045 7156
Table 2.2308.6 GPS week: 2308 Day: 6 MJD: 60406
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 -9 -40 4 .12 22 16 | 7768 -118 4259 20703
esa n/a| 0 0 0 -30 0 -24 .07 40 20 | 259 -432 3976 7975
gfz n/a| 0 0 -2 21 6 -3 .01 18 12 | 0 -555 4021 7115
grg n/a| 2 0 4 8 6 36 .24 23 18 | 4067 -456 4343 20459
iac n/a| 0 -1 -10 -34 -8 -53 -.23 18 17 | 5559 1042 4311 22330
jgx n/a| 0 0 3 22 50 45 -.08 29 29 | 6567 539 4108 7350
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 3.2308.0 GPS week: 2308 Day: 0 MJD: 60400
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1221 18 20 23 29 14 14 9 | 34 37 43 35 37 39 35
R02 | 747 9 8 24 9 13 12 5 | 29 32 28 29 31 26 28
R03 | 2583 9 17 15 13 12 9 5 | 30 41 39 35 35 34 34
R04 | 1447 10 12 11 8 13 14 5 | 30 38 27 29 28 36 29
R05 | 1201 22 19 16 11 16 19 8 | 34 56 45 43 29 41 38
R07 | 1406 10 14 7 12 7 9 4 | 33 30 33 30 32 39 31
R08 | 2053 15 11 12 11 14 15 6 | 31 26 35 30 34 29 29
R09 | 3427 15 18 15 17 15 13 7 | 117 125 126 121 119 120 120
R11 | 1605 18 11 17 18 12 16 7 | 43 45 55 35 43 46 42
R12 | 987 15 15 37 29 9 27 10 | 63 69 84 61 64 53 62
R13 | 1902 30 39 48 28 23 48 16 | 129 107 143 111 117 41 114
R14 | 771 18 25 15 13 13 19 7 | 113 124 113 105 103 102 108
R15 | 1754 19 14 15 17 11 14 7 | 81 70 64 71 62 55 66
R16 | 595 24 22 16 15 11 13 7 | 82 64 65 68 61 52 64
XR17 | 979 13 21 17 12 9 --- 7 | 67 53 66 65 62 --- 62
R18 | 786 8 18 22 10 13 11 6 | 48 64 64 58 51 52 54
R19 | 1163 22 47 54 56 42 86 23 | 75 83 92 71 82 83 75
R20 | 2159 75 86 111 33 38 48 30 | 82 75 99 70 57 53 44
R21 | 1300 20 13 22 19 10 21 8 | 70 51 70 54 56 42 56
R22 | 2899 18 11 18 38 13 17 9 | 75 82 82 96 83 80 82
R24 | 639 9 18 14 17 14 21 7 | 63 57 69 65 64 55 61
XR25 |10511 15 14 --- --- 14 --- 10 | 20 24 --- --- 20 --- 17
XR26 |12913 39 --- --- 36 51 --- 31 | 78 --- --- 70 82 --- 76
------+-----------------------------------------+-------------------------------------
RMS | 1710 24 28 34 23 18 28 |T 62 61 68 61 58 53 57
WRMS | 1710 17 19 17 18 16 28 |NE 62 61 68 61 58 53 57
MEDI | 1406 18 17 17 17 13 15 |MD 63 56 65 61 57 46 56
Table 3.2308.1 GPS week: 2308 Day: 1 MJD: 60401
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 712 25 14 32 25 17 23 10 | 18 23 35 15 26 30 20
R02 | 1241 8 8 22 12 10 18 6 | 19 21 38 15 22 22 19
R03 | 1288 5 10 12 14 13 10 5 | 18 27 21 23 19 23 19
R04 | 1501 8 7 8 9 6 11 3 | 22 28 28 26 23 22 24
R05 | 779 17 21 18 8 13 10 7 | 24 35 40 27 24 29 27
R07 | 1517 12 23 17 27 11 14 8 | 23 32 25 30 23 26 23
R08 | 1515 15 7 11 18 12 20 6 | 16 19 19 25 14 23 15
R09 | 3709 14 19 13 25 14 13 7 | 90 97 99 98 94 98 94
R11 | 2714 17 14 11 30 15 15 8 | 33 46 37 36 35 32 33
R12 | 849 13 12 15 23 8 22 7 | 69 72 79 80 67 64 70
XR13 | 3044 20 41 52 21 17 --- 15 | 98 85 127 104 93 --- 98
R14 | 775 11 17 13 11 6 15 5 | 93 94 85 88 88 85 89
R15 | 917 16 15 13 26 19 27 8 | 59 51 50 71 42 47 50
R16 | 584 25 24 16 18 10 16 8 | 62 59 46 55 48 45 50
XR17 | 739 14 24 16 13 13 --- 8 | 36 30 34 41 32 --- 32
R18 | 667 10 14 21 11 10 15 6 | 29 36 38 44 34 28 33
R19 | 905 41 33 42 43 29 59 18 | 71 86 82 86 69 81 74
R20 | 2621 45 101 90 48 36 85 30 | 50 43 85 69 38 54 37
R21 | 1319 20 12 17 23 11 22 8 | 45 38 37 33 37 32 35
R22 | 2237 16 9 10 22 10 8 6 | 51 65 63 87 66 65 65
R24 | 737 13 13 19 11 10 24 7 | 38 40 36 43 35 40 35
XR25 |11136 17 11 --- --- 13 --- 10 | 24 20 --- --- 21 --- 17
XR26 |16449 49 --- --- 38 53 --- 34 | 59 --- --- 64 69 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 1625 20 28 28 24 15 29 |T 45 47 52 52 44 44 44
WRMS | 1625 15 15 13 20 13 29 |NE 45 47 52 52 44 44 44
MEDI | 1288 16 14 16 21 13 16 |MD 38 38 38 43 35 32 35
Table 3.2308.2 GPS week: 2308 Day: 2 MJD: 60402
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1230 31 14 18 28 14 29 10 | 32 26 37 29 24 28 25
R02 | 2065 9 12 22 14 15 13 6 | 28 38 27 26 37 38 30
R03 | 715 12 11 11 8 8 9 4 | 27 35 33 35 27 29 29
R04 | 1437 11 14 14 11 14 16 6 | 25 27 25 31 29 30 24
R05 | 932 13 8 11 19 20 15 7 | 27 31 33 33 27 34 28
R07 | 2077 11 22 17 10 13 15 6 | 33 37 27 39 32 37 31
R08 | 656 10 13 14 17 7 35 7 | 26 30 33 35 25 35 27
R09 | 3856 12 19 16 21 15 13 7 | 81 92 81 81 79 79 81
R11 | 1904 12 11 15 18 13 17 6 | 42 42 52 44 47 42 43
R12 | 846 14 10 15 20 16 17 7 | 61 57 59 56 58 52 56
XR13 | 2225 34 33 52 31 25 --- 17 | 100 75 113 71 77 --- 84
R14 | 953 13 25 13 17 8 10 6 | 61 61 57 60 54 56 56
R15 | 906 17 18 11 10 16 21 7 | 66 52 55 60 62 50 57
R16 | 769 19 33 13 18 14 22 9 | 69 62 58 62 56 51 57
XR17 | 1074 9 23 13 17 18 --- 8 | 54 53 56 56 67 --- 56
R18 | 601 9 18 15 14 6 10 5 | 38 45 37 45 38 38 38
R19 | 1748 53 27 44 44 20 38 17 | 140 143 143 132 122 149 134
R20 | 1331 59 108 74 54 31 79 30 | 57 89 83 66 34 47 38
R21 | 1636 23 14 28 18 20 31 10 | 53 41 59 53 32 28 42
R22 | 2313 18 9 18 36 13 12 8 | 71 64 79 43 71 63 65
R24 | 693 13 17 18 14 18 29 8 | 53 48 60 55 57 43 51
XR25 |13451 16 10 --- --- 13 --- 9 | 29 29 --- --- 27 --- 27
XR26 |12484 48 --- --- 32 49 --- 31 | 44 --- --- 53 54 --- 48
------+-----------------------------------------+-------------------------------------
RMS | 1609 23 30 25 24 16 28 |T 52 53 57 52 49 48 49
WRMS | 1609 17 18 17 24 15 27 |NE 52 53 57 52 49 48 49
MEDI | 1331 13 14 15 18 15 17 |MD 53 45 56 53 47 42 43
Table 3.2308.3 GPS week: 2308 Day: 3 MJD: 60403
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1325 31 25 14 20 16 26 10 | 29 30 31 26 32 26 25
R02 | 2552 11 10 14 14 12 12 5 | 22 31 22 21 26 26 21
R03 | 1075 13 13 12 19 13 16 6 | 22 36 27 21 30 32 26
R04 | 887 12 7 13 9 10 13 5 | 21 23 28 19 19 26 19
R05 | 1805 18 8 16 9 8 17 5 | 20 19 23 22 14 26 16
R07 | 2383 12 9 22 14 13 16 6 | 28 28 37 26 26 30 26
R08 | 918 13 9 10 15 11 26 6 | 23 24 24 30 19 30 22
R09 | 3482 18 20 19 14 14 13 7 | 53 63 46 52 46 47 49
R11 | 896 13 9 11 13 12 15 5 | 33 30 41 33 44 32 35
R12 | 1154 15 17 18 16 20 18 8 | 43 35 33 39 42 25 33
R13 | 1058 44 17 42 35 21 39 14 | 75 48 55 50 60 45 49
R14 | 924 9 18 8 17 7 23 6 | 60 70 69 71 66 55 64
R15 | 720 12 17 13 21 13 29 8 | 70 57 63 66 67 48 60
R16 | 725 19 25 20 13 14 22 8 | 64 53 68 55 52 47 54
XR17 | 1646 11 22 20 24 12 --- 9 | 54 42 62 47 58 --- 50
R18 | 673 13 22 12 14 9 17 6 | 42 56 42 51 51 43 47
R19 | 1533 54 19 74 45 42 61 22 | 67 57 86 57 57 85 57
R20 | 1801 75 83 60 62 37 52 28 | 63 77 79 57 39 46 38
R21 | 1081 20 19 11 27 13 27 9 | 55 33 39 64 37 30 41
R22 | 1940 14 16 17 32 20 17 9 | 42 54 47 59 35 43 43
R24 | 742 22 13 15 15 18 27 8 | 53 33 42 40 50 31 40
XR25 |13453 15 11 --- --- 11 --- 8 | 23 28 --- --- 31 --- 27
XR26 |11431 40 --- --- 48 55 --- 35 | 31 --- --- 45 48 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 1562 27 24 27 25 18 27 |T 43 42 45 43 41 38 38
WRMS | 1562 21 15 15 20 16 26 |NE 43 42 45 43 41 38 38
MEDI | 1154 15 17 15 16 13 18 |MD 42 35 42 45 42 32 39
Table 3.2308.4 GPS week: 2308 Day: 4 MJD: 60404
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1359 28 33 21 26 23 36 12 | 28 45 33 20 23 41 25
R02 | 1649 15 15 14 11 8 12 5 | 23 23 23 22 17 21 18
R03 | 1476 11 9 13 14 15 17 6 | 18 21 20 17 20 21 16
R04 | 856 14 14 14 13 16 23 7 | 20 21 24 13 26 26 18
R05 | 1628 18 13 11 14 11 17 6 | 25 28 25 20 26 33 22
R07 | 2416 11 15 10 10 12 25 6 | 18 21 21 20 20 36 18
R08 | 1188 9 12 14 15 16 27 7 | 19 30 29 21 12 29 19
R09 | 2974 19 13 14 32 14 20 8 | 88 85 84 84 87 87 84
R11 | 1246 14 12 21 19 14 18 7 | 26 28 31 19 29 32 24
R12 | 2102 11 13 12 22 8 19 6 | 51 51 51 46 53 49 48
R13 | 1094 37 28 27 26 22 43 13 | 103 70 95 82 86 44 83
R14 | 619 5 17 11 16 10 30 7 | 70 73 69 67 74 57 68
R15 | 755 10 12 16 17 9 24 6 | 68 57 69 65 64 51 62
R16 | 973 23 20 21 21 15 26 9 | 66 42 65 49 47 34 49
XR17 | 1410 17 10 11 14 12 --- 6 | 48 41 36 42 33 --- 38
R18 | 739 13 21 16 26 11 20 8 | 37 46 45 58 39 33 40
R19 | 1615 68 22 52 49 27 50 20 | 117 109 111 106 107 112 106
R20 | 1792 70 123 37 54 43 53 29 | 79 65 50 65 37 51 37
R21 | 1668 19 21 19 29 14 34 10 | 48 35 52 62 36 27 41
R22 | 3153 22 9 10 26 12 18 7 | 78 89 89 119 88 81 90
R24 | 796 18 23 17 17 18 33 9 | 53 37 47 40 52 47 45
XR25 | 9076 14 7 --- --- 7 --- 7 | 16 19 --- --- 22 --- 16
XR26 |12967 55 --- --- 47 57 --- 38 | 37 --- --- 44 56 --- 47
------+-----------------------------------------+-------------------------------------
RMS | 1659 28 33 21 25 18 29 |T 49 47 50 49 45 45 44
WRMS | 1659 20 19 16 20 14 28 |NE 49 47 50 49 45 45 44
MEDI | 1476 17 14 14 19 14 24 |MD 48 41 47 44 37 36 40
Table 3.2308.5 GPS week: 2308 Day: 5 MJD: 60405
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 748 31 31 26 44 15 32 13 | 33 37 45 23 29 33 28
R02 | 1177 13 18 13 12 17 20 7 | 18 33 23 17 24 26 19
R03 | 985 9 16 11 16 11 16 5 | 14 29 21 21 17 26 17
R04 | 1463 16 10 9 18 16 15 6 | 17 20 18 18 16 22 13
R05 | 2179 15 17 11 14 8 16 6 | 17 34 25 21 23 31 21
R07 | 2114 5 11 8 9 13 30 6 | 16 19 15 20 18 27 13
R08 | 1312 12 14 11 11 12 24 6 | 15 15 14 17 18 26 12
R09 | 3390 17 15 11 22 10 22 7 | 69 73 79 66 75 77 72
R11 | 1934 15 23 14 14 15 16 7 | 26 41 30 28 33 38 29
R12 | 1954 16 23 14 22 11 17 7 | 48 59 50 48 43 37 46
XR13 | 1880 34 31 30 28 31 --- 15 | 80 84 91 75 72 --- 77
R14 | 1829 10 14 16 17 17 30 8 | 49 58 66 57 58 47 55
R15 | 1024 17 12 20 22 19 31 9 | 62 52 54 47 65 49 53
R16 | 703 18 18 14 19 14 32 8 | 59 46 53 59 54 43 51
XR17 | 919 13 12 16 28 9 --- 8 | 40 36 40 33 34 --- 34
R18 | 1185 12 19 18 26 9 21 8 | 30 41 44 39 32 30 34
R19 | 3059 42 36 32 46 25 41 16 | 42 64 50 52 37 46 44
R20 | 1603 60 98 40 39 56 83 28 | 67 52 64 45 70 64 51
R21 | 915 18 21 22 13 12 23 8 | 39 30 45 38 32 36 35
R22 | 3410 16 11 13 28 18 20 8 | 62 56 56 50 60 64 56
R24 | 1100 18 23 18 17 16 39 9 | 54 42 57 49 48 40 47
XR25 |13302 18 12 --- --- 11 --- 10 | 21 27 --- --- 21 --- 21
XR26 |13565 47 --- --- 42 61 --- 36 | 26 --- --- 22 37 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 1877 23 29 19 24 19 32 |T 39 43 44 38 39 40 37
WRMS | 1877 17 19 14 18 15 27 |NE 39 43 44 38 39 40 37
MEDI | 1603 16 17 14 19 15 23 |MD 39 41 45 38 34 37 34
Table 3.2308.6 GPS week: 2308 Day: 6 MJD: 60406
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1104 35 35 14 35 17 30 12 | 34 33 31 33 32 37 27
R02 | 1534 10 22 11 20 14 22 7 | 30 35 22 25 30 29 24
R03 | 1068 13 12 16 11 11 13 5 | 27 30 32 29 28 29 27
R04 | 1585 18 9 13 12 12 10 6 | 25 23 28 20 24 24 22
R05 | 1765 10 8 11 9 14 15 5 | 24 28 24 21 22 28 22
R07 | 1039 11 10 13 15 11 13 5 | 26 28 32 28 28 32 26
R08 | 2475 11 13 12 15 16 23 7 | 25 23 29 22 25 29 23
R09 | 3218 12 15 12 18 17 11 6 | 94 98 103 92 101 95 97
R11 | 3037 15 8 11 13 17 12 6 | 40 41 43 38 41 41 39
R12 | 1405 10 17 9 19 19 12 6 | 68 71 63 61 60 54 61
XR13 | 1892 38 22 37 50 31 --- 18 | 115 100 126 92 100 --- 103
R14 | 3149 8 13 6 16 9 14 5 | 79 86 83 80 81 73 80
R15 | 1426 15 14 13 17 12 25 7 | 81 71 70 69 77 58 70
R16 | 879 16 20 12 22 22 28 9 | 81 62 70 68 75 53 67
XR17 | 468 10 19 12 15 14 --- 7 | 62 50 65 59 58 --- 58
R18 | 879 16 21 15 29 16 20 8 | 47 65 62 48 57 40 53
R19 | 2628 42 38 36 54 34 65 20 | 66 68 82 64 71 63 63
R20 | 2375 57 155 40 29 31 71 23 | 116 69 93 80 84 60 82
R21 | 1172 16 22 19 16 13 24 8 | 64 50 72 59 56 44 57
R22 | 4205 16 8 10 22 11 16 6 | 68 67 68 66 70 70 67
R24 | 785 14 32 28 17 25 28 11 | 72 52 78 70 70 48 64
XR25 |16023 24 22 --- --- 20 --- 16 | 23 28 --- --- 29 --- 21
XR26 |12482 34 --- --- 26 47 --- 26 | 41 --- --- 35 52 --- 41
------+-----------------------------------------+-------------------------------------
RMS | 2113 22 40 18 23 18 29 |T 56 53 60 52 55 47 51
WRMS | 2113 16 20 12 18 17 29 |NE 56 53 60 52 55 47 51
MEDI | 1585 15 17 13 17 16 20 |MD 62 50 65 59 57 44 57
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