[IGSREPORT-29312] Wk 2259 IGLOS Final Orbits
acc
acc at igs.org
Mon May 15 02:53:46 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2259 (Apr 23, 2023 - Apr 29, 2023)
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 2.2259.
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:
igl2259[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2259 in the SP3 format.
igl22597.sum Combination Report for GPS Week 2259.
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. The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
3. 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).
4. 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
5. 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 | 0.2 ns
1 | 0.7 ns
2 | 0.1 ns
3 | -14.3 ns
4 | -11.1 ns
5 | 0.5 ns
6 | 0.7 ns
6. 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 R22
1 | ESA | R20 R22
2 | ESA | R20 R22
3 | ESA | R20 R22
4 | ESA | R20 R22
5 | ESA | R22
6 | ESA | R20 R22
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 1.2259, 1a.2259).
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 2.2259.0-6)
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 3.2259.0-6).
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 2259 summary. (Apr 23, 2023 - Apr 29, 2023)
Table 1.2259.a GPS week : 2259 MJD: 60057.0-60063.0
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 0 -32 30 .03 18 15 | 32198 145 3243 9376
| 0 0 1 19 10 16 .02 | 6804 828
esa n/a| 0 0 4 0 15 -48 -.10 44 24 | 145 638 3691 9200
| 1 2 1 13 18 25 .03 | 13237 797
gfz n/a| 0 0 -6 23 -25 -42 -.06 27 17 | 0 320 3664 8928
| 0 1 1 13 24 29 .06 | 0 923
grg n/a| 0 0 0 -25 48 52 .11 23 18 | -3608 234 3662 8465
| 1 1 2 10 9 37 .08 | 6659 803
iac n/a| 0 0 -7 -2 -3 -26 -.26 26 22 | -1942 -57 3624 9818
| 1 0 3 3 33 74 .04 | 6820 1169
Table 1.2259.b GPS week : 2259 MJD: 60057.0-60063.0
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 | 15 18 21 15 15 14 22 |
R02 | 10 9 7 8 8 8 7 |
R03 | 7 7 7 9 6 8 6 |
R04 | 8 8 9 7 7 7 9 |
R05 | 8 10 7 10 8 8 8 |
R07 | 12 11 9 8 6 8 7 |
R08 | 8 9 9 8 9 6 8 |
R09 | 7 10 10 9 8 12 8 |
R11 | 7 7 7 8 7 7 7 |
R12 | 8 8 8 8 11 10 12 |
R13 | 19 18 26 21 17 22 25 |
R14 | 9 8 9 12 12 11 11 |
R15 | 11 12 8 10 9 8 8 |
R16 | 20 23 23 22 20 26 19 |
R17 | 7 12 9 12 7 7 11 |
R18 | 8 8 10 12 11 9 8 |
R19 | 18 25 22 24 24 22 23 |
R20 | 19 21 24 26 26 42 28 |
R21 | 10 10 10 11 11 7 10 |
R22 | 15 10 13 13 14 16 15 |
R24 | 10 12 11 10 13 11 15 |
R25 | 0 0 0 0 0 0 0 |
Table 1.2259.c GPS week : 2259 MJD: 60057.0-60063.0
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 2259 0 | -28 99 79 -2932 -117 -2794 82.1 1249 1249 | 183 0
brd 2259 1 | 19 -8 192 -849 217 -2969 80.4 1327 1327 | 735 0
brd 2259 2 | -22 17 162 -33 -900 3090 80.6 1479 1479 | 123 0
brd 2259 3 | -22 -13 197 914 -421 2721 81.4 1444 1444 | -14337 0
brd 2259 4 | -41 -2 155 -524 627 2379 79.9 1350 1350 | -11116 0
brd 2259 5 | 31 -21 203 1093 616 940 81.6 1435 1435 | 502 0
brd 2259 6 | -4 -41 259 2481 317 1596 81.1 1634 1634 | 697 0
-------------+------------------------------------------------------------+----------------
brd 2259 mean| -9 4 178 21 48 709 81.0 1416 1416 | -3316 0
brd 2259 sdev| 26 45 55 1721 563 2554 .8 124 124 | 6499 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 2.2259.0 GPS week: 2259 Day: 0 MJD: 60057
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 -19 -32 32 .02 13 11 | 36059 470 3131 8144
esa n/a| 2 0 4 10 1 -75 -.12 42 25 | 1431 389 3140 7534
gfz n/a| 1 2 -8 31 9 -57 -.05 24 17 | 0 -106 3135 7511
grg n/a| -2 -1 0 -32 42 106 .23 23 21 | 32 240 3117 6893
iac n/a| -1 0 0 -6 38 75 -.31 28 25 | 1109 1589 3057 8153
Table 2.2259.1 GPS week: 2259 Day: 1 MJD: 60058
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 2 -9 -26 31 .04 16 16 | 35431 255 3580 8104
esa n/a| 1 1 2 1 6 -29 -.13 45 26 | 3357 592 3596 7211
gfz n/a| 0 1 -7 28 -39 -6 -.04 32 19 | 0 852 3561 7796
grg n/a| 0 -2 0 -24 51 15 .14 19 15 | 333 477 3565 7346
iac n/a| 0 0 -8 0 -3 19 -.28 27 26 | 1560 929 3506 8252
Table 2.2259.2 GPS week: 2259 Day: 2 MJD: 60059
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 15 -28 13 .01 19 14 | 36274 -182 2968 9908
esa n/a| 1 1 7 7 19 -53 -.07 47 23 | 3212 -278 2920 11513
gfz n/a| 0 0 -8 38 -27 -27 -.18 30 20 | 0 -504 2920 8772
grg n/a| 2 -1 -4 -37 43 62 .11 21 15 | 185 -342 2902 8098
iac n/a| 0 0 -7 0 -34 -56 -.25 28 24 | 3170 -2035 2926 9873
Table 2.2259.3 GPS week: 2259 Day: 3 MJD: 60060
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 -25 -39 15 .02 19 16 | 21362 -1030 3332 9088
esa n/a| 1 1 5 19 53 -35 -.05 44 21 | -16470 -349 3356 7431
gfz n/a| -1 0 -5 25 -60 -79 -.02 27 19 | 0 -1127 3302 7897
grg n/a| 2 -2 0 -6 68 81 .01 24 20 | -13901 -1273 3298 7366
iac n/a| 0 0 -9 -2 -31 12 -.19 29 20 | -13173 76 3273 9077
Table 2.2259.4 GPS week: 2259 Day: 4 MJD: 60061
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 26 -29 51 .05 19 16 | 23209 1502 3286 10091
esa n/a| -1 0 4 -2 20 -36 -.08 43 22 | -18113 1294 5044 8963
gfz n/a| 0 -1 -6 0 -41 -67 -.07 24 18 | 0 1214 5000 10973
grg n/a| 1 0 1 -16 48 35 .06 25 20 | -12777 875 4992 10632
iac n/a| 0 2 -9 2 24 -112 -.26 23 21 | -10448 -748 4936 11836
Table 2.2259.5 GPS week: 2259 Day: 5 MJD: 60062
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 3 -16 53 .07 19 15 | 36248 -562 3063 10332
esa n/a| -2 -2 3 -16 0 -90 -.11 37 23 | 18684 1014 4511 13121
gfz n/a| 1 0 -4 29 -17 -51 -.07 23 14 | 0 592 4457 10857
grg n/a| 1 0 2 -34 40 62 .17 28 20 | 789 630 4453 10503
iac n/a| -1 0 -7 -5 23 3 -.26 24 20 | 2498 135 4366 11720
Table 2.2259.6 GPS week: 2259 Day: 6 MJD: 60063
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 -1 14 -51 14 .01 19 14 | 36807 565 3346 9966
esa n/a| 0 -3 4 -15 5 -20 -.10 53 30 | 8918 1809 3276 8632
gfz n/a| 1 0 -7 9 1 -6 -.01 27 16 | 0 1322 3273 8692
grg n/a| 1 1 3 -26 46 0 .05 22 18 | 81 1036 3313 8423
iac n/a| -1 0 -8 -6 -42 -126 -.30 22 18 | 1690 -348 3305 9817
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 3.2259.0 GPS week: 2259 Day: 0 MJD: 60057
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1861 19 17 31 34 26 14 | 67 61 67 51 46 59
R02 | 656 11 16 15 28 21 10 | 39 38 38 47 46 38
R03 | 1156 9 9 9 19 15 6 | 48 51 48 59 55 50
R04 | 1362 11 16 16 12 16 8 | 43 41 39 41 36 39
R05 | 1025 14 15 14 10 15 8 | 40 51 41 42 40 41
R07 | 653 9 26 12 30 26 11 | 42 44 44 51 51 43
R08 | 844 10 10 16 20 20 8 | 37 39 38 49 41 38
R09E | 2116 11 11 14 10 18 6 | 44 50 52 45 44 46
R11E | 1069 12 10 12 10 15 6 | 32 29 34 35 37 31
R12E | 1340 10 13 19 14 23 8 | 65 66 75 70 62 67
R13E | 1174 20 43 38 32 35 18 | 106 106 107 105 108 102
R14E | 719 9 17 15 23 13 9 | 77 75 78 98 75 80
R15E | 1382 11 21 18 26 27 11 | 85 74 87 97 93 84
R16E | 1086 16 33 54 33 20 20 | 107 108 108 121 111 108
R17 | 596 10 16 9 10 14 6 | 51 41 58 56 53 50
R18 | 550 10 12 18 13 17 7 | 45 55 61 63 56 53
R19 | 714 22 35 33 37 37 18 | 64 38 82 53 52 56
R20 | 2519 16 163 33 32 82 18 | 94 66 112 94 65 95
R21 | 1007 11 25 19 16 13 10 | 46 33 51 43 46 41
XR22 | 3751 --- 363 14 16 20 15 | --- 147 62 69 64 63
R24 | 976 9 20 25 15 31 10 | 40 36 51 44 50 39
XR25 |13025 3 --- --- --- 44 0 | 54 --- --- --- 39 54
------+------------------------------------+--------------------------------
RMS | 1248 13 42 24 23 28 |T 58 59 63 63 57 58
WRMS | 1248 11 25 17 21 25 |NE 50 52 56 54 49 50
MEDI | 1069 11 17 16 19 20 |MD 48 51 58 53 51 50
Table 3.2259.1 GPS week: 2259 Day: 1 MJD: 60058
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1821 30 31 28 32 16 17 | 42 46 39 24 34 34
R02 | 615 12 19 16 14 24 8 | 23 35 22 28 28 24
R03 | 1033 11 11 15 8 14 6 | 33 31 32 33 24 30
R04 | 696 15 13 17 10 18 8 | 26 28 28 29 21 26
R05 | 765 17 23 9 14 9 9 | 21 46 32 35 23 30
R07 | 1124 15 18 21 19 14 10 | 24 34 37 39 27 30
R08 | 1204 9 17 16 21 22 9 | 19 29 26 30 27 22
R09E | 2383 16 16 22 15 21 10 | 44 41 55 48 45 44
R11E | 1038 10 9 18 10 16 6 | 18 23 32 24 25 21
R12E | 1713 12 13 12 14 39 7 | 66 67 67 70 56 67
R13E | 1548 20 30 50 20 48 17 | 65 69 89 65 69 66
R14E | 858 7 20 13 13 13 8 | 59 64 58 59 58 59
R15E | 2207 10 20 27 24 14 11 | 52 57 63 49 48 51
R16E | 1492 25 39 69 26 28 23 | 75 78 71 72 75 70
R17 | 705 13 31 23 16 14 12 | 30 34 36 40 33 30
R18 | 627 13 14 19 10 33 8 | 32 34 41 40 53 34
R19 | 1572 26 45 70 34 29 25 | 46 38 79 44 33 40
R20 | 1355 21 176 46 26 66 21 | 58 71 95 67 35 68
R21 | 565 15 17 17 16 14 9 | 34 29 25 38 27 30
XR22 | 3789 --- 367 13 6 29 10 | --- 122 71 78 60 75
R24 | 1112 13 23 32 13 22 11 | 29 21 33 30 29 23
XR25 |14200 2 --- --- --- 37 0 | 35 --- --- --- 43 35
------+------------------------------------+--------------------------------
RMS | 1327 16 45 32 19 27 |T 39 47 49 44 39 41
WRMS | 1327 16 26 19 15 26 |NE 32 42 42 39 33 35
MEDI | 1124 13 20 19 15 21 |MD 34 38 39 40 33 34
Table 3.2259.2 GPS week: 2259 Day: 2 MJD: 60059
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1880 44 38 31 27 37 21 | 51 23 27 33 37 28
R02 | 742 9 18 8 9 16 6 | 25 41 31 24 30 27
R03 | 1259 11 10 14 13 14 7 | 36 41 39 28 30 33
R04 | 1023 15 11 21 9 15 8 | 33 35 30 28 27 29
R05 | 811 12 13 16 5 16 7 | 37 38 29 34 37 34
R07 | 1770 15 15 10 16 21 8 | 27 40 31 34 33 31
R08 | 995 8 15 17 19 21 9 | 19 24 23 24 20 18
R09E | 2248 15 13 27 9 24 9 | 31 31 33 32 31 28
R11E | 1251 11 9 16 8 14 6 | 18 28 34 23 26 23
R12E | 1634 12 15 12 12 21 7 | 59 64 61 63 59 60
R13E | 2379 21 40 74 39 50 26 | 47 53 104 68 59 57
R14E | 1051 10 16 9 22 21 8 | 82 87 80 98 81 86
R15E | 1470 9 17 14 14 18 8 | 59 54 61 62 59 57
R16E | 747 29 40 59 28 19 22 | 56 65 60 51 42 51
R17 | 1631 6 16 25 15 15 9 | 33 35 49 42 40 37
R18 | 548 14 15 16 19 30 9 | 26 38 40 42 57 34
R19 | 2237 38 30 30 45 35 21 | 49 29 41 37 47 33
R20 | 1006 21 188 49 28 72 23 | 65 93 109 75 42 77
R21 | 576 13 24 16 9 20 9 | 39 28 41 39 37 35
XR22 | 3822 --- 366 14 11 41 12 | --- 160 58 59 62 58
R24 | 2037 7 28 20 14 15 10 | 27 20 41 43 29 29
XR25 |15477 2 --- --- --- 32 0 | 19 --- --- --- 22 19
------+------------------------------------+--------------------------------
RMS | 1479 19 47 30 21 28 |T 39 48 48 44 41 40
WRMS | 1479 14 23 20 15 24 |NE 34 46 42 38 36 34
MEDI | 1259 12 16 16 14 21 |MD 36 38 41 39 37 33
Table 3.2259.3 GPS week: 2259 Day: 3 MJD: 60060
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1095 30 29 15 21 30 14 | 51 37 43 37 39 39
R02 | 499 13 13 10 17 20 8 | 30 36 30 36 34 31
R03 | 1021 12 17 12 17 11 8 | 34 46 32 42 35 37
R04 | 1600 14 9 11 15 15 7 | 39 41 38 31 30 36
R05 | 796 18 8 23 17 34 10 | 33 31 31 34 47 28
R07 | 1658 17 10 15 13 14 8 | 38 52 46 49 46 44
R08 | 620 14 10 11 17 25 7 | 38 49 45 46 32 43
R09E | 3450 16 15 19 12 13 9 | 26 31 29 33 28 27
R11E | 1287 11 12 13 15 18 7 | 17 27 30 27 25 23
R12E | 1397 14 13 14 15 16 8 | 70 69 71 72 72 70
R13E | 2062 34 30 47 30 65 20 | 52 53 79 43 56 46
R14E | 785 11 23 14 28 18 11 | 55 58 59 71 56 57
R15E | 1092 12 13 21 18 12 9 | 43 42 56 57 43 47
R16E | 761 24 30 61 30 15 22 | 34 39 50 41 29 34
R17 | 1654 11 21 27 22 16 12 | 34 30 47 35 31 32
R18 | 513 12 23 14 26 21 11 | 30 44 40 46 29 36
R19 | 1513 37 36 39 54 30 24 | 61 46 81 56 55 57
R20 | 1701 19 177 47 41 76 26 | 87 72 104 80 46 86
R21 | 705 11 26 22 15 21 11 | 38 27 46 44 39 36
XR22 | 2603 --- 377 12 12 13 12 | --- 148 50 40 28 43
R24 | 1434 15 16 19 15 17 9 | 38 27 42 35 36 33
XR25 |13281 3 --- --- --- 22 0 | 16 --- --- --- 27 17
------+------------------------------------+--------------------------------
RMS | 1444 19 44 27 24 29 |T 41 47 49 45 39 41
WRMS | 1444 16 21 19 20 20 |NE 40 49 48 43 36 39
MEDI | 1287 14 17 15 17 18 |MD 38 42 46 42 35 36
Table 3.2259.4 GPS week: 2259 Day: 4 MJD: 60061
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1031 20 27 18 33 24 14 | 43 41 45 40 34 40
R02 | 691 17 8 17 13 20 8 | 26 24 29 24 25 23
R03 | 1381 7 6 11 14 14 5 | 29 27 21 33 22 26
R04 | 1719 12 12 8 15 12 7 | 31 30 33 24 23 27
R05 | 591 14 17 12 11 19 8 | 31 46 39 37 41 37
R07 | 705 12 10 7 14 31 6 | 36 35 33 40 52 35
R08 | 581 21 15 14 10 19 9 | 27 47 40 40 28 36
R09E | 3659 15 9 13 16 19 8 | 33 31 37 28 33 31
R11E | 1339 11 12 15 10 16 7 | 20 27 26 21 25 21
R12E | 943 23 13 14 25 26 11 | 90 93 91 95 85 91
R13E | 1345 23 27 35 28 32 16 | 52 59 69 53 55 54
R14E | 720 7 20 13 34 16 11 | 81 79 78 97 74 81
R15E | 1530 11 14 10 24 23 8 | 49 52 50 66 54 52
R16E | 808 24 24 55 27 18 20 | 50 49 55 52 52 49
R17 | 1168 12 9 8 18 16 7 | 36 34 34 31 30 32
R18 | 542 11 22 20 24 23 11 | 29 36 39 36 25 30
R19 | 639 41 34 36 52 28 23 | 49 37 58 40 49 41
R20 | 1514 23 177 47 38 42 26 | 84 59 69 95 71 79
R21 | 696 9 26 15 17 18 10 | 36 25 42 46 43 35
XR22 | 3225 --- 365 12 14 41 13 | --- 108 53 53 67 51
R24 | 1616 25 17 27 21 29 13 | 40 27 35 28 35 29
XR25 |10112 3 --- --- --- 25 0 | 30 --- --- --- 33 30
------+------------------------------------+--------------------------------
RMS | 1350 19 43 24 25 23 |T 42 46 46 46 43 42
WRMS | 1350 16 22 18 20 21 |NE 37 41 40 40 38 36
MEDI | 1031 14 17 14 18 20 |MD 36 37 40 40 35 35
Table 3.2259.5 GPS week: 2259 Day: 5 MJD: 60062
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 591 21 31 17 27 29 13 | 21 33 32 27 21 22
R02 | 564 12 15 9 15 17 7 | 17 26 24 26 23 20
R03 | 935 9 15 11 22 20 8 | 18 19 15 24 18 15
R04 | 814 13 14 7 10 14 6 | 24 19 24 18 21 20
R05 | 667 14 14 11 13 14 7 | 25 32 29 20 27 23
R07 | 815 6 15 12 17 20 7 | 22 23 18 22 25 18
R08 | 1411 12 12 6 13 10 6 | 20 26 19 23 21 19
R09E | 2734 12 13 25 26 10 11 | 31 36 43 37 33 33
R11E | 1705 11 13 12 15 11 7 | 23 31 29 29 24 25
R12E | 1957 17 13 8 24 29 9 | 76 66 71 70 68 70
R13E | 713 24 39 44 41 32 21 | 88 95 115 84 83 91
R14E | 691 9 21 13 28 15 10 | 66 70 68 67 60 65
R15E | 1250 9 20 8 18 23 8 | 56 56 55 62 46 56
R16E | 925 31 33 64 37 32 25 | 74 80 89 81 71 74
R17 | 1083 10 14 12 9 15 6 | 36 37 30 35 30 33
R18 | 596 14 18 14 18 14 9 | 29 42 43 35 32 34
R19 | 509 35 53 23 41 26 21 | 52 27 36 41 48 35
R20 | 1553 38 130 45 73 59 41 | 82 58 89 83 72 67
R21 | 1058 9 21 8 12 30 7 | 29 31 26 34 48 28
XR22 | 2002 --- 356 13 18 26 15 | --- 56 33 37 26 34
R24 | 3592 23 23 16 12 16 11 | 41 27 23 29 28 28
XR25 |13061 3 --- --- --- 45 0 | 29 --- --- --- 41 28
------+------------------------------------+--------------------------------
RMS | 1434 19 37 23 28 24 |T 40 42 43 42 39 38
WRMS | 1434 15 23 14 20 20 |NE 31 32 31 32 32 28
MEDI | 935 12 18 12 18 20 |MD 29 33 32 35 30 28
Table 3.2259.6 GPS week: 2259 Day: 6 MJD: 60063
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 854 28 49 39 33 25 21 | 65 58 68 51 37 54
R02 | 984 12 13 10 11 16 7 | 38 44 44 46 43 42
R03 | 741 8 7 10 14 20 5 | 42 44 42 55 44 45
R04 | 552 14 16 15 13 16 8 | 44 34 34 41 37 38
R05 | 703 13 12 19 9 13 8 | 41 46 41 40 46 40
R07 | 824 13 10 13 9 15 6 | 52 54 57 57 60 54
R08 | 1655 11 15 10 15 19 7 | 41 45 43 51 45 43
R09E | 3159 11 10 16 14 19 7 | 47 50 55 44 47 48
R11E | 1474 12 12 14 10 11 7 | 25 30 36 29 31 28
R12E | 3667 15 12 22 27 21 11 | 67 67 71 80 62 70
R13E | 773 35 45 52 39 45 24 | 117 96 114 108 126 103
R14E | 891 8 21 12 28 16 10 | 85 80 86 101 84 87
R15E | 1300 9 12 13 20 19 8 | 61 59 60 75 55 63
R16E | 891 20 25 56 23 22 19 | 103 101 106 103 104 102
R17 | 746 12 21 24 17 15 10 | 47 36 54 42 48 44
R18 | 631 15 15 11 8 9 7 | 38 51 50 46 45 45
R19 | 721 25 53 45 37 36 23 | 75 29 87 65 73 62
R20 | 2563 45 210 34 36 38 28 | 125 61 135 134 104 127
R21 | 921 11 26 15 13 12 9 | 47 36 52 49 52 44
XR22 | 2140 --- 362 16 13 25 15 | --- 133 39 41 39 37
R24 | 2924 22 31 23 24 12 14 | 49 30 51 41 42 40
XR25 |13862 3 --- --- --- 38 0 | 33 --- --- --- 37 31
------+------------------------------------+--------------------------------
RMS | 1634 19 53 27 22 22 |T 59 56 63 61 57 56
WRMS | 1634 14 29 16 18 18 |NE 52 50 56 54 50 49
MEDI | 891 13 16 16 15 19 |MD 47 50 54 51 46 45
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