[IGSREPORT-29595] Wk 2286 IGLOS Final Orbits
acc
acc at igs.org
Tue Nov 21 23:43:16 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2286 (Oct 29, 2023 - Nov 04, 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 2.2286.
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:
igl2286[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2286 in the SP3 format.
igl22867.sum Combination Report for GPS Week 2286.
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).
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.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
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 | -0.4 ns
1 | 1.0 ns
2 | -0.1 ns
3 | -0.1 ns
4 | -1.8 ns
5 | 2.0 ns
6 | -0.7 ns
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 1.2286, 1a.2286).
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 2.2286.0-6)
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 3.2286.0-6).
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 2286 summary. (Oct 29, 2023 - Nov 04, 2023)
Table 1.2286.a GPS week : 2286 MJD: 60246.0-60252.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 2 13 -16 40 .04 21 15 | 40950 -276 2915 8896
| 0 1 1 16 15 17 .05 | 616 2370
esa n/a| 0 1 0 -12 -21 -9 -.12 31 22 | 4763 -910 2900 7933
| 1 1 1 12 13 17 .03 | 7759 2401
gfz n/a| 0 1 1 11 6 -19 -.07 23 14 | 0 -370 2936 8124
| 0 0 1 13 16 14 .06 | 0 2471
grg n/a| 0 -4 -5 -18 25 -19 .17 27 21 | -21 -186 2930 7591
| 0 1 2 16 12 43 .04 | 229 2445
iac n/a| 1 1 -9 21 -6 -23 -.22 23 21 | 1929 -392 2904 8794
| 1 2 2 35 29 71 .06 | 725 1649
jgx n/a| 1 1 3 28 18 -26 -.33 29 28 | 43837 -284 2948 8334
| 0 1 3 22 21 51 .04 | 694 2432
Table 1.2286.b GPS week : 2286 MJD: 60246.0-60252.0
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 | 18 14 13 14 16 15 14 |
R02 | 9 6 8 7 5 6 7 |
R03 | 8 9 8 6 8 7 8 |
R04 | 8 7 9 7 5 6 8 |
R05 | 7 5 7 7 6 5 8 |
R07 | 8 10 7 9 9 8 7 |
R08 | 9 11 9 8 5 9 9 |
R09 | 10 10 8 8 8 7 7 |
R11 | 8 9 7 8 7 8 8 |
R12 | 7 8 9 9 14 10 9 |
R13 | 28 23 20 17 22 19 18 |
R14 | 9 10 11 9 14 8 13 |
R15 | 10 11 10 12 25 9 11 |
R16 | 16 12 10 14 18 10 11 |
R17 | 8 6 7 7 8 8 9 |
R18 | 9 10 10 10 9 9 9 |
R19 | 34 34 37 32 29 32 36 |
R20 | 39 38 35 32 21 39 38 |
R21 | 8 9 10 10 9 9 6 |
R22 | 9 7 8 9 7 8 8 |
R24 | 8 8 13 9 10 13 9 |
R25 | 15 14 11 12 14 14 13 |
R26 | 71 322 359 284 262 269 296 |
Table 1.2286.c GPS week : 2286 MJD: 60246.0-60252.0
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 2286 0 | 110 4 11 -1231 -1328 5524 80.3 2057 2057 | -389 0
brd 2286 1 | -28 15 55 -1439 983 5089 81.1 2208 2208 | 1028 0
brd 2286 2 | -131 56 84 -558 3040 8939 81.7 1870 1870 | -52 0
brd 2286 3 | -145 50 84 1459 2356 2905 81.9 1870 1870 | -130 0
brd 2286 4 | -2 -20 44 2791 -2404 -1679 83.1 1802 1802 | -1821 0
brd 2286 5 | -12 -17 23 13 -1179 197 82.6 1870 1870 | 2047 0
brd 2286 6 | -50 5 25 -1636 -2142 1853 83.7 2067 2067 | -721 0
-------------+------------------------------------------------------------+----------------
brd 2286 mean| -37 13 46 -85 -96 3261 82.0 1963 1963 | -5 0
brd 2286 sdev| 86 30 29 1655 2206 3573 1.2 148 148 | 1241 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 2.2286.0 GPS week: 2286 Day: 0 MJD: 60246
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 -1 0 50 .01 20 12 | 39836 9 3324 9414
esa n/a| 0 3 -1 -15 -39 22 -.15 32 22 | -3591 -710 3326 7006
gfz n/a| 0 0 0 37 34 -21 .01 25 15 | 0 -727 3344 8039
grg n/a| 0 -5 -6 -47 17 -94 .24 32 34 | -352 -93 3338 7264
iac n/a| 0 0 -13 15 -24 -26 -.22 22 19 | 1334 -706 3303 9009
jgx n/a| 0 2 1 28 -18 -27 -.37 29 27 | 42798 -80 3358 8348
Table 2.2286.1 GPS week: 2286 Day: 1 MJD: 60247
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 13 -4 45 .01 19 13 | 41230 2076 2706 9257
esa n/a| 0 3 -1 8 -35 -16 -.12 35 22 | 7224 1174 2684 8272
gfz n/a| 0 2 0 7 4 -15 -.04 24 16 | 0 1837 2673 8696
grg n/a| 0 -5 -5 -22 23 -50 .20 26 26 | -48 1768 2639 8138
iac n/a| 0 0 -7 -3 -22 -66 -.27 23 21 | 1987 1151 2696 9246
jgx n/a| 0 1 0 21 28 -87 -.34 29 29 | 44366 1725 2709 8914
Table 2.2286.2 GPS week: 2286 Day: 2 MJD: 60248
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 3 28 -18 12 -.04 17 15 | 41599 -455 2861 7817
esa n/a| 1 2 2 -5 -27 -34 -.07 34 23 | 15471 -615 2844 9769
gfz n/a| 0 1 0 8 4 -1 -.00 23 16 | 0 -329 2889 7530
grg n/a| 0 -4 -8 -22 40 27 .16 27 22 | -117 -201 2909 7071
iac n/a| 3 -1 -8 -43 17 -120 -.27 22 19 | 1998 -58 2858 7946
jgx n/a| 1 1 5 76 12 -50 -.34 25 24 | 44598 -399 2911 7724
Table 2.2286.3 GPS week: 2286 Day: 3 MJD: 60249
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 29 -42 60 .04 18 15 | 41442 -897 2537 8535
esa n/a| 0 0 2 -25 -9 -16 -.10 36 31 | 4327 -2073 2533 7660
gfz n/a| 0 1 2 -7 5 -11 -.17 21 15 | 0 -219 2573 7921
grg n/a| 1 -2 -6 -25 37 -38 .17 21 16 | 351 -363 2557 7425
iac n/a| 0 2 -8 30 39 106 -.26 22 21 | 2109 -323 2528 8543
jgx n/a| 2 0 2 21 9 -88 -.35 33 33 | 44396 -600 2575 8155
Table 2.2286.4 GPS week: 2286 Day: 4 MJD: 60250
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 -15 -16 22 .10 22 17 | 40428 -3968 3097 8013
esa n/a| 0 0 0 -5 -20 3 -.12 27 19 | -7140 -4591 3099 6549
gfz n/a| 0 1 1 9 14 -18 -.07 16 11 | 0 -4426 3143 7356
grg n/a| 1 -3 -4 3 3 1 .17 34 14 | 146 -4233 3166 6765
iac n/a| 0 3 -7 41 -46 -45 -.10 23 23 | 806 -2478 3108 7935
jgx n/a| 1 0 4 11 15 1 -.28 29 29 | 43145 -4430 3169 7607
Table 2.2286.5 GPS week: 2286 Day: 5 MJD: 60251
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 2 0 12 -1 36 .08 27 18 | 41014 3135 3096 8934
esa n/a| 0 0 0 -17 -16 -12 -.11 24 17 | 9074 2737 3057 7423
gfz n/a| -1 1 0 16 -20 -22 -.11 26 14 | 0 3202 3131 8287
grg n/a| 0 -2 -3 -11 29 3 .13 22 15 | 50 3483 3136 7851
iac n/a| 3 2 -9 63 10 -35 -.22 28 22 | 3140 1988 3075 8855
jgx n/a| 0 0 9 27 33 34 -.35 28 28 | 43499 3278 3138 8329
Table 2.2286.6 GPS week: 2286 Day: 6 MJD: 60252
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 0 25 -30 54 .09 22 17 | 41105 -1832 2787 10304
esa n/a| 1 1 -1 -27 -4 -13 -.15 29 20 | 7977 -2295 2760 8853
gfz n/a| 0 1 2 6 1 -47 -.11 23 13 | 0 -1929 2799 9042
grg n/a| 0 -4 -1 -5 25 13 .14 27 19 | -181 -1664 2765 8625
iac n/a| 1 3 -11 42 -19 22 -.18 23 19 | 2129 -2319 2764 10024
jgx n/a| 0 2 0 15 49 29 -.27 33 29 | 44058 -1484 2780 9265
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 3.2286.0 GPS week: 2286 Day: 0 MJD: 60246
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 747 31 27 26 36 25 53 17 | 61 38 48 47 48 46 48
R02 | 958 8 15 15 22 16 12 8 | 40 53 45 36 41 40 42
R03 | 861 11 12 16 14 13 26 8 | 53 58 64 58 65 49 57
R04 | 619 6 13 14 18 9 27 7 | 55 47 55 47 50 39 51
R05 | 731 6 15 11 12 12 31 6 | 31 35 32 34 35 26 32
R07 | 1540 8 15 12 17 17 19 7 | 45 52 53 47 45 46 47
R08 | 980 12 15 19 15 16 18 9 | 39 43 57 43 48 44 44
R09E | 4410 13 14 13 28 27 23 10 | 70 70 62 76 68 66 68
R11E | 2095 11 10 14 16 22 24 7 | 30 35 39 32 33 39 32
R12E | 1706 9 12 14 15 21 21 7 | 94 98 97 98 95 95 96
R13E | 1110 33 29 76 39 43 37 28 | 42 38 93 45 50 39 42
R14E | 835 9 17 10 26 18 19 9 | 36 36 36 44 33 33 34
R15E | 2086 13 16 9 29 22 25 10 | 61 66 65 80 65 70 65
R16E | 1685 12 31 34 35 16 26 16 | 25 35 41 38 23 31 25
R17 | 1568 8 17 17 11 12 --- 7 | 67 63 73 69 70 --- 67
R18 | 773 12 24 9 13 9 29 8 | 53 69 55 58 59 53 57
R19 | 3598 49 82 35 65 27 44 33 | 97 62 119 98 101 70 91
R20 | 3579 49 94 41 89 50 40 39 | 115 81 106 106 79 88 93
R21 | 750 12 18 11 16 10 25 8 | 78 68 72 74 72 65 73
R22 | 4061 10 12 20 12 18 --- 8 | 39 43 36 46 39 --- 38
R24 | 783 10 12 12 23 14 15 8 | 62 65 55 69 58 61 60
XR25 |14088 12 19 --- --- 23 --- 15 | 24 34 --- --- 25 --- 26
XR26 |39070 62 --- 80 --- 594 --- 70 | 464 --- 611 --- 83 --- 490
------+-----------------------------------------+-------------------------------------
RMS | 2056 20 32 25 32 22 29 |T 73 54 87 59 55 52 72
WRMS | 2056 12 22 15 34 19 27 |NE 82 54 98 59 57 52 82
MEDI | 1540 12 15 14 18 18 25 |MD 53 52 55 47 50 46 51
Table 3.2286.1 GPS week: 2286 Day: 1 MJD: 60247
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 632 23 17 24 29 18 35 14 | 41 45 47 32 47 38 40
R02 | 927 8 15 9 10 15 16 6 | 29 35 34 36 29 34 32
R03 | 1466 10 11 18 17 15 16 8 | 33 38 32 30 33 33 30
R04 | 1153 9 9 13 17 19 22 7 | 36 44 44 28 37 32 36
R05 | 831 8 13 9 7 12 21 5 | 20 25 25 21 18 16 20
R07 | 1136 8 14 19 25 8 17 10 | 28 28 33 34 27 21 26
R08 | 990 20 11 23 14 11 17 10 | 24 34 43 33 26 35 31
R09E | 4293 13 15 15 22 25 18 9 | 64 67 60 59 69 66 61
R11E | 2950 12 15 20 12 24 19 9 | 29 39 41 32 30 34 33
R12E | 2718 13 11 11 15 33 26 7 | 67 71 70 79 60 80 70
R13E | 1623 35 43 53 25 36 54 23 | 39 67 102 51 45 63 53
R14E | 1316 10 14 17 23 17 15 9 | 40 45 39 42 37 36 38
R15E | 1381 10 16 18 28 26 17 11 | 88 93 90 96 94 84 89
R16E | 1403 15 28 18 20 19 16 11 | 29 37 33 31 29 31 27
R17 | 1551 7 13 7 12 18 --- 5 | 43 41 48 46 50 --- 44
R18 | 780 11 23 17 18 21 35 10 | 35 38 35 38 41 34 35
R19 | 2793 45 78 51 66 25 55 34 | 47 37 81 53 53 49 53
R20 | 4699 41 115 49 55 54 50 38 | 67 65 71 73 37 60 60
R21 | 834 8 25 9 16 15 30 8 | 55 51 64 62 52 51 57
R22 | 4233 10 14 10 14 17 16 7 | 29 39 35 34 33 39 32
R24 | 622 7 21 12 11 18 21 7 | 39 50 37 38 39 40 39
XR25 |15786 10 18 --- --- 27 --- 14 | 28 24 --- --- 19 --- 23
XR26 |35241 282 --- 366 --- 275 --- 322 | 253 --- 101 --- 48 --- 138
------+-----------------------------------------+-------------------------------------
RMS | 2208 19 35 24 26 23 29 |T 50 46 52 45 41 43 46
WRMS | 2208 13 22 16 26 21 29 |NE 50 39 48 39 36 37 43
MEDI | 1403 10 15 17 17 19 19 |MD 39 39 43 38 37 36 38
Table 3.2286.2 GPS week: 2286 Day: 2 MJD: 60248
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1214 23 21 26 18 18 38 13 | 49 50 50 59 54 36 50
R02 | 1780 12 11 10 18 18 18 7 | 31 33 36 44 29 25 34
R03 | 1615 11 18 9 12 16 17 7 | 42 40 42 45 43 42 40
R04 | 1643 17 13 7 22 13 16 9 | 39 28 32 28 31 23 30
R05 | 1463 8 14 11 12 14 12 6 | 29 32 30 36 30 28 29
R07 | 652 10 13 15 8 13 15 7 | 29 31 42 40 44 28 34
R08 | 1005 16 10 19 11 19 23 8 | 29 37 48 42 44 34 37
R09E | 4394 14 8 16 14 18 16 8 | 47 46 49 50 52 47 46
R11E | 1221 11 8 14 7 21 20 6 | 25 29 32 31 31 32 28
R12E | 2221 12 13 19 17 21 29 9 | 35 45 52 40 46 49 41
R13E | 2759 22 34 44 34 38 43 19 | 23 36 56 34 36 47 28
R14E | 897 11 14 16 29 18 23 10 | 37 41 42 48 32 34 38
R15E | 2002 11 15 21 20 25 15 9 | 79 80 77 75 76 79 76
R16E | 1292 9 22 17 18 18 14 9 | 32 47 42 31 28 43 34
R17 | 979 14 9 9 15 20 --- 7 | 53 46 45 44 53 --- 46
R18 | 658 11 25 17 12 19 14 9 | 44 54 41 52 52 50 46
R19 | 1839 27 89 50 83 26 50 36 | 83 59 106 78 78 74 77
R20 | 2967 42 100 50 46 45 23 35 | 75 58 102 85 56 86 74
R21 | 724 13 20 15 18 15 33 9 | 56 48 51 60 53 43 53
R22 | 2118 10 16 13 18 15 13 8 | 32 37 36 42 35 29 34
R24 | 1210 18 29 21 23 20 18 13 | 51 55 37 43 40 36 41
XR25 |16813 7 15 --- --- 22 --- 11 | 26 25 --- --- 23 --- 24
XR26 |14040 313 --- 410 --- 352 --- 358 | 435 --- 79 --- 61 --- 258
------+-----------------------------------------+-------------------------------------
RMS | 1869 17 34 23 27 22 25 |T 60 43 51 47 44 43 52
WRMS | 1869 15 23 16 22 19 24 |NE 68 42 51 49 45 41 56
MEDI | 1615 12 15 16 18 19 18 |MD 39 41 42 44 44 36 40
Table 3.2286.3 GPS week: 2286 Day: 3 MJD: 60249
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1249 23 40 16 19 35 80 14 | 38 35 27 33 30 36 29
R02 | 1708 8 16 9 17 19 19 7 | 21 25 24 30 35 26 22
R03 | 766 8 11 8 11 23 26 5 | 35 36 38 42 48 23 37
R04 | 1551 14 16 9 12 12 31 7 | 40 30 37 33 37 18 35
R05 | 1581 10 14 14 11 16 10 7 | 31 33 36 33 30 34 31
R07 | 950 7 16 23 12 26 25 9 | 36 29 52 34 39 25 38
R08 | 1766 14 15 17 8 18 22 8 | 24 30 41 32 39 26 30
R09E | 4517 12 14 17 9 22 17 7 | 62 63 59 57 60 57 60
R11E | 2555 12 11 13 15 15 18 7 | 24 29 30 40 27 31 29
R12E | 1956 10 21 17 15 27 25 9 | 38 40 45 37 44 44 38
R13E | 2147 32 24 36 15 33 32 16 | 23 40 59 45 41 41 38
R14E | 766 8 14 16 22 20 21 9 | 33 31 37 43 32 42 34
R15E | 1589 11 13 21 29 26 24 11 | 35 34 35 51 36 38 37
R16E | 1478 17 24 34 18 19 15 14 | 35 47 52 45 42 44 40
R17 | 1450 11 16 9 14 18 --- 7 | 64 56 60 54 63 --- 58
R18 | 612 7 35 14 14 25 21 10 | 46 63 43 47 54 44 47
R19 | 2506 50 81 43 50 17 68 31 | 96 51 115 89 90 85 88
R20 | 1845 22 116 32 38 23 51 31 | 87 29 104 107 79 65 82
R21 | 608 13 27 11 18 11 29 10 | 61 47 59 63 55 44 57
R22 | 1952 15 13 15 16 17 12 8 | 32 33 32 38 32 23 31
R24 | 1540 11 18 13 19 18 21 9 | 65 69 64 73 63 57 65
XR25 |13041 9 15 --- --- 20 --- 12 | 25 32 --- --- 31 --- 26
XR26 |25197 255 --- 316 --- 269 --- 284 | 343 --- 86 --- 61 --- 205
------+-----------------------------------------+-------------------------------------
RMS | 1869 18 36 21 21 22 33 |T 56 40 51 48 46 40 50
WRMS | 1869 15 31 15 16 21 33 |NE 65 39 54 50 49 38 55
MEDI | 1589 12 16 16 15 20 22 |MD 36 34 43 43 41 38 38
Table 3.2286.4 GPS week: 2286 Day: 4 MJD: 60250
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2019 36 35 9 31 19 56 16 | 45 33 38 36 32 40 34
R02 | 2537 10 8 8 9 15 16 5 | 22 20 22 27 22 18 21
R03 | 1039 16 14 10 18 16 26 8 | 25 35 39 41 30 25 33
R04 | 1240 9 11 5 7 12 27 4 | 28 23 24 29 27 19 25
R05 | 2036 10 14 6 8 14 20 5 | 29 31 32 33 30 27 30
R07 | 647 9 12 18 22 25 13 9 | 40 39 52 34 38 33 42
R08 | 1155 6 9 8 10 25 14 5 | 35 38 45 36 47 36 39
R09E | 4036 13 13 12 14 26 12 7 | 64 65 62 57 60 57 61
R11E | 3378 16 7 10 11 20 10 6 | 45 45 43 41 39 40 43
R12E | 625 13 29 8 43 19 11 13 | 105 108 107 115 107 101 107
R13E | 1435 34 38 29 53 46 46 21 | 32 33 55 93 77 45 46
R14E | 918 14 26 10 43 33 29 13 | 27 31 33 62 34 36 31
R15E | 1542 23 15 28 91 28 29 25 | 59 58 69 102 54 62 60
R16E | 859 11 17 25 61 18 23 18 | 39 48 41 68 39 53 41
R17 | 2144 13 18 8 14 17 --- 7 | 65 53 59 65 63 --- 59
R18 | 783 10 24 9 14 15 25 8 | 47 56 46 52 48 46 48
R19 | 1740 59 65 33 46 26 49 29 | 91 65 97 74 81 72 82
R20 | 842 37 61 13 21 23 46 20 | 78 39 67 64 65 56 58
R21 | 812 14 24 10 12 19 20 9 | 60 55 66 55 65 51 58
R22 | 2111 17 9 10 10 17 13 7 | 28 37 40 35 34 31 34
R24 | 977 16 14 16 19 15 28 9 | 65 58 53 67 52 44 58
XR25 |12609 13 13 --- --- 42 --- 13 | 27 35 --- --- 42 --- 29
XR26 |28608 314 --- 217 --- 162 --- 261 | 260 --- 93 --- 43 --- 172
------+-----------------------------------------+-------------------------------------
RMS | 1801 22 27 16 34 23 29 |T 57 45 53 56 49 44 52
WRMS | 1801 17 19 11 14 23 29 |NE 59 41 51 46 44 38 51
MEDI | 1435 14 14 10 18 19 23 |MD 45 39 46 55 43 40 43
Table 3.2286.5 GPS week: 2286 Day: 5 MJD: 60251
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1625 30 28 23 23 30 57 15 | 34 20 39 25 35 25 25
R02 | 2544 9 11 11 11 22 18 6 | 21 23 23 18 22 17 19
R03 | 858 10 10 11 15 17 25 7 | 25 35 39 29 32 23 30
R04 | 2004 12 11 9 10 17 26 6 | 32 29 29 34 27 19 29
R05 | 1878 12 9 8 5 18 22 5 | 23 26 22 24 25 17 22
R07 | 821 9 10 15 17 13 17 7 | 29 36 40 22 30 34 29
R08 | 479 10 16 12 19 20 13 8 | 29 31 27 21 34 26 25
R09E | 4261 14 7 13 10 22 15 6 | 56 51 45 59 59 54 52
R11E | 3104 15 14 15 11 17 15 8 | 25 23 35 29 22 22 26
R12E | 723 10 16 20 17 26 11 9 | 162 171 168 165 163 172 166
R13E | 2524 32 29 47 17 66 31 19 | 38 55 47 43 86 42 40
R14E | 1115 10 15 13 14 24 12 7 | 26 24 28 30 26 33 25
R15E | 975 13 18 11 18 25 25 9 | 60 58 61 65 53 58 58
R16E | 1089 17 21 15 13 24 12 10 | 27 37 31 33 24 37 29
R17 | 2397 7 18 8 18 18 --- 8 | 46 40 40 55 49 --- 44
R18 | 443 18 22 8 11 18 23 9 | 39 41 41 47 35 39 42
R19 | 599 58 68 41 48 34 60 31 | 60 64 74 59 70 38 58
R20 | 1577 82 43 77 62 61 48 39 | 72 57 77 73 40 54 54
R21 | 1162 17 14 17 11 20 17 8 | 46 39 33 39 45 48 37
R22 | 2563 13 10 14 16 11 10 8 | 20 25 35 29 27 19 25
R24 | 545 22 14 32 17 16 16 13 | 44 43 33 41 39 32 37
XR25 |10304 14 13 --- --- 31 --- 13 | 26 29 --- --- 34 --- 25
XR26 |27068 273 --- 264 --- 203 --- 269 | 155 --- 64 --- 32 --- 79
------+-----------------------------------------+-------------------------------------
RMS | 1869 27 24 26 22 28 28 |T 47 43 46 44 43 40 42
WRMS | 1869 18 17 14 15 22 28 |NE 43 35 41 36 36 30 36
MEDI | 1577 14 14 14 16 22 17 |MD 34 36 39 34 34 33 30
Table 3.2286.6 GPS week: 2286 Day: 6 MJD: 60252
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1986 31 24 17 23 15 65 14 | 65 37 49 41 53 30 47
R02 | 2045 7 11 13 12 18 12 6 | 30 35 37 27 38 28 31
R03 | 1088 13 12 12 18 19 32 8 | 42 53 54 61 53 34 51
R04 | 2245 12 14 11 18 15 26 8 | 45 43 42 39 40 32 41
R05 | 1098 8 18 14 16 17 12 8 | 31 45 40 37 32 31 36
R07 | 1183 15 15 7 10 12 11 7 | 47 45 48 41 43 42 44
R08 | 598 13 17 15 18 16 23 9 | 39 51 52 39 55 49 43
R09E | 5337 12 11 12 13 27 16 7 | 75 68 68 73 79 68 71
R11E | 2573 12 12 17 13 18 15 8 | 37 40 44 40 35 39 39
R12E | 509 12 16 16 16 43 19 8 | 141 139 143 131 125 149 138
R13E | 3078 20 35 41 23 25 40 18 | 40 56 60 44 51 58 42
R14E | 748 17 21 26 20 19 12 12 | 25 33 35 32 33 33 26
R15E | 2088 16 19 17 23 32 18 11 | 64 73 68 81 54 63 68
R16E | 1260 15 18 21 20 17 23 11 | 38 47 42 54 37 49 41
R17 | 1840 6 22 12 19 15 --- 9 | 83 74 85 87 82 --- 82
R18 | 726 11 25 12 14 13 16 9 | 63 78 64 69 68 58 67
R19 | 1181 63 74 34 74 19 90 36 | 106 76 128 120 105 72 105
R20 | 1262 49 80 64 67 57 51 37 | 119 90 131 89 96 92 99
R21 | 1658 6 12 9 15 16 20 6 | 84 81 84 89 80 77 84
R22 | 3239 12 16 11 13 12 12 7 | 36 39 42 47 38 35 39
R24 | 948 15 17 13 15 10 18 8 | 82 75 70 77 75 68 75
XR25 | 9826 10 15 --- --- 22 --- 12 | 32 39 --- --- 33 --- 33
XR26 |20962 283 --- 308 --- 220 --- 295 | 403 --- 134 --- 69 --- 252
------+-----------------------------------------+-------------------------------------
RMS | 2067 22 29 23 27 23 33 |T 75 59 69 62 59 55 67
WRMS | 2067 17 20 13 19 19 29 |NE 81 57 70 61 60 49 70
MEDI | 1658 13 17 14 18 18 18 |MD 47 51 54 54 53 49 47
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