[IGSREPORT-29737] Wk 2299 IGLOS Final Orbits
acc
acc at igs.org
Mon Feb 19 06:58:07 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2299 (Jan 28, 2024 - Feb 03, 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 2.2299.
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:
igl2299[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2299 in the SP3 format.
igl22997.sum Combination Report for GPS Week 2299.
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 | -10.2 ns
1 | -6.6 ns
2 | -4.5 ns
3 | -4.9 ns
4 | -7.4 ns
5 | -7.1 ns
6 | -8.4 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
----+--------+---------------
0 | COD | R26
0 | ESA | R26
0 | GFZ | R26
0 | GRG | R26
0 | IAC | R26
0 | JGX | R26
2 | COD | R26
2 | ESA | R26
2 | GFZ | R26
2 | GRG | R26
2 | IAC | R26
2 | JGX | R26
3 | COD | R26
3 | ESA | R26
3 | GFZ | R26
3 | GRG | R26
3 | IAC | R26
3 | JGX | R26
4 | COD | R26
4 | ESA | R26
4 | GFZ | R26
4 | GRG | R26
4 | IAC | R26
4 | JGX | R26
5 | COD | R26
5 | ESA | R26
5 | GFZ | R26
5 | GRG | R26
5 | IAC | R26
5 | JGX | R26
6 | COD | R26
6 | ESA | R26
6 | GFZ | R26
6 | GRG | R26
6 | IAC | R26
6 | JGX | R26
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2299, 1a.2299).
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 2.2299.0-6)
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 3.2299.0-6).
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 2299 summary. (Jan 28, 2024 - Feb 03, 2024)
Table 1.2299.a GPS week : 2299 MJD: 60337.0-60343.0
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 4 -14 -8 71 .13 25 19 | 14659 -600 3191 8071
| 1 0 1 8 16 28 .05 | 497 2289
esa n/a| -1 1 0 -30 -5 -18 -.22 29 20 | -4324 -746 3183 7696
| 0 1 1 7 11 27 .04 | 2422 2270
gfz n/a| 0 1 3 39 4 -13 -.07 28 16 | 0 -753 3230 7298
| 1 0 0 16 13 33 .11 | 0 2481
grg n/a| 2 -4 -3 22 -17 41 .41 29 23 | -6766 -802 3229 6861
| 1 1 3 19 17 40 .07 | 1290 2224
iac n/a| 0 1 -4 32 29 -42 -.12 23 22 | -5445 -425 3183 8038
| 1 1 1 23 23 85 .18 | 1716 976
jgx n/a| 0 1 -5 -16 13 -71 -.19 29 27 | 17400 -747 3247 7475
| 1 1 2 28 13 38 .06 | 777 2334
Table 1.2299.b GPS week : 2299 MJD: 60337.0-60343.0
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 | 19 20 18 19 19 22 22 |
R02 | 14 8 8 7 8 9 8 |
R03 | 9 10 8 7 9 8 10 |
R04 | 12 7 9 9 9 8 9 |
R05 | 15 9 7 8 7 8 9 |
R07 | 11 10 8 9 9 11 9 |
R08 | 9 9 9 10 10 11 10 |
R09 | 13 7 9 10 9 7 6 |
R11 | 7 10 10 9 9 9 8 |
R12 | 7 8 10 11 7 8 8 |
R13 | 12 16 18 19 20 19 24 |
R14 | 6 7 7 8 7 9 9 |
R15 | 10 10 8 8 8 10 10 |
R16 | 11 10 13 11 9 10 10 |
R17 | 10 12 11 10 12 9 14 |
R18 | 8 9 9 7 10 10 9 |
R19 | 23 19 18 17 13 17 21 |
R20 | 41 39 45 42 38 37 38 |
R21 | 12 9 10 9 8 8 9 |
R22 | 8 8 7 8 9 8 8 |
R24 | 10 8 10 8 10 11 11 |
R25 | 19 11 14 14 18 12 14 |
R26 | --- 19 --- --- --- --- --- |
Table 1.2299.c GPS week : 2299 MJD: 60337.0-60343.0
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 2299 0 | -26 -26 -102 -676 82 -5233 77.6 1571 1571 | -10154 0
brd 2299 1 | -87 -3 -65 116 -842 -9111 78.8 1776 1776 | -6605 0
brd 2299 2 | 39 -20 -67 833 -672 -10660 77.5 2016 2016 | -4517 0
brd 2299 3 | 80 -5 -81 1355 -393 -8066 78.9 2375 2375 | -4879 0
brd 2299 4 | -47 -92 -91 -728 -687 -7037 78.0 2249 2249 | -7409 0
brd 2299 5 | -70 -86 -6 -1368 -2267 -5469 79.0 2091 2091 | -7099 0
brd 2299 6 | -52 52 9 -1700 533 -7332 80.7 2078 2078 | -8439 0
-------------+------------------------------------------------------------+----------------
brd 2299 mean| -23 -26 -57 -309 -606 -7558 78.6 2022 2022 | -7014 0
brd 2299 sdev| 61 50 42 1127 879 1931 1.1 273 273 | 1958 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 2.2299.0 GPS week: 2299 Day: 0 MJD: 60337
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 -20 5 55 .17 28 19 | 14471 -3416 3278 9177
esa n/a| 0 2 -2 -29 -15 -16 -.19 35 25 | -5780 -3419 3266 8436
gfz n/a| -1 1 2 51 -7 -25 -.12 27 14 | 0 -4562 3271 8602
grg n/a| 3 -6 0 -6 9 3 .39 31 23 | -8080 -4281 3288 7859
iac n/a| 0 2 -1 46 49 -3 -.19 25 26 | -8161 -127 3258 9106
jgx n/a| -2 0 -10 -60 20 -26 -.12 27 27 | 17158 -4375 3193 8709
Table 2.2299.1 GPS week: 2299 Day: 1 MJD: 60338
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 6 -8 -25 130 .11 24 16 | 14374 -3078 3471 8250
esa n/a| -1 1 -1 -32 3 -70 -.20 30 24 | -3181 -2992 3480 8358
gfz n/a| 0 0 4 51 18 -21 -.24 28 15 | 0 -2651 3498 7624
grg n/a| 0 -4 -4 14 -30 19 .42 25 24 | -5390 -2396 3532 7330
iac n/a| -2 0 -5 29 24 59 .26 24 25 | -5064 -1099 3461 8189
jgx n/a| 0 0 -4 -39 14 -41 -.11 29 29 | 16036 -2286 3563 7861
Table 2.2299.2 GPS week: 2299 Day: 2 MJD: 60339
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 7 -20 18 78 .17 27 22 | 14103 269 3377 7552
esa n/a| -1 0 0 -29 -12 -34 -.20 29 19 | -1447 645 3339 7044
gfz n/a| -1 1 2 36 -11 -29 -.18 30 17 | 0 1396 3441 6592
grg n/a| 3 -4 -7 33 -21 41 .49 32 24 | -5027 779 3387 6164
iac n/a| 0 3 -2 -5 58 -200 -.14 23 21 | -3607 -213 3364 7501
jgx n/a| 0 2 -2 -14 8 -45 -.18 26 26 | 16885 371 3484 6895
Table 2.2299.3 GPS week: 2299 Day: 3 MJD: 60340
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 -9 -28 72 .16 28 21 | 14419 2704 2841 7160
esa n/a| -1 0 2 -32 -9 -19 -.22 24 15 | -3335 2712 2818 6927
gfz n/a| 1 1 3 22 -6 -48 -.06 27 17 | 0 2271 2868 6333
grg n/a| 3 -3 -7 21 0 70 .50 32 22 | -6073 2184 2870 5804
iac n/a| 0 3 -3 71 31 -4 -.29 22 20 | -3408 693 2837 7139
jgx n/a| 1 1 -3 3 28 -75 -.19 30 30 | 17672 2513 2900 6546
Table 2.2299.4 GPS week: 2299 Day: 4 MJD: 60341
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 -6 -6 52 .17 20 17 | 15332 -1767 3176 8705
esa n/a| -1 2 1 -17 -6 9 -.19 29 18 | -3835 -2262 3183 8400
gfz n/a| -1 1 3 54 4 -12 -.03 26 16 | 0 -2006 3236 7968
grg n/a| 3 -4 -3 7 -23 104 .37 26 21 | -6960 -1852 3243 7899
iac n/a| 0 1 -4 29 17 -96 -.19 24 17 | -4978 -2287 3174 8691
jgx n/a| 1 0 -7 -22 29 -134 -.25 29 27 | 18336 -1724 3284 8138
Table 2.2299.5 GPS week: 2299 Day: 5 MJD: 60342
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 4 -10 -14 46 .06 23 19 | 14526 1471 2909 7194
esa n/a| -1 2 0 -32 14 0 -.32 28 20 | -9003 853 2913 7333
gfz n/a| 1 1 4 12 18 -15 .08 29 17 | 0 1117 2972 6302
grg n/a| 3 -3 0 53 -39 60 .34 30 24 | -7610 786 2969 5990
iac n/a| 0 -1 -6 35 -11 -55 -.15 20 19 | -6009 -21 2905 7159
jgx n/a| 1 0 -4 -9 -2 -68 -.21 29 25 | 17672 1311 3008 6474
Table 2.2299.6 GPS week: 2299 Day: 6 MJD: 60343
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 3 -29 -4 65 .08 26 19 | 15388 -384 3286 8459
esa n/a| -1 -2 0 -42 -15 0 -.20 30 20 | -3689 -762 3288 7374
gfz n/a| 0 2 3 44 18 57 .03 28 17 | 0 -839 3324 7668
grg n/a| 2 -2 -2 30 -14 -11 .34 28 23 | -8223 -839 3314 6982
iac n/a| 0 0 -5 17 38 5 -.15 22 24 | -6890 76 3284 8484
jgx n/a| 0 2 -6 26 -2 -106 -.27 30 28 | 18045 -1045 3297 7707
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 3.2299.0 GPS week: 2299 Day: 0 MJD: 60337
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1779 41 43 36 16 36 39 18 | 84 41 79 60 50 44 56
XR02 | 1148 22 13 15 42 19 --- 14 | 168 173 167 175 163 --- 169
R03 | 967 14 11 15 28 11 19 9 | 68 59 56 71 60 53 59
R04 | 1074 15 16 9 41 22 27 11 | 68 68 67 81 62 66 67
R05 | 3515 16 16 10 65 47 20 14 | 56 55 59 101 65 47 59
R07 | 2141 12 14 12 43 29 21 11 | 68 60 66 85 67 63 65
R08 | 876 8 13 14 33 19 13 8 | 64 68 61 75 68 64 64
R09 | 704 23 16 32 12 11 32 12 | 36 44 62 48 44 32 42
R11 | 697 17 14 12 14 22 17 7 | 30 35 40 45 39 33 34
R12 | 863 13 8 7 25 16 6 6 | 40 43 39 34 40 41 38
R13 | 858 23 21 13 34 14 28 12 | 58 55 58 57 50 58 55
R14 | 865 8 8 10 13 14 15 5 | 48 48 45 48 49 47 46
R15 | 859 19 15 7 20 24 34 10 | 44 42 37 43 45 35 38
R16 | 1943 27 28 15 14 19 22 11 | 47 77 61 52 62 52 55
XR17 | 2799 22 14 13 20 20 --- 10 | 115 95 107 97 116 --- 103
R18 | 573 10 24 14 16 29 13 8 | 61 70 56 68 78 50 59
R19 | 2227 60 55 26 40 37 47 23 | 108 58 94 91 87 60 78
R20 | 1306 67 117 94 57 41 48 41 | 137 32 144 76 99 70 86
R21 | 1199 17 28 22 24 16 27 12 | 86 66 91 81 80 58 76
R22 | 1738 16 12 12 18 13 14 7 | 35 39 40 48 35 32 37
R24 | 2177 25 18 12 13 11 27 10 | 66 43 59 61 53 41 52
XR25 | 7631 19 18 --- --- 24 --- 18 | 68 61 --- --- 65 --- 63
------+-----------------------------------------+-------------------------------------
RMS | 1571 28 35 27 31 25 27 |T 69 60 70 70 67 49 63
WRMS | 1571 19 25 14 23 26 27 |NE 69 60 70 70 67 49 63
MEDI | 1148 17 16 13 24 19 22 |MD 64 55 61 61 62 50 59
Table 3.2299.1 GPS week: 2299 Day: 1 MJD: 60338
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2244 28 52 52 10 32 40 20 | 65 39 88 57 46 35 54
R02 | 1731 14 15 17 12 15 17 7 | 149 160 155 155 146 126 154
R03 | 2086 10 15 17 18 21 30 9 | 52 57 56 56 41 54 53
R04 | 1632 10 14 14 12 19 18 7 | 49 56 47 48 46 42 48
R05 | 2873 13 19 16 12 19 25 8 | 49 53 48 55 50 46 48
R07 | 1844 9 17 13 27 17 27 9 | 62 70 64 60 59 70 62
R08 | 1379 8 13 17 26 31 19 8 | 60 58 64 65 61 52 58
R09 | 897 14 17 15 10 19 13 7 | 37 48 41 40 46 46 41
R11 | 711 14 12 15 28 17 26 10 | 41 58 50 72 49 37 49
R12 | 865 21 9 8 23 20 7 8 | 47 56 49 48 53 54 50
R13 | 663 16 12 26 48 28 42 15 | 50 57 62 49 49 52 52
R14 | 1474 8 19 15 11 14 15 7 | 45 48 49 61 46 52 50
R15 | 623 27 15 17 15 17 20 10 | 48 57 58 43 52 46 49
R16 | 2096 21 23 15 19 19 20 10 | 50 76 65 60 55 64 61
XR17 | 2048 18 22 21 17 33 --- 11 | 85 71 93 80 81 --- 81
R18 | 1021 10 15 16 22 34 19 8 | 61 65 57 70 77 52 61
R19 | 3191 35 38 31 45 32 42 19 | 71 67 81 72 67 60 68
R20 | 2818 74 99 86 49 31 70 39 | 87 70 94 56 52 53 60
R21 | 1345 14 17 16 16 34 25 9 | 76 76 82 74 86 68 75
R22 | 1447 13 15 17 23 25 8 8 | 42 58 46 60 41 47 49
R24 | 1403 20 16 14 13 17 19 8 | 57 52 56 58 48 47 53
XR25 | 8623 10 11 --- --- 25 --- 10 | 60 64 --- --- 61 --- 62
XR26 |13500 16 --- --- 20 96 --- 18 | 78 --- --- 98 97 --- 4
------+-----------------------------------------+-------------------------------------
RMS | 1776 24 30 28 25 24 29 |T 61 64 66 65 61 55 58
WRMS | 1776 16 24 15 24 25 29 |NE 61 64 66 65 61 55 58
MEDI | 1632 14 15 16 18 21 20 |MD 57 58 58 60 52 52 53
Table 3.2299.2 GPS week: 2299 Day: 2 MJD: 60339
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2459 47 39 34 15 27 34 18 | 65 38 52 41 27 33 37
R02 | 2754 10 15 18 18 21 11 7 | 157 153 152 166 164 109 155
R03 | 2185 17 15 19 15 25 16 8 | 55 44 57 42 55 36 44
R04 | 2056 17 18 20 20 15 14 9 | 52 43 50 46 38 35 42
R05 | 1900 12 17 12 17 12 13 7 | 83 76 75 90 72 74 78
R07 | 1661 18 12 11 18 24 20 8 | 56 48 41 53 53 34 44
R08 | 3654 14 15 8 21 23 22 8 | 51 49 47 57 39 41 47
R09 | 859 21 16 14 15 26 19 8 | 44 40 51 43 27 44 43
R11 | 1759 15 12 24 29 12 15 10 | 28 39 39 52 33 30 35
R12 | 756 24 15 19 29 15 11 10 | 31 34 42 25 30 26 28
R13 | 973 41 16 18 52 32 42 18 | 38 35 36 39 36 33 33
R14 | 1858 11 10 15 17 20 12 6 | 35 37 35 35 32 35 34
R15 | 483 17 13 15 17 24 17 8 | 34 36 46 39 21 36 36
R16 | 1618 40 27 20 16 28 13 12 | 31 59 49 35 24 48 39
XR17 | 838 21 14 15 26 20 --- 11 | 112 95 102 97 103 --- 100
R18 | 1193 8 13 14 26 18 23 9 | 48 50 43 67 54 40 48
R19 | 2002 26 41 37 45 28 27 18 | 51 46 59 56 52 49 44
R20 | 4184 72 97 104 93 35 72 44 | 92 83 121 53 52 50 63
R21 | 1144 18 14 17 23 24 23 9 | 64 46 57 56 56 38 50
R22 | 1482 14 13 18 14 16 9 7 | 35 40 35 45 38 33 35
R24 | 884 15 16 27 16 16 17 9 | 56 51 69 67 64 51 57
XR25 | 9092 13 14 --- --- 28 --- 13 | 34 39 --- --- 32 --- 34
------+-----------------------------------------+-------------------------------------
RMS | 2015 27 29 30 32 23 26 |T 55 53 59 57 51 43 51
WRMS | 2015 22 19 17 24 21 26 |NE 55 53 59 57 51 43 51
MEDI | 1661 17 15 18 18 23 17 |MD 51 44 50 52 39 36 43
Table 3.2299.3 GPS week: 2299 Day: 3 MJD: 60340
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 2302 52 30 32 31 36 37 18 | 71 25 51 43 28 27 33
R02 | 2280 11 13 12 16 17 16 7 | 87 96 92 105 95 74 92
R03 | 2648 12 12 12 17 22 16 7 | 58 52 57 53 61 47 52
R04 | 3175 16 16 20 15 14 15 8 | 55 52 61 50 49 40 50
R05 | 3422 13 17 16 17 19 13 7 | 59 61 51 50 50 46 52
R07 | 923 8 14 22 18 28 21 8 | 60 50 66 67 76 44 56
R08 | 4519 23 13 18 23 14 25 10 | 61 53 44 67 59 50 53
R09 | 1591 24 10 15 25 13 23 10 | 30 36 28 38 24 27 29
R11 | 2798 16 13 19 25 20 8 8 | 25 34 33 38 33 23 25
R12 | 699 21 9 27 18 13 26 10 | 31 28 39 21 30 29 26
R13 | 1032 37 16 32 48 13 52 18 | 49 35 47 37 42 29 35
R14 | 2629 26 12 14 19 28 7 8 | 35 35 35 31 39 29 31
R15 | 730 24 14 16 15 15 9 8 | 38 30 30 32 36 29 29
R16 | 1013 30 20 23 12 26 15 10 | 47 45 48 40 38 38 40
XR17 | 851 14 14 17 22 15 --- 10 | 79 71 81 74 75 --- 75
R18 | 578 8 14 13 15 13 17 6 | 50 57 50 60 50 45 51
R19 | 2618 20 27 25 52 32 38 16 | 56 44 65 71 63 52 52
R20 | 4475 76 81 84 94 37 88 42 | 94 90 131 45 66 68 68
R21 | 868 22 11 16 19 14 19 8 | 60 43 52 46 49 35 46
R22 | 1789 18 15 15 18 26 13 8 | 25 31 32 39 28 29 28
R24 | 789 11 15 17 21 19 17 8 | 44 38 46 49 54 35 40
XR25 |14360 15 13 --- --- 19 --- 14 | 24 32 --- --- 32 --- 25
------+-----------------------------------------+-------------------------------------
RMS | 2374 28 24 27 32 22 30 |T 50 47 54 50 48 39 44
WRMS | 2374 21 15 17 22 20 30 |NE 50 47 54 50 48 39 44
MEDI | 1789 18 14 17 19 19 17 |MD 50 43 50 46 49 35 40
Table 3.2299.4 GPS week: 2299 Day: 4 MJD: 60341
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 942 43 46 24 29 32 43 19 | 77 33 52 63 37 35 47
R02 | 1133 10 17 10 18 11 21 7 | 152 152 155 151 146 69 150
R03 | 3527 12 15 19 22 17 20 9 | 59 50 49 62 58 43 51
R04 | 3317 14 13 19 16 20 22 8 | 55 48 54 50 45 45 49
R05 | 3529 13 11 14 12 10 19 7 | 68 63 59 69 60 54 62
R07 | 1687 12 19 17 15 18 21 8 | 59 45 51 60 57 43 51
R08 | 3844 20 18 11 18 17 26 9 | 58 51 54 53 61 43 51
R09 | 1700 17 15 17 21 9 15 8 | 36 26 39 26 27 31 31
R11 | 1851 13 15 11 25 17 24 9 | 13 33 21 35 20 24 21
R12 | 677 9 15 16 15 12 10 6 | 25 34 21 30 27 27 24
R13 | 1185 29 16 20 54 16 65 19 | 46 33 44 27 37 30 34
R14 | 2335 11 9 8 24 10 11 6 | 28 28 32 29 36 29 27
R15 | 848 20 12 11 12 9 14 7 | 34 33 32 32 34 30 30
R16 | 814 18 15 17 22 17 10 8 | 39 37 45 41 39 38 38
XR17 | 932 12 22 16 27 18 --- 11 | 93 79 96 85 98 --- 87
R18 | 683 14 15 18 21 17 28 9 | 45 53 54 62 49 33 48
R19 | 2069 20 28 22 30 39 24 12 | 41 54 58 69 35 46 48
R20 | 4414 35 103 95 51 69 66 37 | 56 71 117 98 87 39 60
R21 | 936 22 12 10 18 17 16 8 | 54 43 41 43 49 32 41
R22 | 2100 17 19 11 26 16 16 9 | 29 32 33 49 29 31 31
R24 | 948 18 17 23 17 21 25 10 | 36 42 55 43 49 41 39
XR25 | 8178 15 20 --- --- 22 --- 17 | 31 36 --- --- 32 --- 30
------+-----------------------------------------+-------------------------------------
RMS | 2248 20 29 26 26 24 29 |T 51 48 55 55 50 38 47
WRMS | 2248 17 18 16 21 17 27 |NE 51 48 55 55 50 38 47
MEDI | 1687 15 15 17 21 17 21 |MD 46 42 51 49 45 35 41
Table 3.2299.5 GPS week: 2299 Day: 5 MJD: 60342
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 829 41 60 27 47 29 38 22 | 77 39 67 90 46 35 55
R02 | 848 7 22 19 16 11 16 8 | 130 139 126 128 131 75 128
R03 | 3578 12 10 15 16 16 24 8 | 52 48 55 59 51 38 49
R04 | 2395 12 12 13 21 12 20 8 | 52 46 39 49 45 38 43
R05 | 3424 14 13 14 17 11 23 8 | 56 50 66 64 54 47 55
R07 | 2242 22 24 15 18 20 25 10 | 56 35 47 49 42 33 42
R08 | 3748 21 17 23 22 10 23 10 | 51 44 36 54 41 40 43
R09 | 1806 13 13 18 12 10 11 7 | 23 16 27 19 19 28 20
R11 | 882 9 15 17 25 14 23 9 | 17 26 22 20 21 39 19
R12 | 723 20 13 12 19 11 14 8 | 17 23 24 21 22 24 18
R13 | 1193 25 19 20 51 21 67 19 | 32 38 40 37 42 30 30
R14 | 3556 9 10 29 22 19 17 9 | 22 31 44 17 29 18 25
R15 | 859 24 16 14 15 28 26 10 | 23 22 17 19 38 13 14
R16 | 699 30 17 16 15 14 18 10 | 27 33 31 22 21 25 23
XR17 | 1015 11 17 13 22 17 --- 9 | 90 87 99 96 97 --- 92
R18 | 695 15 10 18 33 25 20 10 | 36 40 50 54 50 35 40
R19 | 2513 26 39 40 37 31 27 17 | 47 33 55 33 32 48 37
R20 | 2002 56 79 95 65 41 64 36 | 52 54 81 40 34 62 38
R21 | 755 12 16 14 15 10 17 7 | 46 42 49 47 46 38 43
R22 | 2189 13 13 12 25 15 12 7 | 30 32 30 34 31 30 29
R24 | 803 14 12 20 36 24 27 11 | 77 73 73 76 70 75 73
XR25 |10342 9 13 --- --- 17 --- 11 | 36 32 --- --- 36 --- 33
------+-----------------------------------------+-------------------------------------
RMS | 2090 23 28 29 30 20 29 |T 47 44 51 48 45 38 43
WRMS | 2090 19 20 17 24 19 25 |NE 47 44 51 48 45 38 43
MEDI | 1193 14 15 17 22 16 23 |MD 46 38 47 40 42 35 38
Table 3.2299.6 GPS week: 2299 Day: 6 MJD: 60343
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 764 49 68 21 29 21 25 21 | 110 43 80 86 63 54 70
R02 | 524 6 22 17 11 17 16 7 | 166 172 161 167 166 94 165
R03 | 3281 15 20 17 20 16 29 10 | 74 63 69 77 65 50 65
R04 | 2014 16 21 15 16 14 24 9 | 76 74 74 68 64 60 68
R05 | 3097 17 13 14 16 16 21 8 | 78 71 82 83 77 59 73
R07 | 2379 15 18 19 15 15 17 8 | 74 59 72 65 71 52 63
R08 | 3219 12 19 15 29 11 22 10 | 70 64 60 77 62 60 65
R09 | 1844 13 10 11 11 11 7 5 | 30 31 40 30 27 29 30
R11 | 1318 19 14 15 14 13 16 8 | 30 30 40 40 37 35 33
R12 | 914 22 14 11 9 17 15 7 | 33 34 34 26 34 29 29
R13 | 2148 32 24 26 74 18 67 24 | 55 53 50 44 54 43 47
R14 | 4426 10 11 20 27 29 9 8 | 43 50 56 43 60 44 46
R15 | 1310 17 16 20 13 19 26 9 | 48 46 51 43 53 33 41
R16 | 986 18 17 19 21 20 27 10 | 56 57 60 48 49 44 50
XR17 | 1024 13 19 25 36 14 --- 14 | 123 115 124 124 122 --- 120
R18 | 727 11 14 23 24 29 18 9 | 60 66 62 74 73 52 61
R19 | 1044 37 51 39 34 26 39 20 | 73 45 70 60 52 47 52
R20 | 1564 65 81 93 56 29 74 37 | 87 51 111 48 58 80 53
R21 | 690 20 14 20 17 16 17 9 | 66 51 59 56 59 46 54
R22 | 2513 14 15 16 17 9 12 7 | 39 48 41 42 45 37 39
R24 | 1146 22 15 21 23 56 21 10 | 55 47 42 54 62 50 47
XR25 | 8198 13 14 --- --- 21 --- 14 | 41 38 --- --- 39 --- 39
------+-----------------------------------------+-------------------------------------
RMS | 2077 26 30 28 28 22 30 |T 66 59 68 64 63 49 59
WRMS | 2077 19 20 17 23 24 28 |NE 66 59 68 64 63 49 59
MEDI | 1318 16 16 19 20 17 21 |MD 60 51 60 56 60 47 52
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