[IGSREPORT-29770] Wk 2302 IGLOS Final Orbits
acc
acc at igs.org
Sat Mar 9 02:32:17 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2302 (Feb 18, 2024 - Feb 24, 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 2.2302.
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:
igl2302[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2302 in the SP3 format.
igl23027.sum Combination Report for GPS Week 2302.
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 | -2.3 ns
1 | -4.3 ns
2 | 0.9 ns
3 | -2.0 ns
4 | -1.4 ns
5 | 1.9 ns
6 | 3.1 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
----+--------+---------------
1 | GFZ | 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 1.2302, 1a.2302).
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 2.2302.0-6)
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 3.2302.0-6).
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 2302 summary. (Feb 18, 2024 - Feb 24, 2024)
Table 1.2302.a GPS week : 2302 MJD: 60358.0-60364.0
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 1 2 -8 -16 73 .10 21 16 | 7947 -585 4007 23485
| 0 0 0 15 14 23 .03 | 7512 2397
esa n/a| 0 0 1 -26 -12 -28 -.15 27 18 | 2471 -384 3297 7926
| 1 0 1 15 12 24 .04 | 5279 2077
gfz n/a| 0 0 3 45 14 -25 -.02 27 19 | 0 -438 3313 7248
| 1 1 1 20 24 41 .04 | 0 2321
grg n/a| 2 -3 -3 5 -11 0 .33 28 22 | 687 -489 4008 23218
| 0 1 2 24 26 27 .05 | 8474 2265
iac n/a| 0 0 -3 6 31 -10 -.18 26 21 | 2504 415 4057 24449
| 1 1 2 27 13 72 .04 | 8837 1537
jgx n/a| -1 0 -4 2 16 -48 -.21 25 24 | 8064 -444 3263 7122
| 1 0 2 23 15 74 .03 | 1439 2294
Table 1.2302.b GPS week : 2302 MJD: 60358.0-60364.0
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 | 20 19 16 20 16 16 17 |
R02 | 7 8 9 6 7 7 9 |
R03 | 9 9 8 9 10 8 6 |
R04 | 8 9 10 9 8 8 10 |
R05 | 8 9 10 9 7 8 9 |
R07 | 9 10 7 8 8 9 8 |
R08 | 9 9 7 6 9 10 9 |
R09 | 7 7 7 8 8 7 7 |
R11 | 8 9 8 8 7 12 9 |
R12 | 7 8 7 8 9 11 10 |
R13 | 16 19 20 14 15 17 14 |
R14 | 6 6 5 6 8 7 6 |
R15 | 10 8 7 8 9 7 9 |
R16 | 9 10 9 8 9 10 7 |
R17 | 10 12 9 8 9 9 15 |
R18 | 9 10 8 7 9 7 7 |
R19 | 17 30 20 21 21 22 21 |
R20 | 31 29 30 27 33 37 34 |
R21 | 8 7 8 8 7 9 11 |
R22 | 8 8 7 8 8 8 9 |
R24 | 8 27 11 9 9 8 17 |
R26 | 18 9 8 19 17 13 10 |
Table 1.2302.c GPS week : 2302 MJD: 60358.0-60364.0
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 2302 0 | -10 69 223 14 1971 -264 79.8 1766 1766 | -2305 0
brd 2302 1 | -20 43 113 -1382 1878 3252 80.8 1450 1450 | -4349 0
brd 2302 2 | 41 69 72 -993 1618 8710 81.7 1434 1434 | 948 0
brd 2302 3 | 0 31 24 -272 484 9898 81.1 1626 1626 | -2022 0
brd 2302 4 | -16 42 58 -585 108 11990 80.2 1769 1769 | -1408 0
brd 2302 5 | 4 42 73 -283 1599 1703 81.7 2369 2369 | 1859 0
brd 2302 6 | 7 35 -84 475 1626 2996 79.9 2194 2194 | 3139 0
-------------+------------------------------------------------------------+----------------
brd 2302 mean| 0 47 68 -432 1326 5469 80.7 1801 1801 | -591 0
brd 2302 sdev| 20 15 92 620 725 4667 .8 357 357 | 2647 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 2.2302.0 GPS week: 2302 Day: 0 MJD: 60358
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 -12 -28 104 .13 18 14 | 4217 -742 3215 7242
esa n/a| 0 0 3 -7 -8 5 -.18 31 19 | -504 -796 3216 7224
gfz n/a| 1 -2 3 49 39 12 -.02 25 15 | 0 -791 3222 7012
grg n/a| 0 -4 -1 2 -53 -11 .35 28 26 | -6264 -695 3227 6976
iac n/a| -1 -3 -5 -8 32 135 -.21 26 19 | -4490 276 3201 7549
jgx n/a| 0 0 -8 -19 15 -155 -.22 22 21 | 9719 -1838 2852 5836
Table 2.2302.1 GPS week: 2302 Day: 1 MJD: 60359
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 -4 -20 99 .07 22 15 | -6355 -4447 2817 15127
esa n/a| 1 0 -2 -45 -24 -14 -.20 30 21 | -1167 -3148 2798 8092
gfz n/a| 0 0 5 32 24 15 .02 35 19 | 0 -4303 2834 8147
grg n/a| 2 -2 -1 42 0 -22 .22 29 24 | -15055 -4206 2830 14800
iac n/a| 0 1 -2 18 23 -62 -.20 28 30 | -14001 -1674 2813 15192
jgx n/a| -3 1 -5 27 18 -111 -.22 29 28 | 6756 -3738 2750 8043
Table 2.2302.2 GPS week: 2302 Day: 2 MJD: 60360
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 -14 -24 42 .13 19 13 | 14496 3549 5236 44026
esa n/a| 0 1 1 -38 -5 -16 -.17 26 20 | 4415 3480 3908 7874
gfz n/a| 0 1 3 21 36 6 -.08 25 18 | 0 3287 3900 7264
grg n/a| 1 -1 -2 32 6 29 .33 27 24 | 7831 3149 5234 44045
iac n/a| 0 0 -5 -17 22 -31 -.10 24 20 | 9843 3140 5346 45888
jgx n/a| 0 1 -6 22 12 -65 -.20 25 23 | 6956 3494 3978 7253
Table 2.2302.3 GPS week: 2302 Day: 3 MJD: 60361
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 1 -27 -1 84 .09 20 16 | 13904 34 4981 41158
esa n/a| 2 1 1 -41 -12 -52 -.13 25 19 | 776 -246 2981 8343
gfz n/a| -1 -1 4 32 -33 -28 .03 24 19 | 0 166 2981 7534
grg n/a| 1 -5 -4 -10 3 -31 .31 24 22 | 5709 53 4976 41094
iac n/a| 0 0 -4 44 48 -43 -.20 27 21 | 9430 -498 5117 42978
jgx n/a| -1 1 -1 19 9 -56 -.15 22 22 | 6739 325 2999 7512
Table 2.2302.4 GPS week: 2302 Day: 4 MJD: 60362
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 6 -27 54 .13 20 15 | 14341 -1750 5004 43289
esa n/a| 0 0 3 -13 -4 -38 -.18 25 17 | -4534 -2043 3421 9286
gfz n/a| 1 1 3 52 7 -46 -.03 23 16 | 0 -1730 3413 7360
grg n/a| 3 -2 -5 -25 -6 43 .36 27 19 | 7977 -1906 5017 43250
iac n/a| -3 -1 -5 36 43 -47 -.18 26 20 | 8954 -369 5124 45169
jgx n/a| 0 1 -4 -32 3 -30 -.22 27 27 | 7475 -1230 3333 7469
Table 2.2302.5 GPS week: 2302 Day: 5 MJD: 60363
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 1 3 14 -21 65 .09 25 19 | 8036 -932 3341 6825
esa n/a| 0 0 2 -21 0 -19 -.09 24 15 | 9236 -95 3310 6897
gfz n/a| -1 0 2 83 19 -38 -.03 30 27 | 0 -428 3360 6782
grg n/a| 2 -2 -8 -16 -43 -4 .38 28 21 | 2031 -512 3349 6379
iac n/a| 0 0 1 -27 9 -59 -.16 25 20 | 3892 703 3339 7276
jgx n/a| -3 0 -2 -7 49 9 -.23 24 24 | 10130 -1004 3316 7002
Table 2.2302.6 GPS week: 2302 Day: 6 MJD: 60364
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 -21 8 61 .08 24 17 | 6995 192 3460 6733
esa n/a| 0 0 2 -19 -34 -63 -.10 25 16 | 9081 160 3448 7767
gfz n/a| 0 0 3 44 7 -98 -.02 26 20 | 0 731 3484 6640
grg n/a| 2 -3 -4 11 13 -6 .37 30 20 | 2584 693 3425 5987
iac n/a| 0 0 -5 0 40 33 -.22 27 21 | 3904 1330 3461 7094
jgx n/a| -1 0 0 7 4 70 -.20 23 23 | 8678 882 3617 6744
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 3.2302.0 GPS week: 2302 Day: 0 MJD: 60358
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1490 28 62 24 56 17 28 20 | 105 64 89 112 83 70 84
R02 | 649 11 21 11 15 11 15 7 | 54 68 54 60 54 52 55
R03 | 779 8 16 15 28 17 20 8 | 64 61 66 78 70 50 61
R04 | 716 10 15 16 20 18 15 7 | 78 74 85 80 71 74 77
R05 | 761 12 14 14 20 14 20 8 | 62 53 57 57 60 46 55
R07 | 782 9 25 16 21 20 16 8 | 74 64 76 81 69 56 69
R08 | 796 12 15 14 21 19 22 8 | 62 63 63 68 64 48 60
R09 | 3016 12 12 16 13 21 12 6 | 32 35 42 35 42 41 35
R11 | 1770 11 13 16 20 14 16 7 | 28 29 34 40 35 24 28
R12 | 648 16 12 12 20 10 11 7 | 52 60 57 42 51 51 51
R13 | 793 19 21 20 57 22 37 16 | 74 74 80 66 78 57 71
R14 | 1087 11 12 11 11 18 10 5 | 55 66 61 63 52 60 60
R15 | 655 19 17 18 15 11 23 9 | 74 72 68 61 68 56 66
R16 | 747 17 18 19 16 16 22 9 | 91 97 94 81 91 78 87
XR17 | 2936 8 21 18 21 21 --- 9 | 120 118 120 118 114 --- 118
R18E | 1866 10 20 23 25 22 12 9 | 62 66 60 65 61 61 61
R19E | 2602 22 27 52 35 54 30 17 | 79 68 92 72 73 66 69
R20E | 4001 43 100 70 47 70 45 31 | 112 101 130 114 117 115 104
R21E | 1233 14 20 15 16 20 14 8 | 62 62 63 63 66 62 61
R22E | 3544 14 15 15 26 24 11 8 | 48 51 56 65 59 51 52
R24E | 981 15 18 13 19 17 16 8 | 428 427 425 420 420 411 422
XR26 |12757 20 --- 31 27 120 --- 18 | 47 --- 9999 52 85 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1765 18 31 25 28 26 22 |T 84 84 89 86 85 76 81
WRMS | 1765 14 19 15 26 19 21 |NE 67 66 69 68 67 54 64
MEDI | 981 12 18 16 20 18 16 |MD 62 66 66 65 68 56 61
Table 3.2302.1 GPS week: 2302 Day: 1 MJD: 60359
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1137 35 67 14 28 21 19 19 | 78 50 63 69 72 62 62
R02 | 712 7 15 12 16 13 23 7 | 44 50 50 54 47 35 45
R03 | 677 6 13 13 24 14 24 8 | 43 44 48 60 48 32 45
R04 | 667 10 22 11 21 23 20 8 | 53 64 58 64 57 52 56
R05 | 1177 16 14 17 17 13 24 9 | 44 39 29 37 31 31 35
R07 | 1425 21 20 20 9 27 20 9 | 50 40 40 43 57 31 40
R08 | 887 9 17 18 21 16 18 8 | 43 46 28 52 40 36 40
R09 | 1219 10 16 18 10 24 9 6 | 24 30 29 27 32 31 25
R11 | 1472 13 14 23 23 22 18 9 | 29 33 38 38 44 26 30
R12 | 937 13 11 22 14 12 17 8 | 41 46 46 41 43 34 40
R13 | 1241 27 24 30 58 13 46 19 | 57 68 54 60 65 46 56
R14 | 1232 11 18 9 10 17 11 6 | 40 58 48 45 38 42 46
R15 | 575 17 12 12 7 10 26 8 | 58 64 55 58 57 46 55
R16 | 1107 20 21 14 13 14 28 10 | 71 90 77 63 67 62 71
XR17 | 1191 10 19 19 29 28 --- 11 | 71 75 69 71 57 --- 69
R18E | 934 11 15 19 33 18 9 9 | 35 36 39 51 32 32 36
R19E | 1030 36 48 109 30 37 52 30 | 63 61 153 64 55 65 72
R20E | 4007 41 61 81 33 57 65 29 | 76 87 107 74 81 98 81
R21E | 647 8 16 17 16 19 16 7 | 24 30 33 29 33 28 27
R22E | 2266 16 14 18 15 21 14 7 | 35 40 40 42 39 38 37
R24E | 1559 47 57 39 74 78 42 26 | 544 526 541 511 539 510 526
XR26 |10731 9 --- 6560 7 103 --- 8 | 41 --- 9999 40 57 --- 38
------+-----------------------------------------+-------------------------------------
RMS | 1450 22 30 35 29 28 29 |T 71 75 78 72 72 66 69
WRMS | 1450 15 21 19 24 30 28 |NE 49 53 48 51 50 40 47
MEDI | 1137 13 17 18 17 19 20 |MD 44 50 48 52 48 36 45
Table 3.2302.2 GPS week: 2302 Day: 2 MJD: 60360
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 773 29 55 22 20 21 20 16 | 81 47 82 70 53 56 67
R02 | 772 13 21 26 12 17 17 9 | 50 53 36 48 36 36 43
R03 | 774 12 15 12 19 13 15 7 | 58 46 40 59 52 40 48
R04 | 600 9 19 16 20 16 29 9 | 59 59 58 65 48 46 55
R05 | 1053 14 27 17 25 19 12 9 | 39 55 49 36 30 34 38
R07 | 1146 8 17 17 10 26 9 6 | 55 41 61 51 67 50 51
R08 | 951 8 15 14 17 13 17 7 | 48 47 53 58 46 37 46
R09 | 2051 11 14 8 12 14 18 6 | 21 31 25 19 25 30 23
R11 | 1337 10 13 23 19 25 10 7 | 28 30 38 29 44 29 27
R12 | 860 10 15 19 12 14 8 6 | 46 53 55 47 44 49 49
R13 | 1530 21 19 15 63 19 62 20 | 74 68 64 79 78 38 64
R14 | 1076 8 12 10 12 10 6 5 | 40 45 43 36 39 43 40
R15 | 492 12 19 11 12 19 10 6 | 51 65 51 58 46 58 55
R16 | 956 21 19 12 13 13 23 9 | 77 72 72 76 65 62 71
XR17 | 735 8 16 16 19 15 --- 8 | 81 82 84 84 78 --- 81
R18E | 899 13 20 13 22 10 11 8 | 42 53 49 54 42 52 48
R19E | 813 33 36 24 56 57 45 19 | 63 64 62 75 52 63 59
R20E | 1895 52 58 82 46 55 56 30 | 69 70 109 65 75 84 66
R21E | 737 10 13 23 20 23 11 8 | 39 47 47 50 47 46 43
R22E | 2439 13 12 18 14 13 12 7 | 33 36 36 46 38 35 35
R24E | 3560 13 24 20 30 18 15 10 | 192 203 204 177 189 188 192
XR26 |17176 8 --- --- 9 97 --- 8 | 17 --- --- 25 61 --- 19
------+-----------------------------------------+-------------------------------------
RMS | 1433 19 26 25 27 24 25 |T 57 60 62 59 57 53 55
WRMS | 1433 13 20 18 24 20 23 |NE 51 52 54 52 50 43 48
MEDI | 951 12 19 17 19 17 15 |MD 50 53 53 54 47 46 48
Table 3.2302.3 GPS week: 2302 Day: 3 MJD: 60361
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 884 38 62 28 27 10 30 19 | 79 23 76 70 54 41 54
R02 | 1226 7 12 19 8 11 12 6 | 36 35 37 40 29 31 35
R03 | 1458 7 17 12 25 13 23 8 | 56 48 56 74 52 43 54
R04 | 693 12 17 17 24 19 20 9 | 56 43 46 65 51 43 49
R05 | 1272 13 18 16 12 16 24 8 | 48 41 47 38 41 23 38
R07 | 1210 7 16 17 24 12 14 8 | 51 42 64 69 54 46 52
R08 | 1165 13 10 16 12 21 10 6 | 43 44 53 48 53 45 45
R09 | 1932 16 16 15 11 12 14 7 | 24 39 38 36 27 27 31
R11 | 1810 10 18 24 10 13 13 8 | 31 34 43 37 41 34 34
R12 | 885 8 14 22 24 9 10 8 | 55 60 64 40 57 49 53
R13 | 1607 18 18 23 44 16 30 13 | 83 66 85 70 83 59 74
R14 | 750 4 8 12 13 12 19 6 | 46 47 47 55 44 39 46
R15 | 491 12 12 17 14 16 24 8 | 50 44 51 50 40 32 44
R16 | 1667 13 14 22 14 13 16 8 | 69 71 61 67 64 58 64
XR17 | 1349 12 13 18 13 17 --- 8 | 124 124 122 125 122 --- 123
R18E | 1096 8 18 13 18 16 13 7 | 67 68 65 72 62 64 66
R19E | 2374 48 36 33 52 59 35 21 | 82 80 81 84 79 70 73
R20E | 1476 48 60 65 38 82 52 26 | 79 71 118 74 79 85 77
R21E | 1223 12 11 18 19 27 14 7 | 58 56 60 55 58 57 56
R22E | 2733 17 16 16 17 14 13 8 | 29 39 37 43 39 38 35
R24E | 3400 13 18 23 22 22 15 9 | 146 136 141 147 132 141 141
XR26 |14935 17 --- --- 21 91 --- 18 | 27 --- --- 40 67 --- 27
------+-----------------------------------------+-------------------------------------
RMS | 1625 20 25 24 24 27 22 |T 60 57 66 63 60 51 57
WRMS | 1625 16 19 19 22 21 22 |NE 54 50 59 57 54 40 51
MEDI | 1272 12 16 18 18 16 15 |MD 55 47 60 55 54 43 52
Table 3.2302.4 GPS week: 2302 Day: 4 MJD: 60362
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1788 32 51 23 21 22 19 16 | 78 48 80 71 56 54 63
R02 | 1408 12 16 11 8 18 19 7 | 35 45 36 42 37 31 36
R03 | 719 12 20 20 17 11 26 9 | 52 32 56 58 46 27 44
R04 | 642 16 15 11 18 9 18 7 | 54 47 46 64 52 52 51
R05 | 1482 15 14 10 15 24 13 6 | 41 36 34 39 45 35 35
R07 | 1379 8 12 15 23 13 15 7 | 52 52 56 59 54 41 51
R08 | 1199 18 11 19 17 20 21 9 | 44 45 45 53 44 37 43
R09 | 1757 15 11 16 21 17 10 7 | 26 27 36 38 25 30 29
R11 | 2319 11 10 17 8 17 19 6 | 29 30 33 29 32 23 27
R12 | 1076 13 18 15 25 24 16 9 | 51 56 43 43 65 53 48
R13 | 910 28 19 21 45 29 33 15 | 79 53 66 65 77 44 63
R14 | 766 10 13 20 16 11 21 8 | 48 57 63 46 52 39 50
R15 | 501 20 17 14 13 18 19 8 | 53 43 41 45 39 42 43
R16 | 2281 18 17 19 18 21 10 8 | 65 68 76 67 59 65 66
XR17 | 1725 9 16 16 20 16 --- 9 | 76 75 79 85 72 --- 77
R18E | 911 10 16 19 31 21 10 9 | 66 70 62 69 62 63 64
R19E | 2990 43 41 34 52 51 35 20 | 93 77 84 82 68 76 75
R20E | 3413 35 65 69 69 68 86 32 | 74 80 90 84 81 90 73
R21E | 1197 9 11 13 18 14 14 6 | 42 39 48 48 43 39 42
R22E | 2206 16 11 16 14 13 14 7 | 34 48 45 46 40 37 40
R24E | 2583 16 19 18 15 14 16 8 | 181 186 192 189 181 172 183
XR26 |76118 13 --- --- 20 94 --- 16 | 24 --- --- 40 54 --- 28
------+-----------------------------------------+-------------------------------------
RMS | 1768 20 25 23 27 26 27 |T 58 57 62 61 58 52 55
WRMS | 1768 15 17 16 19 20 27 |NE 50 47 52 52 50 40 47
MEDI | 1408 15 16 17 18 18 18 |MD 52 48 56 53 52 41 48
Table 3.2302.5 GPS week: 2302 Day: 5 MJD: 60363
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1507 50 29 32 20 27 17 16 | 71 39 35 44 34 45 43
R02 | 1709 13 10 19 18 20 13 7 | 36 45 37 36 33 41 37
R03 | 1715 16 17 16 18 29 14 8 | 46 53 51 44 61 49 46
R04 | 644 18 17 17 14 14 11 8 | 52 45 56 55 52 46 49
R05 | 2645 17 11 18 16 12 15 7 | 41 33 32 36 31 25 31
R07 | 1196 21 11 11 14 21 26 9 | 51 43 41 44 49 34 40
R08 | 878 22 20 19 22 13 17 10 | 45 48 36 38 35 41 40
R09 | 2453 15 11 18 10 12 13 6 | 22 28 35 28 22 29 25
R11 | 2212 19 11 37 22 11 28 12 | 21 37 55 38 33 22 31
R12 | 1269 14 14 25 32 21 16 10 | 44 43 52 23 32 29 36
R13 | 2407 25 13 39 47 26 35 16 | 51 31 56 35 45 54 38
R14 | 754 9 6 24 16 20 8 6 | 39 34 47 28 33 37 35
R15 | 582 13 9 19 13 22 17 7 | 51 51 60 51 38 43 49
R16 | 1776 23 25 17 14 18 12 9 | 61 67 60 51 49 60 58
XR17 | 2024 11 14 18 18 20 --- 9 | 64 54 60 64 54 --- 58
R18E | 1266 9 13 22 17 17 11 7 | 63 64 56 70 67 65 63
R19E | 4624 48 42 49 43 44 33 21 | 68 65 71 65 60 64 56
R20E | 6022 53 78 78 80 61 71 36 | 83 99 112 95 88 93 82
R21E | 995 11 11 21 14 11 23 8 | 26 32 43 35 34 38 32
R22E | 3332 20 12 22 10 14 16 8 | 38 45 51 48 49 43 43
R24E | 853 10 14 26 20 20 10 8 | 285 283 284 282 284 279 282
XR26 |>>>>> 13 --- --- 13 79 --- 13 | 28 --- --- 37 77 --- 32
------+-----------------------------------------+-------------------------------------
RMS | 2368 25 24 30 28 25 24 |T 58 59 63 56 57 56 54
WRMS | 2368 19 15 27 21 20 24 |NE 45 43 47 40 42 39 40
MEDI | 1709 16 13 21 17 20 16 |MD 46 45 52 44 45 43 40
Table 3.2302.6 GPS week: 2302 Day: 6 MJD: 60364
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 776 49 35 21 27 28 20 16 | 92 68 70 69 59 59 67
R02 | 1436 10 26 18 19 19 9 9 | 49 69 52 48 44 44 51
R03 | 2082 10 8 15 8 18 12 5 | 65 62 70 64 60 53 62
R04 | 1473 18 18 23 16 20 20 9 | 74 73 84 77 83 70 74
R05 | 2623 12 10 15 21 15 24 8 | 49 49 46 56 52 39 45
R07 | 802 10 16 15 18 22 19 8 | 71 62 61 74 67 53 63
R08 | 856 26 14 16 12 19 18 9 | 62 62 58 63 57 57 59
R09 | 2171 13 10 17 15 23 12 6 | 28 30 39 29 36 34 30
R11 | 1626 13 14 14 27 17 20 9 | 31 41 42 44 42 31 35
R12 | 935 17 19 15 22 24 22 9 | 61 65 62 43 52 52 55
XR13 | 2835 18 13 22 37 28 --- 13 | 83 67 79 60 75 --- 69
R14 | 921 11 12 16 13 15 10 6 | 56 60 57 51 61 54 55
R15 | 1133 22 13 25 16 20 15 9 | 73 65 72 68 76 63 67
R16 | 1518 14 12 19 10 20 11 6 | 90 88 95 87 84 80 87
XR17 | 1336 17 13 29 41 33 --- 15 | 127 121 126 147 111 --- 128
R18E | 1058 10 15 21 9 20 9 7 | 89 86 80 91 82 82 85
R19E | 3909 40 31 50 40 54 46 21 | 101 83 99 87 88 87 86
R20E | 5829 54 79 58 83 55 59 33 | 130 136 140 123 124 108 118
R21E | 1739 17 17 39 9 19 16 10 | 69 68 73 70 73 70 68
R22E | 2592 18 11 16 26 23 13 8 | 60 64 73 73 68 60 65
R24E | 1113 25 15 22 63 27 23 16 | 373 374 372 371 367 368 371
XR26 |>>>>> 9 --- --- 10 --- --- 9 | 29 --- --- 33 --- --- 28
------+-----------------------------------------+-------------------------------------
RMS | 2194 24 25 26 30 27 23 |T 84 85 88 83 83 77 80
WRMS | 2194 17 16 20 20 21 23 |NE 65 65 67 63 63 53 60
MEDI | 1473 17 14 19 18 20 18 |MD 69 67 72 68 68 59 65
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