[IGSREPORT-29883] Wk 2312 IGLOS Final Orbits
acc
acc at igs.org
Mon May 20 01:18:04 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2312 (Apr 28, 2024 - May 04, 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 2.2312.
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:
igl2312[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2312 in the SP3 format.
igl23127.sum Combination Report for GPS Week 2312.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 4.0 ns
1 | 3.2 ns
2 | 2.6 ns
3 | 0.7 ns
4 | 3.9 ns
5 | 2.4 ns
6 | 2.6 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 | ESA | R20
1 | ESA | R20
2 | ESA | R20
3 | ESA | R20
4 | ESA | R20
5 | ESA | R20
6 | ESA | R20
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2312, 1a.2312).
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 2.2312.0-6)
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 3.2312.0-6).
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 2312 summary. (Apr 28, 2024 - May 04, 2024)
Table 1.2312.a GPS week : 2312 MJD: 60428.0-60434.0
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 -9 -3 22 .09 18 16 | 7310 111 3260 8015
| 1 0 1 17 19 33 .03 | 898 1844
esa n/a| 0 0 2 -4 -11 1 -.03 42 27 | 1711 1612 3262 7673
| 0 0 1 15 19 30 .03 | 5715 1747
gfz n/a| 1 0 0 12 4 -18 .03 19 14 | 0 98 3246 7130
| 1 0 1 16 15 28 .05 | 0 1586
grg n/a| 1 0 3 -12 -14 6 .27 26 21 | 2526 -7 3244 7060
| 1 1 2 21 23 56 .05 | 750 1610
iac n/a| 0 0 -1 17 16 -28 -.13 19 17 | 4850 -394 3256 7998
| 1 1 2 29 27 101 .06 | 1221 1476
jgx n/a| 0 0 -5 -12 24 42 -.16 28 28 | 9559 108 3292 7376
| 0 1 2 20 5 44 .03 | 552 1770
Table 1.2312.b GPS week : 2312 MJD: 60428.0-60434.0
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 | 16 14 12 13 11 15 14 |
R02 | 5 5 6 5 6 7 6 |
R03 | 6 6 7 6 6 6 8 |
R04 | 6 10 7 6 5 7 6 |
R05 | 8 9 7 5 7 7 7 |
R07 | 8 6 6 6 8 8 6 |
R08 | 7 7 7 7 6 7 6 |
R09 | 6 7 6 6 6 7 7 |
R11 | 6 5 7 7 6 6 5 |
R12 | 7 6 7 7 7 10 9 |
R13 | 14 13 22 16 18 17 15 |
R14 | 6 6 6 6 6 6 6 |
R15 | 7 7 7 6 7 7 8 |
R16 | 8 6 6 8 8 7 8 |
R17 | 8 6 7 6 7 5 6 |
R18 | 10 8 7 7 7 8 5 |
R19 | 20 17 19 19 18 18 17 |
R20 | 25 23 18 20 30 24 24 |
R21 | 8 7 8 8 9 8 7 |
R22 | 7 9 7 7 8 7 5 |
R24 | 10 10 9 9 8 7 9 |
R25 | 12 10 11 9 9 15 8 |
R26 | 35 32 27 30 38 32 33 |
Table 1.2312.c GPS week : 2312 MJD: 60428.0-60434.0
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 2312 0 | 58 -46 192 595 1665 8279 79.7 2310 2310 | 3986 0
brd 2312 1 | 72 -101 279 1318 573 7507 79.9 2299 2299 | 3171 0
brd 2312 2 | -23 -59 348 18 -905 2509 80.3 2215 2215 | 2560 0
brd 2312 3 | 81 51 284 796 -1183 -3568 80.6 1803 1803 | 714 0
brd 2312 4 | 44 0 207 621 -435 -1401 79.2 1794 1794 | 3926 0
brd 2312 5 | -28 -51 276 -2272 -1099 1670 76.8 1957 1957 | 2435 0
brd 2312 6 | -49 -35 128 -1111 -692 6189 79.1 1872 1872 | 2615 0
-------------+------------------------------------------------------------+----------------
brd 2312 mean| 21 -34 245 -4 -296 3026 79.4 2035 2035 | 2772 0
brd 2312 sdev| 54 48 73 1258 1047 4525 1.3 231 231 | 1109 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 2.2312.0 GPS week: 2312 Day: 0 MJD: 60428
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 1 -1 34 22 .10 21 20 | 7896 -118 3220 8636
esa n/a| -1 -2 0 -1 -21 30 .02 40 25 | 6015 1484 3221 8514
gfz n/a| 0 0 -2 2 -19 -28 -.00 20 13 | 0 -306 3272 7608
grg n/a| 0 0 7 -26 -45 -62 .25 27 20 | 3983 -260 3235 7522
iac n/a| 0 1 -1 -5 52 99 -.04 21 19 | 6866 -1135 3235 9243
jgx n/a| 0 -1 -2 2 19 -27 -.15 27 23 | 9433 -363 3322 7918
Table 2.2312.1 GPS week: 2312 Day: 1 MJD: 60429
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 1 -16 -5 58 .09 17 16 | 8160 1159 2900 8239
esa n/a| 0 -1 3 -17 -4 56 -.03 46 28 | 5719 2352 2892 8407
gfz n/a| 1 0 0 -13 10 33 .01 18 15 | 0 1300 2929 7486
grg n/a| 1 -1 0 -23 -23 41 .29 24 20 | 2540 1101 2936 7052
iac n/a| -1 0 -2 52 3 -147 -.13 20 17 | 5906 -698 2901 8594
jgx n/a| -1 1 -1 8 33 67 -.20 28 28 | 9359 1137 2970 7525
Table 2.2312.2 GPS week: 2312 Day: 2 MJD: 60430
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| -3 0 1 -1 -17 33 .08 16 13 | 8028 -131 3430 8010
esa n/a| 0 0 0 -17 -24 -4 -.03 50 30 | -7457 1519 3429 8796
gfz n/a| 0 0 -1 12 30 -23 .10 15 13 | 0 14 3435 7826
grg n/a| 1 -2 2 4 -25 -34 .24 24 22 | 2514 -282 3449 7222
iac n/a| 0 2 0 0 40 -15 -.21 19 17 | 4292 845 3422 8155
jgx n/a| 0 -2 -7 -20 26 65 -.17 26 26 | 10331 -450 3371 8122
Table 2.2312.3 GPS week: 2312 Day: 3 MJD: 60431
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 11 3 -39 .12 17 13 | 6761 -3156 3692 7778
esa n/a| 0 -1 1 8 7 -21 -.05 44 42 | 927 -1785 3730 7366
gfz n/a| 3 0 1 37 0 -40 .01 20 16 | 0 -3058 3637 6946
grg n/a| 1 0 2 -47 -29 -54 .20 26 25 | 2357 -3112 3618 6636
iac n/a| -2 2 -4 20 6 44 -.10 16 14 | 4172 -2560 3688 7704
jgx n/a| 0 2 -6 -37 17 81 -.16 33 33 | 9467 -3177 3695 7107
Table 2.2312.4 GPS week: 2312 Day: 4 MJD: 60432
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 -28 4 57 .07 16 15 | 5845 2960 3388 7080
esa n/a| 0 0 3 10 9 -8 -.03 41 23 | 2770 4057 3416 6413
gfz n/a| 0 0 0 15 7 -2 .00 21 13 | 0 1863 3280 6445
grg n/a| 1 -1 4 -14 -12 50 .24 27 22 | 2599 1985 3242 6428
iac n/a| 0 -1 -6 56 -12 -101 -.10 18 15 | 4181 1935 3379 6985
jgx n/a| -2 0 -4 -27 20 59 -.18 31 31 | 8737 2404 3405 6815
Table 2.2312.5 GPS week: 2312 Day: 5 MJD: 60433
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 3 5 -15 26 .14 21 16 | 7874 -412 3267 7750
esa n/a| -1 0 2 -26 -46 -16 -.04 39 21 | 8145 1574 3257 6955
gfz n/a| 1 0 2 8 -2 -14 -.02 22 15 | 0 142 3271 7016
grg n/a| 2 2 3 6 16 82 .31 27 23 | 2227 -219 3291 7102
iac n/a| 2 -1 0 20 42 -140 -.13 20 19 | 5233 -1174 3261 7495
jgx n/a| 0 0 -10 -24 28 65 -.15 28 28 | 10232 27 3337 7371
Table 2.2312.6 GPS week: 2312 Day: 6 MJD: 60434
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 -34 -25 2 .05 22 18 | 6607 481 2924 8614
esa n/a| 0 0 3 9 -3 -23 -.06 36 20 | -4141 2085 2893 7261
gfz n/a| 0 -2 -1 24 6 -53 .08 19 13 | 0 731 2904 6585
grg n/a| 4 1 0 10 16 18 .35 25 19 | 1463 734 2937 7458
iac n/a| -1 1 1 -22 -15 59 -.22 17 15 | 3300 24 2906 7812
jgx n/a| 0 -1 -6 14 25 -17 -.12 24 24 | 9354 1179 2944 6780
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 3.2312.0 GPS week: 2312 Day: 0 MJD: 60428
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1133 42 48 16 28 27 43 16 | 89 53 79 72 76 63 70
R02 | 1155 9 13 7 13 9 15 5 | 60 52 56 58 53 55 55
R03 | 645 12 8 12 15 21 12 6 | 60 61 67 68 67 58 63
R04 | 2341 17 11 14 11 14 12 6 | 67 58 56 58 52 55 57
R05 | 1138 19 19 15 18 13 15 7 | 61 69 64 58 54 58 59
R07 | 1505 12 14 18 14 24 14 7 | 69 62 62 78 76 62 66
R08 | 1225 21 12 11 13 15 10 6 | 59 65 71 74 71 66 67
R09E | 5914 16 10 14 21 11 7 6 | 62 65 66 72 63 68 65
R11E | 5608 14 9 8 17 15 8 5 | 53 54 51 56 49 53 52
R12E | 2411 13 14 11 17 24 15 7 | 154 154 154 154 156 149 153
R13E | 1769 27 24 39 26 27 41 14 | 42 53 79 55 47 51 49
R14E | 1344 11 14 13 17 12 11 6 | 78 83 82 88 72 78 79
R15E | 937 16 16 15 19 11 13 6 | 93 108 104 115 98 98 101
R16E | 1880 15 18 23 17 18 10 7 | 52 58 59 59 45 51 52
XR17 | 1365 9 18 12 13 25 --- 8 | 61 55 59 62 67 --- 59
R18 | 982 12 18 20 17 25 29 9 | 53 60 63 54 60 46 54
R19 | 1419 44 39 44 63 30 38 19 | 71 62 92 77 66 59 68
R20 | 1618 27 155 28 67 32 74 24 | 111 55 133 140 136 115 124
R21 | 584 8 26 19 20 12 16 8 | 63 57 67 71 63 57 62
R22 | 2114 14 11 9 19 22 8 6 | 34 38 40 43 40 40 37
R24 | 1054 24 15 12 12 30 27 9 | 62 58 61 68 73 57 62
XR25 |17835 12 16 --- --- 21 --- 12 | 32 37 --- --- 34 --- 31
XR26 | 9551 42 --- --- 29 69 --- 35 | 120 --- --- 119 156 --- 129
------+-----------------------------------------+-------------------------------------
RMS | 2309 21 40 20 27 21 26 |T 69 64 74 77 72 66 70
WRMS | 2309 20 25 13 20 19 23 |NE 67 56 69 73 71 60 66
MEDI | 1419 15 15 14 17 21 14 |MD 62 58 66 68 66 58 62
Table 3.2312.1 GPS week: 2312 Day: 1 MJD: 60429
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 682 33 46 16 26 13 45 14 | 56 50 66 55 46 45 52
R02 | 1577 12 11 11 10 13 14 5 | 48 43 45 54 33 47 43
R03 | 748 11 16 8 15 17 15 6 | 46 41 48 52 48 49 46
R04 | 1278 21 16 34 10 18 9 9 | 55 51 41 52 39 53 45
R05 | 720 13 20 18 22 23 16 8 | 49 57 35 47 45 50 44
R07 | 653 8 14 17 10 9 19 6 | 56 68 66 62 55 52 58
R08 | 1856 11 11 20 12 8 18 6 | 51 64 66 53 51 51 55
R09E | 5504 15 9 15 18 15 9 6 | 29 35 36 30 35 32 30
R11E | 5198 11 9 8 14 13 11 5 | 24 29 29 29 29 27 25
R12E | 2538 8 18 11 17 14 11 6 | 141 144 140 139 142 140 140
R13E | 2034 21 22 29 28 34 39 13 | 42 52 64 59 34 40 43
R14E | 2239 15 21 10 15 11 9 6 | 33 40 35 35 39 29 33
R15E | 1269 9 16 8 25 15 16 6 | 63 70 65 69 64 64 64
R16E | 1258 12 16 8 18 15 10 6 | 37 42 42 43 32 38 36
XR17 | 876 9 12 7 8 19 --- 6 | 41 42 39 42 42 --- 40
R18 | 669 13 18 12 14 20 24 7 | 39 43 46 36 35 35 37
R19 | 1244 33 43 23 58 19 45 17 | 46 49 55 47 33 44 41
R20 | 3586 18 181 30 52 41 78 22 | 76 92 76 72 70 94 73
R21 | 695 8 24 13 8 13 19 6 | 27 29 30 31 24 23 26
R22 | 2078 13 18 19 21 22 18 8 | 23 25 37 33 22 27 23
R24 | 616 19 23 13 14 26 29 9 | 40 33 32 41 35 26 32
XR25 |14154 12 14 --- --- 16 --- 10 | 26 32 --- --- 28 --- 26
XR26 | 9517 36 --- --- 28 62 --- 31 | 87 --- --- 88 111 --- 93
------+-----------------------------------------+-------------------------------------
RMS | 2298 17 46 18 24 20 28 |T 49 51 52 53 47 48 48
WRMS | 2298 16 28 15 20 17 28 |NE 47 47 48 51 44 45 45
MEDI | 1278 13 16 13 15 16 16 |MD 46 43 45 47 39 44 43
Table 3.2312.2 GPS week: 2312 Day: 2 MJD: 60430
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1438 28 37 9 34 20 28 12 | 69 51 58 64 57 54 59
R02 | 1427 8 16 8 14 14 13 5 | 52 49 49 55 52 53 50
R03 | 836 10 15 10 19 20 14 6 | 48 44 56 51 57 48 50
R04 | 556 15 15 10 19 17 21 7 | 53 49 53 40 49 42 47
R05 | 601 13 17 12 12 26 10 7 | 40 39 30 28 44 34 33
R07 | 580 7 13 18 10 11 15 5 | 60 61 72 63 66 49 62
R08 | 2852 12 12 16 11 19 23 7 | 53 51 63 58 73 54 58
R09E | 5082 12 9 15 16 12 12 6 | 25 32 38 28 35 32 30
R11E | 3187 14 9 11 25 21 13 7 | 28 34 36 34 33 35 31
R12E | 1607 13 16 14 22 10 19 7 | 95 96 98 108 99 102 98
XR13E | 1201 27 43 65 28 30 --- 21 | 41 40 121 49 52 --- 60
R14E | 2791 9 20 9 14 12 14 5 | 40 42 43 39 42 33 39
R15E | 1460 11 17 15 23 14 14 7 | 70 72 78 86 75 71 74
R16E | 1889 10 15 15 14 11 18 6 | 27 31 37 32 29 30 28
XR17 | 540 10 18 10 11 14 --- 6 | 46 39 43 48 46 --- 43
R18 | 575 11 23 12 13 14 23 7 | 45 52 50 43 51 39 45
R19 | 1033 29 49 26 59 38 63 19 | 62 41 57 63 63 51 52
R20 | 4604 30 196 23 39 31 58 18 | 93 46 102 102 104 93 96
R21 | 819 8 15 20 14 20 31 8 | 45 46 49 48 47 47 45
R22 | 1891 13 19 9 13 20 11 6 | 28 32 34 44 38 32 32
R24 | 578 16 31 16 14 15 24 8 | 47 47 52 47 43 49 46
XR25 |13622 12 17 --- --- 17 --- 10 | 37 41 --- --- 39 --- 35
XR26 |12142 28 --- --- 25 54 --- 26 | 128 --- --- 123 133 --- 128
------+-----------------------------------------+-------------------------------------
RMS | 2214 16 50 15 24 19 26 |T 53 47 58 56 57 49 53
WRMS | 2214 13 30 13 22 17 26 |NE 56 45 54 58 60 49 55
MEDI | 1438 12 17 14 14 17 18 |MD 47 44 52 48 51 48 47
Table 3.2312.3 GPS week: 2312 Day: 3 MJD: 60431
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 956 25 30 21 56 13 33 13 | 78 62 71 79 65 52 67
R02 | 1514 10 7 12 12 14 11 5 | 68 61 63 65 56 64 61
R03 | 583 10 13 16 11 11 14 5 | 57 64 60 61 55 60 58
R04 | 644 10 11 12 19 15 19 6 | 46 48 56 52 39 43 45
R05 | 548 9 9 13 11 12 13 5 | 48 45 46 40 35 49 42
R07 | 962 12 14 10 14 11 22 6 | 55 60 50 58 62 60 56
R08 | 3576 17 13 22 17 9 19 7 | 57 66 74 54 64 60 62
R09E | 4604 16 9 13 15 12 12 6 | 26 37 42 32 34 32 32
R11E | 3294 14 10 20 18 13 22 7 | 30 32 46 34 30 28 31
R12E | 1226 10 14 12 20 12 24 6 | 167 173 168 167 179 168 171
R13E | 1211 28 28 39 37 25 58 15 | 49 39 58 59 46 47 40
R14E | 1109 16 14 9 16 9 17 6 | 37 37 37 43 33 32 34
R15E | 606 9 11 13 18 12 20 6 | 41 37 46 44 40 38 39
R16E | 887 15 24 23 15 10 17 8 | 43 54 56 44 39 41 43
XR17 | 562 12 13 10 14 9 --- 6 | 44 45 45 53 40 --- 43
R18 | 601 7 14 15 10 15 30 7 | 35 40 37 37 37 34 34
R19 | 1346 34 43 31 68 27 60 19 | 71 41 66 70 50 57 55
R20 | 1328 23 180 38 25 30 79 19 | 99 50 123 107 114 78 104
R21 | 724 10 18 21 15 10 35 8 | 48 40 56 53 46 34 45
R22 | 2191 12 12 11 18 12 23 6 | 23 29 34 37 29 31 26
R24 | 579 13 29 13 18 19 20 8 | 46 50 52 61 52 53 49
XR25 |12855 15 12 --- --- 10 --- 8 | 33 35 --- --- 28 --- 30
XR26 |13302 34 --- --- 39 50 --- 30 | 71 --- --- 87 88 --- 77
------+-----------------------------------------+-------------------------------------
RMS | 1802 17 44 20 26 16 33 |T 55 52 61 60 54 53 54
WRMS | 1802 13 42 16 25 14 33 |NE 54 49 59 60 53 51 53
MEDI | 1109 13 13 13 17 12 20 |MD 48 45 56 53 46 47 45
Table 3.2312.4 GPS week: 2312 Day: 4 MJD: 60432
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1043 27 25 21 36 16 27 11 | 76 61 71 71 61 54 65
R02 | 899 14 10 11 11 13 19 6 | 61 57 58 51 46 50 53
R03 | 1493 15 8 10 14 15 14 6 | 56 65 57 66 59 68 60
R04 | 2065 13 7 10 10 12 15 5 | 53 52 50 46 42 52 48
R05 | 663 21 11 15 11 15 18 7 | 48 48 43 44 38 42 42
R07 | 648 10 19 10 34 14 15 7 | 58 55 56 81 52 60 57
R08 | 1613 14 12 15 12 12 16 6 | 49 62 62 63 53 59 56
R09E | 3044 12 10 12 15 12 15 5 | 33 36 43 33 32 40 34
R11E | 3774 11 9 15 19 12 16 6 | 26 31 37 31 27 31 28
R12E | 2048 14 12 11 26 12 18 7 | 91 87 86 84 84 80 85
XR13E | 2218 31 32 48 40 27 --- 18 | 39 43 63 38 30 --- 36
R14E | 1769 10 14 14 18 11 14 6 | 40 39 48 45 34 35 38
R15E | 746 11 14 16 21 17 17 7 | 42 40 42 53 40 43 40
R16E | 742 12 22 20 13 9 22 7 | 29 30 36 33 24 30 26
XR17 | 711 12 17 13 10 11 --- 6 | 26 23 26 25 28 --- 23
R18 | 621 11 9 16 12 16 26 7 | 24 28 41 33 33 25 28
R19 | 991 29 44 29 73 29 41 18 | 52 53 55 54 44 50 45
R20 | 2889 31 161 65 36 40 105 30 | 82 59 108 86 98 76 83
R21 | 846 7 21 13 24 20 30 8 | 29 28 27 42 37 29 28
R22 | 2530 12 16 19 29 17 12 8 | 21 28 31 31 34 26 23
R24 | 688 9 20 12 11 26 16 7 | 26 27 23 34 37 27 26
XR25 | 9607 11 13 --- --- 14 --- 9 | 22 26 --- --- 35 --- 26
XR26 |13022 42 --- --- 39 70 --- 38 | 143 --- --- 152 168 --- 151
------+-----------------------------------------+-------------------------------------
RMS | 1793 16 41 21 27 18 31 |T 48 44 50 54 49 46 47
WRMS | 1793 15 23 13 22 15 31 |NE 51 44 50 58 54 47 50
MEDI | 1493 12 14 15 18 15 17 |MD 42 40 48 45 38 43 40
Table 3.2312.5 GPS week: 2312 Day: 5 MJD: 60433
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 974 45 33 23 41 25 29 15 | 56 33 46 39 51 34 40
R02 | 1024 7 13 15 23 10 18 6 | 48 51 55 34 45 37 44
R03 | 1831 4 12 7 15 20 19 6 | 40 35 36 36 44 31 35
R04 | 1187 11 12 14 15 15 21 6 | 41 34 36 45 44 28 36
R05 | 652 14 7 10 22 14 21 6 | 32 30 29 36 30 25 28
R07 | 693 13 22 12 30 17 11 8 | 44 34 49 62 40 48 43
R08 | 881 16 6 10 14 17 20 6 | 39 41 34 46 44 42 39
R09E | 3449 17 12 20 20 12 14 7 | 49 54 56 49 49 53 50
R11E | 3902 11 8 13 16 13 17 6 | 33 35 38 40 31 33 33
R12E | 2589 20 16 17 36 26 19 10 | 187 178 175 162 187 178 178
R13E | 2476 30 22 53 34 35 45 16 | 42 47 61 56 33 54 37
R14E | 738 9 10 14 21 10 13 5 | 53 59 55 58 50 56 54
R15E | 798 11 12 13 14 17 20 6 | 60 58 60 59 53 58 56
R16E | 2355 15 18 16 16 12 14 7 | 40 46 46 52 36 48 42
XR17 | 844 7 11 8 11 9 --- 4 | 28 31 29 40 26 --- 29
R18 | 701 18 18 14 18 13 19 7 | 27 31 27 38 28 28 26
R19 | 1010 44 34 36 58 33 27 17 | 40 31 47 36 46 37 33
R20 | 3556 30 157 41 43 23 82 23 | 56 57 65 62 48 44 46
R21 | 875 11 13 10 16 26 27 8 | 35 30 30 36 36 29 30
R22 | 2389 10 11 25 14 15 12 7 | 24 33 35 30 29 29 26
R24 | 889 12 12 15 18 20 20 7 | 30 38 34 35 31 33 30
XR25 |11886 19 22 --- --- 19 --- 14 | 29 30 --- --- 29 --- 25
XR26 |11711 30 --- --- 41 59 --- 31 | 163 --- --- 159 167 --- 164
------+-----------------------------------------+-------------------------------------
RMS | 1956 21 39 22 27 20 28 |T 52 46 49 55 51 46 48
WRMS | 1956 16 21 15 23 19 28 |NE 45 35 39 48 46 34 42
MEDI | 1024 14 12 14 18 17 19 |MD 40 35 46 40 44 37 37
Table 3.2312.6 GPS week: 2312 Day: 6 MJD: 60434
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 957 46 43 21 24 21 14 13 | 98 57 86 90 84 67 79
R02 | 1446 11 8 9 13 21 9 5 | 79 77 81 73 84 75 78
R03 | 2246 21 19 19 19 15 10 7 | 79 86 88 78 85 77 81
R04 | 2017 15 10 13 18 13 8 6 | 75 65 61 63 64 58 63
R05 | 787 16 9 11 10 15 23 6 | 68 60 57 56 59 48 57
R07 | 838 16 9 15 12 13 12 6 | 77 72 76 86 75 72 75
R08 | 736 16 9 10 12 14 17 6 | 68 79 81 83 81 75 77
R09E | 4040 20 10 11 23 9 13 6 | 51 45 50 43 46 42 45
R11E | 2232 11 11 11 14 9 8 4 | 25 30 31 32 26 24 27
R12E | 2498 16 17 18 32 16 19 9 | 252 260 254 267 248 261 256
R13E | 1893 19 28 44 31 28 43 15 | 37 30 68 46 41 44 36
R14E | 1208 8 12 14 20 11 10 5 | 53 57 52 58 57 55 54
R15E | 1358 10 15 17 23 17 17 7 | 54 62 57 66 52 57 56
R16E | 2505 12 19 20 13 15 16 7 | 31 41 42 40 33 35 34
XR17 | 1411 11 7 9 19 13 --- 6 | 32 29 33 38 28 --- 30
R18 | 975 9 9 11 11 11 9 4 | 28 31 31 32 28 35 28
R19 | 2445 49 23 22 61 23 41 17 | 49 42 56 58 44 44 44
R20 | 1485 38 143 42 51 27 68 23 | 93 66 104 104 101 62 89
R21 | 960 9 18 13 15 9 17 6 | 35 29 38 42 35 26 32
R22 | 2208 11 10 8 12 14 9 5 | 21 25 24 26 23 24 22
R24 | 649 15 25 12 16 24 19 8 | 40 34 43 48 47 36 39
XR25 |16382 12 10 --- --- 9 --- 7 | 17 21 --- --- 17 --- 18
XR26 |11439 36 --- --- 39 56 --- 32 | 177 --- --- 170 187 --- 176
------+-----------------------------------------+-------------------------------------
RMS | 1871 22 36 19 25 17 24 |T 66 59 67 72 67 60 65
WRMS | 1871 18 20 13 19 15 24 |NE 64 51 61 69 65 53 61
MEDI | 1485 15 11 13 18 15 14 |MD 53 45 57 58 52 48 54
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