[IGSREPORT-30140] Wk 2335 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 25 07:25:15 UTC 2024
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2335 (Oct 06, 2024 - Oct 12, 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 2.2335.
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:
igl2335[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2335 in the SP3 format.
igl23357.sum Combination Report for GPS Week 2335.
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 | 5.8 ns
1 | 4.4 ns
2 | 9.5 ns
3 | 5.8 ns
4 | 7.0 ns
5 | 6.3 ns
6 | 5.5 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 1.2335, 1a.2335).
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 2.2335.0-6)
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 3.2335.0-6).
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 2335 summary. (Oct 06, 2024 - Oct 12, 2024)
Table 1.2335.a GPS week : 2335 MJD: 60589.0-60595.0
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 -14 10 46 .18 21 18 | -3891 -14 4042 17160
| 1 0 1 19 19 18 .03 | 1513 1303
esa n/a| 0 0 -1 -23 -10 11 -.04 24 21 | 10965 -255 3211 7611
| 1 1 1 13 12 30 .03 | 4811 2010
gfz n/a| 1 0 3 49 24 -10 -.02 20 16 | 0 -130 3262 7894
| 1 0 1 10 12 22 .07 | 0 2180
grg n/a| 0 0 0 -19 -12 -27 .30 28 21 | 3063 -91 4139 17196
| 2 0 3 14 16 65 .07 | 1332 1661
iac n/a| 1 0 -6 31 27 -32 -.19 25 22 | 6058 -392 4013 16460
| 1 1 4 13 23 87 .11 | 1687 688
jgx n/a| -1 0 1 -29 -39 2 -.22 27 24 | -141980 -142969 3224 8436
| 1 1 2 17 21 42 .05 | 378351 377919
Table 1.2335.b GPS week : 2335 MJD: 60589.0-60595.0
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 | 17 16 11 13 18 15 12 |
R02 | 6 7 7 6 6 6 8 |
R03 | 7 8 8 6 8 7 6 |
R04 | 8 7 7 6 9 5 6 |
R05 | 7 7 6 6 7 7 6 |
R07 | 7 7 6 6 6 6 6 |
R08 | 9 9 9 7 8 9 7 |
R09 | 11 8 7 6 6 7 7 |
R11 | 10 12 9 7 7 6 6 |
R12 | 8 10 21 9 9 8 8 |
R14 | 9 14 6 8 9 8 8 |
R15 | 7 17 13 7 10 6 9 |
R16 | 9 12 16 7 8 10 6 |
R17 | 8 8 9 7 8 8 7 |
R18 | 9 8 9 9 9 9 7 |
R19 | 27 26 29 25 27 23 26 |
R20 | 18 19 20 20 16 19 19 |
R21 | 7 8 9 7 11 6 5 |
R22 | 7 7 6 8 8 6 6 |
R24 | 7 8 9 8 7 9 8 |
R25 | 11 14 14 10 17 12 12 |
R26 | 26 24 29 26 36 25 21 |
Table 1.2335.c GPS week : 2335 MJD: 60589.0-60595.0
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 2335 0 | 89 62 49 -426 1971 -5967 82.0 1274 1274 | 5778 0
brd 2335 1 | 13 34 28 562 2013 -9883 81.1 1512 1512 | 4403 0
brd 2335 2 | 60 -38 130 -105 1191 -12470 80.6 1587 1587 | 9514 0
brd 2335 3 | 39 73 38 -738 454 -5613 78.9 1672 1672 | 5776 0
brd 2335 4 | -46 -40 16 1012 -3514 -5817 80.9 1694 1694 | 7035 0
brd 2335 5 | -64 -39 -11 -652 -3008 -313 84.6 1791 1791 | 6350 0
brd 2335 6 | 11 -53 136 -567 698 2027 81.2 1818 1818 | 5459 0
-------------+------------------------------------------------------------+----------------
brd 2335 mean| 14 0 55 -130 -27 -5433 81.3 1621 1621 | 6330 0
brd 2335 sdev| 55 54 56 672 2289 5027 1.7 186 186 | 1618 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 2.2335.0 GPS week: 2335 Day: 0 MJD: 60589
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 3 11 -12 44 .16 22 18 | -4019 -408 4321 20113
esa n/a| 1 0 -3 -30 -22 -2 -.04 24 21 | 7869 -3 3092 7738
gfz n/a| 0 1 5 45 26 -7 -.16 20 17 | 0 247 3147 7828
grg n/a| 0 0 2 -16 -3 -69 .34 30 21 | 2019 -593 4471 20389
iac n/a| 2 1 -7 21 45 -11 -.07 24 21 | 4383 64 4254 19041
jgx n/a| -1 0 0 -52 -36 52 -.23 28 29 | 1702 -749 3093 8017
Table 2.2335.1 GPS week: 2335 Day: 1 MJD: 60590
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 -1 10 29 .22 18 15 | -5992 -2408 4279 18838
esa n/a| 0 -1 -3 -25 -19 28 -.05 29 27 | 10295 -4028 3070 7776
gfz n/a| 0 0 0 60 23 23 -.07 21 16 | 0 -4016 3130 8443
grg n/a| -2 0 6 -24 -15 92 .21 33 26 | 1997 -2743 4401 18791
iac n/a| 3 1 -4 15 48 -192 -.20 30 25 | 3534 -668 4249 17831
jgx n/a| -2 0 -2 -1 -42 11 -.16 28 25 | 311 -3142 3030 8640
Table 2.2335.2 GPS week: 2335 Day: 2 MJD: 60591
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 -1 1 66 .20 16 14 | -3113 1440 3988 17513
esa n/a| 0 1 0 -44 10 41 -.01 20 17 | 9911 750 3315 7261
gfz n/a| 1 1 2 50 13 9 .01 18 16 | 0 1420 3388 7334
grg n/a| 0 0 -1 7 13 -92 .24 42 19 | 5374 1450 4063 17793
iac n/a| 1 0 -15 37 29 -57 -.41 34 34 | 8468 736 3959 16617
jgx n/a| -3 0 6 -14 -37 -59 -.15 22 21 | -999999 -999999 3249 7700
Table 2.2335.3 GPS week: 2335 Day: 3 MJD: 60592
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -2 0 0 -45 6 44 .16 19 15 | -5394 -791 3904 17482
esa n/a| 0 0 -1 -19 -5 -35 -.05 27 27 | 11783 -1784 2908 7238
gfz n/a| 1 0 4 61 12 -13 .03 17 13 | 0 -2258 2955 7595
grg n/a| 1 0 -2 -13 -13 -68 .30 21 18 | 3154 -1739 4010 17838
iac n/a| 0 -1 -5 26 50 81 -.20 23 19 | 5691 -1208 3878 16701
jgx n/a| 0 2 1 -43 -72 -9 -.24 28 24 | 9 -2078 2942 7589
Table 2.2335.4 GPS week: 2335 Day: 4 MJD: 60593
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 -11 14 34 .13 22 22 | -4283 452 3438 14937
esa n/a| -1 0 -1 0 -1 40 -.09 25 19 | 12170 221 2974 6244
gfz n/a| 3 2 1 54 48 -24 .01 22 19 | 0 627 3024 6569
grg n/a| 3 0 0 -31 -41 -46 .25 22 19 | 3884 338 3544 15261
iac n/a| 1 0 -3 24 0 -79 -.09 26 23 | 7129 -1101 3463 14599
jgx n/a| 0 -1 0 -24 -56 53 -.28 30 26 | 0 1639 3036 9309
Table 2.2335.5 GPS week: 2335 Day: 5 MJD: 60594
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 -27 50 77 .19 29 21 | -2812 915 4086 14218
esa n/a| -2 -1 0 -21 -16 26 -.05 19 16 | 4564 1483 3499 6833
gfz n/a| 2 0 1 37 27 -16 .07 21 17 | 0 1179 3566 7337
grg n/a| -2 1 -1 -38 -13 -38 .35 23 23 | 3450 1368 4099 13056
iac n/a| 2 -2 -2 54 -5 12 -.19 17 16 | 6935 -501 4064 14172
jgx n/a| -2 1 3 -39 -15 -36 -.27 26 22 | 1416 1499 3569 7605
Table 2.2335.6 GPS week: 2335 Day: 6 MJD: 60595
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 3 31 .19 22 18 | -1624 699 4284 17022
esa n/a| 0 -1 0 -25 -20 -20 -.00 21 17 | 20165 1575 3620 10188
gfz n/a| 2 0 4 34 16 -44 -.00 19 13 | 0 1887 3628 10153
grg n/a| 0 1 -4 -19 -10 30 .39 27 19 | 1563 1280 4390 17249
iac n/a| 1 0 -3 39 22 17 -.19 20 17 | 6270 -68 4229 16263
jgx n/a| 0 0 3 -26 -12 1 -.21 25 21 | 2697 2044 3652 10193
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 3.2335.0 GPS week: 2335 Day: 0 MJD: 60589
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 527 44 18 23 38 22 67 17 | 37 31 32 35 37 30 28
R02 | 1297 11 12 14 17 14 16 6 | 29 33 33 26 36 26 29
R03 | 557 8 13 11 14 17 25 6 | 30 31 34 30 37 27 30
R04 | 859 9 9 23 9 16 29 7 | 35 42 47 46 40 36 39
R05 | 1557 13 17 14 9 22 14 7 | 36 38 35 40 44 38 35
R07 | 2600 10 13 11 22 17 16 6 | 35 29 37 39 38 30 32
R08 | 895 15 10 19 16 37 16 9 | 33 30 41 34 42 31 32
R09E | 1663 15 14 17 57 15 17 11 | 83 85 84 112 82 83 85
XR11E | 1272 13 13 21 15 28 --- 9 | 56 60 58 55 65 --- 57
R12E | 866 10 11 9 17 27 22 7 | 127 123 123 136 114 126 123
R14E | 1294 15 13 11 41 17 10 8 | 90 85 89 88 93 82 86
R15E | 637 12 16 9 17 21 13 6 | 122 128 125 133 136 134 127
R16E | 672 18 20 11 26 24 15 8 | 91 108 105 91 108 94 98
R17 | 834 10 22 18 7 19 28 8 | 62 52 70 62 60 45 58
R18 | 504 16 17 11 18 11 38 8 | 47 61 53 55 57 37 50
R19 | 1214 54 76 47 73 48 55 26 | 77 48 112 82 109 46 75
R20 | 1600 45 41 37 45 34 25 17 | 87 51 64 67 62 54 58
R21 | 917 11 16 17 18 18 16 7 | 65 58 65 74 62 53 62
R22 | 2010 11 15 17 12 19 17 7 | 46 53 47 55 44 45 47
R24 | 1384 11 18 17 13 17 13 6 | 63 69 60 52 65 61 61
XR25 |12377 13 14 --- --- 20 --- 11 | 44 43 --- --- 42 --- 40
XR26 |12412 25 --- --- 28 52 --- 25 | 55 --- --- 58 49 --- 52
------+-----------------------------------------+-------------------------------------
RMS | 1274 22 24 20 30 24 28 |T 61 59 65 65 64 56 59
WRMS | 1274 18 21 17 21 21 29 |NE 48 44 52 50 51 39 45
MEDI | 1214 13 15 17 17 19 17 |MD 55 52 58 55 57 45 52
Table 3.2335.1 GPS week: 2335 Day: 1 MJD: 60590
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 783 38 15 35 28 25 57 16 | 41 42 55 43 40 42 38
R02 | 1388 11 13 13 23 13 23 7 | 37 31 38 37 28 38 32
R03 | 703 8 13 16 10 33 19 7 | 38 40 39 38 44 39 36
R04 | 700 14 14 13 15 11 27 7 | 40 49 43 48 35 46 42
R05 | 2181 11 14 15 11 16 22 6 | 40 45 38 51 36 47 41
R07 | 2625 8 18 9 19 23 16 6 | 40 35 45 47 43 33 38
R08 | 740 17 15 18 15 27 21 8 | 41 34 48 52 29 44 39
R09E | 2833 15 18 18 20 18 19 8 | 86 87 91 89 83 88 86
R11E | 1221 14 15 28 48 33 26 12 | 57 59 64 74 65 59 57
R12E | 781 10 13 18 38 32 21 9 | 135 137 136 155 131 137 135
R14E | 1097 14 33 16 67 24 16 13 | 98 107 104 88 109 91 96
XR15E | 587 23 25 18 75 19 --- 17 | 146 145 146 167 158 --- 147
R16E | 1035 12 23 13 49 30 28 11 | 95 97 97 119 92 94 94
R17 | 697 9 20 13 13 20 24 7 | 58 60 54 64 53 57 56
R18 | 679 15 14 11 21 12 32 8 | 52 54 57 58 50 46 52
R19 | 2500 28 84 44 57 84 55 26 | 61 55 88 75 89 69 67
R20 | 2058 39 66 34 48 36 23 19 | 66 68 61 81 63 56 61
R21 | 739 11 18 9 23 17 25 7 | 63 59 56 73 60 58 60
R22 | 1210 16 12 15 19 15 13 6 | 47 56 48 65 40 51 48
R24 | 1360 10 13 13 21 21 24 7 | 63 67 64 62 63 62 62
XR25 |13369 13 17 --- --- 29 --- 13 | 53 45 --- --- 48 --- 49
XR26 | 7834 15 --- --- 35 55 --- 24 | 53 --- --- 66 43 --- 52
------+-----------------------------------------+-------------------------------------
RMS | 1512 18 29 21 33 30 28 |T 64 65 68 73 63 60 63
WRMS | 1512 15 27 16 26 25 25 |NE 49 49 52 57 47 49 48
MEDI | 1097 14 15 15 23 23 23 |MD 53 56 56 65 50 56 52
Table 3.2335.2 GPS week: 2335 Day: 2 MJD: 60591
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 994 21 12 15 41 32 30 10 | 55 53 46 35 56 22 45
R02 | 2317 7 11 7 13 35 17 6 | 42 40 40 41 52 38 39
R03 | 1007 13 14 13 13 14 28 7 | 37 31 40 29 39 31 33
R04 | 1345 17 12 9 15 17 18 6 | 40 44 38 33 39 35 38
R05 | 2786 10 11 10 11 22 18 6 | 42 42 39 38 42 34 38
R07 | 2989 12 11 12 13 25 15 6 | 42 37 36 37 35 34 36
R08 | 1119 16 7 26 32 21 21 9 | 43 41 51 32 48 45 41
R09E | 2245 16 15 11 24 16 19 7 | 56 58 57 61 56 63 56
R11E | 1063 16 17 13 40 26 21 9 | 48 47 48 48 60 51 47
R12E | 617 21 13 34 111 91 25 21 | 115 109 116 164 112 115 110
R14E | 1037 8 13 13 19 13 14 6 | 78 75 77 84 80 75 76
XR15E | 1006 14 13 14 72 14 --- 13 | 111 111 107 115 107 --- 107
R16E | 1100 18 17 20 101 39 14 15 | 69 64 61 103 76 68 62
R17 | 1196 9 14 21 16 40 17 8 | 54 48 61 56 49 48 50
R18 | 1585 16 19 8 19 33 28 9 | 47 55 47 56 55 40 47
XR19 | 3076 26 82 44 76 69 --- 29 | 73 65 101 73 97 --- 74
R20 | 1062 35 62 39 33 40 41 19 | 72 48 94 60 74 42 61
R21 | 679 9 25 17 31 25 18 9 | 55 51 63 72 55 51 55
R22 | 1002 13 7 12 16 21 13 6 | 70 70 70 65 75 61 68
R24 | 1677 14 23 9 19 25 27 8 | 49 48 40 48 45 49 42
XR25 |13633 15 14 --- --- 33 --- 13 | 51 61 --- --- 60 --- 52
XR26 |42899 24 --- --- 16 76 --- 28 | 70 --- --- 57 73 --- 66
------+-----------------------------------------+-------------------------------------
RMS | 1587 16 20 18 42 34 22 |T 59 57 61 62 62 50 56
WRMS | 1587 14 17 16 19 34 21 |NE 52 48 54 48 55 40 49
MEDI | 1119 15 14 13 19 25 18 |MD 54 51 51 56 56 45 50
Table 3.2335.3 GPS week: 2335 Day: 3 MJD: 60592
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 1007 23 13 12 21 30 58 12 | 38 41 38 37 33 41 35
R02 | 2062 10 11 11 15 16 14 5 | 32 34 38 39 30 37 32
R03 | 688 10 16 9 15 15 19 6 | 36 36 41 35 31 34 34
R04 | 1596 15 14 9 10 9 15 5 | 39 43 44 43 33 37 39
R05 | 2738 18 7 9 16 14 9 6 | 43 42 33 47 37 43 39
R07 | 844 8 11 14 11 16 22 6 | 36 38 37 36 41 33 35
R08 | 1847 15 12 11 16 15 20 6 | 32 36 38 33 31 36 33
R09E | 2035 14 7 11 15 13 22 6 | 40 45 47 46 42 50 43
R11E | 1757 14 12 12 18 12 18 6 | 38 43 46 48 41 35 41
R12E | 759 21 14 12 17 32 16 8 | 151 140 138 132 113 145 136
R14E | 1257 10 13 16 21 24 20 8 | 87 88 89 93 88 90 87
R15E | 928 11 13 14 16 21 13 6 | 112 110 114 114 118 79 112
R16E | 1220 15 20 13 19 12 17 7 | 67 73 74 73 70 59 68
R17 | 1861 9 16 12 11 20 20 6 | 54 61 60 60 46 49 54
R18 | 2164 12 28 13 23 27 15 9 | 48 65 52 50 65 47 51
R19 | 3061 38 81 47 62 49 58 25 | 91 52 110 86 100 63 83
R20 | 1537 42 65 32 10 48 55 19 | 66 34 64 64 79 33 51
R21 | 807 10 23 14 12 12 20 7 | 55 53 55 57 49 45 51
R22 | 1418 19 12 18 18 17 16 7 | 39 45 39 42 40 36 37
R24 | 1303 13 17 13 25 9 25 7 | 50 50 47 66 46 35 48
XR25 | 9705 13 11 --- --- 14 --- 9 | 40 44 --- --- 31 --- 38
XR26 |38610 24 --- --- 23 56 --- 25 | 38 --- --- 42 32 --- 37
------+-----------------------------------------+-------------------------------------
RMS | 1671 19 27 17 21 23 28 |T 56 55 60 59 54 51 53
WRMS | 1671 15 27 13 18 19 24 |NE 46 44 49 49 45 40 43
MEDI | 1537 14 13 12 16 16 19 |MD 40 45 47 48 41 41 41
Table 3.2335.4 GPS week: 2335 Day: 4 MJD: 60593
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 708 44 34 20 34 35 60 17 | 52 59 47 51 50 37 47
R02 | 1703 12 13 13 8 18 12 6 | 34 39 29 36 34 33 31
R03 | 1511 13 16 16 18 22 17 7 | 33 41 39 28 43 43 34
R04 | 1799 10 15 28 24 27 10 9 | 37 41 43 34 44 36 35
R05 | 2018 13 13 12 13 17 19 6 | 37 40 45 40 40 44 39
R07 | 1050 10 13 11 8 11 18 5 | 39 36 35 40 36 36 35
R08 | 1486 18 11 22 13 16 18 7 | 36 36 40 38 39 38 35
R09E | 1133 12 12 13 12 14 17 6 | 58 58 61 58 57 55 57
R11E | 2224 15 9 12 19 20 21 7 | 43 45 47 49 47 34 42
R12E | 1260 16 19 19 18 35 12 9 | 69 76 75 71 69 70 69
R14E | 1519 6 16 14 24 31 25 9 | 82 82 83 93 84 88 83
XR15E | 1632 18 13 18 19 28 --- 9 | 93 93 96 90 96 --- 92
R16E | 2122 16 20 12 19 17 15 7 | 56 62 57 54 65 53 55
R17 | 1045 9 16 8 13 26 23 7 | 57 55 60 53 72 51 56
R18 | 2399 16 25 13 22 28 17 9 | 51 62 56 46 66 46 52
R19 | 2315 53 66 56 51 50 79 26 | 87 73 110 68 95 60 79
R20 | 2663 43 45 27 28 32 36 16 | 70 39 67 53 72 46 52
R21 | 833 10 25 33 15 10 37 10 | 63 58 81 68 63 42 61
R22 | 1630 17 17 15 19 25 14 8 | 78 81 77 73 75 68 74
R24 | 950 15 12 19 11 14 24 7 | 55 57 49 57 53 56 52
XR25 | 8027 23 10 --- --- 33 --- 16 | 60 54 --- --- 47 --- 51
XR26 |43691 29 --- --- 37 81 --- 36 | 61 --- --- 48 62 --- 51
------+-----------------------------------------+-------------------------------------
RMS | 1693 22 25 22 22 26 30 |T 56 56 59 54 59 49 53
WRMS | 1693 22 19 19 19 23 26 |NE 53 51 55 48 55 45 49
MEDI | 1630 15 16 15 19 25 18 |MD 56 57 56 53 57 46 52
Table 3.2335.5 GPS week: 2335 Day: 5 MJD: 60594
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 845 45 26 21 34 14 51 14 | 37 41 44 38 34 30 33
R02 | 1554 11 14 11 8 13 13 5 | 19 27 21 18 22 16 17
R03 | 1488 14 10 12 19 15 14 6 | 18 23 26 21 31 22 19
R04 | 946 7 12 13 12 8 16 5 | 19 22 23 21 19 15 16
R05 | 2562 18 8 19 8 14 25 7 | 25 21 29 22 23 21 19
R07 | 811 11 14 17 16 10 7 6 | 30 25 29 26 26 25 24
R08 | 1008 13 16 11 21 27 23 8 | 27 25 32 31 25 34 25
R09E | 1311 16 11 16 15 16 19 7 | 55 54 58 64 58 63 57
R11E | 1276 14 9 16 13 15 15 6 | 25 32 34 27 31 25 29
R12E | 2380 13 15 13 27 17 19 8 | 76 76 77 73 76 79 75
R14E | 2399 12 15 18 29 16 14 8 | 77 80 82 76 83 77 78
R15E | 2030 15 12 15 14 11 11 5 | 95 94 95 94 91 59 93
R16E | 1707 14 24 32 15 21 26 10 | 54 61 75 52 46 43 53
R17 | 540 10 16 13 10 22 25 7 | 45 36 35 44 52 28 39
R18 | 1873 17 22 13 15 12 34 8 | 36 43 37 39 38 28 37
R19 | 3219 75 50 49 49 33 55 23 | 48 62 72 43 45 64 48
R20 | 2885 79 19 37 47 17 43 19 | 54 31 45 40 45 55 31
R21 | 1543 7 19 12 12 12 14 6 | 40 31 35 43 43 53 38
R22 | 1206 16 12 15 7 11 13 5 | 48 49 57 57 53 56 52
R24 | 1247 20 19 29 17 21 14 9 | 39 40 38 30 44 32 34
XR25 |12273 20 11 --- --- 18 --- 11 | 37 33 --- --- 38 --- 34
XR26 |40161 40 --- --- 24 38 --- 24 | 40 --- --- 55 52 --- 50
------+-----------------------------------------+-------------------------------------
RMS | 1791 29 19 21 23 17 26 |T 42 43 47 43 44 41 40
WRMS | 1791 21 16 17 23 16 22 |NE 35 33 37 35 36 34 32
MEDI | 1543 14 15 15 15 15 16 |MD 39 36 37 40 43 32 34
Table 3.2335.6 GPS week: 2335 Day: 6 MJD: 60595
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac jgx IGL | cod esa gfz grg iac jgx IGL
------+-----------------------------------------+-------------------------------------
R01 | 664 37 21 14 28 14 41 12 | 46 40 43 39 41 30 37
R02 | 797 13 16 22 10 19 12 7 | 28 28 22 24 28 21 20
R03 | 940 8 13 9 24 14 16 6 | 22 32 24 32 22 23 23
R04 | 884 13 13 15 12 15 10 6 | 25 33 31 24 26 28 25
R05 | 2264 14 11 11 15 11 11 5 | 31 34 34 32 32 27 30
R07 | 968 18 15 11 15 9 15 6 | 35 28 30 35 31 32 30
R08 | 797 14 13 16 24 19 8 7 | 32 31 42 29 32 32 31
R09E | 2644 15 14 17 19 14 13 7 | 83 84 90 89 85 81 85
R11E | 1150 14 8 13 13 14 11 5 | 38 41 45 38 42 27 39
R12E | 2249 14 15 13 22 18 20 7 | 82 82 86 92 86 91 85
R14E | 4823 11 19 16 30 15 7 7 | 96 89 91 116 95 94 95
R15E | 2610 16 19 16 21 28 17 9 | 125 117 118 128 134 86 124
R16E | 1335 13 18 12 18 12 9 6 | 51 46 52 53 44 43 46
R17 | 526 7 19 10 22 11 22 7 | 66 61 65 65 66 48 61
R18 | 1057 10 19 15 12 16 16 6 | 55 65 57 55 61 49 56
R19 | 1986 50 47 54 83 43 72 26 | 90 72 123 85 106 56 85
R20 | 1002 50 47 31 41 42 41 19 | 79 47 61 54 62 59 54
R21 | 1811 7 10 8 11 12 19 5 | 73 70 75 77 70 63 70
R22 | 1189 15 14 12 14 14 11 6 | 52 56 57 60 57 53 54
R24 | 604 15 14 18 12 21 18 7 | 62 62 53 51 50 45 52
XR25 |10740 17 18 --- --- 15 --- 12 | 41 42 --- --- 47 --- 41
XR26 |42211 24 --- --- 27 33 --- 20 | 55 --- --- 56 66 --- 56
------+-----------------------------------------+-------------------------------------
RMS | 1818 22 21 19 27 20 25 |T 57 55 59 58 58 49 54
WRMS | 1818 18 17 13 19 17 21 |NE 49 46 51 47 49 40 45
MEDI | 1150 14 15 14 19 15 15 |MD 52 47 53 54 50 45 52
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