[IGSREPORT-29540] Wk 2281 IGLOS Final Orbits
acc
acc at igs.org
Fri Oct 13 04:16:43 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2281 (Sep 24, 2023 - Sep 30, 2023)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.2281.
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:
igl2281[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2281 in the SP3 format.
igl22817.sum Combination Report for GPS Week 2281.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
JGX started providing orbit and clock solutions from GPS week 2269. Their solutions
are currently excluded from the combinations until the IGS ACC assessments
are completed. However, they are included for comparison statistics only.
3. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 0.1 ns
1 | 0.8 ns
2 | -0.7 ns
3 | -1.9 ns
4 | 0.6 ns
5 | -18.5 ns
6 | -1.1 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 1.2281, 1a.2281).
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 2.2281.0-6)
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 3.2281.0-6).
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 2281 summary. (Sep 24, 2023 - Sep 30, 2023)
Table 1.2281.a GPS week : 2281 MJD: 60211.0-60217.0
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 5 -6 -8 22 .04 18 13 | 39068 -1419 2870 8798
| 0 0 2 10 16 21 .04 | 6877 2308
esa n/a| 0 0 -2 -10 -14 5 -.11 23 17 | -1478 -1342 2863 7017
| 1 1 1 8 13 17 .05 | 7024 1905
gfz n/a| 0 1 1 25 0 12 -.07 22 14 | 0 -1250 2876 7969
| 0 0 2 18 19 15 .01 | 0 2618
grg n/a| 2 -3 -6 -20 11 -49 .17 26 20 | -2504 -1206 2860 7408
| 1 1 2 27 22 17 .08 | 5892 2633
jgx n/a| 0 1 1 -16 6 92 -.24 33 33 | 42110 -1440 2872 8180
| 1 1 3 26 34 64 .05 | 6793 2765
Table 1.2281.b GPS week : 2281 MJD: 60211.0-60217.0
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 | 14 14 15 16 12 14 14 |
R02 | 6 6 6 7 7 9 10 |
R03 | 7 6 9 6 6 5 10 |
R04 | 8 7 7 6 7 7 7 |
R05 | 10 7 8 9 6 8 7 |
R07 | 7 5 9 10 7 6 8 |
R08 | 5 8 8 8 8 8 9 |
R09 | 9 8 10 9 9 10 8 |
R11 | 7 10 11 7 10 7 10 |
R12 | 7 8 8 8 7 8 10 |
R13 | 16 15 18 16 18 18 18 |
R14 | 6 8 7 8 7 7 7 |
R15 | 11 9 12 8 8 8 9 |
R16 | 10 10 10 11 9 11 11 |
R17 | 8 7 14 16 11 10 8 |
R18 | 10 8 10 14 14 11 10 |
R19 | 21 18 21 23 29 34 20 |
R20 | 39 24 27 32 35 31 29 |
R21 | 7 9 8 19 12 9 9 |
R22 | 7 7 11 8 10 8 14 |
R24 | 11 10 10 20 12 10 11 |
R25 | 13 14 14 15 11 9 14 |
R26 | 109 93 101 80 98 75 96 |
Table 1.2281.c GPS week : 2281 MJD: 60211.0-60217.0
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 2281 0 | -40 -42 92 62 -423 2080 79.5 2003 2003 | 63 0
brd 2281 1 | 47 -21 123 554 584 234 80.8 1843 1843 | 824 0
brd 2281 2 | -5 -37 5 -1068 -76 -4777 79.9 1883 1883 | -662 0
brd 2281 3 | 36 48 94 1056 -113 -8683 80.2 2024 2024 | -1919 0
brd 2281 4 | -91 -58 130 -1925 -3429 -5659 81.2 2072 2072 | 612 0
brd 2281 5 | 63 -28 75 -226 807 -7672 81.9 1839 1839 | -18466 0
brd 2281 6 | -16 34 90 -1370 -132 -13530 81.9 1757 1757 | -1138 0
-------------+------------------------------------------------------------+----------------
brd 2281 mean| 0 -15 87 -416 -397 -5429 80.7 1917 1917 | -2955 0
brd 2281 sdev| 54 40 40 1079 1406 5325 1.0 116 116 | 6908 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 2.2281.0 GPS week: 2281 Day: 0 MJD: 60211
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 -4 3 33 .01 18 13 | 39995 1565 2952 8602
esa n/a| 0 0 0 -10 -13 17 -.15 23 14 | -4292 755 2963 8129
gfz n/a| 0 0 4 30 -34 13 -.07 28 13 | 0 1176 3009 7858
grg n/a| 1 -1 -7 -6 46 -60 .23 18 15 | -915 1792 3002 7169
jgx n/a| 0 1 6 0 -58 54 -.32 30 30 | 43579 1765 3045 8046
Table 2.2281.1 GPS week: 2281 Day: 1 MJD: 60212
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 -16 5 33 .01 16 12 | 44622 -389 3281 8805
esa n/a| 0 0 0 -22 -15 -2 -.17 21 18 | 3627 42 3257 7822
gfz n/a| 0 2 0 28 -5 24 -.06 18 13 | 0 980 3246 8319
grg n/a| 2 -2 -3 1 7 -65 .22 17 15 | 70 836 3238 7721
jgx n/a| -1 0 0 -63 -14 108 -.28 34 31 | 46883 283 3256 8501
Table 2.2281.2 GPS week: 2281 Day: 2 MJD: 60213
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 -4 -11 39 .02 17 13 | 43492 -1315 2743 9475
esa n/a| 0 0 0 -6 -32 -14 -.16 23 19 | -10046 -1104 2744 6163
gfz n/a| 0 2 0 43 4 5 -.07 21 13 | 0 -842 2743 8094
grg n/a| 4 -1 -7 -60 20 -30 .30 26 20 | -244 -959 2729 7499
jgx n/a| 0 0 6 -19 11 189 -.26 33 33 | 46618 -984 2683 8161
Table 2.2281.3 GPS week: 2281 Day: 3 MJD: 60214
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 9 -12 -2 46 .08 22 17 | 41537 -3609 2775 8582
esa n/a| -1 -1 -2 -13 -19 -12 -.08 21 16 | -4414 -2990 2752 6449
gfz n/a| 0 2 0 49 2 -1 -.09 21 16 | 0 -3863 2741 7317
grg n/a| 3 -1 -7 -53 -8 -56 .12 33 24 | -218 -3577 2717 6872
jgx n/a| 0 4 1 -6 20 136 -.19 35 35 | 45002 -4120 2756 7543
Table 2.2281.4 GPS week: 2281 Day: 4 MJD: 60215
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 -36 1 .07 16 10 | 41894 481 2865 9204
esa n/a| 0 2 -4 -12 -10 21 -.04 28 20 | 7333 145 2839 7214
gfz n/a| 1 2 0 16 33 23 -.09 21 13 | 0 1017 2892 8354
grg n/a| 1 -6 -2 -24 23 -56 .09 34 24 | 109 701 2887 7877
jgx n/a| -1 1 -4 -37 25 107 -.21 33 33 | 45020 785 2844 8572
Table 2.2281.5 GPS week: 2281 Day: 5 MJD: 60216
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 2 16 .01 16 11 | 24364 -5102 2959 8832
esa n/a| 0 0 -3 -15 -20 -2 -.07 23 16 | -8432 -4564 2962 6948
gfz n/a| -1 1 3 10 6 -11 -.09 28 17 | 0 -5482 2940 7936
grg n/a| 3 -3 -7 -8 -23 -20 .14 28 22 | -15845 -5556 2900 7455
jgx n/a| 0 0 0 -6 15 58 -.25 33 34 | 27594 -5925 2963 8197
Table 2.2281.6 GPS week: 2281 Day: 6 MJD: 60217
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 -17 -24 -12 .10 20 14 | 37573 -1569 2517 8091
esa n/a| -3 0 -3 4 12 29 -.12 25 19 | 5873 -1684 2525 6394
gfz n/a| 0 1 4 -1 -1 30 -.06 17 12 | 0 -1741 2564 7909
grg n/a| 1 -4 -9 10 16 -55 .11 25 21 | -490 -1681 2549 7269
jgx n/a| 0 0 0 15 47 -9 -.19 36 33 | 40076 -1888 2557 8240
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 3.2281.0 GPS week: 2281 Day: 0 MJD: 60211
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 1455 32 27 17 16 48 14 | 104 83 90 86 82 90
R02 | 1933 10 10 9 11 20 6 | 58 64 64 54 53 59
R03 | 2372 9 9 15 11 31 6 | 61 62 63 70 54 63
R04 | 1593 13 13 14 9 24 7 | 60 67 66 60 53 62
R05 | 1289 11 17 20 20 31 10 | 56 67 70 52 47 59
R07 | 852 13 9 13 10 13 6 | 74 66 64 66 60 67
R08 | 878 7 5 8 9 13 4 | 67 70 71 64 66 68
R09 | 3954 12 9 17 17 10 8 | 43 47 41 39 37 41
R11 | 2273 13 8 9 15 --- 7 | 21 27 28 24 --- 22
R12 | 1669 7 13 11 13 21 6 | 60 61 65 70 55 63
R13 | 761 24 22 35 24 65 15 | 70 49 63 63 59 57
R14 | 1192 9 8 9 11 23 5 | 48 57 55 51 41 52
R15 | 470 14 17 18 23 19 10 | 71 55 60 86 60 68
R16 | 1354 15 22 10 14 19 9 | 77 60 64 69 54 67
R17E | 1606 10 13 19 14 --- 8 | 70 72 74 74 --- 71
R18E | 774 16 22 11 14 13 9 | 39 39 39 40 37 37
R19E | 810 34 30 41 38 40 21 | 106 102 116 113 109 106
R20E | 3148 43 75 101 31 49 38 | 70 86 130 69 56 69
R21E | 2381 9 14 13 13 13 7 | 47 46 48 46 44 45
R22E | 3945 14 9 10 13 15 6 | 34 38 35 44 34 36
R24E | 2108 12 22 15 21 28 10 | 47 43 37 52 49 43
XR25E |13237 12 14 --- --- --- 13 | 44 57 --- --- --- 49
XR26 |19323 100 --- 119 --- --- 109 | 447 --- 519 --- --- 476
------+------------------------------------+--------------------------------
RMS | 2003 18 23 28 18 30 |T 77 59 84 61 55 76
WRMS | 2003 13 14 13 15 30 |NE 87 59 92 61 55 87
MEDI | 1606 13 13 14 14 21 |MD 60 60 64 63 54 62
Table 3.2281.1 GPS week: 2281 Day: 1 MJD: 60212
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 525 21 32 26 15 32 14 | 65 52 81 60 63 64
R02 | 2187 6 9 13 12 26 6 | 38 41 48 36 33 40
R03 | 1407 10 10 11 8 18 5 | 37 46 36 36 38 38
R04 | 1078 12 12 10 14 48 7 | 37 39 35 31 31 35
R05 | 951 12 13 10 14 29 7 | 39 42 39 31 29 37
R07 | 1433 5 6 8 10 23 4 | 43 41 45 43 35 42
R08 | 950 5 14 17 16 16 8 | 38 36 49 42 41 40
R09 | 2869 17 9 12 11 18 7 | 40 44 39 44 34 40
R11 | 2637 18 11 18 16 21 9 | 21 25 25 16 19 18
R12 | 1266 10 11 18 10 27 7 | 50 49 62 49 47 51
R13 | 1016 16 40 24 23 68 15 | 58 40 69 54 47 52
R14 | 1726 12 11 11 16 22 7 | 43 52 40 53 39 45
R15 | 1072 8 16 12 21 25 8 | 53 48 45 66 50 52
R16 | 705 16 17 18 14 30 9 | 57 55 43 58 42 51
R17E | 2077 11 14 9 14 --- 7 | 79 75 84 87 --- 80
R18E | 1097 9 21 11 13 26 8 | 32 36 33 34 36 32
R19E | 1381 34 29 27 33 44 18 | 144 160 148 147 145 148
R20E | 2885 37 55 41 28 67 23 | 56 66 72 56 87 51
R21E | 1469 10 19 11 17 18 8 | 41 44 41 44 40 40
R22E | 3564 13 9 13 13 17 7 | 37 37 44 47 37 40
R24E | 2482 10 17 17 20 35 9 | 40 38 40 41 37 37
XR25E |12341 11 15 --- --- --- 13 | 48 45 --- --- --- 45
XR26 |15220 87 --- 98 --- --- 92 | 276 --- 312 --- --- 283
------+------------------------------------+--------------------------------
RMS | 1842 16 21 18 17 34 |T 59 50 65 51 46 59
WRMS | 1842 12 18 13 15 31 |NE 59 43 64 44 39 59
MEDI | 1433 12 14 13 14 26 |MD 43 44 44 44 38 42
Table 3.2281.2 GPS week: 2281 Day: 2 MJD: 60213
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 778 28 32 16 24 49 15 | 75 61 70 70 70 68
R02 | 1696 10 8 12 12 21 6 | 48 56 61 54 57 54
R03 | 1025 10 20 16 16 17 9 | 46 41 51 57 45 46
R04 | 1038 16 12 7 10 21 7 | 46 35 40 40 39 39
R05 | 1091 9 13 18 12 34 7 | 45 45 45 42 32 43
R07 | 1464 13 16 12 17 28 8 | 51 58 59 47 44 53
R08 | 1703 8 11 13 20 17 7 | 50 50 49 41 51 47
R09 | 2308 13 13 15 25 26 9 | 20 28 26 38 23 23
R11 | 2581 12 12 13 35 26 11 | 22 32 28 34 28 24
R12 | 2043 9 12 12 19 --- 7 | 58 62 47 61 --- 56
R13 | 928 23 45 14 40 41 18 | 64 33 50 72 46 52
R14 | 1289 12 9 10 16 22 7 | 38 43 38 47 38 39
R15 | 1642 12 29 18 22 25 12 | 49 39 63 65 48 51
R16 | 605 15 19 18 13 30 9 | 52 51 70 67 48 58
R17E | 1962 16 18 22 38 --- 13 | 119 128 129 143 --- 126
R18E | 709 8 26 15 16 26 10 | 47 54 51 57 45 49
R19E | 1949 36 24 28 57 40 21 | 103 103 108 89 100 98
R20E | 3989 30 52 61 36 77 27 | 59 56 79 49 71 47
R21E | 1373 11 10 13 17 23 7 | 51 49 50 54 51 49
R22E | 3226 14 10 21 26 20 10 | 27 28 33 41 33 27
R24E | 2115 17 17 16 15 26 9 | 58 60 63 57 54 57
XR25E |14419 11 16 --- --- --- 13 | 35 44 --- --- --- 38
XR26 |16101 95 --- 107 --- --- 101 | 322 --- 431 --- --- 371
------+------------------------------------+--------------------------------
RMS | 1882 17 23 21 26 33 |T 64 52 74 58 48 65
WRMS | 1882 13 19 13 20 33 |NE 65 45 75 52 43 68
MEDI | 1696 13 16 15 19 26 |MD 50 49 51 54 46 49
Table 3.2281.3 GPS week: 2281 Day: 3 MJD: 60214
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 782 35 22 25 27 45 16 | 87 66 74 71 85 74
R02 | 694 16 11 11 10 19 7 | 52 55 54 48 48 51
R03 | 869 10 10 7 13 16 5 | 56 70 64 72 63 64
R04 | 966 11 7 11 9 13 5 | 58 60 61 62 65 59
R05 | 2472 14 16 16 13 28 8 | 53 60 46 53 42 52
R07 | 2290 12 14 12 29 27 9 | 61 62 64 45 51 58
R08 | 2407 14 8 15 12 32 7 | 58 64 73 61 49 64
R09 | 1809 17 9 17 13 27 8 | 26 29 33 29 29 26
R11 | 2375 12 11 14 10 22 7 | 29 30 29 27 24 27
R12 | 2190 10 12 14 15 23 7 | 57 58 70 68 53 62
R13 | 1481 25 31 19 38 28 16 | 74 54 60 85 48 65
R14 | 1014 7 15 18 13 24 8 | 48 55 38 51 42 46
R15 | 1380 8 15 9 22 16 7 | 61 47 58 66 52 56
R16 | 858 19 19 13 25 25 11 | 54 56 50 40 50 49
R17E | 1637 20 21 19 48 --- 15 | 77 88 83 118 --- 86
R18E | 755 15 25 14 42 23 14 | 50 57 53 65 51 51
R19E | 1961 43 33 41 44 62 23 | 186 190 168 187 184 179
R20E | 4396 54 57 56 47 91 31 | 71 90 75 78 105 62
R21E | 2432 18 19 21 66 28 18 | 55 49 56 78 50 50
R22E | 3025 14 10 13 21 24 8 | 42 37 42 48 33 40
R24E | 2246 24 16 22 67 22 19 | 86 87 91 113 83 87
XR25 |16875 15 14 --- --- --- 14 | 25 37 --- --- --- 29
XR26 |16057 81 --- 78 --- --- 80 | 367 --- 428 --- --- 395
------+------------------------------------+--------------------------------
RMS | 2024 22 21 21 33 35 |T 75 63 80 69 60 75
WRMS | 2024 17 15 16 24 35 |NE 76 54 80 55 50 76
MEDI | 1961 15 15 15 22 24 |MD 57 57 60 65 50 58
Table 3.2281.4 GPS week: 2281 Day: 4 MJD: 60215
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 826 19 27 14 25 52 12 | 75 69 73 59 69 71
R02 | 538 9 13 12 19 19 7 | 46 45 46 41 38 44
R03 | 720 7 12 11 9 15 5 | 53 57 59 49 52 54
R04 | 1027 9 16 9 16 21 6 | 50 65 59 46 58 54
R05 | 2991 8 13 9 13 15 6 | 41 49 50 44 53 45
R07 | 1565 9 12 12 17 20 7 | 53 57 44 50 46 50
R08 | 3230 11 12 13 17 10 7 | 50 61 59 46 57 53
R09 | 2063 10 21 14 21 23 9 | 18 29 26 21 19 19
R11 | 2002 10 12 25 18 18 9 | 16 23 29 27 20 17
R12 | 1496 9 11 14 15 12 7 | 65 63 74 69 62 67
R13 | 1427 18 49 28 32 42 18 | 83 50 86 73 68 74
R14 | 972 7 14 10 15 21 6 | 55 61 53 54 42 54
R15 | 1301 8 17 9 22 13 7 | 59 47 55 69 52 56
R16 | 985 12 23 12 18 13 9 | 65 57 65 64 63 62
R17E | 2164 5 29 9 31 --- 10 | 87 88 83 103 --- 87
R18E | 946 11 21 21 48 34 14 | 75 81 80 100 69 79
R19E | 2079 32 51 51 76 68 28 | 117 125 142 96 123 119
R20E | 5396 49 76 51 76 84 34 | 43 89 85 72 67 52
R21E | 943 9 16 14 44 25 11 | 65 66 70 99 69 70
R22E | 2650 13 13 13 30 14 9 | 28 39 41 43 36 34
R24E | 1627 9 22 15 38 20 11 | 110 106 102 128 104 108
XR25 |17865 8 14 --- --- --- 10 | 31 32 --- --- --- 31
XR26 |15141 84 --- 114 --- --- 98 | 287 --- 391 --- --- 325
------+------------------------------------+--------------------------------
RMS | 2071 16 28 21 34 33 |T 68 61 80 64 58 70
WRMS | 2071 10 20 13 24 33 |NE 67 52 77 50 49 69
MEDI | 1565 9 16 13 21 20 |MD 55 57 59 59 57 54
Table 3.2281.5 GPS week: 2281 Day: 5 MJD: 60216
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 677 15 16 31 35 34 13 | 68 85 89 47 82 72
R02 | 638 13 17 17 13 17 8 | 38 58 52 43 41 46
R03 | 729 6 10 9 13 20 5 | 46 47 47 51 41 46
R04 | 2018 11 13 14 11 21 7 | 41 31 40 40 36 37
R05 | 3147 5 8 16 25 13 8 | 32 32 24 51 41 31
R07 | 687 6 8 9 15 27 5 | 47 41 42 54 33 45
R08 | 2938 8 11 21 11 14 7 | 42 45 37 39 35 39
R09 | 3774 10 11 20 30 17 10 | 21 29 40 25 31 24
R11 | 1508 9 11 13 12 13 6 | 20 26 25 26 18 22
R12 | 1277 7 13 11 23 15 7 | 47 37 46 62 39 46
R13 | 1137 22 49 22 26 47 18 | 71 41 75 75 57 63
R14 | 1001 6 12 12 17 30 6 | 54 48 50 63 33 52
R15 | 767 8 13 8 22 26 7 | 54 50 52 59 35 53
R16 | 885 12 22 20 19 16 10 | 53 52 62 44 48 51
R17E | 2142 11 18 17 27 --- 10 | 85 93 99 91 --- 90
R18E | 1129 12 14 15 32 26 10 | 36 42 39 60 33 40
R19E | 1575 21 40 95 72 65 33 | 174 171 193 173 172 171
R20E | 3067 50 62 52 47 85 30 | 57 92 68 72 65 56
R21E | 769 8 20 14 16 29 8 | 43 35 45 49 34 41
R22E | 1804 11 12 12 22 14 8 | 41 42 46 53 40 43
R24E | 1769 14 18 12 26 23 10 | 39 53 50 55 48 45
XR25E |15311 7 11 --- --- --- 9 | 40 41 --- --- --- 39
XR26 |14283 57 --- 98 --- --- 75 | 309 --- 323 --- --- 303
------+------------------------------------+--------------------------------
RMS | 1839 16 23 28 28 33 |T 63 54 70 58 48 63
WRMS | 1839 11 16 17 22 34 |NE 62 44 66 48 40 62
MEDI | 1508 11 13 15 22 21 |MD 46 42 47 53 39 46
Table 3.2281.6 GPS week: 2281 Day: 6 MJD: 60217
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg jgx IGL | cod esa gfz grg jgx IGL
------+------------------------------------+--------------------------------
R01 | 721 19 27 20 30 45 14 | 98 93 99 92 90 95
R02 | 596 19 20 12 14 12 9 | 60 78 67 61 63 65
R03 | 793 16 10 20 15 37 9 | 71 77 87 79 64 77
R04 | 2517 12 15 9 11 29 6 | 70 64 69 67 55 67
R05 | 3361 9 15 13 11 17 7 | 56 63 54 64 58 57
R07 | 1142 15 11 15 15 26 8 | 74 60 60 68 54 65
R08 | 1353 13 11 18 13 30 8 | 65 68 82 73 59 72
R09 | 2410 14 7 14 16 16 7 | 55 52 59 46 51 53
R11 | 1283 18 13 15 19 --- 9 | 43 45 41 42 --- 41
R12 | 1511 9 17 15 28 29 10 | 64 58 66 80 54 65
R13 | 661 28 48 18 29 74 18 | 96 59 89 89 75 82
R14 | 1682 11 14 9 16 19 7 | 72 72 77 86 65 76
R15 | 1461 7 23 16 13 18 9 | 79 62 86 88 70 78
R16 | 1503 16 16 19 21 17 10 | 73 63 81 62 62 69
R17 | 2742 8 19 9 20 --- 8 | 97 98 102 105 --- 99
R18E | 1001 13 19 11 21 28 9 | 64 67 65 80 63 67
R19E | 1590 26 40 24 45 53 19 | 155 161 152 160 161 155
R20E | 2010 54 61 36 52 75 29 | 103 118 89 143 106 104
R21E | 986 14 22 8 17 33 9 | 69 65 68 73 67 67
R22E | 2592 20 22 15 38 17 14 | 36 33 47 55 37 39
R24E | 1543 20 16 14 24 27 11 | 83 79 82 93 75 82
XR25 |13844 12 15 --- --- --- 13 | 32 28 --- --- --- 29
XR26 |15602 103 --- 89 --- --- 96 | 479 --- 539 --- --- 500
------+------------------------------------+--------------------------------
RMS | 1757 20 25 17 25 36 |T 91 71 98 81 69 91
WRMS | 1757 14 19 12 21 33 |NE 97 65 103 71 63 97
MEDI | 1511 15 16 15 19 28 |MD 71 64 77 79 63 69
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