[IGSREPORT-29342] Wk 2262 IGLOS Final Orbits
acc
acc at igs.org
Mon Jun 5 03:46:06 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2262 (May 14, 2023 - May 20, 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 2.2262.
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:
igl2262[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2262 in the SP3 format.
igl22627.sum Combination Report for GPS Week 2262.
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. 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.
3. 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).
4. 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
5. 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 | -1.0 ns
1 | -0.2 ns
2 | -0.3 ns
3 | -18.4 ns
4 | -1.4 ns
5 | 0.5 ns
6 | -0.1 ns
6. 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 R22
1 | ESA | R20 R22
2 | ESA | R20 R22
3 | ESA | R20 R22
4 | ESA | R20 R22
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 1.2262, 1a.2262).
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 2.2262.0-6)
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 3.2262.0-6).
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 2262 summary. (May 14, 2023 - May 20, 2023)
Table 1.2262.a GPS week : 2262 MJD: 60078.0-60084.0
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 1 -10 -12 13 .04 20 16 | 39969 -1256 3080 9257
| 1 1 2 18 17 17 .04 | 7000 1288
esa n/a| 0 0 0 0 -8 -7 -.14 44 25 | -3279 -415 3103 8312
| 1 1 2 13 12 16 .01 | 8305 1623
gfz n/a| 0 0 0 35 6 -32 -.08 23 15 | 0 -1107 3102 8566
| 0 1 2 15 19 30 .04 | 0 1232
grg n/a| 1 0 -2 -38 26 7 .19 28 23 | -2606 -1127 3090 7891
| 1 0 3 21 21 44 .04 | 6800 1225
iac n/a| -1 -1 0 -21 9 -22 -.26 24 21 | -1144 -223 3053 9233
| 2 2 2 24 40 63 .07 | 7084 881
Table 1.2262.b GPS week : 2262 MJD: 60078.0-60084.0
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 19 16 20 20 26 25 |
R02 | 8 6 4 8 10 7 6 |
R03 | 8 7 5 6 7 6 7 |
R04 | 10 10 9 8 7 6 6 |
R05 | 8 7 7 8 9 7 7 |
R07 | 7 8 8 8 8 7 6 |
R08 | 8 8 10 8 6 6 9 |
R09 | 10 7 8 8 7 18 11 |
R11 | 8 9 10 7 7 9 12 |
R12 | 10 13 10 11 9 10 23 |
R13 | 18 23 21 23 22 20 31 |
R14 | 9 7 8 8 8 10 21 |
R15 | 8 7 10 10 7 10 10 |
R16 | 21 19 21 21 17 21 28 |
R17 | 6 8 7 7 7 16 8 |
R18 | 9 9 8 9 7 12 9 |
R19 | 23 24 23 29 21 22 21 |
R20 | 29 24 23 25 20 44 42 |
R21 | 10 8 9 9 7 8 10 |
R22 | 22 9 16 11 15 15 7 |
R24 | 14 16 13 9 11 10 12 |
R25 | 0 0 0 0 0 14 10 |
Table 1.2262.c GPS week : 2262 MJD: 60078.0-60084.0
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 2262 0 | 62 19 187 -1027 -455 -754 78.5 1792 1792 | -981 0
brd 2262 1 | 41 20 190 -1352 -1751 -5212 81.0 1721 1721 | -170 0
brd 2262 2 | 42 -41 259 -1351 -2419 -4687 80.1 2067 2067 | -339 0
brd 2262 3 | 36 65 212 451 1299 5884 79.5 1826 1826 | -18448 0
brd 2262 4 | -27 1 327 788 825 8167 79.5 1643 1643 | -1411 0
brd 2262 5 | -99 -33 168 384 760 6853 80.9 1739 1739 | 483 0
brd 2262 6 | -70 -31 173 607 561 3752 81.6 2214 2214 | -147 0
-------------+------------------------------------------------------------+----------------
brd 2262 mean| -1 0 217 -214 -168 2000 80.1 1857 1857 | -3001 0
brd 2262 sdev| 63 38 57 977 1425 5538 1.1 206 206 | 6838 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 2.2262.0 GPS week: 2262 Day: 0 MJD: 60078
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 0 -19 -32 2 .02 18 16 | 45523 -2475 3410 9584
esa n/a| 0 -3 -1 1 -23 -25 -.16 47 26 | -1032 -1557 3519 7116
gfz n/a| 0 2 3 42 45 -47 -.03 24 16 | 0 -2172 3480 8601
grg n/a| 0 0 -3 -29 15 42 .17 24 22 | 45 -2316 3484 7982
iac n/a| 0 0 -4 -3 77 -23 -.26 22 19 | 1988 -1753 3462 9491
Table 2.2262.1 GPS week: 2262 Day: 1 MJD: 60079
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 0 -5 -20 0 .03 18 15 | 43793 249 3012 9215
esa n/a| -1 -1 0 -3 7 -12 -.13 50 25 | -2517 1346 3038 8432
gfz n/a| 0 0 0 18 3 -66 -.03 25 19 | 0 -160 3032 8751
grg n/a| 0 -1 -3 -23 35 29 .13 22 20 | -163 -124 3014 8105
iac n/a| -1 1 0 -31 2 -27 -.27 22 19 | 1594 -71 2976 9248
Table 2.2262.2 GPS week: 2262 Day: 2 MJD: 60080
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 2 1 -14 14 29 .01 22 18 | 44911 -1376 2929 9201
esa n/a| 0 0 2 26 -6 -25 -.15 47 23 | -11052 -395 2957 8839
gfz n/a| -1 0 -2 35 -12 -43 -.13 22 14 | 0 -1136 2943 8701
grg n/a| 0 -1 -2 -30 24 23 .17 20 16 | 77 -1251 2935 7856
iac n/a| -5 0 1 -59 -8 25 -.34 22 19 | 1838 -473 2897 9253
Table 2.2262.3 GPS week: 2262 Day: 3 MJD: 60081
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 4 20 -12 0 -.02 18 14 | 25014 -1462 3237 8967
esa n/a| 0 0 0 -9 -6 20 -.14 46 24 | -12769 -1229 3332 7883
gfz n/a| 0 0 -2 26 4 7 -.09 26 17 | 0 -1093 3327 8463
grg n/a| 0 -1 -5 -27 18 -24 .16 23 18 | -18026 -1301 3303 7654
iac n/a| 0 -3 -2 -12 -44 -59 -.29 21 20 | -17179 513 3233 9032
Table 2.2262.4 GPS week: 2262 Day: 4 MJD: 60082
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 2 -35 2 24 .06 18 16 | 40658 -3240 3468 8634
esa n/a| 0 2 -1 -3 -25 2 -.15 43 21 | 12728 -2972 3482 10604
gfz n/a| 0 1 -3 67 -11 0 -.11 23 16 | 0 -3204 3465 8021
grg n/a| 2 0 1 -19 26 -31 .21 21 18 | -51 -3015 3445 7608
iac n/a| -2 -3 -1 -4 38 -32 -.24 22 19 | 646 -901 3400 8624
Table 2.2262.5 GPS week: 2262 Day: 5 MJD: 60083
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 4 -34 -2 .05 23 15 | 40044 54 2776 9506
esa n/a| -2 0 1 -15 -7 -1 -.13 38 27 | -4291 1444 2718 6541
gfz n/a| 0 0 0 33 4 -9 -.09 21 13 | 0 324 2741 8536
grg n/a| 3 0 1 -62 67 -55 .23 35 25 | 113 355 2732 7805
iac n/a| 0 0 1 5 21 -122 -.30 30 27 | 1327 618 2717 9398
Table 2.2262.6 GPS week: 2262 Day: 6 MJD: 60084
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 1 -25 -6 39 .12 23 17 | 39842 -545 2733 9692
esa n/a| -1 0 4 2 5 -11 -.12 37 26 | -4022 453 2681 8773
gfz n/a| 0 0 0 28 8 -65 -.09 20 12 | 0 -312 2730 8893
grg n/a| 3 0 -8 -75 0 65 .23 54 39 | -238 -240 2721 8233
iac n/a| -4 -4 0 -46 -17 81 -.13 32 28 | 1775 504 2691 9588
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 3.2262.0 GPS week: 2262 Day: 0 MJD: 60078
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 676 18 36 24 37 23 17 | 87 56 84 80 67 75
R02 | 852 16 6 13 12 16 7 | 63 59 63 63 69 61
R03 | 1014 8 14 13 20 10 8 | 66 64 66 75 69 67
R04M | 655 23 13 14 10 22 9 | 63 52 55 55 50 56
R05M | 1387 14 19 10 12 19 8 | 46 55 45 42 42 45
R07M | 1947 8 12 18 8 25 7 | 70 67 75 73 79 70
R08 | 1436 16 13 7 13 11 7 | 66 82 80 82 81 77
R09E | 4064 11 16 18 24 11 10 | 25 30 38 30 29 25
R11E | 2146 15 10 12 13 15 7 | 25 24 29 28 25 24
R12E | 2162 12 16 15 24 37 10 | 166 159 165 173 155 165
R13E | 2582 30 30 36 23 39 17 | 40 48 59 53 43 41
R14E | 1518 14 11 15 21 12 9 | 89 92 91 93 86 89
R15E | 1490 12 11 13 15 16 7 | 45 40 45 49 51 42
R16E | 2148 29 20 60 20 28 20 | 50 52 63 58 50 50
R17M | 1796 8 9 10 11 25 5 | 46 40 44 43 52 43
R18M | 845 11 21 13 16 14 9 | 31 36 33 31 42 31
R19M | 2146 32 49 23 47 16 22 | 65 50 60 64 65 56
R20M | 1106 31 189 40 52 27 29 | 122 66 127 122 122 120
R21M | 817 7 28 13 14 25 9 | 57 51 62 61 62 56
XR22M | 4320 --- 315 21 21 22 21 | --- 119 34 49 41 39
R24 | 1309 18 20 33 26 25 14 | 64 51 60 69 65 57
XR25M |12102 2 --- --- --- 27 0 | 35 --- --- --- 37 34
------+------------------------------------+--------------------------------
RMS | 1791 18 47 24 24 22 |T 62 61 65 66 62 60
WRMS | 1791 16 26 16 22 19 |NE 69 62 70 73 70 67
MEDI | 1490 14 16 15 20 22 |MD 63 52 60 61 52 56
Table 3.2262.1 GPS week: 2262 Day: 1 MJD: 60079
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 699 31 44 18 29 26 18 | 58 37 51 53 51 48
R02 | 1003 10 9 12 8 28 5 | 40 47 50 39 56 43
R03 | 914 11 13 13 12 10 7 | 41 44 35 46 43 40
R04M | 588 19 15 21 15 10 10 | 41 36 37 38 38 37
R05M | 911 14 13 11 8 18 6 | 34 27 24 32 25 28
R07M | 1312 7 15 11 19 15 8 | 53 57 48 44 53 49
R08 | 901 11 11 13 17 16 7 | 48 51 52 55 51 50
R09E | 3724 9 11 18 11 12 7 | 18 24 31 20 26 20
R11E | 2202 14 15 16 14 14 8 | 20 19 29 19 25 17
R12E | 2551 16 16 19 36 17 13 | 129 133 135 130 128 129
R13E | 1909 29 37 59 24 43 22 | 44 43 94 46 53 49
R14E | 1132 9 14 12 13 12 7 | 83 84 81 83 82 81
R15E | 1894 10 11 13 15 29 7 | 37 40 40 48 35 39
R16E | 1711 18 19 58 24 19 19 | 34 34 34 47 34 33
R17M | 955 8 17 15 10 21 7 | 23 25 27 35 27 25
R18M | 1033 9 20 13 15 27 8 | 22 23 19 24 26 20
R19M | 2423 37 54 25 41 25 23 | 57 34 44 37 43 39
R20M | 1662 29 202 30 40 22 23 | 58 53 46 38 44 48
R21M | 803 8 17 16 13 18 8 | 27 28 31 27 27 25
XR22M | 4252 --- 318 9 9 17 9 | --- 76 27 28 19 25
R24 | 2286 23 27 34 25 21 15 | 39 27 34 41 37 29
XR25M |13460 1 --- --- --- 20 0 | 21 --- --- --- 33 20
------+------------------------------------+--------------------------------
RMS | 1720 18 50 25 22 22 |T 44 44 46 44 43 40
WRMS | 1720 15 25 19 20 19 |NE 45 41 44 46 47 42
MEDI | 1312 11 16 16 15 18 |MD 40 37 37 39 37 37
Table 3.2262.2 GPS week: 2262 Day: 2 MJD: 60080
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 726 32 32 17 27 24 16 | 71 47 55 61 58 56
R02 | 976 8 6 8 6 29 4 | 47 43 36 44 62 42
R03 | 754 12 7 6 9 14 5 | 42 48 44 50 49 46
R04M | 557 21 7 21 10 16 9 | 39 40 39 37 36 36
R05M | 778 14 12 11 8 21 6 | 28 26 18 26 18 23
R07M | 1208 13 16 8 15 16 8 | 50 64 61 59 51 58
R08 | 1287 22 15 16 12 15 9 | 49 70 71 53 55 60
R09E | 4517 14 10 16 12 18 7 | 17 28 33 21 26 23
R11E | 1866 15 10 26 15 15 10 | 18 28 46 22 29 26
R12E | 2985 11 19 12 22 18 10 | 89 96 95 92 93 92
R13E | 2258 29 38 41 35 36 21 | 44 35 57 47 45 39
R14E | 1426 12 10 11 20 14 8 | 54 53 49 51 52 50
R15E | 2717 18 16 17 15 12 9 | 50 59 64 54 50 55
R16E | 1269 30 25 58 17 27 20 | 34 37 49 40 34 35
R17M | 934 10 15 11 11 8 7 | 36 39 42 45 30 39
R18M | 1229 17 14 8 14 25 8 | 26 31 30 33 35 28
R19M | 2311 44 42 19 46 26 23 | 55 45 53 51 46 47
R20M | 1767 39 192 33 23 42 22 | 86 43 114 95 79 97
R21M | 973 17 19 6 13 17 8 | 38 32 34 40 39 34
XR22M | 3396 --- 310 17 15 20 16 | --- 87 27 29 25 26
R24 | 4315 16 28 25 18 13 13 | 48 41 52 52 40 46
XR25M |14328 2 --- --- --- 22 0 | 18 --- --- --- 29 18
------+------------------------------------+--------------------------------
RMS | 2066 22 47 22 20 22 |T 44 47 50 47 44 44
WRMS | 2066 18 23 14 16 19 |NE 51 49 51 52 52 50
MEDI | 1287 16 16 16 15 18 |MD 44 43 49 47 40 39
Table 3.2262.3 GPS week: 2262 Day: 3 MJD: 60081
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1138 34 42 29 32 18 20 | 80 41 69 50 56 59
R02 | 715 6 17 20 10 15 8 | 53 40 63 48 56 50
R03 | 1261 8 8 12 9 21 5 | 51 50 46 54 58 50
R04M | 602 16 5 19 7 16 7 | 36 33 38 32 29 33
R05M | 908 15 11 16 11 19 7 | 33 41 35 37 30 33
R07M | 1240 6 16 9 19 19 7 | 55 47 49 56 49 51
R08 | 1411 15 10 16 11 18 7 | 48 60 56 56 58 54
R09E | 4067 9 12 16 13 12 7 | 27 29 39 32 30 30
R11E | 2527 9 11 13 12 12 6 | 25 26 36 31 30 27
R12E | 1628 12 17 16 26 17 10 | 101 105 109 106 99 103
R13E | 1332 35 43 50 31 27 23 | 37 46 66 37 28 35
R14E | 969 11 9 11 18 13 7 | 83 83 81 93 87 84
R15E | 2830 17 15 9 23 16 10 | 64 52 52 56 52 54
R16E | 568 24 25 65 20 22 21 | 31 37 57 40 31 36
R17M | 1147 6 18 14 9 15 7 | 36 37 42 45 40 38
R18M | 808 15 17 13 12 27 8 | 29 38 35 33 39 31
R19M | 2366 34 64 27 63 39 28 | 58 51 77 78 51 61
R20M | 2517 26 175 42 38 30 24 | 93 63 116 106 101 102
R21M | 1476 11 22 14 13 28 9 | 45 40 50 51 54 45
XR22M | 2139 --- 315 12 10 17 11 | --- 142 28 35 30 30
R24 | 2411 10 19 16 13 14 8 | 47 43 56 56 55 49
XR25M |11779 3 --- --- --- 38 0 | 36 --- --- --- 31 36
------+------------------------------------+--------------------------------
RMS | 1825 18 46 26 23 21 |T 50 52 57 53 49 49
WRMS | 1825 14 24 17 18 19 |NE 55 46 58 52 56 52
MEDI | 1332 12 17 16 13 18 |MD 47 43 52 50 49 45
Table 3.2262.4 GPS week: 2262 Day: 4 MJD: 60082
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 1032 39 43 27 23 16 20 | 73 37 60 61 50 56
R02 | 539 13 6 27 16 20 9 | 46 53 70 43 64 52
R03 | 1299 10 9 11 13 23 6 | 49 53 49 60 65 51
R04M | 790 13 6 17 11 17 7 | 42 35 33 41 41 37
R05M | 674 14 10 16 17 19 8 | 35 26 21 33 23 27
R07M | 1105 7 16 11 15 17 7 | 48 39 41 51 52 43
R08 | 770 11 8 8 12 14 5 | 41 43 43 52 47 44
R09E | 2956 12 12 15 10 19 7 | 20 26 29 23 30 22
R11E | 3106 12 10 11 16 14 7 | 17 20 25 28 23 18
R12E | 901 11 13 16 18 23 8 | 83 86 91 97 80 87
R13E | 694 33 24 59 29 37 22 | 29 38 89 42 32 38
R14E | 993 11 15 10 19 14 8 | 71 76 72 80 73 73
R15E | 2083 9 14 11 13 12 7 | 41 42 45 55 47 44
R16E | 876 20 26 45 20 22 17 | 29 39 34 38 27 28
R17M | 940 7 10 16 12 10 6 | 27 29 33 36 33 29
R18M | 631 13 16 8 9 21 7 | 23 28 30 30 30 26
R19M | 2719 36 37 16 50 22 21 | 45 47 43 47 37 41
R20M | 1934 20 175 32 31 37 19 | 57 62 71 58 72 62
R21M | 770 9 14 10 9 38 6 | 40 36 43 41 44 39
XR22M | 2049 --- 310 15 15 24 15 | --- 171 35 32 35 32
R24 | 3037 10 20 14 26 12 10 | 39 39 43 53 39 40
XR25M |17779 3 --- --- --- 38 0 | 17 --- --- --- 31 18
------+------------------------------------+--------------------------------
RMS | 1642 18 43 23 21 22 |T 41 48 47 47 44 41
WRMS | 1642 16 21 16 18 19 |NE 49 45 53 53 53 48
MEDI | 993 12 14 15 16 19 |MD 41 39 43 43 39 39
Table 3.2262.5 GPS week: 2262 Day: 5 MJD: 60083
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 567 47 76 22 24 19 26 | 75 45 58 62 56 55
R02 | 664 12 11 10 15 15 7 | 47 47 52 54 54 49
R03 | 1855 6 16 6 11 26 5 | 50 51 46 49 67 47
R04M | 574 9 11 7 12 10 5 | 44 46 49 45 46 45
R05M | 1017 10 6 13 13 15 6 | 36 33 37 39 36 35
R07M | 985 12 10 10 14 20 6 | 47 56 47 57 52 49
R08 | 891 10 14 5 15 17 6 | 39 45 40 47 48 41
R09E | 3948 13 22 19 62 37 17 | 25 24 32 66 30 24
R11E | 3082 11 10 14 25 14 8 | 30 30 34 32 33 28
R12E | 598 12 17 12 27 28 9 | 123 127 126 124 116 123
R13E | 829 24 43 39 25 34 19 | 40 49 79 57 47 52
R14E | 1307 15 19 11 26 45 10 | 115 129 117 130 118 119
R15E | 1257 12 19 12 28 35 10 | 73 73 72 80 56 72
R16E | 659 27 28 49 27 24 20 | 42 49 50 56 37 43
R17M | 896 15 24 25 48 19 16 | 23 21 29 47 29 21
R18M | 549 16 23 16 29 25 11 | 28 41 36 34 34 29
R19M | 1439 36 38 15 61 28 21 | 45 36 36 31 34 33
R20M | 3332 58 118 44 89 70 43 | 48 58 83 49 51 48
R21M | 746 10 18 8 22 43 8 | 31 26 24 34 42 27
XR22M | 2519 --- 26 20 15 46 14 | --- 118 34 30 30 28
R24 | 2904 14 26 15 16 16 10 | 38 34 31 47 36 33
XR25M |21236 10 17 --- --- 44 13 | 32 18 --- --- 45 27
------+------------------------------------+--------------------------------
RMS | 1739 23 38 21 35 30 |T 49 52 52 55 49 46
WRMS | 1739 15 27 13 25 27 |NE 49 44 45 51 52 45
MEDI | 985 12 19 14 25 25 |MD 42 45 46 49 45 41
Table 3.2262.6 GPS week: 2262 Day: 6 MJD: 60084
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 585 53 59 19 24 26 24 | 100 39 68 80 72 69
R02 | 784 10 9 6 22 23 6 | 63 58 68 67 66 63
R03 | 1600 13 11 8 14 25 6 | 70 73 74 78 76 73
R04M | 782 11 11 8 10 15 5 | 80 77 75 75 79 76
R05M | 997 10 12 7 21 37 6 | 59 52 53 57 67 54
R07M | 1064 13 7 8 14 29 6 | 64 67 63 72 76 64
R08 | 829 21 14 7 20 27 9 | 53 69 69 75 67 65
R09E | 4086 16 10 14 40 14 11 | 30 30 37 40 31 30
R11E | 2654 14 12 14 45 19 11 | 50 44 54 69 46 49
R12E | 729 26 18 15 101 61 22 | 231 234 235 254 234 234
R13E | 593 26 48 52 101 46 31 | 71 86 111 53 72 73
R14E | 2737 17 19 21 91 38 21 | 152 144 148 176 142 149
R15E | 1416 12 13 9 37 36 9 | 81 77 82 88 96 81
R16E | 1414 38 25 40 98 38 27 | 59 61 61 105 62 59
R17M | 936 12 15 11 19 28 8 | 44 40 46 47 55 43
R18M | 681 7 21 9 26 18 8 | 30 37 32 47 38 32
R19M | 952 35 36 14 71 32 21 | 65 45 62 60 51 57
R20M | 5787 41 128 32 77 50 41 | 99 64 95 110 105 89
R21M | 790 10 25 13 19 21 9 | 56 45 59 62 58 54
XR22M | 2457 --- 10 6 13 18 6 | --- 94 45 42 36 41
R24 | 4308 20 27 19 16 20 12 | 60 52 65 68 63 59
XR25M |19083 8 11 --- --- 31 10 | 28 22 --- --- 35 29
------+------------------------------------+--------------------------------
RMS | 2213 23 37 20 54 32 |T 73 68 76 82 73 70
WRMS | 2213 17 26 12 39 28 |NE 69 58 68 73 68 65
MEDI | 997 14 14 13 24 27 |MD 63 58 65 69 66 59
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