[IGSREPORT-29281] Wk 2256 IGLOS Final Orbits
acc
acc at igs.org
Mon Apr 24 02:14:06 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2256 (Apr 02, 2023 - Apr 08, 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 2.2256.
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:
igl2256[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2256 in the SP3 format.
igl22567.sum Combination Report for GPS Week 2256.
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 | -0.5 ns
1 | 1.4 ns
2 | 1.2 ns
3 | 0.9 ns
4 | -0.9 ns
5 | -0.1 ns
6 | -0.9 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 | R22
1 | ESA | R22
3 | ESA | R22
4 | ESA | R22
5 | ESA | R22
6 | ESA | 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 1.2256, 1a.2256).
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 2.2256.0-6)
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 3.2256.0-6).
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 2256 summary. (Apr 02, 2023 - Apr 08, 2023)
Table 1.2256.a GPS week : 2256 MJD: 60036.0-60042.0
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 0 -15 -19 49 .06 20 14 | 36117 14 3045 8899
| 1 0 1 8 15 23 .04 | 2143 1724
esa n/a| 0 0 0 -11 6 -27 -.08 28 20 | 632 447 3026 7806
| 0 0 1 11 21 30 .03 | 5825 1343
gfz n/a| 0 0 -1 25 -5 -43 -.11 29 15 | 0 -135 3006 8700
| 1 1 2 10 21 26 .05 | 0 1573
grg n/a| 1 -1 0 -4 20 18 .10 25 20 | 34 -61 2995 8053
| 2 1 2 20 23 33 .05 | 329 1303
iac n/a| -1 0 0 0 3 -14 -.29 31 27 | 2220 -435 3018 9258
| 2 2 4 26 32 66 .10 | 1178 514
Table 1.2256.b GPS week : 2256 MJD: 60036.0-60042.0
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 18 20 19 16 12 14 |
R02 | 7 9 8 14 25 10 7 |
R03 | 7 6 7 12 9 11 9 |
R04 | 5 7 10 10 10 8 7 |
R05 | 5 6 10 9 12 10 8 |
R07 | 8 9 11 7 7 6 9 |
R08 | 6 7 7 11 8 8 10 |
R09 | 13 10 8 10 12 10 11 |
R11 | 9 7 8 6 6 7 7 |
R12 | 11 9 10 13 7 14 10 |
R13 | 19 16 18 20 22 21 20 |
R14 | 7 8 9 8 10 10 8 |
R15 | 8 8 11 8 9 9 10 |
R16 | 24 22 25 22 23 24 22 |
R17 | 10 9 8 8 7 9 8 |
R18 | 20 13 11 9 9 7 8 |
R19 | 15 27 25 17 19 18 22 |
R20 | 35 37 35 33 43 34 34 |
R21 | 18 11 1058 0 25 29 21 |
R22 | 16 10 129 28 19 18 12 |
R24 | 17 12 11 11 9 11 9 |
Table 1.2256.c GPS week : 2256 MJD: 60036.0-60042.0
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 2256 0 | -6 22 100 -2564 -1173 2384 80.1 1892 1892 | -491 0
brd 2256 1 | -36 22 144 -1522 -1496 6197 80.3 1423 1423 | 1364 0
brd 2256 2 | -15 25 120 -292 -884 5720 81.5 1181 1181 | 1167 0
brd 2256 3 | 36 -56 90 136 706 5453 81.4 1823 1823 | 906 0
brd 2256 4 | 11 131 130 -1227 1058 4481 79.9 1648 1648 | -895 0
brd 2256 5 | 58 57 116 -536 206 2473 80.3 1746 1746 | -60 0
brd 2256 6 | -63 31 127 380 358 2742 80.2 1708 1708 | -927 0
-------------+------------------------------------------------------------+----------------
brd 2256 mean| -2 33 118 -803 -174 4207 80.5 1631 1631 | 152 0
brd 2256 sdev| 41 55 18 1033 997 1650 .6 248 248 | 982 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 2.2256.0 GPS week: 2256 Day: 0 MJD: 60036
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 -16 -25 48 .08 19 13 | 32498 -581 2886 8332
esa n/a| 0 -1 0 -1 -11 8 -.08 25 19 | 5614 -434 2892 6697
gfz n/a| 0 0 0 36 -1 -59 -.07 29 15 | 0 -1612 2885 8088
grg n/a| 1 0 2 -18 40 -13 .06 33 24 | -389 -496 2890 7385
iac n/a| -1 -2 -8 -34 60 -64 -.42 31 29 | 1407 101 2874 8649
Table 2.2256.1 GPS week: 2256 Day: 1 MJD: 60037
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 -14 -33 48 .10 19 12 | 33964 2262 3246 9778
esa n/a| 0 0 3 -13 7 -44 -.12 27 19 | -7479 1938 3203 9217
gfz n/a| 0 1 1 32 0 -59 -.11 32 13 | 0 1888 3109 9527
grg n/a| 2 -2 -4 -10 34 38 .04 24 17 | 354 1625 3170 9264
iac n/a| -5 1 -2 49 -2 129 -.37 30 28 | 3289 -3 3183 10085
Table 2.2256.2 GPS week: 2256 Day: 2 MJD: 60038
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 -26 -5 43 .13 24 18 | 36238 1154 3102 9481
esa n/a| 0 0 1 -17 32 -15 -.11 24 19 | -3307 1657 3130 8384
gfz n/a| -1 0 0 34 -5 0 -.15 28 17 | 0 1247 3084 9252
grg n/a| 4 0 0 2 -3 8 .18 28 20 | 177 1255 3123 8794
iac n/a| -5 0 -4 0 16 -7 -.24 36 26 | 3563 -1246 3120 9862
Table 2.2256.3 GPS week: 2256 Day: 3 MJD: 60039
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 2 -5 -20 99 .06 23 17 | 37682 1243 3081 8932
esa n/a| 0 -1 0 7 20 3 -.03 25 19 | 2286 1539 3021 8898
gfz n/a| -1 0 -3 20 17 -50 -.12 24 15 | 0 1200 3015 8673
grg n/a| 3 0 2 -32 -9 -24 .11 26 22 | 448 549 3002 7925
iac n/a| 0 0 1 11 8 -28 -.22 35 26 | 3373 -934 3006 9204
Table 2.2256.4 GPS week: 2256 Day: 4 MJD: 60040
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 0 -15 8 39 .00 23 14 | 38198 -1958 3009 9252
esa n/a| 0 0 0 -7 22 -75 -.09 34 21 | -4779 -226 2906 7466
gfz n/a| 0 0 -2 22 -41 -69 -.03 28 14 | 0 -1263 2949 8961
grg n/a| 0 -1 0 2 24 72 .14 26 23 | -363 -994 2803 8014
iac n/a| 3 1 3 4 -25 -43 -.33 33 25 | 1062 -601 2939 9508
Table 2.2256.5 GPS week: 2256 Day: 5 MJD: 60041
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 -23 -33 43 .04 16 13 | 37832 338 2946 8571
esa n/a| 0 0 0 -26 3 -22 -.06 33 22 | 7904 383 2948 6900
gfz n/a| 1 3 -2 6 15 -51 -.13 28 17 | 0 -391 2958 8535
grg n/a| -2 -3 -1 32 2 15 .06 23 19 | -93 -275 2921 7796
iac n/a| 0 -1 2 -10 -41 -40 -.15 26 26 | 2056 -21 2954 9079
Table 2.2256.6 GPS week: 2256 Day: 6 MJD: 60042
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 0 -3 -23 24 .02 16 13 | 36412 -2360 3046 7953
esa n/a| 0 0 0 -19 -28 -46 -.05 31 22 | 4185 -1725 3083 7080
gfz n/a| -1 0 -4 27 -25 -15 -.18 35 15 | 0 -2019 3042 7868
grg n/a| 0 -1 2 -8 52 35 .09 19 18 | 104 -2095 3056 7196
iac n/a| 0 -4 3 -17 9 -48 -.27 26 25 | 795 -342 3054 8419
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 3.2256.0 GPS week: 2256 Day: 0 MJD: 60036
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 586 27 19 38 33 28 16 | 76 54 51 57 51 60
R02 | 546 11 6 19 13 23 7 | 47 39 41 50 41 44
R03 | 644 10 13 13 12 22 7 | 61 60 69 56 64 62
R04 | 963 6 7 12 8 10 4 | 59 56 63 59 52 58
R05 | 2039 8 8 7 10 17 5 | 51 54 54 54 55 52
R07 | 717 8 7 20 18 19 7 | 65 66 58 68 67 63
R08 | 830 8 6 12 11 20 5 | 56 58 61 60 52 57
R09 | 3474 12 25 20 32 17 12 | 35 48 39 30 39 34
R11 | 838 13 14 24 10 24 9 | 65 60 69 63 63 63
R12 | 1155 7 19 28 16 25 10 | 70 82 62 64 61 69
R13 | 989 24 46 33 23 28 19 | 113 70 121 101 118 100
R14 | 1033 7 10 12 17 18 6 | 92 96 99 94 103 95
R15 | 726 8 11 14 21 27 7 | 98 94 96 88 78 94
R16 | 2036 22 33 71 28 29 23 | 147 150 147 131 136 142
R17 | 1523 18 10 13 27 54 10 | 130 125 123 138 109 128
R18E | 558 11 25 28 68 30 20 | 150 160 147 174 157 154
R19E | 792 18 24 35 29 35 15 | 183 190 194 192 197 188
R20E | 5060 53 72 49 64 72 34 | 59 116 106 77 68 71
R21E | 1406 21 13 20 59 29 17 | 9999 36 318 9999 54 9999
XR22E | 3242 --- 361 16 16 18 16 | --- 177 68 63 65 71
R24E | 3544 22 16 28 48 31 16 | 69 63 75 84 67 67
------+------------------------------------+--------------------------------
RMS | 1892 19 25 29 33 31 |T 85 88 98 85 80 83
WRMS | 1892 13 19 15 24 29 |NE 77 74 76 74 72 74
MEDI | 989 11 14 20 21 25 |MD 69 66 69 64 65 67
Table 3.2256.1 GPS week: 2256 Day: 1 MJD: 60037
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 582 30 37 21 30 26 17 | 38 55 43 29 32 37
R02 | 653 13 21 10 17 19 9 | 28 41 40 27 33 30
R03 | 533 9 10 15 8 36 6 | 40 40 45 35 49 39
R04 | 599 8 11 15 11 25 6 | 38 36 35 33 23 35
R05 | 1688 9 12 10 7 14 5 | 31 39 36 33 33 33
R07 | 1363 12 11 23 13 23 8 | 48 48 41 47 39 44
R08 | 1032 6 13 10 18 18 7 | 35 43 38 39 36 37
R09 | 2321 12 22 11 17 12 9 | 28 43 37 28 34 32
R11 | 975 10 14 11 11 18 6 | 41 42 38 38 41 39
R12 | 1099 6 17 14 23 20 9 | 44 59 60 41 43 49
R13 | 1378 19 42 25 19 34 16 | 71 45 72 71 78 63
R14 | 1233 9 14 12 17 24 7 | 64 62 56 67 78 62
R15 | 942 9 12 10 20 24 7 | 70 68 69 62 56 67
R16 | 1835 20 26 67 27 21 21 | 98 103 94 87 96 93
R17 | 699 11 13 12 21 19 8 | 55 54 53 69 59 56
R18E | 760 14 27 18 31 30 13 | 104 113 102 127 104 109
R19E | 1258 48 31 64 40 34 27 | 176 196 198 189 193 186
R20E | 3221 44 74 86 52 63 37 | 58 76 103 62 57 58
R21E | 1096 10 19 18 24 48 10 | 9999 31 395 9999 30 9999
XR22E | 3937 --- 374 11 9 29 10 | --- 162 71 74 72 75
R24E | 1969 15 11 32 22 37 12 | 62 58 55 67 60 58
------+------------------------------------+--------------------------------
RMS | 1423 19 27 32 24 30 |T 59 67 80 61 59 60
WRMS | 1423 12 19 13 17 28 |NE 48 51 50 47 48 47
MEDI | 1099 11 17 15 19 24 |MD 48 54 55 47 49 49
Table 3.2256.2 GPS week: 2256 Day: 2 MJD: 60038
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 803 39 34 30 31 25 20 | 56 48 48 43 32 45
R02 | 742 14 14 6 20 23 8 | 32 42 35 25 24 30
R03 | 618 13 9 9 15 23 7 | 44 52 55 68 61 51
R04 | 601 22 15 19 8 16 10 | 50 35 40 45 36 41
R05 | 1279 11 10 20 22 22 9 | 33 34 39 46 41 34
R07 | 1732 14 15 22 24 26 11 | 44 42 34 45 53 39
R08 | 1539 9 13 9 13 41 6 | 44 44 37 43 67 42
R09 | 843 13 14 13 16 15 8 | 33 38 41 33 40 35
R11 | 1210 10 13 13 16 15 7 | 48 44 42 56 48 47
R12 | 1160 12 21 12 22 15 10 | 43 45 31 34 43 36
R13 | 646 23 40 26 34 21 18 | 93 73 77 110 95 82
R14 | 916 16 16 12 15 19 8 | 90 90 95 101 87 92
R15 | 1026 18 14 21 20 17 10 | 76 69 57 70 65 66
R16 | 1011 29 31 71 27 31 25 | 134 126 139 131 129 132
R17 | 867 11 12 13 19 18 8 | 53 41 46 51 49 46
R18E | 785 7 21 19 25 24 10 | 75 83 68 79 71 75
R19E | 1188 41 33 41 57 73 24 | 133 132 157 169 137 143
R20E | 1360 61 57 57 62 104 34 | 68 98 89 105 72 78
XR21E |10381 983 --- 1138 --- 56 1058 | 9999 --- 664 --- 34 9999
XR22E | 2915 --- 238 141 136 144 128 | --- 188 90 101 98 165
R24E | 2459 18 14 17 21 24 10 | 57 50 57 56 45 53
------+------------------------------------+--------------------------------
RMS | 1180 24 24 28 28 36 |T 63 68 92 70 63 66
WRMS | 1180 18 19 17 20 26 |NE 58 54 54 60 58 54
MEDI | 1026 14 15 19 21 23 |MD 53 48 55 56 53 47
Table 3.2256.3 GPS week: 2256 Day: 3 MJD: 60039
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 737 34 41 22 29 23 19 | 64 48 41 62 44 50
XR02 | 626 15 --- 26 17 57 14 | 42 --- 67 46 30 49
XR03 | 805 15 18 14 --- 21 11 | 49 39 51 --- 56 46
R04 | 739 17 14 12 22 15 9 | 51 50 45 41 42 45
R05 | 875 15 14 14 14 25 8 | 39 46 44 44 53 41
R07 | 1000 10 11 13 15 8 7 | 54 49 57 59 55 53
R08 | 881 11 8 25 22 20 10 | 45 47 52 46 57 46
R09 | 1083 15 16 18 21 19 10 | 34 48 53 29 41 39
R11 | 1895 10 9 13 7 19 6 | 29 28 40 29 38 31
R12 | 1341 12 28 12 29 20 12 | 45 58 36 31 30 40
XR13 | 773 24 34 26 --- 37 20 | 84 72 92 --- 96 78
R14 | 882 11 15 11 15 32 7 | 65 76 76 65 59 70
R15 | 1488 13 12 11 19 23 8 | 66 61 56 60 44 60
R16 | 809 26 31 59 25 26 22 | 73 49 63 65 69 61
R17 | 961 8 16 15 12 20 7 | 57 47 63 54 39 55
R18E | 664 10 20 10 20 19 9 | 63 77 66 57 71 65
R19E | 1534 32 24 23 38 64 17 | 104 107 111 112 113 104
R20E | 1863 62 59 45 58 97 32 | 74 92 102 85 77 75
XR21E | ---- 5 --- --- --- --- 0 | 9999 --- --- --- --- 9999
XR22E | 3103 --- 381 26 30 33 28 | --- 222 102 100 92 101
R24E | 5667 17 18 25 17 13 11 | 57 52 54 55 48 52
------+------------------------------------+--------------------------------
RMS | 1822 23 24 24 26 35 |T 57 66 63 57 57 58
WRMS | 1822 17 19 15 22 26 |NE 53 51 55 48 50 50
MEDI | 882 15 18 15 20 21 |MD 57 50 56 55 53 52
Table 3.2256.4 GPS week: 2256 Day: 4 MJD: 60040
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 630 18 34 23 32 28 15 | 57 40 41 61 44 50
XR02 | 739 40 --- 40 16 51 24 | 61 --- 31 29 36 34
XR03 | 1029 10 13 13 --- 23 8 | 47 49 47 --- 40 47
R04 | 855 20 20 9 13 14 9 | 48 31 32 34 36 36
R05 | 1072 14 18 23 27 10 12 | 39 50 52 29 43 39
R07 | 919 7 12 17 12 16 7 | 52 58 65 55 57 57
R08 | 993 8 12 18 13 13 7 | 52 49 56 50 57 52
R09 | 1380 13 24 15 27 25 11 | 31 48 46 39 31 37
R11 | 2051 10 11 11 11 24 6 | 61 61 58 56 65 58
R12 | 1231 7 13 10 15 28 6 | 45 51 50 44 28 46
R13 | 667 26 60 24 40 32 21 | 107 93 110 91 106 98
R14 | 1054 9 20 18 19 34 9 | 109 117 108 109 107 109
R15 | 1647 5 20 18 16 21 8 | 71 58 77 79 62 71
R16 | 1189 25 31 64 23 39 23 | 142 133 142 138 138 138
R17 | 778 10 16 10 11 16 6 | 55 45 55 53 43 51
R18E | 486 8 18 10 22 20 8 | 67 69 64 52 66 61
R19E | 806 29 38 30 37 33 19 | 121 127 136 128 123 125
R20E | 1651 72 97 65 61 92 42 | 79 92 93 73 53 63
XR21E | ---- 22 --- --- 29 --- 25 | 9999 --- --- 9999 --- 9999
XR22E | 2813 --- 396 17 19 33 18 | --- 218 143 150 133 143
R24E | 4949 13 16 17 12 16 8 | 50 46 39 48 47 44
------+------------------------------------+--------------------------------
RMS | 1647 23 34 28 26 33 |T 68 75 72 69 65 67
WRMS | 1647 14 21 14 23 25 |NE 65 63 64 61 59 61
MEDI | 1029 13 20 17 19 24 |MD 57 58 56 55 53 52
Table 3.2256.5 GPS week: 2256 Day: 5 MJD: 60041
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 811 15 17 24 24 21 11 | 38 42 40 38 50 39
R02 | 799 13 17 21 14 14 9 | 34 21 25 26 34 24
R03 | 1275 15 19 16 22 14 10 | 33 32 33 37 24 30
R04 | 613 10 12 18 13 21 7 | 33 38 40 42 44 37
R05 | 812 15 18 15 22 23 10 | 37 48 42 32 36 36
R07 | 584 9 12 10 11 20 6 | 36 41 47 39 45 39
R08 | 814 10 11 17 17 14 8 | 38 46 39 43 38 40
R09 | 1658 12 22 23 14 23 10 | 36 47 36 44 39 37
R11 | 2447 8 13 14 13 17 7 | 45 38 43 41 44 41
R12 | 1157 10 24 11 39 18 13 | 43 50 46 31 30 37
R13 | 756 24 56 37 28 14 20 | 101 81 97 90 91 92
R14 | 685 9 21 16 21 21 9 | 89 83 81 94 87 86
R15 | 2037 14 11 20 14 18 9 | 76 81 76 77 65 76
R16 | 1464 22 38 71 25 35 24 | 130 133 128 127 127 128
R17 | 552 7 22 13 18 13 8 | 48 42 56 57 46 49
R18E | 509 8 16 11 16 12 7 | 62 64 68 68 57 63
R19E | 1185 12 42 42 29 26 18 | 110 119 133 123 116 117
R20E | 3232 44 99 47 39 79 33 | 64 88 82 60 69 60
XR21E | ---- 23 --- --- 36 --- 29 | 9999 --- --- 9999 --- 9999
XR22E | 2216 --- 396 17 18 28 18 | --- 191 76 87 86 82
R24E | 4806 13 18 21 24 11 11 | 39 38 53 55 41 43
------+------------------------------------+--------------------------------
RMS | 1745 16 33 28 23 26 |T 57 66 62 60 58 57
WRMS | 1745 13 22 17 19 26 |NE 54 54 55 54 53 52
MEDI | 814 12 18 17 21 18 |MD 43 47 47 44 45 41
Table 3.2256.6 GPS week: 2256 Day: 6 MJD: 60042
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01 | 793 20 21 36 23 27 14 | 72 59 56 62 66 62
R02 | 470 10 14 14 12 14 7 | 45 43 49 51 41 47
R03 | 533 9 22 14 15 16 8 | 54 46 53 48 59 52
R04 | 691 6 11 14 14 18 6 | 53 47 55 61 45 53
R05 | 746 14 10 14 13 22 7 | 49 45 49 55 57 48
R07 | 623 13 19 18 12 15 8 | 64 67 66 68 66 65
R08 | 1457 13 14 29 14 13 10 | 58 56 55 60 60 57
R09 | 1615 15 17 22 19 16 10 | 42 62 62 45 45 48
R11 | 2165 10 11 16 13 17 7 | 46 44 45 47 48 44
R12 | 1282 11 22 18 20 21 10 | 54 62 44 41 44 48
R13 | 869 20 51 43 26 35 19 | 122 84 121 102 103 107
R14 | 914 7 20 17 14 26 8 | 98 99 90 94 96 95
R15 | 2033 18 17 14 19 18 10 | 100 104 94 91 87 96
R16 | 1894 20 34 68 31 17 22 | 159 171 157 154 156 159
R17 | 1047 10 15 11 15 19 7 | 69 57 65 62 61 63
R18E | 611 8 17 12 17 16 8 | 80 84 76 81 85 79
R19E | 1130 30 36 59 30 24 21 | 121 129 154 138 123 130
R20E | 3554 26 94 90 18 69 34 | 76 67 119 77 67 70
XR21E | ---- 18 --- --- 23 --- 21 | 9999 --- --- 9999 --- 9999
XR22E | 2200 --- 380 14 9 21 11 | --- 261 94 103 97 98
R24E | 4138 14 18 16 16 27 9 | 68 60 66 66 69 64
------+------------------------------------+--------------------------------
RMS | 1708 16 31 35 19 26 |T 75 82 78 75 73 74
WRMS | 1708 13 22 15 18 25 |NE 72 69 70 69 68 69
MEDI | 1047 13 18 16 16 18 |MD 68 62 65 62 66 63
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