[IGSREPORT-24458] Wk 1895 IGLOS Final Orbits
IGS ACC
acc at igs.org
Thu May 19 16:20:30 PDT 2016
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 1895 (May 01, 2016 - May 07, 2016)
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 2.1895.
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:
igl1895[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1895 in the SP3 format.
igl18957.sum Combination Report for GPS Week 1895.
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.
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:
ftp://igs.org/igscb/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:
ftp://igs.org/igscb/station/general/igs08.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 | -0.5 ns
1 | -1.5 ns
2 | 2.0 ns
3 | -1.4 ns
4 | -1.6 ns
5 | -0.5 ns
6 | -0.3 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 1.1895, 1a.1895).
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 2.1895.0-6)
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 3.1895.0-6).
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 1895 summary. (May 01, 2016 - May 07, 2016)
Table 1.1895.a GPS week : 1895 MJD: 57509.0-57515.0
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 1 24 7 -26 -31 .23 43 41 | --- --- --- ---
| 2 1 4 18 25 37 .04 | --- ---
cof n/a| 0 0 27 3 -21 -55 .20 45 42 | --- --- --- ---
| 2 2 2 33 31 60 .06 | --- ---
emx n/a| 0 1 6 1 -55 -32 .24 26 27 | -5173 39 3588 7078
| 1 1 2 22 30 46 .05 | 5456 1315
esx n/a| -1 -1 1 -13 -2 -29 -.17 16 15 | -1792 -3227 3606 8220
| 0 0 1 10 28 18 .03 | 2250 5037
gfz n/a| -1 0 -10 5 65 60 .07 25 21 | 0 -431 3559 6753
| 1 1 2 21 37 36 .05 | 0 2662
grg n/a| 0 0 -12 1 15 76 -.39 37 35 | -434486 -477 4347 616587
| 0 1 4 25 38 39 .07 | 682 2577
iac n/a| 2 0 -2 -1 0 1 .09 18 18 | 806 -376 3604 6766
| 1 1 1 17 52 37 .03 | 1471 2215
mcc n/a| 3 -3 13 88 -55 774 -.27 98 98 | --- --- --- ---
| 3 5 16 98 113 577 .38 | --- ---
Table 1.1895.b GPS week : 1895 MJD: 57509.0-57515.0
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 | 13 12 12 13 14 12 12 |
R02 | 8 7 8 7 8 8 9 |
R03 | 8 9 9 8 9 10 9 |
R04 | 8 8 8 9 9 10 8 |
R05 | 13 13 14 12 14 12 13 |
R06 | 8 10 10 9 9 9 8 |
R07 | 8 10 11 9 9 10 9 |
R08 | 9 8 10 10 9 9 10 |
R09 | 7 8 9 11 10 8 8 |
R10 | 8 9 10 10 9 10 10 |
R13 | 10 12 11 11 12 10 10 |
R14 | 17 17 13 15 17 18 13 |
R15 | 25 14 10 11 12 10 10 |
R16 | 14 16 16 12 11 11 15 |
R17 | 9 9 11 10 10 8 9 |
R18 | 9 8 8 9 9 10 8 |
R19 | 10 10 9 10 10 10 9 |
R20 | 12 12 13 14 13 14 12 |
R21 | 10 9 10 9 10 11 10 |
R22 | 12 11 10 11 12 11 10 |
R23 | 11 9 13 12 8 9 9 |
R24 | 13 14 19 16 16 12 13 |
R26 | 31 35 33 34 28 31 36 |
Table 1.1895.c GPS week : 1895 MJD: 57509.0-57515.0
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 1895 0 | 60 12 226 -104 -1141 -880 83.1 1221 1221 | -457 0
brd 1895 1 | 5 34 197 -1862 -1311 598 84.2 1407 1407 | -1529 0
brd 1895 2 | 67 73 154 -1382 632 1634 83.9 1947 1947 | 1971 0
brd 1895 3 | -15 -50 152 157 -105 -532 84.3 1819 1819 | -1393 0
brd 1895 4 | 7 -20 242 -822 120 -67 83.5 1458 1458 | -1627 0
brd 1895 5 | 11 88 324 -532 1159 -630 84.5 1373 1373 | -514 0
brd 1895 6 | -29 -48 335 -429 616 -1967 83.3 1683 1683 | -266 0
-------------+------------------------------------------------------------+----------------
brd 1895 mean| 15 12 233 -710 -4 -263 83.8 1558 1558 | -545 0
brd 1895 sdev| 36 55 74 709 928 1145 .6 263 263 | 1243 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 2.1895.0 GPS week: 1895 Day: 0 MJD: 57509
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 23 22 11 -49 .19 42 39 | --- --- --- ---
cof n/a| 1 1 24 -2 -3 -73 .22 44 41 | --- --- --- ---
emx n/a| -2 0 4 16 -52 39 .18 26 26 | -5878 222 3493 7309
esx n/a| 0 0 0 -26 47 -40 -.14 18 17 | 2506 -12420 3502 8956
gfz n/a| -1 1 -8 -27 118 44 .09 33 21 | 0 -1864 3431 7019
grg n/a| 1 0 -11 36 17 87 -.44 36 34 | -434127 -1916 8728 615445
iac n/a| 3 -1 -1 -7 -65 -7 .07 18 18 | 956 -826 3474 7113
mcc n/a| -2 0 0 -11 -52 1259 -.11 112 112 | --- --- --- ---
Table 2.1895.1 GPS week: 1895 Day: 1 MJD: 57510
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 24 15 -37 -17 .19 43 40 | --- --- --- ---
cof n/a| -2 -1 27 25 -44 -101 .20 44 42 | --- --- --- ---
emx n/a| 0 1 5 15 -33 -42 .29 27 26 | -2943 -1819 3380 7364
esx n/a| -1 -2 2 -6 -13 -27 -.11 15 15 | -2951 -5723 3396 8562
gfz n/a| -3 0 -9 3 25 104 .03 22 21 | 0 -4102 3289 6712
grg n/a| 0 2 -15 16 -33 61 -.44 36 34 | -434251 -3798 3397 616424
iac n/a| 4 2 0 -32 19 -12 .07 20 20 | -1321 -777 3402 6739
mcc n/a| 3 -11 -7 -46 -31 1180 .13 65 65 | --- --- --- ---
Table 2.1895.2 GPS week: 1895 Day: 2 MJD: 57511
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 20 31 -52 -89 .23 43 40 | --- --- --- ---
cof n/a| 1 2 26 30 -61 -125 .10 48 42 | --- --- --- ---
emx n/a| -1 2 8 18 -43 -75 .26 26 28 | -4110 2509 3517 6303
esx n/a| 0 -1 0 -8 -31 -43 -.20 19 18 | -1277 1890 3563 6893
gfz n/a| -2 -1 -10 -15 31 25 .09 21 21 | 0 4405 3543 6055
grg n/a| 0 0 -10 21 23 108 -.34 35 35 | -435019 4419 3559 617882
iac n/a| 0 0 -3 -1 42 55 .10 17 17 | 1802 3237 3569 6067
mcc n/a| 4 -3 16 39 -29 1631 .08 61 61 | --- --- --- ---
Table 2.1895.3 GPS week: 1895 Day: 3 MJD: 57512
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| 4 4 24 11 -38 16 .32 44 41 | --- --- --- ---
cof n/a| 0 3 25 40 36 -7 .26 47 42 | --- --- --- ---
emx n/a| 1 0 12 -37 -14 -10 .24 25 25 | -12057 -793 3481 6732
esx n/a| -1 -2 1 -5 21 -21 -.18 16 14 | -2648 -4630 3490 8438
gfz n/a| -3 -2 -10 4 106 55 -.02 25 24 | 0 -1831 3426 6414
grg n/a| 1 -2 -20 2 -18 52 -.34 39 35 | -433536 -1927 3464 616503
iac n/a| 3 0 -4 15 -70 -10 .10 18 18 | 3306 -4146 3462 6391
mcc n/a| 5 -2 0 129 -116 558 -.21 122 122 | --- --- --- ---
Table 2.1895.4 GPS week: 1895 Day: 4 MJD: 57513
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 22 0 -55 12 .24 42 40 | --- --- --- ---
cof n/a| -4 -4 25 -51 -37 44 .25 42 42 | --- --- --- ---
emx n/a| 0 4 5 -10 -74 -103 .21 26 27 | -7620 41 4206 7475
esx n/a| -2 0 2 -26 -18 -35 -.20 17 16 | -3247 915 4231 8300
gfz n/a| -1 0 -12 29 63 117 .11 26 19 | 0 -577 4230 7325
grg n/a| 1 0 -16 -3 -7 127 -.47 39 39 | -435494 -314 4241 616792
iac n/a| 2 0 -1 3 42 4 .11 16 16 | -186 -633 4300 7340
mcc n/a| 8 -9 23 171 -58 312 -.56 102 102 | --- --- --- ---
Table 2.1895.5 GPS week: 1895 Day: 5 MJD: 57514
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 3 28 -23 -8 -46 .24 44 44 | --- --- --- ---
cof n/a| 0 0 28 -27 -18 -29 .16 45 43 | --- --- --- ---
emx n/a| 0 1 4 -15 -108 -24 .31 27 28 | -8729 -168 3625 7753
esx n/a| 0 0 3 -16 -23 8 -.17 16 15 | -653 795 3634 8877
gfz n/a| -1 -1 -9 17 33 44 .04 21 19 | 0 508 3548 7351
grg n/a| 0 -2 -5 -28 56 91 -.40 38 34 | -434942 144 3620 616238
iac n/a| 2 0 -6 22 51 -57 .13 18 18 | 344 -438 3598 7358
mcc n/a| 2 1 34 118 141 102 -.29 98 98 | --- --- --- ---
Table 2.1895.6 GPS week: 1895 Day: 6 MJD: 57515
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 32 -8 -4 -44 .22 43 42 | --- --- --- ---
cof n/a| -1 -2 32 7 -18 -95 .23 46 45 | --- --- --- ---
emx n/a| 0 2 5 23 -64 -12 .21 25 26 | 5124 284 3418 6615
esx n/a| 0 0 0 -2 -1 -43 -.20 14 13 | -4274 -3422 3432 7517
gfz n/a| 0 -1 -13 27 82 28 .13 25 24 | 0 439 3448 6399
grg n/a| 0 -1 -10 -32 69 8 -.29 39 35 | -434036 47 3422 616825
iac n/a| 1 -1 -2 -10 -19 41 .05 17 17 | 743 950 3428 6357
mcc n/a| 0 0 27 222 -237 380 -.95 130 130 | --- --- --- ---
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 3.1895.0 GPS week: 1895 Day: 0 MJD: 57509
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 874 59 59 28 22 20 34 25 --- 12 | 71 70 34 45 35 23 18 --- 26
R02 | 663 27 30 15 16 19 30 11 --- 8 | 63 67 48 54 35 33 39 --- 42
R03 | 871 43 45 17 13 13 32 9 74 8 | 80 81 38 41 32 23 36 50 35
R04 | 824 32 32 20 17 18 23 12 --- 8 | 91 95 69 75 69 60 69 --- 69
R05 | 853 43 46 24 15 32 34 30 --- 12 | 86 91 66 71 62 44 75 --- 64
R06 | 1446 31 28 13 11 19 26 12 --- 7 | 80 80 53 57 42 38 48 --- 50
R07 | 1313 36 38 16 16 9 28 14 141 8 | 83 85 49 53 38 32 38 73 44
R08 | 726 30 29 19 19 15 25 15 --- 8 | 75 75 52 49 35 23 40 --- 41
R09 | 1675 23 19 13 11 13 30 12 --- 7 | 23 27 22 25 31 33 27 --- 23
R10 | 994 21 27 16 18 9 31 11 --- 7 | 26 26 27 25 22 30 21 --- 20
R13 | 905 43 46 12 13 30 33 10 --- 9 | 41 41 26 25 22 20 12 --- 17
R14 | 936 69 83 54 22 20 48 28 --- 16 | 47 66 29 34 26 29 16 --- 21
R15 | 1922 30 30 34 28 118 68 26 --- 24 | 29 30 23 24 124 27 12 --- 24
R16 | 853 52 32 38 21 31 40 25 --- 14 | 39 37 47 25 31 23 19 --- 21
R17 | 970 41 43 15 14 18 37 13 --- 9 | 51 51 29 25 33 35 20 --- 21
R18 | 1523 33 35 24 13 23 34 11 --- 9 | 45 45 35 26 32 28 24 --- 23
R19 | 969 44 47 25 11 32 20 8 --- 9 | 58 60 39 27 38 24 24 --- 25
R20 | 1257 53 51 27 16 20 40 27 --- 12 | 78 76 57 43 45 42 36 --- 42
R21 | 465 48 55 23 15 17 27 22 110 10 | 61 66 39 30 28 31 29 39 27
R22 | 1042 57 61 30 16 28 40 12 --- 12 | 67 72 38 36 33 35 27 --- 27
R23 | 2574 38 41 30 24 15 40 11 --- 11 | 28 28 32 51 37 25 35 --- 34
R24 | 1191 26 38 32 24 24 48 20 --- 12 | 71 77 50 60 55 29 49 --- 47
XR26 | ---- 64 47 --- --- --- --- 14 --- 30 | 61 182 --- --- --- --- 40 --- 30
------+---------------------------------------------------+-----------------------------------------------
RMS | 1220 42 44 26 18 33 36 18 112 |T 58 66 41 40 41 31 32 54 33
WRMS | 1220 39 41 26 17 21 34 18 112 |NE 58 66 41 40 41 31 32 54 33
MEDI | 969 41 41 23 16 19 33 13 110 |MD 61 67 38 36 35 29 29 50 27
Table 3.1895.1 GPS week: 1895 Day: 1 MJD: 57510
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1478 53 54 33 17 19 37 17 --- 11 | 54 52 37 41 26 18 24 --- 28
R02 | 1279 27 24 14 15 16 23 8 --- 7 | 41 35 34 39 31 26 31 --- 32
R03 | 799 38 42 26 14 13 29 12 67 8 | 51 55 28 37 26 20 28 38 27
R04 | 755 35 40 11 15 15 27 15 --- 8 | 70 73 57 60 58 54 59 --- 56
R05 | 1104 41 40 21 16 29 39 33 --- 12 | 49 60 36 45 49 37 54 --- 40
R06 | 1081 45 56 27 11 20 24 16 --- 9 | 55 66 28 30 32 21 30 --- 26
R07 | 2041 56 61 14 10 26 31 15 68 10 | 60 66 32 34 23 23 27 42 27
R08 | 1730 38 47 17 14 16 18 17 --- 8 | 50 57 33 30 22 16 27 --- 25
R09 | 1826 25 34 18 10 16 31 20 --- 8 | 18 22 18 19 22 18 24 --- 15
R10 | 1775 27 26 19 15 18 40 14 --- 9 | 25 23 32 19 25 23 18 --- 18
R13 | 1346 44 46 37 16 25 34 21 --- 12 | 30 29 42 28 20 21 18 --- 18
R14 | 1739 65 59 49 21 21 56 38 --- 17 | 36 41 42 33 30 27 31 --- 19
R15 | 2556 38 39 27 16 47 42 22 --- 13 | 33 34 27 32 55 20 14 --- 22
R16 | 581 58 49 39 20 20 72 21 --- 15 | 43 35 29 26 22 39 23 --- 19
R17 | 968 36 36 25 16 21 14 17 --- 9 | 42 42 32 37 35 25 22 --- 27
R18 | 1447 33 32 16 12 17 37 10 --- 8 | 40 39 31 28 20 24 22 --- 22
R19 | 813 45 40 20 14 25 29 14 --- 9 | 50 47 34 35 23 24 22 --- 26
R20 | 1113 39 45 32 17 25 37 23 --- 11 | 55 60 52 35 29 42 35 --- 34
R21 | 625 49 51 19 10 15 14 20 58 8 | 48 46 37 28 30 28 29 37 27
R22 | 1049 51 57 33 15 26 22 21 --- 11 | 48 52 35 35 33 29 24 --- 27
R23 | 1683 26 34 25 22 12 27 13 --- 9 | 24 25 26 30 27 19 22 --- 21
R24 | 1234 37 35 43 18 23 48 28 --- 13 | 39 44 61 28 32 29 34 --- 28
XR26 | ---- 66 154 --- --- --- --- 18 --- 34 | 58 273 --- --- --- --- 21 --- 19
------+---------------------------------------------------+-----------------------------------------------
RMS | 1407 42 44 27 15 22 36 20 65 |T 44 55 35 33 30 26 27 39 26
WRMS | 1407 40 42 26 15 21 34 20 65 |NE 44 55 35 33 30 26 27 39 26
MEDI | 1234 39 42 25 15 20 31 17 67 |MD 48 46 33 32 27 24 24 38 26
Table 3.1895.2 GPS week: 1895 Day: 2 MJD: 57511
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1768 69 66 29 18 24 20 11 --- 11 | 58 64 30 35 25 23 21 --- 21
R02 | 2351 24 22 12 17 13 29 11 --- 7 | 50 52 40 48 33 39 31 --- 37
R03 | 853 37 31 16 18 16 25 16 55 8 | 58 56 35 46 30 35 34 55 35
R04 | 825 36 34 19 15 17 27 10 --- 8 | 74 74 63 62 58 61 63 --- 60
R05 | 876 31 33 42 21 21 45 30 --- 14 | 57 60 38 61 52 33 65 --- 50
R06 | 1648 53 57 25 17 15 22 13 --- 9 | 78 81 45 50 34 41 36 --- 41
R07 | 2548 64 73 27 13 22 21 10 87 10 | 78 83 41 39 39 35 31 94 35
R08 | 2002 52 52 14 17 25 25 16 --- 10 | 64 65 39 40 27 16 32 --- 31
R09 | 2029 35 31 20 14 19 33 10 --- 8 | 28 22 23 23 25 18 24 --- 19
R10 | 2099 17 23 20 20 23 39 16 --- 10 | 22 25 24 21 25 34 20 --- 16
R13 | 2106 37 45 21 23 23 39 15 --- 10 | 29 33 28 29 18 20 19 --- 15
R14 | 667 60 67 23 24 26 36 25 --- 13 | 41 53 27 47 34 30 20 --- 26
R15 | 5441 35 45 19 15 21 47 12 --- 10 | 35 44 26 26 38 23 19 --- 19
R16 | 609 48 75 48 16 29 69 24 --- 16 | 38 65 56 29 43 39 24 --- 27
R17 | 1665 46 45 23 15 25 32 16 --- 10 | 38 38 26 32 38 35 21 --- 22
R18 | 1145 28 27 14 13 24 26 14 --- 8 | 38 39 29 32 34 18 26 --- 25
R19 | 1848 39 42 28 16 21 25 8 --- 9 | 53 58 44 39 27 20 27 --- 30
R20 | 840 27 41 33 20 24 58 23 --- 13 | 33 53 52 39 35 21 31 --- 30
R21 | 527 51 54 20 19 20 23 13 24 9 | 45 49 26 23 30 29 26 69 22
R22 | 1592 44 46 22 11 17 13 24 --- 9 | 52 55 30 27 35 32 26 --- 26
R23 | 1078 38 31 34 36 17 22 17 --- 12 | 24 32 25 57 38 39 25 --- 32
XR24 | 943 52 58 39 30 --- 54 30 --- 18 | 69 76 27 39 --- 18 33 --- 26
XR26 | ---- 71 268 --- --- --- --- 15 --- 33 | 34 237 --- --- --- --- 45 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1947 43 48 26 19 21 35 17 61 |T 47 61 35 38 34 29 30 72 29
WRMS | 1947 40 42 28 18 21 35 17 61 |NE 47 61 35 38 34 29 30 72 29
MEDI | 1592 39 45 22 17 21 27 15 55 |MD 45 55 30 39 34 30 26 69 27
Table 3.1895.3 GPS week: 1895 Day: 3 MJD: 57512
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1812 73 88 21 13 31 29 22 --- 12 | 66 79 41 40 48 28 25 --- 29
R02 | 1757 29 30 18 10 15 21 12 --- 7 | 56 60 45 44 32 31 31 --- 37
R03 | 723 33 39 15 16 14 23 13 132 7 | 64 71 43 54 34 37 35 70 41
R04 | 1252 27 27 17 14 19 41 13 --- 8 | 78 80 68 72 65 60 64 --- 65
R05 | 1089 28 27 28 21 13 45 30 --- 12 | 55 58 45 64 51 27 63 --- 52
R06 | 1471 46 51 12 13 27 24 15 --- 9 | 70 74 31 37 22 22 33 --- 30
R07 | 1737 54 47 13 13 25 25 12 113 9 | 81 78 45 47 26 26 27 99 36
R08 | 2136 51 57 22 11 21 31 10 --- 9 | 75 81 51 43 33 21 36 --- 38
R09 | 2652 33 43 29 13 21 53 12 --- 10 | 29 40 22 26 35 26 23 --- 20
R10 | 1075 26 26 21 13 18 50 13 --- 9 | 17 20 20 21 21 32 17 --- 15
R13 | 2411 33 35 25 14 29 43 13 --- 10 | 26 29 31 23 26 14 14 --- 16
R14 | 722 66 63 36 25 34 43 24 --- 15 | 36 44 47 48 43 25 23 --- 29
R15 | 5051 39 42 19 12 37 40 12 --- 10 | 32 34 25 16 45 18 15 --- 12
R16 | 863 45 27 34 16 24 44 23 --- 12 | 42 39 35 21 26 20 30 --- 18
R17 | 975 45 40 24 12 27 31 13 --- 10 | 42 39 31 23 38 35 22 --- 19
R18 | 709 37 34 20 15 26 22 7 --- 8 | 45 45 24 31 32 23 25 --- 22
R19 | 2403 46 40 25 13 27 28 14 --- 10 | 55 55 43 33 39 33 22 --- 28
R20 | 595 26 29 32 18 24 67 27 --- 13 | 37 39 41 39 36 25 39 --- 32
R21 | 587 46 41 23 9 17 36 12 119 9 | 51 49 35 28 28 35 26 69 25
R22 | 1504 53 55 35 11 28 21 14 --- 11 | 52 59 42 26 33 30 25 --- 24
R23 | 1217 40 40 33 24 16 25 28 --- 12 | 25 28 28 49 45 35 38 --- 36
R24 | 946 55 92 36 28 35 61 26 --- 16 | 87 123 34 62 48 37 47 --- 45
XR26 | ---- 72 420 --- --- --- --- 15 --- 33 | 58 396 --- --- --- --- 52 --- 51
------+---------------------------------------------------+-----------------------------------------------
RMS | 1818 44 47 25 16 25 39 18 122 |T 51 70 37 38 36 29 31 79 31
WRMS | 1818 41 42 25 14 24 35 18 122 |NE 51 70 37 38 36 29 31 79 31
MEDI | 1217 45 40 23 13 24 31 13 119 |MD 52 55 35 37 34 27 27 70 29
Table 3.1895.4 GPS week: 1895 Day: 4 MJD: 57513
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 1463 66 39 36 13 44 48 11 --- 14 | 61 42 31 28 45 33 20 --- 19
R02 | 890 31 36 13 12 25 21 14 --- 7 | 52 56 31 38 22 23 32 --- 30
R03 | 671 38 41 21 13 18 22 18 135 8 | 55 56 35 30 13 21 19 53 23
R04 | 894 26 33 29 14 15 24 12 --- 8 | 65 73 63 61 56 58 58 --- 58
R05 | 810 27 27 33 29 19 56 26 --- 13 | 54 72 53 80 71 30 57 --- 59
R06 | 1243 35 30 14 13 25 28 15 --- 8 | 53 46 40 44 24 37 32 --- 34
R07 | 1053 54 57 14 9 22 31 12 76 9 | 67 68 33 29 30 26 25 49 26
R08 | 1688 45 39 21 14 24 25 11 --- 9 | 65 62 45 47 30 31 31 --- 36
R09 | 2131 33 33 25 23 13 43 13 --- 10 | 26 32 22 37 29 22 30 --- 23
R10 | 1262 21 24 13 20 14 45 12 --- 8 | 24 32 27 36 28 17 22 --- 23
R13 | 1072 41 42 29 15 35 40 16 --- 11 | 24 26 33 23 27 13 16 --- 15
R14 | 656 59 60 48 28 30 53 26 --- 16 | 32 39 50 48 44 14 16 --- 28
R15 | 3615 35 29 19 17 49 46 12 --- 12 | 27 32 27 18 52 18 12 --- 15
R16 | 1767 44 47 28 12 25 42 14 --- 10 | 46 47 27 27 25 31 19 --- 20
R17 | 580 49 56 18 16 29 26 14 --- 10 | 47 56 27 32 41 20 22 --- 24
R18 | 848 43 47 17 16 25 24 13 --- 9 | 45 49 26 26 30 24 23 --- 19
R19 | 2242 51 46 19 13 25 33 11 --- 9 | 45 41 28 25 34 37 23 --- 22
R20 | 669 26 48 38 14 23 67 21 --- 13 | 33 46 39 28 33 31 35 --- 25
R21 | 541 39 41 24 20 15 40 16 85 10 | 50 52 38 42 30 27 29 43 30
R22 | 1445 53 53 39 15 28 36 16 --- 12 | 53 53 39 24 32 38 25 --- 21
R23 | 1199 23 34 21 20 16 21 9 --- 8 | 30 29 36 40 29 21 35 --- 30
XR24 | 1080 61 61 17 23 --- 49 30 --- 15 | 88 85 57 51 --- 28 52 --- 48
XR26 | ---- 61 698 --- --- --- --- 12 --- 28 | 44 587 --- --- --- --- 30 --- 26
------+---------------------------------------------------+-----------------------------------------------
RMS | 1457 42 42 26 17 26 39 16 102 |T 47 73 36 37 34 27 28 48 28
WRMS | 1457 40 42 27 16 18 39 16 102 |NE 47 73 36 37 34 27 28 48 28
MEDI | 1072 41 41 21 15 25 36 14 85 |MD 47 49 33 32 30 26 25 49 25
Table 3.1895.5 GPS week: 1895 Day: 5 MJD: 57514
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 953 64 58 40 11 27 26 13 --- 12 | 56 52 40 27 27 17 20 --- 19
R02 | 467 34 32 22 10 19 22 14 --- 8 | 52 53 30 35 25 26 29 --- 28
R03 | 843 50 44 21 16 17 40 14 100 10 | 59 52 25 30 21 27 19 44 21
R04 | 1054 30 28 33 13 15 21 24 --- 10 | 121 121 103 117 122 118 119 --- 115
R05 | 643 28 29 22 21 19 49 31 --- 12 | 46 55 51 55 48 40 45 --- 43
R06 | 1182 36 35 22 15 23 23 14 --- 9 | 48 47 37 33 18 30 28 --- 27
R07 | 700 52 58 10 19 21 28 17 112 9 | 66 73 35 45 26 30 32 42 33
R08 | 1306 45 41 20 11 18 29 12 --- 8 | 59 56 45 38 30 11 37 --- 33
R09 | 2152 25 30 23 10 10 32 11 --- 7 | 20 28 31 25 27 20 27 --- 24
R10 | 2240 31 32 23 16 21 38 14 --- 9 | 28 28 28 25 15 15 17 --- 17
R13 | 597 43 46 18 16 26 39 14 --- 10 | 22 26 25 20 24 20 14 --- 13
R14 | 755 73 77 44 24 18 78 32 --- 17 | 27 42 43 38 20 37 18 --- 22
R15 | 2441 33 27 23 13 28 38 15 --- 10 | 22 26 23 19 31 18 16 --- 13
R16 | 1848 33 59 34 23 17 41 16 --- 11 | 27 50 34 37 26 21 23 --- 24
R17 | 705 48 51 13 10 13 29 11 --- 8 | 44 47 19 21 23 26 21 --- 18
R18 | 470 35 44 35 17 14 18 14 --- 9 | 36 46 28 28 21 20 21 --- 19
R19 | 2026 46 49 19 12 27 29 12 --- 9 | 37 40 24 19 33 31 20 --- 17
R20 | 595 41 33 32 17 29 63 24 --- 13 | 36 33 39 28 38 51 31 --- 25
R21 | 474 48 47 29 18 20 34 17 77 11 | 44 42 29 30 36 33 25 25 24
R22 | 1050 57 55 32 9 23 25 14 --- 10 | 46 46 32 26 32 32 24 --- 22
R23 | 2441 26 19 21 20 13 29 12 --- 8 | 27 41 35 37 29 18 26 --- 28
R24 | 1436 54 50 34 17 24 40 21 --- 12 | 71 64 41 36 31 36 43 --- 32
XR26 | ---- 64 170 --- --- --- --- 15 --- 30 | 70 258 --- --- --- --- 35 --- 33
------+---------------------------------------------------+-----------------------------------------------
RMS | 1372 44 45 27 16 21 38 18 97 |T 46 57 36 34 31 30 30 37 28
WRMS | 1372 44 43 28 15 19 34 18 97 |NE 46 57 36 34 31 30 30 37 28
MEDI | 953 43 44 23 16 19 29 14 100 |MD 44 47 32 30 27 26 25 42 24
Table 3.1895.6 GPS week: 1895 Day: 6 MJD: 57515
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod cof emx esx gfz grg iac mcc IGL | cod cof emx esx gfz grg iac mcc IGL
------+---------------------------------------------------+-----------------------------------------------
R01 | 949 60 72 26 9 37 30 20 --- 11 | 76 88 45 26 35 34 24 --- 24
R02 | 579 30 29 25 11 21 31 13 --- 8 | 66 63 44 46 26 27 35 --- 37
R03 | 522 45 58 19 9 25 28 17 59 9 | 75 86 39 38 25 25 33 57 33
R04 | 1308 38 42 22 9 20 27 14 --- 8 | 125 128 110 110 114 109 111 --- 110
R05 | 520 28 36 23 15 21 64 37 --- 13 | 58 58 51 55 42 29 52 --- 46
R06 | 1275 41 43 20 12 23 17 14 --- 8 | 69 70 31 41 32 33 31 --- 35
R07 | 586 41 42 12 16 18 28 17 173 8 | 77 79 42 51 34 33 35 61 41
R08 | 907 41 49 27 14 30 33 16 --- 10 | 79 85 51 53 41 25 47 --- 45
R09 | 5481 20 21 15 11 14 44 16 --- 8 | 20 26 17 21 21 22 31 --- 20
R10 | 861 40 42 19 11 29 38 15 --- 9 | 30 41 26 21 17 24 19 --- 15
R13 | 1052 42 44 19 17 23 44 13 --- 10 | 32 33 24 27 18 16 13 --- 15
R14 | 1119 61 64 24 17 32 54 20 --- 13 | 37 38 30 38 30 31 20 --- 24
R15 | 2853 35 36 22 11 35 35 11 --- 9 | 27 32 27 23 40 26 12 --- 18
R16 | 1449 36 49 46 24 21 70 12 --- 14 | 38 44 29 36 26 26 22 --- 25
R17 | 1086 53 49 23 8 27 26 11 --- 9 | 57 56 29 29 40 39 24 --- 25
R18 | 502 30 22 21 11 20 11 16 --- 7 | 54 48 30 31 24 26 27 --- 25
R19 | 1432 38 43 21 14 23 33 13 --- 9 | 56 61 41 37 43 26 28 --- 32
R20 | 649 38 41 25 15 36 42 25 --- 12 | 47 50 42 37 45 33 37 --- 32
R21 | 977 51 51 28 10 23 37 11 131 10 | 61 60 38 33 38 46 29 44 29
R22 | 659 51 58 36 9 21 32 11 --- 10 | 68 74 38 27 31 28 25 --- 25
R23 | 2600 33 32 28 20 11 31 11 --- 9 | 38 42 40 60 43 30 45 --- 45
R24 | 769 57 61 26 18 22 58 22 --- 12 | 93 101 52 55 39 41 53 --- 49
XR26 | ---- 79 1532 --- --- --- --- 14 --- 36 | 83 888 --- --- --- --- 25 --- 28
------+---------------------------------------------------+-----------------------------------------------
RMS | 1683 43 46 25 14 25 39 17 130 |T 59 97 39 40 36 33 33 54 33
WRMS | 1683 42 45 26 13 24 35 17 130 |NE 59 97 39 40 36 33 33 54 33
MEDI | 949 41 43 23 11 23 33 14 131 |MD 58 60 38 37 34 28 29 57 29
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