[IGSREPORT-17223] Wk 1521 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Mar 19 05:26:07 PDT 2009
******************************************************************************
IGS Electronic Report 19 Mar 05:26:29 PDT 2009 Message Number 17223
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1521 (Mar 01, 2009 - Mar 07, 2009)
Contact: J. Ray (jim.ray at noaa.gov),
J. Griffiths (jake.griffiths at noaa.gov)
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the centers
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 2.1521.
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:
igl1521[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1521 in the SP3 format.
igl15217.sum Combination Report for GPS Week 1521.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
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.
3. Starting on 01-May-2005 (GPS Week 1321; MJD 53491)[IGSMAIL-5151]
BKG, ESA, and CODE will start to refer their GLONASS orbit products
to the following satellite antenna offset (SAO) values:
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.
4. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets derived from the
bkg summary files were added to the broadcast clocks.
Day | applied clock offset
----+---------------------
0 | 192.0 ns
1 | 236.8 ns
2 | 174.1 ns
3 | 183.4 ns
4 | 177.5 ns
5 | 238.1 ns
6 | 236.7 ns
5. 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
----+--------+---------------
6 | ESX | R23
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 1.1521, 1a.1521).
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 2.1521.0-6)
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 3.1521.0-6).
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 1521 summary. (Mar 01, 2009 - Mar 07, 2009)
Table 1.1521.a GPS week : 1521 MJD: 54891.0-54897.0
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]
--------+----------------------------------------------------+------------------------------
bkg 95| 1 0 0 -12 -9 -196 -.23 34 32 | 0 40 2543 2615
| 1 2 2 27 30 185 .06 | 0 152
cod 239| -2 0 -3 12 -8 113 -.20 20 17 | --- --- --- ---
| 1 0 2 20 14 41 .04 | --- ---
esx 118| 0 0 0 29 42 49 .34 30 25 | 76069 1922 7109 19057
| 2 2 3 30 36 71 .05 | 34331 4200
iac n/a| 1 0 7 -63 -10 -57 .11 38 38 | 874908 103610 234574 344230
| 2 1 3 16 33 97 .07 | 1057649 161780
mcc n/a| 8 -1 5 -61 -27 468 -.07 151 151 | --- --- --- ---
| 10 4 8 144 140 170 .32 | --- ---
Table 1.1521.b GPS week : 1521 MJD: 54891.0-54897.0
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
------+------------------------------------+------------------------------------------
R02 | 9 11 13 10 8 14 14 |
R03 | 10 16 13 13 10 10 9 |
R04 | 12 12 12 12 37 11 17 |
R06 | 17 17 23 13 16 22 21 |
R07 | 14 9 8 15 9 13 12 |
R08 | 16 18 10 13 13 13 13 |
R10 | 8 10 13 11 11 13 11 |
R11 | 8 11 11 14 16 11 11 |
R13 | 14 9 14 14 12 16 15 |
R14 | 18 11 10 8 8 14 10 |
R15 | 10 13 14 12 10 17 13 |
R17 | 22 20 24 20 22 23 23 |
R18 | 18 21 21 19 17 20 22 |
R19 | 15 23 29 27 26 36 36 |
R20 | 28 24 25 27 25 22 25 |
R21 | 21 20 17 23 23 17 23 |
R22 | 17 19 23 19 19 21 30 |
R23 | 21 20 27 24 20 29 506 |
R24 | 29 22 24 22 19 26 17 |
Table 1.1521.c GPS week : 1521 MJD: 54891.0-54897.0
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 1521 0 | 38 -121 244 -1707 673 -9802 94.5 >>>>> >>>>> | 191991 0
brd 1521 1 | 1874 -388 -699 -401 -3049 -8576 <<<< >>>>> >>>>> | 236769 0
brd 1521 2 | 28 78 268 675 -767 -5874 103.3 >>>>> >>>>> | 174110 0
brd 1521 3 | -125 46 153 -997 -3520 -16830 91.5 >>>>> >>>>> | 183377 0
brd 1521 4 | 187 -63 322 2221 345 -17860 99.5 >>>>> >>>>> | 177501 0
brd 1521 5 | -180 452 201 -4544 404 -18410 88.1 >>>>> >>>>> | 238118 0
brd 1521 6 | 50 -43 260 -642 1033 -17280 88.0 >>>>> >>>>> | 236675 0
-------------+------------------------------------------------------------+----------------
brd 1521 mean| 267 -5 107 -770 -697 -13518 -56.7 >>>>> >>>>> | 205505 0
brd 1521 sdev| 718 253 359 2096 1856 5237 399.0 >>>>> >>>>> | 30151 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 2.1521.0 GPS week: 1521 Day: 0 MJD: 54891
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]
--------+----------------------------------------------------+------------------------------
bkg 95| 0 -2 -2 -18 -21 -65 -.29 36 35 | 0 -151 2202 2280
cod 239| -2 0 -1 5 0 101 -.19 18 15 | --- --- --- ---
esx 118| 0 2 3 36 62 33 .42 27 23 | 63911 360 6276 13985
iac n/a| -1 0 4 -52 -72 -142 .08 33 33 | 2126515 309337 569730 999999
mcc n/a| 24 -6 3 109 114 652 -.37 176 176 | --- --- --- ---
Table 2.1521.1 GPS week: 1521 Day: 1 MJD: 54892
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]
--------+----------------------------------------------------+------------------------------
bkg 95| 2 2 -2 -53 26 -38 -.30 34 33 | 0 326 2595 2683
cod 239| -2 -1 -6 4 -7 78 -.20 19 18 | --- --- --- ---
esx 118| 0 1 3 61 -6 26 .31 25 22 | 106763 1051 5486 12151
iac n/a| 0 -1 7 -44 23 -150 .06 36 36 | 2347465 315568 809278 999999
mcc n/a| 4 0 -11 63 12 409 .05 192 192 | --- --- --- ---
Table 2.1521.2 GPS week: 1521 Day: 2 MJD: 54893
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]
--------+----------------------------------------------------+------------------------------
bkg 95| 2 1 3 -39 33 -121 -.17 32 32 | 0 -77 2580 2638
cod 239| -2 0 -6 44 -31 72 -.21 20 16 | --- --- --- ---
esx 118| -3 2 0 0 38 63 .28 32 27 | 44593 -1564 6570 24117
iac n/a| 3 0 5 -73 6 -39 .04 41 41 | 176505 -629 6323 15779
mcc n/a| 15 6 16 -238 158 277 -.25 218 218 | --- --- --- ---
Table 2.1521.3 GPS week: 1521 Day: 3 MJD: 54894
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]
--------+----------------------------------------------------+------------------------------
bkg 95| 2 -2 -1 14 -48 -209 -.19 31 31 | 0 12 2771 2844
cod 239| -3 1 -6 -2 -4 113 -.28 19 17 | --- --- --- ---
esx 118| 3 -3 3 42 101 44 .34 29 26 | 50269 -4240 7515 25701
iac n/a| 3 1 8 -70 -22 51 .09 39 39 | 184119 -844 7347 18420
mcc n/a| -4 -7 5 -271 -194 217 -.40 151 151 | --- --- --- ---
Table 2.1521.4 GPS week: 1521 Day: 4 MJD: 54895
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]
--------+----------------------------------------------------+------------------------------
bkg 95| 3 0 0 -16 -2 -38 -.18 24 24 | 0 117 2325 2408
cod 239| -2 0 -2 39 -27 96 -.15 22 20 | --- --- --- ---
esx 118| -1 -3 -4 16 50 -79 .34 43 29 | 38511 4827 7936 23293
iac n/a| 2 0 13 -50 6 61 .22 38 38 | 174740 -525 7523 11844
mcc n/a| 10 1 12 -5 -210 523 .53 84 84 | --- --- --- ---
Table 2.1521.5 GPS week: 1521 Day: 5 MJD: 54896
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]
--------+----------------------------------------------------+------------------------------
bkg 95| 0 3 -3 12 -28 -407 -.18 36 33 | 0 19 2487 2566
cod 239| -1 0 -2 -8 4 139 -.16 18 15 | --- --- --- ---
esx 118| 0 -1 3 -15 47 131 .37 24 21 | 112833 7513 8570 14886
mcc n/a| -4 0 5 -60 -15 609 .03 102 102 | --- --- --- ---
Table 2.1521.6 GPS week: 1521 Day: 6 MJD: 54897
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]
--------+----------------------------------------------------+------------------------------
bkg 95| -1 -1 1 14 -25 -496 -.28 42 37 | 0 37 2841 2892
cod 239| 0 0 -1 1 3 192 -.19 21 16 | --- --- --- ---
esx 118| 1 -1 -3 64 3 129 .30 26 24 | 115607 5507 7414 19268
iac n/a| 0 0 4 -86 -3 -127 .15 38 38 | 240104 -1242 7248 19343
mcc n/a| 16 -4 7 -24 -57 589 -.10 133 133 | --- --- --- ---
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 3.1521.0 GPS week: 1521 Day: 0 MJD: 54891
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 20 8 21 13 --- 9 | 29 32 42 19 --- 28
R03 |>>>>> 28 9 9 19 --- 9 | 40 35 31 31 --- 31
R04 |>>>>> 18 18 17 26 --- 11 | 33 27 37 46 --- 32
R06 |>>>>> 20 25 29 37 --- 16 | 176 184 182 154 --- 180
R07 |>>>>> 26 16 25 32 --- 14 | 26 35 37 26 --- 28
R08 |>>>>> 41 12 29 26 --- 15 | 102 85 102 86 --- 90
R10 |>>>>> 21 11 12 14 --- 8 | 22 25 27 22 --- 21
R11 |>>>>> 18 5 10 18 243 7 | 19 20 27 17 59 18
R13 |>>>>> 30 17 31 20 --- 14 | 28 26 44 28 --- 25
R14 |>>>>> 63 19 16 19 --- 18 | 76 25 24 23 --- 28
R15 |>>>>> 19 13 17 23 52 10 | 23 28 41 30 56 28
R17E |>>>>> 28 24 39 59 --- 21 | 46 52 72 47 --- 49
R18E |>>>>> 34 24 29 41 --- 18 | 41 37 61 56 --- 42
R19E |>>>>> 23 16 18 42 --- 14 | 42 47 7 65 --- 48
R20E |>>>>> 63 29 56 48 --- 27 | 56 46 99 72 --- 61
R21E |>>>>> 60 22 28 34 --- 20 | 39 28 46 46 --- 34
R22E |>>>>> 28 20 32 37 --- 16 | 44 24 39 42 --- 29
R23E |>>>>> 50 21 31 46 --- 20 | 61 9999 9999 55 --- 9999
XR24E |13424 55 32 --- 38 235 28 | 50 79 --- 66 166 63
------+------------------------------------+--------------------------------
RMS |>>>>> 36 18 27 33 176 |T 50 46 54 49 93 46
WRMS |>>>>> 35 15 23 33 176 |NE 52 47 54 43 57 46
MEDI |>>>>> 28 18 25 32 235 |MD 41 32 41 46 59 31
Table 3.1521.1 GPS week: 1521 Day: 1 MJD: 54892
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 26 12 23 17 --- 11 | 15 15 27 18 --- 14
R03 |>>>>> 34 23 27 24 --- 15 | 42 30 33 46 --- 29
R04 |>>>>> 23 15 20 25 --- 12 | 23 21 26 28 --- 15
R06 |>>>>> 47 27 13 20 --- 16 | 175 202 219 157 --- 198
R07 |>>>>> 19 5 11 24 --- 8 | 27 24 30 25 --- 24
R08 |>>>>> 41 9 43 22 --- 17 | 96 76 93 82 --- 80
R10 |>>>>> 24 13 14 21 --- 10 | 14 28 37 19 --- 24
R11 |>>>>> 17 16 23 19 259 11 | 14 15 28 15 79 13
R13 |>>>>> 19 14 15 15 --- 9 | 15 22 27 23 --- 15
XR14 |>>>>> --- 14 13 18 --- 10 | --- 28 25 18 --- 19
R15 |>>>>> 18 24 13 32 80 13 | 16 31 24 19 54 17
R17E |>>>>> 23 24 26 60 --- 19 | 30 22 29 22 --- 19
R18E |>>>>> 22 22 26 68 --- 21 | 17 24 37 41 --- 20
XR19E |>>>>> 23 23 --- 48 --- 22 | 25 29 --- 60 --- 33
R20E |>>>>> 57 25 33 54 --- 23 | 40 40 33 50 --- 34
R21E |>>>>> 51 20 26 39 --- 19 | 25 22 35 43 --- 26
R22E |>>>>> 46 24 29 36 --- 19 | 32 23 40 36 --- 21
R23E |>>>>> 43 17 29 48 --- 19 | 46 9999 9999 46 --- 9999
XR24E |19611 42 25 --- 30 554 22 | 41 44 --- 37 364 33
------+------------------------------------+--------------------------------
RMS |>>>>> 34 19 25 36 192 |T 38 38 46 41 165 35
WRMS |>>>>> 33 18 22 36 192 |NE 43 44 51 40 66 40
MEDI |>>>>> 24 20 23 25 259 |MD 25 24 30 36 79 21
Table 3.1521.2 GPS week: 1521 Day: 2 MJD: 54893
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 23 12 30 28 --- 13 | 14 28 37 17 --- 20
R03 |>>>>> 12 13 29 30 --- 12 | 35 34 21 39 --- 27
R04 |>>>>> 13 11 25 34 --- 12 | 25 25 44 29 --- 22
R06 |>>>>> 38 20 58 41 --- 22 | 78 106 140 85 --- 100
R07 |>>>>> 16 10 16 15 --- 8 | 19 23 40 32 --- 25
R08 |>>>>> 20 12 16 19 --- 9 | 81 73 78 71 --- 74
R10 |>>>>> 33 20 17 17 --- 13 | 15 32 35 23 --- 21
R11 |>>>>> 16 16 20 28 129 11 | 15 18 33 22 71 18
R13 |>>>>> 26 15 34 14 --- 13 | 14 24 42 26 --- 20
R14 |>>>>> 10 13 20 22 --- 9 | 20 25 27 19 --- 17
R15 |>>>>> 25 16 31 27 153 14 | 19 26 52 32 76 27
R17E |>>>>> 44 25 45 53 --- 23 | 26 19 45 35 --- 21
R18E |>>>>> 20 26 21 71 --- 21 | 20 26 28 45 --- 19
XR19E |>>>>> 21 31 --- 67 --- 28 | 31 37 --- 46 --- 31
R20E |>>>>> 50 30 30 62 --- 24 | 33 28 33 52 --- 23
R21E |>>>>> 28 21 25 47 --- 17 | 22 25 30 47 --- 21
R22E |>>>>> 48 27 32 51 --- 22 | 25 20 33 39 --- 19
R23E |>>>>> 63 26 53 39 --- 26 | 46 968 965 33 --- 973
R24E | 8347 33 33 34 67 320 24 | 63 66 75 40 347 56
------+------------------------------------+--------------------------------
RMS |>>>>> 32 20 32 41 218 |T 31 84 97 38 164 80
WRMS |>>>>> 32 16 27 41 218 |NE 30 37 49 35 73 33
MEDI |>>>>> 25 20 29 34 153 |MD 25 26 37 35 76 22
Table 3.1521.3 GPS week: 1521 Day: 3 MJD: 54894
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 14 12 24 19 --- 10 | 18 25 36 19 --- 20
R03 |>>>>> 15 18 30 25 --- 13 | 22 30 33 19 --- 21
R04 |>>>>> 12 7 27 35 --- 12 | 28 23 49 32 --- 19
R06 |>>>>> 27 17 27 21 --- 13 | 159 178 172 141 --- 171
R07 |>>>>> 32 25 15 28 --- 14 | 35 30 27 27 --- 19
R08 |>>>>> 28 18 17 28 --- 13 | 92 81 94 85 --- 86
R10 |>>>>> 13 20 18 22 --- 11 | 14 28 35 14 --- 18
R11 |>>>>> 24 15 29 27 98 13 | 10 26 48 30 50 22
R13 |>>>>> 25 17 23 29 --- 13 | 21 29 50 28 --- 26
R14 |>>>>> 12 10 12 21 --- 7 | 22 22 25 17 --- 18
R15 |>>>>> 22 11 26 20 98 11 | 19 34 43 30 35 28
R17E |>>>>> 45 17 36 44 --- 20 | 33 31 40 30 --- 27
R18E |>>>>> 21 23 27 60 --- 19 | 28 23 45 46 --- 26
XR19E |>>>>> 16 29 --- 64 --- 26 | 30 35 --- 57 --- 35
R20E |>>>>> 43 29 40 76 --- 26 | 40 38 62 62 --- 42
R21E |>>>>> 51 17 31 57 --- 22 | 32 25 47 54 --- 29
R22E |>>>>> 31 23 28 49 --- 18 | 40 23 33 39 --- 22
R23E |>>>>> 53 19 53 43 --- 24 | 32 9999 9999 40 --- 9999
R24E |18689 39 29 39 47 221 21 | 39 43 57 37 185 35
------+------------------------------------+--------------------------------
RMS |>>>>> 31 19 29 39 150 |T 37 40 52 42 90 36
WRMS |>>>>> 31 17 26 39 150 |NE 40 46 55 40 42 40
MEDI |>>>>> 25 18 27 29 98 |MD 30 29 45 32 50 26
Table 3.1521.4 GPS week: 1521 Day: 4 MJD: 54895
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 10 12 16 17 --- 7 | 23 30 32 32 --- 26
R03 |>>>>> 13 14 26 18 --- 10 | 21 27 38 20 --- 21
R04 |>>>>> 19 35 132 42 --- 36 | 18 23 128 30 --- 29
R06 |>>>>> 30 22 31 29 --- 16 | 81 85 79 112 --- 80
R07 |>>>>> 8 12 15 28 --- 9 | 22 24 28 23 --- 19
R08 |>>>>> 21 21 25 20 --- 12 | 84 79 88 80 --- 80
R10 |>>>>> 14 15 20 29 --- 11 | 14 31 37 19 --- 19
R11 |>>>>> 19 22 40 29 40 15 | 17 22 48 24 26 12
R13 |>>>>> 17 11 33 22 --- 11 | 15 24 40 23 --- 19
R14 |>>>>> 9 9 17 23 --- 8 | 19 25 28 22 --- 21
R15 |>>>>> 10 15 24 23 51 10 | 21 30 35 24 27 22
R17E |>>>>> 48 23 43 37 --- 22 | 26 25 28 27 --- 22
R18E |>>>>> 20 21 29 50 --- 17 | 30 24 47 40 --- 27
XR19E |>>>>> 19 32 --- 59 --- 25 | 31 48 --- 60 --- 47
R20E |>>>>> 28 32 35 80 --- 25 | 29 35 64 70 --- 44
R21E |>>>>> 33 33 32 61 --- 22 | 33 25 37 58 --- 28
R22E |>>>>> 36 29 18 45 --- 19 | 34 24 39 44 --- 29
R23E |>>>>> 38 20 39 42 --- 19 | 38 9999 9999 43 --- 9999
R24E |21403 19 18 56 37 130 18 | 70 52 71 42 94 54
------+------------------------------------+--------------------------------
RMS |>>>>> 24 22 43 38 84 |T 32 35 51 41 49 33
WRMS |>>>>> 24 20 29 38 84 |NE 30 36 52 37 26 31
MEDI |>>>>> 19 21 29 29 51 |MD 26 25 39 32 27 26
Table 3.1521.5 GPS week: 1521 Day: 5 MJD: 54896
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx mcc IGL | bkg cod esx mcc IGL
------+-------------------------------+---------------------------
R02 |>>>>> 16 17 24 --- 14 | 28 33 56 --- 37
R03 |>>>>> 10 11 17 --- 9 | 26 21 30 --- 23
R04 |>>>>> 15 15 17 --- 11 | 20 24 69 --- 27
R06 |>>>>> 53 16 22 --- 21 | 137 191 203 --- 180
R07 |>>>>> 25 11 18 --- 12 | 37 22 21 --- 19
R08 |>>>>> 27 16 14 --- 13 | 81 70 78 --- 74
R10 |>>>>> 18 16 20 --- 12 | 19 26 29 --- 21
R11 |>>>>> 16 12 18 69 10 | 10 18 24 43 13
R13 |>>>>> 32 14 23 --- 16 | 13 23 41 --- 23
R14 |>>>>> 28 10 19 --- 13 | 15 19 33 --- 20
R15 |>>>>> 20 20 28 74 16 | 17 24 37 29 21
R17E |>>>>> 54 20 24 --- 23 | 32 26 42 --- 29
R18E |>>>>> 44 15 26 --- 19 | 26 21 38 --- 25
XR19E |>>>>> 49 27 --- --- 36 | 36 40 --- --- 40
R20E |>>>>> 43 22 29 --- 21 | 48 51 79 --- 57
R21E |>>>>> 39 16 15 --- 16 | 44 28 32 --- 30
R22E |>>>>> 49 20 21 --- 21 | 33 16 39 --- 24
R23E |>>>>> 56 18 49 --- 29 | 58 9999 9999 --- 9999
R24E |>>>>> 47 35 29 145 25 | 44 45 51 159 44
------+-------------------------------+---------------------------
RMS |>>>>> 36 18 24 102 |T 38 38 53 77 39
WRMS |>>>>> 33 15 21 102 |NE 36 42 56 36 41
MEDI |>>>>> 32 16 21 74 |MD 32 24 39 43 25
Table 3.1521.6 GPS week: 1521 Day: 6 MJD: 54897
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R02 |>>>>> 31 21 20 22 --- 13 | 36 41 33 18 --- 27
R03 |>>>>> 28 9 17 11 --- 9 | 47 32 38 38 --- 32
R04 |>>>>> 43 21 38 17 --- 17 | 48 32 31 27 --- 27
R06 |>>>>> 53 17 40 36 --- 20 | 132 164 163 165 --- 152
R07 |>>>>> 32 12 19 19 --- 11 | 35 32 19 33 --- 25
R08 |>>>>> 41 18 14 18 --- 13 | 102 86 102 88 --- 91
R10 |>>>>> 32 12 18 16 --- 11 | 29 21 32 15 --- 19
R11 |>>>>> 30 7 16 20 159 10 | 31 19 28 20 53 16
R13 |>>>>> 38 20 27 22 --- 15 | 46 30 37 17 --- 24
R14 |>>>>> 26 10 14 19 --- 9 | 45 31 34 27 --- 31
R15 |>>>>> 32 11 20 27 124 12 | 41 32 39 29 32 29
R17E |>>>>> 47 22 34 55 --- 22 | 41 21 39 50 --- 26
R18E |>>>>> 56 23 31 47 --- 22 | 53 24 29 52 --- 28
XR19E |>>>>> 70 42 --- 44 --- 35 | 40 52 --- 67 --- 39
R20E |>>>>> 41 40 35 57 --- 25 | 41 33 51 54 --- 34
R21E |>>>>> 41 25 21 66 --- 23 | 45 28 40 53 --- 34
R22E |>>>>> 69 34 33 74 --- 29 | 80 24 42 63 --- 36
XR23E |>>>>> --- 224 1446 778 --- 506 | --- 9999 9999 79 --- 9999
R24E |>>>>> 51 15 28 25 112 16 | 51 73 45 46 95 58
------+------------------------------------+--------------------------------
RMS |>>>>> 42 21 26 38 133 |T 52 43 47 49 60 40
WRMS |>>>>> 37 16 24 38 133 |NE 53 47 50 43 42 43
MEDI |>>>>> 41 20 21 25 124 |MD 45 32 38 46 53 29
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