[IGSREPORT-16321] Wk 1481 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jun 12 05:00:57 PDT 2008
******************************************************************************
IGS Electronic Report 12 Jun 05:01:00 PDT 2008 Message Number 16321
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1481 (May 25, 2008 - May 31, 2008)
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 2.1481.
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:
igl1481[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1481 in the SP3 format.
igl14817.sum Combination Report for GPS Week 1481.
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 | 929.1 ns
1 | 970.6 ns
2 | 906.5 ns
3 | 957.8 ns
4 | 885.3 ns
5 | 888.7 ns
6 | 956.0 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
----+--------+---------------
2 | ESX | R04
3 | ESX | R08
3 | IAC | R15
4 | IAC | R15
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 1.1481, 1a.1481).
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 2.1481.0-6)
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 3.1481.0-6).
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 1481 summary. (May 25, 2008 - May 31, 2008)
Table 1.1481.a GPS week : 1481 MJD: 54611.0-54617.0
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 67| 4 0 -5 2 18 11 -.16 43 40 | 0 125 2872 2974
| 2 4 7 39 39 155 .04 | 0 482
cod 203| -5 0 6 25 25 67 -.18 33 30 | --- --- --- ---
| 1 3 5 35 28 92 .06 | --- ---
esx 115| 0 0 9 -49 -17 -30 .48 60 51 | 17616 3168 8130 19984
| 5 4 5 54 54 88 .13 | 35385 7775
iac n/a| 3 0 -12 -25 -30 -95 .02 54 54 | 928478 -1474 8226 16607
| 3 3 9 50 35 113 .11 | 36042 3882
mcc n/a| -4 17 33 28 -69 154 1.27 308 308 | --- --- --- ---
| 26 48 44 353 230 402 1.58 | --- ---
Table 1.1481.b GPS week : 1481 MJD: 54611.0-54617.0
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
------+------------------------------------+------------------------------------------
R04 | 25 21 24 16 18 24 23 |
R06 | 16 27 30 23 20 25 22 |
R07 | 0 0 0 654 53 39 28 |
R08 | 35 32 38 26 19 32 18 |
R09 | 0 0 0 0 0 0 --- |
R10 | 20 20 20 21 20 11 14 |
R11 | 21 22 25 29 23 31 25 |
R13 | 37 31 35 37 31 56 32 |
R14 | 15 18 18 25 22 23 19 |
R15 | 27 23 31 41 33 33 31 |
R17 | 31 19 19 37 28 24 35 |
R19 | 16 25 15 25 15 15 18 |
R20 | 24 18 14 15 17 15 18 |
R23 | 21 21 21 22 25 24 30 |
R24 | 23 18 22 19 17 17 12 |
Table 1.1481.c GPS week : 1481 MJD: 54611.0-54617.0
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 1481 0 | 10 282 539 -4684 648 -15480 97.7 4396 4396 | 929099 0
brd 1481 1 | -146 125 980 4137 -4701 2833 76.0 >>>>> >>>>> | 970585 0
brd 1481 2 | -131 -20 554 926 1501 -6433 106.9 5498 5498 | 906489 0
brd 1481 3 | -114 -235 373 3802 -1637 -8562 102.8 4521 4521 | 957786 0
brd 1481 4 | -18 -197 434 -518 2896 -13440 98.7 4312 4312 | 885323 0
brd 1481 5 | 55 -339 408 5834 1120 -17670 97.9 3051 3051 | 888735 0
brd 1481 6 | -23 -71 514 2611 -130 -20790 95.7 3180 3180 | 955956 0
-------------+------------------------------------------------------------+----------------
brd 1481 mean| -52 -65 543 1729 -43 -11363 96.5 >>>>> >>>>> | 927710 0
brd 1481 sdev| 78 216 204 3524 2486 7995 9.8 >>>>> >>>>> | 34901 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 2.1481.0 GPS week: 1481 Day: 0 MJD: 54611
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 67| 5 4 2 4 6 183 -.23 40 39 | 0 -56 2249 2331
cod 203| -6 0 3 15 -8 -61 -.19 33 31 | --- --- --- ---
esx 115| -3 -7 -2 -75 -9 -114 .32 57 45 | 8455 11848 7835 19754
iac n/a| 9 0 -3 -25 8 -96 .13 44 44 | 930388 363 8329 16158
mcc n/a| 0 9 50 -123 -98 -495 .37 75 75 | --- --- --- ---
Table 2.1481.1 GPS week: 1481 Day: 1 MJD: 54612
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 67| 1 2 -5 13 55 162 -.09 34 33 | 0 1056 4285 4478
cod 203| -3 -5 0 9 72 -36 -.13 36 36 | --- --- --- ---
esx 115| 1 4 16 -126 -94 -56 .32 48 41 | 59767 2394 9410 20038
iac n/a| 3 3 -9 48 2 -194 .04 42 42 | 972889 812 9264 18452
mcc n/a| -41 -13 49 -515 48 504 1.36 207 207 | --- --- --- ---
Table 2.1481.2 GPS week: 1481 Day: 2 MJD: 54613
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 67| 7 -5 -13 -67 76 60 -.15 49 41 | 0 -295 2418 2499
cod 203| -7 3 10 82 41 86 -.21 28 24 | --- --- --- ---
esx 115| 8 3 9 -93 -9 -65 .54 66 54 | -12935 8942 6703 18738
iac n/a| 1 -1 -7 13 -39 -176 .02 49 49 | 902902 1391 6889 14392
mcc n/a| -2 -2 7 318 233 685 .92 106 106 | --- --- --- ---
Table 2.1481.3 GPS week: 1481 Day: 3 MJD: 54614
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 67| 0 -5 -15 -18 -47 -30 -.16 38 38 | 0 -13 2493 2564
cod 203| -2 2 11 36 26 124 -.08 41 35 | --- --- --- ---
esx 115| -2 -3 12 -45 -54 -113 .50 87 54 | 45542 5109 7567 19740
iac n/a| 6 0 -8 -26 7 65 .01 61 61 | 958838 -835 7296 14936
mcc n/a| 0 0 0 0 0 0 .0 100 100 | --- --- --- ---
Table 2.1481.4 GPS week: 1481 Day: 4 MJD: 54615
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 67| 4 -4 -3 21 23 -118 -.19 58 44 | 0 -172 2956 3016
cod 203| -5 -1 8 44 34 28 -.27 27 23 | --- --- --- ---
esx 115| 1 2 9 6 -25 71 .68 44 76 | -22201 -638 9120 19547
iac n/a| -1 0 -29 -114 -57 -38 -.20 78 78 | 886088 -3931 9209 16564
mcc n/a| 0 0 0 0 0 0 .0 86 86 | --- --- --- ---
Table 2.1481.5 GPS week: 1481 Day: 5 MJD: 54616
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 67| 6 2 2 0 10 73 -.15 44 46 | 0 499 3052 3128
cod 203| -7 2 11 25 16 164 -.16 38 33 | --- --- --- ---
esx 115| -1 -4 8 29 85 -47 .46 69 47 | -11633 6356 8846 18841
iac n/a| 5 -7 -20 -26 -66 -236 .03 49 49 | 889425 1126 8988 16108
mcc n/a| 41 3 121 -83 -161 -22 1.71 782 782 | --- --- --- ---
Table 2.1481.6 GPS week: 1481 Day: 6 MJD: 54617
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 67| 4 0 -3 62 5 -249 -.17 36 36 | 0 -144 2656 2807
cod 203| -3 0 2 -35 -6 164 -.19 30 27 | --- --- --- ---
esx 115| -7 1 13 -39 -17 112 .55 49 39 | 56320 -11834 7431 23230
iac n/a| 0 0 -7 -49 -69 10 .11 57 57 | 958820 -9248 7613 19643
mcc n/a| -29 125 5 603 -509 410 4.52 797 797 | --- --- --- ---
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 3.1481.0 GPS week: 1481 Day: 0 MJD: 54611
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2875 27 46 65 33 --- 25 | 34 69 46 34 --- 32
R06 | 6933 35 18 26 28 --- 15 | 130 134 125 120 --- 127
XR07 | ---- --- 6 --- --- --- 0 | --- 197 --- --- --- 221
R08 | 4560 44 68 85 39 --- 35 | 49 61 49 45 --- 40
XR09E |>>>>> --- 6 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 5060 24 24 55 36 --- 19 | 26 24 24 37 --- 19
R11E | 5119 35 17 52 42 --- 21 | 34 21 72 43 --- 33
R13E | 3438 62 36 82 82 --- 37 | 44 37 74 60 --- 35
R14E | 3966 22 19 27 32 --- 14 | 45 33 52 46 --- 36
R15E | 3144 49 36 37 59 75 26 | 61 30 42 61 44 35
R17 | 7076 29 24 83 70 --- 30 | 52 72 113 31 --- 59
R19 | 2084 38 16 32 25 --- 16 | 29 43 60 23 --- 31
R20 | 1537 50 23 50 39 --- 23 | 30 49 73 62 --- 41
R23 | 4839 32 28 60 23 --- 20 | 35 50 73 32 --- 34
R24 | 2152 51 38 35 22 --- 22 | 46 82 84 45 --- 57
------+------------------------------------+--------------------------------
RMS | 4395 40 33 57 44 75 |T 47 64 68 49 44 57
WRMS | 4395 39 31 45 44 75 |NE 50 84 77 49 --- 71
MEDI | 3966 35 24 52 36 75 |MD 44 49 72 45 44 35
Table 3.1481.1 GPS week: 1481 Day: 1 MJD: 54612
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 |>>>>> 23 48 33 30 --- 20 | 36 64 92 47 --- 42
R06 |>>>>> 50 42 52 39 --- 26 | 71 136 142 102 --- 106
XR07 | ---- --- 6 --- --- --- 0 | --- 509 --- --- --- 496
R08 |>>>>> 60 62 51 42 --- 32 | 35 43 46 40 --- 28
XR09E | ---- --- --- --- --- --- 0 | --- 9999 9999 --- --- 0
R10E |>>>>> 36 29 33 35 --- 19 | 42 32 40 47 --- 32
R11E |>>>>> 31 17 45 54 --- 22 | 34 32 77 57 --- 42
R13E |>>>>> 34 27 69 75 --- 30 | 39 26 65 79 --- 31
R14E |>>>>> 31 25 32 33 --- 17 | 46 44 49 41 --- 35
R15E |>>>>> 43 30 39 48 207 23 | 68 33 68 61 101 42
R17 |>>>>> 26 25 43 34 --- 18 | 36 43 39 32 --- 32
R19 |>>>>> 17 37 76 30 --- 25 | 27 52 104 30 --- 37
R20 |>>>>> 17 31 49 24 --- 18 | 34 27 76 30 --- 33
R23 |>>>>> 27 36 43 41 --- 21 | 38 62 61 22 --- 33
R24 |>>>>> 23 32 29 39 --- 18 | 49 74 67 47 --- 56
------+------------------------------------+--------------------------------
RMS |>>>>> 34 36 48 42 207 |T 42 84 71 48 101 74
WRMS |>>>>> 33 36 41 42 207 |NE 40 112 78 43 --- 95
MEDI |>>>>> 31 30 43 39 207 |MD 38 43 67 47 101 35
Table 3.1481.2 GPS week: 1481 Day: 2 MJD: 54613
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2140 44 27 161 29 --- 23 | 23 51 122 53 --- 38
R06 |11908 73 47 42 39 --- 29 | 185 241 227 217 --- 217
XR07 | ---- --- 11 --- --- --- 0 | --- 637 --- --- --- 645
R08 | 5924 97 29 93 33 --- 37 | 66 47 114 57 --- 44
XR09E | ---- --- --- --- --- --- 0 | --- 9999 9999 --- --- 0
R10E | 2514 43 25 30 38 --- 19 | 40 48 31 49 --- 33
R11E | 2130 41 21 54 62 --- 25 | 29 24 61 82 --- 33
R13E | 8756 42 32 80 85 --- 34 | 32 46 112 118 --- 48
R14E | 4367 26 24 20 47 --- 17 | 29 30 32 44 --- 24
R15E | 4291 50 31 37 90 106 31 | 75 41 45 48 62 35
R17 | 1864 35 19 40 36 --- 18 | 39 73 72 56 --- 55
R19 | 2991 22 11 29 40 --- 14 | 21 39 27 43 --- 29
R20 | 2881 22 22 35 17 --- 14 | 28 50 42 36 --- 34
R23 | 7908 26 33 45 36 --- 20 | 43 34 62 31 --- 28
R24 | 1778 53 23 47 28 --- 21 | 27 59 90 52 --- 48
------+------------------------------------+--------------------------------
RMS | 5497 49 28 66 49 106 |T 49 101 79 68 62 93
WRMS | 5497 41 24 54 49 106 |NE 54 136 94 68 --- 126
MEDI | 2991 42 24 42 38 106 |MD 32 47 62 52 62 35
Table 3.1481.3 GPS week: 1481 Day: 3 MJD: 54614
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 2723 28 23 34 29 --- 16 | 49 50 51 66 --- 48
R06 | 8615 28 32 56 43 --- 22 | 174 192 178 227 --- 186
XR07 |14474 635 672 --- --- --- 653 | 393 317 --- --- --- 470
R08 | 5015 28 46 247 32 --- 26 | 42 48 214 52 --- 36
XR09E | ---- --- --- --- --- --- 0 | --- 9999 9999 --- --- 0
R10E | 1777 40 31 29 39 --- 20 | 28 30 41 44 --- 26
R11E | 2661 38 31 46 78 --- 28 | 28 26 48 78 --- 32
R13E | 3967 38 80 59 71 --- 36 | 33 90 77 58 --- 42
R14E | 4689 55 39 34 39 --- 25 | 49 35 59 50 --- 38
R15E | 5309 67 48 53 151 100 41 | 98 35 61 84 43 55
R17 | 1969 55 28 119 40 --- 37 | 30 74 161 66 --- 67
R19 | 2975 17 47 73 27 --- 25 | 42 56 100 31 --- 46
R20 | 2913 24 24 22 33 --- 15 | 26 31 43 55 --- 29
R23 | 7321 19 27 46 57 --- 21 | 63 67 37 94 --- 60
R24 | 2810 14 36 44 32 --- 18 | 49 57 60 22 --- 40
------+------------------------------------+--------------------------------
RMS | 4520 38 41 87 61 100 |T 78 79 86 71 43 83
WRMS | 4520 38 35 54 61 100 |NE 96 99 105 76 --- 109
MEDI | 2975 28 32 46 39 100 |MD 42 50 60 58 43 42
Table 3.1481.4 GPS week: 1481 Day: 4 MJD: 54615
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3323 38 23 34 31 --- 17 | 50 39 57 55 --- 39
R06 | 2322 47 25 26 44 --- 19 | 113 143 157 153 --- 143
R07 |11364 135 40 79 133 --- 52 | 289 131 54 49 --- 161
R08 | 5415 46 17 42 25 --- 18 | 60 55 154 76 --- 72
XR09E | ---- --- 8 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 1448 45 26 35 36 --- 19 | 22 40 47 37 --- 30
R11E | 2713 43 29 29 63 --- 22 | 33 38 81 68 --- 42
R13E | 1979 87 28 51 60 --- 31 | 51 32 80 54 --- 34
R14E | 3340 54 24 24 56 --- 21 | 34 32 35 37 --- 26
R15E | 4138 59 36 51 201 86 33 | 47 44 78 123 31 40
R17 | 2163 37 43 58 57 --- 28 | 24 65 88 28 --- 45
R19 | 1945 27 18 28 31 --- 14 | 28 35 36 44 --- 28
R20 | 2908 27 14 34 48 --- 17 | 19 39 54 59 --- 34
R23 | 4829 39 24 58 56 --- 25 | 23 37 89 81 --- 41
R24 | 1867 39 16 28 41 --- 17 | 17 42 52 33 --- 31
------+------------------------------------+--------------------------------
RMS | 4312 58 27 44 78 86 |T 57 55 75 64 31 54
WRMS | 4312 44 23 76 78 86 |NE 69 65 82 64 --- 66
MEDI | 2713 43 24 34 48 86 |MD 33 39 57 54 31 39
Table 3.1481.5 GPS week: 1481 Day: 5 MJD: 54616
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3471 29 29 42 59 --- 23 | 28 42 43 40 --- 23
R06 | 2097 35 40 33 60 --- 25 | 123 150 150 177 --- 147
R07 | 7121 46 77 88 54 --- 39 | 99 141 99 40 --- 149
R08 | 3820 49 40 94 31 --- 31 | 57 79 138 72 --- 78
XR09E | ---- --- 12 --- --- --- 0 | --- 9999 --- --- --- 9999
R10E | 820 21 15 19 22 --- 11 | 40 20 31 26 --- 18
R11E | 1658 42 39 80 54 --- 30 | 24 29 79 54 --- 25
R13E | 2789 100 48 167 56 --- 56 | 45 44 158 49 --- 41
R14E | 1446 46 24 45 45 --- 23 | 33 28 37 31 --- 16
R15E | 3491 45 29 68 83 131 33 | 59 46 77 90 26 42
R17 | 2891 34 30 38 58 --- 23 | 30 41 77 62 --- 39
R19 | 1212 21 29 24 28 --- 15 | 47 27 40 26 --- 26
R20 | 2209 25 21 35 22 --- 14 | 18 40 38 33 --- 23
R23 | 2257 30 42 49 41 --- 23 | 56 59 24 28 --- 35
R24 | 1800 26 29 21 35 1099 16 | 43 58 47 35 8 40
------+------------------------------------+--------------------------------
RMS | 3050 44 38 69 49 782 |T 50 57 74 54 17 50
WRMS | 3050 46 33 47 49 782 |NE 55 70 72 57 8 62
MEDI | 2209 34 29 42 45 131 |MD 43 42 47 40 8 35
Table 3.1481.6 GPS week: 1481 Day: 6 MJD: 54617
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04 | 3756 23 43 42 46 --- 22 | 26 49 27 39 --- 27
R06 | 1518 35 38 45 26 --- 21 | 167 150 167 167 --- 160
R07 | 5589 59 40 50 41 --- 28 | 130 109 61 26 --- 120
R08 | 2205 27 14 54 28 --- 18 | 33 34 52 44 --- 38
R10E | 1499 27 14 25 31 --- 14 | 44 28 32 30 --- 24
R11E | 2358 28 24 42 75 --- 24 | 31 29 50 66 --- 34
R13E | 6272 65 25 43 85 --- 32 | 39 41 73 61 --- 30
R14E | 972 44 18 30 36 --- 18 | 34 25 24 39 --- 18
R15E | 4240 35 39 43 93 360 30 | 35 40 49 82 36 31
R17 | 3414 27 31 83 100 --- 34 | 46 47 104 62 --- 41
R19 | 1432 11 30 45 35 --- 18 | 51 60 53 38 --- 46
R20 | 1880 35 24 39 26 --- 18 | 30 36 47 37 --- 27
R23 | 1631 35 45 74 58 --- 30 | 42 77 79 54 --- 48
R24 | 1750 15 9 31 27 1068 11 | 67 64 55 57 7 57
------+------------------------------------+--------------------------------
RMS | 3180 36 30 49 57 797 |T 55 56 62 57 21 50
WRMS | 3180 36 27 39 57 797 |NE 65 69 71 58 7 62
MEDI | 1880 28 25 43 36 360 |MD 39 41 52 44 7 34
More information about the IGSREPORT
mailing list