[IGSREPORT-15227] Wk 1431 IGLOS Final Orbits
Gerd Gendt3
igsacc at kg31.gfz-potsdam.de
Tue Jun 26 23:36:33 PDT 2007
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IGS Electronic Report 26 Jun 23:36:38 PDT 2007 Message Number 15227
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1431 (Jun 10, 2007 - Jun 16, 2007)
Contact: Gerd Gendt (gendt at gfz-potsdam.de)
Thomas Nischan ( nisn at gfz-potsdam.de)
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 2.1431.
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:
igl1431[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1431 in the SP3 format.
igl14317.sum Combination Report for GPS Week 1431.
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 | 1092.1 ns
1 | 1121.7 ns
2 | 1120.1 ns
3 | 1137.2 ns
4 | 1091.3 ns
5 | 1113.1 ns
6 | 1077.0 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
----+--------+---------------
0 | ESX | R23 R24
1 | ESX | R23 R24
2 | ESX | R23
3 | ESX | R23 R24
4 | ESX | R23 R24
5 | ESX | R19 R23
6 | ESX | R23 R24
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 1.1431, 1a.1431).
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 2.1431.0-6)
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 3.1431.0-6).
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 1431 summary. (Jun 10, 2007 - Jun 16, 2007)
Table 1.1431.a GPS week : 1431 MJD: 54261.0-54267.0
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 58| -2 0 -4 3 34 1 -.04 36 33 | 0 385 4672 4906
| 3 1 7 43 41 214 .10 | 0 611
cod 168| 1 0 1 15 -64 138 .02 42 41 | --- --- --- ---
| 7 4 5 70 74 160 .14 | --- ---
esx 44| -3 2 7 28 -9 -273 -.36 202 74 | 364935 262091 255435 445534
| 4 5 9 51 116 271 .17 | 846350 699435
iac n/a| 1 0 6 -12 -38 -40 .16 49 49 | 1332814 195853 252680 445066
| 3 2 12 58 47 153 .08 | 514301 527303
mcc n/a| -6 1 6 -11 -102 1597 .50 217 217 | --- --- --- ---
| 17 10 20 265 102 389 .57 | --- ---
Table 1.1431.b GPS week : 1431 MJD: 54261.0-54267.0
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 | 16 18 16 27 20 25 24 |
R03 | 24 27 35 33 29 30 31 |
R04 | 25 36 24 26 19 24 24 |
R06 | 22 18 19 25 18 22 16 |
R07 | 16 26 18 20 19 20 16 |
R08 | 15 26 31 26 24 55 24 |
R10E | 21 30 49 36 25 24 21 |
R14E | 26 20 27 21 30 24 33 |
R15E | 0 0 0 0 0 0 0 |
R19 | 30 23 25 39 33 18 28 |
R21 | 40 29 38 26 21 25 50 |
R22 | 1289 1570 0 0 0 0 0 |
R23 | 33 22 40 40 24 48 49 |
R24 | 26 23 23 17 17 18 17 |
Table 1.1431.c GPS week : 1431 MJD: 54261.0-54267.0
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 1431 0 | 371 -361 -1213 -8000 -4194 -327900 94.5 5738 5738 | 1092130 0
brd 1431 1 | -34 194 -1303 -3995 -1346 -348400 83.5 3315 3315 | 1121658 0
brd 1431 2 | -130 -305 -1118 -4285 -4574 -351100 81.9 4083 4083 | 1120093 0
brd 1431 3 | -158 554 -828 480 5914 -353200 73.4 8321 8321 | 1137235 0
brd 1431 4 | 10 -823 -1360 3688 3643 -344900 78.2 10180 10180 | 1091286 0
brd 1431 5 | 33 336 -1499 -9904 -2032 -339200 87.1 9412 9412 | 1113061 0
brd 1431 6 | -487 56 -40 -189 10260 -352300 83.9 7779 7779 | 1076978 0
-------------+------------------------------------------------------------+----------------
brd 1431 mean| -56 -49 -1051 -3172 1095 -345285 83.2 6975 6975 | 1107491 0
brd 1431 sdev| 257 473 493 4827 5620 9081 6.7 2644 2644 | 21232 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 2.1431.0 GPS week: 1431 Day: 0 MJD: 54261
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 58| -5 0 0 -46 117 -327 -.13 27 24 | 0 588 4679 4992
cod 168| -7 4 4 45 -182 459 -.07 48 48 | --- --- --- ---
esx 44| 1 0 -1 5 -61 -45 -.38 219 69 | -20403 29737 24514 33015
iac n/a| 5 -3 1 10 -25 56 .16 32 32 | 1082567 13689 23507 31638
mcc n/a| -5 -11 14 -70 -188 1879 .00 359 359 | --- --- --- ---
Table 2.1431.1 GPS week: 1431 Day: 1 MJD: 54262
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 58| 2 -2 5 4 -8 33 -.05 33 30 | 0 343 3429 3617
cod 168| -4 -6 9 121 -63 11 -.25 45 43 | --- --- --- ---
esx 44| -5 3 3 -52 -35 -494 -.55 221 92 | 8830 -15630 15162 34869
iac n/a| 1 0 -1 -18 35 -9 .24 30 30 | 1132243 -8449 14225 32967
mcc n/a| -9 11 8 42 -107 1335 .10 269 269 | --- --- --- ---
Table 2.1431.2 GPS week: 1431 Day: 2 MJD: 54263
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 58| -3 2 0 62 17 -244 -.10 27 23 | 0 568 3812 3964
cod 168| 11 0 -7 -23 -138 179 .16 52 57 | --- --- --- ---
esx 44| -7 -3 -1 -15 137 152 -.52 168 67 | 2039908 -4928 282441 999999
iac n/a| -4 -2 6 73 -68 183 .24 55 55 | 2279943 -737 347017 999999
mcc n/a| 10 13 8 2 -55 1713 .85 84 84 | --- --- --- ---
Table 2.1431.3 GPS week: 1431 Day: 3 MJD: 54264
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 58| 0 1 -2 0 27 -22 -.11 40 36 | 0 -284 4099 4238
cod 168| 12 6 1 -15 -21 6 .04 53 49 | --- --- --- ---
esx 44| -5 6 21 84 130 -97 -.24 229 67 | 54686 -8235 11760 25108
iac n/a| 0 -3 -3 -36 -83 30 .06 38 38 | 1137572 -2606 11495 24910
mcc n/a| 1 0 18 127 -149 1536 .14 98 98 | --- --- --- ---
Table 2.1431.4 GPS week: 1431 Day: 4 MJD: 54265
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 58| -5 1 -6 20 7 166 -.05 43 44 | 0 -407 3687 3899
cod 168| 0 -1 1 -31 -10 121 .12 27 29 | --- --- --- ---
esx 44| 0 -4 18 70 42 -424 -.48 211 58 | -39092 -2339 13231 25751
iac n/a| 1 0 -4 34 7 -140 .22 35 35 | 1091048 -13554 12900 25953
mcc n/a| -41 -5 7 206 -78 1081 1.48 294 294 | --- --- --- ---
Table 2.1431.5 GPS week: 1431 Day: 5 MJD: 54266
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 58| 0 -1 -15 -58 28 199 .14 58 49 | 0 1427 6720 7141
cod 168| -4 -5 0 85 30 169 .09 40 32 | --- --- --- ---
esx 44| -8 11 2 37 -146 -528 -.29 161 73 | -427882 1847901 999999 999999
iac n/a| 6 4 13 -106 -42 -121 .07 56 56 | 808794 1391500 999999 999999
mcc n/a| -6 -7 -37 184 86 2254 .88 171 171 | --- --- --- ---
Table 2.1431.6 GPS week: 1431 Day: 6 MJD: 54267
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 58| -2 0 -11 41 53 202 .04 25 25 | 0 466 6278 6494
cod 168| 0 1 -1 -75 -65 17 .08 31 27 | --- --- --- ---
esx 44| -2 4 7 72 -134 -474 -.09 206 93 | 938498 -11869 440942 999999
iac n/a| -1 -1 30 -47 -93 -283 .13 100 100 | 1797531 -8872 359620 999999
mcc n/a| 9 7 23 -569 -224 1385 .05 246 246 | --- --- --- ---
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 3.1431.0 GPS week: 1431 Day: 0 MJD: 54261
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5025 26 41 22 20 --- 16 | 77 51 65 69 --- 64
R03 | 9623 34 43 61 37 --- 23 | 66 55 69 77 --- 63
R04 | 4812 34 51 69 39 --- 25 | 64 58 39 62 --- 54
R06 | 7275 19 58 63 29 --- 22 | 36 37 62 41 --- 37
R07 | 2604 23 30 37 25 25 15 | 35 42 37 36 43 29
R08 | 3578 21 38 31 20 --- 15 | 43 58 66 60 --- 43
XR10E | 6272 28 28 --- 32 --- 21 | 24 29 --- 45 --- 26
XR14E | 5025 29 38 --- 42 --- 26 | 36 32 --- 44 --- 32
XR15E | ---- --- 28 --- --- 5022 0 | --- 9999 --- --- 56 9999
R19 | 3186 23 29 147 31 --- 30 | 59 68 125 67 --- 59
R21 | 9677 42 52 193 25 --- 40 | 42 46 165 48 --- 38
XR22 | ---- --- 1750 --- 952 --- 1289 | --- 396 --- 159 --- 880
R23 | 2518 23 67 448 48 --- 32 | 29 39 357 64 --- 26
R24 | 2348 19 56 452 34 507 25 | 44 70 365 65 66 48
------+------------------------------------+--------------------------------
RMS | 5737 27 48 219 32 359 |T 46 75 135 64 55 107
WRMS | 5737 24 48 69 32 359 |NE 49 83 135 68 54 121
MEDI | 4812 23 41 63 32 507 |MD 42 51 66 62 56 43
Table 3.1431.1 GPS week: 1431 Day: 1 MJD: 54262
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3762 32 42 53 14 --- 18 | 45 39 69 33 --- 34
R03 | 3671 34 63 76 35 --- 27 | 45 71 92 82 --- 59
R04 | 1818 57 39 155 29 --- 35 | 59 52 109 70 --- 45
R06 | 3807 20 38 60 25 --- 18 | 38 41 68 67 --- 43
R07 | 2339 33 34 71 51 60 26 | 36 27 46 40 30 29
R08 | 2994 28 46 112 25 --- 26 | 66 50 87 75 --- 62
XR10E | 6216 42 57 --- 33 --- 30 | 22 26 --- 57 --- 30
XR14E | 4083 28 28 --- 26 --- 19 | 30 34 --- 36 --- 26
XR15E | ---- --- 11 --- --- 5324 0 | --- 9999 --- --- 47 9999
R19 | 2209 22 49 87 21 --- 22 | 35 45 123 50 --- 42
R21 | 4645 25 58 125 25 --- 29 | 27 51 88 39 --- 17
XR22 | ---- --- 1501 --- 1605 --- 1570 | --- 351 --- 137 --- 9999
R23 | 4030 14 45 471 31 --- 22 | 28 36 237 35 --- 31
R24 | 2706 41 30 436 26 376 23 | 32 58 267 69 46 51
------+------------------------------------+--------------------------------
RMS | 3315 33 45 221 30 269 |T 38 67 118 60 41 39
WRMS | 3315 30 43 92 30 269 |NE 41 74 118 63 38 41
MEDI | 3671 28 42 87 26 376 |MD 35 45 88 57 46 34
Table 3.1431.2 GPS week: 1431 Day: 2 MJD: 54263
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3434 8 37 49 23 --- 15 | 47 52 57 43 --- 36
R03 | 7217 49 61 87 62 --- 35 | 67 55 113 58 --- 58
R04 | 1508 28 33 62 53 --- 23 | 40 47 79 30 --- 24
R06 | 6657 17 25 50 48 --- 19 | 30 27 41 44 --- 22
R07 | 2067 20 44 32 31 84 17 | 33 41 64 37 40 24
R08 | 2879 30 43 80 72 --- 30 | 44 62 83 89 --- 52
XR10E | 4287 63 83 --- 65 --- 49 | 37 27 --- 58 --- 25
XR14E | 5427 29 26 --- 55 --- 26 | 32 34 --- 34 --- 24
XR15E | ---- --- 15 --- --- 5393 0 | --- 9999 --- --- 42 9999
R19 | 1766 20 54 92 19 --- 25 | 47 76 74 61 --- 53
R21 | 3650 21 73 125 71 --- 38 | 25 53 60 86 --- 25
XR22 | ---- --- 15 --- --- --- 0 | --- 532 --- --- --- 724
R23 | 3243 26 74 453 76 --- 40 | 40 33 268 77 --- 39
XR24 | 1931 31 37 --- 29 213 23 | 39 64 --- 63 64 44
------+------------------------------------+--------------------------------
RMS | 4082 27 52 168 55 84 |T 40 84 93 56 48 88
WRMS | 4082 23 57 67 55 84 |NE 41 94 93 58 52 100
MEDI | 3243 26 37 80 53 213 |MD 39 52 74 58 42 36
Table 3.1431.3 GPS week: 1431 Day: 3 MJD: 54264
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2787 17 79 45 37 --- 27 | 47 83 50 43 --- 38
R03 |24036 74 60 59 29 --- 33 | 77 45 60 45 --- 41
R04 | 1979 45 38 60 39 --- 26 | 47 45 65 56 --- 44
R06 | 8288 37 57 43 34 --- 24 | 40 63 75 53 --- 37
R07 | 2591 24 30 42 41 91 20 | 29 29 28 40 65 25
R08 | 3299 52 25 65 34 --- 26 | 75 48 96 89 --- 62
XR10E | 2977 62 50 --- 38 --- 36 | 34 27 --- 42 --- 29
XR14E | 4033 30 27 --- 29 --- 20 | 29 33 --- 44 --- 28
XR15E | ---- --- 8 --- --- 2429 0 | --- 9999 --- --- 61 9999
R19 | 1523 33 61 128 50 --- 39 | 65 60 168 85 --- 69
R21 | 1898 26 41 85 30 --- 26 | 38 33 92 68 --- 42
XR22 | ---- --- 8 --- --- --- 0 | --- 694 --- --- --- 797
R23 | 2563 37 81 482 50 --- 39 | 24 55 341 52 --- 25
R24 | 2036 23 21 503 27 105 17 | 56 52 446 64 160 56
------+------------------------------------+--------------------------------
RMS | 8320 40 53 229 38 98 |T 46 97 142 56 95 99
WRMS | 8320 36 49 67 38 98 |NE 49 109 142 59 112 112
MEDI | 2591 33 38 60 34 105 |MD 40 48 75 52 65 41
Table 3.1431.4 GPS week: 1431 Day: 4 MJD: 54265
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6635 43 29 40 32 --- 20 | 40 58 56 46 --- 43
R03 |29194 79 29 47 40 --- 28 | 45 49 53 49 --- 35
R04 | 2485 39 25 42 32 --- 19 | 28 32 39 39 --- 21
R06 | 7577 32 28 48 24 --- 18 | 29 38 48 40 --- 32
R07 | 5145 24 22 27 47 142 18 | 29 30 43 38 51 27
R08 | 3632 53 27 52 42 --- 24 | 60 84 70 61 --- 61
XR10E | 3275 45 27 --- 34 --- 24 | 31 27 --- 47 --- 27
XR14E | 4683 56 32 --- 39 --- 29 | 32 38 --- 44 --- 27
XR15E | ---- --- 7 --- --- 2303 0 | --- 9999 --- --- 87 9999
R19 | 2664 29 35 117 42 --- 32 | 50 61 85 60 --- 48
R21 | 1919 31 20 72 22 --- 20 | 31 42 71 65 --- 39
XR22 | ---- --- 7 --- --- --- 0 | --- 978 --- --- --- 9999
R23 | 3726 41 30 390 30 --- 23 | 32 49 262 71 --- 46
R24 | 3472 28 16 514 27 391 16 | 48 43 401 69 176 52
------+------------------------------------+--------------------------------
RMS |10180 43 27 211 35 294 |T 37 117 112 52 104 38
WRMS |10180 44 29 58 35 294 |NE 39 133 112 53 113 40
MEDI | 3632 39 27 48 32 391 |MD 32 43 56 47 87 35
Table 3.1431.5 GPS week: 1431 Day: 5 MJD: 54266
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7436 73 22 50 32 --- 25 | 58 58 63 49 --- 49
R03 |25824 52 39 77 45 --- 29 | 66 40 85 56 --- 46
R04 | 4614 59 36 43 29 --- 23 | 46 51 52 45 --- 36
R06 | 3463 19 40 57 28 --- 21 | 25 33 54 29 --- 20
R07 | 1796 28 22 64 26 171 20 | 50 34 46 47 33 37
R08 | 3456 104 75 77 115 --- 54 | 87 88 58 76 --- 54
XR10E | 2840 31 30 --- 39 --- 24 | 28 23 --- 34 --- 20
XR14E | 4212 47 25 --- 31 --- 23 | 29 24 --- 48 --- 25
XR15E | ---- --- 11 --- --- 5385 0 | --- 9999 --- --- 48 9999
R19 | 1731 27 23 293 24 --- 17 | 42 37 219 27 --- 36
R21 | 2850 50 21 75 29 --- 24 | 29 55 68 71 --- 41
XR22 | ---- --- 11 --- --- --- 0 | --- 392 --- --- --- 416
R23 | 3944 58 49 346 89 --- 48 | 42 41 132 58 --- 30
XR24 | 5446 37 19 --- 20 281 17 | 35 39 --- 39 74 35
------+------------------------------------+--------------------------------
RMS | 9412 58 40 161 56 171 |T 44 70 86 48 51 65
WRMS | 9412 49 32 73 56 171 |NE 48 78 86 49 53 72
MEDI | 3463 47 23 75 29 281 |MD 42 40 63 47 48 36
Table 3.1431.6 GPS week: 1431 Day: 6 MJD: 54267
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7780 28 24 95 47 --- 23 | 62 60 64 50 --- 49
R03 |18325 27 41 115 72 --- 30 | 67 60 66 101 --- 65
R04 | 3555 34 29 69 57 --- 23 | 72 78 45 63 --- 64
R06 | 2514 10 21 60 40 --- 15 | 33 36 48 40 --- 31
R07 | 6194 16 26 44 43 187 15 | 25 25 57 38 37 28
R08 | 6687 22 31 51 85 --- 23 | 71 86 74 65 --- 70
XR10E | 2809 19 23 --- 59 --- 20 | 22 21 --- 48 --- 19
XR14E | 5074 40 34 --- 86 --- 33 | 29 30 --- 68 --- 31
XR15E | ---- --- 6 --- --- 7534 0 | --- 9999 --- --- 47 9999
R19 | 4164 16 38 115 56 --- 27 | 64 62 139 57 --- 61
R21 | 5689 22 29 123 218 --- 50 | 37 40 102 217 --- 51
XR22 | ---- --- 6 --- --- --- 0 | --- 350 --- --- --- 498
R23 | 6442 40 42 393 162 --- 49 | 25 50 315 131 --- 34
R24 | 3929 22 22 456 33 293 17 | 46 66 421 72 88 58
------+------------------------------------+--------------------------------
RMS | 7778 25 31 206 100 246 |T 46 74 133 79 57 81
WRMS | 7778 25 27 93 100 246 |NE 50 83 133 83 62 91
MEDI | 5074 22 26 95 57 293 |MD 37 60 66 63 47 51
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