[IGSREPORT-15626] Wk 1449 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Nov 2 09:07:13 PDT 2007
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IGS Electronic Report 02 Nov 09:07:31 PDT 2007 Message Number 15626
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1449 (Oct 14, 2007 - Oct 20, 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 2.1449.
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:
igl1449[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1449 in the SP3 format.
igl14497.sum Combination Report for GPS Week 1449.
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 | 1278.7 ns
1 | 1285.2 ns
2 | 1292.7 ns
3 | 1316.8 ns
4 | 1296.7 ns
5 | 1276.3 ns
6 | 1246.0 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 | R10 R14 R23
1 | ESX | R10 R14 R23
2 | ESX | R10 R14 R23
3 | BKG | R15
3 | ESX | R10 R14 R23
4 | COD | R15
4 | ESX | R10 R14 R23
5 | ESX | R10 R14 R23
6 | ESX | R10 R14 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 1.1449, 1a.1449).
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 2.1449.0-6)
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 3.1449.0-6).
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 1449 summary. (Oct 14, 2007 - Oct 20, 2007)
Table 1.1449.a GPS week : 1449 MJD: 54387.0-54393.0
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| 0 0 5 28 4 -119 -.04 40 36 | 0 326 4045 4353
| 4 2 6 44 79 206 .07 | 0 623
cod 175| -4 -3 -5 -31 -64 -71 -.11 41 36 | --- --- --- ---
| 5 3 6 85 43 76 .08 | --- ---
esx 52| 4 5 28 -116 96 188 -.24 229 66 | 5211 4972 9494 21126
| 6 9 14 128 129 237 .20 | 11654 20638
iac n/a| 4 0 -14 16 3 72 .14 34 34 | 1285846 82 9693 21607
| 2 1 6 50 30 88 .09 | 18513 7420
mcc n/a| 1 0 20 27 -38 -79 .05 53 53 | --- --- --- ---
| 8 4 9 168 126 1160 .18 | --- ---
Table 1.1449.b GPS week : 1449 MJD: 54387.0-54393.0
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 | 14 19 24 20 21 26 30 |
R04 | 24 18 13 15 29 19 20 |
R06 | 23 22 18 16 33 22 31 |
R07 | 17 17 17 20 39 26 19 |
R08 | 25 37 29 25 36 22 24 |
R10 | 45 15 23 25 23 24 18 |
R14 | 25 19 27 21 17 22 19 |
R15 | 219 222 271 134 316 307 182 |
R21 | 24 29 21 14 25 25 24 |
R23 | 32 43 33 37 33 33 34 |
R24 | 0 0 0 0 0 1139 708 |
Table 1.1449.c GPS week : 1449 MJD: 54387.0-54393.0
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 1449 0 | 117 130 173 -8131 9275 12320 99.4 4833 4833 | 1278677 0
brd 1449 1 | 600 238 100 413 -2899 15270 75.1 5525 5525 | 1285209 0
brd 1449 2 | 47 310 -252 -5357 5344 9048 83.2 5247 5247 | 1292684 0
brd 1449 3 | -8 194 -926 -3270 1020 -419 104.4 4359 4359 | 1316820 0
brd 1449 4 | -221 -107 -500 -2778 -1718 -4000 98.9 4941 4941 | 1296652 0
brd 1449 5 | -70 -16 -138 -5706 -877 -9399 92.0 4981 4981 | 1276272 0
brd 1449 6 | -115 52 -49 -3968 -1008 -10630 95.1 4562 4562 | 1246049 0
-------------+------------------------------------------------------------+----------------
brd 1449 mean| 50 114 -227 -4113 1305 1741 92.6 4921 4921 | 1284623 0
brd 1449 sdev| 266 147 381 2684 4412 10512 10.2 393 393 | 21755 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 2.1449.0 GPS week: 1449 Day: 0 MJD: 54387
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| 7 0 8 71 -25 74 -.04 46 38 | 0 203 3002 3183
cod 175| -2 0 -17 -70 -67 -168 .01 35 29 | --- --- --- ---
esx 52| 2 16 34 -268 -88 245 -.17 181 58 | -6951 -2836 9674 32403
iac n/a| 3 1 -6 80 50 19 .04 32 32 | 1268711 -3727 10093 33219
mcc n/a| 2 0 25 295 -158 1267 .25 39 39 | --- --- --- ---
Table 2.1449.1 GPS week: 1449 Day: 1 MJD: 54388
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 1 9 88 -70 19 -.01 38 33 | 0 804 3366 3662
cod 175| -5 -8 -11 -164 0 -190 -.06 42 34 | --- --- --- ---
esx 52| -1 15 32 84 192 261 -.06 237 73 | -1059 16784 9697 13264
iac n/a| 5 0 -9 52 12 35 .08 32 32 | 1283440 12379 9486 13286
mcc n/a| -6 1 30 223 -11 1881 -.13 56 56 | --- --- --- ---
Table 2.1449.2 GPS week: 1449 Day: 2 MJD: 54389
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| -1 0 10 35 58 -61 -.08 28 26 | 0 370 4306 4627
cod 175| 2 -2 -1 -102 -101 -20 -.08 36 33 | --- --- --- ---
esx 52| -4 -6 10 -90 -82 115 -.31 244 59 | 26709 -28842 8274 17759
iac n/a| 4 0 -15 18 15 -6 .26 37 37 | 1297842 -9685 8400 18295
mcc n/a| 0 -1 30 -37 43 -604 .06 32 32 | --- --- --- ---
Table 2.1449.3 GPS week: 1449 Day: 3 MJD: 54390
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| -6 -3 8 -25 17 -122 .03 45 41 | 0 -824 4175 4413
cod 175| -6 -1 0 -15 -134 -52 -.18 28 29 | --- --- --- ---
esx 52| 16 5 11 -64 227 -7 -.20 256 59 | 8429 2295 8296 17249
iac n/a| 0 0 -8 36 -2 145 .13 30 30 | 1313107 2600 8766 17948
mcc n/a| 5 -2 21 -107 2 -859 .10 61 61 | --- --- --- ---
Table 2.1449.4 GPS week: 1449 Day: 4 MJD: 54391
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 -4 -8 26 -103 -105 -.02 45 44 | 0 70 3645 4107
cod 175| -3 -2 -3 61 -34 0 -.19 72 63 | --- --- --- ---
esx 52| 5 -1 51 -41 177 -193 -.65 228 74 | 8738 19823 9401 23123
iac n/a| 4 -2 -18 -77 18 33 .15 31 31 | 1299744 -3131 9981 23527
mcc n/a| 16 2 7 -140 -98 -806 .16 63 63 | --- --- --- ---
Table 2.1449.5 GPS week: 1449 Day: 5 MJD: 54392
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| 1 0 1 31 25 -79 -.19 36 33 | 0 522 4067 4425
cod 175| -13 -7 -6 63 -49 -42 -.07 34 34 | --- --- --- ---
esx 52| 2 10 32 -273 126 411 -.07 226 75 | -6572 34143 10062 21010
iac n/a| 7 3 -19 18 -41 36 .07 39 39 | 1276528 6103 10060 21634
mcc n/a| -8 5 11 -68 162 -400 -.26 47 47 | --- --- --- ---
Table 2.1449.6 GPS week: 1449 Day: 6 MJD: 54393
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 -1 7 -28 132 -559 .01 42 37 | 0 1141 5758 6055
cod 175| -1 -3 0 9 -66 -22 -.18 37 32 | --- --- --- ---
esx 52| 8 -3 25 -160 120 488 -.22 228 68 | 7183 -6562 11058 23077
iac n/a| 4 2 -24 -9 -28 241 .28 36 36 | 1261553 -3960 11070 23344
mcc n/a| 4 -7 13 25 -208 -1036 .15 73 73 | --- --- --- ---
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 3.1449.0 GPS week: 1449 Day: 0 MJD: 54387
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 7922 23 20 34 23 --- 14 | 42 54 87 67 --- 55
R04 | 3387 38 35 76 26 --- 23 | 54 62 79 47 --- 50
R06 | 3713 27 40 69 31 --- 23 | 22 59 68 34 --- 28
R07 | 3596 22 34 45 19 39 16 | 35 33 59 22 37 21
R08 | 7149 49 27 72 30 --- 24 | 42 51 93 54 --- 48
R10 | 1905 89 37 346 54 --- 44 | 60 52 62 48 --- 49
R14 | 4707 38 25 351 37 --- 24 | 36 29 106 39 --- 28
XR15 |15532 --- 265 --- 179 181 218 | --- 192 --- 146 46 145
R21 | 2996 45 51 46 22 --- 23 | 114 124 95 125 --- 116
XR23 | ---- --- 37 415 27 --- 31 | --- 76 156 88 --- 78
XR24 | ---- --- 14 --- --- --- 0 | --- 365 --- --- --- 336
------+------------------------------------+--------------------------------
RMS | 4832 46 35 181 32 39 |T 50 99 89 67 41 86
WRMS | 4832 38 29 58 32 39 |NE 50 99 89 67 41 86
MEDI | 3713 38 35 72 27 39 |MD 42 59 87 48 37 50
Table 3.1449.1 GPS week: 1449 Day: 1 MJD: 54388
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6595 37 20 32 35 --- 19 | 52 35 57 62 --- 45
R04 | 6189 21 37 40 29 --- 17 | 32 38 66 55 --- 40
R06 | 2811 17 34 66 39 --- 21 | 33 39 53 41 --- 32
R07 | 3273 20 27 66 18 56 17 | 16 42 72 31 73 26
R08 | 8099 58 57 138 33 --- 37 | 32 53 154 62 --- 50
R10 | 1499 23 21 368 17 --- 14 | 29 25 71 52 --- 27
R14 | 6384 21 36 385 22 --- 18 | 25 32 84 28 --- 22
XR15 | 8885 --- 279 --- 175 207 222 | --- 179 --- 146 71 119
R21 | 4474 34 57 100 29 --- 28 | 106 111 52 100 --- 95
R23 | 6754 73 63 425 48 --- 43 | 83 84 97 48 --- 60
XR24 | ---- --- 17 --- --- 456 0 | --- 231 --- --- 196 247
------+------------------------------------+--------------------------------
RMS | 5524 38 42 237 32 56 |T 45 79 78 62 113 69
WRMS | 5524 33 34 73 32 56 |NE 45 79 78 62 113 69
MEDI | 6189 23 36 100 29 207 |MD 32 42 71 52 73 45
Table 3.1449.2 GPS week: 1449 Day: 2 MJD: 54389
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3389 16 33 75 50 --- 23 | 39 57 84 32 --- 39
R04 | 9645 15 19 41 21 --- 12 | 38 43 56 37 --- 37
R06 | 1753 28 22 34 41 --- 18 | 14 35 55 48 --- 24
R07 | 1899 24 23 66 10 32 17 | 26 31 41 36 74 27
R08 | 6204 31 49 97 39 --- 28 | 30 40 136 51 --- 36
R10 | 1607 27 24 323 44 --- 23 | 28 44 31 39 --- 31
R14 | 1613 32 50 405 31 --- 27 | 35 32 99 38 --- 27
XR15 | 7709 --- 272 --- 269 200 271 | --- 245 --- 333 58 138
R21 | 7403 22 38 65 33 --- 21 | 33 55 96 51 --- 44
R23 | 6168 48 46 490 44 --- 32 | 57 86 183 61 --- 67
XR24 | ---- --- 9 --- --- 599 0 | --- 491 --- --- 270 513
------+------------------------------------+--------------------------------
RMS | 5246 28 36 244 37 32 |T 33 105 86 72 134 89
WRMS | 5246 26 33 59 37 32 |NE 33 105 86 72 134 89
MEDI | 3389 27 33 75 39 200 |MD 33 44 84 39 74 37
Table 3.1449.3 GPS week: 1449 Day: 3 MJD: 54390
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 1887 37 30 49 27 --- 19 | 57 63 78 38 --- 49
R04 | 6295 32 23 36 16 --- 14 | 45 37 52 44 --- 40
R06 | 1650 37 21 38 19 --- 15 | 24 30 68 49 --- 34
R07 | 2879 57 26 36 27 61 20 | 28 52 57 49 43 40
R08 | 4204 46 36 70 30 --- 25 | 33 65 84 48 --- 43
R10 | 3824 29 32 365 40 --- 24 | 30 42 77 46 --- 33
R14 | 1842 21 33 436 28 --- 20 | 23 26 152 33 --- 27
XR15 | 9815 1435 137 --- 131 251 134 | 828 185 --- 268 51 211
R21 | 8177 35 15 31 21 --- 14 | 60 78 58 51 --- 55
R23 | 3774 80 33 504 51 --- 37 | 54 101 199 136 --- 105
XR24 | ---- --- 9 --- --- 551 0 | --- 426 --- --- 138 366
------+------------------------------------+--------------------------------
RMS | 4359 45 28 256 30 61 |T 118 100 91 76 77 91
WRMS | 4359 41 29 59 30 61 |NE 118 100 91 76 77 91
MEDI | 3774 37 30 49 27 251 |MD 33 63 77 48 51 43
Table 3.1449.4 GPS week: 1449 Day: 4 MJD: 54391
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5312 50 26 41 20 --- 20 | 29 70 84 51 --- 49
R04 | 4196 65 33 56 37 --- 28 | 44 43 58 39 --- 30
R06 | 1022 35 105 60 28 --- 32 | 22 113 42 41 --- 35
R07 | 2661 50 136 47 30 63 38 | 23 126 35 30 20 31
R08 | 3002 40 61 102 45 --- 36 | 36 63 116 39 --- 33
R10 | 3965 28 48 383 25 --- 22 | 25 58 100 30 --- 23
R14 | 2476 22 32 388 20 --- 16 | 26 35 110 42 --- 25
XR15 | 7086 382 524 --- 263 214 316 | 422 477 --- 170 32 88
R21 |10462 33 75 43 28 --- 25 | 69 73 136 88 --- 82
R23 | 5039 61 45 386 35 --- 33 | 58 92 120 110 --- 80
XR24 | ---- --- 5 --- --- --- 0 | --- 669 --- --- --- 595
------+------------------------------------+--------------------------------
RMS | 4940 45 72 228 31 63 |T 75 165 89 64 26 97
WRMS | 4940 44 63 74 31 63 |NE 75 165 89 64 26 97
MEDI | 3965 40 48 60 28 63 |MD 29 73 100 41 20 35
Table 3.1449.5 GPS week: 1449 Day: 5 MJD: 54392
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3452 40 39 51 54 --- 26 | 32 65 37 43 --- 32
R04 | 3964 23 31 43 37 --- 19 | 28 52 67 54 --- 43
R06 | 775 33 32 62 29 --- 22 | 37 62 67 49 --- 44
R07 | 5276 41 20 80 37 47 25 | 26 66 51 23 22 24
R08 | 3669 35 35 48 35 --- 21 | 23 54 47 33 --- 26
R10 | 3123 22 36 396 40 --- 23 | 20 35 107 49 --- 18
R14 | 3111 24 29 370 40 --- 22 | 23 38 81 56 --- 27
XR15 | 6228 434 373 --- 498 444 306 | 315 538 --- 246 44 289
R21 | 8980 42 31 63 39 --- 24 | 50 74 72 81 --- 62
R23 | 7323 54 46 381 34 --- 32 | 58 53 113 77 --- 50
XR24 | 5744 1210 1071 --- --- --- 1138 | 289 617 --- --- --- 919
------+------------------------------------+--------------------------------
RMS | 4980 36 34 226 39 47 |T 81 150 71 71 33 139
WRMS | 4980 33 34 75 39 47 |NE 81 150 71 71 33 139
MEDI | 3964 40 35 63 37 47 |MD 32 62 67 49 22 43
Table 3.1449.6 GPS week: 1449 Day: 6 MJD: 54393
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6338 60 25 88 27 --- 30 | 61 62 68 64 --- 56
R04 | 1696 22 35 28 45 --- 20 | 30 48 54 38 --- 38
R06 | 748 52 67 51 42 --- 31 | 43 90 50 39 --- 40
R07 | 2544 32 23 52 19 73 18 | 21 41 64 29 41 23
R08 | 5338 30 51 51 33 --- 24 | 35 34 40 47 --- 28
R10 | 3755 31 26 387 19 --- 18 | 47 39 80 46 --- 39
R14 | 4005 23 22 352 30 --- 18 | 25 28 102 53 --- 31
XR15 | 9532 361 260 --- 130 182 182 | 303 356 --- 187 69 215
R21 | 6745 60 29 36 33 --- 23 | 59 94 74 87 --- 79
R23 | 5750 50 35 420 56 --- 34 | 72 87 148 89 --- 78
XR24 | 3879 767 652 --- --- --- 707 | 240 804 --- --- --- 483
------+------------------------------------+--------------------------------
RMS | 4561 42 37 228 36 73 |T 85 153 75 67 55 100
WRMS | 4561 37 32 68 36 73 |NE 85 153 75 67 55 100
MEDI | 4005 50 35 52 33 73 |MD 47 62 68 47 41 40
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