[IGSREPORT-15670] Wk 1451 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Fri Nov 16 02:30:20 PST 2007
******************************************************************************
IGS Electronic Report 16 Nov 02:30:28 PST 2007 Message Number 15670
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1451 (Oct 28, 2007 - Nov 03, 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 2.1451.
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:
igl1451[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1451 in the SP3 format.
igl14517.sum Combination Report for GPS Week 1451.
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 | 1241.9 ns
1 | 1290.9 ns
2 | 1277.8 ns
3 | 1284.4 ns
4 | 1285.7 ns
5 | 1242.4 ns
6 | 1277.5 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
0 | IAC | R15 R24
1 | ESX | R10 R14 R23
1 | IAC | R15 R24
2 | COD | R15
2 | ESX | R10 R14 R23
2 | IAC | R24
3 | ESX | R10 R14 R23
4 | ESX | R10 R14 R23 R24
5 | ESX | R04 R10 R23 R24
6 | ESX | R10 R14 R21 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 1.1451, 1a.1451).
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 2.1451.0-6)
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 3.1451.0-6).
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 1451 summary. (Oct 28, 2007 - Nov 03, 2007)
Table 1.1451.a GPS week : 1451 MJD: 54401.0-54407.0
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| -1 0 11 27 15 -90 .04 41 35 | 0 165 3681 3915
| 3 2 8 38 52 148 .06 | 0 1741
cod 175| 0 -1 5 -50 22 -37 .01 48 41 | --- --- --- ---
| 7 3 11 75 86 164 .14 | --- ---
esx 52| 0 -2 11 26 -21 73 -.33 258 72 | 33417 -666 8859 18037
| 5 7 15 121 104 133 .20 | 81908 23755
iac n/a| 0 -1 -17 25 -25 45 .11 35 35 | 1270577 3788 9003 17997
| 4 3 5 58 81 145 .08 | 22811 8138
mcc n/a| 2 0 43 54 -135 -437 .08 236 236 | --- --- --- ---
| 9 12 19 89 141 735 .44 | --- ---
Table 1.1451.b GPS week : 1451 MJD: 54401.0-54407.0
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 | 19 15 14 19 54 250 255 |
R04 | 15 27 24 22 45 0 0 |
R06 | 16 17 40 17 18 13 17 |
R07 | 27 32 18 15 12 19 12 |
R08 | 27 18 28 24 20 28 38 |
R10 | 26 28 15 18 39 25 27 |
R14 | 21 21 18 26 12 18 21 |
R15 | 184 144 122 81 38 54 82 |
R21 | 25 20 24 24 22 17 20 |
R23 | 33 30 29 25 30 50 34 |
R24 | 104 75 137 72 25 24 28 |
Table 1.1451.c GPS week : 1451 MJD: 54401.0-54407.0
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 1451 0 | 60 109 -304 287 -3026 7897 95.0 3254 3254 | 1241948 0
brd 1451 1 | 21 364 -977 -5712 -3374 9353 101.4 3206 3206 | 1290914 0
brd 1451 2 | 118 -277 -833 -957 2791 10420 101.1 4126 4126 | 1277813 0
brd 1451 3 | -118 365 -400 -1835 1421 2393 91.1 5009 5009 | 1284355 0
brd 1451 4 | -54 -215 83 2367 -3423 5343 93.5 6178 6178 | 1285731 0
brd 1451 5 | 11 -144 357 -1993 824 5857 99.6 5509 5509 | 1242391 0
brd 1451 6 | -102 -17 -390 3819 1392 963 98.7 4909 4909 | 1277492 0
-------------+------------------------------------------------------------+----------------
brd 1451 mean| -9 26 -352 -574 -484 6032 97.2 4598 4598 | 1271520 0
brd 1451 sdev| 86 263 469 3131 2678 3492 4.0 1122 1122 | 20579 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 2.1451.0 GPS week: 1451 Day: 0 MJD: 54401
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 8 48 47 120 .07 26 22 | 0 -210 3183 3380
cod 175| -6 0 -11 15 8 -272 -.16 43 39 | --- --- --- ---
esx 52| 0 -6 -2 -155 -35 -108 -.16 249 59 | -38889 3783 5545 20223
iac n/a| -2 1 -18 28 17 18 .16 42 42 | 1237038 4044 6241 20001
mcc n/a| 1 -12 29 122 -146 -760 -.27 97 97 | --- --- --- ---
Table 2.1451.1 GPS week: 1451 Day: 1 MJD: 54402
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 13 35 -103 -100 .14 35 36 | 0 -514 2689 2949
cod 175| 1 -6 -1 -166 25 -246 -.20 43 39 | --- --- --- ---
esx 52| 4 2 21 201 0 90 -.18 247 69 | 45053 -281 8082 17654
iac n/a| 1 -3 -15 59 39 156 .07 29 29 | 1289307 5205 8382 18096
mcc n/a| 23 -9 19 90 -310 -246 -.17 94 94 | --- --- --- ---
Table 2.1451.2 GPS week: 1451 Day: 2 MJD: 54403
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 12 -29 20 -239 .06 32 31 | 0 298 2952 3063
cod 175| 5 -5 5 -70 23 6 .13 34 31 | --- --- --- ---
esx 52| -3 -6 2 17 -26 238 -.39 256 66 | 7413 -12324 8969 15630
iac n/a| -2 4 -16 105 44 62 .14 39 39 | 1278551 -2468 8531 15543
mcc n/a| -1 15 30 148 -228 442 .53 58 58 | --- --- --- ---
Table 2.1451.3 GPS week: 1451 Day: 3 MJD: 54404
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 21 58 38 94 -.05 56 30 | 0 257 2664 2805
cod 175| -1 0 7 -58 35 -7 .06 41 36 | --- --- --- ---
esx 52| 8 6 11 70 -127 107 -.44 232 66 | 26192 1434 10360 19605
iac n/a| 0 -2 -18 46 -68 -97 .14 46 46 | 1280838 8137 10287 19169
mcc n/a| 2 13 50 17 -156 293 .75 398 398 | --- --- --- ---
Table 2.1451.4 GPS week: 1451 Day: 4 MJD: 54405
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 -3 21 7 33 -137 .02 66 59 | 0 -1527 3841 4022
cod 175| 5 0 20 -119 -145 182 .11 86 60 | --- --- --- ---
esx 52| 5 -7 -9 -103 172 -86 -.71 280 87 | 4577 10302 9887 19930
iac n/a| 0 0 -10 26 -19 -59 .14 20 20 | 1276261 7708 9735 19972
mcc n/a| 0 11 79 52 130 -1408 .09 363 363 | --- --- --- ---
Table 2.1451.5 GPS week: 1451 Day: 5 MJD: 54406
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 4 3 76 35 -113 .03 44 47 | 0 -972 4115 4378
cod 175| -14 2 0 9 140 12 -.04 45 42 | --- --- --- ---
esx 52| -5 3 21 96 9 210 -.31 255 66 | 208362 35492 7507 12407
iac n/a| 10 -6 -15 -82 -5 -72 .16 33 33 | 1239531 14500 8016 12423
mcc n/a| -1 -14 46 -121 -188 -1294 -.51 357 357 | --- --- --- ---
Table 2.1451.6 GPS week: 1451 Day: 6 MJD: 54407
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 0 -7 33 -260 .01 26 22 | 0 3827 6329 6811
cod 175| 5 1 18 36 70 62 .15 41 37 | --- --- --- ---
esx 52| -5 -13 33 54 -143 65 -.16 289 89 | -18783 -43068 11667 20812
iac n/a| 0 -4 -29 -4 -187 308 -.06 39 39 | 1292518 -10605 11832 20780
mcc n/a| -8 -1 49 75 -50 -90 .11 289 289 | --- --- --- ---
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 3.1451.0 GPS week: 1451 Day: 0 MJD: 54401
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4172 18 33 37 48 --- 19 | 52 --- 53 42 --- 55
R04 | 4185 14 36 22 28 --- 14 | 41 --- 9999 15 --- 75
R06 | 940 26 33 21 25 --- 15 | 41 --- 29 30 --- 24
R07 | 2352 15 40 90 28 97 26 | 22 --- 82 31 --- 20
R08 | 3927 18 63 52 55 --- 27 | 25 --- 44 50 --- 33
R10 | 2792 34 48 468 28 --- 26 | 53 --- 155 48 --- 43
R14 | 1596 19 33 394 40 --- 21 | 30 --- 190 54 --- 30
XR15 |16535 141 238 --- 674 157 183 | 114 --- --- 262 --- 102
R21 | 4037 47 17 48 51 --- 25 | 68 --- 84 63 --- 65
R23 | 3449 22 62 414 58 --- 33 | 62 --- 116 83 --- 79
XR24 |13261 79 136 --- 4052 451 104 | 160 --- --- 9999 --- 126
------+------------------------------------+--------------------------------
RMS | 3254 26 43 249 42 97 |T 60 --- 94 67 --- 59
WRMS | 3254 22 39 59 42 97 |NE 60 --- 94 67 --- 59
MEDI | 3927 22 40 52 48 157 |MD 52 --- 82 48 --- 55
Table 3.1451.1 GPS week: 1451 Day: 1 MJD: 54402
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 2996 24 34 31 20 --- 15 | 43 --- 30 28 --- 31
R04 | 4158 56 31 66 36 --- 27 | 31 --- 9999 19 --- 66
R06 | 1470 32 27 23 31 --- 17 | 22 --- 39 32 --- 20
R07 | 2328 28 73 102 14 94 31 | 45 --- 111 39 --- 35
R08 | 5139 16 25 57 27 --- 18 | 30 --- 65 23 --- 25
R10 | 2003 33 59 425 24 --- 27 | 32 --- 123 40 --- 29
R14 | 1689 33 32 426 23 --- 20 | 27 --- 127 38 --- 27
XR15 |12831 122 168 --- 635 178 144 | 80 --- --- 211 --- 124
R21 | 4522 40 31 28 34 --- 20 | 63 --- 53 65 --- 57
R23 | 2221 36 51 408 40 --- 29 | 54 --- 145 56 --- 58
XR24 |11355 68 82 --- 4409 373 75 | 200 --- --- 9999 --- 152
------+------------------------------------+--------------------------------
RMS | 3206 35 43 247 29 94 |T 57 --- 86 55 --- 56
WRMS | 3206 36 39 69 29 94 |NE 57 --- 86 55 --- 56
MEDI | 2996 33 34 66 31 178 |MD 43 --- 65 38 --- 35
Table 3.1451.2 GPS week: 1451 Day: 2 MJD: 54403
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4963 20 26 29 22 --- 14 | 58 --- 38 25 --- 51
R04 | 2588 30 31 68 45 --- 24 | 40 --- 9999 27 --- 56
R06 | 2187 45 42 146 47 --- 39 | 46 --- 167 25 --- 34
R07 | 2502 28 22 46 34 58 18 | 47 --- 42 27 --- 27
R08 | 4828 28 49 25 68 --- 27 | 32 --- 44 48 --- 32
R10 | 2920 18 23 413 20 --- 14 | 39 --- 130 39 --- 38
R14 | 2348 24 26 442 26 --- 18 | 31 --- 152 29 --- 25
XR15 |15420 115 335 --- 129 220 122 | 72 --- --- 116 --- 129
R21 | 8051 38 41 71 18 --- 24 | 75 --- 102 100 --- 84
R23 | 2942 42 32 434 46 --- 29 | 63 --- 154 112 --- 83
XR24 |10620 131 142 --- 1067 599 136 | 296 --- --- 9999 --- 212
------+------------------------------------+--------------------------------
RMS | 4126 32 34 256 39 58 |T 72 --- 103 54 --- 70
WRMS | 4126 31 31 66 39 58 |NE 72 --- 103 54 --- 70
MEDI | 2942 30 32 71 45 220 |MD 47 --- 102 29 --- 51
Table 3.1451.3 GPS week: 1451 Day: 3 MJD: 54404
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4297 30 19 49 35 --- 19 | 55 --- 27 48 --- 46
R04 | 1802 23 44 58 24 --- 21 | 25 --- 9999 21 --- 114
R06 | 1764 30 26 48 18 --- 17 | 20 --- 64 39 --- 34
R07 | 2823 15 26 43 17 41 14 | 21 --- 60 33 --- 23
R08 | 4324 29 45 36 44 --- 23 | 38 --- 53 83 --- 58
R10 | 2947 28 26 388 21 --- 17 | 30 --- 111 58 --- 42
R14 | 2698 20 40 443 41 --- 25 | 28 --- 172 66 --- 34
XR15 |10727 89 103 --- 138 124 81 | 89 --- --- 166 --- 73
R21 | 6931 53 34 35 39 --- 23 | 57 --- 89 65 --- 53
R23 | 3090 22 42 390 36 --- 25 | 66 --- 106 59 --- 66
R24 |11219 155 78 171 108 562 72 | 140 --- 105 376 --- 93
------+------------------------------------+--------------------------------
RMS | 5009 56 41 232 46 398 |T 51 --- 87 92 --- 57
WRMS | 5009 30 36 66 46 398 |NE 51 --- 87 92 --- 57
MEDI | 3090 29 40 49 36 124 |MD 38 --- 89 59 --- 53
Table 3.1451.4 GPS week: 1451 Day: 4 MJD: 54405
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9744 119 208 86 17 --- 54 | 170 --- 41 49 --- 166
R04 | 2821 114 62 162 21 --- 44 | 25 --- 9999 24 --- 147
R06 | 1476 20 49 49 21 --- 17 | 36 --- 40 47 --- 35
R07 | 913 23 30 36 9 41 11 | 25 --- 74 32 --- 32
R08 | 6538 31 48 72 15 --- 20 | 28 --- 62 31 --- 29
R10 | 3229 77 82 379 38 --- 39 | 27 --- 95 72 --- 57
R14 | 5105 23 28 509 11 --- 12 | 31 --- 199 48 --- 39
XR15 | 6553 97 65 --- 31 58 38 | 105 --- --- 79 --- 69
R21 | 3599 57 55 60 9 --- 21 | 37 --- 98 64 --- 62
R23 | 4882 46 88 450 18 --- 29 | 25 --- 135 63 --- 54
R24 |12635 55 55 367 19 512 25 | 62 --- 105 408 --- 75
------+------------------------------------+--------------------------------
RMS | 6177 66 86 280 20 363 |T 51 --- 94 83 --- 69
WRMS | 6177 59 59 87 20 363 |NE 51 --- 94 83 --- 69
MEDI | 4882 55 55 86 18 58 |MD 31 --- 95 49 --- 57
Table 3.1451.5 GPS week: 1451 Day: 5 MJD: 54406
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |20294 191 323 --- --- --- 249 | 204 --- --- --- --- 172
XR04 | ---- --- 11 >>>> --- --- 0 | --- --- 9999 --- --- 252
R06 | 1709 21 11 29 22 --- 12 | 37 --- 27 30 --- 22
R07 | 814 31 50 37 20 58 19 | 22 --- 67 50 --- 40
R08 | 6357 27 72 78 24 --- 28 | 20 --- 73 41 --- 32
R10 | 3411 37 42 386 30 --- 25 | 28 --- 114 58 --- 41
XR14 | 5789 20 26 --- 27 --- 17 | 23 --- --- 43 --- 32
XR15 | 6760 75 66 --- 82 67 54 | 57 --- --- 106 --- 51
R21 | 2659 25 44 35 17 --- 16 | 83 --- 89 84 --- 73
R23 | 4946 89 40 358 63 --- 49 | 30 --- 77 109 --- 61
R24 |11191 39 32 410 30 501 24 | 79 --- 104 332 --- 78
------+------------------------------------+--------------------------------
RMS | 5508 44 45 255 33 356 |T 58 --- 78 94 --- 77
WRMS | 5508 47 42 66 33 356 |NE 58 --- 78 94 --- 77
MEDI | 4946 31 42 78 27 67 |MD 30 --- 77 58 --- 51
Table 3.1451.6 GPS week: 1451 Day: 6 MJD: 54407
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR01 |19635 188 342 --- --- --- 254 | 175 --- --- --- --- 196
XR04 | ---- --- 12 --- --- --- 0 | --- --- --- --- --- 326
R06 | 2496 21 19 40 38 --- 16 | 26 --- 38 53 --- 30
R07 | 2244 12 27 33 19 36 12 | 25 --- 33 34 --- 26
R08 | 6297 20 57 179 45 --- 38 | 24 --- 94 50 --- 24
R10 | 3139 30 41 391 44 --- 26 | 25 --- 127 70 --- 41
R14 | 3646 15 32 455 41 --- 21 | 36 --- 257 40 --- 36
XR15 | 6908 60 116 --- 167 87 82 | 67 --- --- 127 --- 77
R21 | 3963 19 36 244 30 --- 19 | 73 --- 219 76 --- 71
R23 | 3073 39 65 321 44 --- 34 | 64 --- 106 100 --- 86
R24 | 9672 39 34 334 43 407 28 | 105 --- 88 473 --- 105
------+------------------------------------+--------------------------------
RMS | 4909 26 41 289 39 289 |T 62 --- 120 113 --- 92
WRMS | 4909 22 37 89 39 289 |NE 62 --- 120 113 --- 92
MEDI | 3646 21 36 244 43 87 |MD 36 --- 94 70 --- 71
More information about the IGSREPORT
mailing list