[IGSREPORT-15794] Wk 1457 IGLOS Final Orbits
Gerd Gendt3
igsacc at gfz-potsdam.de
Thu Dec 27 05:58:50 PST 2007
******************************************************************************
IGS Electronic Report 27 Dec 05:58:53 PST 2007 Message Number 15794
******************************************************************************
Author: AC Coordinator / GFZ Potsdam
sum-file Version 2.0
IGLOS Orbit Combination - Week 1457 (Dec 09, 2007 - Dec 15, 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 2.1457.
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:
igl1457[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1457 in the SP3 format.
igl14577.sum Combination Report for GPS Week 1457.
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 | 1485.5 ns
1 | 1500.9 ns
2 | 1506.8 ns
3 | 1497.5 ns
4 | 1473.1 ns
5 | 1477.8 ns
6 | 1485.7 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
----+--------+---------------
0 | BKG | R14 R15
0 | ESX | R19 R20 R23 R24
0 | IAC | R10
1 | BKG | R14 R15
1 | ESX | R19 R20 R23 R24
1 | IAC | R10
2 | BKG | R14
2 | ESX | R19 R20 R23 R24
3 | BKG | R14
3 | ESX | R19 R20 R23 R24
4 | BKG | R15 R21
4 | ESX | R19 R20 R23 R24
5 | BKG | R21
5 | COD | R14
5 | ESX | R19 R20 R23 R24
6 | BKG | R21
6 | ESX | R19 R20 R23 R24
6 | IAC | R14 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 1.1457, 1a.1457).
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 2.1457.0-6)
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 3.1457.0-6).
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 1457 summary. (Dec 09, 2007 - Dec 15, 2007)
Table 1.1457.a GPS week : 1457 MJD: 54443.0-54449.0
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 1 4 8 -130 .02 51 54 | 0 132 3145 3345
| 8 3 11 62 63 62 .17 | 0 343
cod 175| -3 0 -2 -8 37 -39 -.06 39 33 | --- --- --- ---
| 3 5 9 55 39 122 .08 | --- ---
esx 51| 0 6 7 33 56 43 -.21 278 70 | 48383 1655 9750 18948
| 8 6 15 146 116 255 .07 | 48750 5397
iac n/a| 0 0 0 -16 -76 149 .24 42 42 | 1493655 -2892 9050 19045
| 5 5 5 52 62 174 .23 | 13282 4144
mcc n/a| 0 7 49 -26 91 433 .66 688 688 | --- --- --- ---
| 16 25 25 316 342 871 .87 | --- ---
Table 1.1457.b GPS week : 1457 MJD: 54443.0-54449.0
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 | 20 15 36 20 27 23 20 |
R04 | 30 32 28 24 19 32 26 |
R06 | 25 33 34 31 34 26 23 |
R07 | 13 19 21 24 34 31 21 |
R08 | 30 28 33 33 27 24 16 |
R10E | 87 83 84 64 65 57 79 |
R14E | 164 173 381 493 210 400 170 |
R15E | 60 57 99 130 188 165 70 |
R17 | 54 37 39 32 67 60 29 |
R19 | 18 18 20 18 20 15 20 |
R20 | 22 35 35 22 33 15 18 |
R21 | 74 38 62 34 46 60 24 |
R23 | 23 26 35 44 40 33 28 |
R24 | 27 31 26 33 25 50 31 |
Table 1.1457.c GPS week : 1457 MJD: 54443.0-54449.0
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 1457 0 | -118 -26 -674 361 4827 -19080 87.2 4459 4459 | 1485475 0
brd 1457 1 | 481 -58 -524 3261 1904 -23150 81.0 4617 4617 | 1500890 0
brd 1457 2 | -69 -161 -497 -470 -1438 -29190 96.9 3947 3947 | 1506758 0
brd 1457 3 | -291 -10 -87 1782 -1083 -40860 103.7 3803 3803 | 1497543 0
brd 1457 4 | 125 -55 -85 -3229 -479 -37460 87.9 4064 4064 | 1473124 0
brd 1457 5 | -480 -287 53 9265 -947 -40590 91.7 5539 5539 | 1477760 0
brd 1457 6 | -183 -144 449 6881 3386 -54180 106.0 6280 6280 | 1485714 0
-------------+------------------------------------------------------------+----------------
brd 1457 mean| -76 -106 -195 2550 881 -34930 93.5 4672 4672 | 1489609 0
brd 1457 sdev| 309 98 393 4325 2494 12021 9.2 916 916 | 12441 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 2.1457.0 GPS week: 1457 Day: 0 MJD: 54443
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 0 13 -17 -54 -141 -.12 32 28 | 0 795 4498 4908
cod 175| -2 -7 -8 5 10 171 -.02 41 42 | --- --- --- ---
esx 51| 10 7 -4 30 97 -298 -.11 271 77 | -2958 1254 13435 33101
iac n/a| -1 1 -2 26 -22 216 .02 31 31 | 1493785 -1429 12084 35117
mcc n/a| -29 -1 19 35 333 1389 .76 807 807 | --- --- --- ---
Table 2.1457.1 GPS week: 1457 Day: 1 MJD: 54444
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| 13 -6 18 117 31 -85 -.28 57 76 | 0 -66 4279 4742
cod 175| -5 -4 6 12 51 17 -.03 30 27 | --- --- --- ---
esx 51| 3 8 -14 -259 82 -43 -.17 300 62 | 21840 -3627 13299 25712
iac n/a| -3 2 0 14 -123 44 .21 44 44 | 1512189 -10463 13360 26424
mcc n/a| -15 4 33 -96 561 1559 .82 1101 1101 | --- --- --- ---
Table 2.1457.2 GPS week: 1457 Day: 2 MJD: 54445
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| -12 0 1 -73 -66 -251 .20 63 66 | 0 -130 2458 2557
cod 175| -1 5 6 75 -1 -163 -.17 39 32 | --- --- --- ---
esx 51| 7 0 11 -8 270 195 -.29 307 75 | 119668 -2655 8515 14718
iac n/a| -3 -4 3 -6 -150 398 .53 50 50 | 1507687 -2295 7661 14328
mcc n/a| 2 -27 66 -517 -17 219 .51 965 965 | --- --- --- ---
Table 2.1457.3 GPS week: 1457 Day: 3 MJD: 54446
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 4 -5 23 43 -125 .10 60 68 | 0 -116 2602 2683
cod 175| -2 -4 -11 0 8 -24 .05 27 22 | --- --- --- ---
esx 51| -2 3 28 38 48 -153 -.26 221 52 | -1427 11605 8196 15802
iac n/a| 7 -1 5 -27 5 315 .51 56 56 | 1497414 1629 6740 14258
mcc n/a| 15 18 45 -74 125 868 .02 110 110 | --- --- --- ---
Table 2.1457.4 GPS week: 1457 Day: 4 MJD: 54447
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 -9 3 96 -140 .08 49 47 | 0 352 2800 2876
cod 175| -10 -1 -14 -108 19 -202 -.01 61 45 | --- --- --- ---
esx 51| -7 16 22 183 -112 -89 -.29 243 76 | 85177 1271 7233 15023
iac n/a| 5 -7 -5 5 -32 152 .05 36 36 | 1477479 -5893 6727 14315
mcc n/a| 4 30 36 561 305 111 .15 77 77 | --- --- --- ---
Table 2.1457.5 GPS week: 1457 Day: 5 MJD: 54448
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 -9 -51 -46 -110 -.00 48 44 | 0 182 2388 2510
cod 175| -3 4 7 -29 110 -50 -.12 50 41 | --- --- --- ---
esx 51| -12 9 1 92 18 397 -.14 293 84 | 88276 5673 7193 12509
iac n/a| 6 -4 -4 1 -74 -2 .02 33 33 | 1479229 812 6781 13112
mcc n/a| 8 -18 45 3 -335 -354 -.09 1633 1633 | --- --- --- ---
Table 2.1457.6 GPS week: 1457 Day: 6 MJD: 54449
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 -1 30 55 -54 .19 44 51 | 0 -91 2996 3139
cod 175| -1 3 -6 -14 59 -22 -.11 24 24 | --- --- --- ---
esx 51| -4 0 5 159 -5 294 -.24 316 64 | 28107 -1936 10382 15773
iac n/a| -4 8 7 -128 -141 -81 .36 41 41 | 1487803 -2609 9998 15765
mcc n/a| 9 44 97 -95 -335 -756 2.47 123 123 | --- --- --- ---
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 3.1457.0 GPS week: 1457 Day: 0 MJD: 54443
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 3442 30 37 56 29 --- 20 | 68 61 79 57 --- 60
R04 | 2020 58 41 35 55 --- 30 | 54 35 37 54 --- 34
R06 | 3063 24 58 71 36 --- 25 | 22 58 58 43 --- 36
R07 | 5058 19 23 45 12 127 13 | 33 33 53 36 61 30
R08 | 2542 17 47 133 16 --- 29 | 95 80 91 76 --- 78
XR10E | 7793 65 116 --- 649 --- 87 | 82 116 --- 456 --- 65
XR14E |11067 820 210 --- 127 --- 164 | 502 216 --- 268 --- 137
XR15E | 8176 517 77 --- 45 248 59 | 305 72 --- 98 49 74
XR17 | 8466 56 84 --- 87 --- 53 | 96 131 --- 117 --- 94
R19 | 960 23 18 448 31 --- 18 | 117 124 441 129 --- 124
XR20 | 5277 18 32 --- 41 --- 22 | 178 173 --- 198 --- 184
XR21 | ---- --- 94 --- 57 --- 73 | --- 80 --- 144 --- 110
R23 | 6906 26 38 412 32 --- 22 | 57 68 406 52 --- 55
R24 | 7287 40 54 432 16 1135 26 | 117 123 405 115 590 115
------+------------------------------------+--------------------------------
RMS | 4459 32 41 270 31 807 |T 132 97 196 131 233 85
WRMS | 4459 28 42 77 31 807 |NE 83 87 196 92 325 83
MEDI | 5277 30 47 71 36 248 |MD 95 80 79 98 61 74
Table 3.1457.1 GPS week: 1457 Day: 1 MJD: 54444
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4437 30 10 42 25 --- 15 | 98 80 114 65 --- 84
R04 | 1939 72 34 65 58 --- 31 | 88 42 80 48 --- 50
R06 | 2866 108 33 56 28 --- 32 | 40 39 56 34 --- 23
R07 | 4376 52 22 37 19 132 18 | 50 26 53 58 71 37
R08 | 2709 16 36 54 69 --- 28 | 139 106 138 90 --- 108
XR10E | 9046 125 52 --- 499 --- 82 | 72 97 --- 504 --- 65
XR14E |19999 1115 140 --- 212 --- 172 | 9999 79 --- 235 --- 121
XR15E |12185 407 48 --- 68 208 57 | 458 127 --- 59 83 96
XR17 | 7343 83 20 --- 58 --- 37 | 78 50 --- 79 --- 58
R19 | 2456 26 23 455 27 --- 17 | 101 117 310 94 --- 108
R20 | 8419 49 31 473 67 --- 34 | 146 151 325 199 --- 163
XR21 | ---- --- 29 --- 47 --- 37 | --- 51 --- 64 --- 52
R23 | 4058 50 33 399 30 --- 26 | 38 55 248 34 --- 40
R24 | 6344 59 41 453 33 1551 31 | 82 84 281 60 9999 73
------+------------------------------------+--------------------------------
RMS | 4616 57 30 300 44 1100 |T 115 78 178 115 77 77
WRMS | 4616 76 27 62 44 1100 |NE 86 72 178 75 71 72
MEDI | 4437 59 33 65 47 208 |MD 82 79 138 64 71 65
Table 3.1457.2 GPS week: 1457 Day: 2 MJD: 54445
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 4709 63 36 75 72 --- 35 | 41 91 117 70 --- 72
R04 | 2935 62 27 43 60 --- 27 | 62 40 54 55 --- 42
R06 | 3304 82 62 44 44 --- 33 | 26 40 88 46 --- 36
R07 | 3942 43 20 40 40 147 20 | 54 37 69 57 84 41
R08 | 1995 101 36 40 55 --- 33 | 65 80 91 60 --- 60
XR10E | 7679 148 92 --- 127 --- 84 | 58 140 --- 200 --- 97
XR14E | 7732 1277 323 --- 447 --- 380 | 398 160 --- 394 --- 224
XR15E |12158 194 121 --- 115 269 98 | 153 80 --- 151 67 99
XR17 | 6293 78 49 --- 40 --- 39 | 88 124 --- 174 --- 132
R19 | 2503 21 25 479 33 --- 19 | 63 86 359 63 --- 72
R20 | 4059 59 48 516 42 --- 35 | 61 100 298 62 --- 75
XR21 | ---- --- 49 --- 75 --- 61 | --- 68 --- 70 --- 63
R23 | 5755 58 46 421 45 --- 34 | 42 80 337 59 --- 54
R24 | 4804 36 28 402 45 1358 25 | 75 87 380 114 9999 92
------+------------------------------------+--------------------------------
RMS | 3946 63 39 307 50 965 |T 91 86 199 112 75 82
WRMS | 3946 66 32 75 50 965 |NE 57 75 199 75 84 67
MEDI | 4709 63 46 75 45 269 |MD 62 80 117 63 67 72
Table 3.1457.3 GPS week: 1457 Day: 3 MJD: 54446
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5539 32 28 35 46 --- 20 | 89 88 116 127 --- 97
R04 | 3126 46 30 44 52 --- 24 | 47 46 57 55 --- 39
R06 | 3500 95 35 33 39 --- 31 | 33 58 87 63 --- 56
R07 | 5237 34 19 49 68 110 23 | 54 39 37 55 68 31
R08 | 2875 41 20 88 82 --- 33 | 109 122 201 87 --- 125
XR10E | 9806 116 79 --- 77 --- 63 | 81 147 --- 111 --- 95
XR14E |24839 2325 323 --- 749 --- 493 | 9999 80 --- 854 --- 337
XR15E |20517 216 112 --- 258 150 129 | 345 151 --- 256 65 142
XR17 | 6914 34 32 --- 71 --- 31 | 104 122 --- 101 --- 106
R19 | 2011 41 12 420 24 --- 18 | 43 77 328 63 --- 63
XR20 | 2341 33 22 --- 41 --- 21 | 68 86 --- 90 --- 78
XR21 | ---- --- 23 --- 51 --- 34 | --- 53 --- 99 --- 70
R23 | 2962 93 37 389 62 --- 43 | 92 59 320 44 --- 45
XR24 | 5174 41 38 --- 66 857 33 | 88 68 --- 106 490 71
------+------------------------------------+--------------------------------
RMS | 3802 60 27 221 56 110 |T 96 85 163 150 207 96
WRMS | 3802 68 22 52 56 110 |NE 72 74 163 80 279 71
MEDI | 5174 41 30 49 62 150 |MD 81 77 116 90 68 71
Table 3.1457.4 GPS week: 1457 Day: 4 MJD: 54447
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 5931 46 61 50 35 --- 26 | 50 69 96 56 --- 57
R04 | 2796 20 62 33 18 --- 18 | 43 42 85 47 --- 47
R06 | 2052 72 60 46 52 --- 33 | 33 62 36 63 --- 36
R07 | 5620 38 113 74 19 77 33 | 35 81 63 49 39 28
R08 | 4122 32 57 68 36 --- 26 | 37 44 101 46 --- 41
XR10E | 6690 98 90 --- 87 --- 65 | 61 104 --- 153 --- 95
XR14E |19448 299 284 --- 300 --- 210 | 693 217 --- 570 --- 335
XR15E |11028 500 309 --- 114 366 188 | 142 110 --- 375 46 295
XR17 |10014 107 83 --- 89 --- 67 | 96 126 --- 188 --- 135
R19 | 1912 38 26 390 17 --- 19 | 56 83 275 69 --- 62
R20 | 4559 62 33 399 35 --- 32 | 93 79 311 104 --- 83
XR21 | ---- >>>> 75 --- 28 --- 46 | 412 70 --- 54 --- 51
R23 | 3450 64 38 382 55 --- 39 | 68 53 250 30 --- 25
XR24 | 8922 44 35 --- 25 1131 24 | 61 90 --- 91 294 76
------+------------------------------------+--------------------------------
RMS | 4064 49 61 243 36 77 |T 134 87 152 135 126 97
WRMS | 4064 47 45 76 36 77 |NE 89 72 152 72 166 58
MEDI | 5620 62 61 68 35 366 |MD 61 79 96 63 46 57
Table 3.1457.5 GPS week: 1457 Day: 5 MJD: 54448
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 6249 20 44 65 32 --- 23 | 71 57 103 67 --- 67
R04 | 3440 69 52 71 24 --- 31 | 43 38 45 40 --- 29
R06 | 1677 32 37 68 43 --- 25 | 25 61 35 55 --- 33
R07 | 4132 38 79 52 37 84 30 | 30 87 48 36 57 27
R08 | 7135 43 22 59 37 --- 23 | 83 84 81 67 --- 69
XR10E | 2251 73 74 --- 91 --- 57 | 44 58 --- 90 --- 43
XR14E |11788 425 942 --- 376 --- 400 | 374 179 --- 9999 --- 734
XR15E |10957 242 201 --- 246 359 164 | 189 134 --- 321 132 193
XR17 |12913 42 113 --- 87 --- 59 | 82 38 --- 141 --- 81
R19 | 1727 25 20 459 17 --- 15 | 87 83 309 91 --- 85
R20 | 6357 22 25 426 15 --- 14 | 57 59 187 72 --- 59
XR21 | ---- >>>> 69 --- 51 --- 59 | 493 43 --- 72 --- 43
R23 | 3603 33 62 425 42 --- 32 | 53 44 207 63 --- 44
R24 | 9899 96 70 425 38 2307 50 | 207 190 335 216 445 195
------+------------------------------------+--------------------------------
RMS | 5538 48 50 293 33 1632 |T 131 82 150 102 211 121
WRMS | 5538 44 41 84 33 1632 |NE 111 71 150 83 251 66
MEDI | 6249 42 62 71 38 359 |MD 71 59 103 72 132 59
Table 3.1457.6 GPS week: 1457 Day: 6 MJD: 54449
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R01 | 9325 37 18 43 44 --- 19 | 84 57 69 57 --- 61
R04 | 5915 75 19 57 33 --- 26 | 42 26 58 53 --- 35
R06 | 3466 31 34 57 34 --- 22 | 30 53 36 44 --- 35
R07 | 3222 39 21 30 57 123 21 | 47 45 44 38 73 29
R08 | 7885 32 16 42 28 --- 16 | 122 122 146 94 --- 115
XR10E | 3292 69 65 --- 188 --- 78 | 63 64 --- 246 --- 94
XR14E | 8651 250 115 --- 324 --- 169 | 362 241 --- 620 --- 395
XR15E |14814 100 49 --- 346 316 69 | 145 124 --- 252 93 158
XR17 | 8786 54 21 --- 52 --- 28 | 95 103 --- 133 --- 104
R19 | 2439 33 15 468 38 --- 19 | 91 110 445 105 --- 101
R20 | 6799 25 13 474 39 --- 18 | 98 97 358 107 --- 98
XR21 | ---- >>>> 18 --- 32 --- 24 | 310 81 --- 96 --- 79
R23 | 6668 50 29 416 43 --- 27 | 48 69 375 46 --- 41
R24 | 7194 55 36 519 45 --- 31 | 235 237 443 228 --- 231
------+------------------------------------+--------------------------------
RMS | 6280 44 24 316 41 123 |T 126 102 219 151 83 112
WRMS | 6280 51 24 64 41 123 |NE 109 90 219 91 73 84
MEDI | 6799 50 21 57 43 123 |MD 91 81 146 96 73 94
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