[IGSREPORT-16465] Wk 1487 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Jul 24 07:18:43 PDT 2008
******************************************************************************
IGS Electronic Report 24 Jul 07:18:45 PDT 2008 Message Number 16465
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1487 (Jul 06, 2008 - Jul 12, 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 2.1487.
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:
igl1487[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1487 in the SP3 format.
igl14877.sum Combination Report for GPS Week 1487.
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 | 859.1 ns
1 | 858.1 ns
2 | 846.5 ns
3 | 774.9 ns
4 | 842.1 ns
5 | 841.3 ns
6 | 838.4 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
----+--------+---------------
4 | ESX | R04
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 1.1487, 1a.1487).
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 2.1487.0-6)
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 3.1487.0-6).
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 1487 summary. (Jul 06, 2008 - Jul 12, 2008)
Table 1.1487.a GPS week : 1487 MJD: 54653.0-54659.0
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 65| 1 0 -9 -16 5 28 -.11 37 32 | 0 -82 2596 2742
| 3 2 2 31 32 101 .03 | 0 333
cod 215| -3 -2 0 -7 4 -47 -.09 28 23 | --- --- --- ---
| 2 1 2 43 29 29 .05 | --- ---
esx 112| 2 3 11 127 -40 7 .37 79 56 | 33141 3497 7621 16041
| 6 4 8 48 56 81 .13 | 25636 5154
iac n/a| 3 0 3 -38 3 -62 .03 42 42 | 835934 -515 7389 14422
| 2 1 6 28 43 117 .06 | 27663 2109
mcc n/a| 2 2 37 -91 -33 -584 .61 395 395 | --- --- --- ---
| 7 8 16 92 104 441 .67 | --- ---
Table 1.1487.b GPS week : 1487 MJD: 54653.0-54659.0
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 | 34 20 44 20 30 35 46 |
R06 | 19 19 24 22 24 26 36 |
R07 | 28 32 34 44 24 45 36 |
R10 | 17 23 18 12 17 12 15 |
R11 | 15 16 16 16 13 16 19 |
R13 | 23 20 20 16 12 25 33 |
R14 | 14 12 13 13 13 14 16 |
R15 | 33 19 20 23 13 17 18 |
R17 | 18 28 26 27 30 26 25 |
R19 | 18 18 18 15 36 37 18 |
R20 | 19 18 18 19 17 22 22 |
R23 | 32 29 22 30 24 24 18 |
R24 | 21 17 29 17 20 17 23 |
Table 1.1487.c GPS week : 1487 MJD: 54653.0-54659.0
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 1487 0 | 372 79 369 -2840 3595 -15540 103.9 4749 4749 | 859135 0
brd 1487 1 | 60 271 618 -1618 -3055 -12380 96.7 >>>>> >>>>> | 858113 0
brd 1487 2 | -413 -36 420 1886 -3331 -21570 94.8 3506 3506 | 846452 0
brd 1487 3 | -20 -127 524 -2031 1552 -19280 100.1 3350 3350 | 774912 0
brd 1487 4 | 267 142 676 -282 3085 -14240 95.1 3417 3417 | 842052 0
brd 1487 5 | 440 26 394 -81 1817 -11130 100.8 4192 4192 | 841264 0
brd 1487 6 | 53 399 478 -1863 -1262 -15090 96.4 5373 5373 | 838366 0
-------------+------------------------------------------------------------+----------------
brd 1487 mean| 108 107 497 -975 343 -15604 98.3 >>>>> >>>>> | 837184 0
brd 1487 sdev| 288 180 115 1594 2867 3688 3.4 >>>>> >>>>> | 28651 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 2.1487.0 GPS week: 1487 Day: 0 MJD: 54653
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 65| 1 -2 -11 -32 -5 36 -.06 36 26 | 0 546 4531 4845
cod 215| -3 0 3 48 20 -41 -.02 22 18 | --- --- --- ---
esx 112| 6 -1 27 109 -68 -111 .27 80 66 | 50463 113 10821 19585
iac n/a| 3 1 -8 -76 55 54 .08 45 45 | 858241 -261 10413 18689
mcc n/a| 0 9 14 -60 -4 -1301 .89 533 533 | --- --- --- ---
Table 2.1487.1 GPS week: 1487 Day: 1 MJD: 54654
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 65| 0 0 -6 -29 -11 25 -.11 31 31 | 0 56 1915 2139
cod 215| -1 -2 0 33 2 -31 -.12 27 23 | --- --- --- ---
esx 112| -3 7 3 102 -65 10 .22 76 64 | 41015 8807 10830 22966
iac n/a| 0 1 7 -47 13 -23 -.00 31 31 | 852137 434 11025 20669
mcc n/a| 14 -11 31 -197 73 -1032 1.09 289 289 | --- --- --- ---
Table 2.1487.2 GPS week: 1487 Day: 2 MJD: 54655
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 65| 0 0 -8 22 -21 -172 -.12 43 33 | 0 82 2347 2421
cod 215| 0 -4 -1 27 27 -34 -.13 31 21 | --- --- --- ---
esx 112| -2 -3 11 87 76 126 .45 57 53 | 38471 11961 6549 14922
iac n/a| 1 1 0 -40 -32 100 .11 42 42 | 844840 3508 6263 13126
mcc n/a| -3 -3 24 -119 -241 -422 .62 139 139 | --- --- --- ---
Table 2.1487.3 GPS week: 1487 Day: 3 MJD: 54656
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 65| -3 0 -12 22 -2 120 -.12 30 30 | 0 -252 2211 2318
cod 215| -8 -2 -2 -40 33 -107 -.03 30 27 | --- --- --- ---
esx 112| 12 6 10 84 -19 -30 .27 69 49 | -24142 1284 5657 14033
iac n/a| 4 -1 8 -8 -16 -57 .04 38 38 | 775370 -2358 5437 12973
mcc n/a| -6 -2 38 35 14 -151 1.30 263 263 | --- --- --- ---
Table 2.1487.4 GPS week: 1487 Day: 4 MJD: 54657
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 65| 0 0 -12 -14 -25 60 -.06 32 32 | 0 -396 2226 2362
cod 215| -4 -1 4 -43 14 -16 -.10 26 27 | --- --- --- ---
esx 112| 8 0 14 145 -36 -47 .42 135 52 | 44674 -999 6139 11991
iac n/a| 3 -1 2 -17 -63 -111 .02 43 43 | 842161 -2326 5755 10564
mcc n/a| 5 10 63 -18 -35 -651 -.25 348 348 | --- --- --- ---
Table 2.1487.5 GPS week: 1487 Day: 5 MJD: 54658
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 65| 1 -5 -7 -64 48 134 -.14 37 35 | 0 -306 2260 2338
cod 215| -2 0 2 -16 -52 -57 -.08 31 22 | --- --- --- ---
esx 112| 0 9 4 222 -80 15 .38 68 58 | 44123 -1193 6821 15155
iac n/a| 3 0 10 -7 51 -220 -.05 53 53 | 842664 -2204 6487 13255
mcc n/a| 2 7 54 -216 41 -402 -.39 487 487 | --- --- --- ---
Table 2.1487.6 GPS week: 1487 Day: 6 MJD: 54659
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 65| 7 1 -9 -19 55 -8 -.15 50 39 | 0 -305 2686 2773
cod 215| -5 -3 -1 -59 -17 -43 -.16 30 25 | --- --- --- ---
esx 112| -1 3 8 141 -86 91 .59 65 54 | 37389 4510 6536 13638
iac n/a| 7 -1 7 -70 16 -181 -.02 45 45 | 836125 -399 6348 11681
mcc n/a| 7 5 33 -61 -79 -133 1.02 703 703 | --- --- --- ---
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 3.1487.0 GPS week: 1487 Day: 0 MJD: 54653
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 3794 82 21 70 64 --- 33 | 114 88 86 81 --- 82
R06E | 3112 39 20 36 39 --- 18 | 50 49 87 66 --- 52
R07E | 4050 46 35 66 60 --- 27 | 55 45 56 49 --- 39
R10 | 5133 31 20 36 36 --- 16 | 36 34 40 33 --- 25
R11 | 4716 12 19 46 34 149 14 | 16 23 38 34 113 17
R13 |11580 24 18 106 26 --- 22 | 29 25 69 31 --- 23
R14 | 3879 18 10 61 23 --- 14 | 28 32 42 29 --- 29
R15 | 3537 26 27 123 79 90 32 | 24 47 75 18 25 25
R17 | 3009 15 10 81 35 --- 18 | 36 55 63 44 --- 42
R19 | 1591 34 12 59 33 --- 17 | 36 49 64 39 --- 42
R20 | 1428 20 18 71 37 --- 18 | 21 26 76 34 --- 24
R23 | 4201 34 25 144 44 --- 31 | 47 52 105 55 --- 35
R24 | 3337 27 31 53 43 906 20 | 163 183 181 160 215 171
------+------------------------------------+--------------------------------
RMS | 4748 36 22 80 45 532 |T 50 54 75 51 117 46
WRMS | 4748 26 18 66 45 532 |NE 43 52 75 47 117 43
MEDI | 3794 27 20 66 37 149 |MD 36 47 69 39 113 35
Table 3.1487.1 GPS week: 1487 Day: 1 MJD: 54654
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
XR04E |>>>>> --- 27 34 27 --- 20 | --- 98 139 111 --- 110
R06E |>>>>> 31 26 43 36 --- 19 | 44 78 78 62 --- 59
R07E | 3968 53 30 101 54 --- 31 | 29 47 112 61 --- 37
R10 |>>>>> 41 24 85 25 --- 23 | 21 40 62 24 --- 22
R11 |>>>>> 20 17 58 23 97 15 | 17 20 61 32 25 16
R13 |>>>>> 25 23 86 15 --- 19 | 12 29 115 30 --- 24
R14 |>>>>> 19 10 34 23 --- 11 | 15 18 38 21 --- 16
R15 |>>>>> 27 22 46 42 83 19 | 21 28 56 21 19 19
R17 |>>>>> 27 29 124 28 --- 27 | 54 59 117 51 --- 42
R19 |>>>>> 31 21 68 20 --- 18 | 26 43 84 52 --- 38
R20 |>>>>> 16 27 52 33 --- 17 | 28 35 51 39 --- 26
R23 |>>>>> 31 46 108 34 --- 28 | 34 44 88 24 --- 21
R24 |>>>>> 28 31 47 18 484 17 | 158 171 156 144 72 156
------+------------------------------------+--------------------------------
RMS |>>>>> 31 27 76 31 289 |T 38 54 89 51 38 45
WRMS |>>>>> 31 23 64 31 289 |NE 38 48 82 43 38 38
MEDI |>>>>> 27 26 58 27 97 |MD 26 43 84 39 25 26
Table 3.1487.2 GPS week: 1487 Day: 2 MJD: 54655
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2595 101 59 101 38 --- 44 | 105 106 141 105 --- 117
R06E | 5045 51 22 52 41 --- 23 | 36 56 96 63 --- 53
R07E | 5525 34 46 56 86 --- 33 | 60 70 61 52 --- 41
R10 | 2810 39 17 41 25 --- 17 | 19 22 39 30 --- 19
R11 | 2289 16 15 48 33 106 16 | 20 22 51 28 35 19
R13 | 4223 24 28 49 40 --- 20 | 18 43 68 46 --- 30
R14 | 2231 22 17 32 23 --- 13 | 21 30 44 20 --- 23
R15 | 5478 26 21 57 37 111 20 | 24 26 63 26 23 20
XR17 | 2881 37 36 --- 35 --- 25 | 48 66 --- 58 --- 49
R19 | 2620 21 28 45 33 --- 18 | 18 36 53 26 --- 23
R20 | 2071 21 23 57 19 --- 17 | 40 22 82 26 --- 31
R23 | 1505 39 27 40 46 --- 21 | 45 27 46 35 --- 17
R24 | 2314 51 32 72 47 185 28 | 109 146 187 117 138 132
------+------------------------------------+--------------------------------
RMS | 3505 43 31 57 42 139 |T 43 51 77 48 65 44
WRMS | 3505 33 21 53 42 139 |NE 36 44 70 41 65 36
MEDI | 2620 34 27 49 37 111 |MD 36 36 61 35 35 30
Table 3.1487.3 GPS week: 1487 Day: 3 MJD: 54656
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2028 30 24 53 37 --- 19 | 46 53 106 62 --- 43
R06E | 3266 28 25 50 51 --- 21 | 61 46 74 70 --- 51
R07E | 4429 40 64 175 28 --- 44 | 37 57 171 36 --- 28
R10 | 1668 16 11 42 21 --- 12 | 38 29 60 37 --- 32
R11 | 2266 13 13 59 25 137 15 | 21 18 75 17 70 16
R13 | 5655 18 27 38 28 --- 15 | 21 40 44 28 --- 23
R14 | 3541 18 19 30 23 --- 12 | 19 36 42 25 --- 24
R15 | 4764 37 25 60 44 144 23 | 37 32 54 27 35 20
R17 | 2479 31 51 57 51 --- 27 | 27 53 83 48 --- 42
R19 | 2857 26 14 48 20 --- 15 | 46 57 119 55 --- 56
R20 | 3369 31 24 45 36 --- 18 | 27 37 38 23 --- 15
R23 | 2200 49 22 69 67 --- 29 | 25 30 45 64 --- 24
R24 | 2410 26 20 51 27 410 17 | 58 84 105 78 240 73
------+------------------------------------+--------------------------------
RMS | 3349 30 30 69 38 263 |T 35 44 78 43 115 34
WRMS | 3349 30 27 49 38 263 |NE 31 41 66 40 115 32
MEDI | 2857 28 24 51 28 144 |MD 37 40 74 37 70 28
Table 3.1487.4 GPS week: 1487 Day: 4 MJD: 54657
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 2509 53 35 444 34 --- 29 | 45 59 354 63 --- 52
R06E | 4603 26 29 54 60 --- 23 | 38 31 65 62 --- 34
R07E | 4280 36 30 38 61 --- 23 | 43 28 48 36 --- 28
R10 | 1630 25 23 47 26 --- 17 | 25 45 48 44 --- 32
R11 | 2784 16 12 43 15 57 12 | 29 20 55 26 34 21
R13 | 4080 14 17 35 21 --- 12 | 19 35 42 29 --- 22
R14 | 3522 21 15 32 28 --- 13 | 24 41 43 25 --- 28
R15 | 5538 19 15 30 26 113 12 | 26 27 37 18 27 22
R17 | 2614 40 44 51 75 --- 30 | 48 57 56 39 --- 36
R19 | 2787 29 40 134 40 --- 36 | 21 60 111 53 --- 38
R20 | 4091 28 17 36 42 --- 17 | 34 49 66 28 --- 36
R23 | 1367 47 18 56 46 --- 23 | 41 29 21 41 --- 27
R24 | 1613 34 16 55 36 590 19 | 118 101 136 85 227 104
------+------------------------------------+--------------------------------
RMS | 3417 32 26 135 43 348 |T 39 44 83 42 96 36
WRMS | 3417 32 27 52 43 348 |NE 38 46 61 38 96 36
MEDI | 2787 28 18 47 36 113 |MD 34 41 55 39 34 32
Table 3.1487.5 GPS week: 1487 Day: 5 MJD: 54658
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 4593 67 46 81 50 --- 34 | 41 37 147 35 --- 25
R06E | 7285 30 28 71 60 --- 26 | 37 53 86 71 --- 46
R07E | 2336 53 57 65 126 --- 44 | 57 53 62 50 --- 36
R10 | 4826 15 19 29 24 --- 12 | 34 37 49 44 --- 33
R11 | 3608 16 19 56 21 67 16 | 37 29 78 30 30 32
R13 | 2133 41 28 77 32 --- 25 | 24 54 119 24 --- 38
R14 | 4827 18 16 36 31 --- 14 | 17 25 41 26 --- 20
R15 | 6035 12 22 58 20 112 16 | 22 28 51 25 19 22
R17 | 2982 40 26 51 65 --- 25 | 41 49 79 29 --- 39
R19 | 2695 45 20 143 35 --- 36 | 61 63 106 44 --- 55
R20 | 4380 41 32 45 34 --- 22 | 24 45 38 24 --- 19
R23 | 1962 27 36 63 49 --- 24 | 44 71 45 38 --- 43
R24 | 3009 25 22 30 41 834 16 | 107 101 100 95 111 98
------+------------------------------------+--------------------------------
RMS | 4192 37 31 68 53 487 |T 42 49 77 41 53 38
WRMS | 4192 35 22 57 53 487 |NE 41 50 70 37 53 39
MEDI | 3608 30 26 58 35 112 |MD 37 49 78 35 30 36
Table 3.1487.6 GPS week: 1487 Day: 6 MJD: 54659
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg cod esx iac mcc IGL | bkg cod esx iac mcc IGL
------+------------------------------------+--------------------------------
R04E | 7170 133 49 53 51 --- 45 | 46 51 91 51 --- 37
R06E | 5563 55 35 112 55 --- 36 | 66 57 137 100 --- 74
R07E | 7589 41 43 82 87 --- 36 | 54 63 63 57 --- 45
R10 | 6248 24 24 41 19 --- 15 | 23 49 67 37 --- 37
R11 | 3248 14 23 40 50 84 19 | 29 28 50 33 23 26
R13 | 1989 26 44 112 41 --- 32 | 28 76 94 26 --- 33
R14 | 2320 22 25 26 35 --- 15 | 20 36 32 22 --- 21
R15 | 6695 20 19 60 23 128 17 | 23 23 67 28 19 23
R17 | 9160 54 23 60 41 --- 25 | 38 64 95 36 --- 51
R19 | 1339 35 23 33 33 --- 17 | 64 63 82 57 --- 57
R20 | 3096 31 18 58 45 --- 21 | 43 55 62 39 --- 42
R23 | 2571 14 18 65 27 --- 18 | 51 56 72 65 --- 50
R24 | 5450 57 31 36 30 1208 22 | 136 165 167 140 153 150
------+------------------------------------+--------------------------------
RMS | 5373 50 30 65 45 703 |T 47 60 83 53 65 49
WRMS | 5373 39 25 54 45 703 |NE 45 61 78 48 65 49
MEDI | 5450 31 24 58 41 128 |MD 43 56 72 39 23 42
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