[IGSREPORT-18094] Wk 1560 IGLOS Final Orbits
Jim Ray
IGS.ACC at noaa.gov
Thu Dec 17 14:47:22 PST 2009
******************************************************************************
IGS Electronic Report 17 Dec 14:47:45 PST 2009 Message Number 18094
******************************************************************************
Author: AC Coordinator / NOAA NGS
sum-file Version 2.0
IGLOS Orbit Combination - Week 1560 (Nov 29, 2009 - Dec 05, 2009)
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 2.1560.
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:
igl1560[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 1560 in the SP3 format.
igl15607.sum Combination Report for GPS Week 1560.
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 | 506.2 ns
1 | 504.0 ns
2 | 510.1 ns
3 | 520.5 ns
4 | 515.6 ns
5 | 436.4 ns
6 | 440.8 ns
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 1.1560, 1a.1560).
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 2.1560.0-6)
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 3.1560.0-6).
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 1560 summary. (Nov 29, 2009 - Dec 05, 2009)
Table 1.1560.a GPS week : 1560 MJD: 55164.0-55170.0
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 114| 0 -1 4 23 9 34 -.21 32 31 | 0 71 2509 2717
| 1 1 4 23 26 93 .05 | 0 964
esx 129| -1 0 -10 -7 -29 6 .38 33 28 | 116396 1195 4242 9291
| 3 4 8 28 14 81 .12 | 38934 3705
iac n/a| 1 0 3 -8 6 -50 -.16 24 24 | 490687 -634 4228 8362
| 1 2 7 18 20 91 .14 | 35477 1683
mcc n/a| -13 13 38 -310 68 -165 -.24 436 436 | --- --- --- ---
| 16 32 95 326 258 914 1.04 | --- ---
Table 1.1560.b GPS week : 1560 MJD: 55164.0-55170.0
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
------+------------------------------------+------------------------------------------
R02 | 12 15 12 16 16 14 12 |
R03 | 14 15 13 14 18 21 17 |
R07 | 30 28 23 19 17 20 26 |
R08 | 9 8 19 40 31 10 14 |
R10 | 17 29 13 18 10 12 13 |
R11 | 23 25 22 21 17 21 21 |
R13 | 26 28 15 19 15 13 15 |
R14 | 27 16 9 12 15 16 20 |
R15 | 28 19 14 18 20 17 12 |
R17 | 17 19 18 26 23 20 29 |
R18 | 24 21 15 14 12 13 11 |
R19 | 20 15 20 16 12 12 12 |
R20 | 20 24 24 36 24 17 22 |
R21 | 16 26 27 23 26 22 16 |
R23 | 39 39 15 26 37 48 34 |
Table 1.1560.c GPS week : 1560 MJD: 55164.0-55170.0
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 1560 0 | -149 78 78 2504 -567 -12400 90.1 2353 2353 | 506237 0
brd 1560 1 | -56 44 108 -2067 -123 -11150 91.1 2406 2406 | 504043 0
brd 1560 2 | 34 26 107 -1626 3509 -6798 87.4 2511 2511 | 510054 0
brd 1560 3 | 49 -105 140 2081 1872 -7960 86.3 2556 2556 | 520455 0
brd 1560 4 | 77 17 51 242 291 -12040 90.4 2620 2620 | 515551 0
brd 1560 5 | 50 -6 -15 90 68 -18400 87.1 2152 2152 | 436350 0
brd 1560 6 | -84 75 91 -84 -4759 -23780 89.1 2147 2147 | 440823 0
-------------+------------------------------------------------------------+----------------
brd 1560 mean| -11 18 80 162 41 -13218 88.8 2392 2392 | 490501 0
brd 1560 sdev| 85 62 50 1703 2545 5966 1.9 188 188 | 35912 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 2.1560.0 GPS week: 1560 Day: 0 MJD: 55164
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 114| 0 -1 0 18 -21 115 -.16 31 32 | 0 730 4262 4796
esx 129| -4 2 -24 -26 -36 -95 .51 43 37 | 135444 -1102 4382 9669
iac n/a| 0 -2 13 -4 13 -50 -.26 24 24 | 507271 -2098 4359 8908
mcc n/a| -9 21 -100 -707 465 502 -1.12 477 477 | --- --- --- ---
Table 2.1560.1 GPS week: 1560 Day: 1 MJD: 55165
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 114| 2 0 -1 24 -22 -85 -.25 37 34 | 0 -441 2227 2354
esx 129| -4 -6 -10 41 -26 -62 .46 37 31 | 135654 4615 4041 8229
iac n/a| 3 3 11 -39 41 72 -.12 23 23 | 503073 676 3986 8052
mcc n/a| -18 -18 -67 -204 -274 -1351 -.81 370 370 | --- --- --- ---
Table 2.1560.2 GPS week: 1560 Day: 2 MJD: 55166
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 114| -1 -1 5 -25 30 49 -.23 32 32 | 0 1458 2662 2781
esx 129| 0 0 -13 10 -35 32 .15 26 21 | 142614 -4301 4012 8256
iac n/a| 1 -1 8 0 7 -72 .13 18 18 | 512139 -2135 4015 7866
mcc n/a| -33 0 39 -671 170 1216 -1.74 387 387 | --- --- --- ---
Table 2.1560.3 GPS week: 1560 Day: 3 MJD: 55167
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 114| 0 -2 8 21 19 184 -.28 33 31 | 0 -985 2063 2249
esx 129| 0 0 2 -33 -45 32 .42 37 39 | 139762 126 4541 8998
iac n/a| 3 0 -7 13 -23 -219 -.15 25 25 | 518351 -309 4554 8208
mcc n/a| 1 -8 67 -249 -213 355 .75 70 70 | --- --- --- ---
Table 2.1560.4 GPS week: 1560 Day: 4 MJD: 55168
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 114| 2 0 9 45 44 15 -.17 34 31 | 0 -1004 2602 2869
esx 129| -4 -5 -7 -28 -41 0 .29 26 22 | 142186 6202 5257 11158
iac n/a| 3 4 -1 0 -9 5 -.21 28 28 | 515345 2176 5219 9525
mcc n/a| -20 77 182 -469 230 -1061 -.05 940 940 | --- --- --- ---
Table 2.1560.5 GPS week: 1560 Day: 5 MJD: 55169
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 114| 0 -1 7 35 23 18 -.20 29 30 | 0 -131 1901 1993
esx 129| 3 -1 -11 6 -13 -19 .42 28 24 | 58575 -696 3810 9288
iac n/a| 0 0 0 -27 5 -2 -.25 27 27 | 436867 -2322 3812 8485
mcc n/a| 12 -4 71 180 -19 -234 1.18 408 408 | --- --- --- ---
Table 2.1560.6 GPS week: 1560 Day: 6 MJD: 55170
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 114| 1 -3 2 42 -7 -54 -.17 27 28 | 0 876 1851 1980
esx 129| -2 6 -6 -24 -7 158 .43 30 24 | 60540 3527 3651 9442
iac n/a| 0 -2 0 0 11 -84 -.26 24 24 | 441764 -426 3652 7495
mcc n/a| -28 28 78 -48 122 -588 .12 398 398 | --- --- --- ---
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 3.1560.0 GPS week: 1560 Day: 0 MJD: 55164
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg esx iac mcc IGL | bkg esx iac mcc IGL
------+-------------------------------+---------------------------
R02 | 830 17 20 15 --- 12 | 26 36 35 --- 29
R03 | 912 21 25 14 --- 14 | 34 39 40 --- 34
R07E | 1598 29 66 31 --- 29 | 97 129 78 --- 91
R08 | 1584 12 16 11 129 9 | 40 46 50 158 43
R10E | 4544 26 31 15 --- 16 | 55 85 77 --- 69
R11E | 2882 33 48 13 567 22 | 46 63 63 188 54
R13E | 3477 44 32 34 --- 26 | 50 71 67 --- 58
R14E | 1541 17 61 32 --- 27 | 35 92 44 --- 44
R15E | 1307 22 62 33 588 28 | 45 93 54 495 52
R17 | 728 20 33 18 --- 16 | 38 72 55 --- 52
R18 | 3789 41 20 33 --- 24 | 36 55 80 --- 57
R19 | 3129 28 44 12 --- 19 | 42 79 56 --- 55
R20 | 1210 27 31 28 --- 20 | 53 66 71 --- 63
R21 | 1397 19 36 13 --- 16 | 62 87 80 --- 74
R23 | 1796 67 69 29 --- 38 | 44 84 43 --- 40
------+-------------------------------+---------------------------
RMS | 2353 31 43 24 477 |T 46 73 59 280 54
WRMS | 2353 32 37 24 477 |NE 45 73 64 --- 56
MEDI | 1584 26 33 18 567 |MD 44 72 56 188 54
Table 3.1560.1 GPS week: 1560 Day: 1 MJD: 55165
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg esx iac mcc IGL | bkg esx iac mcc IGL
------+-------------------------------+---------------------------
R02 | 1064 22 23 20 --- 15 | 30 30 35 --- 29
R03 | 934 26 21 17 --- 15 | 34 52 41 --- 40
R07E | 1243 37 56 21 --- 27 | 36 81 57 --- 46
R08 | 748 11 11 11 161 8 | 39 46 47 120 42
R10 | 3582 48 47 27 --- 28 | 20 74 53 --- 41
R11E | 3760 27 46 29 --- 24 | 43 92 56 --- 53
R13 | 3934 46 52 22 --- 28 | 53 101 61 --- 64
R14 | 1844 31 21 15 --- 16 | 24 46 41 --- 32
R15 | 800 37 25 17 498 19 | 30 56 66 283 50
R17 | 879 33 33 16 --- 19 | 43 74 62 --- 57
R18 | 2880 29 31 27 --- 20 | 35 63 66 --- 54
R19 | 2803 13 25 21 --- 14 | 35 51 69 --- 50
R20 | 4171 47 28 25 --- 24 | 39 64 43 --- 46
R21 | 993 31 55 19 --- 25 | 32 84 46 --- 48
R23 | 961 74 48 43 --- 39 | 52 62 43 --- 34
------+-------------------------------+---------------------------
RMS | 2406 37 37 23 370 |T 36 65 52 201 45
WRMS | 2406 34 31 23 370 |NE 39 66 54 --- 48
MEDI | 1243 31 31 21 161 |MD 35 63 53 120 46
Table 3.1560.2 GPS week: 1560 Day: 2 MJD: 55166
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg esx iac mcc IGL | bkg esx iac mcc IGL
------+-------------------------------+---------------------------
R02 | 1040 20 16 13 --- 11 | 31 46 40 --- 37
R03 | 1296 23 17 14 --- 12 | 39 42 49 --- 42
R07E | 1892 39 31 27 --- 22 | 67 87 57 --- 64
R08 | 846 38 17 24 220 19 | 70 71 78 224 70
R10 | 3427 17 22 14 --- 12 | 56 63 62 --- 59
R11 | 3634 41 32 19 101 21 | 32 73 51 177 50
R13 | 3956 27 19 17 --- 14 | 33 50 54 --- 44
R14 | 1456 11 11 13 --- 8 | 36 35 35 --- 33
R15 | 2464 20 21 19 625 14 | 36 41 51 383 41
R17 | 986 37 24 13 --- 17 | 41 75 82 --- 67
R18 | 2343 26 23 16 --- 15 | 44 79 64 --- 62
R19 | 2239 40 27 16 --- 19 | 31 84 64 --- 60
R20 | 4412 45 31 25 --- 23 | 32 56 45 --- 43
R21 | 2075 46 48 16 --- 26 | 36 102 55 --- 64
R23 | 1849 21 23 20 --- 15 | 33 53 31 --- 30
------+-------------------------------+---------------------------
RMS | 2510 32 26 18 387 |T 41 63 54 261 51
WRMS | 2510 32 21 18 387 |NE 36 74 56 --- 54
MEDI | 2075 27 23 16 220 |MD 36 63 54 224 50
Table 3.1560.3 GPS week: 1560 Day: 3 MJD: 55167
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg esx iac mcc IGL | bkg esx iac mcc IGL
------+-------------------------------+---------------------------
R02E | 1023 18 26 23 --- 16 | 30 39 31 --- 25
R03E | 2388 22 22 15 --- 14 | 29 43 40 --- 34
R07E | 2938 21 33 25 --- 19 | 46 56 40 --- 42
R08 | 1130 50 82 32 --- 40 | 54 160 76 --- 86
R10 | 4342 25 26 24 --- 18 | 32 51 54 --- 40
R11 | 3461 38 25 23 70 21 | 49 71 71 98 60
R13 | 3801 19 36 24 --- 19 | 41 61 53 --- 46
R14 | 1402 11 19 19 --- 12 | 35 35 40 --- 35
R15 | 1991 26 19 29 --- 18 | 32 55 50 --- 42
R17 | 1664 46 36 27 --- 26 | 59 68 73 --- 63
R18 | 2496 22 22 16 --- 14 | 36 33 58 --- 41
R19 | 2602 22 26 19 --- 16 | 35 62 69 --- 52
R20 | 2909 62 58 32 --- 36 | 40 90 62 --- 57
R21 | 1710 35 23 34 --- 22 | 44 60 87 --- 61
R23 | 1717 34 46 30 --- 26 | 30 58 43 --- 30
------+-------------------------------+---------------------------
RMS | 2556 33 37 25 70 |T 39 62 56 98 47
WRMS | 2556 31 39 25 70 |NE 40 61 65 --- 50
MEDI | 2388 25 26 24 70 |MD 36 58 54 98 42
Table 3.1560.4 GPS week: 1560 Day: 4 MJD: 55168
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg esx iac mcc IGL | bkg esx iac mcc IGL
------+-------------------------------+---------------------------
R02E | 1169 14 20 27 --- 15 | 35 52 38 --- 37
R03E | 2502 30 22 25 --- 18 | 44 67 41 --- 49
R07E | 2752 20 25 25 --- 17 | 40 42 36 --- 35
R08E | 1512 62 37 28 1316 30 | 60 121 105 761 95
R10 | 4320 16 13 14 --- 10 | 28 37 35 --- 31
R11 | 3920 23 24 23 192 16 | 24 46 42 130 34
R13 | 2915 25 20 17 --- 15 | 37 51 41 --- 38
R14 | 1285 27 15 19 --- 14 | 22 47 41 --- 35
R15 | 1689 29 19 35 --- 20 | 29 44 42 --- 35
R17 | 2326 38 19 38 --- 23 | 49 65 57 --- 55
R18 | 2988 23 14 12 --- 12 | 41 61 59 --- 53
R19 | 3080 19 12 18 --- 11 | 32 45 48 --- 39
R20 | 1930 41 35 24 --- 24 | 31 43 41 --- 34
R21 | 1373 33 34 40 --- 25 | 40 69 45 --- 49
R23 | 2998 58 50 48 --- 37 | 38 77 17 --- 41
------+-------------------------------+---------------------------
RMS | 2620 34 26 28 940 |T 36 57 45 445 44
WRMS | 2620 31 22 28 940 |NE 38 60 44 --- 45
MEDI | 2502 27 20 25 192 |MD 37 51 41 130 38
Table 3.1560.5 GPS week: 1560 Day: 5 MJD: 55169
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg esx iac mcc IGL | bkg esx iac mcc IGL
------+-------------------------------+---------------------------
R02E | 852 15 25 17 --- 14 | 30 46 31 --- 30
R03E | 2469 28 28 29 --- 20 | 30 55 36 --- 35
R07E | 2210 29 28 24 --- 19 | 39 49 43 --- 39
R08E | 1031 13 11 15 657 9 | 48 55 50 399 47
R10 | 3386 14 16 19 --- 12 | 32 31 41 --- 32
R11 | 2146 24 34 29 120 21 | 25 55 34 71 33
R13 | 2834 17 22 16 --- 13 | 36 49 36 --- 39
R14 | 1885 20 20 27 --- 16 | 23 35 38 --- 27
R15 | 887 26 15 27 234 16 | 20 35 34 240 25
R17 | 1452 33 24 27 --- 20 | 31 69 52 --- 48
R18 | 1970 19 23 9 --- 12 | 25 53 32 --- 35
R19 | 1002 18 19 14 --- 12 | 23 46 40 --- 34
R20 | 2296 29 18 21 --- 16 | 15 31 28 --- 21
R21 | 841 30 39 20 --- 21 | 30 43 42 --- 32
R23 | 3905 71 62 67 --- 47 | 25 81 54 --- 36
------+-------------------------------+---------------------------
RMS | 2152 29 28 27 408 |T 28 48 39 236 34
WRMS | 2152 30 24 27 408 |NE 24 53 41 --- 34
MEDI | 1970 24 23 21 234 |MD 30 49 38 240 34
Table 3.1560.6 GPS week: 1560 Day: 6 MJD: 55170
Weighted Average Orbit Dynamics (7 days)
PRN | brd bkg esx iac mcc IGL | bkg esx iac mcc IGL
------+-------------------------------+---------------------------
R02E | 1301 19 16 14 --- 11 | 42 50 35 --- 40
R03E | 1910 23 22 25 --- 17 | 39 58 43 --- 43
R07E | 2175 38 41 31 --- 26 | 53 56 52 --- 47
R08E | 962 20 16 21 656 13 | 75 89 84 324 81
R10 | 2485 15 19 18 --- 12 | 40 44 58 --- 47
R11 | 1240 31 39 16 151 21 | 34 66 49 47 44
R13 | 1919 20 25 20 --- 15 | 57 81 62 --- 64
R14 | 1258 18 41 23 --- 20 | 32 44 33 --- 31
R15 | 1942 15 16 19 147 12 | 33 31 39 148 31
R17 | 1690 45 44 31 --- 28 | 46 98 77 --- 68
R18 | 2902 15 19 10 --- 10 | 64 76 80 --- 72
R19 | 2235 17 17 15 --- 12 | 34 68 63 --- 54
R20 | 2750 41 17 29 --- 22 | 32 73 75 --- 58
R21 | 2261 26 21 16 --- 15 | 41 68 60 --- 54
R23 | 3528 36 58 45 --- 33 | 23 73 32 --- 26
------+-------------------------------+---------------------------
RMS | 2147 27 30 24 398 |T 43 65 56 173 50
WRMS | 2147 28 24 24 398 |NE 40 76 64 --- 55
MEDI | 1942 20 21 20 151 |MD 40 68 58 148 47
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