home
***
CD-ROM
|
disk
|
FTP
|
other
***
search
/
Multimedia Plus
/
Multimedia Plus with ClearVue Version 10-94 (Knowledge Media Inc.).ISO
/
media
/
images
/
jpg
/
weather
/
93061219.txt
< prev
Wrap
Text File
|
1993-06-13
|
6KB
|
145 lines
Scan mode = 0
Scan Status = 51
Frame Flag = -1
Picture Flag = -1
Picture Flag Set Line Number = 266
Picture Flag Reset Line Number = 2556
Scan Count = 268
West Horizon point = -1
East Horizon point = -1
SYNC Lock = 0
Bit Error Count = 0
Year = 1993
Month = 6
Day = 12
Hour = 18
Minute = 32
Second = 52
Second/100 = 70
Calibration Table ID = 6374
MANAM Revision No = 462
Data Source = -1
Earth Radius(m): Equatorial Radius of Earth = 6377397
Satellite Elevation(m) = 35792045
Stepping Angle For IR Sensor (nrad) = 140000
Sampling Angle For IR Sensor (nrad) = 140000
Latitude of Sub-satellite point(mDEG) = 230
Longitude of Sub-satellite point(mDEG) = 140013
Line Number of SSP = 1411
Pixel Number of SSP = 1161
Ratio of Circumference = 3.141592
Sensor Deference for Line Number (X) = 0.000000
Sensor Deference for Pixel Number(Y) = 0.000000
Time of First Attitude Prediction Data(MJD) = 49150.767361
Time of Last Attitude Prediction Data(MJD) = 49150.798611
Interval Time of Attitude Prediction(MJD) = 0.003472
Number of Attitude Prediction Data = 10
Time of First Orbit Prediction Data(MJD) = 49150.770833
Time of Last Orbit Prediction Data(MJD) = 49150.795139
Interval Time of Orbit Prediction(MJD) = 0.003472
Number of Orbit Prediction Data = 8
Observation start time = 49150.771528
VIS Stepping angle along line = 0.000035
IR Stepping angle along line = 0.000140
VIS Channel Sampling Angle = 0.000035
IR Channel Sampling Angle = 0.000140
VIS Centre Line No = 5534.500000
IR Centre Line No = 1384.000000
VIS Centre Pixel No = 4582.500000
IR Centre Pixel No = 1146.000000
No of VIS sensors = 4
No of IR sensors = 1
VIS total Line Number = 11024
IR total Line Number = 2756
VIS total Pixel Number = 9164
IR total Pixel Number = 2291
Misalignment angle along X axis = -0.000788
Misalignment angle along Y axis = -0.001007
Misalignment angle along Z axis = 0.002644
Misalignment Matrix element 11 = 0.999996
Misalignment Matrix element 21 = -0.002644
Misalignment Matrix element 31 = -0.001007
Misalignment Matrix element 12 = 0.002644
Misalignment Matrix element 22 = 0.999996
Misalignment Matrix element 32 = 0.000788
Misalignment Matrix element 13 = 0.001005
Misalignment Matrix element 23 = -0.000791
Misalignment Matrix element 33 = 0.999999
Ratio of circumference/180 = 0.017453
180/Ratio of circumference = 57.295776
Oblateness of Earth = 0.003343
Eccentricity of Earth = 0.081697
Angle Between VISSR and the view
direction of Sun Sensor = -0.626722
Epoch Time of Orbital Parameters = 49151.000000
Semi Major Axis (KM) = 42165.733612
Eccentricity (Orbit) = 0.000173
Orbital Inclination = 0.038882
Longitude of Ascending Node (deg) = 248.954007
Argument of Perigee (deg) = 203.138394
Mean Anomaly (deg) = 308.679580
Sub satellite East Longitude (deg) = 1.400098
Sub satellite North Longitude (deg) = 0.002018
Epoch Time of Attitude Parameters = 49151.000000
Angle between Z-Axis and Satellite
Spin Axis Projected = 3.140208
Change rate of Alpha (rad/sec) = -0.000000
Angle Between Satellite Spin Axis and yz-plane
in inertial coordinate system 'delta' (rad) = -0.003749
Change rate of Delta (rad/sec) = 0.000000
Daily Mean of Satellite Spin Rate (rpm) = 99.910077
Prediction Time( UTC represented in MJD ) = 49150.767361
Anno Domino represented by BCD = 930612182500
Change rate of Alpha (rad/sec) = 3.140212
Angle Between Satellite Spin Axis and yz-plane
in inertial coordinate system 'delta' (rad) = -0.003773
Dihedral Angle Between the Sun and the Earth
measured from the north (rad) = 5.301350
Spin Rate:Spin speed of the Satellite (rpm) = 99.910077
Right Ascension on the Satellite Orbit Plane
Coordinate System at the Attitude Epoch (rad) = 1.786696
Declination and otherwise same as above = -1.566246
X component of Satellite Position in the 1950.0
Mean Coordinate System = 31356295.643567
Y component of Satellite Position in the 1950.0
Mean Coordinate System = -28198134.018803
Z component of Satellite Position in the 1950.0
Mean Coordinate System = 26932.552447
X component of Satellite Position in the 1950.0
Mean Coordinate System = 2055.392385
Y component of Satellite Position in the 1950.0
Mean Coordinate System = 2286.130534
Z component of Satellite Position in the 1950.0
Mean Coordinate System = 0.736324
X component of Satellite Position in the Earth-fixed
Coordinate System = -32310889.301360
Y component of Satellite Position in the Earth-fixed
Coordinate System = 27098582.344777
Z component of Satellite Position in the Earth-fixed
Coordinate System = 161342.653830
X component of Satellite Position in the Earth-fixed
Coordinate System = 0.855955
Y component of Satellite Position in the Earth-fixed
Coordinate System = 0.407294
Z component of Satellite Position in the Earth-fixed
Coordinate System = 9.393081
Greenwich sidereal time in True of Date System = 178.581714
Sun Direction: Right Ascension from the Satellite
to the sun in the 1950.0 Mean Coordinate System(deg) = 80.411581
Declination and otherwise same as above = 23.143075
Right Ascension from the Satellite to the Sun
in the Earth fixed Coordinate System (deg) = 262.493365
Declination and otherwise same as above = 23.181336
Element11 of Nutation and Precession Matrix = 0.999943
Element21 of Nutation and Precession Matrix = 0.009783
Element31 of Nutation and Precession Matrix = 0.004252
Element12 of Nutation and Precession Matrix = -0.009783
Element22 of Nutation and Precession Matrix = 0.999952
Element32 of Nutation and Precession Matrix = -0.000037
Element13 of Nutation and Precession Matrix = -0.004253
Element23 of Nutation and Precession Matrix = -0.000005
Element33 of Nutation and Precession Matrix = 0.999991
Sub-satellite Point: North Latitude(deg) = 0.219434
Sub-satellite Point: East Latitude(deg) = 140.014023
Height of Satellite above Earth's surface(m) = 35792382.394904