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OrbView-2 (renamed from SeaStar in 1997)
OrbView-2 is an imaging satellite,
developed, owned, managed and operated by Orbital Imaging Corporation
(OrbImage) of Dulles, VA. The overall objective of the
OrbView-2/SeaWiFS mission is to
provide quantitative data on global ocean bio-optical properties to the
Earth science community. The
OrbView-2 satellite includes the SeaWiFS (Sea-Viewing Wide
Field-of-View Sensor) imaging system, an 8-band multispectral imaging
instrument with a one kilometer spatial resolution.
Spacecraft:
The spacecraft design is based on
PegaStar, a multi-purpose bus of OSC. The platform combines functions
common to both satellites and launch vehicles, including guidance and
control, power, communications, and data systems. The S/C is three-axis
stabilized (0.5º with 0.08º knowledge) using three
orthogonal magnetic torque rods for roll and yaw control and two
momentum wheels for pitch stabilization. Attitude is sensed with three
2-axis sun sensors, two scanning horizon sensors, and two 2-axis
magnetometers. Redundant GPS receivers are used for orbit
determination. The propulsion system
consists of two subsystems, a reaction control system and a hydrazine
propulsion system. Nominal design life = 5 years. S/C mass = 390 kg. A
hydrazine propulsion system using four thrusters is used for
orbit raising and orbit maintenance. Four deployed solar panels with
zenith-facing cells and two
body-mounted side-facing solar panels produce 165 W orbit-average power
after 5 years. 1) 2) 3) 4) 5)
Figure 1: Illustration of the OrbView-2 spacecraft
The OrbView-2 satellite operations
as well as the commercial data processing and distribution functions
are performed by ORBIMAGE. The processing and distribution of data for
research applications
is handled by the SeaWiFS Project at NASA/GSFC; the SeaWiFS mission is
part of NASA's ESE (Earth
Science Enterprise) program.
Application: Ocean-color data, ocean biology and ecology, phytoplankton concentrations and
growth, pollution, algae blooms, etc. The data may help scientists to understand the role of ocean plant
life in the Earth's carbon cycle.
Orbit: Sun-synchronous polar circular orbit, altitude = 705 km, inclination =98.2º, equator crossing
time at local noon (12:00 hours on descending node), successive orbit equatorial crossing longitude =
-24.721º, period = 98.2 minutes, orbital repeat time = 16 days (233 orbits).
Launch: The OrbView-2 S/C was air-launched on August 1, 1997 by a Pegasus XL rocket (also of
OSC) from Vandenberg AFB, CA.
RF communications: On-board
storage of sensor data is provided. With two dumps/day, this allows
global observations at reduced spatial resolution to be recorded, and a
limited amount (about 20 min/day) of high-resolution Local Area
Coverage (LAC) data. The real-time LAC data stream is merged
with S/C health and instrument telemetry at a rate of 665.4 kbit/s;
this is transmitted at L-band with a
frequency of 1702.56 MHz.
To increase the coverage of LAC data, NASA encourages the operation of HRPT (High Resolution
Picture Transmission) stations by the user community throughout the world. These HRPT stations can
collect real time LAC data via direct broadcast whenever the spacecraft is in view. The other telemetry
stream consists of stored GAC and selected LAC data, along with S/C health and instrument telemetry,
at 2.0 Mbit/s; this is transmitted at S-band with a frequency of 2275.5 MHz. 6)
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Satellite transmitting power
HRPT L-band frequency
Frequency stability
Modulation
Modulation rate
Satellite transmitter antenna loss
Satellite antenna gain
EIRP
Slant range
Free space loss
Fading and rain margin
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5 Watt
1702.56 MHz
± 20 ppm
Split-Phase
0.6654 Mbit/s
2.0 dB
1.8 - 2.1 dBiC
31 - 37 dBm
2900 km
166.1 dB
5 dB
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Table 1: Requirements for a SeaWiFS LAC downlink ground station HRPT
Figure 2: Artist's rendition of the deployed OrbView-2 spacecraft (image credit: NASA)
Mission status: The OrbView-2 spacecraft and its payload are operational as of 2007 (completing its
10th year on orbit in August 2007).
• OrbView-2 continues to perform exceedingly well on orbit, exceeding its design life by far. The
contract with NASA has been extended to provide further coverage to the worldwide data user community.
• In Dec. 2002, NASA extended the original 5-year contract with OrbImage for continued service
provision.
Sensor complement:
SeaWiFS (Sea-Viewing Wide
Field-of-View Sensor) built by Raytheon SBRC of Goleta, CA. Objective:
measurement of reflected visible sunlight from the ocean surface for
the derivation of ocean-color data. The SeaWiFS sensor may be regarded
as a next generation instrument of CZCS (Nimbus-7
sensor which ceased operations in 1986, after an eight-year mission).
The SeaWiFS instrument employs scanning mechanisms to drive an off-axis
(afocal) folded-optics scanning telescope and a rotating half-angle
mirror that is phase-synchronized with, and rotating at half the speed
of, the folded
telescope. The scanning telescope design minimizes the polarization
sensitivity and, correspondingly,
maximizes the radiometric fidelity of its ocean color measurements.
The SeaWiFS scanning concept employs
a 360º uni-directional cross-track rotating telescope scanner. A
small counter-rotating flat scan mirror between the telescope and the
focal planes eliminates
image rotation which would otherwise occur as the telescope rotates.
The absence of FOV rotation permits the use of a multichannel, time
delay integration (TDI) processing in each of the eight spectral
bands to achieve the required SNR. Incoming scene radiation is
collected by the folded telescope and
reflected onto the rotating half-angle mirror. The collected radiation
is then relayed through dichroic
beam splitters to separate the radiation into four wavelength intervals
(each wavelength encompassing
two of the eight SeaWiFS spectral bands). The radiation in the four
separate wavelength intervals is
directed by four corresponding aft-optics assemblies through two
separate spectral bandpass filters
that further separate the radiation into the eight required SeaWiFS
spectral bands. The aft-optics also
image each of the resultant bands of radiation onto four silicon
detectors that are aligned in the scan
direction. The detected signals are then amplified for TDI processing
in the electronics module. 7) 8)
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Nr. of imaging bands
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8
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Spectral ranges (nm)
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402-422, 433-453, 480-500, 545-565, 660-680, 745-785,
845-885
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Spatial resolution
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1 km
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Swath width
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2800 km (continuous imaging)
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Radiometric accuracy
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< 5% absolute each band
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Calibration/stability monitor
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solar diffuser, lunar view
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Relative precision
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< 1% linearity of signal output to radiance
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Between-band precision
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< 5% relative band/band over 50 - 90% of saturation
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Polarization sensitivity
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< 2% worst case, all scan and tilt angles
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Dynamic range
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15,000:1 using bilinear gain
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Bright target recovery
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< 10 samples
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Location knowledge
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0.5 km, at 1-sigma level for instrument
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Revisit time
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1 day
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Maximum data rate
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2 Mbit/s
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Instrument mass, design life
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45 kg, 5 years
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Table 2: Parameters of the multispectral imager SeaWiFS
The off-axis telescope (with an
aperture of 7.6 cm; f/2) rotates at six revolutions per second (or 360
rpm) in the cross-track direction (for HRPT format compatibility) to
provide contiguous scan coverage. Data quantization = 10 bit; spatial
resolution = 1.6 mrad (1.13 km at nadir); an active scan angle of
±58.3º is used. A scanner tilt mechanism enables the entire
sensor to be oriented in the along-track
direction to )20º, 0º, or -20º to avoid specular sun
reflection (sun glint from the sea surface).
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Band
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Wavelength
(nm)
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Measurement Parameter
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Saturation
Radiance
(mW/cm2)
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Input Radiance
(mW/cm2)
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SNR (Measured
at Input
Radiance)
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1
2
3
4
5
6
7
8
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402 - 422
433 - 453
480 - 500
500 - 520
545 - 565
660 - 680
745 - 785
845 - 885
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Gelbstoffe
Chlorophyll absorption
Pigment concentration
Chlorophyll absorption
Sediments/hinge point
Atmospheric aerosols
Atmospheric aerosols
Atmospheric aerosols
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13.63
13.25
10.50
9.08
7.44
4.20
3.00
2.13
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9.10
8.41
6.56
5.64
4.57
2.46
1.61
1.09
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499
674
667
640
596
442
455
467
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Table 3: SeaWiFS spectral performance summary
Instrument calibration: SeaWiFS uses
short-period solar calibration (for a few orbits) and long-term
lunar calibration (for a few months and longer). Solar calibration
employs a solar radiation diffuser and
an input port located in a fixed position outside of the 58.3º
SeaWIFS scene-scan interval. Lunar calibration is accomplished by a S/C
maneuver to view the moon during the nighttime portion of an orbit.
Of particular importance to the postlaunch validation period are field
measurements from MOBY
(Marine Optical Buoy, located off the coast of Lanai, Hawaii. 9) 10) 11) 12)
Figure 3: Schematic illustration of the SeaWiFS sensor (image credit: NASA)
To protect the commercial interests of the builder and operator of the mission, ORBIMAGE, SeaWiFS
real time LAC data are encrypted. All data users require a license from OSC (a decryptor is furnished
with the license). Commercial data users pay a fee for their license, research licences are issued at no
cost, but are subject to certain restrictions. Commercial stations requesting HRPT stations for research
data use must obtain prior approval from NASA (SeaWiFS Project Office at GSFC).
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Sensor Parameter
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GAC Mode
(Global Area Coverage)
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LAC Mode
(Local Area Coverage)
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Scan width (degree)
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45º
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58.3º
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IFOV at sensor (mrad)
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1.5835
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1.5835
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Ground IFOV at nadir (km) - spatial resolution
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4.5
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1.13
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Ground swath width, km
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1500
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2800
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Pixels along-scan
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248
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1285
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Pixel numbers
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(147 - 1135, by 4)
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(1-1285)
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Scans/second
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1.5
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6
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Scan plane tilt
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20º
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20º
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Table 4: SeaWiFS sensor/transmission characteristics
Figure 4: Illustration of the SeaWiFS instrument (image credit: NASA)
1) "Orbital Sciences Captures $120 Million in Business, Pegasus Launches Ocean Satellite Ordered," Space News, March 11-17,
1991, p. 7
2) "OSC Reviews Seastar Design," Space News, Oct. 28 - Nov. 3, 1991, p. 22
3) P. R. Leygraaf, "OrbView-2 (SeaStar) Flight Operations and Data Delivery," Proceedings of the 11th AIAA/USU Conference
on Small Satellites, Sept. 15-18, 1997, Logan, UT
4) http://oceancolor.gsfc.nasa.gov/SeaWiFS/BACKGROUND/
5) http://www.orbimage.com/corp/orbimage_system/ov2/index.html
6) "Roles and Responsibilities of HRPT Stations for SeaWiFS," SeaWiFS Project Office, GSFC, Dec. 19, 1991
7) "System Concept for Wide-Field-Of View Observations of Ocean Phenomena from Space," NASA-NOAA-Eosat publication, 1987
8) H. v.d. Piepen, V. Amman, R. Doerffer, "Remote Sensing of Substances in Water," GeoJournal 24.1, pp. 24-27, 1991 (May) by
Kluwer Academic Publishers
9) G. Valenti, "Sea-viewing Wide Field-of-view Sensor," The Earth Observer, March/April 1998, Vol 10, pp. 20-22
10) Note: the reflected radiance is related to the concentration of chlorophyll and other plant pigments present, since chlorophyll
is a green pigment and the color of the water changes from blue to green as the concentration of chlorophyll increases. If the
concentration of chlorophyll is known, the amount of phytoplankton, or `ocean color,' may be calculated.
11) SeaWiFS Project Home Page at http://seawifs.gsfc.nasa.gov/SEAWIFS.html
12) http://oceancolor.gsfc.nasa.gov/SeaWiFS/SEASTAR/SPACECRAFT.html
This description was provided by Herbert J. Kramer from his documentation of: "Observation of the Earth and Its Environment: Survey of Missions and Sensors" - comments and corrections to this
article are welcomed by the author.
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