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Launch Information
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Date: Launched September 18, 2007
Launch Vehicle: Delta 7920 (9 strap-ons)
Launch Site: Vandenberg Air Force Base
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Orbit
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Altitude: 496 kilometers
Type: Sun synchronous, 10:30 am descending node
Period: 94.6 minutes |
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Mission Life
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7.25 years, including all consumables and degradables
(e.g. propellant) |
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Spacecraft Size, Mass & Power
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3.6 meters (12 feet) tall x 2.5 meters (8 feet) across,
7.1 meters (23 feet) across the deployed solar arrays
2500 kilograms (5500 pounds)
3.2 kW solar array, 100 Ahr battery |
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Sensor Bands
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Panchromatic |
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Sensor Resolution
(GSD = Ground Sample Distance)
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0.50 meters GSD at nadir
0.59 meters GSD at 25º off-nadir |
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Dynamic Range
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11-bits per pixel |
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Time Delay Integration (TDI)
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6 selectable levels from 8 to 64 |
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Swath Width
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17.6 kilometers at nadir |
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Attitude Determination and Control
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3-axis stabilized
Actuators: Control Moment Gyros (CMGs)
Sensors: Star trackers, solid state IRU, GPS |
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Pointing Accuracy & Knowledge
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Accuracy: <500 meters at image start and stop
Knowledge: Supports geolocation accuracy below |
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Retargeting Agility
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Acceleration: 2.5 deg/s/s
Rate: 4.5 deg/s
Time to slew 300 kilometers: 10.5 seconds |
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Onboard Storage
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2199 gigabits solid state with EDAC |
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Communications
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Image and Ancillary Data: 800 Mbps X-band
Housekeeping: 4, 16 or 32 kbps real-time,
524 kbps stored, X-band
Command: 2 or 64 kbps S-band |
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Max Viewing Angle /
Accessible Ground Swath
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Nominally +/-40º off-nadir = 775 km wide swath
Higher angles selectively available |
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Per Orbit Collection
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331 gigabits |
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Max Contiguous Area
Collected in a Single Pass
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60 x 110 km mono
30 x 110 km stereo |
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Revisit Frequency
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1.7 days at 1 meter GSD or less
4.6 days at 25º off-nadir or less (0.59 meter GSD) |
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Geolocation Accuracy
(CE 90)
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- Specifications of 6.5 m CE90 at nadir, with actual accuracy in the range of 4.0 - 5.5 m CE90 at nadir, excluding terrain and off-nadir effects
- With registration to GCPs in image: 2.0 m (6.6 ft)
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