The GeoEye company (from 29 January 2013 – DigitalGlobe) was the main developer of the satellite, alongside with General Dynamics (satellite platform), IBM (processor), MDA (ground segment), Kodak and ITT Industries (optics, camera).
Spacecraft design and mission details
Name satellite;GeoEye-1
Country;USA
Developer;General Dynamics, ITT, IBM, Kodak, MDA
Operator;DigitalGlobe
Launch vehicle;Delta II 7420-10
Launch date;September 6, 2008
Date of deactivation;—
Orbit: Type<br>Altitude, km<br>Inclination, deg.;Sun-synchronous<br>684<br>98,0
Mission duration, years;10
Revisit frequency, days;1-3
Power, W;3862
Spacecraft dimensions, m;4,4×2,7
Mass, kg;1955
Swath widths and representative area sizes;Standard swath width at nadir: 15,2 km<br>Coverage of one image: 225 km2 (15×15 km)<br>Maximum coverage: 15,000 km2 (300×15 km)<br>Square area 1°×1°: 10,000 km2 (100×100 km)<br>In stereo mode: 6,270 km2 (224×28 km)
Daily acquisition capacity;Total amount of shots in the PAN mode: 2400<br>Coverage in PAN mode: 700,000 km2<br>Coverage in MS mode: 350,000 km2
Datum;WGS84, NAD83…
Projection;UTM
Spectral bands;Panchromatic, Multispectral (8 bands), Bundle (PAN+8-bands MS)
Minimum order size;49 km2 – for archive data<br>100 km2 – for new tasking
Delivery formats;TIFF, GeoTIFF 1.0, NITF 2.1 or NITF 2.0, UTM
Delivery method;CD, DVD, FTP, Hard Drive