• Ikonos-2 of DigitalGlobe is operating nominally in 2014 in its 15 Orbit: Sun-synchronous near-polar circular orbit, altitude = 681-709 km, inclination = 98.1º, period = 98 min, repeat cycle = 14 days (max), revisit cycle = 1-3 days (for observations at 40º latitude or higher). • The CU provides the cabling between the various electronic boxes. For example, the Ikonos satellite images, available since 2000, have an improved resolution of 1 m that afford mapping of a lot of ground objects from the satellite images. To access this item, please sign in to your personal account. You currently do not have any folders to save your paper to! • In 2000, Space Imaging was awarded one of the most coveted prizes for technological achievement in the space industry - “The Industry Innovation Award in the Technology Category” - from the Society of Space Professionals International, due to the excellent performance of Ikonos-2. * Technical briefing IKONOS. SPIE 4881, Sensors, Systems, and Next-Generation Satellites VI, (8 April 2003); EDAF is located at DLR, Oberpfaffenhofen and is jointly operated by EUSI and DLR. SNR (80% scene reflectance, 20% background reflectance, 2.66 mW/cm The data acquisitions of PAN and MS imagery data are simultaneous and fully co-registered; mono or stereo. This provides excellent observation capabilities. Mass = 8 kg, power 75 W. There is full redundancy. The data is a composite of the blue, green and red bands of the original dataset. The initial values of the interlock angles and the FAM parameters were determined by pre-launch measurements. Satellite Imagery Requisition. The attitude is measured by two star trackers and a sun sensor and controlled by four reaction wheels (actuators); location knowledge is provided by a GPS receiver.

Translations are not retained in our system. OTU has a mass of 45 kg, the power consumption is 15 W. As of July 1999, Kodak/C&GS (Commercial & Government Systems) is offering a “Model 1000™ camera system” of OSA camera heritage as an off-the-shelf product - at a 30% discount, deliverable within 24 months of order placement. The design life is 7 years; S/C body size=1.83 m x 1.57 m (hexagonal configuration); S/C mass = 817 kg; power = 1.5 kW provided by 3 solar panels. Ikonos-2 . • On Sept. 24, 2009, the Ikonos-2 spacecraft marked 10 years in orbit. Timing and command signals are received from the DPU, power is received from the PSU. DPU accepts S/C commands over a standard 1553 bus and routes the information to the FPU and PSU. Both are based at DLR Oberpfaffenhofen. Standard products are: - Ikonos-2 focus assessment: A yearly focus assessment is performed by imaging the same target multiple times while moving the focus mirror from an out-of-focus position through its ideal focus. 0.09 (camera geometric mean of in- and cross-track)

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