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Launch Schedules

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   QuickBird 1 - Summary
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QuickBird 1 was planned for orbit a circular 590 km (319 nmi) orbit, inclined at 66 degrees. This inclination was to permit unique imaging times. QuickBird 1 was to collect both one-meter resolution digital black-and-white imagery and four-meter resolution digital color images. These high resolution images were to be taken by the QuickBird instrument, a high resolution camera, during orbital day-time. Digital images taken from orbit were expected to rival aerial photography in terms of both cost and possible economic and scientific applications. The 950 kg (2094 lbm) spacecraft was manufactured by Ball Aerospace and Technologies, Corp., Boulder, Colorado and was based on the Ball Commercial Platform 2000 (BCP 2000) satellite bus. 

QuickBird 1

SATELLITE

Int'l Designation 2000 074A

Launch Failure

Owner / Sponsor EarthWatch, Inc.
Mission Remote Sensing
Satellite Bus Ball Aerospace and Technologies, Corp.

BCP 2000

Launch Mass 950 kg (2094 lbm) 
Mission Orbit LEO / 590 km (319 nmi) circular

66°

Design Life  > 5 years
Power (EOL)  0.250 kW

LAUNCH

Launch Vehicle Model Kosmos 3M
Launch Date / Time 2000 Nov 20

23:00

Financial

Satellite cost  US$60 million
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