|
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
|
| Web Links |
|
|