XSS 10

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General

Designation	27664 / 03005B
Launch date	29 Jan 2003
Country of origin	United States
Mission	Technology
Perigee/Apogee	518/805 km
Inclination	39.7°
Period	98 min
Launch vehicle	Delta 2 #295

For the US Air Force Research Lab.
Conducted autonomous navigation test and inspect (visually) the Delta 2 second stage.

XSS 10 travelled within 100 meters of the second-stage booster of the Delta II rocket, to take photographs and transmit the images back to earth.

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External resources

sat-index articles

Technical data

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Specifications

Prime contractor
Platform
Mass at launch	28 kg
Mass in orbit
Dimension
Solar array
Stabilization
DC power	battery only
Design lifetime	24 hours

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