Photo: Jeff Caplan, Langley Research Centre, NASA · Public domain (US government)

ST-5 FWD

Success Orbital Sciences Corporation, Pegasus XL

Mission

Test Flight · LEO

NASA's three micro-sats were launched to test and validate new technologies for future science missions. ST5's objective was to demonstrate and flight qualify several innovative technologies and concepts for application to future space missions.

What it put in orbit

ObjectTypeOrbitGlobe
ST5-A 2006-008A Payload 298 × 2850 km · 105.5° Globe
ST5-B 2006-008B Payload re-entered 2025-07-20
ST5-C 2006-008C Payload 254 × 1253 km · 105.5° Globe
PEGASUS R/B 2006-008D Rocket body 292 × 2686 km · 105.5° Globe
PEGASUS DEB 2006-008E Debris re-entered 2009-06-26

COSPAR ID 2006-008 (data from GCAT, J. McDowell, CC BY 4.0). Orbits from the CelesTrak satellite catalogue (perigee × apogee, inclination).

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