Chamran-1

Success Islamic Revolutionary Guard Corps Aerospace Force, Qaem 100

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Mission

Technology · LEO

Iranian technological demonstration satellite to test out a propulsion system, with mass of 60 kg.

What it put in orbit

ObjectTypeOrbit
QAEM 100 R/B 2024-165A Rocket body 466 × 572 km · 64.1° Globe
CHAMRAN-1 2024-165B Payload 487 × 574 km · 64.1° Globe
QAEM 100 DEB 2024-165C Debris re-entered 2024-12-07

COSPAR ID 2024-165 (data from GCAT, J. McDowell, CC BY 4.0). Orbits from the CelesTrak satellite catalogue (perigee × apogee, inclination).

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