Iridium's specifications

Prime contractor	Lockheed Martin
Platform	Iridium (LM700 bus)
Mass at launch	690 kg
Mass in orbit
Dry mass	556 kg
Dimension	1 x 2 m
Solar array	5 m span
Stabilization	3-axis
DC power	EOL: 1400 W
Design lifetime	5 years

This document is part of The Satellite Encyclopedia, © Tag's Broadcasting Services, all rights reserved, NO REPRODUCTION ALLOWED. Please notify any errors, omissions, etc.
V0.146 - Converted on Sun, 08 Sep 2024 16:27:17 GMT - Updated quarterly

© TBS Internet, all rights reserved. All reproduction, copy or mirroring prohibited. Legal notice