IRIDIUM 41 is a communication satellite launched on November 9, 1997, from AFWTR Launch Site SLC2W using a Delta 7920-10C launch vehicle. It has the OBJECT_ID of 1997-069B and a NORAD_CAT_ID of 25040. The satellite measures 3.5 meters in length, with a diameter of 1 meter and a span of 5 meters. Its configuration is LM-700A, based on the LM700 bus, manufactured by MOTO/LMMS for the US owner IRID. It has a dry mass of 556 kg and a launch mass of 662 kg, powered by two deployable solar arrays and batteries. The satellite's mission is communication, with a payload designated Iridium SV041. Its shape is described as Box + 2 Pan, with an RCS value of 3.6007. The expected lifetime of IRIDIUM 41 is 8 years.