SOYUZ-TM 26, also known as Soyuz TM-26, is a crewed spacecraft with the OBJECT_ID 1997-038A and NORAD_CAT_ID 24886. It was manufactured by RKKE and launched on August 5, 1997, from the TYMSC site using a Soyuz-U launch vehicle from LC1 pad. The satellite has dimensions of 7.2 meters in length, 2.2 meters in diameter, and a span of 10.6 meters. It weighs 2850 kilograms both at launch and dry mass. Its shape is described as Sphere + Cone + Cyl + 2 Pan. The spacecraft is powered by two deployable fixed solar arrays and batteries and was launched for the purpose of being a crewed spacecraft, carrying Soyuz 7K-STM No. 75 payload. The satellite's motor type is KTDU-80 (S5.80).