The Tempo 1 and 2 satellites can transmit more than 200 channels of high-fidelity broadcast programming to cable companies and home dishes. Tempo has twice the power and capacity of comparable satellites. It features 32 high-powered Ku-band transponders at 115 Watts, switchable to 16 transpondersders at 220 Watts. Total on-board transmitter power totals 3500 Watts.
Geostationary OrbitThe Mozhayets 2 (Zeya, RS 16) satellite was a Russian Military experimental communications satellite launched on 4 March 1997. Zeya was named after the Zeya River, which is very close to its launch site, Cosmodrome Svobodniy. A Start-1.2 rocket transported it into orbit. This was the first satellite launched from this new Russian launch site in far eastern Russia.
Low Earth OrbitThe Intelsat VIII-VIII/A series has been designed to meet the needs of Intelsat users throughout the system for improved C-band coverage and service. These spacecraft will incorporate six-fold C-band frequency reuse, two-fold frequency reuse of expanded C-band capacity, and the highest C-band power level ever for an Intelsat satellite. Consequently, Intelsat VIII will provide significantly more C-band capacity for public switched telephony and Intelsat Business Service, better quality for video services, and encourage new international VSAT applications.
Geostationary OrbitGonets- satellite were the civilian derivate of the military Strela-3 satellite system. The Gonets system was offered to support international health organizations to meet their global communications needs for the transfer of medical data and records to remote sites. Strela-3 was second generation of strategic store-dump military communications satellite. Development of this generation to replace the first generation Strela-1M and Strela-2M satellites began in 1973.
Low Earth OrbitHALCA (Highly Advanced Laboratory for Communication and Astronomy), a.k.a. VSOP (Very Large Baseline Interferometry Space Observatory Programme) or Muses-B, is the first astronomical satellite dedicated to Very-Long Baseline Interferometry (VLBI). It was launched on its maiden flight by ISAS's M-5 [KM-V1] launch vehicle from Kagoshima Space Center on 12 February 1997.
Elliptical Orbit