EchoStar IV
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EchoStar IV is a
communications satellite A communications satellite is an artificial satellite that relays and amplifies radio telecommunication signals via a transponder; it creates a communication channel between a source transmitter and a receiver at different locations on Earth ...
operated by EchoStar. Launched in 1998 it was operated in geostationary orbit at a longitude of 77 degrees west for 12 years.


Satellite

The launch of EchoStar IV made use of a
Proton rocket Proton (Russian: Протон) (formal designation: UR-500) is an expendable launch system used for both commercial and Russian government space launches. The first Proton rocket was launched in 1965. Modern versions of the launch system are sti ...
flying from Site 81 at the Baikonur Cosmodrome,
Kazakhstan Kazakhstan, officially the Republic of Kazakhstan, is a transcontinental country located mainly in Central Asia and partly in Eastern Europe. It borders Russia to the north and west, China to the east, Kyrgyzstan to the southeast, Uzbeki ...
. The launch took place at 23:45 UTC on May 7, 1998, with the spacecraft entering a
geosynchronous transfer orbit A geosynchronous transfer orbit or geostationary transfer orbit (GTO) is a type of geocentric orbit. Satellites that are destined for geosynchronous (GSO) or geostationary orbit (GEO) are (almost) always put into a GTO as an intermediate step f ...
. EchoStar IV carried 32 Ku band
transponder In telecommunications, a transponder is a device that, upon receiving a signal, emits a different signal in response. The term is a blend of ''transmitter'' and ''responder''. In air navigation or radio frequency identification, a flight trans ...
s to provide direct voice and video
communication Communication (from la, communicare, meaning "to share" or "to be in relation with") is usually defined as the transmission of information. The term may also refer to the message communicated through such transmissions or the field of inqui ...
s to small dishes in North America after parking over 119° W or 148° W longitude.


Specifications

* Launch mass: *
Power Power most often refers to: * Power (physics), meaning "rate of doing work" ** Engine power, the power put out by an engine ** Electric power * Power (social and political), the ability to influence people or events ** Abusive power Power may a ...
: 2 deployable
solar array A photovoltaic system, also PV system or solar power system, is an electric power system designed to supply usable solar power by means of photovoltaics. It consists of an arrangement of several components, including solar panels to absorb and ...
s, batteries * Stabilization: 3-axis *
Propulsion Propulsion is the generation of force by any combination of pushing or pulling to modify the translational motion of an object, which is typically a rigid body (or an articulated rigid body) but may also concern a fluid. The term is derived f ...
: LEROS-1C * Longitude: 77° west


See also

*
1998 in spaceflight This article outlines notable events occurring in 1998 in spaceflight, including major launches and EVAs. Launches , colspan=8, January , - , colspan=8, February , - , colspan=8, March , - ...


References

Spacecraft launched in 1998 Communications satellites in geostationary orbit Satellites using the A2100 bus Spacecraft launched by Proton rockets Derelict satellites orbiting Earth E04 {{US-spacecraft-stub