gptkbp:instance_of
|
gptkb:satellite
|
gptkbp:communication
|
C-band and Ku-band
used for telecommunications
|
gptkbp:controls
|
reaction wheels
|
gptkbp:cooling_system
|
passive thermal control
|
gptkbp:data_usage
|
up to 155 Mbps
|
gptkbp:debut
|
gptkb:1994
gptkb:2000
|
gptkbp:decommissioned
|
various dates
|
gptkbp:design
|
15 years
|
gptkbp:development
|
gptkb:1980s
|
gptkbp:first_flight
|
gptkb:1994
|
gptkbp:frequency
|
C-band, Ku-band, Ka-band
|
gptkbp:has_units
|
over 30
|
gptkbp:home_ground
|
Boeing ground control systems
|
https://www.w3.org/2000/01/rdf-schema#label
|
Boeing 601 satellite platform
|
gptkbp:launch_date
|
gptkb:1994
|
gptkbp:launch_platform
|
gptkb:United_Launch_Alliance
|
gptkbp:launch_price
|
approximately $100 million
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
gptkbp:launch_vehicle
|
gptkb:Atlas_II
|
gptkbp:manufacturer
|
gptkb:Boeing
|
gptkbp:mission_type
|
gptkb:Telecommunications
|
gptkbp:notable_features
|
modular design
|
gptkbp:notable_users
|
gptkb:Intelsat
|
gptkbp:orbit_type
|
gptkb:geostationary_orbit
gptkb:Boeing_601_spacecraft_bus
gptkb:Boeing_601_bus
modular design
2,500 kg
high power output
multiple launches
commercial satellite
varied by satellite
standard configuration
Boeing 601 legacy
broadcasting, internet, data services
part of Boeing's satellite history.
|
gptkbp:orbital_inclination
|
0 degrees
|
gptkbp:orbital_period
|
24 hours
|
gptkbp:payload_capacity
|
up to 20 transponders
up to 10 k W
|
gptkbp:powers
|
up to 10 k W
|
gptkbp:propulsion
|
chemical propulsion system
|
gptkbp:ram
|
20 transponders
|
gptkbp:related_to
|
gptkb:Boeing_702_SP
|
gptkbp:satellite_development
|
gptkb:Boeing_Space_and_Launch
|
gptkbp:services_provided
|
gptkb:Boeing
|
gptkbp:status
|
retired
|
gptkbp:successor
|
gptkb:Boeing_702
|
gptkbp:transponders
|
solid-state transponders
|
gptkbp:type
|
geostationary satellite
|
gptkbp:user_countries
|
gptkb:various_countries
|
gptkbp:weight
|
approximately 2,500 kg
|
gptkbp:bfsParent
|
gptkb:Boeing_702_satellite_platform
|
gptkbp:bfsLayer
|
5
|