|
gptkbp:instance_of
|
gptkb:satellite
|
|
gptkbp:antenna_diameter
|
5.4 m
|
|
gptkbp:bus_connections
|
gptkb:Boeing_702
|
|
gptkbp:collaboration
|
gptkb:Yes
|
|
gptkbp:commander
|
gptkb:Yes
|
|
gptkbp:communication
|
gptkb:Mars_rovers
gptkb:International_Space_Station
gptkb:Hubble_Space_Telescope
gptkb:Earth_observation
|
|
gptkbp:communication_latency
|
gptkb:Low
|
|
gptkbp:controls
|
Reaction wheels
|
|
gptkbp:cooling_system
|
Passive and active systems
|
|
gptkbp:data_relay_capability
|
gptkb:Yes
|
|
gptkbp:data_transmission
|
gptkb:Yes
|
|
gptkbp:data_usage
|
up to 300 Mbps
|
|
gptkbp:design
|
15 years
|
|
gptkbp:frequency
|
C-band
S-band
Ka-band
|
|
gptkbp:healthcare
|
gptkb:Yes
|
|
gptkbp:home_ground
|
gptkb:White_Sands_Complex
Multiple ground stations
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TDRS-L
|
|
gptkbp:image_processing
|
Onboard
|
|
gptkbp:launch_date
|
January 23, 2014
|
|
gptkbp:launch_mass
|
3,200 kg
|
|
gptkbp:launch_platform
|
gptkb:United_Launch_Alliance
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas_V_401
|
|
gptkbp:launch_window
|
gptkb:N/_A
|
|
gptkbp:manufacturer
|
gptkb:Boeing
|
|
gptkbp:mass
|
3,200 kg
|
|
gptkbp:mission
|
gptkb:NASA_Goddard_Space_Flight_Center
|
|
gptkbp:mission_duration
|
15 years
|
|
gptkbp:mission_type
|
Satellite communication
tracking and data relay
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_use
|
gptkb:2014
TBD
|
|
gptkbp:operator
|
gptkb:NASA
|
|
gptkbp:orbit_type
|
gptkb:Boeing_702_series
Geostationary orbit
Parabolic
|
|
gptkbp:orbital_altitude
|
gptkb:geostationary_orbit
|
|
gptkbp:orbital_inclination
|
0 degrees
|
|
gptkbp:payload_capacity
|
1,500 kg
10 k W
|
|
gptkbp:power_source
|
Solar panels
|
|
gptkbp:powers
|
10 k W
|
|
gptkbp:propulsion
|
Chemical propulsion
|
|
gptkbp:provides_information_on
|
gptkb:Yes
|
|
gptkbp:purpose
|
gptkb:communication
|
|
gptkbp:reliability
|
gptkb:High
|
|
gptkbp:scientific_instruments
|
Communication payloads
|
|
gptkbp:series
|
gptkb:TDRS-K
gptkb:TDRS-M
|
|
gptkbp:service_area
|
Low Earth Orbit
|
|
gptkbp:spacecraft
|
gptkb:geostationary_orbit
Modular design
Standard configuration
|
|
gptkbp:status
|
operational
Operational
|
|
gptkbp:storage
|
gptkb:Yes
|
|
gptkbp:successor
|
gptkb:TDRS-M
|
|
gptkbp:track
|
gptkb:Yes
|
|
gptkbp:weight
|
3,200 kg
|
|
gptkbp:bfsParent
|
gptkb:TDRS-M
|
|
gptkbp:bfsLayer
|
6
|