gptkbp:instance_of
|
gptkb:satellite
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gptkbp:constellation
|
gptkb:GPS_constellation
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gptkbp:data_transmission
|
S-band
|
gptkbp:data_usage
|
50 bps
|
gptkbp:decommissioned
|
no
|
gptkbp:frequency
|
L1, L2
1.57542 GHz
1.2276 GHz
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gptkbp:home_ground
|
gptkb:Schriever_Space_Force_Base
gptkb:Vandenberg_Space_Force_Base
24th Space Operations Squadron
|
https://www.w3.org/2000/01/rdf-schema#label
|
GPS IIR-30(M)
|
gptkbp:is_aplace_for
|
20,200 km
|
gptkbp:last_status_update
|
gptkb:2023
|
gptkbp:launch_date
|
2005-05-05
May 5, 2005
|
gptkbp:launch_mass
|
1,600 kg
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Air_Force_Station
|
gptkbp:launch_vehicle
|
gptkb:Delta_II
|
gptkbp:manufacturer
|
gptkb:Lockheed_Martin
|
gptkbp:market_segment
|
gptkb:GPS_Control_Segment
|
gptkbp:mass
|
1,600 kg
|
gptkbp:navigation_system
|
GPS navigation message
|
gptkbp:operated_by
|
gptkb:United_States_Air_Force
|
gptkbp:operational_since
|
gptkb:2005
|
gptkbp:orbit_type
|
active
A2100
navigation satellite
C/ A code
P(Y) code
second generation GPS satellite
|
gptkbp:orbital_inclination
|
55 degrees
|
gptkbp:orbital_period
|
12 hours
|
gptkbp:part_of
|
gptkb:GPS_Block_IIR
|
gptkbp:performance
|
< 5 meters
|
gptkbp:perigee
|
20,200 km
|
gptkbp:positioning_system
|
gptkb:Earth_observation
|
gptkbp:power_source
|
solar panels
|
gptkbp:purpose
|
gptkb:navigation
|
gptkbp:replaced_by
|
gptkb:GPS_III
|
gptkbp:series
|
GPS IIR-29(M)
GPS IIR-31(M)
|
gptkbp:service_lifetime
|
7.5 years
|
gptkbp:status
|
operational
|
gptkbp:successor
|
gptkb:GPS_IIF
|
gptkbp:transponders
|
dual-frequency transponder
|
gptkbp:type
|
gptkb:Earth_observation
|
gptkbp:bfsParent
|
gptkb:GPS_IIR-24(M)
|
gptkbp:bfsLayer
|
6
|