GPS Block II series

GPTKB entity

Statements (59)
Predicate Object
gptkbp:instance_of gptkb:Earth_observation
gptkbp:communication_system gptkb:CDMA
gptkbp:constellation gptkb:GPS_constellation
gptkbp:data_usage 50 bps
gptkbp:debut gptkb:1994
February 14, 1989
Multiple launches from 1989 to 1994
gptkbp:decommissioned gptkb:2009
gptkbp:development gptkb:1980s
gptkbp:frequency L1, L2
gptkbp:frequency_stability ±5 ppm
gptkbp:home_ground gptkb:GPS_Control_Segment
gptkb:GPS_Master_Control_Station
GPS ground stations
https://www.w3.org/2000/01/rdf-schema#label GPS Block II series
gptkbp:is_integrated_with Integrated with GPS Control Segment
gptkbp:launch_date gptkb:1989
gptkbp:launch_mass 1,000 kg
gptkbp:launch_site gptkb:Cape_Canaveral_Air_Force_Station
gptkbp:launch_vehicle gptkb:Delta_II
gptkbp:launched gptkb:12
gptkbp:manufacturer gptkb:Rockwell_International
gptkbp:market_segment gptkb:Master_Control_Station
gptkbp:military_technology gptkb:Yes
gptkbp:modulation BPSK
gptkbp:navigation_system gptkb:Standard_Positioning_Service_(SPS)
gptkb:Earth_observation
10 meters
gptkbp:operational_status Decommissioned
Operational until decommissioned
gptkbp:operational_use 7.5 years
gptkbp:orbit_type gptkb:Delta_II_rocket
gptkb:GPS_IIR-1
gptkb:Pseudorandom_noise_code_(PRN)
gptkb:12
gptkb:GPS_IIA-1
Modular design
Radio frequency communication
Medium Earth Orbit (MEO)
Solar power system
A2100
3-axis stabilized
7.5 years
Deployed in orbit from 1989 to 1994
Navigation satellite
gptkbp:orbital_altitude 20,200 km
gptkbp:orbital_period 12 hours
gptkbp:performance 10 meters
gptkbp:power_source Solar panels
gptkbp:primary_use Navigation
gptkbp:replaced_by gptkb:GPS_Block_IIR
gptkbp:signal_frequency_l1 1575.42 MHz
gptkbp:signal_frequency_l2 1227.60 MHz
gptkbp:successor gptkb:GPS_Block_III_series
gptkbp:track Ground-based tracking stations
gptkbp:user_countries gptkb:Yes
gptkbp:weight 1,000 kg
gptkbp:bfsParent gptkb:GPS_IIR_satellites
gptkbp:bfsLayer 6