Operational
Satellite is in orbit and operational
Launch Date
2018-12-03T18:32:00+00:00
A 2U CubeSat -The Mission is: 1. Space station for amateur radio communication training. Sends beacon signals using UHF band with GMSK modulation. Earth stations that have capability of receiving S-band will be able to receive S-band signals. 2. Technology demonstration of in-house developed dual frequency GPS receiver. 3. Technology demonstration of measuring TEC and magnetic field using dual frequency GPS receiver and fine magnetometer with a boom. Requesting a UHF downlink for 9k6 GMSK packet and a 2.4GHz downlink for 460kbps or 1Mbps DQPSK. Planning a SpaceX launch from Vandenberg into a 600km SSO in August 2017.
Type
Transmitter
Downlink Mode
GMSK
Downlink Frequency
437.275 MHz
Baud
9600
IARU Coordination
IARU Coordinated
https://iaru.amsat-uk.org/finished_detail.php?serialnum=529
Observer
Latest Data
ISAE.Supaero UHF/VHF-JN03rn
2025-07-13 09:29:15 UTC
PE0SAT-JO21mr
2025-07-13 09:25:13 UTC
PE0SAT-21-JO21mr
2025-07-13 09:25:13 UTC
PE0SAT-11-JO21mr
2025-07-13 09:23:16 UTC
Drachten-JO33bc
2025-07-13 09:22:46 UTC
There is no decoded data for this satellite in the last 30
days.
destination_callsignsource_callsigncsp_header_prioritycsp_header_sourcecsp_header_destinationcsp_header_destination_portcsp_header_source_portcsp_header_reservedcsp_header_flagsfirmware_versionpositioning_flagposition_xposition_yposition_zvelocity_xvelocity_yvelocity_zbattery_modebattery_voltagebattery_currentpower_switch_gps_sidepower_switch_magnetometerpower_switch_sd_cardpower_switch_gps_uppower_switch_uhfpower_switch_boompower_supply_current_boompower_supply_current_uhfpower_supply_current_gps_uppower_supply_current_sd_cardpower_supply_current_magnetometerpower_supply_current_gps_sidesolar_cell_input_voltage_xsolar_cell_input_voltage_ysolar_cell_input_voltage_zsolar_cell_input_current_xsolar_cell_input_current_ysolar_cell_input_current_zestimated_attitude_q0estimated_attitude_q1estimated_attitude_q2estimated_attitude_q3estimated_gyro_bias_rollestimated_gyro_bias_pitchestimated_gyro_bias_yawestimated_angular_rate_rollestimated_angular_rate_pitchestimated_angular_rate_yawmeasured_angular_rate_rollmeasured_angular_rate_pitchmeasured_angular_rate_yawsun_eclipseattitude_convergenceattitude_variance_q0attitude_variance_q1attitude_variance_q2attitude_variance_q3current_operation_modeelapsed_timetemperature_solar_panel_plus_xtemperature_solar_panel_plus_ytemperature_solar_panel_minus_xtemperature_solar_panel_minus_ytemperature_solar_panel_minus_ztemperature_obc_1temperature_obc_2temperature_eps_module_1temperature_eps_module_2temperature_eps_module_3temperature_eps_module_4temperature_uhf_module_1temperature_uhf_module_2boom_release_statusantenna_release_statuscount_antenna_release_trialcount_boom_release_trialbeacon_typesatellite_time
Latest Two-Line Element (TLE)
TLE Source
Space-Track.org
TLE Updated
2025-07-13 09:02:46 UTC
TLE Set
1 43784U 18099AC 25194.10349979 .00007373 00000-0 36522-3 0 9997
Satellite Suggestion History
Transmitter Suggestion History
Select Transmitter
-----------------
GMSK9k6 TLM | NTAbJCQ75TbkNGqXA4gMYi
