MDQSAT-1B
Mission information
Name
MDQSAT-1B
Alternate Names
"Simón Bolivar"
Satellite ID
QEYL-4712-2825-4820-1289
Temporary NORAD ID
99240
Followed NORAD ID
None
Website
https://www.innova-space.com/en/
Country of Origin

Argentina

Status
Satellite future
Future

Satellite is not yet in orbit


Frequency Misuse

Satellite is reported to be transmitting at an uncoordinated or denied frequency. Details

Image
MDQSAT-1B
Mission timeline
Launch Date
2023-01-02T14:55:00+00:00
Description

he MDQSAT-1B satellite, "Simón Bolivar", is the third in the "Libertadores de América" constellation. It’s a 0.5U CubeSat (10 x 10 x 5cm) and it weights 549g.

MDQSAT-1A/B are proof of concept for IoT communications through picosatellites in LEO. They have UHF communications (1W LoRa), stabilization through magnetorquers, a GNSS receiver, 3J solar cells and a Li-Ion battery. They also have temperature, current, light, and absolute orientation sensors that are needed for the satellite to operate and their data is sent as housekeeping telemetry.

They are developed by Innova Space in Argentina and their main purpose is to test the satellite platform for use in future missions.

Type
Transmitter
Downlink Mode
FM
Downlink Frequency
437800000
IARU Coordination
IARU Uncoordinated
Type
Transmitter
Downlink Mode
FM
Downlink Frequency
436900000
IARU Coordination
IARU Uncoordinated
Most Recent Observers (last 24h)

No observations recorded for MDQSAT-1B in the last 24h

Data Frames Decoded - 30 Days
There is no decoded data for this satellite in the last 30 days.
No Decoders Found
Help us develop a decoder, you can find instructions at this wiki link
MDQSAT-1B Suggestion
Name
MDQSAT-1B
NORAD ID
99240
Alternative Names
"Simón Bolivar"
Description
he MDQSAT-1B satellite, "Simón Bolivar", is the third in the "Libertadores de América" constellation. It’s a 0.5U CubeSat (10 x 10 x 5cm) and it weights 549g. MDQSAT-1A/B are proof of concept for IoT communications through picosatellites in LEO. They have UHF communications (1W LoRa), stabilization through magnetorquers, a GNSS receiver, 3J solar cells and a Li-Ion battery. They also have temperature, current, light, and absolute orientation sensors that are needed for the satellite to operate and their data is sent as housekeeping telemetry. They are developed by Innova Space in Argentina and their main purpose is to test the satellite platform for use in future missions.
image
Satellite image
status
dead
countries
website
https://blog.preciouspayload.com/launchers-orbiter-sn1-failure-rip-spaceryde-and-more-smallsat-updates/
launched
Jan. 2, 2023, 2:55 p.m.