To conduct the UVSQ-SAT mission on the best way, the ham radio community is involved in many major project activities. To formalize this partnership, an agreement protocol has been signed on 1st October 2019 between LATMOS, F6KRK, and AMSAT-Francophone. The Saint-Quentin-en-Yvelines Radio-Club (F6KRK) works jointly with the LATMOS on the project ground station preparation and commissioning.

As part of the ham radio mission, the UVSQ-SAT one-unit CubeSat embeds a radio transponder which will be accessible to the community in parallel of the other scientific objectives according to the power budget. The UVSQ-SAT team will provide an availability of the transponder up to 20% (schedule 7 to 15 days in advance with a distribution via the project's website and / or tweeter account, transponder activation/deactivation dates, satellite status information's (battery level, ...), constraints (ex: eclipses), ...).

UVSQ-Sat has been coordinated by IARU to use the radioamateur spectrum : Here

Help us to spot UVSQ-SAT!

UVSQ-SAT is planned to be launch end of 2020. Like many CubeSat spacecraft, it will take time before having confirmed TLE for orbit prediction. The more people who can help us spot UVSQ-SAT, the sooner our operations phase can officially begin! If you would like to help listen for UVSQ-SAT, you can do so with the information below.

When the time comes, it will be possible to upload received telemetry on SatNOGS database or on AMSAT-Francophone database.

Alternatively, it will be possible to complete a Google form (with your contact information, lat/long location, TLE used, waterfall (if obtained), and any raw data that you have received from the spacecraft (screenshot or text file).
If you haven’t Google account, please email this information to uvsqsat.telemetry@latmos.ipsl.fr

UVSQ-SAT transceiver characteristics

Hardware model: ISIS UHF downlink Full Duplex Transceiver

Operating frequency: 437,020 MHz

Beacon baud rate: 1200 bps and 9600 bps

Beacon interval: 30 seconds

Bandwidth: 20 kHz

Modulation type: BPSK

Protocol: AX-25 framing

Encoding: NRZI encoding and G3RUH scrambling

Spacecraft Callsign: LATMOS-01

Note for conventional ground station transceiver users

It should be noted that conventional transceivers could have a limited bandwidth that could create a limitation on the usable data rate of the Link. An example is that, due to the limitation of the IF filter bandwidth of the ICOM IC-910 radio the data rate cannot go higher than 1200 bps. 2400 bps may be possible, but with some degradation of the performance.

Another issue when using a conventional radio is the locking procedure. Because the TRXVU uses data scrambling, the audio output of a conventional transceiver is difficult to use as an indication for correct frequency setting by ear. This is due to the fact that the randomized data sounds like noise and is therefore very difficult to recognize. It is recommended to observe a waterfall plot or spectrum plot to ensure correct downlink frequency setting.

Recommended telemetry data flow for your ground station

The recommended telemetry data flow of the ground segment is depicted in the figure below.



Receiver filter:
To limit the bandwidth of the received spectrum the ground segment demodulation chain could have an input receiver bandpass filter.

BPSK demodulation:
The implementation of the BPSK demodulator could be based on a software defined implementation.

NRZ-I decode:
The NRZ-I decoding takes care of decoding the differentially encoded data, it decodes a bit transition into a logic “0”, and no bit transition into a logic “1”.

Descrambling (derandomiser):
After NRZ-I decoding, the data should be passed through a descrambler, where the original data is recovered. It is identical to the scrambling system used in G3RUH FSK AX.25 systems. The descrambling polynomial is 1 + X^12 + X^17.

AX.25 deframing:
The AX.25 deframing block should deframe the AX.25 block and extract the frame contents (addresses, info field, FCS checking, …).
More details about AX.25 could be found Here

LATMOS ground station

The LATMOS ground station is SDR based. It has been successfully used to decode several inflight CubeSat.

The hardware:

Radio: Nooelec “NESDR SMART” (RTL2832U chipset + R820T2 tuner)

Antenna/Yagi: M2 Antenna Inc. “2MCP22” high gain UHF Yagi (RHCP)

Amplifier: SSB Inc. “SP-70” low noise amplifier

Rotator System: Yaesu “G5500” rotator (Azimuth and Elevation pointing)

The software:

SatPC32: Used to control rotator and frequency Doppler correction

SDR#: Used to control SDR dongle

Virtual Audio Cable: Used to redirect audio from SDR dongle

Sound Modem: Used for audio processing

UVSQ-SAT ground software for packet decoding

To properly decode the telemetry sent by UVSQ-SAT, you can find hereafter the ground software developed by AMSAT-Francophone: Here.
You do not need to be amateur operator licensed to simply receive telemetry.

Moreover, the ground software has to decode the PUS protocol. This is the European encapsulation standard for space telecommunication.
More details about PUS could be found here: Here.

Recorded UVSQ-SAT telemetry could be observed on AMSAT-F website:
- Graphical views of the data: Here
- List of contributors: Here

And also on SatNOGS website:
- List of all observations: Here
- Status of UVSQ-SAT: Here

UVSQ-SAT beacon audio file

To test your setup, you can find hereafter a recorded audio file:
These audio files contain some UVSQ-SAT beacons generated with two speeds.

Telemetry speed Download

1200 bps (BPSK / G3RUH)

SDRSharp_20201023_143925Z_437017790Hz_IQ --- Beacon_1200.wav

9600 bps (BPSK / G3RUH)

SDRSharp_20201023_144839Z_437011810Hz_IQ---Beacon_9600.wav

UVSQ-SAT beacon format

UVSQ-SAT transmits a health beacon every 30 seconds. This health beacon contains the most vital housekeeping telemetry on the spacecraft to allow mission operators to quickly assess the overall status of the spacecraft.
If you capture a message that looks similar to the following format, it means that you’ve heard our spacecraft!

Transmission will begin approximately 30 minutes after deployment when the spacecraft systems are initiated. (To be confirmed)

Hereafter is an example of beacon interpretation: UVSQ-SAT Beacon description for web site.pdf

TLE Information

TLE data of all CubeSats deployed are published and can be found via the web pages listed below. You can type “UVSQ-SAT” in the search box.

Space-track (account needed): Here

CelesTrack (no account needed): Here