Ham Satellite news


An update of GOLF-TEE project from AMSAT-NA ANS-030:

AMSAT’s GOLF-TEE CubeSat de-manifested from launch on ELaNa-46 NASA has de-manifested GOLF-TEE from the ELaNa-46 mission at the request of AMSAT. ELaNa-46 was expected to launch no earlier than 2022. COVID-related restrictions and supply chain disruptions, affecting both AMSAT’s vendors and team, have put AMSAT’s ability to meet the mission integration timeline at high risk.

AMSAT Vice-President Engineering Jerry Buxton, N0JY, described some of the reasons for this decision:
• AMSAT finds itself in a similar situation to what other payloads and space-industry providers are experiencing. The worldwide pandemic and supply chain shortages are threatening everyone’s ability to properly and successfully deliver for launches.
• Out of respect for NASA, the launch provider, and other payloads, it is important to withdraw now, rather than later or, even worst, missing a launch integration deadline, which has possible financial penalty implications.
• GOLF-TEE and GOLF-1 have both been selected to participate in NASA’s CubeSat Launch Initiative program, and NASA will continue to look for another launch for GOLF-TEE.

AMSAT’s GOLF program plays an important role in AMSAT’s return to highly elliptical orbits. In addition to proving the maneuverability capabilities required by current and proposed orbital debris regulations, the GOLF program will work through a series of increasingly capable spacecraft to develop skills and learn systems for which we do not yet have the necessary low-risk experience. Among these are active attitude control, deployable/steerable solar panels, radiation tolerance for Commercial off the Shelf (COTS) components in higher orbits, and propulsion.

The TEE designation in GOLF-TEE stands for “Technology Exploration Environment” and reflects GOLF-TEE’s mission goal to test two critical systems needed for higher orbits. The first is an Attitude Determination and Control System (ADCS) that will allow active pointing of high gain satellite antennas, provide accurate attitude adjustments in future missions with maneuverability systems, and allow pointing the fixed solar panel array for best solar power in any given orbit type. The second is the Radiation-Tolerant Integrated Housekeeping Unit (RTIHU), which will allow AMSAT to gain initial orbit and space radiation exposure for radiation event-induced fault tolerant systems designed using COTS components. GOLF-TEE’s RTIHU includes a command transceiver, and its design is based on the Hercules line of ARM architecture-based microcontrollers.

GOLF-TEE will also evaluate a low-cost, deployable, fixed attitude, solar panel array design as part of AMSAT Engineering’s exploration of fixed panel arrays that allow for outfitting a variable number of “wings” in order to best match the power requirements of various CubeSat missions. Additionally, GOLF-TEE will carry a modified Ettus E310 commercial software-defined radio (SDR), as an experimental package, to test the high speed data downlink in the 10 GHz band and a parrot V/x mode linear transponder to provide users with an opportunity to experiment with the 10 GHz microwave downlink. GOLF-TEE will also carry a legacy V/u linear transponder.

GOLF-1 will build on technology and lessons learned from the GOLF-TEE mission; however, it will be a return to STEM-based educational missions, including hosted student radiation and imaging experiments in collaboration with AMSAT’s educational partners. GOLF-1 will require a more comprehensive de-orbiting plan and hardware that are in compliance with NASA’s NPR 8715.6 NASA Procedural Requirements for Limiting Orbital Debris in order to be manifested on an ELaNa launch to the high altitude AMSAT is seeking.

A significant amount of funding is necessary to complete the development and construction of the GOLF series of CubeSats. Please consider a donation today. Donations designated for the AMSAT GOLF program may be made at

[ANS thanks Robert Bankston, KE4AL, President AMSAT for the above information]

Ham Satellite news

EASAT-2 and HADES Updates

Info from ANS:

Felix Paez, EA4GQS, AMSAT-EA Mission Manager provided the last information on their satellites as of January 18, 2022.

“We confirm the reception of both EASAT-2 and HADES, as well as the decoding of telemetry and the FM recorded voice beacon with the callsign AM5SAT of the first one. EASAT-2 appears to be working well except for the deployment of the antennas, something that apparently has not yet occurred and causes weak signals. However, the AMSAT-EA team confirms that, based on the reception of FSK, CW, the FM voice beacon and the telemetry data that has been decoded, it can be said that the satellite is working perfectly. In the event of low battery or system malfunction, the on-board computer would not transmit CW messages or the voice beacon-callsign, as it would be in a ‘safe’ state with only fast and slow telemetry transmissions.

“These signals that have been able to confirm the operation of both satellites were received by Dr. Daniel Estévez EA4GPZ at 18:07 UTC on Saturday, January 15, using two antennas from the Allen Telescope Array. The TLEs used were obtained from the radio amateur community, with Doppler observations from the Delfi-PQ satellite, deployed together with EASAT-2 and Hades.

“TLEs used were these ones:

Daniel, EA4GPZ, performed a preliminary analysis using just one polarization of one of the satellite dishes. EASAT-2 has been detected with a relatively strong signal, close to the Delfi-PQ signal, obtaining said recorded voice FM beacon transmissions and FSK, FSK-CW at 50 baud.

“The CW beacon clearly shows the message: VVV AM5SAT SOL Y PLAYA, which is one of several that both satellites emit, although the callsign AM5SAT confirms that it is EASAT-2.

“In the recording made by Daniel EA4GPZ there is also a faint trace confirmed to be from Hades and stronger packets probably from the IRIS-A satellite.

“HADES, like EASAT-2, is transmitting weak signals, weaker than the ones of EASAT-2, most likely because the on-board computer has not yet managed to deploy the antennas either, although it will continue trying regularly. The reason the signals are suspected to be weaker at Hades is that the antennas are more tightly folded than those of EASAT-2. In any case, this is great news, since the transmission pattern confirms the proper functioning of the satellite. In the observations you can see the FSK tones with a deviation of about 5 kHz interspersed with the FM carrier corresponding to the voice beacon of the satellite, which has callsign AM6SAT. The AMSAT-EA team is working to try to decode the telemetry signals and obtain more detailed information on the state of the satellite.

“We kindly ask you, if you have very high gain antennas, to try to receive them, specially Hades. If we could decode telemetry it would be very helpful for us.

“Until antennas are deployed it will be very difficult to use their repeaters or to receive any SSTV camera images from Hades, but we hope that this will happen sooner or later, at least because even if the computer doesn’t succeed applying heat to the resistor where the thread is attached, with time, the thread should break due to the space environment conditions.

Details of the decoded telemetry and voice, as well as more details in: (Texts are In Spanish)

And in the following Twitter threads:

EASAT-2 transmissions:
EASAT-2 decodings by Gabriel Otero:
HADES transmissions:”

[ANS thanks Felix Paez, EA4GQS, AMSAT-EA Mission Manager for the above information.]

Ham Satellite news Members news

AMSAT-SM 40 years during 2022

During this year 2022 AMSAT-SM celebrate 40 years as a satellite group in Sweden. Stand by for more events later this year! As you can see we have also updated our logos.

73 from the steering group of AMSAT-SM

Ham Satellite news

Updated XW-3 CAS-9 User Manual v1.11

Alan BA1DU has sent an updated XW-3 CAS-9 User Manual and can be downloaded here:

Ham Satellite news

CAS-9 XW-3 successful launch

The CAS-9 XW-3 satellite was launched today 26 dec 2021. Several reports on Twitter reporting the satellite to be active on both CW, GMSK and transponder. Congratulation to the CAMSAT team! Some examples from the Twitter feed:

Vlad Chorney @EU1SAT received raw telemetry:

Several reports on the SatNOGS network:

K8YSE has done several QSOs via the transponder:

Ham Satellite news

CAS-9 XW-3 launch Dec 26 2021

CAS-9 XW-3

Updated info 22 dec from Alan Kung, BA1DU:

Hello OM,
The CAMSAT XW-3 (CAS-9) amateur radio satellite will be launched at UTC 03:11:31 on 2021-12-26 , and will be deployed at 98.858° east longitude and 28.413° north latitude at UTC 03:35:58, location close to Western Australia.

Radio amateurs will receive CW beacon and GMSK telemetry signals approximately 38 seconds after the satellite is separated from the launch vehicle, and then the linear transponder will be put into use after approximately 49 seconds.

Attached is the launch schedule and the Two-Line Orbital Element file.

Alan Kung, BA1DU

1 99999U 21360.14997609 .00000032 00000-0 10363-4 0 00007
2 99999 098.5836 072.3686 0004232 307.2415 261.3002 14.38559758000156

This is an example how a pass can look like over north NA and EU:

According to info from ANS-353 and BA1DU, Alan Kung, CAMSAT XW-3(CAS-9) amateur radio satellite will be launched by Chinese CZ-4C Y39 launch vehicle on December 25, 2021 from the Taiyuan Satellite Launch Center in China. XW-3(CAS-9) satellite will be piggybacked on the rocket with primary payload ZY-1(02E) satellite.

The satellite orbit is a circular sun-synchronous orbit with an altitude of 770.1 kilometers and an inclination of 98.58 degrees, the running cycle is 100.14 minutes. The functions of XW-3(CAS-9) satellite include UHF CW telemetry beacon, GMSK telemetry data transmission, V/U mode linear transponder, a visible light band space camera and an experimental thermoelectric generator for high school students. After the satellite completes the in-orbit test and works normally, the space camera photo download will be open to amateur radio enthusiasts all over the world.

When the relevant remote control command is received by the satellite, the GMSK telemetry channel will be used to downlink the photo storage information and photo data, and the telemetry data will stop sending at that time.

XW-3(CAS-9) satellite adopts a 6U CubeSat structure with a mass of about 10kg, an onorbit envelope size of 340.5×121.76x998mm with four solar array panels and a threeaxis stabilized attitude control system is used, long-term power consumption is about 15.2 Watts.

Technical specifications:
● VHF antenna: 1/4 wavelength whip antenna
● UHF antenna: 1/4 wavelength whip antenna
● CW telemetry beacon:
Frequency: 435.575MHz RF power: 20dBm CW rate: 22wpm
● GMSK telemetry:
Frequency: 435.725MHz RF power: 23dBm Data rate: 4800bps
● V/U mode linear transponder:
Uplink frequency: 145.870MHz
Downlink frequency: 435.180MHz
RF power: 20dBm Bandwidth: 30kHz Spectrum inverted