FoxTelem Version 1.06 Released

​I am releasing version 1.06 of FoxTelem today.  This release addresses several defects and instabilities in FoxTelem 1.05 and earlier.  It also introduces a new Earth Plot that allows any telemetry value to be plotted as a heat map against a map of the earth.  For more details about the Earth Plot and some example plots, you can read a quick tutorial that I have written here:

As always, let me know if you see any issues or log them on Github at

* EARTH PLOTS allow you to plot any telemetry value as a heat map on a map of the earth
* Allow graphs and telemetry results to be searched with UTC dates and for ranges of uptime/dates
* Allow stepping through the telemetry with up/down arrows
* Prevent hang when decoder starts if FCD returns an error
* Fixed bug where TLEs were not updated in the name is changed in the spacecraft settings window
* Fixed crashes introduced in 1.05 release
* Display all HERCI High Speed payloads when Raw Byte Payloads shown.
* Fix bug where missing TLE disables spacecraft from being tracked at all
* Fixes bug where DDE connection to SatPC32 fails with European decimal point format
* Add MPPT calibration values for Fox-1D
* Improved the RF signal measurements
* Improved the Find Signal algorithm
* Space graph labels more evenly
* Put the spacecraft tabs in FoxId order

And many other bug fixes. Full list of changes here:

You can download the latest version of the program from:

AO-92 Commissioned, Open for Amateur Use

On the 03:25 UTC pass on January 26, 2018, AMSAT Vice President – Engineering Jerry Buxton, N0JY, announced that AO-92 had been commissioned and formally turned the satellite over to AMSAT Operations. AMSAT Vice President – Operations Drew Glasbrenner, KO4MA, then declared that AO-92 was now open for amateur use. Audio of the handover and first operational pass can be heard here:


Initially, the U/v FM transponder will be open continuously for a period of one week. After the first week, operations will be scheduled among the U/v FM transponder, L-Band Downshifter, Virginia Tech Camera, and the University of Iowa’s High Energy Radiation CubeSat Instrument (HERCI).

Schedule updates will appear in the AMSAT News Service Weekly Bulletins and will also be posted to the AMSAT-BB, AMSAT’s Twitter account (@AMSAT), the AMSAT North America Facebook group, and the AMSAT website at

AO-92 was launched on the PSLV-C40 mission from Satish Dhawan Space Centre in Sriharikota, India on January 12, 2018. For the past two weeks, the AMSAT Engineering and Operations teams have been testing the various modes and experiments on board. Testing has shown that both the U/v FM transponder and L-Band Downshifter work very well. The Virginia Tech camera has returned stunning photos and data from HERCI has been successfully downlinked.

AMSAT thanks the 178 stations worldwide that have used FoxTelem to collect telemetry and experiment data from AO-92 during the commissioning process. The collection of this data is crucial to the missions of AMSAT’s Fox-1 satellites. Please continue to collect data from AO-85, AO-91, and AO-92.

Radio Programming Charts

AO-92 Doppler Shift Correction (Mode U/v)


Your Transmit Frequency

(With 67 Hz Tone)

Your Receive Frequency

Acquisition of Signal (AOS) 435.340 MHz 145.880 MHz
Approaching 435.345 MHz 145.880 MHz
Time of Closest Approach (TCA) 435.350 MHz 145.880 MHz
Departing 435.355 MHz 145.880 MHz
Loss of Signal (LOS) 435.360 MHz 145.880 MHz

AO-92 Doppler Shift Correction (Mode L/v)


Your Transmit Frequency

(With 67 Hz Tone)

Your Receive Frequency

Acquisition of Signal (AOS) 1267.320 MHz 145.880 MHz
Approaching 1 1267.325 MHz 145.880 MHz
Approaching 2 1267.330 MHz 145.880 MHz
Approaching 3 1267.335 MHz 145.880 MHz
Approaching 4 1267.340 MHz 145.880 MHz
Approaching 5 1267.345 MHz 145.880 MHz
Time of Closest Approach (TCA) 1267.350 MHz 145.880 MHz
Departing 1 1267.355 MHz 145.880 MHz
Departing 2 1267.360 MHz 145.880 MHz
Departing 3 1267.365 MHz 145.880 MHz
Departing 4 1267.370 MHz 145.880 MHz
Departing 5 1267.375 MHz 145.880 MHz
Loss of Signal (LOS) 1267.380 MHz 145.880 MHz

AO-92 Commissioning Update: HERCI Experiment and L-Band Downshifter Tested

The AMSAT Engineering and Operations teams have been hard at work testing the various modes and experiments aboard AO-92 since its launch on January 12th. Since the last update, testing has concentrated on the University of Iowa’s High Energy CubeSat Radiation Instrument (HERCI) experiment and the AMSAT L-Band Downshifter.

The HERCI experiment was activated for the first time on January 18, 2018. According to Don Kirchner, KDØL, Research Engineer at the University of Iowa, “HERCI is intended to provide a mapping of radiation in a low earth orbit. This is of scientific interest for planning CubeSat test flights for low energy X-Ray detectors.”

“The instrument consists of a digital processing unit (DPU) derived from processors currently in orbit around Saturn on Cassini and on the way to Jupiter on the Juno spacecraft,” said Kirchner during a 2015 interview. “The DPU was shrunk to a CubeSat form factor with funding from the Iowa Space Grant Consortium.”

While the HERCI experiment collects data continuously while the transponder is in operation, the data is only downlinked in the satellite’s high-speed data.

The HERCI Engineering Model boards prior to initial test. The boards will be tested before installation of the radiation detector and hybrid circuits. The digital processor board is the first use of the Y90 microprocessor firmware which was donated by Monte Dalrymple, KR6DC, of Systemyde Corporation.


In a Space Physics laboratory in Van Allen Hall, University of Iowa Electrical Engineering students Patrick Maloney, KD9CPD; Tyler Dunkel, KE0CHR; Kevin Klosterman, KD9CPF; and Bryan Senchuk, KD9CPE inspect the HERCI development boards.

After testing operation of the HERCI experiment and the downlinking of the experiment data, focus turned to the AMSAT L-Band Downshifter. When enabled, the L-Band Downshifter converts signals received on 1267.350 MHz and injects them into the satellite’s 435 MHz receiver. Due to the increased path loss on 1267 MHz and the utilization of the satellite’s 435 MHz receive antenna on 1267 MHz, pre-launch estimates suggested that around 100 watts ERP may be required for horizon to horizon access in this mode. As always, pre-launch estimates are subject to change after real-world testing in-orbit.

At 02:19 UTC on January 20, 2018, the L-Band Downshifter was commanded on for the first time. Initial testing showed promising results. Your author was able to access the transponder with an Alinco DJ-G7T HT with 1 watt output into a Comet CYA-1216E yagi. Telemetry analysis showed that the Downshifter was functioning normally and AMSAT announced open testing.

Reports flowed in of QSOs occurring over Europe and Japan. Many reported QSOs made with 10 watts or less to modest yagi antennas. EB1AO reported success using 2-3 watts output to a small yagi. IW1DTU reported using 10 watts to a horizontally polarized 10 element loop yagi. IU2EFA reported two QSOs made using 10 watts to a vertical groundplane antenna. Reports from Japan were similar. JK2XXK reported two QSOs with 10 watts to a vertically polarized 17 element loop yagi and JA6PL reported a QSO with 10 watts to a horizontally polarized 23 element yagi.

EB1AO setting up for his first pass of AO-92 in Mode L/v

The first open pass over North America occurred at around 02:00 UTC on January 21, 2018. Seven stations were heard, your author, KE4AL, WB8OTH, WB8RJY, NS3L, N8TLV, and VE4AMU. KE4AL and VE4AMU were using similar stations, KE4AL was using a Kenwood TM-942A (10 watts output) and a Comet CYA-1216E yagi modified with holes drilled in the boom to add 2 meter Arrow II elements. VE4AMU was using the same antenna with a Kenwood TM-941A mobile radio. Your author was also using that antenna, but with an Alinco DJ-G7T handheld and was able to open the transponder at around 10 degrees of elevation. Most impressively, N8TLV was heard using just a Yaesu FT-104 handheld transceiver and the stock rubber duck for the uplink. He was weak, but readable from around 35-38 degrees of elevation. AMSAT plans to publish articles in the future discussing equipment options for use on the L-Band uplink.

Rick Behma, VE4AMU, working AO-92 in Mode L/v with a Kenwood TM-941 mobile transceiver and Comet CYA-1216E yagi crossed with 2 meter Arrow II elements.

Audio from your author’s recording of the AO-92 Mode L/v pass over North America can be heard here:


The L-Band Downshifter operates on a 24 hour timer and shut off on schedule around 02:19 UTC on January 21, 2018. Tests of the various modes and experiments continue. AO-92 is on track to be commissioned and handed over to AMSAT Operations on Friday, January 26th.

AO-92 Commissioning Update: Transponder and Camera Tested, Further Camera Tests Planned

The first thirty-six hours of AO-92’s life in orbit have seen a flurry of activity as the AMSAT Engineering and Operations teams walk through an extensive checklist of tests required to check the functionality of the satellite’s on-board systems.

The first crucial test came on the initial pass over AMSAT command stations hours after launch. Around 15:00 UTC on January 12, 2018, AMSAT command stations successfully issued the first command to the satellite, changing it from the initial Beacon Mode to Safe Mode. The switch to Safe Mode allowed the collection of min and max data for the various telemetry values.

As AMSAT Engineering continued to evaluate the data received, the decision was made to test the U/v FM transponder briefly on the evening passes over North America. At approximately 01:30 UTC on January 13, 2018, the satellite was commanded to Transponder Mode for the first time. Initial tests show the transponder functions very well. One testing station was able to access the satellite using 5 watts from an HT to a whip antenna from inside his house at approximately ten degrees of elevation. AMSAT Engineering reminds all amateur radio operators that, although the satellite may be found in Transponder Mode at times during the commissioning process, it is essential to not transmit to the satellite before it is opened for general use as you may interfere with various tests that need to be performed.

The first image received from the Virginia Tech camera.

With the transponder successfully tested and telemetry values continuing to be nominal, attention turned to the Virginia Tech camera. At about 14:30 UTC, the camera was turned on and quickly returned it’s first image of Earth. On the next pass over North America, the camera was again turned on and several images flowed into AMSAT servers. Images captured and uploaded can be found at

AMSAT plans further testing of the Virginia Tech camera during the early hours of January 14, 2018 (UTC). If not shut off by a command station, the camera remains active for a period of 40 minutes following activation, so the active period may vary depending on when the camera is activated.

January 14, 2018 Camera On Times (Approximate)

The first image of Earth received from the Virginia Tech camera.

01:12 UTC – 01:52 UTC

02:42 UTC – 02:51 UTC

This should provide an opportunity for stations in areas including Russia, China, and Japan to receive pictures from the Virginia Tech camera. Please be sure that FoxTelem’s source is set to “Auto” so you will be able to receive either high-speed frames carrying camera payloads or data under voice (DUV) frames when the satellite is in Safe Mode or Transponder Mode. If using an external audio source for FoxTelem, be sure you are set for a minimum bandwidth of 20 kHz to receive the high-speed data.

Thank you to all stations who have uploaded telemetry data to AMSAT servers. As of 18:00 UTC on January 13, 2018, a total of 90 unique stations have contributed telemetry from AO-92. Continued collection of telemetry data is essential to the commissioning process. AMSAT greatly appreciates the participation of the amateur radio community in collecting telemetry for the Fox-1 satellites.

A view of the curvature of the Earth seen from the Virginia Tech camera. At the top of the image in the middle of the frame, you can see the tip of the satellite’s receive antenna and a piece of the line that held the antenna down prior to deployment.