
Swayam-1 CubeSat Flight Model – Credit COEP
Mineo Wakita JE9PEL reports on the Indian ISRO PSLV-C34 amateur radio satellite launch planned for June 22, 2016 at 0355 UT into a 500 km 98 degree inclination orbit.
Main Payload, Cartosat-2C, Earth Observing
PSLV-XL(C-34), Satish Dharwan Space Centre, Sriharikota, India
Satellite Uplink Downlink Beacon Mode ------------ ------- -------- ------- --------------- BEESAT-4 . 435.950 435.950 4800bps GMSK,CW BIROS . 437.525 . 4800bps GMSK LAPAN-A3435.880 145.880 145.825 FM,APRSMax Valier . 145.860 145.960 CWSathyabamasat . 145.980 . 2400bps BPSK Swayam COEP . 437.025 437.025 1200bps BPSK,CWVenta-1 . . 437.325 CW------------ ------- -------- ------- ---------------
http://www.ne.jp/asahi/hamradio/je9pel/be4lapan.htm
Among the satellites being launched is Swayam-1 developed by students at the College of Engineering Pune (COEP). It will provide a text messaging facility using the COEPSAT protocol.
http://amsatindia.org/coep-satellite-swayam-project/
http://www.coep.org.in/csat/track-swayam/
UPDATE: Yono YD0NXX reports the Indonesian built LAPAN-A3 does not have an amateur radio payload.

On May 21, 2016 the CubeSat UWE-3 celebrated 2.5 years in space without any significant failures.
Some weeks ago we have re-initiated operations with UWE-3 on an interim basis. The goal is to test new magnetic control algorithms in space. Therefore we operate the satellite on the 436.395200 MHz frequency and perform data downloads from time to time. In the figure below the satellite’s rotation rate w is shown for one of the experiments. The goal was to establish a rotation about the satellite’s X-axis (blue) at 10 deg/s while the Y/Z-axes should be at 0 deg/s. In general the desired rotation rate could be achieved but with major deviations from the setpoint. With the intention of optimizing the relevant control laws we will continue with these experiments within the next days and weeks.




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