07:57 UTC
jj2ypm s1 59 00 00 00 s2 56 02 00 b4
jj2ypm s1 5a 00 00 00 s2 5a 02 00 bd
jj2ypm s1 59 00 00 00 s2 57 02 00 b6
jj2ypm s1 58 00 00 00 s2 5b 02 00 .f
jj2ypm s1 58 00 00 00 s2 57 02 00 b8
Category: STARS
STARS-C CW Beacon
21:17 UTC
STARS-C Mother CW beacon
07:42 UTC
jj2ypl s1 57 00 00 00 s2 68 01 00 d8
jj2ypl s1 55 00 00 00 s2 6d 01 00 e9
jj2ypl s1 56 00 00 00 s2 67 01 00 d9
STARS-C Mother
STARS-C Mother Telemetry
JJ2YPL S1 5* 00 00 00 S2 67 01 00 D9 JJ2YPL S1 56 00 00 00 S2 68 01 00 D9 JJ2YPL S1 54 00 00 00 S2 67 01 00 D9 JJ2YPL S1 5* 00 00 00 S2 67 01 00 D8 JJ2YPL S1 54 00 00 00 S2 69 01 00 D* JJ2YPL S1 56 00 00 00 S2 6* 01 00 D9
STARS-C Mother CW beacon
16:34 UTC
jj2ypl s1 54 00 00 00 s2 68 01 00 d8 jj2ypl s1 54 00 00 00 s2 68 01 00 d8 jj2ypl .. 01 00 d9 jj2ypl s1 54 00 00 00 s2 .. 01 00 d8 jj2ypl s1 54 00 00 00 s2 67 01 00 d7 jj2ypl s1 52 00 00 00 s2 67 ...
STARS-C deployed
STARS-C has been deployed at 08:55 UTC
STARS-C 1 00000U 00000A 16354.36827862 .00000000 00000-0 00000-0 0 0000 2 00000 51.6492 214.6791 0009020 33.9061 293.7118 15.53379777 00000
STARS-C Mother
…next round of cubesat deployments begins on ISS
A new set of cubesats will be released tomorrow, December 19th, 2016.
For the deployment, the Japanese robotic arm moves the deployer to a specific position to ensure the satellites depart on a safe trajectory with no risk of re-contact with ISS on any subsequent orbits after which drag will have separated ISS and the much smaller CubeSats.
Here is a list of the CubeSats on Japan’s payload manifest, with descriptions offered by JAXA :
AOBA-Velox 3 – from the Kyushu Institute of Technology in Japan and the Nanyang Technological University in Singapore, will evaluate the performance of a pulsed plasma thruster
TuPOD – from the Italian company GAUSS, will attempt deployment of two daughter nanosatellites from Brazilian and U.S. builders
ITF-2 – from the University of Tsukuba, will connect amateur radio users
STARS-C – from Shizuoka University, will attempt to extend a tether between two 1U CubeSats
WASEDA-SAT 3 – from Waseda University, will also deploy a “film-type” de-orbiting device and project an image onto the film surface using a micro-miniature projector
STARS Mother CW beacon
15:55 UTC
hello, world. m3 8a404144 m5 fffff4ff
hello, world. m3 8c424243 m5 ffffffff
hello, world. m3 c23f433f m5 ffffffff
hello, world. m3 8f403d3f m5 fffffaff
hello, world. m3 8e3e3f41 m5 ffffe7ff
hello, world. m3 88413e40 m5 fffff5ff
hello, world. m3 a0434041 m5 fffff8ff
hello, world. m3 78424142 m5 fffff1ff
STARS Mother CW beacon
16:20 UTC
hello, world. m3 95 3f 43 3f m5 ff ff ec ff
hello, world. m3 9b 3e 3e 3e m5 ff ff ea ff
hello, world. m3 99 3d 3d 3e m5 ff ff d1 ff
RSSI : 77.5 Temperature 1 : 58.67 C Temperature 2 : 58.67 C Temperature 3 : 58.67 C Solar Cell Current : 2.02 mA Solar Cell Voltage : 15.02 V Total System Current : 5.25 mA Total Voltage : 15.02 V
STARS Mother CW beacons
15:06 UTC
hello, world. m3 98423f3f m5 fffff5ff hello, world. m3 a1434340 m5 ffffe5ff hello, world. m3 c83c3f41 m5 ffffe5ff hello, world. m3 c83f3e41 m5 ffffe0ff hello, world. m3 c63f3e3e m5 ffffe7ff hello, world. m3 b23c3d3e m5 ffffdfff RSSI : 89.0 Temperature 1 : 59.75 C Temperature 2 : 59.21 C Temperature 3 : 58.67 C Solar Cell Current : 2.02 mA Solar Cell Voltage : 15.02 V Total System Current : 5.61 mA Total Voltage : 15.02 V
