From Wikipedia, the free encyclopedia
Ginrei
or
ShindaiSat
was a 400x400x450mm cube-like microsatellite intended to text experimental visible light communication.
[3]
The satellite is made in
Shinshu University
(Japan). The ground station was completed by 18 March 2014 and attempts to communicate with satellite have started the same day. 2-way optical communication with ground station is planned. Also, advanced attitude control using visible light communication is planned as well.
Mission results
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The
Ginrei
optical signals were received 10 seconds per pass, averaged over 56 passes over the control station.
[4]
The narrow beam and infrequent operation of optical transmitter have resulted in severe disappointment in amateur optical tracking community.
[5]
See also
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References
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External links
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January
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February
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March
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April
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May
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June
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- Kosmos 2500
/
GLONASS-M
755
- AprizeSat
9,
AprizeSat
10,
BRITE-Montreal
,
BRITE-Toronto
,
BugSat 1
,
Deimos-2
,
Hodoyoshi 3
,
Hodoyoshi 4
,
KazEOSat 2
,
Perseus-M1
,
Perseus-M2
,
SaudiSat-4
,
TabletSat-Aurora
,
UniSat-6
(
Lemur-1
,
Tigrisat
),
Flock-1c
× 11
- SPOT 7
,
CanX-4
,
CanX-5
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July
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August
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September
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October
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November
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December
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Launches are separated by dots ( ? ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights
are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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