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BEEAGLESAT

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BEEAGLESAT is classified as:


NORAD ID: 42736
Int'l Code: 1998-067MR
Perigee: 324.8 km
Apogee: 328.3 km
Inclination: 51.6 °
Period: 90.9 minutes
Semi major axis: 6697 km
RCS: Unknown
Launch date: November 20, 1998
Source: Turkey (TURK)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

Uplink (MHz):
Downlink (MHz): 437.370
Beacon (MHz):
Mode: 9600bps GMSK
Call sign: ON01TR
Status: Active


BEEAGLESAT is a 2U CubeSat launched within the EU FP7 project QB 50, manufactured by Istanbul Technical University and Turkish Air Force Academy. The X-ray detector utilizes cross strip geometry to test the detection system in space, but it does not carry a mask for imaging. The readout is established by an application specific integrated circuit controlled by a microcontroller. The system has its own battery and is turned on intermittently due to power and telemetry constraints. The satellite measures the hard X-ray background in 20-150 keV at low Earth orbit conditions as a function of altitude. As a payload for QB50, the satellite carries a multineedle Langmuir probe (mNLP) sampling the electron density of the space around it.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1 42736U 98067MR  19022.18834249  .00047859  00000-0  21216-3 0  9993
2 42736  51.6308 312.2738 0002629  24.9442 335.1688 15.83892365 94947
Source of the keplerian elements: AMSAT