EO-80

Mode :
Band :
Uplink :
Downlink :
Status :Active - Change the status :
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Latitude : °Longitude :° Altitude : km
EO-80, also known as QB50p2, is a 2U cubesat (10cm x 10cm x 20cm) built and launched as a collaborative effort led by the von Karman Institute and ISIS-BV. The primary function of the satellite is testing of the systems designed for the QB50 mission cubesats, including the Attitude Determination and Control System, Ion & Neutral Mass Spectrometer, Oxygen Flux Probe, Satellite Control Software, and the Quadpack deployer. Additionally, the satellite carries a AMSAT-F constructed repeater as a return favor for support of the use of the amateur bands for the primary QB50 mission. Unfortunately the primary transceiver was damaged during a test of the repeater, and the repeater is power negative. Further activation of the repeater is unlikely at this time.

Frequencies are as follows:

• 145.880 MHz 1k2 BPSK or CW Telemetry

• FM Voice Repeater

– 435.080 MHz 210.7 HZ PL Tone Uplink

– 145.840 MHz Downlink (also 9k6 FSK data)

Launched June 19, 2014 on a Dnepr rocket, EO-80 was placed in a 622 x 606 km sun-synchronous orbit, inclined 97.98 degrees. NORAD ID 40032, International Designation 2014-033Y

Actual Surface Range : km
Actual speed : km/s
Maximum Visibility Time : minutes


Two-Line Element set (TLE) :

EO-80
1 40032U 14033Y 19226.77458339 .00000127 00000-0 19679-4 0 9992
2 40032 097.8960 144.4295 0010687 223.4986 136.5389 14.88498878279216