Mode :
Band :
Uplink :
Downlink :
Status :Active - Change the status :
6 Mar5 Mar4 Mar3 Mar2 Mar

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) :

1 40032U 14033Y 21063.34454512 .00000517 00000-0 61121-4 0 9998
2 40032 97.9136 350.6501 0012248 155.2506 204.9300 14.88861125363652