Mission type | Astrophysics |
---|---|
Operator | Tokyo Metropolitan University |
Website | www |
Mission duration | 1.5 years (planned)[1] |
Spacecraft properties | |
Spacecraft type | microsatellite |
Launch mass | 46 kg[2] |
Dimensions | 46 ×46 ×44 cm [2] |
Power | 78 W[3] (solar panels) |
Start of mission | |
Launch date | ? |
Orbital parameters | |
Regime | Low Earth orbit |
Periapsis altitude | 550 km [2] |
Apoapsis altitude | 550 km |
Inclination | 3° [2] |
Period | 96 min [2] |
Epoch | planned |
Main X-ray astronomy | |
Focal length | 20 cm (7.9 in)[2] |
Wavelengths | X-ray |
Transponders | |
Band | S band[1] |
Orbiting Binary Black Hole Investigation Satellite (ORBIS) is a small space telescope still in development by Japan that will study binary black holes in the X-ray region.
The ORBIS concept won the first prize at the 18th Satellite Design Contest in 2010,[3] and of 2015 it was on preliminary design and undergoing thermal simulations by the Tokyo Metropolitan University[3][4] with support from Japan Aerospace Exploration Agency (JAXA) and the Institute of Space and Astronautical Science (ISAS).[3][1][2]
The spacecraft will have a mass of about 46 kg and it features a propulsion system using 60 wt% hydrogen peroxide.[1] Launch was aimed for 2020.[5][6][7]