Mission type | Technology demonstration |
---|---|
Operator | Terran Orbital [1] |
COSPAR ID | 2017-042V |
Website | tyvak.eu/missions/nanoace |
Spacecraft properties | |
Spacecraft type | CubeSat (3U) [2] |
Manufacturer | Tyvak Nano-Satellite Systems |
Launch mass | 5.2 kg (11 lb) [1] |
Dimensions | 30 cm × 10 cm × 10 cm (11.8 in × 3.9 in × 3.9 in) [2] |
Power | 4 deployable solar panels |
Start of mission | |
Launch date | July 14, 2017, 7:36am UTC [3] |
Rocket | Soyuz-2.1a |
Launch site | Baikonur Cosmodrome |
Contractor | Roscosmos |
Orbital parameters | |
Regime | Low Earth Orbit [4] |
Periapsis altitude | 566.9 km (352.3 mi) [5] |
Apoapsis altitude | 581.5 km (361.3 mi) [5] |
Inclination | 97.4° [5] |
Period | 96 minuets [5] |
NanoACE is a technology demonstration CubeSat by Tyvak Nano-Satellite Systems to validate their communications, navigation, guidance, and software technology. [1] [6] NanoACE was launched onboard a Soyuz-2.1a Fregat-M, on July 14, 2017, along with Russian Earth imaging satellite Kanopus-V-IK and 71 other CubeSats. [7]
The satellite has two Infrared and two visible light cameras. [6] It can maneuver via its cold gas propulsion system. [2] [6]