SIMBA (original) (raw)

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SIMBA [Royal Meteorological Institute of Belgium]

SIMBA (Sun-earth Imbalance) is a Belgian 3U CubeSat, designed by the Royal Meteorological Institute of Belgiumw ith the participation of the Royal Meteorological Institute of Belgium, the University of Leuven and ISIS-Innovative Solutions In Space as a technology demonstration mission.

The satellite will have three objectives:

The satellite was to be originally part of the QB50 constellation, but dropped out later. Launch into a sun synchroneous orbit is now planned for 2018.

Nation: Belgium
Type / Application: Technology
Operator: Royal Meteorological Institute of Belgium
Contractors: Royal Meteorological Institute of Belgium; ISIS (bus)
Equipment:
Configuration: CubeSat (3U)
Propulsion: None
Power: 2 deployable fixed solar arrays, solar cells, batteries
Lifetime:
Mass: 4 kg
Orbit: 534 km � 536 km, 97.52�
Satellite COSPAR Date LS Launch Vehicle Remarks
SIMBA (ex QB50 BE02) 2020-061H 03.09.2020 Ko ELV Vega with Athena, ION-SCV 1, ESAIL, UPMSat 2, NEMO-HD, �uSat 6, GHGSat C1, Flock-4v 1, ..., 26, Lemur-2 112, ..., 119, SpaceBEE 10, ..., 21, FSSCat A, B, NAPA 1, TARS, EG 2, OSM 1 CICERO, DIDO 3, PICASSO, TRISAT, AMICal-Sat, TT�100

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