Official name DHABISAT
Alternative name DhabiSat
Cospar ID 2021-013F
Norad ID 49016
Launch date 2021-02-20
Launch site WLPIS
Launch vehicle Antares-230+
Country/Organization United Arab Emirates
Type application Technology, education
Operator Yahsat Space Lab, Khalifa University
RCS size SMALL
Decay date 2024-01-17
Shape Box
Mass (kg) 4
Height (m) 0.3
Width (m) 0.1
Depth (m) 0.1
Span (m^2) 0.3
Contractors Yahsat Space Lab, Khalifa University
Equipment Camera
Propulsion None
Configuration CubeSat (2U)
Power Solar cells, batteries

DhabiSat or MYSAT 2 is an 2U CubeSat eductional mission, developed by Khalifa University students with support from Al Yah Satellite Company (Yahsat) and Northrop Grumman.

The primary mission of the second CubeSat, previously known as MYSat-2, is to enable students to design, implement, and test software modules for attitude determination and control systems (ADCS). The work has been conducted at the Yahsat Space Lab, which is part of the Khalifa University Space Technology and Innovation Center (KUSTIC).

DhabiSat will assess the accuracy of various ADCS pointing control strategies and validate the same by taking images using a digital camera onboard pointed in specific directions. The new ADCS algorithms shall improve the pointing accuracy of the CubeSat and its response time to attitude changes as compared to conventional algorithms. In terms of system resources, DhabiSat will require less power to achieve the targeted pointings and if successful, the algorithms will gain flight heritage on board DhabiSat, which then can be used as a baseline in future CubeSat missions.

The satellite was launched on board of the Cygnus CRS-15 cargo mission and was deployed on 29 June 2021 from the spacecrafts external deployer after departing from the ISS.

Satellite COSPAR Date LS Launch Vehicle Remarks
DHABISAT 2021-013F 2021-02-20 WLPIS Antares-230+ with Cygnus CRS-15, Lawkanat 1, Gunsmoke-J 2, ORCA 6, ORCA 7, IT-SPINS, TAU-SAT 1, STARS-EC, OPUSAT 2, RSP 01, WARP 01, Maya 2, Guaranisat 1, Tsuru, ThinSat 2A, ..., 2I