Official name DMSAT-1
Alternative name DMSat-1
Cospar ID 2021-022J
Norad ID 47940
Launch date 2021-03-22
Launch site TTMTR
Launch vehicle Soyuz-2-1a Fregat
Country/Organization United Arab Emirates
Type application Earth observation
Operator EIAST
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 94.26
Inclination (deg) 97.47
Perigee (km) 476
Apogee (km) 489
Eccentricity 0.0134715025906736
Mean motion (revs. per day) 15.2768936982813
Semi-Major axis (km) 6860.635
Raan (deg) 32.8306
Arg of perigee (deg) 247.6807
Shape Box
Mass (kg) 15
Height (m) 0.4
Width (m) 0.2
Depth (m) 0.2
Span (m^2) 0.4
Contractors UTIAS
Configuration Nemo-V1 bus
Power Solar cells, batteries

The DMSat-1 satellite is a 15-kilogram earth-monitoring microsatellite developed by the Space Flight Laboratory (SFL) for the Mohammend Bin Rashid Space Centre (MBRSC) in Dubai.

SFL?s Next-generation Earth Monitoring and Observation (NEMO) platform technology, which incorporates high performance ground target tracking capability, is a key enabler for the mission.

DMSat-1 leverages past developments at SFL for a rapidly developed mission that will incorporate two payloads. It is based on the NEMO-AM satellite. The primary payload is a multispectral polarimeter used to monitor aerosols ? fine particles of liquid and solids in the upper atmosphere normally caused by man-made sources, but also correlating to natural phenomena such as dust storms. The secondary instrument is a pair of spectrometers that will enable MBRSC to detect greenhouse gases like carbon dioxide and methane over the United Arab Emirates.

Satellite COSPAR Date LS Launch Vehicle Remarks
DMSAT-1 2021-022J 2021-03-22 TTMTR Soyuz-2-1a Fregat with CAS500 1, ELSA-d Servicer, ELSA-d Client, GRUS 1B, ..., 1E, Najm 1, UniSat 7, BCCSAT 1, FEES, DIY 1, SMOG 1, STECCO, SAMSON 1, 2, 3, Kepler 6, 7, NanoSatC-Br 2, KMSL, CANYVAL-C 1, 2, BeeSat 5, ..., 8, Hiber 3, CubeSX-HSE, CubeSX-Sirius-HSE, Orbicraft-Zorkiy, WildTrackCube-SIMBA, GRBAlpha, 3B5GSAT, LacunaSat 2b, ChallengeOne, KSU-Cubesat