Official name MEZNSAT
Alternative name MeznSat
Cospar ID 2020-068D
Norad ID 46489
Launch date 2020-09-28
Launch site PKMTR
Launch vehicle Soyuz-2-1b Fregat
Country/Organization United Arab Emirates
Type application Earth observation
Operator Khalifa University of Science and Technology (KUST), American University of Ras Al-Khaimah (AURAK)
RCS size SMALL
Decay date ON ORBIT
Period (min) 94.46
Inclination (deg) 97.81
Perigee (km) 482
Apogee (km) 502
Eccentricity 0.0203252032520325
Mean motion (revs. per day) 15.2445479568071
Semi-Major axis (km) 6870.135
Raan (deg) 95.1112
Arg of perigee (deg) 72.9518
Shape Box
Mass (kg) 5
Height (m) 0.3
Width (m) 0.1
Depth (m) 0.1
Contractors Khalifa University of Science and Technology (KUST), American University of Ras Al-Khaimah (AURAK)
Equipment Argus-2000 SWIR spectrometer, HD camera
Propulsion None
Configuration CubeSat (3U)
Power Solar cells, batteries

MeznSat is a 3U CubeSat that will carry a shortwave infrared (SWIR) micro-spectrometer as its primary payload, with the aim of deriving greenhouse gas concentrations in the atmosphere by making observations in the 1000?1650 nm wavelength region.

Climate change and global warming are attributed to the increased levels of greenhouse Gases in the atmosphere. Miniature low-cost, lightweight instruments on-board low-cost nanosatellite platforms such as CubeSats could be used to provide precise measurements of greenhouse gases levels. CubeSats, which usually have a narrow field of view, cost a fraction of what more expensive satellites with wide swaths cost.

The satellite, which is planned for launch in March 2020, is the result of a collaborative project between Khalifa University of Science and Technology (KUST) and the American University of Ras Al-Khaimah (AURAK) with a fund from the United Arab Emirates Space Agency (UAE-SA).

The primary payload, Argus 2000, is a miniature, low-cost, space-qualified spectrometer that operates in the shortwave infrared (SWIR) bands. Argus 2000 is a ruggedized unit with a mass of less than 230 g and power consumption of less than 1 W. Also, the Argus 2000 has 0.15 degrees viewing angle and 15 mm fore-optics.

The secondary payload will consist of a high definition (HD) camera that will allow post-processing to achieve the high geolocation accuracy required for the SWIR spectrometer data. The RGB combination of visible and SWIR bands setup makes MeznSat a unique CubeSat mission that will generate an interesting dataset to explore atmospheric correction algorithms, which employ SWIR data to process visible channels.

Satellite COSPAR Date LS Launch Vehicle Remarks
MEZNSAT 2020-068D 2020-09-28 PKMTR Soyuz-2-1b Fregat with Gonets-M 17, Gonets-M 18, Gonets-M 19, ICEYE X6, ICEYE X7, SALSAT, Kepler 4, 5, Dekart, Norbi, Lemur-2 120, ..., 123, NetSat 1, ..., 4, LacunaSat 3, Yarilo 1, 2