Official name MIRATA
Alternative name MiRaTA
Cospar ID 2017-073C
Norad ID 43015
Launch date 2017-11-18
Launch site AFWTR
Launch vehicle Delta-7920-10C
Country/Organization USA
Type application Earth observation, technology
Operator Massachusetts Institute of Technology (MIT) - Lincoln Laboratory
RCS size SMALL
Decay date ON ORBIT
Period (min) 95.64
Inclination (deg) 97.6
Perigee (km) 428
Apogee (km) 672
Eccentricity 0.221818181818182
Mean motion (revs. per day) 15.0564617314931
Semi-Major axis (km) 6928.135
Raan (deg) 16.3782
Arg of perigee (deg) 31.335
Shape Box + 2 Pan
Mass (kg) 4
Height (m) 0.3
Width (m) 0.1
Depth (m) 0.1
Span (m^2) 0.3
Lifetime 90 days
Contractors Massachusetts Institute of Technology (MIT) - Lincoln Laboratory
Equipment microwave radiometer, tri-band atmospheric sounder, compact TEC (Total Electron Count) / atmospheric GPS sensor (CTAGS)
Propulsion None
Configuration CubeSat (3U)
Power 2 deployable fixed solar arrays, batteries

MiRaTA (Microwave Radiometer Technology Acceleration), is a three-unit CubeSat being developed by the MIT Lincoln Laboratory.

Mission to demonstrate a multi-band miniaturized microwave radiometer to image tropical storms, hurricanes, and cyclones, paired with an experimental calibration method using GPS radio occultation. A slow pitch up/down maneuver will be executed once per orbit to permit the radiometer and GPSRO observations to sound overlapping volumes of atmosphere through the Earth's limb, where sensitivity, calibration, and dynamic range are optimal. These observations will be compared to radiosondes, global high-resolution analysis fields, other satellite observations, and with each other using radiative transfer models.

MiRaTA mission is to:

  • Validate new ultra-compact and low-power technology for CubeSat-sized microwave radiometers operating near 52-58, 175-191, and 206-208 GHz;
  • Validate new GPS receiver and antenna array technology necessary for CubeSat tropospheric radio occultation sounding, and
  • Test a new approach to radiometer calibration using concurrent GPS radio occultation (GPSRO) measurements.

The payload consists of a microwave radiometer, a tri-band atmospheric sounder and a compact TEC (Total Electron Count) / atmospheric GPS sensor (CTAGS)

MiRaTA was selected in 2014 for launch with NASA?s ELaNa program.

It was launched on the ELaNa-14 mission.

Satellite COSPAR Date LS Launch Vehicle Remarks
MIRATA 2017-073C 2017-11-18 AFWTR Delta-7920-10C with JPSS 1, Buccaneer RMM, EagleSat, RadFxSat (Fox 1B), MakerSat 0