Official name SDO
Alternative name SDO
Cospar ID 2010-005A
Norad ID 36395
Launch date 2010-02-11
Launch site AFETR
Launch vehicle Atlas-5(401)
Country/Organization USA
Type application Solar Observatory
Operator NASA Goddard Space Flight Center
RCS size LARGE
Decay date ON ORBIT
Period (min) 1436.09
Inclination (deg) 33.04
Perigee (km) 35781
Apogee (km) 35792
Eccentricity 0.000153689240356
Mean motion (revs. per day) 1.00272267058471
Semi-Major axis (km) 42164.635
Raan (deg) 98.2146
Arg of perigee (deg) 223.4749
Shape Box + 2 Pan
Mass (kg) 3100
Height (m) 4.5
Width (m) 2.2
Depth (m) 2.2
Span (m^2) 6.5
Lifetime 5 years (design); 10 years (fuel)
Contractors NASA Goddard Space Flight Center
Equipment HMI, AIA, EVE
Propulsion R-4D
Power 2 deployable fixed solar arrays, batteries

The SDO (Solar Dynamics Observatory) solar observing satellite will be a follow up to SOHO. SDO has four main goals:

  • Research on the Solar Cycle.
  • Identify the role of the magnetic field in delivering energy to the solar atmosphere and its many layers.
  • Study how the outer regions of the Sun's atmosphere evolve over time - ranging from seconds to centuries - and space.
  • Monitor the radiation (ex: UV, EUV, etc.) levels of solar output.

SDO will contain a suite of instruments which will provide the observations that will lead to a more complete understanding of the solar dynamics that drive variability in the Earth's environment. Following instruments are mounted on the spacecraft:

  • HMI (Helioseismic and Magnetic Imager):
    The Helioseismic and Magnetic Imager will extend the capabilities of the SOHO/MDI instrument with continuous full-disk coverage at considerably higher spatial and temporal resolution line-of-sight magnetograms with the optional channel for full Stokes polarization measurements and hence vector magnetogram determination.
  • AIA (Atmospheric Imaging Assembly):
    The Atmospheric Imaging Assembly will image the solar atmosphere in multiple wavelengths to link changes to surface and interior changes.
  • EVE (Extreme Ultraviolet Variablity Experiment):
    The Extreme Ultraviolet Variablity Experiment will measure the solar Extreme-Ultraviolet (EUV) irradiance with unprecedented spectral resolution, temporal cadence, and precision.

The large data outtput (> 1 TByte/day) dictated the use of a geostationary orbit for continuous data downlink via a Ka-band transponder.

Satellite COSPAR Date LS Launch Vehicle Remarks
SDO 2010-005A 2010-02-11 AFETR Atlas-5(401)