LARES Mission

Objectives and Applications

Scientific objectives are the measurement of the dragging of inertial frames due to the Earth's angular momentum, or Lense-Thirring effect, and a high precision test of the Earth's gravitomagnetic field with accuracy of the order of a few percent. Gravitomagnetic field and dragging of inertial frames are predictions of Einstein's theory of General Relativity. In addition, LARES will allow other measurements in geodesy and geodynamics.

Mission Summary

Full Name
LAser RElativity Satellite
Mission Status
Operational (nominal)
Mission Agencies
ASI
Launch Date
13 Feb 2012
Mission Links
EOL Date
Feb 2052
EO Portal Info

Orbit Details

Orbit Type
Inclined, non-sun-synchronous
Orbit Period
99.1 minutes
Orbit Sense
Ascending
Orbit Inclination
71 deg
Orbit Altitude
1450 km
Orbit Longitude
Orbit LST
Repeat Cycle
NORAD Catalog #
International Designator

Mission Instruments

LCCRA (LARES) - Laser Corner Cube Reflector Assembly

Mission Measurements

CategoryParameterInstrument(s)
Gravity and Magnetic FieldsGravity, Magnetic and Geodynamic measurements LCCRA (LARES)