Generated Narrative: Observation Observation.Kepler.ECI.1

status: Final

code: Satellite Observation

method: Earth Centered Inertial

component

code: Eccentricity

value: 0.6

component

code: Semimajor Axis

value: 2.7

component

code: Angle of Inclination

value: 53 deg

component

code: Longitude of the ascending node

value: 0 deg

component

code: Argument of Periapsis

value: 22.1 deg

component

code: True anomaly

value: 30 s