Table 2. Simulation input parameters by each payload

Inputs	AIS	EO/IR	SAR	RF
Simulation Time	Starting Time: Jan.1,2030, Duration: 7days, Timestep: 5 seconds
Ground Points	54 lattice points around Korea Peninsula (33°N–43°N, 119°E–135°E)
Orbit: Altitude	500 km, Circular Orbit
Orbit: Propagator	J2 Perturbation
Orbit: Inclination	45°	98° SSO	45°	45°
Payload: FOV	120°	60°	Incidence Angle 15° < FOV < 35°	60°
Payload Specific Characteristics	Simple Conic	Simple Conic	70° FOV Access–30° FOV Access	Formation flight of 3 SATs, receiving simultaneously
Post-Processing Strategy from Access chart	N/A	N/A (Unconstrained)	Deduct 30° FOV Contact Sequence from 70° FOV Contacts	Consider valid contact only if ≥ 3 SATs contacts single GS

AIS, automatic identification system; EO/IR, electro-optic/infra-red; SAR, synthetic aperture radar; RF, radio-frequency; SSO, sun synchronous orbit; FOV, field-of-view; SATs, satellites; GS, ground station.