MISSION DESIGNER
Define your mission, configure your satellite, compare launch options, and review your design summary.
Early screening only. Verify launch performance, component limits, and ground segment assumptions against the latest public specifications from launch providers, vendors, and ground station operators before any real mission decision.
1
Mission
2
Config
3
Analysis
4
Launch
5
Summary
ORBIT
Orbit type
Altitude
550km
SSO recommended: 500–700 km
Inclination
97.4deg
Eccentricity
0.001
BUS
Total mass
120kg
Optical EO typical: 80–200 kg
Solar panels
4.0m²
Battery
240Wh
Design life
5yr
COMMUNICATIONS
Downlink band
TX power
10W
Ant. gain
18dBi
Ground station
G/T
10m, G/T 28 dB/K
PAYLOAD
Payload mass
35kg
Peak power
60W
Duty cycle
30%
Data rate
150Mbps
Ranked by payload margin to target orbit. Rideshare-capable vehicles are prioritized for cost efficiency.
ORBITSMITH — MISSION SUMMARY
SYS:NOMINALOPTICAL EO · 120 KGSSO 550 KM · 97.4°