MISSION DESIGNER
Define your mission, configure your satellite, analyze feasibility, find a ride to orbit, and review your complete design summary.
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°