| Mission type | Earth observation |
|---|---|
| COSPAR ID | 2023-001AW |
| SATCAT no. | 55053 |
| Website | eos |
| Mission duration | 3 years, 10 months and 4 days (in progress) |
| Spacecraft properties | |
| Manufacturer | Dragonfly Aerospace |
| Launch mass | 176.64 kg (389.4 lb) |
| Dimensions | 1130.3 х 1390 х 821 mm |
| Start of mission | |
| Launch date | 3 January 2023, 14:56:09 UTC |
| Rocket | Falcon 9 |
| Launch site | Cape Canaveral Space Force Station (CCSFS) |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth orbit |
| Perigee altitude | 516 km |
| Apogee altitude | 537 km |
| Inclination | 97.496 degrees |
| Period | 95.15 min (1 h 35 min 09 s) |
EOS SAT-1 is an optical Earth observation satellite for agricultural land monitoring by EOS Data Analytics, a satellite imagery analytics provider. The space optics instrument and satellite manufacturer Dragonfly Aerospace built the satellite and equipped it with two high-resolution DragonEye cameras. It is the first satellite within the planned EOS SAT agriculture-focused satellite constellation.
EOS SAT-1 is developed for EOS Data Analytics, a US-Ukrainian company founded by Max Polyakov. It is the first satellite within the company's planned constellation EOS SAT. It will have a daily imaging capacity of up to 1 million square kilometers and capture imagery in 11 agri-related spectral bands. Satellite cameras will produce panchromatic and multispectral images.
Once fully operational, the seven small optical EOS SAT satellites will cover up to 100% of the countries with the largest cropland and forest areas, 98.5% of such lands worldwide. The satellite constellation will monitor up to 12 million square kilometers daily.
The satellite was launched on 3 January 2023, on the SpaceX’s Transporter-6 mission. The Falcon 9 rocket lifted off from the Cape Canaveral Space Force Station (CCSFS) and launched 114 spacecraft into orbit, including the EOS SAT-1 satellite. Since the launch into low Earth orbit, the EOS SAT-1 satellite has established contact and sent telemetry and data on the status of its systems to Earth.

A single EOS SAT-1 satellite scene covers a territory that is 42 km in width and can be over 1000 km in length. The altitude of the satellite's sun-synchronous orbit is 520–560 km.
Orbit average power: 140 W.
Design lifetime: 5–7 years.
Mass: 176.6400 kg.
Bus voltage: 24.5 — 33.6 V.
GSD (ground sample distance), resolution:
Swath width: double optical payload with a 44 km swath width for an altitude of 500 km.
Spectral bands — 11 agri-related bands: