SUOMI100
NORAD 43804
Payload
LEO
2018-099AY
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LEO · NORAD 43804
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
475 km
Apogee
486 km
Inclination
97.4°
Period
94.2 min
Mean Motion
15.28463082 rev/day
TLE Epoch
2026-06-19 16:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude481 km
Orbital Velocity27,459 km/h
Velocity7.63 km/s
Orbital Period94 minutes
Orbits / Day15.28
Eccentricity0.0008
Semi-Major Axis6,852 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
Aalto University (Finland)
Launch Date
2018-12-03
Launch Site
Vandenberg SFB, California
Int'l Designator
2018-099AY
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SUOMI100 is an active satellite operated by Aalto University (Finland), launched on 2018-12-03 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 475 km and 486 km with an inclination of 97.4°. It travels at approximately 27,459 km/h (7.63 km/s), completing one full orbit every 94 minutes — that’s roughly 15.28 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks SUOMI100 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SUOMI100 orbits at an average altitude of 481 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of SUOMI100’s average altitude, there are currently 8,070 active payloads and 215 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 46.3% of all active satellites. With an inclination of 97.4°, SUOMI100 passes over latitudes between 97.4°N and 97.4°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. Finland operates approximately 30 active satellites in total, of which 13 share a similar altitude band with SUOMI100.
❓ Frequently Asked Questions
SUOMI100 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 481 km altitude. Its 97.4° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 94 minutes, travelling at 27,459 km/h.
SUOMI100 is operated by Aalto University (Finland). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43804. You can track SUOMI100 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SUOMI100 was launched on 2018-12-03 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks SUOMI100 (NORAD ID 43804) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
SUOMI100 travels at approximately 27,459 km/h (17,062 mph) — roughly 7.63 km/s. It completes 15.28 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.