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ICEYE-X31

NORAD 58288 Payload LEO 2023-174AJ ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
462 km
Apogee
464 km
Inclination
97.4°
Period
93.8 min
Mean Motion
15.34359997 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude463 km
Orbital Velocity27,494 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.34
Eccentricity0.0001
Semi-Major Axis6,834 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
ICEYE (Finland)
Launch Date
2023-11-11
Launch Site
Vandenberg SFB, California
Int'l Designator
2023-174AJ
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ICEYE-X31 is an active satellite operated by ICEYE (Finland), launched on 2023-11-11 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 462 km and 464 km with an inclination of 97.4°. It travels at approximately 27,494 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.34 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 ICEYE-X31 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ICEYE-X31 orbits at an average altitude of 463 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 ICEYE-X31’s average altitude, there are currently 7,982 active payloads and 179 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 45.8% of all active satellites. With an inclination of 97.4°, ICEYE-X31 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 10 share a similar altitude band with ICEYE-X31.
❓ Frequently Asked Questions
ICEYE-X31 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 463 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 27,494 km/h.
ICEYE-X31 is operated by ICEYE (Finland). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58288. You can track ICEYE-X31 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ICEYE-X31 was launched on 2023-11-11 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 ICEYE-X31 (NORAD ID 58288) 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.
ICEYE-X31 travels at approximately 27,494 km/h (17,084 mph) — roughly 7.64 km/s. It completes 15.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.