ICEYE-X38
NORAD 59100
Payload
LEO
2024-043C
● Active
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LEO · NORAD 59100
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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
525 km
Apogee
530 km
Inclination
97.8°
Period
95.2 min
Mean Motion
15.12874671 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude528 km
Orbital Velocity27,365 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.13
Eccentricity0.0004
Semi-Major Axis6,899 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
ICEYE (Finland)
Launch Date
2024-03-04
Launch Site
Vandenberg SFB, California
Int'l Designator
2024-043C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ICEYE-X38 is an active satellite operated by ICEYE (Finland), launched on 2024-03-04 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 525 km and 530 km with an inclination of 97.8°. It travels at approximately 27,365 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.13 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 ~3–10 years. Orbital Radar tracks ICEYE-X38 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-X38 orbits at an average altitude of 528 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-X38’s average altitude, there are currently 6,788 active payloads and 286 tracked debris or rocket body fragments — notable neighbours include STARLINK-1039, STARLINK-1184, STARLINK-1231. This makes it one of the more crowded altitude bands, containing roughly 38.9% of all active satellites. With an inclination of 97.8°, ICEYE-X38 passes over latitudes between 97.8°N and 97.8°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 12 share a similar altitude band with ICEYE-X38.
❓ Frequently Asked Questions
ICEYE-X38 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 528 km altitude. Its 97.8° 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 95 minutes, travelling at 27,365 km/h.
ICEYE-X38 is operated by ICEYE (Finland). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59100. You can track ICEYE-X38 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ICEYE-X38 was launched on 2024-03-04 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks ICEYE-X38 (NORAD ID 59100) 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-X38 travels at approximately 27,365 km/h (17,004 mph) — roughly 7.60 km/s. It completes 15.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.