ICEYE-X56
NORAD 64574
Payload
LEO
2025-135AY
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LEO · NORAD 64574
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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
579 km
Apogee
581 km
Inclination
97.8°
Period
96.3 min
Mean Motion
14.95619606 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude580 km
Orbital Velocity27,261 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.96
Eccentricity0.0001
Semi-Major Axis6,951 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
ICEYE (Finland)
Launch Date
2025-06-23
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-135AY
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ICEYE-X56 is an active satellite operated by ICEYE (Finland), launched on 2025-06-23 from Vandenberg SFB, California. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 579 km and 581 km with an inclination of 97.8°. It travels at approximately 27,261 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.96 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-X56 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-X56 orbits at an average altitude of 580 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-X56’s average altitude, there are currently 3,250 active payloads and 539 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 18.6% of all active satellites. With an inclination of 97.8°, ICEYE-X56 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-X56.
❓ Frequently Asked Questions
ICEYE-X56 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 580 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 96 minutes, travelling at 27,261 km/h.
ICEYE-X56 is operated by ICEYE (Finland). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 64574. You can track ICEYE-X56 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ICEYE-X56 was launched on 2025-06-23 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-X56 (NORAD ID 64574) 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-X56 travels at approximately 27,261 km/h (16,939 mph) — roughly 7.57 km/s. It completes 14.96 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.