ICEYE-X62
NORAD 66755
Payload
LEO
2025-276CT
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LEO · NORAD 66755
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
534 km
Apogee
538 km
Inclination
97.4°
Period
95.4 min
Mean Motion
15.10034561 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude536 km
Orbital Velocity27,348 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.10
Eccentricity0.0003
Semi-Major Axis6,907 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
ICEYE (Poland)
Launch Date
2025-11-28
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-276CT
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ICEYE-X62 is an active satellite operated by ICEYE (Poland), launched on 2025-11-28 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 534 km and 538 km with an inclination of 97.4°. It travels at approximately 27,348 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.10 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-X62 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-X62 orbits at an average altitude of 536 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-X62’s average altitude, there are currently 3,494 active payloads and 316 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 20.1% of all active satellites. With an inclination of 97.4°, ICEYE-X62 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. Poland operates approximately 12 active satellites in total, of which 6 share a similar altitude band with ICEYE-X62.
❓ Frequently Asked Questions
ICEYE-X62 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 536 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 95 minutes, travelling at 27,348 km/h.
ICEYE-X62 is operated by ICEYE (Poland). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 66755. You can track ICEYE-X62 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ICEYE-X62 was launched on 2025-11-28 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-X62 (NORAD ID 66755) 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-X62 travels at approximately 27,348 km/h (16,993 mph) — roughly 7.60 km/s. It completes 15.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.