ICEYE-X36
NORAD 59103
Payload
LEO
2024-043F
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LEO · NORAD 59103
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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
542 km
Apogee
549 km
Inclination
97.8°
Period
95.6 min
Mean Motion
15.06882133 rev/day
TLE Epoch
2026-06-19 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude546 km
Orbital Velocity27,329 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.07
Eccentricity0.0005
Semi-Major Axis6,917 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 ICEYE (United States)
Launch Date
2024-03-04
Launch Site
Vandenberg SFB, California
Int'l Designator
2024-043F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ICEYE-X36 is an active satellite operated by ICEYE (United States), launched on 2024-03-04 from Vandenberg SFB, California. It orbits in Low Earth Orbit (LEO) at altitudes between 542 km and 549 km with an inclination of 97.8°. It travels at approximately 27,329 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.07 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-X36 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-X36 orbits at an average altitude of 546 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-X36’s average altitude, there are currently 3,512 active payloads and 349 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 97.8°, ICEYE-X36 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. United States operates approximately 12,360 active satellites in total, of which 2,821 share a similar altitude band with ICEYE-X36.
❓ Frequently Asked Questions
ICEYE-X36 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 546 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 27,329 km/h.
ICEYE-X36 is operated by ICEYE (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59103. You can track ICEYE-X36 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ICEYE-X36 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-X36 (NORAD ID 59103) 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-X36 travels at approximately 27,329 km/h (16,982 mph) — roughly 7.59 km/s. It completes 15.07 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.