ICEYE-X39
NORAD 60546
Payload
LEO
2024-149CG
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LEO · NORAD 60546
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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
557 km
Apogee
575 km
Inclination
97.7°
Period
96.0 min
Mean Motion
15.00262808 rev/day
TLE Epoch
2026-11-01 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude566 km
Orbital Velocity27,289 km/h
Velocity7.58 km/s
Orbital Period96 minutes
Orbits / Day15.00
Eccentricity0.0013
Semi-Major Axis6,937 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇧🇷 FAB / ICEYE (Brazil)
Launch Date
2024-08-16
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2024-149CG
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ICEYE-X39 is an active satellite operated by FAB / ICEYE (Brazil), launched on 2024-08-16 from Vandenberg Space Force Base, United States on the Transporter-11 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 557 km and 575 km with an inclination of 97.7°. It travels at approximately 27,289 km/h (7.58 km/s), completing one full orbit every 96 minutes — that’s roughly 15.00 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks ICEYE-X39 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-X39 orbits at an average altitude of 566 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-X39’s average altitude, there are currently 1,083 active payloads and 512 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 5.7% of all active satellites. With an inclination of 97.7°, ICEYE-X39 passes over latitudes between 97.7°N and 97.7°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. Brazil operates approximately 31 active satellites in total, of which 2 share a similar altitude band with ICEYE-X39.
❓ Frequently Asked Questions
ICEYE-X39 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 566 km altitude. Its 97.7° 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 27,289 km/h.
ICEYE-X39 is operated by FAB / ICEYE (Brazil). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 60546. You can track ICEYE-X39 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ICEYE-X39 was launched on 2024-08-16 from Vandenberg Space Force Base, United States, 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-X39 (NORAD ID 60546) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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-X39 travels at approximately 27,289 km/h (16,957 mph) — roughly 7.58 km/s. It completes 15.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.