ICEYE-X81
NORAD 69889
Payload
LEO
2026-156W
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LEO · NORAD 69889
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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
588 km
Apogee
598 km
Inclination
97.8°
Period
96.5 min
Mean Motion
14.91476104 rev/day
TLE Epoch
2026-07-28 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude593 km
Orbital Velocity27,236 km/h
Velocity7.57 km/s
Orbital Period97 minutes
Orbits / Day14.91
Eccentricity0.0007
Semi-Major Axis6,964 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇺🇸 ICEYE (United States)
Launch Date
2026-07-07
Launch Site
Vandenberg SFB, California
Int'l Designator
2026-156W
Object Type
Payload
RCS Size
Unknown
📖 About This Object
ICEYE-X81 is an active satellite operated by ICEYE (United States), launched on 2026-07-07 from Vandenberg SFB, California on the Transporter-17 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 588 km and 598 km with an inclination of 97.8°. It travels at approximately 27,236 km/h (7.57 km/s), completing one full orbit every 97 minutes — that’s roughly 14.91 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-X81 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-X81 orbits at an average altitude of 593 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-X81’s average altitude, there are currently 2,075 active payloads and 618 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 11.7% of all active satellites. With an inclination of 97.8°, ICEYE-X81 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 12,550 active satellites in total, of which 1,507 share a similar altitude band with ICEYE-X81.
❓ Frequently Asked Questions
ICEYE-X81 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 593 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 97 minutes, travelling at 27,236 km/h.
ICEYE-X81 is operated by ICEYE (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69889. You can track ICEYE-X81 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ICEYE-X81 was launched on 2026-07-07 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-X81 (NORAD ID 69889) 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-X81 travels at approximately 27,236 km/h (16,924 mph) — roughly 7.57 km/s. It completes 14.91 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.