AE5RB
NORAD 66693
Payload
LEO
2025-276AD
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LEO · NORAD 66693
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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
495 km
Apogee
500 km
Inclination
97.4°
Period
94.6 min
Mean Motion
15.22847069 rev/day
TLE Epoch
2026-06-19 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude498 km
Orbital Velocity27,425 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.23
Eccentricity0.0004
Semi-Major Axis6,869 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2025-11-28
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-276AD
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
AE5RB is an active satellite operated by Japan, 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 495 km and 500 km with an inclination of 97.4°. It travels at approximately 27,425 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.23 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 ~1–3 years. Orbital Radar tracks AE5RB in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
AE5RB orbits at an average altitude of 498 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 AE5RB’s average altitude, there are currently 9,156 active payloads and 242 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 52.5% of all active satellites. With an inclination of 97.4°, AE5RB 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. Japan operates approximately 189 active satellites in total, of which 31 share a similar altitude band with AE5RB.
❓ Frequently Asked Questions
AE5RB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 498 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 27,425 km/h.
AE5RB is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 66693. You can track AE5RB in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AE5RB 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: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks AE5RB (NORAD ID 66693) 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.
AE5RB travels at approximately 27,425 km/h (17,041 mph) — roughly 7.62 km/s. It completes 15.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.