AE2A
NORAD 64591
Payload
LEO
2025-135BR
● Active
CONNECTING…
LEO · NORAD 64591
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
573 km
Apogee
579 km
Inclination
97.8°
Period
96.2 min
Mean Motion
14.97145630 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude576 km
Orbital Velocity27,269 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.97
Eccentricity0.0004
Semi-Major Axis6,947 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2025-06-23
Launch Site
Vandenberg SFB, California
Int'l Designator
2025-135BR
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
AE2A is an active satellite operated by Japan, launched on 2025-06-23 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 573 km and 579 km with an inclination of 97.8°. It travels at approximately 27,269 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.97 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 AE2A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
AE2A orbits at an average altitude of 576 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 AE2A’s average altitude, there are currently 3,104 active payloads and 515 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-2112, STARLINK-2722. This makes it one of the more crowded altitude bands, containing roughly 17.8% of all active satellites. With an inclination of 97.8°, AE2A 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. Japan operates approximately 189 active satellites in total, of which 40 share a similar altitude band with AE2A.
❓ Frequently Asked Questions
AE2A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 576 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 27,269 km/h.
AE2A is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 64591. You can track AE2A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AE2A was launched on 2025-06-23 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 AE2A (NORAD ID 64591) 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.
AE2A travels at approximately 27,269 km/h (16,944 mph) — roughly 7.57 km/s. It completes 14.97 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.