Skip to content
Home Library Satellite Directory AE1D

AE1D

NORAD 62618 Payload LEO 2025-009K ● Active
CONNECTING… LEO · NORAD 62618
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
278 km
Apogee
290 km
Inclination
97.4°
Period
90.2 min
Mean Motion
16.02223145 rev/day
TLE Epoch
2026-09-17 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude284 km
Orbital Velocity27,861 km/h
Velocity7.74 km/s
Orbital Period90 minutes
Orbits / Day16.02
Eccentricity0.0009
Semi-Major Axis6,655 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeWeeks to months
🚀 Launch & Identity
Country / Operator
🇯🇵 ArkEdge (Japan)
Launch Date
2025-01-14
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2025-009K
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
AE1D is an active satellite operated by ArkEdge (Japan), launched on 2025-01-14 from Vandenberg Space Force Base, United States on the Transporter-12 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 278 km and 290 km with an inclination of 97.4°. It travels at approximately 27,861 km/h (7.74 km/s), completing one full orbit every 90 minutes — that’s roughly 16.02 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 weeks to months. Orbital Radar tracks AE1D in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
AE1D orbits at an average altitude of 284 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 AE1D’s average altitude, there are currently 206 active payloads and 15 tracked debris or rocket body fragments — notable neighbours include STARLINK-1036, STARLINK-1048, STARLINK-1068. With an inclination of 97.4°, AE1D 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 208 active satellites in total, of which 2 share a similar altitude band with AE1D.
❓ Frequently Asked Questions
AE1D is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 284 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 90 minutes, travelling at 27,861 km/h.
AE1D is operated by ArkEdge (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 62618. You can track AE1D in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
AE1D was launched on 2025-01-14 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: weeks to months. View the full satellite launch log.
Yes — Orbital Radar tracks AE1D (NORAD ID 62618) 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.
AE1D travels at approximately 27,861 km/h (17,312 mph) — roughly 7.74 km/s. It completes 16.02 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.