AE2A, 64591
Orbit data source: Space-Track
AE2A, 64591 is a payload satellite owned by ArkEdge (JP) in SSO that was launched on Mon, 23 Jun 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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64591 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
ArkEdge
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 AE2A
1 64591U 25135BR 26225.15786406 .00001594 00000-0 14149-3 0 9996
2 64591 97.7737 340.0578 0006422 129.9278 230.2509 14.97578823 62481Epoch: 2026-08-13T03:47Z
TLE epoch observation values (Epoch: 2026-08-13T03:47:19.454Z)
Latitude
-0.00005°
Longitude
-38.37472°
Altitude
580.286 km
Speed
7.569 km/s
True Right ascension
22h 40m 13s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
00:30:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.855 km
Perigee altitude
566.929 km
Semi-major axis
6,949.529 km
Eccentricity
0.00064
Inclination
97.7737°
RAAN
340.0578°
Arg. of periapsis
129.9278°
True anomaly
230.19435°
Mean anomaly
230.2509°
Eccentric anomaly
230.22262°
Mean motion
3.74637 °/min
Orbital period
96.09 mins
BSTAR
0.00014149
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Other satellites on launch #135 in the year 2025 (2025-06-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.AE2A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-13 20:23:24.616Z | 21.186° NNE | 2026-08-13 20:26:24.616Z | 65.928° ENE | 39.593° | 2026-08-13 20:30:24.616Z | 180.607° SSW |
| 5 mins | 2026-08-14 07:12:24.616Z | 118.471° SE | 2026-08-14 07:14:24.616Z | 64.598° ENE | 29.492° | 2026-08-14 07:17:24.616Z | 9.242° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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