AE3VA, 64563
Orbit data source: Space-Track
AE3VA, 64563 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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64563 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
ArkEdge
Mission
Operational Commercial Communications
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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 AE3VA
1 64563U 25135AM 26132.19555741 .00004181 00000-0 37099-3 0 9996
2 64563 97.7629 247.3371 0003319 62.6108 297.5450 14.96723627 48553Epoch: 2026-05-12T04:41Z
TLE epoch observation values (Epoch: 2026-05-12T04:41:36.160Z)
Latitude
-0.00009°
Longitude
-53.03697°
Altitude
579.009 km
Speed
7.572 km/s
True Right ascension
16h 29m 20s
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
17:38:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.348 km
Perigee altitude
571.733 km
Semi-major axis
6,952.177 km
Eccentricity
0.00033
Inclination
97.7629°
RAAN
247.3371°
Arg. of periapsis
62.6108°
True anomaly
297.51127°
Mean anomaly
297.545°
Eccentric anomaly
297.52814°
Mean motion
3.74422 °/min
Orbital period
96.15 mins
BSTAR
0.00037099
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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.AE3VA 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-12 19:42:37.699Z | 43.604° NE | 2026-05-12 19:45:37.699Z | 92.824° ESE | 20.903° | 2026-05-12 19:48:37.699Z | 144.587° SSE |
| 5 mins | 2026-05-12 21:18:37.699Z | 336.554° NNW | 2026-05-12 21:20:37.699Z | 298.122° NW | 23.827° | 2026-05-12 21:23:37.699Z | 239.49° WSW |
| 5 mins | 2026-05-13 08:06:37.699Z | 201.668° SSW | 2026-05-13 08:08:37.699Z | 257.87° W | 34.737° | 2026-05-13 08:11:37.699Z | 328.539° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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