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: 11 hours ago
TLE from 11 hours ago
0 AE3VA
1 64563U 25135AM 26133.13151262 .00004494 00000-0 39828-3 0 9990
2 64563 97.7632 248.2661 0003339 60.9430 299.2126 14.96731480 48690Epoch: 2026-05-13T03:09Z
TLE epoch observation values (Epoch: 2026-05-13T03:09:22.690Z)
Latitude
0.00002°
Longitude
-29.97438°
Altitude
578.919 km
Speed
7.572 km/s
True Right ascension
16h 33m 03s
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
22:52:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.337 km
Perigee altitude
571.695 km
Semi-major axis
6,952.153 km
Eccentricity
0.00033
Inclination
97.7632°
RAAN
248.2661°
Arg. of periapsis
60.943°
True anomaly
299.1792°
Mean anomaly
299.2126°
Eccentric anomaly
299.1959°
Mean motion
3.74424 °/min
Orbital period
96.15 mins
BSTAR
0.00039828
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-13 19:47:13.471Z | 47.94° ENE | 2026-05-13 19:50:13.471Z | 107.278° ESE | 22.352° | 2026-05-13 19:52:13.471Z | 142.919° SSE |
| 4 mins | 2026-05-13 21:23:13.471Z | 325.95° NNW | 2026-05-13 21:25:13.471Z | 283.199° WNW | 21.993° | 2026-05-13 21:27:13.471Z | 246.703° WSW |
| 6 mins | 2026-05-14 08:10:13.471Z | 201.391° SSW | 2026-05-14 08:12:13.471Z | 243.413° WSW | 31.458° | 2026-05-14 08:16:13.471Z | 330.086° 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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