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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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
ArkEdge
Mission
Operational Commercial Technology
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: 10 hours ago
TLE from 10 hours ago
0 AE3VA
1 64563U 25135AM 25328.30115248 .00008024 00000-0 76331-3 0 9991
2 64563 97.7555 80.1938 0002191 217.8945 142.2121 14.93697499 23315Epoch: 2025-11-24T07:13Z
TLE epoch observation values (Epoch: 2025-11-24T07:13:39.574Z)
Latitude
0°
Longitude
-91.72418°
Altitude
590.669 km
Speed
7.564 km/s
True Right ascension
05h 20m 46s
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
14:23:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.96 km
Perigee altitude
581.909 km
Semi-major axis
6,961.572 km
Eccentricity
0.00022
Inclination
97.7555°
RAAN
80.1938°
Arg. of periapsis
217.8945°
True anomaly
142.22748°
Mean anomaly
142.2121°
Eccentric anomaly
142.21979°
Mean motion
3.73665 °/min
Orbital period
96.34 mins
BSTAR
0.00076331
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-24 20:39:22.325Z | 5.974° NNE | 2025-11-24 20:42:22.325Z | 315.962° NNW | 42.576° | 2025-11-24 20:46:22.325Z | 202.011° SSW |
| 6 mins | 2025-11-25 07:29:22.325Z | 152.678° SSE | 2025-11-25 07:31:22.325Z | 93.361° ESE | 42.92° | 2025-11-25 07:35:22.325Z | 353.115° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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