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 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 26036.28278436 .00012890 00000-0 11758-2 0 9991
2 64563 97.7557 152.3040 0002476 14.8481 345.2812 14.95222726 34211Epoch: 2026-02-05T06:47Z
TLE epoch observation values (Epoch: 2026-02-05T06:47:12.568Z)
Latitude
-0.00003°
Longitude
-84.9356°
Altitude
583.061 km
Speed
7.57 km/s
True Right ascension
10h 09m 12s
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
14:08:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.418 km
Perigee altitude
576.973 km
Semi-major axis
6,956.833 km
Eccentricity
0.00025
Inclination
97.7557°
RAAN
152.304°
Arg. of periapsis
14.8481°
True anomaly
345.27399°
Mean anomaly
345.2812°
Eccentric anomaly
345.27759°
Mean motion
3.74047 °/min
Orbital period
96.24 mins
BSTAR
0.0011758
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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 | 2026-02-05 20:12:00.657Z | 23.433° NE | 2026-02-05 20:16:00.657Z | 120.603° SE | 38.055° | 2026-02-05 20:19:00.657Z | 175.342° S |
| 5 mins | 2026-02-06 07:02:00.657Z | 117.622° SE | 2026-02-06 07:04:00.657Z | 70.403° E | 27.691° | 2026-02-06 07:07:00.657Z | 12.718° NNE |
| 4 mins | 2026-02-06 08:38:00.657Z | 240.516° WSW | 2026-02-06 08:39:00.657Z | 258.665° W | 17.744° | 2026-02-06 08:42:00.657Z | 308.769° NW |
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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