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 Civil 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, 1.0 m
Radar Cross Section
0.683 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 AE3VA
1 64563U 25135AM 25269.25634163 .00013982 00000-0 13735-2 0 9998
2 64563 97.7510 22.0060 0003474 83.9778 276.1837 14.92265511 14505Epoch: 2025-09-26T06:09Z
TLE epoch observation values (Epoch: 2025-09-26T06:09:07.916Z)
Latitude
-0.00003°
Longitude
-75.5827°
Altitude
593.656 km
Speed
7.563 km/s
True Right ascension
01h 28m 01s
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
15:13:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.311 km
Perigee altitude
585.471 km
Semi-major axis
6,966.028 km
Eccentricity
0.00035
Inclination
97.751°
RAAN
22.006°
Arg. of periapsis
83.9778°
True anomaly
276.14412°
Mean anomaly
276.1837°
Eccentric anomaly
276.16391°
Mean motion
3.73306 °/min
Orbital period
96.44 mins
BSTAR
0.0013735
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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 | 2025-09-27 08:02:05.238Z | 195.436° SSW | 2025-09-27 08:04:05.238Z | 237.694° WSW | 34.759° | 2025-09-27 08:08:05.238Z | 332.927° NNW |
| 5 mins | 2025-09-27 19:46:05.238Z | 60.566° ENE | 2025-09-27 19:48:05.238Z | 105.325° ESE | 23.239° | 2025-09-27 19:51:05.238Z | 152.4° SSE |
| 5 mins | 2025-09-27 21:21:05.238Z | 330.877° NNW | 2025-09-27 21:23:05.238Z | 291.907° WNW | 22.157° | 2025-09-27 21:26:05.238Z | 240.519° WSW |
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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