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: 15 hours ago
TLE from 15 hours ago
0 AE3VA
1 64563U 25135AM 26182.25958030 .00008400 00000-0 72855-3 0 9993
2 64563 97.7689 297.0664 0002488 189.5676 170.5498 14.97319319 56046Epoch: 2026-07-01T06:13Z
TLE epoch observation values (Epoch: 2026-07-01T06:13:47.737Z)
Latitude
-0.00013°
Longitude
-75.70137°
Altitude
579.939 km
Speed
7.57 km/s
True Right ascension
19h 48m 15s
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
09:01:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.924 km
Perigee altitude
570.466 km
Semi-major axis
6,950.332 km
Eccentricity
0.00025
Inclination
97.7689°
RAAN
297.0664°
Arg. of periapsis
189.5676°
True anomaly
170.55448°
Mean anomaly
170.5498°
Eccentric anomaly
170.55214°
Mean motion
3.74572 °/min
Orbital period
96.11 mins
BSTAR
0.00072855
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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 | 2026-07-02 08:01:35.005Z | 190.214° SSW | 2026-07-02 08:03:35.005Z | 232.966° WSW | 37.15° | 2026-07-02 08:07:35.005Z | 335.831° NNW |
| 4 mins | 2026-07-02 19:43:35.005Z | 69.581° E | 2026-07-02 19:44:35.005Z | 89.55° E | 19.631° | 2026-07-02 19:47:35.005Z | 141.385° SSE |
| 5 mins | 2026-07-02 21:17:35.005Z | 339.34° N | 2026-07-02 21:19:35.005Z | 301.703° NW | 24.721° | 2026-07-02 21:22:35.005Z | 238.918° WSW |
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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