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: 12 hours ago
TLE from 12 hours ago
0 AE3VA
1 64563U 25135AM 26083.31540991 .00007288 00000-0 65389-3 0 9990
2 64563 97.7562 198.8626 0003179 174.8542 185.2712 14.96039740 41243Epoch: 2026-03-24T07:34Z
TLE epoch observation values (Epoch: 2026-03-24T07:34:11.416Z)
Latitude
-0.00004°
Longitude
-96.47979°
Altitude
584.398 km
Speed
7.567 km/s
True Right ascension
13h 15m 27s
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
00:41:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
578.371 km
Perigee altitude
573.95 km
Semi-major axis
6,954.297 km
Eccentricity
0.00032
Inclination
97.7562°
RAAN
198.8626°
Arg. of periapsis
174.8542°
True anomaly
185.26785°
Mean anomaly
185.2712°
Eccentric anomaly
185.26953°
Mean motion
3.74251 °/min
Orbital period
96.19 mins
BSTAR
0.00065389
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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 | 2026-03-24 20:58:01.971Z | 357.008° N | 2026-03-24 21:02:01.971Z | 272.062° WNW | 33.275° | 2026-03-24 21:05:01.971Z | 218.971° SW |
| 6 mins | 2026-03-25 07:47:01.971Z | 175.41° S | 2026-03-25 07:50:01.971Z | 310.309° NW | 42.361° | 2026-03-25 07:53:01.971Z | 343.034° 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 descending 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 descending order |
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