AE5RA, 66685
Orbit data source: Space-Track
AE5RA, 66685 is a payload satellite owned by ArkEdge (JP) in SSO that was launched on Fri, 28 Nov 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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66685 intel report (Beta)
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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, 0.5 m
Radar Cross Section
0.575 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 AE5RA
1 66685U 25276V 26192.45492933 .00007098 00000-0 30125-3 0 9990
2 66685 97.4207 266.1887 0002815 280.6323 79.4597 15.23394039 34142Epoch: 2026-07-11T10:55Z
TLE epoch observation values (Epoch: 2026-07-11T10:55:05.894Z)
Latitude
0.00002°
Longitude
173.04623°
Altitude
498.353 km
Speed
7.616 km/s
True Right ascension
17h 44m 45s
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
15:41:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.508 km
Perigee altitude
490.64 km
Semi-major axis
6,870.711 km
Eccentricity
0.00028
Inclination
97.4207°
RAAN
266.1887°
Arg. of periapsis
280.6323°
True anomaly
79.49142°
Mean anomaly
79.4597°
Eccentric anomaly
79.47556°
Mean motion
3.81101 °/min
Orbital period
94.46 mins
BSTAR
0.00030125
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Other satellites on launch #276 in the year 2025 (2025-11-28 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.AE5RA 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 | 2026-07-12 04:23:41.397Z | 130.409° SE | 2026-07-12 04:26:41.397Z | 68.479° E | 25.822° | 2026-07-12 04:29:41.397Z | 11.329° NNE |
| 5 mins | 2026-07-12 17:26:41.397Z | 33.828° NE | 2026-07-12 17:28:41.397Z | 78.14° E | 32.471° | 2026-07-12 17:31:41.397Z | 164.813° S |
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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