AE5RB, 66693
Orbit data source: Space-Track
AE5RB, 66693 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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66693 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
ArkEdge
Mission
Operational Commercial Sigint
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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 AE5RB
1 66693U 25276AD 26238.48615693 .00011443 00000-0 46966-3 0 9992
2 66693 97.4128 311.5628 0005371 114.1382 246.0418 15.24372069 41150Epoch: 2026-08-26T11:40Z
TLE epoch observation values (Epoch: 2026-08-26T11:40:03.958Z)
Latitude
-0°
Longitude
161.80784°
Altitude
497.268 km
Speed
7.615 km/s
True Right ascension
20h 46m 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
11:46:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.321 km
Perigee altitude
485.943 km
Semi-major axis
6,867.769 km
Eccentricity
0.00054
Inclination
97.4128°
RAAN
311.5628°
Arg. of periapsis
114.1382°
True anomaly
245.98557°
Mean anomaly
246.0418°
Eccentric anomaly
246.01368°
Mean motion
3.81346 °/min
Orbital period
94.4 mins
BSTAR
0.00046966
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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.AE5RB 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 | 2026-08-27 05:07:39.995Z | 176.12° S | 2026-08-27 05:10:39.995Z | 301.92° NW | 42.071° | 2026-08-27 05:13:39.995Z | 343.084° N |
| 5 mins | 2026-08-27 18:10:39.995Z | 346.722° N | 2026-08-27 18:12:39.995Z | 271.116° WNW | 35.728° | 2026-08-27 18:15:39.995Z | 212.338° SW |
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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