AEROCUBE 18A, 63220
Orbit data source: Space-Track
AEROCUBE 18A, 63220 is a payload satellite owned by AERO (US) in SSO that was launched on Sat, 15 Mar 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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63220 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AERO
Mission
Operational Defense 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 + 2 Pan, 14.5 m
Radar Cross Section
0.045 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 AEROCUBE 18A
1 63220U 25052L 26252.61353861 .00005057 00000-0 20374-3 0 9993
2 63220 97.3839 144.9964 0004120 160.7652 199.3743 15.25286891 82761Epoch: 2026-09-09T14:43Z
TLE epoch observation values (Epoch: 2026-09-09T14:43:29.735Z)
Latitude
0.00002°
Longitude
-64.54058°
Altitude
495.692 km
Speed
7.615 km/s
True Right ascension
09h 39m 59s
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
13:45:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.71 km
Perigee altitude
484.054 km
Semi-major axis
6,865.019 km
Eccentricity
0.00041
Inclination
97.3839°
RAAN
144.9964°
Arg. of periapsis
160.7652°
True anomaly
199.35865°
Mean anomaly
199.3743°
Eccentric anomaly
199.36647°
Mean motion
3.81576 °/min
Orbital period
94.35 mins
BSTAR
0.00020374
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.AEROCUBE 18A 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 | 2026-09-10 05:27:34.322Z | 26.957° NE | 2026-09-10 05:30:34.322Z | 100.456° ESE | 46.293° | 2026-09-10 05:33:34.322Z | 171.803° S |
| 4 mins | 2026-09-10 16:04:34.322Z | 102.339° ESE | 2026-09-10 16:06:34.322Z | 63.345° ENE | 17.634° | 2026-09-10 16:08:34.322Z | 28.174° NE |
| 4 mins | 2026-09-10 17:38:34.322Z | 233.523° WSW | 2026-09-10 17:39:34.322Z | 260.51° W | 26.46° | 2026-09-10 17:42:34.322Z | 320.868° NNW |
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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