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: 1 day ago
TLE from 1 day ago
0 AEROCUBE 18A
1 63220U 25052L 26206.22538068 .00006147 00000-0 25027-3 0 9994
2 63220 97.3923 99.2146 0004183 18.4367 341.7022 15.24852508 75690Epoch: 2026-07-25T05:24Z
TLE epoch observation values (Epoch: 2026-07-25T05:24:32.890Z)
Latitude
-0.00001°
Longitude
75.13684°
Altitude
491.597 km
Speed
7.621 km/s
True Right ascension
06h 36m 51s
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
23:03:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
491.059 km
Perigee altitude
485.315 km
Semi-major axis
6,866.324 km
Eccentricity
0.00042
Inclination
97.3923°
RAAN
99.2146°
Arg. of periapsis
18.4367°
True anomaly
341.68714°
Mean anomaly
341.7022°
Eccentric anomaly
341.69467°
Mean motion
3.81467 °/min
Orbital period
94.37 mins
BSTAR
0.00025027
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-07-26 16:12:02.046Z | 119.564° SE | 2026-07-26 16:15:02.046Z | 59.888° ENE | 20.103° | 2026-07-26 16:17:02.046Z | 22.885° NE |
| 4 mins | 2026-07-27 05:15:02.046Z | 59.707° ENE | 2026-07-27 05:16:02.046Z | 87.577° E | 26.305° | 2026-07-27 05:19:02.046Z | 155.833° SSE |
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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