AEROCUBE 18B, 63222
Orbit data source: Space-Track
AEROCUBE 18B, 63222 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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63222 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, 0.2 m
Radar Cross Section
0.045 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 AEROCUBE 18B
1 63222U 25052N 26297.12564239 .00005742 00000-0 22849-3 0 9993
2 63222 97.3795 188.8909 0005759 51.1659 309.0093 15.25638828 89541Epoch: 2026-10-24T03:00Z
TLE epoch observation values (Epoch: 2026-10-24T03:00:55.502Z)
Latitude
0.00002°
Longitude
111.12332°
Altitude
489.478 km
Speed
7.622 km/s
True Right ascension
12h 35m 33s
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
18:33:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.778 km
Perigee altitude
481.872 km
Semi-major axis
6,863.962 km
Eccentricity
0.00058
Inclination
97.3795°
RAAN
188.8909°
Arg. of periapsis
51.1659°
True anomaly
308.958°
Mean anomaly
309.0093°
Eccentric anomaly
308.98365°
Mean motion
3.81664 °/min
Orbital period
94.32 mins
BSTAR
0.00022849
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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 18B 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-25 06:21:17.366Z | 329.884° NNW | 2026-10-25 06:22:17.366Z | 302.711° NW | 31.321° | 2026-10-25 06:25:17.366Z | 228.849° WSW |
| 5 mins | 2026-10-25 16:56:17.366Z | 162.447° S | 2026-10-25 16:58:17.366Z | 42.932° NE | 80.583° | 2026-10-25 17:01:17.366Z | 350.281° 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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