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: 7 hours ago
TLE from 7 hours ago
0 AEROCUBE 18B
1 63222U 25052N 26260.52232448 .00004894 00000-0 19740-3 0 9994
2 63222 97.3826 152.7763 0005230 143.7919 216.3674 15.25260873 83961Epoch: 2026-09-17T12:32Z
TLE epoch observation values (Epoch: 2026-09-17T12:32:08.835Z)
Latitude
0.00001°
Longitude
-31.71887°
Altitude
495.994 km
Speed
7.615 km/s
True Right ascension
10h 11m 06s
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
12:09:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.55 km
Perigee altitude
483.37 km
Semi-major axis
6,865.097 km
Eccentricity
0.00052
Inclination
97.3826°
RAAN
152.7763°
Arg. of periapsis
143.7919°
True anomaly
216.33188°
Mean anomaly
216.3674°
Eccentric anomaly
216.34964°
Mean motion
3.81569 °/min
Orbital period
94.35 mins
BSTAR
0.0001974
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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 | 2026-09-18 04:52:04.756Z | 60.404° ENE | 2026-09-18 04:54:04.756Z | 97.441° ESE | 15.921° | 2026-09-18 04:56:04.756Z | 131.966° SE |
| 4 mins | 2026-09-18 06:26:04.756Z | 326.08° NNW | 2026-09-18 06:27:04.756Z | 300.559° NW | 27.445° | 2026-09-18 06:30:04.756Z | 232.884° WSW |
| 5 mins | 2026-09-18 17:01:04.756Z | 170.502° S | 2026-09-18 17:03:04.756Z | 235.835° WSW | 83.991° | 2026-09-18 17:06:04.756Z | 346.397° N |
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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