AEROCUBE 8D, 41852
Orbit data source: Space-Track
AEROCUBE 8D, 41852 is a payload satellite owned by AERO (US) in SSO that was launched on Fri, 11 Nov 2016 UTC via an ATLAS V 401 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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41852 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
AERO
Mission
Operational Defense Technology
Bus & Motor
CUBESAT 1.5U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.025 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 AEROCUBE 8D
1 41852U 16067E 25294.68800341 .00011694 00000-0 54937-3 0 9994
2 41852 98.0958 142.0042 0002549 225.4095 134.6931 15.19790080489784Epoch: 2025-10-21T16:30Z
TLE epoch observation values (Epoch: 2025-10-21T16:30:43.494Z)
Latitude
0.00004°
Longitude
-136.04941°
Altitude
510.779 km
Speed
7.608 km/s
True Right ascension
09h 28m 01s
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
22:53:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
505.226 km
Perigee altitude
501.717 km
Semi-major axis
6,881.608 km
Eccentricity
0.00025
Inclination
98.0958°
RAAN
142.0042°
Arg. of periapsis
225.4095°
True anomaly
134.71386°
Mean anomaly
134.6931°
Eccentric anomaly
134.70348°
Mean motion
3.80197 °/min
Orbital period
94.69 mins
BSTAR
0.00054937
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Other satellites on launch #67 in the year 2016 (2016-11-11 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 8D 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 | 2025-10-22 13:13:26.746Z | 95.407° ESE | 2025-10-22 13:14:26.746Z | 71.314° E | 21.491° | 2025-10-22 13:17:26.746Z | 16.174° NNE |
| 4 mins | 2025-10-22 14:46:26.746Z | 226.805° WSW | 2025-10-22 14:48:26.746Z | 268.849° W | 19.603° | 2025-10-22 14:50:26.746Z | 307.175° NW |
| 4 mins | 2025-10-23 02:17:26.746Z | 60.69° ENE | 2025-10-23 02:18:26.746Z | 87.057° E | 25.635° | 2025-10-23 02:21:26.746Z | 154.573° SSE |
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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