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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 AEROCUBE 8D
1 41852U 16067E 26294.12215653 .00008523 00000-0 33502-3 0 9992
2 41852 98.0461 173.8754 0004892 68.4738 291.7020 15.25949250545269Epoch: 2026-10-21T02:55Z
TLE epoch observation values (Epoch: 2026-10-21T02:55:54.324Z)
Latitude
0.00004°
Longitude
100.3231°
Altitude
489.775 km
Speed
7.621 km/s
True Right ascension
11h 35m 30s
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
14:18:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.28 km
Perigee altitude
481.566 km
Semi-major axis
6,863.06 km
Eccentricity
0.00049
Inclination
98.0461°
RAAN
173.8754°
Arg. of periapsis
68.4738°
True anomaly
291.6499°
Mean anomaly
291.702°
Eccentric anomaly
291.67595°
Mean motion
3.81739 °/min
Orbital period
94.31 mins
BSTAR
0.00033502
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-23 04:17:37.584Z | 48.02° ENE | 2026-10-23 04:19:37.584Z | 84.646° E | 21.342° | 2026-10-23 04:22:37.584Z | 145.367° SSE |
| 5 mins | 2026-10-23 16:26:37.584Z | 189.813° SSW | 2026-10-23 16:28:37.584Z | 243.985° WSW | 49.546° | 2026-10-23 16:31:37.584Z | 332.946° NNW |
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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