AEROCUBE 8C, 41853
Orbit data source: Space-Track
AEROCUBE 8C, 41853 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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41853 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: 3 days ago
TLE from 3 days ago
0 AEROCUBE 8C
1 41853U 16067F 26170.60887759 .00005876 00000-0 24098-3 0 9999
2 41853 98.0546 38.1882 0006504 62.3132 297.8763 15.24674232526435Epoch: 2026-06-19T14:36Z
TLE epoch observation values (Epoch: 2026-06-19T14:36:47.023Z)
Latitude
-0.00005°
Longitude
-88.84313°
Altitude
492.754 km
Speed
7.62 km/s
True Right ascension
02h 32m 45s
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
21:36:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.219 km
Perigee altitude
484.286 km
Semi-major axis
6,866.889 km
Eccentricity
0.00065
Inclination
98.0546°
RAAN
38.1882°
Arg. of periapsis
62.3132°
True anomaly
297.81039°
Mean anomaly
297.8763°
Eccentric anomaly
297.84335°
Mean motion
3.8142 °/min
Orbital period
94.38 mins
BSTAR
0.00024098
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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 8C 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 15:11:35.031Z | 164.885° S | 2026-06-22 15:14:35.031Z | 75.582° E | 44.952° | 2026-06-22 15:17:35.031Z | 348.148° N |
| 5 mins | 2026-06-23 04:14:35.031Z | 5.162° NNE | 2026-06-23 04:16:35.031Z | 276.603° WNW | 43.841° | 2026-06-23 04:19:35.031Z | 200.435° SSW |
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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