AEROCUBE 7, 40966
Orbit data source: Space-Track
AEROCUBE 7, 40966 is a payload satellite owned by AERO (US) in LEO that was launched on Thu, 08 Oct 2015 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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40966 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: 1 day ago
TLE from 1 day ago
0 AEROCUBE 7
1 40966U 15058C 26082.36403292 .00004444 00000-0 36480-3 0 9991
2 40966 64.7620 153.4872 0119959 96.0065 265.4735 14.95022844353127Epoch: 2026-03-23T08:44Z
TLE epoch observation values (Epoch: 2026-03-23T08:44:12.444Z)
Latitude
0.00001°
Longitude
-158.42175°
Altitude
591.897 km
Speed
7.56 km/s
True Right ascension
10h 13m 56s
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
15:04:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
664.347 km
Perigee altitude
497.388 km
Semi-major axis
6,959.005 km
Eccentricity
0.012
Inclination
64.762°
RAAN
153.4872°
Arg. of periapsis
96.0065°
True anomaly
264.10491°
Mean anomaly
265.4735°
Eccentric anomaly
264.78903°
Mean motion
3.73872 °/min
Orbital period
96.29 mins
BSTAR
0.0003648
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Other satellites on launch #58 in the year 2015 (2015-10-08 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 7 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 | 2026-03-24 14:09:20.640Z | 7.748° NNE | 2026-03-24 14:11:20.640Z | 44.052° NE | 18.064° | 2026-03-24 14:13:20.640Z | 82.343° E |
| 5 mins | 2026-03-24 15:48:20.640Z | 301.197° NW | 2026-03-24 15:50:20.640Z | 255.726° W | 30.201° | 2026-03-24 15:53:20.640Z | 183.186° SSW |
| 6 mins | 2026-03-25 05:50:20.640Z | 188.03° SSW | 2026-03-25 05:52:20.640Z | 144.524° SSE | 37.42° | 2026-03-25 05:56:20.640Z | 42.164° NE |
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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