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 week ago
TLE from 1 week ago
0 AEROCUBE 7
1 40966U 15058C 26154.79454420 .00004353 00000-0 35185-3 0 9997
2 40966 64.7636 286.7614 0120013 67.0259 294.3464 14.95631029363957Epoch: 2026-06-03T19:04Z
TLE epoch observation values (Epoch: 2026-06-03T19:04:08.618Z)
Latitude
-0.00003°
Longitude
108.47743°
Altitude
548.832 km
Speed
7.606 km/s
True Right ascension
19h 07m 02s
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
19:42:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
662.475 km
Perigee altitude
495.486 km
Semi-major axis
6,957.117 km
Eccentricity
0.012
Inclination
64.7636°
RAAN
286.7614°
Arg. of periapsis
67.0259°
True anomaly
293.08576°
Mean anomaly
294.3464°
Eccentric anomaly
293.71685°
Mean motion
3.74024 °/min
Orbital period
96.25 mins
BSTAR
0.00035185
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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 | 2026-06-10 10:07:52.739Z | 271.776° WNW | 2026-06-10 10:09:52.739Z | 305.817° NW | 17.04° | 2026-06-10 10:11:52.739Z | 344.909° N |
| 5 mins | 2026-06-10 16:52:52.739Z | 4.862° NNE | 2026-06-10 16:54:52.739Z | 43.83° NE | 22.284° | 2026-06-10 16:57:52.739Z | 99.703° ESE |
| 5 mins | 2026-06-10 18:31:52.739Z | 294.518° NW | 2026-06-10 18:33:52.739Z | 252.274° W | 26.548° | 2026-06-10 18:36:52.739Z | 190.721° SSW |
| 5 mins | 2026-06-11 08:33:52.739Z | 195.756° SSW | 2026-06-11 08:35:52.739Z | 113.319° SE | 42.649° | 2026-06-11 08:38:52.739Z | 38.624° 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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