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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 AEROCUBE 7
1 40966U 15058C 25355.95851209 .00004633 00000-0 38304-3 0 9990
2 40966 64.7640 79.2587 0126943 132.1998 228.9977 14.94063138339468Epoch: 2025-12-21T23:00Z
TLE epoch observation values (Epoch: 2025-12-21T23:00:15.444Z)
Latitude
-0°
Longitude
3.43086°
Altitude
645.925 km
Speed
7.504 km/s
True Right ascension
05h 17m 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
10:49:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
672.226 km
Perigee altitude
495.471 km
Semi-major axis
6,961.985 km
Eccentricity
0.01269
Inclination
64.764°
RAAN
79.2587°
Arg. of periapsis
132.1998°
True anomaly
227.91127°
Mean anomaly
228.9977°
Eccentric anomaly
228.45335°
Mean motion
3.73632 °/min
Orbital period
96.35 mins
BSTAR
0.00038304
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-22 15:35:49.682Z | 358.823° N | 2025-12-22 15:38:49.682Z | 62.162° ENE | 22.182° | 2025-12-22 15:40:49.682Z | 99.734° ESE |
| 4 mins | 2025-12-22 17:15:49.682Z | 282.512° WNW | 2025-12-22 17:17:49.682Z | 234.763° WSW | 21.887° | 2025-12-22 17:19:49.682Z | 197.55° SSW |
| 7 mins | 2025-12-23 07:16:49.682Z | 206.055° SW | 2025-12-23 07:19:49.682Z | 163.127° S | 44.284° | 2025-12-23 07:23:49.682Z | 34.273° 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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