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: 20 hours ago
TLE from 20 hours ago
0 AEROCUBE 7
1 40966U 15058C 25302.19551259 .00004958 00000-0 40911-3 0 9997
2 40966 64.7629 247.1247 0134429 152.4167 208.4165 14.93331406331431Epoch: 2025-10-29T04:41Z
TLE epoch observation values (Epoch: 2025-10-29T04:41:32.287Z)
Latitude
-0.00007°
Longitude
138.96801°
Altitude
672.212 km
Speed
7.477 km/s
True Right ascension
16h 28m 29s
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
19:49:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
679.743 km
Perigee altitude
492.504 km
Semi-major axis
6,964.261 km
Eccentricity
0.01344
Inclination
64.7629°
RAAN
247.1247°
Arg. of periapsis
152.4167°
True anomaly
207.69414°
Mean anomaly
208.4165°
Eccentric anomaly
208.05426°
Mean motion
3.73448 °/min
Orbital period
96.4 mins
BSTAR
0.00040911
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-30 06:57:26.650Z | 332.849° NNW | 2025-10-30 07:00:26.650Z | 79.768° E | 43.88° | 2025-10-30 07:03:26.650Z | 142.772° SSE |
| 5 mins | 2025-10-30 21:01:26.650Z | 145.492° SSE | 2025-10-30 21:03:26.650Z | 108.573° ESE | 21.256° | 2025-10-30 21:06:26.650Z | 62.88° ENE |
| 6 mins | 2025-10-30 22:39:26.650Z | 248.596° W | 2025-10-30 22:42:26.650Z | 313.183° NW | 30.87° | 2025-10-30 22:45:26.650Z | 10.434° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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