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 26037.13715942 .00006304 00000-0 51427-3 0 9999
2 40966 64.7631 294.9393 0122790 114.2145 247.1859 14.94540405346366Epoch: 2026-02-06T03:17Z
TLE epoch observation values (Epoch: 2026-02-06T03:17:30.573Z)
Latitude
-0.00006°
Longitude
109.28253°
Altitude
619.846 km
Speed
7.531 km/s
True Right ascension
19h 39m 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
18:01:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
667.834 km
Perigee altitude
496.898 km
Semi-major axis
6,960.503 km
Eccentricity
0.01228
Inclination
64.7631°
RAAN
294.9393°
Arg. of periapsis
114.2145°
True anomaly
245.89669°
Mean anomaly
247.1859°
Eccentric anomaly
246.54052°
Mean motion
3.73751 °/min
Orbital period
96.32 mins
BSTAR
0.00051427
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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 | 2026-02-06 17:52:20.520Z | 158.339° S | 2026-02-06 17:55:20.520Z | 112.092° ESE | 18.372° | 2026-02-06 17:57:20.520Z | 76.695° E |
| 5 mins | 2026-02-06 19:32:20.520Z | 257.233° W | 2026-02-06 19:34:20.520Z | 312.05° NW | 30.547° | 2026-02-06 19:37:20.520Z | 11.778° NNE |
| 6 mins | 2026-02-07 03:56:20.520Z | 317.31° NNW | 2026-02-07 03:58:20.520Z | 277.637° WNW | 40.031° | 2026-02-07 04:02:20.520Z | 160.395° S |
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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