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: 23 hours ago
TLE from 23 hours ago
0 AEROCUBE 7
1 40966U 15058C 26067.71390171 .00007369 00000-0 59605-3 0 9997
2 40966 64.7633 199.3176 0120661 101.9776 259.4893 14.94886868350931Epoch: 2026-03-08T17:08Z
TLE epoch observation values (Epoch: 2026-03-08T17:08:01.107Z)
Latitude
-0.00008°
Longitude
135.89571°
Altitude
601.034 km
Speed
7.551 km/s
True Right ascension
13h 17m 16s
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
19:47:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
665.263 km
Perigee altitude
497.317 km
Semi-major axis
6,959.427 km
Eccentricity
0.01207
Inclination
64.7633°
RAAN
199.3176°
Arg. of periapsis
101.9776°
True anomaly
258.13368°
Mean anomaly
259.4893°
Eccentric anomaly
258.8111°
Mean motion
3.73838 °/min
Orbital period
96.3 mins
BSTAR
0.00059605
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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 | 2026-03-09 19:22:47.126Z | 324.938° NNW | 2026-03-09 19:24:47.126Z | 284.967° WNW | 44.488° | 2026-03-09 19:28:47.126Z | 152.134° SSE |
| 4 mins | 2026-03-10 09:25:47.126Z | 145.506° SSE | 2026-03-10 09:26:47.126Z | 123.785° SE | 22.689° | 2026-03-10 09:29:47.126Z | 64.284° ENE |
| 5 mins | 2026-03-10 11:03:47.126Z | 260.184° W | 2026-03-10 11:05:47.126Z | 299.214° NW | 24.216° | 2026-03-10 11:08:47.126Z | 2.39° NNE |
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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