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 Commercial 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
0.040 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 AEROCUBE 7
1 40966U 15058C 25256.78207796 .00006423 00000-0 52444-3 0 9997
2 40966 64.7653 28.7860 0141800 168.6106 191.8276 14.92668967324653Epoch: 2025-09-13T18:46Z
TLE epoch observation values (Epoch: 2025-09-13T18:46:11.535Z)
Latitude
0.00003°
Longitude
114.22745°
Altitude
688.399 km
Speed
7.46 km/s
True Right ascension
01h 55m 08s
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
23:09:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
686.967 km
Perigee altitude
489.402 km
Semi-major axis
6,966.321 km
Eccentricity
0.01418
Inclination
64.7653°
RAAN
28.786°
Arg. of periapsis
168.6106°
True anomaly
191.50023°
Mean anomaly
191.8276°
Eccentric anomaly
191.66335°
Mean motion
3.73283 °/min
Orbital period
96.44 mins
BSTAR
0.00052444
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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 | 2025-09-14 09:22:42.378Z | 140.165° SSE | 2025-09-14 09:24:42.378Z | 113.832° SE | 14.45° | 2025-09-14 09:26:42.378Z | 85.269° E |
| 7 mins | 2025-09-14 11:00:42.378Z | 228.352° WSW | 2025-09-14 11:03:42.378Z | 294.606° NW | 40.88° | 2025-09-14 11:07:42.378Z | 23.222° NE |
| 6 mins | 2025-09-14 19:26:42.378Z | 331.471° NNW | 2025-09-14 19:29:42.378Z | 106.541° ESE | 44.071° | 2025-09-14 19:32:42.378Z | 145.087° SSE |
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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