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: 11 hours ago
TLE from 11 hours ago
0 AEROCUBE 7
1 40966U 15058C 26261.15119818 .00002090 00000-0 17042-3 0 9993
2 40966 64.7612 313.4766 0127683 26.3084 334.4439 14.96318467379865Epoch: 2026-09-18T03:37Z
TLE epoch observation values (Epoch: 2026-09-18T03:37:43.522Z)
Latitude
-0.00006°
Longitude
-98.03297°
Altitude
500.369 km
Speed
7.658 km/s
True Right ascension
20h 53m 54s
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
07:37:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
665.652 km
Perigee altitude
488.045 km
Semi-major axis
6,954.986 km
Eccentricity
0.01277
Inclination
64.7612°
RAAN
313.4766°
Arg. of periapsis
26.3084°
True anomaly
333.80351°
Mean anomaly
334.4439°
Eccentric anomaly
334.12463°
Mean motion
3.74196 °/min
Orbital period
96.21 mins
BSTAR
0.00017042
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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 | 2026-09-18 15:25:33.715Z | 292.641° NW | 2026-09-18 15:28:33.715Z | 244.717° WSW | 21.228° | 2026-09-18 15:31:33.715Z | 200.938° SSW |
| 5 mins | 2026-09-19 05:27:33.715Z | 223.068° SW | 2026-09-19 05:29:33.715Z | 304.176° NW | 71.231° | 2026-09-19 05:32:33.715Z | 26.132° NE |
| 6 mins | 2026-09-19 13:51:33.715Z | 342.826° N | 2026-09-19 13:53:33.715Z | 33.47° NE | 60.52° | 2026-09-19 13:57:33.715Z | 135.995° 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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