AEROCUBE 6A, 40045
Orbit data source: Space-Track
AEROCUBE 6A, 40045 is a payload satellite owned by AERO (US) in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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40045 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
AERO
Mission
Operational Defense Technology
Bus & Motor
CUBESAT 0.5U, Unknown motor
Mass
~0.5 kg wet, ~0.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.075 m
Radar Cross Section
0.010 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 AEROCUBE 6A
1 40045U 14033AM 26311.23311033 .00007109 00000-0 57811-3 0 9995
2 40045 97.7363 116.9317 0035531 256.2294 103.4973 14.99380666668048Epoch: 2026-11-07T05:35Z
TLE epoch observation values (Epoch: 2026-11-07T05:35:40.732Z)
Latitude
-0.00007°
Longitude
-13.42932°
Altitude
577.707 km
Speed
7.569 km/s
True Right ascension
07h 47m 43s
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
16:23:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.489 km
Perigee altitude
541.144 km
Semi-major axis
6,943.953 km
Eccentricity
0.00355
Inclination
97.7363°
RAAN
116.9317°
Arg. of periapsis
256.2294°
True anomaly
103.8928°
Mean anomaly
103.4973°
Eccentric anomaly
103.69509°
Mean motion
3.75088 °/min
Orbital period
95.98 mins
BSTAR
0.00057811
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Other satellites on launch #33 in the year 2014 (2014-06-19 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 6A 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-07 23:47:19.475Z | 25.703° NE | 2026-11-07 23:50:19.475Z | 93.676° ESE | 53.842° | 2026-11-07 23:54:19.475Z | 177.868° S |
| 6 mins | 2026-11-08 10:34:19.475Z | 122.077° SE | 2026-11-08 10:36:19.475Z | 84.027° E | 29.956° | 2026-11-08 10:40:19.475Z | 9.816° NNE |
| 4 mins | 2026-11-08 12:10:19.475Z | 236.308° WSW | 2026-11-08 12:12:19.475Z | 274.527° WNW | 20.108° | 2026-11-08 12:14:19.475Z | 307.144° NW |
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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