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, 0.1 m
Radar Cross Section
0.010 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 AEROCUBE 6A
1 40045U 14033AM 26098.20626509 .00006899 00000-0 59119-3 0 9999
2 40045 97.7172 265.9629 0037808 248.5293 111.1895 14.97303781636145Epoch: 2026-04-08T04:57Z
TLE epoch observation values (Epoch: 2026-04-08T04:57:01.303Z)
Latitude
-0.00007°
Longitude
-4.76448°
Altitude
587.872 km
Speed
7.561 km/s
True Right ascension
17h 43m 51s
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
21:39:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
598.519 km
Perigee altitude
545.963 km
Semi-major axis
6,950.378 km
Eccentricity
0.00378
Inclination
97.7172°
RAAN
265.9629°
Arg. of periapsis
248.5293°
True anomaly
111.59276°
Mean anomaly
111.1895°
Eccentric anomaly
111.3912°
Mean motion
3.74568 °/min
Orbital period
96.11 mins
BSTAR
0.00059119
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-08 23:11:05.054Z | 51.209° ENE | 2026-04-08 23:13:05.054Z | 85.692° E | 20.554° | 2026-04-08 23:16:05.054Z | 140.663° SSE |
| 5 mins | 2026-04-09 00:47:05.054Z | 326.283° NNW | 2026-04-09 00:49:05.054Z | 279.575° WNW | 24.135° | 2026-04-09 00:52:05.054Z | 232.658° WSW |
| 6 mins | 2026-04-09 11:33:05.054Z | 192.247° SSW | 2026-04-09 11:36:05.054Z | 264.206° W | 36.048° | 2026-04-09 11:39:05.054Z | 330.274° NNW |
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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