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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Edit Public Description
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: 15 hours ago
TLE from 15 hours ago
0 AEROCUBE 6A
1 40045U 14033AM 25315.99338768 .00009486 00000-0 86576-3 0 9995
2 40045 97.7040 121.0132 0041331 23.4399 336.8693 14.94628334614131Epoch: 2025-11-11T23:50Z
TLE epoch observation values (Epoch: 2025-11-11T23:50:28.695Z)
Latitude
-0.00009°
Longitude
72.02168°
Altitude
560.126 km
Speed
7.596 km/s
True Right ascension
08h 04m 03s
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
10:49:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
609.3 km
Perigee altitude
551.778 km
Semi-major axis
6,958.676 km
Eccentricity
0.00413
Inclination
97.704°
RAAN
121.0132°
Arg. of periapsis
23.4399°
True anomaly
336.68236°
Mean anomaly
336.8693°
Eccentric anomaly
336.77592°
Mean motion
3.73898 °/min
Orbital period
96.28 mins
BSTAR
0.00086576
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-12 22:55:56.489Z | 63.361° ENE | 2025-11-12 22:57:56.489Z | 94.69° ESE | 14.803° | 2025-11-12 22:59:56.489Z | 124.883° SE |
| 6 mins | 2025-11-13 00:30:56.489Z | 347.07° N | 2025-11-13 00:32:56.489Z | 303.951° NW | 32.681° | 2025-11-13 00:36:56.489Z | 219.174° SW |
| 5 mins | 2025-11-13 11:19:56.489Z | 180.56° SSW | 2025-11-13 11:21:56.489Z | 258.084° W | 43.198° | 2025-11-13 11:24:56.489Z | 340.721° N |
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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