AEROCUBE 6B, 40046
Orbit data source: Space-Track
AEROCUBE 6B, 40046 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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40046 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: 11 hours ago
TLE from 11 hours ago
0 AEROCUBE 6B
1 40046U 14033AN 25345.28627258 .00015423 00000-0 13393-2 0 9990
2 40046 97.7035 149.2220 0037776 277.1345 82.5582 14.96557696618627Epoch: 2025-12-11T06:52Z
TLE epoch observation values (Epoch: 2025-12-11T06:52:13.950Z)
Latitude
-0.00004°
Longitude
-34.08055°
Altitude
577.286 km
Speed
7.574 km/s
True Right ascension
09h 56m 53s
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
15:56:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
600.816 km
Perigee altitude
548.287 km
Semi-major axis
6,952.689 km
Eccentricity
0.00378
Inclination
97.7035°
RAAN
149.222°
Arg. of periapsis
277.1345°
True anomaly
82.98769°
Mean anomaly
82.5582°
Eccentric anomaly
82.77292°
Mean motion
3.74381 °/min
Orbital period
96.16 mins
BSTAR
0.0013393
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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 6B 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 | 2025-12-11 23:29:05.072Z | 29.085° NE | 2025-12-11 23:33:05.072Z | 108.198° ESE | 32.232° | 2025-12-11 23:36:05.072Z | 164.476° S |
| 4 mins | 2025-12-12 01:06:05.072Z | 321.451° NNW | 2025-12-12 01:08:05.072Z | 287.975° WNW | 16.059° | 2025-12-12 01:10:05.072Z | 257.629° W |
| 4 mins | 2025-12-12 10:19:05.072Z | 99.174° ESE | 2025-12-12 10:20:05.072Z | 78.908° E | 21.862° | 2025-12-12 10:23:05.072Z | 22.687° NE |
| 5 mins | 2025-12-12 11:54:05.072Z | 229.332° WSW | 2025-12-12 11:56:05.072Z | 274.646° WNW | 23.501° | 2025-12-12 11:59:05.072Z | 321.28° 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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