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: 21 hours ago
TLE from 21 hours ago
0 AEROCUBE 6B
1 40046U 14033AN 25259.98519216 .00007082 00000-0 64841-3 0 9992
2 40046 97.6995 65.3585 0040567 200.7319 159.2258 14.94621670605875Epoch: 2025-09-16T23:38Z
TLE epoch observation values (Epoch: 2025-09-16T23:38:40.602Z)
Latitude
-0.00001°
Longitude
74.52169°
Altitude
613.02 km
Speed
7.538 km/s
True Right ascension
04h 21m 26s
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
13:10:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.789 km
Perigee altitude
552.33 km
Semi-major axis
6,958.697 km
Eccentricity
0.00406
Inclination
97.6995°
RAAN
65.3585°
Arg. of periapsis
200.7319°
True anomaly
159.3899°
Mean anomaly
159.2258°
Eccentric anomaly
159.30793°
Mean motion
3.73896 °/min
Orbital period
96.28 mins
BSTAR
0.00064841
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 00:19:41.493Z | 353.814° N | 2025-09-18 00:21:41.493Z | 305.264° NW | 37.69° | 2025-09-18 00:25:41.493Z | 210.469° SW |
| 6 mins | 2025-09-18 11:07:41.493Z | 165.646° S | 2025-09-18 11:10:41.493Z | 357.134° N | 44.546° | 2025-09-18 11:13:41.493Z | 348.222° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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