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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AEROCUBE 6B
1 40046U 14033AN 26264.68559885 .00004293 00000-0 33959-3 0 9999
2 40046 97.7362 70.7027 0040985 36.3610 324.0385 15.00499962661225Epoch: 2026-09-21T16:27Z
TLE epoch observation values (Epoch: 2026-09-21T16:27:15.740Z)
Latitude
-0.00007°
Longitude
-176.67475°
Altitude
545.409 km
Speed
7.602 km/s
True Right ascension
04h 42m 48s
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
09:04:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.805 km
Perigee altitude
533.914 km
Semi-major axis
6,940.497 km
Eccentricity
0.0041
Inclination
97.7362°
RAAN
70.7027°
Arg. of periapsis
36.361°
True anomaly
323.76155°
Mean anomaly
324.0385°
Eccentric anomaly
323.90014°
Mean motion
3.75368 °/min
Orbital period
95.91 mins
BSTAR
0.00033959
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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 | 2026-09-22 23:25:45.258Z | 35.31° NE | 2026-09-22 23:28:45.258Z | 84.726° E | 30.255° | 2026-09-22 23:32:45.258Z | 159.836° S |
| 4 mins | 2026-09-23 01:02:45.258Z | 315.978° NNW | 2026-09-23 01:03:45.258Z | 296.801° NW | 19.764° | 2026-09-23 01:06:45.258Z | 247.195° WSW |
| 5 mins | 2026-09-23 11:48:45.258Z | 221.011° SW | 2026-09-23 11:50:45.258Z | 277.254° WNW | 30.575° | 2026-09-23 11:53:45.258Z | 326.61° 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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