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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 AEROCUBE 6A
1 40045U 14033AM 26177.44101836 .00004894 00000-0 41142-3 0 9994
2 40045 97.7229 344.2929 0038208 345.8751 14.1399 14.98182404648004Epoch: 2026-06-26T10:35Z
TLE epoch observation values (Epoch: 2026-06-26T10:35:03.986Z)
Latitude
-0.00006°
Longitude
-89.04319°
Altitude
549.812 km
Speed
7.601 km/s
True Right ascension
22h 57m 10s
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
08:04:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
596.067 km
Perigee altitude
542.975 km
Semi-major axis
6,947.658 km
Eccentricity
0.00382
Inclination
97.7229°
RAAN
344.2929°
Arg. of periapsis
345.8751°
True anomaly
14.24736°
Mean anomaly
14.1399°
Eccentric anomaly
14.19358°
Mean motion
3.74788 °/min
Orbital period
96.05 mins
BSTAR
0.00041142
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-26 23:57:39.879Z | 14.139° NNE | 2026-06-27 00:01:39.879Z | 72.131° E | 44.634° | 2026-06-27 00:05:39.879Z | 190.347° SSW |
| 5 mins | 2026-06-27 10:46:39.879Z | 132.229° SE | 2026-06-27 10:48:39.879Z | 75.141° E | 34.673° | 2026-06-27 10:51:39.879Z | 5.709° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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