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: 1 day ago
TLE from 1 day ago
0 AEROCUBE 6A
1 40045U 14033AM 25301.39748236 .00009043 00000-0 83077-3 0 9991
2 40045 97.7042 106.6842 0042107 71.4975 289.0814 14.94355705611955Epoch: 2025-10-28T09:32Z
TLE epoch observation values (Epoch: 2025-10-28T09:32:22.475Z)
Latitude
-0.00006°
Longitude
-73.39499°
Altitude
577.945 km
Speed
7.577 km/s
True Right ascension
07h 06m 44s
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
09:27:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
610.691 km
Perigee altitude
552.082 km
Semi-major axis
6,959.523 km
Eccentricity
0.00421
Inclination
97.7042°
RAAN
106.6842°
Arg. of periapsis
71.4975°
True anomaly
288.62462°
Mean anomaly
289.0814°
Eccentric anomaly
288.85309°
Mean motion
3.7383 °/min
Orbital period
96.3 mins
BSTAR
0.00083077
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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 | 2025-10-29 23:05:34.956Z | 58.319° ENE | 2025-10-29 23:07:34.956Z | 93.023° ESE | 17.816° | 2025-10-29 23:09:34.956Z | 128.23° SE |
| 6 mins | 2025-10-30 00:40:34.956Z | 342.208° N | 2025-10-30 00:43:34.956Z | 273.937° WNW | 26.799° | 2025-10-30 00:46:34.956Z | 227.114° WSW |
| 6 mins | 2025-10-30 11:29:34.956Z | 191.053° SSW | 2025-10-30 11:31:34.956Z | 238.617° WSW | 37.363° | 2025-10-30 11:35:34.956Z | 336.534° 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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