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: 4 days ago
TLE from 4 days ago
0 AEROCUBE 6A
1 40045U 14033AM 26154.93166257 .00006356 00000-0 53535-3 0 9995
2 40045 97.7216 322.0234 0039359 61.3448 299.1723 14.97953444644634Epoch: 2026-06-03T22:21Z
TLE epoch observation values (Epoch: 2026-06-03T22:21:35.646Z)
Latitude
-0.00002°
Longitude
94.24168°
Altitude
563.015 km
Speed
7.587 km/s
True Right ascension
21h 28m 05s
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
12:24:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
597.578 km
Perigee altitude
542.881 km
Semi-major axis
6,948.366 km
Eccentricity
0.00394
Inclination
97.7216°
RAAN
322.0234°
Arg. of periapsis
61.3448°
True anomaly
298.77754°
Mean anomaly
299.1723°
Eccentric anomaly
298.97502°
Mean motion
3.74731 °/min
Orbital period
96.07 mins
BSTAR
0.00053535
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-08 11:30:29.472Z | 191.899° SSW | 2026-06-08 11:32:29.472Z | 237.19° WSW | 36.196° | 2026-06-08 11:36:29.472Z | 335.659° NNW |
| 4 mins | 2026-06-08 23:11:29.472Z | 60.925° ENE | 2026-06-08 23:13:29.472Z | 100.59° ESE | 20.121° | 2026-06-08 23:15:29.472Z | 136.129° SSE |
| 5 mins | 2026-06-09 00:46:29.472Z | 331.464° NNW | 2026-06-09 00:48:29.472Z | 286.792° WNW | 24.702° | 2026-06-09 00:51:29.472Z | 234.246° WSW |
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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