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
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AEROCUBE 6B
1 40046U 14033AN 25359.45988160 .00009321 00000-0 80717-3 0 9991
2 40046 97.7019 163.1817 0038420 228.4352 131.3574 14.96777298620742Epoch: 2025-12-25T11:02Z
TLE epoch observation values (Epoch: 2025-12-25T11:02:13.770Z)
Latitude
0.00002°
Longitude
-96.59029°
Altitude
597.629 km
Speed
7.551 km/s
True Right ascension
10h 52m 43s
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
12:29:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
600.581 km
Perigee altitude
547.162 km
Semi-major axis
6,952.008 km
Eccentricity
0.00384
Inclination
97.7019°
RAAN
163.1817°
Arg. of periapsis
228.4352°
True anomaly
131.68681°
Mean anomaly
131.3574°
Eccentric anomaly
131.52221°
Mean motion
3.74436 °/min
Orbital period
96.14 mins
BSTAR
0.00080717
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-26 22:55:47.852Z | 57.644° ENE | 2025-12-26 22:57:47.852Z | 88.488° E | 15.089° | 2025-12-26 22:59:47.852Z | 121.624° SE |
| 6 mins | 2025-12-27 00:30:47.852Z | 347.449° N | 2025-12-27 00:33:47.852Z | 274.442° WNW | 30.697° | 2025-12-27 00:36:47.852Z | 222.555° SW |
| 7 mins | 2025-12-27 11:17:47.852Z | 177.797° S | 2025-12-27 11:20:47.852Z | 245.968° WSW | 42.73° | 2025-12-27 11:24:47.852Z | 341.754° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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