SPACEBEE-6, 43818 (Decayed)
Orbit data source: Space-Track
SPACEBEE-6, 43818 was a payload satellite owned by Swarm Tech (US) in LEO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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43818 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Swarm Tech
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.087 m
Radar Cross Section
0.017 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 years ago
TLE from 2 years ago
0 SPACEBEE-6
1 43818U 18099BN 25010.48851419 .16961137 26159-5 51406-3 0 9990
2 43818 97.4834 92.6686 0012345 275.1930 84.7963 16.44020427334894Epoch: 2025-01-10T11:43Z
TLE epoch observation values (Epoch: 2025-01-10T11:43:27.626Z)
Latitude
0.00007°
Longitude
166.55159°
Altitude
157.662 km
Speed
7.812 km/s
True Right ascension
06h 10m 40s
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
05:14:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
159.997 km
Perigee altitude
143.874 km
Semi-major axis
6,530.073 km
Eccentricity
0.00123
Inclination
97.4834°
RAAN
92.6686°
Arg. of periapsis
275.193°
True anomaly
84.9372°
Mean anomaly
84.7963°
Eccentric anomaly
84.86675°
Mean motion
4.11307 °/min
Orbital period
87.53 mins
BSTAR
0.00051406
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.SPACEBEE-6 Visibility
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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. |
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| This satellite is decayed. |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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