SPACEBEE-143, 52394 (Decayed)
Orbit data source: Space-Track
SPACEBEE-143, 52394 was a payload satellite owned by Swarm Tech (US) in LEO that was launched on Mon, 02 May 2022 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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52394 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Swarm Tech
Mission
Decayed Commercial Communications
Bus & Motor
CUBESAT 0.25U, Unknown motor
Mass
0.284 kg wet, 0.284 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Ant, 0.5 m
Radar Cross Section
0.016 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 SPACEBEE-143
1 52394U 22047A 24121.05613099 .16628333 25733-5 29064-3 0 9992
2 52394 97.3659 216.4690 0016324 284.4454 75.5037 16.46554337112789Epoch: 2024-04-30T01:20Z
TLE epoch observation values (Epoch: 2024-04-30T01:20:49.717Z)
Latitude
-0.00006°
Longitude
-22.22379°
Altitude
149.035 km
Speed
7.818 km/s
True Right ascension
14h 25m 52s
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
13:25:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
155.871 km
Perigee altitude
134.574 km
Semi-major axis
6,523.359 km
Eccentricity
0.00163
Inclination
97.3659°
RAAN
216.469°
Arg. of periapsis
284.4454°
True anomaly
75.6849°
Mean anomaly
75.5037°
Eccentric anomaly
75.59429°
Mean motion
4.11942 °/min
Orbital period
87.39 mins
BSTAR
0.00029064
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Other satellites on launch #47 in the year 2022 (2022-05-02 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-143 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 ascending 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 ascending order |
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