FLOCK 4BE 16, 60483
Orbit data source: Space-Track
FLOCK 4BE 16, 60483 is a payload satellite owned by Planet (US) in SSO that was launched on Fri, 16 Aug 2024 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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60483 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5.7 kg wet, 5.7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.072 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 FLOCK 4BE 16
1 60483U 24149R 25312.64904378 .00103187 00000-0 30331-2 0 9997
2 60483 97.3966 30.4064 0003851 335.1620 24.9437 15.34691471 68427Epoch: 2025-11-08T15:34Z
TLE epoch observation values (Epoch: 2025-11-08T15:34:37.382Z)
Latitude
-0.00005°
Longitude
108.67502°
Altitude
462.559 km
Speed
7.637 km/s
True Right ascension
02h 01m 37s
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
15:27:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.416 km
Perigee altitude
456.15 km
Semi-major axis
6,836.92 km
Eccentricity
0.00039
Inclination
97.3966°
RAAN
30.4064°
Arg. of periapsis
335.162°
True anomaly
24.96232°
Mean anomaly
24.9437°
Eccentric anomaly
24.95301°
Mean motion
3.8393 °/min
Orbital period
93.77 mins
BSTAR
0.0030331
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.FLOCK 4BE 16 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-11 04:43:54.472Z | 128.101° SE | 2025-11-11 04:46:54.472Z | 65.727° ENE | 23.172° | 2025-11-11 04:48:54.472Z | 21.642° NNE |
| 4 mins | 2025-11-11 17:41:54.472Z | 56.611° ENE | 2025-11-11 17:42:54.472Z | 85.246° E | 26.566° | 2025-11-11 17:45:54.472Z | 157.771° S |
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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