FLOCK 4BE 18, 60480
Orbit data source: Space-Track
FLOCK 4BE 18, 60480 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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60480 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Planet
Mission
Partially 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: 7 hours ago
TLE from 7 hours ago
0 FLOCK 4BE 18
1 60480U 24149N 26221.78840929 .00013611 00000-0 30533-3 0 9997
2 60480 97.3711 306.1350 0004773 77.1253 283.0528 15.43508560110571Epoch: 2026-08-09T18:55Z
TLE epoch observation values (Epoch: 2026-08-09T18:55:18.562Z)
Latitude
-0.00002°
Longitude
64.02729°
Altitude
438.154 km
Speed
7.649 km/s
True Right ascension
20h 24m 32s
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
16:33:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
435.948 km
Perigee altitude
429.446 km
Semi-major axis
6,810.834 km
Eccentricity
0.00048
Inclination
97.3711°
RAAN
306.135°
Arg. of periapsis
77.1253°
True anomaly
282.99951°
Mean anomaly
283.0528°
Eccentric anomaly
283.02616°
Mean motion
3.86138 °/min
Orbital period
93.23 mins
BSTAR
0.00030533
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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 18 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 | 2026-08-10 05:56:28.108Z | 181.492° SSW | 2026-08-10 05:59:28.108Z | 292.614° NW | 38.617° | 2026-08-10 06:01:28.108Z | 336.244° NNW |
| 5 mins | 2026-08-10 18:49:28.108Z | 356.051° N | 2026-08-10 18:51:28.108Z | 295.954° NW | 38.081° | 2026-08-10 18:54:28.108Z | 209.087° SW |
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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