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
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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 18
1 60480U 24149N 26173.53215365 .00013151 00000-0 31037-3 0 9995
2 60480 97.3724 257.3181 0003364 212.6358 147.4682 15.41999865103139Epoch: 2026-06-22T12:46Z
TLE epoch observation values (Epoch: 2026-06-22T12:46:18.075Z)
Latitude
0.00002°
Longitude
155.02606°
Altitude
445.263 km
Speed
7.644 km/s
True Right ascension
17h 09m 16s
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
10:52:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
439.435 km
Perigee altitude
434.85 km
Semi-major axis
6,815.28 km
Eccentricity
0.00034
Inclination
97.3724°
RAAN
257.3181°
Arg. of periapsis
212.6358°
True anomaly
147.48892°
Mean anomaly
147.4682°
Eccentric anomaly
147.47856°
Mean motion
3.8576 °/min
Orbital period
93.32 mins
BSTAR
0.00031037
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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 | 2026-06-24 05:23:57.489Z | 148.096° SSE | 2026-06-24 05:26:57.489Z | 43.636° NE | 35.78° | 2026-06-24 05:28:57.489Z | 2.513° NNE |
| 5 mins | 2026-06-24 18:17:57.489Z | 28.229° NE | 2026-06-24 18:19:57.489Z | 118.287° SE | 39.817° | 2026-06-24 18:22:57.489Z | 180.601° SSW |
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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