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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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: 5 hours ago
TLE from 5 hours ago
0 FLOCK 4BE 18
1 60480U 24149N 25289.61282697 .00019754 00000-0 64717-3 0 9999
2 60480 97.3972 7.2412 0005241 59.8922 300.2839 15.31677303 64898Epoch: 2025-10-16T14:42Z
TLE epoch observation values (Epoch: 2025-10-16T14:42:28.250Z)
Latitude
0.00005°
Longitude
121.25344°
Altitude
472.105 km
Speed
7.631 km/s
True Right ascension
00h 28m 57s
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
14:42:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
471.345 km
Perigee altitude
464.17 km
Semi-major axis
6,845.895 km
Eccentricity
0.00052
Inclination
97.3972°
RAAN
7.2412°
Arg. of periapsis
59.8922°
True anomaly
300.23202°
Mean anomaly
300.2839°
Eccentric anomaly
300.25796°
Mean motion
3.83176 °/min
Orbital period
93.95 mins
BSTAR
0.00064717
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-17 04:57:09.394Z | 141.558° SSE | 2025-10-17 05:00:09.394Z | 62.147° ENE | 32.794° | 2025-10-17 05:03:09.394Z | 3.26° NNE |
| 5 mins | 2025-10-17 17:56:09.394Z | 28.105° NE | 2025-10-17 17:58:09.394Z | 88.013° E | 38.915° | 2025-10-17 18:01:09.394Z | 176.592° S |
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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