FLOCK 4BE 1, 60518
Orbit data source: Space-Track
FLOCK 4BE 1, 60518 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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60518 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: 8 hours ago
TLE from 8 hours ago
0 FLOCK 4BE 1
1 60518U 24149BC 25304.19821524 .00021447 00000-0 66691-3 0 9995
2 60518 97.3999 22.7155 0005050 46.4840 313.6822 15.33333152 67171Epoch: 2025-10-31T04:45Z
TLE epoch observation values (Epoch: 2025-10-31T04:45:25.796Z)
Latitude
0.00003°
Longitude
-88.38808°
Altitude
466.598 km
Speed
7.634 km/s
True Right ascension
01h 30m 51s
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
08:03:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
466.278 km
Perigee altitude
459.369 km
Semi-major axis
6,840.961 km
Eccentricity
0.00051
Inclination
97.3999°
RAAN
22.7155°
Arg. of periapsis
46.484°
True anomaly
313.64033°
Mean anomaly
313.6822°
Eccentric anomaly
313.66127°
Mean motion
3.8359 °/min
Orbital period
93.85 mins
BSTAR
0.00066691
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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 1 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 | 2025-10-31 17:50:45.763Z | 28.583° NE | 2025-10-31 17:53:45.763Z | 95.187° ESE | 32.703° | 2025-10-31 17:56:45.763Z | 167.928° S |
| 4 mins | 2025-11-01 05:57:45.763Z | 219.671° SW | 2025-11-01 05:58:45.763Z | 246.96° WSW | 26.244° | 2025-11-01 06:01:45.763Z | 321.894° NNW |
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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