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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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 1
1 60518U 24149BC 26173.50240155 .00013831 00000-0 31829-3 0 9993
2 60518 97.3776 258.6116 0002979 260.1342 99.9569 15.42746729103193Epoch: 2026-06-22T12:03Z
TLE epoch observation values (Epoch: 2026-06-22T12:03:27.493Z)
Latitude
-0.00008°
Longitude
167.05966°
Altitude
441.481 km
Speed
7.647 km/s
True Right ascension
17h 14m 26s
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
09:32:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
436.971 km
Perigee altitude
432.912 km
Semi-major axis
6,813.078 km
Eccentricity
0.0003
Inclination
97.3776°
RAAN
258.6116°
Arg. of periapsis
260.1342°
True anomaly
99.99052°
Mean anomaly
99.9569°
Eccentric anomaly
99.97371°
Mean motion
3.85947 °/min
Orbital period
93.28 mins
BSTAR
0.00031829
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-24 06:14:19.744Z | 222.979° SW | 2026-06-24 06:15:19.744Z | 257.846° W | 28.598° | 2026-06-24 06:18:19.744Z | 327.508° NNW |
| 4 mins | 2026-06-24 19:06:19.744Z | 339.498° N | 2026-06-24 19:08:19.744Z | 284.385° WNW | 26.771° | 2026-06-24 19:10:19.744Z | 233.128° WSW |
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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