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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 18
1 60480U 24149N 26259.05085580 .00032663 00000-0 69236-3 0 9992
2 60480 97.3676 343.8903 0002444 280.4365 79.6609 15.45013636116324Epoch: 2026-09-16T01:13Z
TLE epoch observation values (Epoch: 2026-09-16T01:13:13.941Z)
Latitude
0.00007°
Longitude
-29.4258°
Altitude
434.165 km
Speed
7.651 km/s
True Right ascension
22h 55m 33s
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
03:01:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.932 km
Perigee altitude
426.605 km
Semi-major axis
6,806.406 km
Eccentricity
0.00024
Inclination
97.3676°
RAAN
343.8903°
Arg. of periapsis
280.4365°
True anomaly
79.68845°
Mean anomaly
79.6609°
Eccentric anomaly
79.67468°
Mean motion
3.86515 °/min
Orbital period
93.14 mins
BSTAR
0.00069236
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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 | 2026-09-17 18:12:16.819Z | 38.743° NE | 2026-09-17 18:14:16.819Z | 91.398° ESE | 34.274° | 2026-09-17 18:17:16.819Z | 164.411° S |
| 6 mins | 2026-09-18 06:11:16.819Z | 191.051° SSW | 2026-09-18 06:14:16.819Z | 263.159° W | 39.149° | 2026-09-18 06:17:16.819Z | 331.87° NNW |
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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