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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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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4BE 18
1 60480U 24149N 26036.20221371 .00030075 00000-0 83445-3 0 9995
2 60480 97.3827 118.9726 0004360 22.7748 337.3689 15.36860389 82001Epoch: 2026-02-05T04:51Z
TLE epoch observation values (Epoch: 2026-02-05T04:51:11.264Z)
Latitude
-0.00002°
Longitude
-89.18216°
Altitude
455.764 km
Speed
7.641 km/s
True Right ascension
07h 55m 53s
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
16:57:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
455.321 km
Perigee altitude
449.364 km
Semi-major axis
6,830.48 km
Eccentricity
0.00044
Inclination
97.3827°
RAAN
118.9726°
Arg. of periapsis
22.7748°
True anomaly
337.34967°
Mean anomaly
337.3689°
Eccentric anomaly
337.35928°
Mean motion
3.84473 °/min
Orbital period
93.63 mins
BSTAR
0.00083445
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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 | 2026-02-05 17:55:30.795Z | 33.935° NE | 2026-02-05 17:57:30.795Z | 85.028° E | 32.98° | 2026-02-05 18:00:30.795Z | 167.974° S |
| 4 mins | 2026-02-06 05:59:30.795Z | 210.131° SW | 2026-02-06 06:01:30.795Z | 263.855° W | 26.849° | 2026-02-06 06:03:30.795Z | 315.904° 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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