FLOCK 4BE 26, 60484
Orbit data source: Space-Track
FLOCK 4BE 26, 60484 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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60484 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: 19 hours ago
TLE from 19 hours ago
0 FLOCK 4BE 26
1 60484U 24149S 25345.17451020 .00025124 00000-0 77164-3 0 9993
2 60484 97.3904 62.5593 0003360 189.2357 170.8824 15.33701239 73399Epoch: 2025-12-11T04:11Z
TLE epoch observation values (Epoch: 2025-12-11T04:11:17.681Z)
Latitude
-0.00005°
Longitude
-80.39863°
Altitude
470.161 km
Speed
7.63 km/s
True Right ascension
04h 10m 14s
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
22:04:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.026 km
Perigee altitude
459.43 km
Semi-major axis
6,839.865 km
Eccentricity
0.00034
Inclination
97.3904°
RAAN
62.5593°
Arg. of periapsis
189.2357°
True anomaly
170.8885°
Mean anomaly
170.8824°
Eccentric anomaly
170.88545°
Mean motion
3.83682 °/min
Orbital period
93.83 mins
BSTAR
0.00077164
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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 26 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 | 2025-12-12 05:21:46.658Z | 166.686° S | 2025-12-12 05:24:46.658Z | 162.382° S | 44.374° | 2025-12-12 05:27:46.658Z | 348.351° N |
| 5 mins | 2025-12-12 18:20:46.658Z | 1.124° NNE | 2025-12-12 18:22:46.658Z | 237.948° WSW | 41.673° | 2025-12-12 18:25:46.658Z | 200.026° SSW |
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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