FLOCK 4BE 24, 60505
Orbit data source: Space-Track
FLOCK 4BE 24, 60505 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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60505 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: 2 days ago
TLE from 2 days ago
0 FLOCK 4BE 24
1 60505U 24149AP 26235.68709572 .00019023 00000-0 39811-3 0 9998
2 60505 97.3685 321.0249 0004347 60.6542 299.5141 15.45492144112787Epoch: 2026-08-23T16:29Z
TLE epoch observation values (Epoch: 2026-08-23T16:29:25.070Z)
Latitude
0.00002°
Longitude
101.69086°
Altitude
431.601 km
Speed
7.653 km/s
True Right ascension
21h 24m 05s
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
00:22:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.821 km
Perigee altitude
423.905 km
Semi-major axis
6,805 km
Eccentricity
0.00043
Inclination
97.3685°
RAAN
321.0249°
Arg. of periapsis
60.6542°
True anomaly
299.47074°
Mean anomaly
299.5141°
Eccentric anomaly
299.49242°
Mean motion
3.86635 °/min
Orbital period
93.11 mins
BSTAR
0.00039811
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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 24 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 | 2026-08-25 18:46:17.707Z | 5.55° NNE | 2026-08-25 18:49:17.707Z | 235.394° WSW | 40.98° | 2026-08-25 18:51:17.707Z | 202.15° 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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