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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4BE 24
1 60505U 24149AP 26132.68089955 .00011653 00000-0 27773-3 0 9995
2 60505 97.3717 216.7021 0004560 71.1936 288.9805 15.41729198 96892Epoch: 2026-05-12T16:20Z
TLE epoch observation values (Epoch: 2026-05-12T16:20:29.721Z)
Latitude
-0.00003°
Longitude
101.12648°
Altitude
443.116 km
Speed
7.647 km/s
True Right ascension
14h 26m 48s
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
11:05:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.049 km
Perigee altitude
434.833 km
Semi-major axis
6,816.078 km
Eccentricity
0.00046
Inclination
97.3717°
RAAN
216.7021°
Arg. of periapsis
71.1936°
True anomaly
288.93108°
Mean anomaly
288.9805°
Eccentric anomaly
288.95579°
Mean motion
3.85693 °/min
Orbital period
93.34 mins
BSTAR
0.00027773
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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 | 2026-05-13 04:56:42.330Z | 122.117° SE | 2026-05-13 04:58:42.330Z | 84.329° E | 20.133° | 2026-05-13 05:01:42.330Z | 19.119° NNE |
| 4 mins | 2026-05-13 17:50:42.330Z | 53.777° ENE | 2026-05-13 17:52:42.330Z | 105.774° ESE | 22.039° | 2026-05-13 17:54:42.330Z | 148.037° SSE |
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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