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: 6 hours ago
TLE from 6 hours ago
0 FLOCK 4BE 24
1 60505U 24149AP 26260.54045886 .00036531 00000-0 72638-3 0 9999
2 60505 97.3658 346.2748 0002583 312.4699 47.6332 15.46864614116628Epoch: 2026-09-17T12:58Z
TLE epoch observation values (Epoch: 2026-09-17T12:58:15.645Z)
Latitude
-0.00004°
Longitude
155.23339°
Altitude
427.848 km
Speed
7.655 km/s
True Right ascension
23h 05m 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
12:13:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
424.59 km
Perigee altitude
421.076 km
Semi-major axis
6,800.97 km
Eccentricity
0.00026
Inclination
97.3658°
RAAN
346.2748°
Arg. of periapsis
312.4699°
True anomaly
47.65507°
Mean anomaly
47.6332°
Eccentric anomaly
47.64414°
Mean motion
3.86979 °/min
Orbital period
93.03 mins
BSTAR
0.00072638
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-18 06:11:36.919Z | 200.459° SSW | 2026-09-18 06:13:36.919Z | 289.653° WNW | 41.686° | 2026-09-18 06:15:36.919Z | 331.548° NNW |
| 4 mins | 2026-09-18 19:02:36.919Z | 341.466° N | 2026-09-18 19:03:36.919Z | 308.45° NW | 41.336° | 2026-09-18 19:06:36.919Z | 215.562° SW |
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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