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 26129.50050102 .00014909 00000-0 35553-3 0 9996
2 60505 97.3709 213.4897 0004783 79.9429 280.2357 15.41650476 96404Epoch: 2026-05-09T12:00Z
TLE epoch observation values (Epoch: 2026-05-09T12:00:43.288Z)
Latitude
-0.00004°
Longitude
165.9923°
Altitude
443.78 km
Speed
7.646 km/s
True Right ascension
14h 13m 57s
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
06:37:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.434 km
Perigee altitude
434.913 km
Semi-major axis
6,816.31 km
Eccentricity
0.00048
Inclination
97.3709°
RAAN
213.4897°
Arg. of periapsis
79.9429°
True anomaly
280.18176°
Mean anomaly
280.2357°
Eccentric anomaly
280.20873°
Mean motion
3.85673 °/min
Orbital period
93.34 mins
BSTAR
0.00035553
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-10 05:16:31.600Z | 145.531° SSE | 2026-05-10 05:19:31.600Z | 74.823° E | 33.869° | 2026-05-10 05:22:31.600Z | 3.149° NNE |
| 4 mins | 2026-05-10 18:11:31.600Z | 39.898° NE | 2026-05-10 18:12:31.600Z | 72.887° E | 35.068° | 2026-05-10 18:15:31.600Z | 172.257° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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