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: 1 day ago
TLE from 1 day ago
0 FLOCK 4BE 24
1 60505U 24149AP 26311.97926234 .00039915 00000-0 71454-3 0 9992
2 60505 97.3639 38.7036 0004276 119.6518 240.5160 15.49865422124586Epoch: 2026-11-07T23:30Z
TLE epoch observation values (Epoch: 2026-11-07T23:30:08.266Z)
Latitude
0.00003°
Longitude
-1.0076°
Altitude
421.683 km
Speed
7.657 km/s
True Right ascension
02h 34m 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
23:23:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
416.948 km
Perigee altitude
411.139 km
Semi-major axis
6,792.181 km
Eccentricity
0.00043
Inclination
97.3639°
RAAN
38.7036°
Arg. of periapsis
119.6518°
True anomaly
240.47336°
Mean anomaly
240.516°
Eccentric anomaly
240.49468°
Mean motion
3.8773 °/min
Orbital period
92.85 mins
BSTAR
0.00071454
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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 | 2026-11-09 06:38:11.069Z | 226.095° WSW | 2026-11-09 06:39:11.069Z | 251.494° W | 22.927° | 2026-11-09 06:42:11.069Z | 319.142° NNW |
| 4 mins | 2026-11-09 19:27:11.069Z | 330.538° NNW | 2026-11-09 19:29:11.069Z | 276.135° WNW | 23.458° | 2026-11-09 19:31:11.069Z | 235.116° WSW |
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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