FLOCK 4BE 14, 60517
Orbit data source: Space-Track
FLOCK 4BE 14, 60517 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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60517 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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4BE 14
1 60517U 24149BB 26069.16956317 .00019964 00000-0 54057-3 0 9993
2 60517 97.3736 152.2986 0003260 284.8429 75.2454 15.37705407 87097Epoch: 2026-03-10T04:04Z
TLE epoch observation values (Epoch: 2026-03-10T04:04:10.257Z)
Latitude
-0.00011°
Longitude
-76.59613°
Altitude
455.445 km
Speed
7.64 km/s
True Right ascension
10h 09m 11s
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
17:19:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452.063 km
Perigee altitude
447.611 km
Semi-major axis
6,827.974 km
Eccentricity
0.00033
Inclination
97.3736°
RAAN
152.2986°
Arg. of periapsis
284.8429°
True anomaly
75.28153°
Mean anomaly
75.2454°
Eccentric anomaly
75.26346°
Mean motion
3.84685 °/min
Orbital period
93.58 mins
BSTAR
0.00054057
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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 14 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 | 2026-03-10 18:41:18.077Z | 352.295° N | 2026-03-10 18:43:18.077Z | 303.411° NW | 33.91° | 2026-03-10 18:46:18.077Z | 216.211° SW |
| 5 mins | 2026-03-11 05:12:18.077Z | 137.497° SSE | 2026-03-11 05:14:18.077Z | 65.736° ENE | 35.29° | 2026-03-11 05:17:18.077Z | 1.402° NNE |
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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