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: 12 hours ago
TLE from 12 hours ago
0 FLOCK 4BE 14
1 60517U 24149BB 26171.47916215 .00013283 00000-0 32320-3 0 9991
2 60517 97.3691 255.2742 0003096 273.0986 86.9906 15.41076009102831Epoch: 2026-06-20T11:29Z
TLE epoch observation values (Epoch: 2026-06-20T11:29:59.609Z)
Latitude
-0.00008°
Longitude
174.08264°
Altitude
445.942 km
Speed
7.645 km/s
True Right ascension
17h 01m 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
10:18:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.979 km
Perigee altitude
437.758 km
Semi-major axis
6,818.006 km
Eccentricity
0.00031
Inclination
97.3691°
RAAN
255.2742°
Arg. of periapsis
273.0986°
True anomaly
87.02603°
Mean anomaly
86.9906°
Eccentric anomaly
87.00831°
Mean motion
3.85529 °/min
Orbital period
93.38 mins
BSTAR
0.0003232
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 04:47:33.664Z | 109.673° ESE | 2026-06-21 04:49:33.664Z | 72.214° E | 16.005° | 2026-06-21 04:51:33.664Z | 32.319° NE |
| 4 mins | 2026-06-21 06:20:33.664Z | 225.011° WSW | 2026-06-21 06:22:33.664Z | 276.322° WNW | 20.842° | 2026-06-21 06:24:33.664Z | 315.527° NNW |
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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