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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Edit Public Description
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: 2 days ago
TLE from 2 days ago
0 FLOCK 4BE 14
1 60517U 24149BB 25312.81704250 .00026999 00000-0 84841-3 0 9992
2 60517 97.3919 30.6993 0004981 19.4720 340.6712 15.32951099 68476Epoch: 2025-11-08T19:36Z
TLE epoch observation values (Epoch: 2025-11-08T19:36:32.472Z)
Latitude
-0.00001°
Longitude
48.32279°
Altitude
466.903 km
Speed
7.635 km/s
True Right ascension
02h 02m 47s
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
15:27:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
467.369 km
Perigee altitude
460.553 km
Semi-major axis
6,842.098 km
Eccentricity
0.0005
Inclination
97.3919°
RAAN
30.6993°
Arg. of periapsis
19.472°
True anomaly
340.6523°
Mean anomaly
340.6712°
Eccentric anomaly
340.66175°
Mean motion
3.83495 °/min
Orbital period
93.87 mins
BSTAR
0.00084841
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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 | 2025-11-10 19:09:54.056Z | 328.826° NNW | 2025-11-10 19:11:54.056Z | 292.697° NW | 15.24° | 2025-11-10 19:13:54.056Z | 255.873° W |
| 5 mins | 2025-11-11 05:42:54.056Z | 199.148° SSW | 2025-11-11 05:44:54.056Z | 278.954° WNW | 35.125° | 2025-11-11 05:47:54.056Z | 335.586° NNW |
| 4 mins | 2025-11-11 18:40:54.056Z | 333.163° NNW | 2025-11-11 18:41:54.056Z | 302.758° NW | 29.871° | 2025-11-11 18:44:54.056Z | 223.34° 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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