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: 9 hours ago
TLE from 9 hours ago
0 FLOCK 4BE 14
1 60517U 24149BB 25364.67432837 .00021275 00000-0 62752-3 0 9991
2 60517 97.3875 82.5912 0005588 167.9615 192.1763 15.35007570 76429Epoch: 2025-12-30T16:11Z
TLE epoch observation values (Epoch: 2025-12-30T16:11:01.971Z)
Latitude
0.00001°
Longitude
100.47877°
Altitude
467.746 km
Speed
7.63 km/s
True Right ascension
05h 30m 21s
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
01:16:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.663 km
Perigee altitude
454.023 km
Semi-major axis
6,835.98 km
Eccentricity
0.00056
Inclination
97.3875°
RAAN
82.5912°
Arg. of periapsis
167.9615°
True anomaly
192.1628°
Mean anomaly
192.1763°
Eccentric anomaly
192.16955°
Mean motion
3.8401 °/min
Orbital period
93.75 mins
BSTAR
0.00062752
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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 | 2025-12-31 04:50:14.363Z | 129.474° SE | 2025-12-31 04:53:14.363Z | 62.586° ENE | 24.658° | 2025-12-31 04:55:14.363Z | 18.903° NNE |
| 4 mins | 2025-12-31 17:48:14.363Z | 53.715° ENE | 2025-12-31 17:49:14.363Z | 83.525° E | 28.123° | 2025-12-31 17:52:14.363Z | 160.371° S |
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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