FLOCK 4BE 9, 60514
Orbit data source: Space-Track
FLOCK 4BE 9, 60514 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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60514 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: 18 hours ago
TLE from 18 hours ago
0 FLOCK 4BE 9
1 60514U 24149AY 25345.21793375 .00023423 00000-0 70594-3 0 9994
2 60514 97.3961 63.4179 0002302 237.3722 122.7299 15.34318156 73432Epoch: 2025-12-11T05:13Z
TLE epoch observation values (Epoch: 2025-12-11T05:13:49.475Z)
Latitude
-0.00005°
Longitude
-95.21531°
Altitude
466.908 km
Speed
7.632 km/s
True Right ascension
04h 13m 40s
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
22:04:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.467 km
Perigee altitude
458.319 km
Semi-major axis
6,838.03 km
Eccentricity
0.00023
Inclination
97.3961°
RAAN
63.4179°
Arg. of periapsis
237.3722°
True anomaly
122.75209°
Mean anomaly
122.7299°
Eccentric anomaly
122.74099°
Mean motion
3.83837 °/min
Orbital period
93.79 mins
BSTAR
0.00070594
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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 9 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 | 2025-12-12 04:51:26.127Z | 121.859° SE | 2025-12-12 04:53:26.127Z | 72.69° E | 25.264° | 2025-12-12 04:56:26.127Z | 11.664° NNE |
| 5 mins | 2025-12-12 17:48:26.127Z | 41.886° NE | 2025-12-12 17:50:26.127Z | 97.295° ESE | 29.458° | 2025-12-12 17:53:26.127Z | 163.988° 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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