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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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: 10 hours ago
TLE from 10 hours ago
0 FLOCK 4BE 9
1 60514U 24149AY 26131.96774772 .00011109 00000-0 28317-3 0 9994
2 60514 97.3789 215.9206 0004023 85.5943 274.5762 15.39701467 96741Epoch: 2026-05-11T23:13Z
TLE epoch observation values (Epoch: 2026-05-11T23:13:33.403Z)
Latitude
-0.00004°
Longitude
-2.21745°
Altitude
449.891 km
Speed
7.642 km/s
True Right ascension
14h 23m 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
17:16:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
446.674 km
Perigee altitude
441.185 km
Semi-major axis
6,822.067 km
Eccentricity
0.0004
Inclination
97.3789°
RAAN
215.9206°
Arg. of periapsis
85.5943°
True anomaly
274.53024°
Mean anomaly
274.5762°
Eccentric anomaly
274.55322°
Mean motion
3.85185 °/min
Orbital period
93.46 mins
BSTAR
0.00028317
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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 | 2026-05-12 18:30:13.330Z | 9.476° NNE | 2026-05-12 18:33:13.330Z | 210.663° SW | 42.266° | 2026-05-12 18:35:13.330Z | 196.365° SSW |
| 4 mins | 2026-05-13 05:01:13.330Z | 108.862° ESE | 2026-05-13 05:02:13.330Z | 83.563° E | 22.495° | 2026-05-13 05:05:13.330Z | 16.349° 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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