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: 18 hours ago
TLE from 18 hours ago
0 FLOCK 4BE 9
1 60514U 24149AY 26174.64910037 .00012935 00000-0 31605-3 0 9994
2 60514 97.3790 258.9836 0001644 249.6756 110.4314 15.40957098103318Epoch: 2026-06-23T15:34Z
TLE epoch observation values (Epoch: 2026-06-23T15:34:42.271Z)
Latitude
-0.00005°
Longitude
113.48984°
Altitude
446.795 km
Speed
7.644 km/s
True Right ascension
17h 15m 56s
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
20:48:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.341 km
Perigee altitude
439.099 km
Semi-major axis
6,818.357 km
Eccentricity
0.00016
Inclination
97.379°
RAAN
258.9836°
Arg. of periapsis
249.6756°
True anomaly
110.44905°
Mean anomaly
110.4314°
Eccentric anomaly
110.44023°
Mean motion
3.85499 °/min
Orbital period
93.39 mins
BSTAR
0.00031605
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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 | 2026-06-24 18:37:56.086Z | 6.181° NNE | 2026-06-24 18:40:56.086Z | 231.627° WSW | 41.401° | 2026-06-24 18:42:56.086Z | 201.204° SSW |
| 4 mins | 2026-06-25 05:07:56.086Z | 120.066° SE | 2026-06-25 05:09:56.086Z | 67.147° ENE | 24.693° | 2026-06-25 05:11:56.086Z | 19.952° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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